TM-1-1520-240-BD Army CH-47D Heilcopter (NSN 1520年01月08日8-3869) (EIC:RCD) Manual

CHAPTER 1 GENERAL INFORMATION AND ASSESSMENT
1-5. QUALITY ASSURANCE AND QUALITY CONTROL
Figure 1-1. DA Form 2408-13
Figure 1-2. DA Form 2408-13-1
Figure 1-3. DA Form 2408-13-2
Figure 1-4. DA Form 2408-13-3
Figure 1-5. DA Form 2408-18
Figure 1-6. DA Form 2408-14-1 (Sheet 1 of 2)
Figure 1-6. DA Form 2408-14-1 (Sheet 2 of 2)
SECTION II. BATTLE-DAMAGE ASSESSMENT CONCEPTS
SECTION III. COMBAT THREATS
Figure 1-8. Fragmentation Patterns Associated with a Typical HEI Projectile
SECTION IV. BATTLE-DAMAGE ASSESSMENT
Figure 1-9. Damage Assessment Markings (Sheet 1 of 3)
Figure 1-9. Damage Assessment Markings (Sheet 2 of 3)
Figure 1-9. Damage Assessment Markings (Sheet 3 of 3)
Figure 1-10. General Assessment (Sheet 1 of 7)
Figure 1-10. General Assessment (Sheet 2 of 7)
Figure 1-10. General Assessment (Sheet 3 of 7)
Figure 1-10. General Assessment (Sheet 4 of 7)
Figure 1-10. General Assessment (Sheet 5 of 7)
Figure 1-10. General Assessment (Sheet 6 of 7)
Figure 1-10. General Assessment (Sheet 7 of 7)
Table 1-1. Ballistic Damage Modes
Ballistic Damage Modes (Continued)
CHAPTER 2 AIRFRAME
Figure 2-1. Basic Structure
Figure 2-2. Inboard Profile
Figure 2-3. General Arrangement
a. Initial Assessment
Table 2-1. Structure Damage Assessment Procedures
(3) Inspecting for Structural Changes
Figure 2-4. DA Form 2404
Figure 2-5. Measuring Cap or Longeron Damage
Figure 2-6. Damaged Cross Section
Figure 2-7. Measuring Skin Panel Damage
Figure 2-8. Measuring Damage In Floors and Decks
Figure 2-9. Measuring Damage In Honeycomb Panels
e. General Damage Assessment
Figure 2-10. Station and Waterlines
Figure 2-11. Aircraft Breakdown
Figure 2-12. Fairing Structure, LH.
Figure 2-13. Fairing Structure, R. H.
Figure 2-14. Production Breakdown, L. H.
Figure 2-15. Production Breakdown, R. H.
Figure 2-16. Section 41
Figure 2-17. Forward Pylon
Figure 2-18. Section 43, L. H.
Figure 2-19. Section 43, R. H.
Figure 2-20. Section 46, L. H.
Figure 2-21. Section 46, R. H.
Figure 2-22. Aft Pylon, L. H.
Figure 2-23. Aft Pylon, R. H.
Figure 2-24. Basic Structure, L. H.
Figure 2-25. Basic Structure, R. H.
Figure 2-26. Centerline, R. H.
Figure 2-27. Centerline, L. H.
Figure 2-28. Airframe
Figure 2-29. Secondary Structure
Figure 2-31. Cabin Fuselage
Figure 2-32. Aft Fuselage and Pylon
SECTION II. GENERAL STRUCTURAL REPAIRS
2-7. SUBSTITUTE HUCK, HI-LOK, OR NAS BOLTS
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 1 of 6)
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 2 of 6)
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 3 of 6)
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 4 of 6)
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 5 of 6)
Figure 2-33. Rivet Spacing, Selection, and Acceptability Limits (Sheet 6 of 6)
SECTION III. MAINTENANCE AND REPAIR PROCEDURES
Table 2-2. Information on Bolts and Screws
Table 2-3. Adhesive System Selection
Table 2-4. Adhesive System Criteria - TM-1-1520-240-BD_85
Table 2-4. Adhesive System Criteria - TM-1-1520-240-BD_86
c. Preparation of Bonding Surfaces
Table 2-5. Acceptable Adhesives
f. Application of Adhesive System No. 4
g. Application of Adhesive System No. 5
j. Application of Adhesive System No. 8.
