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(a) Structural movement which

might change the location or alignment

of a component.

Controls and drive-

shafts will be particularly critical.

(b) Structural damage which

could affect the security of wire
bundles and fluid lines, causing them to
vibrate, chafe, and fatigue during
flight.

might interfere with the free travel or
movement of a system component during

operation.

(3) If the assessor determines

that structural damage will or might
create any of the above conditions,

TM 55-1520-228-BD

AIRFRAME

classify the structure as failed even if
the physical damage is within allowable

limits.

4-14. BDAR REPAIR PROCEDURE INDEX.

PARA.

Skin/Stiffener Damage. . . . . 4-16
Cap, Skin, Web, Doubler

Damage. . . . . . . . . . . 4-17

Cap or Longeron Damage . . . . 4-18

Frame, Bulkhead, Skin and

Stringer Damage. . . . . . . 4-19

Honeycomb Core Floor or

Panel Damage . . . . . . . . 4-20

Windshield/Window Damage . . . 4-21

Tail Boom Skin Damage . . . . 4-22

Section II. EXPEDIENT STRUCTURAL REPAIRS

4-15. GENERAL.

Many of these expedient repairs

will restore the airframe to condition

Inspection for damage growth will

generally be required after every

flight, and damage should be repaired

as soon as practical by standard main-

tenance procedures.

Multiple Damage. Special atten-

tion should be given to structural com-
ponents which have sustained damage in

multiple locations.

It is essential

that damage to an individual structural
item not be considered by itself. Suit-

able repair will often depend on the

condition of the adjacent structure. In
some cases, undamaged adjacent structure

may satisfactorily take the load of the

damaged item.

Since time is an over-

riding consideration on the battlefield,

BDAR airframe repairs are usually per-

formed on the outside of the aircraft to
save the time required to gain access to
the interior.

If, however, access to the

interior damaged structure is already

available, inside BDAR repairs may be

made.

c. Fasteners. BDAR can be carried

out using any form of fastening device,

which is available at the time (e.g.,

nuts, bolts, rivets, etc.), as long as

strength requirements are met.

Use

accepted practices regarding fastener
edge distance and spacing.

The faste-

ners used in a single repair should be
of the same type.

Metal Selection.

All repair

patches should be manufactured from

material of the same or similar specifi-

cation as the damaged area but at least
one gauge or 10 percent thicker. When

required repair materials are una-

vailable, substitutions can often be

made to produce a desired strength.

Table 4-8 cross lists various types of

metal and instructions on how to substi-

tute one type of metal for another.

Alternate repair materials can be
obtained from scrapped aircraft.

It is

also permissible to fabricate from

thinner gauge material and use multiple
thickness.

4-49

Содержание OH-58 C

Страница 1: ...R PLANT CHAPTER 7 ROTORS CHAPTER 8 DRIVE TRAIN SYSTEM CHAPTER 9 HYDRAULIC SYSTEM CHAPTER 10 INSTRUMENT SYSTEMS CHAPTER 11 ELECTRICAL SYSTEM CHAPTER 12 FUEL SYSTEM CHAPTER 13 FLIGHT CONTROLS CHAPTER 14...

Страница 2: ...ANDER AND SHALL BE REPAIRED BY STANDARD MAINTENANCE PROCEDURES AS SOON AS PRACTICABLE AFTER THE MISSION IS COMPLETED BDAR TECHNIQUES IN THIS MANUAL PERTAIN to the following helicopters OH 58A Helicopt...

Страница 3: ...ed representative EXPLOSIVES Battle damaged areas should be inspected for unexploded ordnance before attempting repairs Disposal of unexploded ordnance should be accomplished by qualified personnel AR...

Страница 4: ...equipment and who is competent in administering first aid When the technician is aided by operators he must warn them about dangerous areas Whenever the nature of the operation permits keep one hand...

Страница 5: ...l i c o p t e r m u s t b e e l e c t r i c a l l y g r o u n d e d p r i o r t o d e f u e l i n g F u e l l i n e a n d t a n k r e p a i r s o f t e n i n v o l v e h a n d l i n g o f h i g h l y...

Страница 6: ...as aviator helmet or ear plugs are required to be worn RADIOACTIVE MATERIALS Self luminous dials and ignition units may contain radioactive materials If such an instrument or unit is broken or becomes...

Страница 7: ...sert pages as indicated below New or changed text material is indicated by a vertical bar in the margin An illustration change is indicated by a miniature pointing hand Remove Pages Insert Pages A B b...

Страница 8: ......

Страница 9: ...PAGES IN THIS PUBLICATION IS 762 CONSISTING OF THE FOLLOWING Page Change Page Change No No No No Cover 0 A through d 0 i 1 ii through ix 0 x blank 0 1 1 through 1 5 0 1 6 1 1 7 through 1 11 0 1 12 bla...

Страница 10: ......

Страница 11: ...s CHAPTER 2 ASSESSING BATTLEFIELD DAMAGE Section I Introduction Section II General Fault Assessment Table CHAPTER 3 GENERAL REPAIRS CHAPTER 4 AIRFRAME Section I Introduction Section II Expedient Struc...

Страница 12: ...SYSTEM Section I Introduction Section II Electrical and Avionics Wiring Damage CHAPTER 12 FUEL SYSTEMS Section I Introduction Section II Lines and Hoses Section III Fuel Cell Damage CHAPTER 13 FLIGHT...

Страница 13: ...S 1 INDEX 1 LIST OF ILLUSTRATIONS Title DA Form 2408 13 DA Form 2408 18 Damage Assessment Markings Sheet 1 of 3 Aircraft Sections DA Form 2404 Evaluating Damage to Angles Channels and Z Angles Damaged...

Страница 14: ...late Installation Double Check Valve System Possible Alternatives Wood Plug Sealant for Small Holes Repair Using Screw Washer and Gasket Hose Assembly Sealant Nut and Bolt Sheet Metal with Sealant and...

Страница 15: ...ield Terminator Repair Nickel Plated Shield Terminator Preparation Nickel Plated Shield Terminator Repair Terminal Lug Repair Self Clinching Cable Strap Self Clinching Cable Strap and Tool Tie Tape Re...

Страница 16: ...ating System A C Heating and Ventilating System Bleed Air A Model Heating and Ventilating System Bleed Air C Model Combustion Heater Shroud Heater System Schematic Bleed Air Line Installation Bleed Li...

Страница 17: ...em Assessment Procedures Flight Control System Assessment Procedures Nominal Tube Splice Sizes Bolt Drill Sizes for Control Tube Repairs Assessment Procedures Essential Spare Parts Spare and Repair Pa...

Страница 18: ...r detailed repair procedures of the major functional groups The major functional groups correspond with the functional groups of the 23 series manuals that are employed in routine repairs to the helic...

Страница 19: ...procedures so as not to further damage and or jeopardize either personnel or the equipment during or subsequent to the BDAR action Ensure all documentation is completed as directed in this manual and...

Страница 20: ......

Страница 21: ...ible types of combat damage and failure modes cannot be pre dicted nor are all effective field expedient repairs known This TM pro vides guidelines for assessing and repairing battlefield failures of...

Страница 22: ...d equipment 3 Repair using parts that serve a noncritical function elsewhere on the same equipment for the purpose of restoring a critical function 4 Bypassing of noncritical com ponents in order to r...

Страница 23: ...ity of a battle damaged helicopter to retrieve itself fly out from a battlefield environment It usually will involve flying with degraded flight status and with restrictions and limitations placed on...

Страница 24: ...he minimum functional combat capability MFCC criteria for the OH 58 is as follows a Flight Capability for Mission Completion Helicopter s flight charac teristics degraded to a minimum of combat capabl...

Страница 25: ...orm 2408 18 as per DA PAM 738 751 See Figures 1 1 1 2 b Recording of BDAR repairs and the use of status symbols as defined in DA PAM 738 751 will be completed as soon as practical to indicate any limi...

Страница 26: ...include a statement that a temporary repair has been made 2 If the temporary repair limits the capability of the aircraft the following entry will be made on DA Form 2408 13 a Place a circled red X in...

Страница 27: ...Quarts 13 14 15 SERVICED ANTl SERV 0XYGEN ICING TOTAL ADDED TOTAL GRADE ADDED ADDED TOTAL FLUID IN GRADE N0 1 IN TANKS N0 2 ENG APU TANKS ENG TANKS Gals BY STATION 1 2 3 4 5 6 7 TOTAL 16 STATUS 17 FA...

