USCG MH-65E Helicopter Flight Manual (CGTO 1H-65E-1) PDF

1H-65E-1SS-1 CGTO 1H-65E-1SS-1 SAFETY SUPPLEMENT FLIGHT MANUAL U.S. COAST GUARD SERIES MH–65E AIRCRAFT INTERACTION BETWEEN FLIGHT DIRECTOR MODES WHILE IN A HOVER AND AUTOMATED TRANSITIONS OF FLIGHT PLAN SEQUENCING THIS PUBLICATION SUPPLEMENTS CGTO 1H-65E-1, DATED 07 JULY 2020. COMMANDING OFFICERS ARE RESPONSIBLE FOR BRINGING THIS SUPPLEMENT TO THE ATTENTION OF ALL AFFECTED COAST GUARD PERSONNEL. PUBLISHED BY THE DIRECTION OF THE COMMANDANT, U.S. COAST GUARD. Distribution Statement D: Distribution is authorized to the DHS/CG/DoD and their contractors for Administrative or Operational use, 12 March 2021. Other requests shall be referred to Commanding Officer, CG Aviation Training Center, MH-65 Training Division, 8501 Tanner Williams Road, Mobile, AL 36608-9682. WARNING: This document contains technical data whose export is restricted by the Arms Export-Control Act (Title 22, U.S.C., Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DESTRUCTION NOTICE: For classified documents, follow procedures in DoD 5220.22-M, National Industrial Security Program Operating Manual, Section 5-705, or DoD 5200.1-R, Information Security Program Regulation, Chapter VI, Section 7. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. 12 March 2021 TITLE: INTERACTION BETWEEN FLIGHT DIRECTOR MODES WHILE IN A HOVER AND AUTOMATED TRANSITIONS OF FLIGHT PLAN SEQUENCING 1. PURPOSE To provide MH-65E flight crews safety of flight information when manipulating the flight plan while simultaneously using Flight Director (FD) flight plan (FPLN) mode, transition to hover (THOV) lateral mode, or hover (HOV) mode. 1 1H-65E-1SS-1 2. GENERAL The MH-65E FD and Civil Flight Manager Systems (FMS) include automated interactions to reduce workload for pilots during various approach profiles. However, in certain circumstances manipulating the CDU FPLN may trigger this automated interaction, creating an undesired transition from a hover to forward flight. This safety supplement highlights these issues and provides guidance on flight plan manipulation, automated sequencing, and FD use during critical phases of flight. 3. INSTRUCTIONS CGTO 1H-65E-1SS-1 will be inserted in the front of the Flight Manual and will remain there until a design change is integrated, information contained therein is incorporated in the manual, or rescinded. FD AUTOMATION AND FLIGHT PLAN SEQUENCING Flight plan leg types (CRZ, HOV, LND, STP, etc) carry specific sequencing mode attributes. The FMS flight plan sequencing mode will change from AUTO to MANUAL when certain leg types become active and MANUAL back to AUTO as a result of pilot input to the CDU FPLN. This can be viewed on the CDU FPLN page. The three common scenarios where the FMS will automatically change the flight plan sequence mode from AUTO to MANUAL are: When an Approach (APR) leg type generated for a Missed Approach Point (MAP) associated with an instrument approach procedure (any Civil approach from the navigation database or Tactical approach) becomes active. This scenario can be associated with an area navigation or conventional approach (FPLN/VNV mode, ILS mode or VOR/TACAN mode using VSPD). When a HOVER AT fix (HOV leg type) associated with a CATCH procedure becomes active. When a pilot created Land (LND), Hover (HOV), or Stop (STP) leg type becomes active. The three common scenarios where the FMS flight plan sequence mode transitions from MANUAL to AUTO are: When a pilot manually switches the flight plan sequence mode from MANUAL to AUTO. When a pilot performs a direct-to function to a Cruise (CRZ), Circle (CIR), Pattern (PTN), Discontinuity (Disco), Hold (HLD) leg type. When a pilot deletes an active LND, HOV, STP, or APR leg type. 2. 1H-65E-1SS-1 Automated FD mode engagement will occur if a LND, HOV, STP, or APR leg is active, FPLN, THOV lateral, or HOV lateral modes are captured/engaged, ACP is the source on the side with FLT XFER, and the pilot sequences the flight plan from MANUAL to AUTO as described in the three scenarios above. The FD will automatically activate FPLN mode lateral, FBALT/FRALT, and FASPD/FGSPD to execute the altitude, speed, and heading data contained in the next flight plan leg. The intent of this automation is to reduce pilot workload when transitioning on missed approaches or manipulating the flight plan to continue on a mission. This automation may result in an undesired climb away from the water/ground, acceleration, and turn to achieve the new leg altitude, speed, and course. At speeds below 40 KIAS, the climb rate will be limited to +/- 225 FPM. At speeds above 40 KIAS, the climb rate will be limited by the CDU FD SELECT VSPEED value. If the course for the next leg is different from the hover heading, a turn will occur almost immediately. The turn may happen at a low speed without regard to wind direction. If a source other than ACP (i.e. VOR/ILS or TCN) is selected on the side with FLT XFER and the flight plan is sequenced by pilot manipulation from a LND, HOV, STP, or APR leg, then BALT/RALT and ASPD/GSPD will engage and capture current aircraft altitude and speed. To prevent an automated transition from THOV or HOV, the THOV or HOV lateral modes need to first be deselected before editing an active LND, HOV, STP, or APR leg in the flight plan. This can be accomplished by selecting another mode (HAUG, RALT, BALT) or by deselecting all modes. The active LND, HOV, STP, or APR leg can then be removed from the flight plan by executing a direct-to a future leg, deleting the leg, or by changing the sequencing mode from MANUAL back to AUTO. THOV can then be re-selected to engage HOV, and the active FPP can be manipulated without risk of the FD commanding an automated transition from the hover. 3 U.S. Department o Commandant 2703 Martin Luther King Jr Ave SE Homeland Security United States Coast Guard Washington DC. 20593-7331...,.,, Phone: (202) 372-2225 ·t-\11. - Fax: (202) 372-8338 United States Coast Guard 3710 JL'L C 7 2020 From: Reply to CG-7112 Attn of: LCDR J. D. Slapak To: Distribution Subj: FLIGHT MANUAL, USCG MH-65E HELICOPTER (CGTO 1H-65E-1) 1. PURPOSE. This memorandum promulgates the USCG Series MH-65E Flight Manual CGTO 1H-65E-1, Emergency Procedures (Red Book) CGTO 1H-65E- l -CL1, Normal Procedures (Blue Book) CGTO 1H-65E-1-CL2, MH-65E Fan-Fold Checklist CGTO 1H-65E-1-CL3, Ship-Helo Checklist CGTO 1H-65E-1-CL4, and the Rescue Checklist CGTO 1H-65E-1-CL5. 2. ACTION. The MH-65E Flight Manual will be promulgated electronically. Commanding Officers shall ensure compliance with this Flight Manual and are authorized to remove traditional hard copies from all aircraft in accordance with COMDTINST M3710 (series). 3. DIRECTIVES AFFECTED. None. 4. DISCUSSION. The MH-65E Flight Manual is a new operators manual to the MH-65 platform. This manual is the culmination of the collaborative work of ATC Mobile, ALC-SRR, CG-711, CG-9315 and industry human performance experts. This manual incorporates changes for the Common Avionics Architecture System, updates to the Automatic Flight Control System, GPS capability, radar, and other systems. This manual provides critical updates to Normal Procedures, Emergency Procedures, and aircraft limitations. 5. CHANGES. Recommendations for changes and improvements to this manual shall be submitted via the chain of command using the MH-65E Flight Manual Recommendation for Change of Publication, Form CG-847. This manual will be reviewed on a regular basis. # Enclosure: (1) MH-65E Flight Manual, COTO 1H-65E-1 (2) MH-65E Emergency Procedures (Red Book), COTO 1H-65E-1-CL1 (3) MH-65E Normal Procedures (Blue Book), COTO 1H-65E-1-CL2 (4) MH-65E Tri-Fold Checklist, CGTO 1H-65E-1-CL3 (5) MH-65E Ship-Helo Checklist, CGTO 1H-65E-1-CL4 (6) MH-65E Rescue Checklist, CGTO 1H-65E-1-CL5 Dist: All operators of the MH-65E This page intentionally left blank. CGTO 1H-65E-1 FLIGHT MANUAL U.S. COAST GUARD SERIES MH-65E HELICOPTER COMMANDING OFFICERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL AFFECTED PERSONNEL. PUBLISHED BY DIRECTION OF THE COMMANDANT OF THE U.S. COAST GUARD Distribution Statement D: Distribution authorized to the DHS/CG/DoD and their contractors for Administrative or Operational use, 7 July 2020. Other requests shall be referred to USCG MH-65E Training Division, 8501 Tanner Williams Road, Mobile, AL 36608-9682. WARNING: This document contains technical data whose export is restricted by the Arms Export-Control Act (Title 22, U.S.C., Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C. App 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DESTRUCTION NOTICE: For classified documents, follow the procedures in DoD 5220.22-M, National Indus- trial Security Program Operating Manual, Section 5-705 or DoD 5200.1-R, Information Security Program Reg- ulation, Chapter VI, Section 7. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. 7 July 2020 This page intentionally left blank. CGTO 1H-65E-1 Dates of issue for original and changed pages are: Original 0................................................................................................................... 7 July 2020 Total number of pages in this publication is 695, consisting of the following: Page No. Change No.* Title.............................................................................................................................. 0 blank............................................................................................................................ 