l. Application of Adhesive System No. 9
o. Application of Adhesive System No. 1P
2-14. APPLICATION OF TAPES
b. Removal of Antichafing Tape
2-17. SKIN AND WEB REPAIRS
b. Backing Plate Repair for Webs
Table 2-6. Substitute Materials
Figure 2-34. Skin and Web Repairs (Sheet 1 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 2 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 3 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 4 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 5 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 6 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 7 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 8 of 9)
Figure 2-34. Skin and Web Repairs (Sheet 9 of 9)
Figure 2-35. Formed Parts Repairs (Sheet 1 of 6)
Figure 2-35. Formed Parts Repairs (Sheet 2 of 6)
Figure 2-35. Formed Parts Repairs (Sheet 3 of 6)
Figure 2-35. Formed Parts Repairs (Sheet 4 of 6)
Figure 2-35. Formed Parts Repairs (Sheet 5 of 6)
Figure 2-35. Formed Parts Repairs (Sheet 6 of 6)
2-22. BEAMS.
Figure 3-1. Landing Gar Assessment Logic
3-1. LANDING GEAR REPAIRS
Figure 4-1. Powerplant Assessment Logic
4-1. BATTLE DAMAGE
CHAPTER 5 ROTOR SYSTEM
CHAPTER 6 POWERTRAIN SYSTEM
6-7. OPTION 2
CHAPTER 7 PNEUDRAULICS
Figure 7-1. Pneudraulics Assessment Logic
SECTION III. BATTLE-DAMAGE REPAIRS - TM-1-1520-240-BD_124
Figure 7-2. Tubing Repair (Union)
7-10. REPAIR HIGH-PRESSURE TUBING
Figure 7-3. Tubing Repair (High Pressure)
Figure 7-4. Repair (Flareless) Seat
Figure 7-6. Damaged Tube Section Straight Tube
Figure 7-7. Splice Repair Assembly
Figure 7-9. Damaged Tube Section - Complex Bends
Figure 7-10. Splice Adapter Assembly installation
Figure 7-12. MS Fittings on Tubing Assembly
Figure 7-13. Tube Spice Length
Figure 7-15. MS Fitting/Complex Bends Repair
Figure 8-1. Instruments Assessment Logic
8-1. INSTRUMENT DAMAGE
CHAPTER 9 ELECTRICAL AND AVIONICS SYSTEM
SECTION III. BATTLE-DAMAGE REPAIRS - TM-1-1520-240-BD_139
(1) Test Equipment Kit.
(2) Connector Repair Kit
(3) Wire Repair Kit.
(4) Emergency Wire Repair and Aircraft Recovery Kit.
Figure 9-3. ACM/BDR Electrical Wiring System Repair Sequence Flow Diagram By Mission
9-8. ACM/BDR ELECTRICAL WIRING SYSTEM REPAIR DEFINITIONS AND CAPABILITIES
Figure 9-4. Item B15 Crimp Splice
Figure 9-5. Item B16 Crimp Splice
Figure 9-7. Item B18 Crimp Splice
Figure 9-9. Item 820 Crimp Splice
Figure 9-11. Item B21 Shielded Cable Splice
Figure 9-13. Item B23 Shielded Cable Splice
Figure 9-14. Item B13 Shielded Cable Repair
Figure 9-15. Item B5 Shield Terminator M83519/2-7
Figure 9-17. Item B7 Shield Terminator M8351912-10
Figure 9-19. Item B10 Terminal Boards
Table 9-1. Selection Table for Item B30 -- B35
Figure 9-21. Items A40, A41, andA42
Figure 9-23. Items BI, B2, B3, and B4 Contacts
Figure 9-24. Replacement of Damaged Connectors
Figure 9-26. Item B9 Self-Clinching Cable Straps
Figure 9-27. Item B24 Coax Spike
Figure 9-29. Item B26 Coax Splice
Figure 9-31. Item B28 Coax Splice
Figure 9-32. Item B29 Coax Splice
Figure 9-33. Item B11 Spilt Bolt Splice
Figure 9-35. Item A6 Heat-Shrlnkable Repair Tape
c. Emergency Repair Techniques.