Страница 28: ...OF PAGES 5 ITEM TO BE INSPECTED 6 REEFERENCE 7 FREQUENCY 8 NEXT DUE DA FORM 2404 18 1 JAN 64 EQUIPMENT INSPECTION LIST For use of this form see TM 38 750 the proponent agency is DCSLOG TM 55 1520 228...

Страница 29: ...es or crosshatch between the two circular lines STRINGER REPAIR Place an X to the left and right of the circle FRAME REPAIR Place an X above and below the circle TO INDICATE DAMAGE TO SYSTEMS REQUIRIN...

Страница 30: ...e conditions Continual assessment or reinspection is required after each sortie Instruction markings for system are in two parts 1 Repair instruction markings and meanings are shown on this sheet and...

Страница 31: ...Electrical AV Avionics Flt Cont Flight Control Main Rotor Main Rotor Group Tail Rotor Tail Rotor Group Air Pneumatic Air Cond Air Conditioning BL Air Bleed Air System BLC Boundary Layer Control N2 Nit...

Страница 32: ......

Страница 33: ...icopter location can have a considerable effect on the assessment The following appraisal shall be accomplished 1 If possible and time permits inspect and check the helicopter using operator s check l...

Страница 34: ...TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE Table 2 1 General Decision Logic SEE TM 55 1520 328 25 2 2...

Страница 35: ...t The BDAR assessment procedure will refer you to a guide fix in this manual a stan dard TM 55 1520 228 23 repair if it is feasible or a higher AVIM level of repair if extent of damage time con strain...

Страница 36: ...TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE Table 2 2 General Assessment Cont 2 4...

Страница 37: ...TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE Table 2 2 General Assessment Cont 2 5...

Страница 38: ...TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE Table 2 2 General Assessment Cont 2 6...

Страница 39: ...Table 2 2 General Assessment Cont TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE 2 7...

Страница 40: ...I 2 8 TM 55 1520 228 BD ASSESSING BATTLEFIED DAMAGE Table 2 2 General Assessment Cont...

Страница 41: ...TM 55 1520 228 BD ASSESSING BATTLEFIELD DAMAGE Table 2 2 General Assessment Cont I 2 9 2 10 Blank...

Страница 42: ......

Страница 43: ...OF THE COMMANDER AUTHORIZED TRAINING FIXES ARE LISTED IN APPENDIX E IN EITHER CASE DANAGES SHALL BE REPAIRED BY STANDARD PROCEDURES AS SOON AS PRACTICABLE No general repairs have been identified Chapt...

Страница 44: ......

Страница 45: ...ture No amount of structural damage to secondary struc tures will restrict combat capability from a structural point of view however secondary structure may be required for aerodynamic reasons or to a...

Страница 46: ...TM 55 1520 228 BD AIRFRAME 4 2 Table 4 1 Aircraft Structure Damage Assessment Prodecures...

Страница 47: ...TM 55 1520 228 BD AIRFRAME Figure 4 1 Aircraft Sections 4 3...

Страница 48: ...y impact or penetration in regions away from the site of primary damage 2 Inspect for small and large cracks caused by projectile damage Small cracks will enlarge under con tinued loading particularly...

Страница 49: ...pecting for broken and missing fasteners Inspect fasteners for security shear pull through tear out and elongated fastener holes Where possible inspect fasteners from both sides h Inspecting for Delam...

Страница 50: ...TM 55 1520 228 BD AIRFRAME Figure 4 2 DA Form 2404 4 6...

Страница 51: ...damages In Figure 4 4 the length of the flat tened cross section of the angle is a b CD is the depth of the damage into the flattened cross section The length of the remaining effective cross section...

Страница 52: ...TM 55 1520 228 BD AIRFRAME Figure 4 3 Evaluating Damage to Angles Channels and Z Angles 4 8...

Страница 53: ...TM 55 1520 228 BD AIRFRAME Figure 4 4 Damaged Cross Section 4 9...

Страница 54: ...TM 55 1520 228 BD AIRFRAME Figure 4 5 Measuring Skin Panel Damage 4 10 IMPORTANT MEASURED LATERAL DAMAGE MUST INCLUDE ALL RADIATED CRACKS...

Страница 55: ...TM 55 1520 228 BD AIRFRAME Figure 4 6 Measuring Damage in Webs and Panels 4 11...

Страница 56: ...4 7 are designated for a given condition as follows CD Allowable depth of damage CL Allowable length width of damage A Allowable area of damage D Minimum allowable distance between damages WL Allowabl...

Страница 57: ...TM 55 1520 228 BD AIRFRAME Figure 4 7 Measuring Damage in Honeycomb Sandwich Panels 4 13...

Страница 58: ...sible Self recovery is preferable to disassembly and boxing an aircraft for transportation As time permits proceed as follows 1 Mark all visible cracks and the extent of other structural damage with c...

Страница 59: ...ircraft to condition 1 a determine the required repairs for all damaged structural elements that are below condition 1 b Repairs on damaged struc tural elements that are better than condition 1 may be...

Страница 60: ...is a full mono coque structure utilizing a tapered cir cular section of aluminum alloy skin Redistribution in the forward end which is required to transfer loads from the monocoque structure to the f...

Страница 61: ...TM 55 1520 228 BD AIRFRAME Figure 4 8 OH 58 Helicopter 4 17...

Страница 62: ...ED CENTER TAILROTOR BEARING HANGER TANGENCY POINT CONTOURS IN BOOM STATIONS ARE CIRCLES RADIUS AT 31 87 IS 7 3555 RADIUS AT 182 405 IS 3 286 TAPER OF BOOM IS 0 02703 PER INCH BOOM STATION IS 90 TO HOR...

Страница 63: ...TM 55 1520 228 BD AIRFRAME Figure 4 10 Cockpit 4 19...

Страница 64: ...TM 55 1520 228 BD AIRFRAME Figure 4 11 Fuselage Pylon Support Structure Sheet 1 of 5 4 20...

Страница 65: ...TM 55 1520 228 BD AIRFRAME Figure 4 11 Fuselage Pylon Support Structure Sheet 2 of 5 4 21...

Страница 66: ...TM 55 1520 228 BD AIRFRAME Figure 4 11 Fuselage Pylon Support Structure Sheet 3 of 5 4 22...

Страница 67: ...TM 55 1520 228 BD AIRFRAME FS130 FUSELAGE STA 130 BULKHEAD FS117 71 WL 21 00 Figure 4 11 Fuselage Pylon Support Structure Sheet 4 of 5 4 23...

Страница 68: ...TM 55 1520 228 BD AIRFRAME Figure 4 11 Fuselage Pylon Support Structure Sheet 5 of 5 4 24...

Страница 69: ...TM 55 1520 228 BD AIRFRAME Figure 4 12 Upper and Lower Shell Structure 4 25...

Страница 70: ...TM 55 1520 228 BD AIRFRAME Figure 4 13 Aft Fuselage Structure 4 26...

Страница 71: ...TM 55 1520 228 BD AIRFRAME Figure 4 14 Tail Boom 4 27...

Страница 72: ...TM 55 1520 228 BD AIRFRAME Figure 4 15 Cowling and Firewalls 4 28...

Страница 73: ...onent to other major components are sheared pulled through or missing at one or more locations 4 Three or more fasteners next to each other which join a cap longeron and stringer to the web are sheare...

Страница 74: ...personnel cargo or equipment for which it was designed 3 The panel is on the outside of the aircraft where it is exposed to aerodynamic forces and the damage is 4 30 oriented so as to produce peeling...

Страница 75: ...10 65 Section 73 04 30 29 17 31L R Pilot s Copilot s 73 04 30 29 Collective 21 00 Jackshaft 73 04 30 29 Pedestal 55 14 20 00 5 06R Structure 73 04 30 17 3 06L age Limits Forward Fuselage Condition I D...

Страница 76: ...0 25 0 50 10 73 00 87 85 27 48 72 00 3 00L 3 00R Side Webs and Doublers 2 25 5 74 52 81 30 54 50 72 00 3 00L 3 00R Web Front 0 80 00 87 85 62 00 72 00 3 00L 3 00R Splices 0 73 00 87 85 20 00 72 00 3...

Страница 77: ...1 50 1 50 5 5 Bulkhead FS130 Upper 130 51 72 72 00 Inboard Outboard Frame Caps 0 30 0 60 10 130 51 72 72 00 Frame Webs 2 40 5 130 51 72 72 00 Clips Splices Supports Flanges 0 30 0 60 10 Bulkhead FS13...