0 A – B............................................................................................................................ 0 i/(ii blank)..................................................................................................................... 0 iii – ix/(x blank)............................................................................................................. 0 xi – xxix/(xxx blank)...................................................................................................... 0 1-A-1 – 1-A-3/(1-A-4 blank)......................................................................................... 0 1-A-5 – 1-A-96............................................................................................................. 0 1-B-1/(1-B-2 blank)...................................................................................................... 0 1-B-3 – 1-B-40............................................................................................................. 0 1-C-1/(1-C-2 blank)...................................................................................................... 0 1-C-3 – 1-C-22............................................................................................................. 0 1-D-1/(1-D-2 blank)...................................................................................................... 0 1-D-3 – 1-D-44............................................................................................................. 0 1-E-1/(1-E-2 blank)...................................................................................................... 0 1-E-3 – 1-E-18............................................................................................................. 0 2-A-1 – 2-A-66............................................................................................................. 0 2-B-1 – 2-B-52............................................................................................................. 0 2-C-1/(2-C-2 blank)...................................................................................................... 0 2-C-3 – 2-C-19/(2C-20 blank)...................................................................................... 0 3-1 – 3-7/(3-8 blank).................................................................................................... 0 3-9 – 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blank)........................................................................................ 0 3-115/(3-116 blank)..................................................................................................... 0 3-117 – 3-148.............................................................................................................. 0 4-1/(4-2 blank)............................................................................................................ 0 4-3 – 4-8...................................................................................................................... 0 5-1/(5-2 blank)............................................................................................................ 0 5-3 – 5-20.................................................................................................................... 0 6-1/(6-2 blank)............................................................................................................. 0 6-3 – 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FP-7/(FP-8 blank)........................................................................................................ 0 A CGTO 1H-65E -1 Page No. Change No.* FP-9/(FP-10 blank)...................................................................................................... 0 FP-11/(FP-12 blank).................................................................................................... 0 FP-13/(FP-14 blank).................................................................................................... 0 FP-15/(FP-16 blank).................................................................................................... 0 FP-17/(FP-18 blank).................................................................................................... 0 FP-19/(FP-20 blank).................................................................................................... 0 FP-21/(FP-22 blank).................................................................................................... 0 FP-23/(FP-24 blank).................................................................................................... 0 FP-25/(FP-26 blank).................................................................................................... 0 FP-27/(FP-28 blank).................................................................................................... 0 FP-29/(FP-30 blank).................................................................................................... 0 FP-31/(FP-32 blank).................................................................................................... 0 FP-33........................................................................................................................... 0 *ZERO IN CHANGE NO. COLUMN INDICATES AN ORIGINAL PAGE. UPON RECEIPT OF THE FIRST AND SUBSEQUENT CHANGES TO THIS TECHNICAL ORDER, PERSONNEL RESPONSIBLE FOR MAINTAINING THIS PUBLICATION IN CURRENT STATUS WILL ASCERTAIN THAT ALL CHANGES HAVE BEEN RECEIVED AND INCORPORATED. ACTION SHOULD BE TAKEN PROMPTLY IF THE PUBLICATION IS INCOMPLETE. B CGTO 1H-65E-1 OPERATIONAL SUPPLEMENT SUMMARY Operational Supplements are sequentially numbered, CGTO 1H-65E-1S-1, -2, etc. The supplements you receive should follow in sequence. If you are missing a supplement, ask your Publication Distribution Officer for the supple- ment you need. OPERATIONAL SUPPLEMENTS REPLACED BY THIS CHANGE OR RESCINDED Number Date Short Title Disposition ACTIVE OPERATIONAL SUPPLEMENTS As you receive additional supplements, add them to this list. Supplements outstanding when this page was prepared are listed below. Number Date Short Title CGTO 1H-65E-1 INTERIM CHANGE SUMMARY Essential and urgent changes to this technical manual may be issued by an interim change. These changes shall be distributed on a nonscheduled, as needed basis to disseminate important information at the earliest possible date. Periodically all interim changes will be considered to become a permanent part of the basic manual and will be incorporated in a formal, printed change or reissue. INTERIM CHANGES REPLACED BY THIS CHANGE OR RESCINDED Number Date Short Title Disposition ACTIVE INTERIM CHANGES As you receive additional interim changes, add them below and file a copy in the front of the manual. Interim changes outstanding when this page was prepared are listed below. Number Date Short Title CGTO 1H-65E-1 SAFETY SUPPLEMENT SUMMARY Safety Supplements are sequentially numbered, CGTO 1H-65E-1SS-1, -2, etc. The supplements you receive should follow in sequence. If you are missing a supplement, ask your Publication Distribution Officer for the supplement you need. SAFETY SUPPLEMENTS REPLACED BY THIS CHANGE OR RESCINDED Number Date Short Title Disposition ACTIVE SAFETY SUPPLEMENTS As you receive additional supplements, add them to this list. Supplements outstanding when this page was prepared are listed below. Number Date Short Title This page intentionally left blank. CGTO 1H-65E-1 RECORD OF CHANGES Change No. Regular or Interim Date of Change By Whom Entered Date Entered Original Regular 7 July 2020 This page intentionally left blank. CGTO 1H-65E-1 TABLE OF CONTENTS PAGE SECTION I SYSTEM DESCRIPTION............................................................................... 1-A-1 PART A AIRFRAME, POWERPLANT, AND SYSTEMS......................... 1-A-1 PART B AVIONICS ARCHITECTURE/NAVIGATION............................. 1-B-1 PART C COMMUNICATION/NAVIGATION/IFF SYSTEMS.................... 1-C-1 PART D SENSOR SYSTEMS................................................................. 1-D-1 PART E MISSION EQUIPMENT............................................................ 1-E-1 SECTION II NORMAL PROCEDURES.............................................................................. 2-A-1 PART A NORMAL PROCEDURES........................................................ 2-A-1 PART B OPERATIONAL PROCEDURES.............................................. 2-B-1 PART C SPECIAL PROCEDURES........................................................ 2-C-1 SECTION III EMERGENCY OPERATING PROCEDURES................................................ 3-1 SECTION IV CREW DUTIES.............................................................................................. 4-1 SECTION V OPERATING LIMITATIONS............................................................................ 5-1 SECTION VI FLIGHT CHARACTERISTICS........................................................................ 6-1 SECTION VII ADVERSE WEATHER OPERATIONS........................................................... 7-1 SECTION VIII PERFORMANCE DATA CHARTS.................................................................. 