Table 9-4. Wire Size Selection
Figure 9-37. MK-0015 Wire Repair Kit (Compartment A)
Figure 9-38. MK-0015 Wire Repair Kit (Compartment B)
Figure 9-39. MK-0015 Wire Repair Kit (Component Selection Chart) (Sheet 1 of 2)
Figure 9-39. MK-0015 Wire Repair Kit (Component Selection Chart) (Sheet 2 of 2)
Figure 9-40. DM664A Repair Kit (Compartment A)
Figure 9-41. DM664A Connector Repair Kit (Compartment B)
Figure 9-42. DM664A Connector Repair Kit (Compartment)
Figure 9-43. Cross Reference Chart (Sheet 1 of 4)
Figure 9-43. Cross Reference Chart (Sheet 2 of 4)
Figure 9-43. Cross Reference Chart (Sheet 3 of 4)
Figure 9-43. Cross Reference Chart (Sheet 4 of 4)
Figure 9-44. Emergency Wiring Repair Kit (instruction and Tool Description Chart)
Figure 9-45. Emergency Wire Repair Kit (Contents Chart, Items 1-8)
Figure 9-46. Emergency Wire Repair Kit (Contents Chart, Items 9-20)
Figure 9-47. Emergency Wire Repair Kit (Cross Reference Chart)
Figure 9-48. Test Equipment Kit
Figure 9-49. Test Equipment Kit (Cross Reference Chart) (Sheet 1 of 2)
Figure 9-49. Test Equipment Kit (Cross Reference Chart) (Sheet 2 of 2)
Figure 9-50. Test Equipment Kit (Cross Reference Chart) (Sheet 1 of 2)
Figure 9-50. Test Equipment Kit (Cross Reference Chart) (Sheet 2 of 2)
Table 9-5. ACMI/BDR Wiring Repair Set Permanent Repair Capabilities (One Hour/One Flight)
ACIWBDR Wiring Repair Set Permanent Repair Capabilities (One Hour/One Flight) (Continued)
CHAPTER 10 FUEL SYSTEM
Figure 10-1. Fuel System Assessment Logic
Figure 10-4. Fuel Tubing Elbow Repair (One Time Flight)
CHAPTER 11 FLIGHT CONTROLS SYSTEM
Figure 11-1. Flight Controls Assessment Logic
CHAPTER 12 AIRCRAFT AERIAL RECOVERY FOR CH-47D
Figure 12-1. Hoisting (Sheet 1 of 3)
Figure 12-1. Hoisting (Sheet 2 of 3)
Figure 12-1. Hoisting (Sheet 3 of 3)
Figure 12-2. Dual Hook Lifting Configuration (Sheet 1 of 4)
Figure 12-2. Dual Hook Lifting Configuration (Sheet 2 of 4)
Figure 12-2. Dual Hook Lifting Configuration (Sheet 3 of 4)
Figure 12-2. Dual Hook Lifting Configuration (Sheet 4 of 4)
APPENDIX A REFERENCES - TM-1-1520-240-BD_204
APPENDIX B SPECIAL OR FABRICATED TOOLS
SPECIAL TOOLS UST FOR BATTLE-DAMAGE REPAIRS - Continued - TM-1-1520-240-BD_206
SPECIAL TOOLS UST FOR BATTLE-DAMAGE REPAIRS - Continued - TM-1-1520-240-BD_207
SPECIAL TOOLS UST FOR BATTLE-DAMAGE REPAIRS - Continued - TM-1-1520-240-BD_208
SPECIAL TOOLS UST FOR BATTLE-DAMAGE REPAIRS - Continued - TM-1-1520-240-BD_209
DESCRIPTION - TM-1-1520-240-BD_210
Figure B-1. Blind Fastener Installation
APPENDIX C EXPENDABLE/DURABLE SUPPLIES AND MATERIALS LIST
EXPENDABLE/DURABLE SUPPLIES AND MATERIALS LIST (Continued)
EXPENDABLE/DURABLE SUPPUES AND MATERIALS LIST (Continued) - TM-1-1520-240-BD_214
EXPENDABLE/DURABLE SUPPUES AND MATERIALS LIST (Continued) - TM-1-1520-240-BD_215
EXPENDABLE/DURABLE SUPPUES AND MATERIALS LIST (Continued) - TM-1-1520-240-BD_216
EXPENDABLE/DURABLE SUPPUES AND MATERIALS LIST (Continued) - TM-1-1520-240-BD_217
GLOSSARY SECTION I. TERMS AND DEFINITIONS
Debriefing, Flight-Crew
SECTION II. ACRONYMS AND ABBREVIATIONS
ACRONYMS AND ABBREVIATIONS -cont

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