Страница 78: ...s No Damage Allowed 120 90 67 92 71 96 3 00L 3 00R Bulkhead Skin and Doubler 2 00 5 80 46 130 00 67 92 3 00L 3 00R Bottom Skin and Access Cover 0 75 5 Lower Cabin Shell 73 18 113 00 20 00 25 25 18 40L...

Страница 79: ...L R Cross Tube Aft Strap 0 31 0 62 73 00 18 30 13 30L R Cross Tube Forward Strap 0 10 0 20 73 00 130 00 18 30 20 75 13 30L R 10 25L R Back Up Supports No Damage Allowed 73 00 130 00 18 30 20 75 13 30L...

Страница 80: ...5 61 76 Tail Boom Attach Fittings No Damage Allowed Lower Longeron 130 00 192 84 29 40 44 50 22 50 1 10L R Angle No Damage Allowed 130 00 29 40 Splice No Damage Allowed Aft Fuselage 130 00 206 35 Lowe...

Страница 81: ...130 00 167 00 71 74 14 12L 14 12R Doublers Splices Vertical Stiffeners 0 75 1 50 10 Canted Web 130 00 192 84 51 67 59 98 25 00L R 7 00L R Stiffeners 1 15 2 30 10 130 00 192 84 51 67 59 98 15 00L R 7 0...

Страница 82: ...L R Fitting No Damage Allowed 4 38 Table 4 4 Damage Limits Tail Boom and Landing Gear Condition I DAMAGE LIMITS LOCATION CAP FLANGE SKIN WEB COMPONENT MEMBER BS WL BL ELEMENT CD CL N WL N NOTES CAUTIO...

Страница 83: ...MEMBER FS WL BL ELEMENT CD CL N WL N NOTES CAUTIONS D N x CL D N x WL Fin Fin to Antenna Attaching Flanges 1 20 2 40 10 Fin to Boom Inserts No Damage Within 3 of Inserts Tail Skid Tube Fitting No Dam...

Страница 84: ...ter Bulkhead Section 73 04 30 29 54 89 Web 12 00 5 73 04 21 00 30 29 10 64 17 31L R Vertical Stiffeners 2 20 4 40 Pilot s Copilot s Seat 73 04 30 29 Aft Attachment Angle 0 70 1 40 5 Collective Jacksha...

Страница 85: ...No Damage Within 3 of Gun Mount If Used 96 44 114 76 24 70 29 92 23 08L R Honeycomb Side Panels 2 00 5 96 44 20 00 29 92 23 08L 23 08R Honeycomb Front Panel 4 5 5 96 44 114 76 20 00 29 92 23 08L 23 0...

Страница 86: ...0 00 50 04 69 00 20 55L R Inner Skin and Doublers 5 30 5 117 71 130 00 50 04 67 20 25 25L Outer Skin 7 50 5 117 71 130 00 50 04 67 20 25 25R Outer Skin and Door Panel 7 50 5 117 71 130 00 50 00 72 00...

Страница 87: ...00 130 00 20 00 54 65 Honeycomb Panel 10 00 5 No Damage Within 3 Radius of Inserts 96 44 20 00 Splice 1 50 3 00 5 36 00 130 00 20 00 54 65 Frames Angles Stiffeners 0 75 1 50 5 Upper Cabin Roof Shell 5...

Страница 88: ...50L Fitting No Damage Allowed Anti Torque Support Fittings 78 95 23 83 3 06L Fitting No Damage Allowed 4 44 Table 4 6 Damage Limits Aft Fuselage Condition II DAMAGE LIMITS LOCATION CAP FLANGE SKIN WE...

Страница 89: ...2 205 76 72 00 8 33L 8 33R Skin 3 75 5 Oil Cooler 167 00 179 92 72 00 10 18L 10 18R Honeycomb Support Panel 3 00 5 No Damage Within 2 of Inserts 171 50 72 00 0 Pan Drain No Damage Allowed Anti Torque...

Страница 90: ...34 46 Inserts Damage Limited to Two Inserts to Each Group of Four 130 00 167 00 29 47 34 46 Honeycomb 15 0 5 No Damage Within 2 of Effective Inserts Bulkheads 142 154 167 179 192 Frame Section 1 10 2...

Страница 91: ...182 40 31 87 42 59 79 82 98 29 116 84 150 22 Bulkheads 1 00 2 00 5 174 10 182 40 Bulkheads 1 05 2 10 5 174 10 182 40 Fin Supports 0 50 1 00 5 174 10 182 40 Gearbox Mounting Plate No Damage Allowed 17...

Страница 92: ...verstress such as buckling and misalignment 2 Fasteners securing the fire wall to the upper deck structure are sheared stripped pulled through or missing at three or more adjoining loca tions 3 Twenty...

Страница 93: ...ained damage in multiple locations It is essential that damage to an individual structural item not be considered by itself Suit able repair will often depend on the condition of the adjacent structur...

Страница 94: ...4 50 Table 4 8 Metal Substitution Chart TM 55 1520 228 BD AIRFRAME...

Страница 95: ...ctural stiffness should be sufficient to assure loads are properly distributed and to avoid serious vibrations Use shims to avoid joggles Avoid hand formed and fitted parts Where a stringer stiffener...

Страница 96: ...TM 55 1520 228 BD AIRFRAME Figure 4 16 Typical Former Repair Sheet 1 of 2 4 52...

Страница 97: ...TM 55 1520 228 BD AIRFRAME Figure 4 16 Typical Former Repair Sheet 2 of 2 4 53...

Страница 98: ...nger to match existing holes Attempt to interpitch new fasteners within the existing rivet pattern if the area is inaccessible for back drilling 5 Rivet the substitute stiffener stringer in place Figu...

Страница 99: ...its and will require repair A patch plate can often be used to repair the damage LIMITATIONS None Condition 1 Inspect after every flight for damage growth PERSONNEL TIME REQUIRED 2 Soldiers 2 Hours MA...

Страница 100: ...TM 55 1520 228 BD AIRFRAME Figure 4 19 Typical Patch Plate Repair 4 56...

Страница 101: ...be at least that of the damaged cap or longeron Refer to Table 4 8 for substitute materials to use on repair if a longeron or cap section is not available Skin Patch Blind Rivets item 41 Appx C PROCE...

Страница 102: ...TM 55 1520 228 BD AIRFRAME Figure 4 20 Expedient Cap Longeron Repair 4 58...

Страница 103: ...ortion of damaged stringers The strap should be long enough to overlap both ends of the damaged bulkhead or frame flange by six rivets on each end In the areas where the repair strap will overlap on t...

Страница 104: ...TM 55 1520 228 BD AIRFRAME Figure 4 21 Repair of Damaged Bulkhead Flange 4 60...

Страница 105: ...TM 55 1520 228 BD AIRFRAME Figure 4 22 Typical Combination Repair Sheet 1 of 2 4 61...

Страница 106: ...TM 55 1520 228 BD AIRFRAME Figure 4 22 Typical Combination Repair Sheet 2 of 2 4 62...

Страница 107: ...Remove ragged edges Figure 4 23 2 Apply tape over repair to keep out moisture 3 Record BDAR action taken When mission is complete as soon as practical repair the equipment system using standard mainte...

Страница 108: ...d Honeycomb Core Panel 2 8 Inch Damage One Skin and Core MAKE PATCH FROM 2024 T3 OR 7075 T6 ALCLAD ALUMINUM 1 8 CHERRY RIVET 2 DIA EDGE DISTANCE 4 DIA RIVET SPACING THRU ONE SKIN ONLY PATCH REPAIR PAT...

Страница 109: ...ins and Core LIMITATIONS None PERSONNEL TIME REQUIRED 1 Soldier 2 Hours MATERIALS TOOLS REQUIRED 2 Patch Plates Cherry Rivets PROCEDURAL STEPS 1 Remove damaged skin and core Figure 4 28 Clean top and...

Страница 110: ...TM 55 1520 228 BD AIRFRAME Figure 4 26 Damage Repair Accessible One Side Only Figure 4 27 Patch Plates One Side Accessible Repair 4 66...

Страница 111: ...TM 55 1520 228 BD AIRFRAME Figure 4 28 Damage Over Repair of Honeycomb Core Panel 8 Inches Both Skins and Core 4 67...

Страница 112: ...to 3 4 inch spacing 3 8 inch edge distance along both sides of any crack and along the sides of the hole 3 Lace safety wire with needle nose pliers through holes and across cracks and over hole formin...