8-1 INDEX........................................................................................................................ Index-1 FOLDOUTS........................................................................................................................ FP-1 i/(ii blank) This page intentionally left blank. CGTO 1H-65E-1 LIST OF FIGURES Figure Page 1-A-1. Dimensions................................................................................................................ 1-A-6 1-A-2. Turning Radius and Ground Clearance Diagram....................................................... 1-A-7 1-A-3. Danger Areas............................................................................................................. 1-A-8 1-A-4. Emergency Flotation System..................................................................................... 1-A-11 1-A-5. Flotation Gear Controls.............................................................................................. 1-A-12 1-A-6. Emergency Locator Transmitter................................................................................. 1-A-13 1-A-7. Turbomeca Arriel 2C2-CG Engine............................................................................. 1-A-14 1-A-8. Engine Fuel System................................................................................................... 1-A-16 1-A-9. Overhead Quadrant................................................................................................... 1-A-17 1-A-10. Engine Oil System..................................................................................................... 1-A-19 1-A-11. Engine Indication and Crew Alerting System Data Display....................................... 1-A-21 1-A-12. Engine Data Display.................................................................................................. 1-A-22 1-A-13. Engine Out Indication................................................................................................ 1-A-22 1-A-14. Full Authority Digital Engine Control System............................................................. 1-A-27 1-A-15. OEI GOV.................................................................................................................... 1-A-28 1-A-16. PFD Torque Tape One Engine Inoperative Mode Selected Hi, Lo, or Continuous Indicator Examples.................................................................................................... 1-A-29 1-A-17. Usage Flag Symbology 30-Second Torque............................................................... 1-A-29 1-A-18. Usage Flag Symbology 2-Minute Torque................................................................... 1-A-30 1-A-19. Engine No. 1 - One Engine Inoperative Training Mode Display................................ 1-A-30 1-A-20. Training Switch.......................................................................................................... 1-A-31 1-A-21. Engine Ratings.......................................................................................................... 1-A-31 1-A-22. Hover Increased Power Search and Rescue Mission Usage Flag Symbology......... 1-A-32 1-A-23. Engine Fire Warning and Extinguisher Controls........................................................ 1-A-33 1-A-24. Main Rotor Head........................................................................................................ 1-A-35 1-A-25. Main Rotor Blade....................................................................................................... 1-A-36 1-A-26. Tail Rotor System....................................................................................................... 1-A-37 1-A-27. Transmission System................................................................................................. 1-A-38 1-A-28. Main Gearbox Lubrication System............................................................................. 1-A-40 1-A-29. Main Gear Box Indications and Warning Messages Display Examples.................... 1-A-41 1-A-30. Fuel Management Panel and Fuel Quantity Indicator............................................... 1-A-45 1-A-31. Fuel Quantity and Tank Arrangement........................................................................ 1-A-46 1-A-32. Fuel Cell Location and Feeder Tank Assembly......................................................... 1-A-47 1-A-33. Primary and Secondary Hydraulic System................................................................ 1-A-58 1-A-34. Hydraulic System Components................................................................................. 1-A-61 1-A-35. Landing Gear Hydraulic System................................................................................ 1-A-62 1-A-36. Nose Landing Gear Locking Mechanism (Locked Position)...................................... 1-A-63 1-A-37. Landing Gear Control and Indicators......................................................................... 1-A-66 iii CGTO 1H-65E-1 Figure Page 1-A-38. Wheel Brake System................................................................................................. 1-A-67 1-A-39. Main Rotor Flight Control System.............................................................................. 1-A-69 1-A-40. Tail Rotor Control....................................................................................................... 1-A-70 1-A-41. Collective and Cyclic Grips........................................................................................ 1-A-71 1-A-42. Air Data System Diagram.......................................................................................... 1-A-74 1-A-43. Automatic Flight Control System Control Panel and Indications............................... 1-A-76 1-A-44. Environmental Control System Controls and Indications........................................... 1-A-84 1-A-45. Windshield Wiper and Anti-Ice System...................................................................... 1-A-88 1-A-46. Lighting System Controls........................................................................................... 1-A-90 1-A-47. Airframe Lighting System........................................................................................... 1-A-91 1-A-48. Rescue Hoist............................................................................................................. 1-A-93 1-A-49. Rescue Hoist Controls............................................................................................... 1-A-94 1-A-50. Cargo Hook................................................................................................................ 1-A-96 1-B-1. Common Avionics Architecture System Block Diagram............................................ 1-B-3 1-B-2. Cockpit Multifunction Displays................................................................................... 1-B-4 1-B-3. Multifunction Display Controls................................................................................... 1-B-4 1-B-4. Common Avionics Architecture System Control Panel.............................................. 1-B-8 1-B-5. EGI (H764GU)........................................................................................................... 1-B-11 1-B-6. EGI and Associated Equipment Data Flow Diagram................................................. 1-B-12 1-B-7. Magnetic Field Unsuitablity........................................................................................ 1-B-14 1-B-8. Display Unit System Block Diagram.......................................................................... 1-B-15 1-B-9. Display Layout........................................................................................................... 1-B-15 1-B-10. Attitude Display.......................................................................................................... 1-B-16 1-B-11. Excessive Pitch Up and Pitch Down Indications........................................................ 1-B-16 1-B-12. Attitude Fail Display................................................................................................... 1-B-16 1-B-13. Standard Alignment Message.................................................................................... 1-B-17 1-B-14. In-Motion Alignment Message................................................................................... 1-B-17 1-B-15. Alignment Cancelled Message.................................................................................. 1-B-17 1-B-16. Degraded Attitude Annunciation................................................................................ 1-B-18 1-B-17. Bank Scale Display.................................................................................................... 1-B-18 1-B-18. Airspeed Display........................................................................................................ 1-B-19 1-B-19. Airspeed Color Band.................................................................................................. 1-B-19 1-B-20. High Speed Awareness Operating Modes and Caution Airspeed Operating Mode.. 1-B-19 1-B-21. Airspeed Failure Display............................................................................................ 1-B-19 1-B-22. Altitude Display.......................................................................................................... 1-B-20 1-B-23. Altitude Fail Display................................................................................................... 