Страница 113: ...TM 55 1520 228 BD AIRFRAME Figure 4 29 Fracture Lacing With Safety Wire 4 69...

Страница 114: ...contour of tail boom The patch must extend a minimum of 3 inches forward and aft and 1 inch above and below the damaged area Figure 4 30 3 Sand surfaces lightly to remove all surface finish Clean are...

Страница 115: ...PROCEDURE INDEX PARA Hard Landings Sudden Stops 5 6 Skid Damage 5 7 Section II SKID TUBE 5 5 GENERAL INFORMATION a In battle conditions part of the skid tube may sustain various amounts of damage whi...

Страница 116: ...TM 55 1520 228 BD ALIGHTING GEAR Figure 5 1 Landing Gear and Support Installation Figure 5 2 Skid Tube Damage Zones 5 2...

Страница 117: ...TM 55 1520 228 BD ALIGHTING GEAR Table 5 1 Assessment Procedure Logic 5 3...

Страница 118: ...ected This will most likely go beyond scope of BDAR Section III SKID DAMAGE 5 7 SKID DAMAGE GENERAL INFORMATION Landing skids may be damaged by wear or enemy fire If time is available repair can be pe...

Страница 119: ...TM 55 1520 228 BD ALIGHTING GEAR Figure 5 3 Skid Repair Figure 5 4 Clamp Repair 5 5...

Страница 120: ...TM 55 1520 228 BD ALIGHTING GEAR Figure 5 5 Fabricated Clamp 5 6...

Страница 121: ...alve Inoperative 6 5 Double Check Valve Inoperative 6 6 Oil Tank Punctured 6 7 Oil Lines Rigid Type Repair 9 7 Fuel Oil Pneumatic Line Repair Section II COMPONENT EXPEDIENT FIXES This section has vari...

Страница 122: ...TM 55 1520 228 BD POWER PLANT Figure 6 1 T63 Series Engine 6 2...

Страница 123: ...POWER PLANT Table 6 1 Engine BDAR Assessment Logic 6 3...

Страница 124: ...wly b Monitor TOT and N1 gauges for possible stall readings NOTE Stall usually occurs between 65 percent and 75 percent N1 c If stall is present TOT will rise rapidly and N1 RPMs will fluctuate betwee...

Страница 125: ...the pilot must be made aware that if any component of the system is removed or bypassed any input will result in erratic engine response At all times the integrity of all fuel control lines must be m...

Страница 126: ...RIALS TOOLS REQUIRED Flex Line Tubing ID 0 25 in Length 12 in rein No 4 Fittings 1 Refer to Figure 6 3 b to establish bypass configuration 2 Disconnect clamp from flexible hose and extend flexible hos...

Страница 127: ...TM 55 1520 228 BD POWER PLANT Figure 6 3 Double Check Valve System Possible Alternatives 6 7...

Страница 128: ...ean area around crack with solvent to remove the oil 2 Seal crack with tape 3 Replenish oil supply 4 Record BDAR action taken When mission is complete as soon as practical repair the equipment system...

Страница 129: ...hole 2 Pierce a small hole in the center of the gasket material 3 Using the sheet metal screw and washer screw the gasket material through the pierced hole and through the small hole on the oil tank...

Страница 130: ...se assembly about half way through hole Tighten nut on bolt expand hose to seal hole If necessary remove oil tank plate to allow a wrench or pliers inside of oil tank to hold nut while turning bolt 4...

Страница 131: ...item 20 Appx C PROCEDURAL STEPS 2 If sealant is to be used clean area around hole with solvent so sealant will stick 3 Put sealant or gasket material over hole Put sheet metal plate over hole and sec...

Страница 132: ...TM 55 1520 228 BD POWER PLANT I Figure 6 8 Sheet Metal Plate with Sealant and or Cherry Rivets 6 12...

Страница 133: ...rotor is driven by the tail rotor gearbox and provides for directional control See Figures 7 1 and 7 2 for system configuration Assessment proce dures are found in Table 7 1 Section II REPAIRS 7 5 GEN...

Страница 134: ...Latch 2 Lever 11 Blade Assy 3 Idler Link 12 Retaining Bolt 4 Swashplate Assy 13 Grip 5 Link 14 Mast Nut 6 Collective Lever 15 Hub Assy Oil Lubricated shown 7 Inner Ring 16 Pitch Horn 8 Outer Ring 17...

Страница 135: ...1 Hub 2 Pitch Horn 3 Blade 4 Tail Rotor Gearbox TM 55 1520 228 BD ROTORS Figure 7 2 Tail Rotor System 7 3...

Страница 136: ...TM 55 1520 228 BD ROTORS Table 7 1 Assessment Procedures 7 4...

Страница 137: ...TM 55 1520 228 BD ROTORS Figure 7 3 Rotor Blades Damage Sensitive Areas 7 5...

Страница 138: ...r Inspection of repaired area after each flight would be required PERSONNEL TIME REQUIRED 2 Soldiers 1 Hour MATERIALS TOOLS REQUIRED Army Green Tape Maximum Width Available 3 Inches Minimum or Alumini...

Страница 139: ...TM 55 1520 228 BD ROTORS Figure 7 4 Rotor Blade Repair Application of Tape 7 7...

Страница 140: ...When entire blade and over the repaired area mission is complete as soon as practical repair the equipment system 9 Wrap exact number of tape wraps on using standard maintenance procedures opposite s...

Страница 141: ...mitter Leak 8 7 Low Pressure Sensing Switch 8 8 Oil Hoses and Lines Leaks or Restrictions 8 9 Transmission Bullet Damage 8 10 Tail Rotor Gearbox Bullet Damage 8 11 Section 11 REPAIR 8 5 SENSITIVITY OF...

Страница 142: ...ler Driveshaft 14 Coupling Main Driveshaft Oil Cooling Blower and 15 Splined Adapter Shaft Assy 16 Oil Filter Assy Aft Short Tail Rotor Driveshaft 17 Tail Rotor Driveshaft Long Tail Rotor Driveshaft S...

Страница 143: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM 8 3 Figure 8 1 Drive Train System Sheet 2 of 4...

Страница 144: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM Figure 8 1 Drive Train System Sheet 3 of 4 8 4...

Страница 145: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM Figure 8 1 Drive Train System Sheet 4 of 4 8 5...

Страница 146: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM Table 8 1 Drive Train System BDAR Assessment Procedures 8 6...

Страница 147: ...ot in a bend portion of duct routing a repair can be applied as shown at either repair B C or D If area to be repaired is in a bend portion of duct routing a repair can be applied as shown at either r...

Страница 148: ...Assy Transfer Tube 11 Filter Bypass Valve Nozzle Jet 12 Oil Temperature Switch Pressure Regulating Valve 13 Oil Pump Hoses and Lines 14 Chip Detector Oil Pressure Transmitter 15 Chip Detector P l u g...

Страница 149: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM Figure 8 3 Flex Duct Repair Sheet 1 of 2 8 9...

Страница 150: ...TM 55 1520 228 BD DRIVE TRAIN SYSTEM Figure 8 3 Flex Duct Repair Sheet 2 of 2 8 10...

Страница 151: ...Record BDAR action taken When mission is complete as soon as practical repair the equipment system using standard maintenance procedures 8 9 OIL HOSES AND LINES LEAK OR RESTRICTION CRIMP GENERAL INFOR...

Страница 152: ...am bind or lose lubricant repair may be deferred LIMITATIONS Small oil loss can be tolerated If aircraft is run for an extended period of time with little or no oil gearbox will jam PERSONNEL TIME REQ...

Страница 153: ...tallation They may be routed along any convenient path as long as they do not interfere with personnel or with operating equipment Long lines and hoses should be clamped to hard sup ports at convenien...

Страница 154: ...ve 9 Hydraulic Pump 10 Case Drain Hose 11 Solenoid Valve 12 Hose Return 13 Hose Return 14 15 16 17 18 19 20 21 22 23 24 25 Hose Pressure Hose Pressure Hose Pressure Hose Return pressure Switch Relief...

Страница 155: ...0 4 Quick Disconnects 11 5 Pump 12 6 Check Valve 13 7 Filter Filter Bypass Valve Relief Valve Solenoid Valve Pressure Switch Servo Actuator Cyclic Servo Actuator Collective TM 55 1520 228 BD HYDRAULIC...

Страница 156: ...TM 55 1520 228 BD HYDRAULIC Table 9 1 Assessment Logic Figure 9 3 Two Part Fitting 9 4...