1-B-20 1-B-24. Heading Display......................................................................................................... 1-B-20 1-B-25. Invalid Heading Display............................................................................................. 1-B-21 1-B-26. DG Annunciation........................................................................................................ 1-B-21 iv CGTO 1H-65E-1 Figure Page 1-B-27. Both Primary Attitude Data Not Available or Invalid.................................................. 1-B-21 1-B-28. Both Primary Heading Data Not Available or Invalid................................................. 1-B-22 1-B-29. SFI Block Diagram..................................................................................................... 1-B-23 1-B-30. Miscompare Annunciation........................................................................................ 1-B-25 1-B-31. DG Mode – Selected EGI for Miscompare............................................................... 1-B-25 1-B-32. DG Mode – Selected EGI Invalid for Miscompare..................................................... 1-B-26 1-B-33. Display Control Keys................................................................................................. 1-B-26 1-B-34. Flight Menu................................................................................................................ 1-B-26 1-B-35. Flight Menu Sequence - HDG Mode: MAG............................................................... 1-B-27 1-B-36. Flight Menu Sequence - HDG Mode: DG.................................................................. 1-B-28 1-B-37. Flight Menu - DG Slew Heading................................................................................ 1-B-28 1-B-38. Flight Menu - MAG VAR............................................................................................ 1-B-28 1-B-39. Flight Menu - HDG Mode.......................................................................................... 1-B-28 1-B-40. Flight Menu - HDG Mode Sequence after DG Selection........................................... 1-B-29 1-B-41. Flight Menu - HDG Miscompare................................................................................ 1-B-29 1-B-42. Flight Menu - HDG Miscompare Invalid Option......................................................... 1-B-29 1-B-43. Flight Menu - Display Brightness............................................................................... 1-B-29 1-B-44. Flight Menu - Alignment............................................................................................. 1-B-30 1-B-45. Flight Menu - Alignment Options............................................................................... 1-B-30 1-B-46. Flight Menu - Alignment Confirm............................................................................... 1-B-30 1-B-47. Flight Menu - Alignment Invalid Option...................................................................... 1-B-30 1-B-48. Flight Menu - Barometric Setting............................................................................... 1-B-30 1-B-49. Flight Menu - Display Metric...................................................................................... 1-B-31 1-B-50. Flight Menu - Keypad Brightness............................................................................... 1-B-31 1-B-51. Flight Menu - VS Mode.............................................................................................. 1-B-31 1-B-52. Identification Friend or Foe/Communication/Emergency Locator Transmitter Control Panel............................................................................................................. 1-B-35 1-B-53. Crypto Appliqué (KIV-77).......................................................................................... 1-B-36 1-C-1. Communications System Control (Sheet 1 of 2)........................................................ 1-C-4 1-C-1. Communications System Control (Sheet 2 of 2)........................................................ 1-C-5 1-C-2. Interface Control Unit Inputs/Outputs........................................................................ 1-C-6 1-C-3. Low Profile Control Audio Panel................................................................................ 1-C-7 1-C-4. Frequency Bands - AN/ARC-210.............................................................................. 1-C-12 1-C-5. Avionics Data Fill Panel............................................................................................. 1-C-16 1-C-6. Control Head (KY-100).............................................................................................. 1-C-18 1-C-7. Liquid Crystal Display (KY-100)................................................................................ 1-C-19 1-C-8. Data and Voice Privacy-200 Control Head................................................................ 1-C-20 1-C-9. Data Storage Unit...................................................................................................... 1-C-22 1-D-1. Radar Display Features............................................................................................. 1-D-4 v CGTO 1H-65E-1 Figure Page 1-D-2. Controller (WC-700).................................................................................................. 1-D-4 1-D-3. Rain Echo Attenuation Compensation Technique Mode........................................... 1-D-5 1-D-4. Radar Test Pattern..................................................................................................... 1-D-8 1-D-5. Radar Status Displayed on Primary Flight Display.................................................... 1-D-9 1-D-6. Electro-Optical Infrared Sensor System Subsystems................................................ 1-D-11 1-D-7. Forward Looking Infrared Laser Anti-Ice Control Panel............................................. 1-D-12 1-D-8. EO/IR LASER RNG POSN........................................................................................ 1-D-13 1-D-9. EO/IR LSR POSN page............................................................................................. 1-D-13 1-D-10. Multifunction Display.................................................................................................. 1-D-14 1-D-11. Display Unit Controls and Indicators.......................................................................... 1-D-16 1-D-12. Joystick Control Unit.................................................................................................. 1-D-17 1-D-13. Display Information.................................................................................................... 1-D-26 1-D-14. Display Symbology Level Options............................................................................. 1-D-27 1-D-15. Removable Memory Module, Mission Data Recorder, and Hoist Camera................ 1-D-29 1-D-16. Traffic Alert and Collision Avoidance System Relative Bearing Accuracy................. 1-D-31 1-D-17. Traffic Alert and Collision Avoidance System Display............................................... 1-D-33 1-D-18. Traffic Alert and Collision Avoidance System Status Page........................................ 1-D-36 1-D-19. Traffic Alert and Collision Avoidance System Surveillance Airspace......................... 1-D-38 1-D-20. Heads Up Display Master Mode Symbology............................................................. 1-D-41 1-E-1. Rescue Basket........................................................................................................... 1-E-7 1-E-2. Folding Rescue Litter................................................................................................. 1-E-8 1-E-3. Hoist Quick Splice...................................................................................................... 1-E-13 1-E-4. Self-Locating Datum Marker Buoy Packaged View................................................... 1-E-14 1-E-5. Self-Locating Datum Marker Buoy Deployed View.................................................... 1-E-15 1-E-6. USB Utility Panel...................................................................................................... 1-E-18 2-A-1. Technical Data List 1/2 Page.................................................................................... 2-A-13 2-A-2. Helipad Marking Example.......................................................................................... 2-A-52 2-A-3. Daytime Convective (Valley Winds)........................................................................... 2-A-56 2-A-4. Mechanical Turbulence.............................................................................................. 2-A-56 2-A-5. Wind Zones Around an Obstacle............................................................................... 2-A-57 2-A-6. Wind Zones Around Multiple Obstacles..................................................................... 2-A-57 2-A-7. Demarcation Lines and Low Pressure Areas............................................................ 2-A-58 2-A-8. Conditions Conducive to Vortex Ring State............................................................... 2-A-58 2-B-1. Correct Interconnect of Weight Bag Snap Hook to the Trail Line Eye Splice............ 2-B-19 2-B-2. Wave Type Examples................................................................................................ 2-B-31 2-B-3. Plunging Breaker....................................................................................................... 2-B-32 2-B-4. Spilling Breaker......................................................................................................... 2-B-32 2-B-5. Surging Breaker......................................................................................................... 2-B-33 2-B-6. Quick Splice............................................................................................................... 2-B-42 vi CGTO 1H-65E-1 Figure Page 2-B-7. Launch Container with Warning Sticker..................................................................... 2-B-47 2-B-8. Launch Container with Draped Chute........................................................................ 2-B-47 2-C-1. Refuel Operations C-130 to MH-65........................................................................... 2-C-8 2-C-2. TCAS Control Page................................................................................................... 2-C-14 3-1. Main Gearbox Overtorque......................................................................................... 3-12 3-2. Emergency Exits........................................................................................................ 3-109 3-3. Emergency Equipment.............................................................................................. 3-110 3-4. Cockpit Avionics Panel.............................................................................................. 3-137 3-5. Pilot Forward Panel................................................................................................... 3-138 3-6. Pilot Aft Panel............................................................................................................ 3-139 3-7. Copilot Panel............................................................................................................. 3-140 3-8. Avionics Rack Panel.................................................................................................. 3-141 3-9. Miscellaneous Circuit Panels..................................................................................... 3-142 5-1. Airspeed Display........................................................................................................ 5-5 5-2. Hovering Flight Wind Envelope................................................................................. 5-6 5-3. Center of Gravity Chart Example............................................................................... 5-8 5-4. Main Gearbox - Pressure and Temperature Limits.................................................... 5-9 5-5. Torque Limits............................................................................................................. 5-9 5-6. Rotor Engagement/Disengagement Wind Limits....................................................... 5-10 5-7. Rotor Engagement Wind Envelope with START R.BK Switch................................... 5-11 5-8. Triple Tach Display - Main Rotor Speed Limits.......................................................... 5-12 5-9. Engine Instrument Crew Alerting System Display - Engine Limits............................ 5-13 5-10. Triple Tach Display - Free Turbine Speed Limits....................................................... 5-14 5-11. One Engine Inoperative Mode Selected Hi, Lo, or Continuous Indicator Examples.. 5-14 5-12. Hover Increased Power Search and Rescue Mission Operations............................. 5-15 5-13. Example of Warnings and Cautions Critical to Engine Start...................................... 5-15 5-14. Technical Data List 1/2 page All Items Present......................................................... 5-16 5-15. Technical Data List 2/2 page..................................................................................... 5-16 5-16. Climatic Engine Starting and Relighting Envelope Limitations Chart........................ 5-17 5-17. Fuel System Limits.................................................................................................... 5-18 5-18. Hydraulic Limits......................................................................................................... 5-18 6-1. Conditions Conducive to Vortex Ring State............................................................... 6-6 6-2. Aerodynamic Factors Affecting Aircraft Yaw Control in the MH-65........................... 6-9 6-3. Low Airspeed Pedal Workload Critical Azimuth in the MH-65................................... 6-10 8-1. Pressure Altitude/Density Altitude Chart.................................................................... 8-8 8-2. Maximum Hovering Weight, In Ground Effect............................................................ 8-10 8-3. Maximum Hovering Weight, Out of Ground Effect..................................................... 8-11 8-4. Indicated Torque Required to Hover, In Ground Effect.............................................. 8-12 8-5. Indicated Torque Required to Hover, Out of Ground Effect....................................... 8-13 vii CGTO 1H-65E-1 Figure Page 8-6. Performance in Hover Out of Ground Effect.............................................................. 8-14 8-7. Transfer Scale........................................................................................................... 8-15 8-8. Weight Index.............................................................................................................. 8-16 8-9. One Engine Inoperative Rate-of-Climb...................................................................... 8-17 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 1 of 17)...... 8-18 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 2 of 17)...... 8-19 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 3 of 17)...... 8-20 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 4 of 17)...... 8-21 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 5 of 17)...... 8-22 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 6 of 17)...... 8-23 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 7 of 17)...... 8-24 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 8 of 17)...... 8-25 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 9 of 17)...... 8-26 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 10 of 17).... 8-27 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 11 of 17).... 8-28 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 12 of 17).... 8-29 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 13 of 17).... 8-30 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 14 of 17).... 8-31 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 15 of 17).... 8-32 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 16 of 17).... 8-33 8-10. Level Flight All Engines Operating and One Engine Inoperative (Sheet 17 of 17).... 8-34 8-11. Never Exceed Speed................................................................................................. 8-35 8-12. Height Loss After Engine Failures in Hover Out of Ground Effect............................. 8-36 8-13. Height/Velocity Diagram (Sheet 1 of 3)...................................................................... 8-37 8-13. Height/Velocity Diagram (Sheet 2 of 3)...................................................................... 8-38 8-13. Height/Velocity Diagram (Sheet 3 of 3)...................................................................... 8-39 8-14. Performance in Hover Out of Ground Effect with One Engine at 30-Second One Engine Inoperative Rating with Wind Effect............................................................... 8-40 8-15. True Airspeed - Calibrated Airspeed Correspondence Chart.................................... 8-41 8-16. Hover Flight Side and Tail Wind Envelope................................................................. 8-42 8-17. Distance Required to Clear a 50-ft Obstacle at Twin-Engine Takeoff........................ 8-43 8-18. Distance Required for Landing After Clearing a 50-ft Obstacle................................. 8-44 8-19. Service Ceiling in Forward Flight with Both Engines at Maximum Continuous Power Rating........................................................................................................................ 8-45 8-20. Service Ceiling in Forward Flight with One Engine Inoperative at 2-Minute Rating.. 8-46 8-21. Service Ceiling in Forward Flight with One Engine Inoperative Continuous Rating.. 8-47 8-22. Maximum Weight to Maintain Level Flight After Flyaway.......................................... 8-48 8-23. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 30-second Rating (Sheet 1 of 3)................................................................................ 8-49 viii CGTO 1H-65E-1 Figure Page 8-23. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 30-second Rating (Sheet 2 of 3)................................................................................ 8-50 8-23. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 30-second Rating (Sheet 3 of 3)................................................................................ 8-51 8-24. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 2-Minute Rating (Sheet 1 of 3)................................................................................... 8-52 8-24. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 2-Minute Rating (Sheet 2 of 3)................................................................................... 