Страница 157: ...TM 55 1520 228 BD HYDRAULIC Figure 9 4 Four Part Fitting Figure 9 5 Using Tube Cutter 9 5...

Страница 158: ...INFORMATION Aluminum tubing is subject to damage by projectiles and fragments Replacement with original replacement parts is desirable but not essential In BDAR tubing and hose AN and MS fittings and...

Страница 159: ...TM 55 1520 228 BD HYDRAULIC SECTION A A Figure 9 6 Properly Burred Tubing Figure 9 7 Damaged Tube Section 9 7...

Страница 160: ...TM 55 1520 228 BD HYDRAULIC Figure 9 8 Splice Repair Assembly Figure 9 9 Repair Fitting and Tube Installation 9 8...

Страница 161: ...on the OH 58 are braided wire covered rubber hose Repair of damage or wear to the wire braids is deferrable for one more flight provided the rubber inner hose is not leaking under pressure Inspect aft...

Страница 162: ...TM 55 1520 228 BD HYDRAULIC Figure 9 10 Damaged Tube Section Complex Bends Figure 9 11 Splice Adapter Assembly Installation 9 10...

Страница 163: ...re braid cover and the inner rubber hose Force onto hose until the edge of the sleeve is even with the end of the rubber hose 5 Reem inside end of Teflon hose with a square tool or a wooden plug so th...

Страница 164: ...TM 55 1520 228 BD Figure 9 12 Installation of Socket and Sleeve Figure 9 13 Assembly of MS Fitting 9 12...

Страница 165: ...dent primarily on the resilience of the o rings When moving parts are involved minor seepage may be normal and acceptable A moist surface found on moving parts of a hydraulic unit piston shaft is an i...

Страница 166: ...ough B87 are equivalent to MS28775 426 through 460 AN6227B88 is equivalent to MS28775 425 AN6230 B1 through B25 are equivalent to MS28775 223 through 247 9 10 HYDRAULIC FLUID SUBSTITUTIONS a If the or...

Страница 167: ...ILE MIL H 5606 2 3 MIL P 551O N507 9 BUNA N 65 F to 180 F 90 MIL H 83282 NAS1593 MIL R 25897 Fluoro 1 High temperature NAS1595 CL 1 77 545 Elastomer 20 F to 400 F 70 fluid resistant NAS1594 MIL R 2589...

Страница 168: ...2 N103 7 BUNA N 65 F to 225 F 70 pneumatic service Mineral oil hydraulic fluids alkalies gasolines NITRILE diesel oils 2 3 SB715BE1 E3 F1 N109 7 BUNA N 30 F to 250 F 70 pneumatics AN1239XX Petroleum b...

Страница 169: ...pneu NITRILE matics High extru 2 3 SB915B E1 E3 N183 9 BUNA N 30 F to 250 F 90 sion resistance Mineral oil NITRILE hydraulic fluids 2 3 SB915B E1 E3 N552 9 BUNA N 30 F to 250 F 90 pneumatics Air gase...

Страница 170: ......

Страница 171: ...COMBAT OR FOR TRAINING AT THE DISCRETION OF THE COMMANDER AUTHORIZED TRAINING FIXES ARE LISTED IN APPENDIX E IN EITHER CASE DAMAGES SHALL BE REPAIRED BY STANDARD PROCEDURES AS SOON AS PRACTICABLE The...

Страница 172: ......

Страница 173: ...the major components cable routes and wiring terminations for the more complex avionics systems b Circuit Function The unit number and circuit designation letter INTRODUCTION It is used to distinguis...

Страница 174: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Table 11 1 Electrical and Avionics Assessment Logic Figure 11 1 Circuit Identification 11 2...

Страница 175: ...RUMENT Tailpipe temperature Fuel flow Fuel quantity Fuel capacity Oil temperature Oil pressure Manifold pressure Fuel pressure Engine oil quantity Tachometer Warning F FLIGHT INSTRUMENT Bank and turn...

Страница 176: ...SSIGNED O In order to avoid confusion with the numeral zero the letter O shall not be used for circuit or cable identi fication P DC POWER Q FUEL AND OIL Fuel valves Fuel booster pump motor Moisture c...

Страница 177: ...devices U MISCELLANEOUS ELECTRONIC Electronic wiring for which no R S or T designation has been assigned by the procuring activity shall have the circuit function letter U assigned Examples of wiring...

Страница 178: ...1 18 Component Bridging 11 19 Connector Repair 11 20 Circuit Protection Device Repair 11 21 Bus Bars 11 22 Battery Repair BB 476 A 11 23 Damaged or Defective Power Relays 11 24 Substitute Emergency An...

Страница 179: ...use of wiring repair tools and materials 11 5 SPLICING UNSHIELDED WIRES GENERAL INFORMATION This procedure provides for repairing damaged unshielded wires WARNING Do not be misled by the term low vol...

Страница 180: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 2 Crimp Splice 11 8...

Страница 181: ...DAR action taken When mission is complete as soon as practical repair the equipment system using standard maintenance procedures OPTION 3 Split Bolt Splice Connectors LIMITATIONS Only to be used on wi...

Страница 182: ...equipment system using standard maintenance procedures OPTION 4 Twist Wire LIMITATIONS This is a temporary type repair PERSONNEL TIME 1 Soldier 10 Minutes MATERIALS TOOLS REQUIRED Tape Electrical ite...

Страница 183: ...flight only PERSONNEL TIME REQUIRED 1 Soldier 10 Minutes MATERIALS TOOLS REQUIRED Cylindrical metal casing such as ball point pen refills expended cartridges etc Insulation Sleeve or Tape item 10 Appx...

Страница 184: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 5 Replacement Section Twist Wire Repair Figure 11 6 Metal Casing Splice Repair 11 12...

Страница 185: ...erminal lugs together as shown in Figure 11 7 7 Slide the insulating sleeve over the splice so that the ends of the insu lating sleeve extend at least 3 4 of an inch beyond the ends of each terminal l...

Страница 186: ...e two wire ends together so that the strands interlink 7 Secure with screw clamp control cable clamp safety wire or other suitable means Figure 11 9 8 Insulate with tape or insulation sleeve 9 Record...

Страница 187: ...with nylon braid or some other means CAUTION Make sure aircraft power is off Disconnect battery before touching wires OPTION 1 Heat Shrinkable Repair Tape LIMITATIONS This is a temporary repair PERSON...

Страница 188: ...move damaged insulation and examine to insure center conductor is not damaged 2 Prepare a transparent sleeve of flexible tubing 1 1 2 times the outside diameter of the wire and 2 inches longer than th...

Страница 189: ...m pound over the exposed center conductor 3 Allow time to dry If compound coating does not seem to be sufficient apply additional layers as needed 4 Record BDAR action taken When mission is complete a...

Страница 190: ...et at 900 F Keep hot air away from shield sleeve 5 Center and shrink the shield over the splice area so that the solder melts and flows Shield sleeve braid must overlap cable braid at both ends Refer...

Страница 191: ...nt splice or by using one of the splicing procedures in paragraph 11 9 6 Push the free end of the grounding wire into the uncrimped grounding sheath connector Crimp securely Figure 11 15 7 If an insul...

Страница 192: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 15 Shielded Cable Repair 11 20...

Страница 193: ...cable TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Shielding must be long enough to overlap the shielding on both sides of the cable being repaired after the center conduc tor is repaired Shieldi...

Страница 194: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM PIGTAILS STEP A STEP B Figure 11 16 Pigtail Method Repair 11 22...

Страница 195: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 17 Substitute Shielded Braid Repair 11 23...

Страница 196: ...TIONS This is a temporary repair PERSONNEL TIME REQUIRED 1 Soldier 15 Minutes MATERIALS TOOLS REQUIRED Shield Terminator item 10 Appx B Reflector Heat Gun Heat Source Stripper or Knife Insulating Slee...

Страница 197: ...fe Insulating Sleeve item 10 Appx B PROCEDURAL STEPS 1 Prepare cable Figure 11 20 for repair Refer to 2 Position ground lead and shield ter minator as shown in Figure 11 21 3 Heat shield terminator un...

Страница 198: ...Record BDAR action taken When mission is complete as soon as practical repair the equipment system using standard maintenance procedures 11 13 TERMINAL LUGS GENERAL INFORMATION Terminal lugs are provi...