8-53 8-24. Minimum Airspeed Permitting Climb at 100 foot/minute at One Engine Inoperative 2-Minute Rating (Sheet 3 of 3)................................................................................... 8-54 8-25. Twin-Engine Rate-of-Climb........................................................................................ 8-55 8-26. Maximum Takeoff Weights Permitting Climb at 150 foot/minute 1,000 foot Above Ground with One Engine Inoperative......................................................................... 8-56 8-27. Performances in Hover OGE with One Engine at 2-Minute OEI Rating with (Head) Wind Effect................................................................................................................ 8-57 8-28. Performance in Hover IGE with One Engine at 30-Second OEI Rating.................... 8-58 8-29. Performance in Hover IGE with One Engine 2-Minute OEI Rating............................ 8-59 8-30. Torque Available - All Engines Operating: Maximum Takeoff Power......................... 8-60 8-31. Torque Available - One Engine Inoperative: HI......................................................... 8-61 8-32. Torque Available - One Engine Inoperative: Lo......................................................... 8-62 8-33. Torque Available - One Engine Inoperative: Continuous........................................... 8-63 FO-1. General Arrangement Diagram Left........................................................................... FP-1 FO-2. General Arrangement Diagram Right........................................................................ FP-3 FO-3. Cockpit Arrangement Diagram.................................................................................. FP-5 FO-4. Cockpit Instruments and Controls.............................................................................. FP-7 FO-6. Fuel Supply System................................................................................................... FP-9 FO-7. Direct Current Electrical System................................................................................ FP-11 FO-7. Direct Current Electrical System................................................................................ FP-13 FO-8. Alternating Current Electrical System........................................................................ FP-15 FO-9. Automatic Flight Control System Block Diagram....................................................... FP-17 FO-10. Common Avionics Architecture System Block Diagram............................................ FP-19 FO-11. Coast Guard Rescue Swimmer Deployment Hand Signals (Sheet 1 of 4)................ FP-21 FO-11. Coast Guard Rescue Swimmer Deployment Hand Signals (Sheet 2 of 4)................ FP-23 FO-11. Coast Guard Rescue Swimmer Deployment Hand Signals (Sheet 3 of 4)................ FP-25 FO-11. Coast Guard Rescue Swimmer Deployment Hand Signals (Sheet 4 of 4)................ FP-27 FO-12. Coast Guard Boat Crew Hand Signals...................................................................... FP-29 FO-13. Ship/Helicopter Hand Signals (Sheet 1 of 2)............................................................. FP-31 FO-13. Ship/Helicopter Hand Signals (Sheet 2 of 2)............................................................. FP-33 ix/(x blank) This page intentionally left blank. CGTO 1H-65E-1 LIST OF TABLES Table Page 1-A-1. Authorized Engine Lubricants.................................................................................... 1-A-20 1-A-2. Authorized Gearbox Lubricants................................................................................. 1-A-42 1-A-3. Authorized Normal Fuels........................................................................................... 1-A-48 1-A-4. Authorized Alternative Fuels...................................................................................... 1-A-49 1-A-5. Electric Control Panel Indicators and Functions........................................................ 1-A-54 1-A-6. Hydraulic Isolation Valve Position Matrix................................................................... 1-A-60 1-A-7. WOW Switch Functions............................................................................................. 1-A-64 1-A-8. WOW System Component Airborne and On Ground................................................ 1-A-64 1-A-9. AFCS and FD Caution Indications............................................................................. 1-A-77 1-A-10. Advisory Indications................................................................................................... 1-A-77 1-B-1. Common Avionics Architecture System Control Panel Functions............................. 1-B-8 1-B-2. Tactical Air Navigation Modes of Operation............................................................... 1-B-33 1-B-3. Identification Friend or Foe Operational Modes......................................................... 1-B-34 1-B-4. Identification Friend or Foe Control Panel Functions................................................. 1-B-36 1-B-5. The APX-119 and KIV-77 Controls and Functions.................................................... 1-B-37 1-C-1. Communication Radios.............................................................................................. 1-C-3 1-C-2. Operational Modes and Features - AN/ARC-210..................................................... 1-C-12 1-C-3. COMM2 RT-5000 Module Frequencies and Modulation Type.................................. 1-C-13 1-C-4. COMM3 Search and Rescue RT-5000 Module Frequencies and Modulation Type. 1-C-14 1-C-5. Avionics Data Fill Panel Load Select - Type III Operation......................................... 1-C-17 1-C-6. Avionics Data Fill Panel Load Select - Type I Operation........................................... 1-C-17 1-C-7. Control Head (KY-100) Operating Controls, Indicators, and Connectors.................. 1-C-18 1-C-8. Liquid Crystal Display (KY-100) Annunciators and Display Fields............................ 1-C-20 1-C-9. Data and Voice Privacy-200 Value Pushbutton Function.......................................... 1-C-21 1-D-1. Primus 700 Functions Table...................................................................................... 1-D-6 1-D-2. Display Levels Related to Video Integrated Processor Levels.................................. 1-D-6 1-D-3. Turbulence Level Related to NASA Levels................................................................ 1-D-7 1-D-4. Target Alert Depth and Range Characteristics.......................................................... 1-D-9 1-D-5. Display Levels Related to VIP Levels........................................................................ 1-D-10 1-D-6. ESS MFD Only Modes............................................................................................... 1-D-15 1-D-7. ESS EICAS Advisories.............................................................................................. 1-D-16 1-D-8. Joystick Control Unit Controls and Functions............................................................ 1-D-18 1-D-9. Tracker Mode Performance Summary....................................................................... 1-D-24 1-D-10. Traffic Alert And Collision Avoidance System Traffic Display Symbology................. 1-D-32 1-D-11. Display Control and Indicator Functions.................................................................... 1-D-34 1-D-12. TCAS Modes............................................................................................................. 1-D-35 1-E-1. Tactical and Beacon Scan Status.............................................................................. 1-E-3 1-E-2. Search and Rescue Scan Status............................................................................... 1-E-4 xi CGTO 1H-65E-1 Table Page 2-A-1. Cautions and Advisories that Limit Global Positioning System/Required Navigation Performance Operation............................................................................................. 2-A-41 2-A-2. External Load Operations - Command/Advisory Reports.......................................... 2-A-65 2-B-1. Hoist Commands....................................................................................................... 2-B-38 2-B-2. Hoist Advisory Reports.............................................................................................. 2-B-38 2-B-3. Rescue Swimmer Commands and Advisory Reports................................................ 2-B-40 3-1. Warning, Caution, and Advisory Indication Examples............................................... 3-7 3-2. EICAS Indications...................................................................................................... 3-54 3-3. MFD STAT Page Indications...................................................................................... 3-54 3-4. Warning, Caution, and Advisory Indication Examples............................................... 3-117 3-5. Warning Indications................................................................................................... 3-117 3-6. Caution Indications.................................................................................................... 3-120 3-7. Advisory Indications................................................................................................... 