Страница 199: ...1 Self Clinching Cable Straps LIMITATIONS These straps are not to be used under the following conditions In temperature environments which exceed 85 C 185 F On coaxial cables or bundles con taining c...

Страница 200: ...all broken straps and strap ends that were cut off Figure 11 24 Self Clinching Cable Strap and Tool OPTION 2 Tie Tape LIMITATIONS 1 Do not use ties on that part of a wire group or bundle located insi...

Страница 201: ...tring can cut into or deform insulation 2 Space ties at 12 inches or less 3 Record BDAR action taken When mission is complete as soon as practical repair the equipment system using standard maintenanc...

Страница 202: ...URAL STEPS 1 Prepare coax cable Figure 11 26 Refer to Table 11 5 2 Slide shield sleeve inner sleeve and filler sleeve onto one of the coaxial cables in the given order 3 Splice the center conductor Us...

Страница 203: ...e area so that the solder melts and flows Figure 11 29 Shield sleeve must overlap coax braid at both ends Use same reflector and tem perature Keep hot air away from tubing 6 Center and shrink the tubi...

Страница 204: ...e 6 Record BDAR action taken When mission is complete as soon as practical repair the equipment system using standard maintenance procedures 11 19 COMPONENT BRIDGING GENERAL INFORMATION In most cases...

Страница 205: ...acement Pins Sockets item 2 Appx B Insertion Extraction Tool item 2 Appx B Knife PROCEDURAL STEPS 1 Solder or crimp wires to pin sockets Figure 11 33 2 Insert the pins sockets into the connector TM 55...

Страница 206: ...URAL STEPS 1 Obtain a replacement connector with a pigtail Replacement may be obtained from a crash damaged aircraft Cut pigtail so that splices can be staggered Figure 11 34 2 Remove damaged connecto...

Страница 207: ...DAR Repair LIMITATIONS None LIMITATIONS Emergency repair PERSONNEL TIME REQUIRED 1 Soldier 20 Minutes MATERIALS TOOLS REQUIRED Salvaged Circuit Breaker Electrical Tape item 49 Appx C PROCEDURAL STEPS...

Страница 208: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 35 Circuit Breakers 11 36...

Страница 209: ...e 11 37 Slip 1 inch piece of insulation over side Pull tight against the piece of insulation and twist tight Insulate bare end of terminal lugs on both sides of 1 inch piece of insulation with tape Us...

Страница 210: ...p around the repair and tie with string 6 Same lengthen repair procedure bus bars Figure can be used to 11 39 7 Record BDAR action taken When mission is complete as soon as practical repair the equipm...

Страница 211: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 39 Lengthening Bus Bars 11 39 Figure 11 38 Splicing Bus Bars...

Страница 212: ...dily injury and equip ment damage may result if any metal tools or parts accidentally cause a short circuit 4 To remove bad cells use a 3 8 inch socket or equivalent to loosen and remove terminal scre...

Страница 213: ...s Xl and X2 to the aircraft fuselage ground Figure 11 41 One of the two terminals should have 24 28 V dc on it when the power relay control circuit is energized No dc voltage indicates ELECTRICAL AND...

Страница 214: ...practical repair the equipment system using standard maintenance procedures OPTION 2 Creating a Jumper for Damaged Power Relays CAUTION Do not jumper battery relay on an aircraft This procedure is to...

Страница 215: ...NG PART DESIGNATION NUMBER FUNCTION K6 MS24183D1 Relay BATTERY K1 MS24183D1 Relay External Pwr K11 3S2791G200F 9 Relay Gen Fail K12 MS24183D1 Relay Line Cont K3 MS24183D1 Relay Non Ess Bus BT1 BB 4761...

Страница 216: ...tion contains expedient repair procedures to restore radio communication needed to complete the mission GENERAL INFORMATION These procedures give instructions for use of substitute and or construction...

Страница 217: ...tennas may also be used as emergency transmitting anten nas by using either coax cable 1 ARC 114 102A or 1 ARC 114 103A connected to J2 TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM 7 To replace No...

Страница 218: ...length of the required radiating element Remove the outer insulation and shield from the piece of coax cable and then strip a 1 inch piece of insulation from each end exposing the center conductor Fig...

Страница 219: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 45 Preparation of Coax 11 47...

Страница 220: ...e coax antenna by wrapping and twisting it around the plug where the coax was disconnected 9 Secure with tape to hold the antenna and coax in place inside the tail boom Replace the structural panel an...

Страница 221: ...TM 55 1520 228 BD ELECTRICAL AND AVIONICS SYSTEM Figure 11 47 Installation of Field Expedient Antenna 11 49 11 50 Blank...

Страница 222: ......

Страница 223: ...inches b Tubing in the OH 58 fuel system is limited to the fuel vent line When damage occurs to any of the lines tubes or hoses they may be substituted with a flexible type hose from the kit c If hos...

Страница 224: ...ADAPTER ON HELICOPTERS EQUIPPED WITH CLOSED CIRCUIT REFUELING PROVISIONS 1 Cover Assembly 2 Low Level Switch 3 Lower Transmitter 4 Fuel Pump 5 Fuel Shut Off Valve 6 Fuel Shut Off Cable 7 Fuel Shut Off...

Страница 225: ...TM 55 1520 228 BD FUEL SYSTEMS Table 12 1 Fuel System Assessment Procedures 12 3...

Страница 226: ...ch Knife PROCEDURAL STEPS 1 Defuel the fuel cell by the following procedure a Remove the fuel drain cover panel b Push or twist drain valve located under aircraft where fuel pump is located c Place a...

Страница 227: ...TM 55 1520 228 BD FUEL SYSTEMS Figure 12 2 Emergency Mechanical Clamp Repair 12 5...

Страница 228: ...Mix the adhesive as described below in steps 5a thru 5h refer to Figure 12 3 Wear goggles or other eye protec tion during all operations a Remove the tape band from Semkit cartridge and pull the mixi...

Страница 229: ...osition until the adhesive sufficiently sets approx 30 min NOTE Allow the adhesive to cure for two hours before refueling 9 Tighten drain valve and install cover plate 10 Refuel the aircraft 11 Record...

Страница 230: ...e rubber plug and insert it through the hole in the cell NOTE Retain cord to prevent loss of plug in the cell 9 Pull the plug into position and rotate it in position to smooth out the adhesive interfa...

Страница 231: ...TM 55 1520 228 BD FUEL SYSTEMS Figure 12 4 Rubber Repair Plug Assembly Figure 12 5 Plug Modification for Three Plane Repair 12 9 12 10 Blank...

Страница 232: ......

Страница 233: ...apa bilities Refer to Table 13 1 for assessment procedures a Force Trim System If the force trim system is malfunctioning the aircraft is still fully mission capable with no limitations presented b Co...

Страница 234: ...Figure 13 1 OH 58 Flight Controls Schematic 13 2 TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM...

Страница 235: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM Table 13 1 Flight Control System Assessment Procedures 13 3...

Страница 236: ...ize tubes Holes should go through the splicer and the damaged tube and should be positioned in a cross pattern Figure 13 7 Make sure that the original center to center length b Figure 13 6 is maintain...

Страница 237: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM Figure 13 2 Collective Flight Control 13 5...

Страница 238: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM Figure 13 3 Cyclic Flight Control 13 6...

Страница 239: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM Figure 13 4 Flight Control Actuators 13 7...

Страница 240: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM 13 8 NOTE THIS IS A CONFIGURATION OF THE OH 58A SERIES HELlCOPTER Figure 13 5 Anti Torque Controls Sheet 1 of 2...

Страница 241: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM NOTE THIS IS A CONFIGURATION OF THE OH 58C SERIES HELlCOPTER Figure 13 5 Anti Torque Controls Sheet 2 of 2 13 9...

Страница 242: ...TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM Refer to Figures 13 2 thru 13 5 Figure 13 6 Control Tube Dimensions Figure 13 7 Suggested Repair for Control Rods or Tubes 13 10...

Страница 243: ...206 001 020 67 206 001 020 69 206 001 020 59 206 001 020 29 206 001 020 33 206 001 096 25 206 001 021 13 1 1 3 8 2 1 3 8 3 4 3 4 3 4 5 8 5 8 1 1 8 1 1 8 1 7 8 7 8 15 16 1 15 16 9 16 9 16 1 1 16 1 1 1...

Страница 244: ...Figure 13 8 Control Rod with Bearing and Clevis Assemblies 13 12 TM 55 1520 228 BD FLIGHT CONTROLS SYSTEM...

Страница 245: ...BD FLIGHT CONTROLS SYSTEM Figure 13 9 Flattened End of Fabricated Flight Control Figure 13 10 Corner Rounding on Fabricated Flight Control Figure 13 11 Bearing Assembly Connection of Fabricated Flight...

Страница 246: ...termine the 6 Record BDAR action taken When correct distance between holes of the mission is complete as soon as flight tube Mark this distance Drill practical repair the equipment system the hole and...

Страница 247: ...ng repair options OPTION 1 Splice Repair LIMITATIONS None PERSONNEL TIME REQUIRED 1 Soldier 2 Hours MATERIALS TOOLS REQUIRED Flat or Round Piece of Material Example engine cowl hold open rod Drill wit...

Страница 248: ...TM 55 1520 228 BD UTILITY SYSTEMS Figure 14 1 Engine De Ice System 14 2...

Страница 249: ...the instrument panel in full view of the pilot WARNING If CO indicator is noted to be dark turn off heater pull fire wall shut off open vents and land as soon as practicable 15 3 ASSESSMENT PROCEDURE...

Страница 250: ...TM 55 1520 228 BD ENVIRONMENTAL CONTROL SYSTEM Figure 15 1 Bleed Air Heating and Ventilating System A C 15 2...

Страница 251: ...alve Plenum Remote Sensor Fresh Air Inlet Post Plenum Air Distribution Valves 11 12 13 14 15 16 17 18 20 Windshield Defog Nozzle Plenum Drain Plenum Valve Assembly Ventilating and Defogging Blower Ram...

Страница 252: ...Air Inlet 9 Center Post Duct 10 Air Distribution 11 Windshield Defog Nozzle 12 13 14 15 16 17 18 19 20 21 Plenum Drain Plenum Valve Assembly Ventilating and Defogging Blower Ram Air Intake Grill Air...

Страница 253: ...13 14 Combustion Heater Plenum Fuel Shut Off Valve Fuel Pump Fuel Pressure Relief Valve Fuel Filter Heater Combustion Blower Air Scoop Igniter Plug Duct Firewall Shut Off Control Temperature Control...

Страница 254: ...ng Valve 7 Firewall Shut Off Valve 8 Air Mixing Valve Control 9 Firewall Shut Off Valve 10 Control 11 Defogger Distribution Valves Cockpit Distribution Valves Cabin Distribution Valves Fan Air Intake...

Страница 255: ...TM 55 1520 228 BD ENVIRONMENTAL CONTROL SYSTEM Table 15 1 Assessment Procedures 15 7...

Страница 256: ...aintenance procedures LIMITATIONS Inspect after every flight 15 6 FLEXIBLE DUCT DAMAGE PERSONNEL TIME REQUIRED 1 Soldier 1 Hour MATERIALS TOOLS REQUIRED 0 016 inch Sheet Metal Minimum Sealant item 4 A...

Страница 257: ...e 0 042 inch item 27 Appx C PROCEDURAL STEPS 1 Locate damaged area and remove panels and other items as necessary to gain access to the line to be repaired Refer to Figure 15 6 for locations of bleed...

Страница 258: ...TM 55 1520 228 BD ENVIRONMENTAL CONTROL SYSTEM Figure 15 6 Bleed Air Line Installation 15 10...

Страница 259: ...TM 55 1520 228 BD ENVIRONMENTAL CONTROL SYSTEM Figure 15 7 Bleed Line Patch Repair 15 11 15 12 Blank...

Страница 260: ......

Страница 261: ...OR FOR TRAINING AT THE DISCRETION OF THE COMMANDER AUTHORIZED TRAINING FIXES ARE LISTED IN APPENDIX E IN EITHER CASE DAMAGES SHALL BE REPAIRED BY STANDARD PROCEDURES AS SOON AS PRACTICABLE There are n...

Страница 262: ......

Страница 263: ...IN COMBAT OR FOR TRAINING AT THE DISCRETION OF THE COMMANDER AUTHORIZED TRAINING FIXES ARE LISTED IN APPENDIX E IN EITHER CASE DAMAGES SHALL BE REPAIRED BY STANDARD PROCEDURES AS SOON AS PRACTICABLE...

Страница 264: ......

Страница 265: ...for use by repair personnel to accomplish the instructions set forth in this TM PUBLICATION NUMBER TITLE DA PAM 738 751 Functional User s Manual for the Army Mainte nance Management Systems Aviation...

Страница 266: ......

Страница 267: ...s spe and durable supplies not listed in other cial tools and test equipment Several appendices Each kit contains its own special tools are contained in the BDAR inventory list and tool usage instruc...

Страница 268: ...4920 01 266 7534 Fluid Line Repair Kit Special and 78286 Common Tools for Tubing and Hose 70700 20900 041 Repair Including Repair Parts 5 Not Assigned Fuel Cell Repair Kit 6 Not Assigned High Energy...

Страница 269: ...Expendable Items Except Medical Class V Repair Parts Heraldic Items or CTA 8 1OO C 2 EXPLANATION OF COLUMNS and a Item Number This number is assigned to the entry in the listing and is referenced in t...

Страница 270: ...4 33564 EA9340 Adhesive EX1675 B2 Pro Seal 890 B2 Adhesive General Purpose 81348 EC1300121 Adhesive Silicone Rubber 80244 MIL A 46106 Aliphatic Naphtha 81348 TTN95 Brush Stiff Fiber Bristle 80244 H B...

Страница 271: ...348 QQ W 423 Lockwire Steel 0 041 81348 QQ W 423 Lubricating Oil MIL L 2104 Grade 30 15958 Lubricating Oil MIL L 23699 81349 Lubricating Oil MIL L 7808 81349 Nut Assortment 81348 FFN836 Packing Prefor...

Страница 272: ...minal Quick Disconnect BX Wire Gage 16 14 MS27429 2 96906 58 5940 00 804 9185 Terminal Quick Disconnect BX Size 18 MS27429 1 96906 59 6810 00 664 0387 Trichloroethane 1 1 1 T 620 CN 81348 60 6515 00 3...

Страница 273: ...junction with specification numbers to distinguish them from foreign pro ducts The identification of NATO product numbers relate directly to U S Military Specification numbers and thus are considered...

Страница 274: ...06 00 206 4911 5306 00 141 4511 1005 00 832 4549 1005 00 921 6241 2925 00 444 1186 5310 00 807 1474 5310 00 844 4872 5310 00 807 1467 5310 00 807 1475 5310 00 807 1469 5340 00 921 5135 5305 00 X86 301...

Страница 275: ...x x x x x VERTICAL SPEED IND 6610 00 935 4278 x x x x x x VOLTMETER INDICATOR 6625 00 003 8745 x x x x x PRESSURE ALTIMETER 6610 00 110 3368 x x x x x x x x VERTICAL SPEED INDICATOR 6610 00 029 6703...

Страница 276: ...x x x x AN ARC 114 5821 00 935 5071 x x x x x RADIO SET AN ARC 115 5821 00 935 5072 x x x x x INVERTER 5841 01 140 0941 ELECTRICAL INDICATOR 6620 01 065 3740 x x x x x x HOT AIR MIXING VALVE 4810 01 0...

Страница 277: ...subcomponents of the major components may be removed and substituted however the level of disassembly must be consistent wlth the field tools and skill levels available D 5 Table D 2 Spare and Repair...

Страница 278: ...oint and cloud point b Some substitute fuels which alone cannot be used on the OH 58 helicopter can be blended with a primary fuel and can then be utilized for engine operation c When using substitute...

Страница 279: ...T 5624 JP 5 NATO F 44 Aviation Turbine ASTM D 1655 Jet B Aviation Turbine MIL T 83133 JP 8 NATO F 34 Aviation Turbine ASTM D 1655 Jet A 1 Fuels for JP 4 EXPEDIENT FUEL Kerosene ASTM D 3699 Kerosene N...

Страница 280: ...a AF Iss 3Amd 2 n a AF FRANCE AIR 3407 B AF AIR 3405 C n a AF FEDERAL REPUBLIC TL 9130 006 Iss 4 TL 9130 007 Iss 4 OF GERMANY n a AF n AF Grade JP 4 n AF ITALY AA M C 142p AA M C 143b AA M C 141d n a...

Страница 281: ...ing B P A T G B P A T K Caltex Petroleum Corp Caltex Jet B Caltex Jet A 1 City Service Co CITCO A Continental Oil Co Conoco JP 4 Conoco Jet 50 Conoco Jet 60 Exxon Co U S A Exxon Turbo Fuel B Exxon A E...