3-126 3-8. Circuit Breaker Locations........................................................................................... 3-143 4-1. Automated Flight Duties............................................................................................ 4-7 4-2. Manual Flight Duties.................................................................................................. 4-8 5-1. Aural Warnings.......................................................................................................... 5-3 5-2. Torque Limits............................................................................................................. 5-10 5-3. One Engine Inoperative Limits................................................................................... 5-14 5-4. Technical Data List 2/2 Page Main Rotor Speed Digital Readout and Color............. 5-16 5-5. Flight Director System Limitations............................................................................. 5-19 8-1. Pressure Altitude Conversion Chart.......................................................................... 8-7 8-2. Temperature Conversion Chart.................................................................................. 8-9 8-3. Kilograms/Pounds Conversion Chart......................................................................... 8-64 8-4. Takeoff and Destination Data Card............................................................................ 8-65 xii CGTO 1H-65E-1 FOREWORD SCOPE This manual contains the necessary information for safe and efficient operation of your aircraft. These in- structions provide you with a general knowledge of the aircraft and its characteristics and specific normal and emergency operating procedures. Your experience is recognized; therefore, basic flight principles are avoided. PERMISSIBLE OPERATIONS Unusual operations or configurations are prohibited unless specifically covered herein. Procedures pre- scribed in this manual are mandatory but it is expected that they will be executed with sound professional judgment. Nothing in this manual shall be construed to relieve personnel of responsibility for using initiative in prosecuting a mission or taking such emergency action as the situation warrants. ARRANGEMENT The manual is divided into eight sections, a glossary, an index, and foldout illustrations. SAFETY SUPPLEMENTS Information involving safety will be promptly forwarded to you in a safety supplement. Urgent information is published in interim safety supplements and transmitted by message. Formal supplements are mailed or sent out electronically. The supplement title block and status page (published with formal supplements only) should be checked to determine the effect of the supplement on the manual and other outstanding supplements. OPERATIONAL SUPPLEMENTS Information involving changes to operating procedures will be forwarded to you by operational supplements. The procedure for handling operational supplements is the same as for safety supplements. CHECKLISTS The flight manual contains itemized procedures with necessary amplifications. The checklist contains item- ized procedures without the amplification. Primary line items in the flight manual and checklists are identical. If a formal safety or operational supplement effects your checklist, the affected checklist page will be issued as soon as possible incorporating the new supplement. DISTRIBUTIONS AND CHANGES All aircraft flight manuals, sub-manuals, and checklists (red book, blue book, tri-fold, and fanfold) are main- tained and accessed electronically via the Electronic Flight Bag (EFB) and the Aviation Technical Information Portal (ATIP) thru CG-LIMS via http://osc-s-lim-ap100.osc.uscg.mil:7108/ATIP/ATIP//. Safety supplements, operational supplements, and changes will be provided on a per copy basis to all holders through normal channels. xiii CGTO 1H-65E-1 WARNINGS, CAUTIONS, AND NOTES The following definitions apply to warnings, cautions, and notes found throughout the manual. WARNING Operating procedures, techniques, etc., which could result in personal in- jury or loss of life if not carefully followed. CAUTION Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed. NOTE An operating procedure, technique, etc., which is considered essential to emphasize. Warnings, cautions, and notes may contain more than one paragraph. When this occurs, each paragraph will be prefaced with the bullet ( ) symbol. USE OF WORDS SHALL, WILL, SHOULD, AND MAY The words shall or will are to be used to indicate a mandatory requirement. The word should is to be used to indicate a nonmandatory desired or preferred method of accomplishment. The word may is used to indicate an acceptable or suggested means of accomplishment. YOUR RESPONSIBILITY − TO LET US KNOW Every effort is made to keep the flight manual correct. Review conferences with operating personnel, and a constant review of accident and flight test reports assure inclusion of the latest data in the manual. However, we cannot correct an error unless we know of its existence. In this regard, it is essential that you do your part. Comments, corrections, and questions regarding this manual or any phase of the operation of this aircraft are welcomed. These should be forwarded on Form CG-847 (https://cg.portal.uscg.mil/units/atc/Publica- tions/default.aspx) through your Standardization Officer to: Commanding Officer USCG Aviation Training Center 8501 Tanner Williams Rd. Mobile, AL 36608 ATTN: MH-65E Training Division xiv CGTO 1H-65E-1 xv CGTO 1H-65E-1 xvi CGTO 1H-65E-1 ABBREVIATIONS AND ACRONYMS The following abbreviations and acronyms are used throughout this manual and associated checklist: A/C Aircraft AAR Air-to-Air Receive AASE Advanced Aircraft Survivability Equipment AATR Air-to-Air Transmit/Receive AC Alternating Current or Aircraft Commander ACK Acknowledgement ACP Air Control Point ACU Alternator Control Unit ADC Air Data Computer AEO All Engines Operating AES Advanced Encryption Standard AFB Air Force Base AFCS Automatic Flight Control System AGL Above Ground Level AHRS Attitude and Heading Referencing System ALC Aviation Logistics Center ALE Automatic Link Establishment ALMIS Aviation Logistics Management Information System ALTNR Alternator AM Amplitude Modulation AM-CW Amplitude Modulation-Continuous Wave AME Amplitude Modulation Equivalent AMS Avionics Management System ANC Active Noise Cancellation ANDVT Advanced Narrowband Digital Voice Terminal ANT Antenna APPR Approach ARINC Aeronautical Radio Incorporated ASL Avionics System Local Area Network ASM Aviation Special Missions ASPD Airspeed xvii CGTO 1H-65E-1 ASU Aerosonic Sensing Unit ATC Air Traffic Control ATT Attitude AUF Airborne Use of Force AWL Above Water Level AZ Azimuth BA Basic Aircrew BALT or BARALT Barometric Altitude BARO Barometric BATT Battery BATT RLY Battery Relay BC Back Course BIM Engine Interface Unit BIT Built-in-Test BITF Built-in-Test Failure BKLT Backlight BKP or BU Backup BLOS Beyond-Line-of-Sight BTC Bus Tie Contactor C/B Circuit Breaker CAAS Common Avionics Architecture System CAL Calibration CASP Common Advanced System Processor CAWS Central Aural Warning System CBIT Continuous Built-in-Test CCD Charged Coupled Device CCI Controlled Cryptographic Item CCP CAAS Control Panel CD Counter Drug CDU Control Display Unit CEP Communications Ear Piece CEU Control Electronics Unit CF Compact Flash CG Center of Gravity or Coast Guard xviii CGTO 1H-65E-1 CH Channel CIK Crypto Ignition Key CLR Clear CM1 COMM1 (ARC-210) CM2 COMM2 (RT-5000) CM3 COMM3 (RT-5000 SAR) CNI Communications/Navigation/IFF CNTL or CONT Control COMM Communication COMSEC Communication Security CON Contrast CP or CPLT Copilot CR Clutter Reduction CRM Crew Resource Management CRT Cathode Ray Tube C-S COSPAS-SARSAT C-SYNC Collective Synchronization CT Cipher Text CTDB Centroid Black Tracking Mode DA Decision Altitude or Density Altitude DAFIF Digital Aeronautical Flight Information File DAMA Demand Assigned Multiple Access dB Decibel DBCU Data Bus Converter Unit DC Direct Current DCU Data Concentrator Unit DECU Digital Engine Control Unit DES Data Encryption Standard DF Direction Finder or Direction Finding DG Directional Gyro DH Decision Height DIGIMAP Digital Map DIS or DSPL Display DIW Dead in the Water xix CGTO 1H-65E-1 DMB Datum Marker Buoy DoD Department of Defense DP Display Processor DSC Digital Selective Calling DSU Data Storage Unit DTD Data Transfer Device DTU Data Transfer Unit DU Display Unit DVP Digital Voice Privacy EB Emergency Backup EBCAU Emergency Backup Control Auxiliary Unit ECMS Engine Condition Monitoring System ECS Environmental Control System EFSL Emergency Fuel Shutoff Lever EGI Embedded Global Positioning System/Inertial Navigation System EGR Embedded GPS Receiver EICAS Engine Indication and Crew Alerting System EIU Engine Interface Unit EL Elevation ELT Emergency Locator Transmitter EMCCD Electron Multiplying Charge Coupled Device EMCON Emmisions Control EMER or EMERG Emergency EMI Electromagnetic Interference EMT Emergency Medical Technician EO/IR Electro-Optical Infrared EOS Electro-Optical Sensor EOT Engine Oil Temperature EPU Estimated Position Uncertainty (GPS) ESS Electro-Optical Infared Sensor System ETL Effective Transitional Lift EXT External FADEC Full Authority Digital Engine Controller FAR Federal Aviation Regulations xx CGTO 1H-65E-1 FAT Forward Avionics Tower FCS FADEC Control Switch FD Flight Director FDE Fault Detection and Exclusion FDS Flight Director System FFD Foundation Feature Data FLAC FLIR Laser Anti-Ice Control FLIR Forward Looking Infrared FLT Flight FLT XFER Flight Transfer FM Flight Mechanic or Frequency Modulation FMS Flight Management System FMT Frequency Managed Training FOD Foreign Object Debris/Damage FORM Formation FOV Field of View FP Summ Flight Plan Summary FPLN Flight Plan fpm Feet per Minute FWD Forward GA Go-Around GCU Generator Control Unit GEN Generator GMT Greenwich Mean Time GNSS Global Navigation Satellite Systems GPM Gallons Per Minute GPNT Geopointing GPPU General Purpose Processing Unit GPS Global Positioning System GS Glideslope or Groundspeed GSPD Groundspeed H or HI High HAT Height Above Touchdown HAVS Helicopter Airborne Video System xxi CGTO 1H-65E-1 HDG Heading HDG SEL Heading Select HDU Helmet Display Unit HF High Frequency or ARC-220 Radio HF-ALE High Frequency Automatic Link Establishment HIDS Helicopter Integrated Data Storage HIFR Helicopter Inflight Refueling HIPSARM Hover Increased Power Search and Rescue Mission HOGE Hover Out of Ground Effect HSD Hoist Static Discharge or Horizontal Situation Display HUD Heads Up Display HYD Hydraulic HUD Heads Up Display I/O Input/Output IAP Instrument Approach Procedure IAS Indicated Airspeed IBC Instrument Landing System Back Course IBIT Initiated Built-in-Test ICOM Internal Intercommunication ICS Intercommunication System ICU Interface Control Unit IE Inertial Electronics IFF Identification Friend or Foe IGE In Ground Effect IIMC Inadvertent Instrument Meteorological Conditions ILS Instrument Landing System IM-ALIGN In-Motion Alignment IMC Instrument Meteorological Conditions IMU Inertial Management Unit in/hr Inches Per Hour INAV Integrated Navigation INIT Initiate INS Inertial Navigation System INU Inertial Navigation Unit xxii CGTO 1H-65E-1 IR Infrared ISA Inertial Sensor Assembly ITO Instrument Takeoff JAIC Joint Avionics Interface Card JCU Joystick Control Unit KGS Knots Groundspeed kHz Kilohertz KIAS Knots Indicated Airspeed kt Knots L Left LAT Latitude LCD Liquid Crystal Display LE Law Enforcement LED Light Emitting Diode LKD Locked LLB Local Loopback LO Low LOC Localizer LONG Longitude LOS Line-of-Sight LPCAP Low Profile Control Audio Panel LRF Laser Rangefinder LRU Line Replaceable Unit LSB Lower Side Band LSK Line Select Key LSO Landing Signal Officer LTS Lights M Menu M1 Module 1 (RT-5000 main transceiver) M2 Module 2 (RT-5000 VHF transceiver) M3 Module 3 (RT-5000 UHF transceiver) MAAF Mishap Analysis Animation Facility MADPU Military Aviation Double Pickup MAG Magnetic xxiii CGTO 1H-65E-1 MAN Manual MAP Missed Approach Point MB Marker Beacon MC Miscompare MDA Minimum Descent Altitude MDR Mission Data Recorder MEDEVAC Medical Evacuation MFD Multifunction Display MGB Main Gearbox MGP Multigraphic Processor MGW Maximum Gross Weight MHz Megahertz MIC Microphone MIN Minimum mm/hr Milimeters per Hour MLEVEL Manual Level MMS Master Mode Symbology MON Monitor MPC Maintenance Procedure Card MPEG-4 Motion Pictures Expert Group-4 MSL Mean Sea Level MSU Magnetic Sensing Unit MTM Multitrack Mode MTOP Maximum Takeoff Power MWOD Multiple Word of the Day N1 Gas Generator Turbine Speed N2 Free Power Turbine Speed NAR Nonaltitude Reporting NASA National Aeronautics and Space Administration NAV Navigation NAVAID Navigational Aid NAVDB Navigation Database NB Narrowband NLOS Nonline-of-Sight xxiv CGTO 1H-65E-1 NM Nautical Mile NOAA National Oceanic and Atmospheric Administration NOE Nap-of-the-Earth NOTAM Notice to Airmen NORM Normal NR Main Rotor Speed NUC Nonuniformity Correction NVG Night Vision Goggle OASIS Original Aerosonic Standby Instrument System OAT Outside Air Temperature ODK Operator Display Keyboard OEI One Engine Inoperative/Inoperable OEI GOV One Engine Inoperable with Governed Fuel Flow OFL Offline OFP Operational Flight Planning ORM Operational Risk Management OTAR Over-the-Air Rekeying OTH Over-the-Horizon P or PLT Pilot PA Pressure Altitude PAX Passenger PBIT Power-on Built-in-Test PDU Pilot Display Unit PERF Performance PF Pilot Flying PFD Primary Flight Display PIC Pilot in Command PIP Picture-in-Picture PIW Person in the Water PK Public Key PM Pilot Monitoring PM-A Precision Marksman-Aviation PNL Panel POS Position xxv CGTO 1H-65E-1 PRI Primary PSCU Power Supply and Calibration Unit psi Pounds per Square Inch PSM Processor Switch Module PT Plain Text PTT Push-to-Test or Push-to-Talk PVT Private PWR Power QT Total Torque R Right R/T or RT Receiver/Transmitter RADALT Radar Altimeter RAIM Receiver Autonomous Integrity Monitoring RALT Radar Altitude RCU Remote Control Unit RDR Radar REACT Rain Echo Attenuation Compensation Technique REM or RMT Remote REV Reversionary RF Radio Frequency RHIB Rigid Hull Inflatable Boat RLG Ring Laser Gyro RMM Removable Memory Module RNAV Area Navigation RNG Range RNP Required Navigation Performance ROC Roll Offset Compensation RPM Revolutions Per Minute RPU Receiver Processor Unit RS Rescue Swimmer RTN Return RWAI Rotary-Wing Air Intercept RX Receive SA/AS Selective Availability/Antispoof xxvi CGTO 1H-65E-1 SADPU Sling Augmented Double Pickup SAR Search and Rescue SAROPS Search and Rescue Optimal Planning System SATCOM Satellite Communications SDC Signal Data Converter SDR Signal Driver Board SE Single-Engine SEC Secondary SFI Standby Flight Instrument SHP Shaft Horsepower SINCGARS Single-Channel Ground and Airborne Radio System SKL Simple Key Loader SLDMB Self-Locating Datum Marker Buoy SNSR Sensor SOV Shutoff Valve STAT Status STBY Standby SYNC Synchronous T Temperature or True T/R Transformer Rectifier TA Traffic Alert TAC Tactical TACAN or TCN Tactical Air Navigation TAS True Airspeed TCAS Traffic Alert and Collision Avoidance System TDL Technical Data List TDZE Touchdown Zone Elevation TGB Tail Gearbox TGT Target T-HOV or T-HV Transition-to-Hover THZE Threshold Zone Elevation TOD Time-of-Day TODD Takeoff and Destination Data Card TOI Target-of-Interest xxvii CGTO 1H-65E-1 TOT Turbine Outlet Temperature TR Transmit/Receive TR/G Transmit/Receive/Guard TRB Turbulence TRK Track TRNG Training TRQ or TQ Torque TSA Transportation Security Administration TSK Transmission Security Key TSU Turret Sensor Unit TTP Tatics, Techniques, and Procedures TX Transmit UAB Underwater Acoustic Beacon UHF Ultra High Frequency ULY Uncommanded Left Yaw USB Universal Serial Bus USCG United States Coast Guard UTC Universal Time Coordinated VAC Volts Alternating Current VAR Variance VDC Volts Direct Current VFDR Voice and Flight Data Recorder VHF Very High Frequency VIP Video Integrated Processor or Very Important Person VMC Visual Meteorological Conditions VNE Never Exceed Speed VOL Volume VOR VHF Omnidirectional Range VOR/ILS VHF Omnidirectional Range/Instrument Landing System VORTAC VHF Omnidirectional Range with TACAN VOX Voice Operated Transmitter VPM Video Processing Module VPS Video Processing System VS or VSPD Vertical Speed xxviii CGTO 1H-65E-1 VSI Vertical Speed Indicator VX Best Angle of Climb Speed VY Optimal Climb Speed W/S Windshield WB Wideband WFOV Wide Field of View WOW Weight-on-Wheels WTA Wind and Terrain Analysis WX Weather WXR Weather Radar XFER Transfer XMT or XMIT Transmit ZER Zeroize xxix/(xxx blank) This page intentionally left blank. CGTO 1H-65E-1 SECTION I SYSTEM DESCRIPTION PART A - AIRFRAME, POWERPLANT, AND SYSTEMS TABLE OF CONTENTS THE HELICOPTER.................................................................................................................. 1-A-5 CABIN INTERIOR ARRANGEMENT....................................................................................... 1-A-8 Pilot, Copilot, and Flight Mechanic Seats............................................................................. 1-A-8 Safety Belts.......................................................................................................................... 1-A-9 Rescue Swimmer Seat......................................................................................................... 1-A-9 Safety Harness (Gunner's Belt)............................................................................................ 1-A-9 Cargo................................................................................................................................... 1-A-9 DOORS.................................................................................................................................... 1-A-10 Cockpit Doors....................................................................................................................... 1-A-10 Passenger Doors................................................................................................................. 1-A-10 Baggage Compartment Door............................................................................................... 1-A-10 Hoist Operator Hatch........................................................................................................... 1-A-10 EMERGENCY EQUIPMENT.................................................................................................... 1-A-11 Emergency Flotation System............................................................................................... 1-A-11 Portable Fire Extinguisher......

USCG MH-65E Helicopter Flight Manual (CGTO 1H-65E-1) PDF

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