Страница 282: ...y Fuel Any Primary or Alternate Fuel Any Primary or Alternate Fuel Any Alternate or Primary Fuel Any Alternate Fuel Any Alternate Fuel MIL F 815 Distillate NATO F 76 Navy Distillate Dry Cleaning Solut...

Страница 283: ...term performance therefore they are recommended only as a last resort c Expedient lubricants can cause one of three problems 1 They may not allow proper efficient operations because of improper viscos...

Страница 284: ......

Страница 285: ...ct Hose Damage HYDRAULIC SYSTEM Lines and Hoses Aluminum Tube Damage Hydraulic Hose Damage ELECTRICAL AND AVIONICS SYSTEM Splicing Unshielded Wires Damaged Wire Insulation Shielded Cable Repair Shield...

Страница 286: ...AR FIXES AUTHORIZED FOR TRAINING Cont REPAIR PROCEDURE PARA NO FLIGHT CONTROL SYSTEM Tubes Flight Control 13 4 ENVIRONMENTAL CONTROL SYSTEM Rigid Plastic Ventilation Duct 15 5 Flexible Duct Damage 15...

Страница 287: ...n aid to expedient repair techniques described in Chapter 11 F 2 GENERAL The actual configura tions may vary depending on particular requirements or changes incorporated through modification work orde...

Страница 288: ...TM 55 1520 228 BD APPENDIX F Figure F 1 Intercom System Sheet 1 of 2 F 2...

Страница 289: ...gure F 1 Intercom System Sheet 2 of 2 Table F 1 Wiring WIRE NUMBER TYPE 1 C6533A 3A22 RED 1A22 GRN 45A22 1OA22 14A22 18A22 C6533B 3A22 RED 1A22 GRN 45A22 1OA22 14A22 18A22 C6533C 3A22 RED 1A22 GRN 45A...

Страница 290: ...TM 55 1520 228 BD APPENDIX F NOTE THIS UNIT IS A CONTROL PANEL ONLY IN AIRCRAFT USING AN ARC 51BX TRANSMITTER Figure F 2 UHF AM Communication System Sheet 1 of 2 F 4...

Страница 291: ...2 Wiring Table UHF AM Communication System WIRE NUMBER OH 58A ARC51 124A20 125A20 128A20 RED 129A20 BLK 131A20 140A ARC116 10A22 101A 101B SAME WIRING USED FOR AN ARC 164 OH 58C ARC116 1OB22 RED 11B22...

Страница 292: ...TM 55 1520 228 BD APPENDIX F Figure F 3 VHF AM Communication System and Connecting Cables Sheet 1 of 2 F 6...

Страница 293: ...lug Connector Electric Connector Electric Figure F 3 VHF AM Communication System and Connecting Cables Sheet 2 of 2 Table F 3 WIRE NUMBER OH 58A ARC115 1OA22 101A 101B ARC115 101C OH 58C ARC115 1OB22...

Страница 294: ...0 028 206 022 114 1 206 022 114 3 KC 59 212 KC 19 120 Filter Low Pass Board Capacitor A3 Radio Set No 1 FM Radio Set No 2 FM Control Indicator TSEC KY 28 Antenna No 2 FM Antenna R H No 1 FM Com Securi...

Страница 295: ...SHIELD SHIELD COAX COAX COAX COAX COAX PR S PR S COAX COAX Wiring Table VHF FM END 1 P209 B P209 J P209 K P209 L P209 T P209 U P209 V P209 c P209 d P209 e P21O P239 J242 P211 P212 P207 P208 P315 P209...

Страница 296: ...TM 55 1520 228 BD APPENDIX F Figure F 5 Gyromagnetic Compass Set AN ASN 43 and Connecting Cables Sheet 1 of 2 F 10...

Страница 297: ...agnetic Compass Set AN ASN 43 and Connecting Cables Sheet 2 of 2 Table F 5 Wiring WIRE NUMBER TYPE TN1705D22 10A22 BLU 11A22 GRN 12A22 YEL 13A22 14A22 15A22 20A22 BLU 21A22 GRN 22A22 YEL SHIELD TWT S...

Страница 298: ...TM 55 1520 228 BD APPENDIX F Figure F 6 Direction Finder Set AN ARN 89 Sheet 1 of 2 F 12...

Страница 299: ...ce Matching 206 032 310 3 Antenna Sense AS 2108 ARN 89 Antenna Loop Direction Finder Set AN ARN 89 Sheet 2 of 2 SHIELD SHIELD SHIELD COAX COAX COAX COAX SHIELD SHIELD SHIELD SHIELD COAX COAX COAX COAX...

Страница 300: ...TM 55 1520 228 BD APPENDIX F Figure F 7 Radio Receiving Set AN ARN 123 V 1 Sheet 1 of 2 F 14...

Страница 301: ...TWT S 33A22 WHT TWT S 33B22 SHIELD 33A22 BLU TWT S 34A22 BLU SHIELD 33C22 34A22 WHT TWT S 35A22 WHT PR S 35A22 BLU PR S 36A22 WHT PR S 36A22 BLU PR S 38A22 WHT PR S 38A22 BLU PR S 38B22 39A22 WHT PR S...

Страница 302: ...TM 55 1520 228 BD APPENDIX F Figure F 8 Radar Altimeter System AN APN 209 Sheet 1 of 2 F 16...

Страница 303: ...N18 Resistor Fixed Connector Plug Electric Connector Plug Connector Plug IND RCVR Transmitter Connector Plug Antenna Connector Plug Antenna Knob Control Radar Altimeter System AN APN 209 Sheet 2 of 2...

Страница 304: ...206 077 109 1 KIT 1A TSEC MT 3513 APX AT 884 APX MT 3809 APX 72 Test Set Transponder Receiver Transponder Control Transponder APX Transponder The APX 1OO V Used On The OH 58C Does Not Require The TS...

Страница 305: ...SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD SHIELD COAX COAX COAX COAX COAX COAX P234 SPLICE P234 P234 P234 P234 P234 P234 P...

Страница 306: ...APX1OO 5O2OA PR S PR S COAX COAX SHIELD COAX COAX COAX COAX Table IFF END 1 341OTR1P1 341OTR1P1 341OTR5P1 341OTR4P1 341OTR1P1 341OTR1P1 341OTR1P1 341OTR1P1 341OTR1P1 21 23 19 43 45 47 49 J600 J600 341...

Страница 307: ...2892 APR 39 V R 1838 APR 39 AS 2890 APR 39 V CM 440 APR 39 V C 9326 APR 39 V AS 2891 APR 39 V R 1838 APR 39 V Antenna Left Spiral Indicator Radar Signal Antenna Right Spiral Antenna Left Spiral Recei...

Страница 308: ...1P1 3422Z1P1 3422Z1P1 3422Z1P2 3422DS1P1 3422Z1P1 3422Z1P1 3422A1P1 TB20 TB20 3422Z1P1 3422RE1P3 3422RE2P3 3422RE2P4 3422RE1P4 3422Z1P2 3422Z1P1 3422RE1P5 3422RE2P5 3422A1P1 TB20 TB20 3422Z1P1 PIN 8 1...

Страница 309: ...ght Controls System Fuel Systems Hydraulic Power Plant Rotors Utility Systems Battery Repair BDAR Characteristics Bleed Air Line Damage Blending Fuels Bus Bars Cap or Longeron Damage Cap Skin Web Doub...

Страница 310: ...tion Environmental Control System Bleed Air Line Damage Flexible Duct Damage Rigid Plastic Ventilation Duct Flexible Duct Damage F Flight Controls System Subsystems and Assemblies Frame Bulkhead Skin...

Страница 311: ...4 Inches Diameter Maximum Manner of Blending Fuels N O Oil Hoses and Lines Leaks or Restriction Crimp Oil Lines Rigid Type Repair Oil Pressure Transmitter Leak 0il Tank Punctured Operating Characteri...

Страница 312: ...8 5 11 10 11 8 11 9 5 7 4 16 11 5 4 4 11 25 19 2 Shielded Cable Repair Segments Skid Damage Skin Stiffener Damage Splicinq Unshielded Wires Structural Damage Assessment and Repair Substitute Emergenc...

Страница 313: ...TM 55 1520 228 BD INDEX INDEX Cont Paragraph U V Waiver of Precautions Window Shield Window Damage 4 21 Wire Bundle Tie Wraps 11 14 Wire Repair Segments Unshielded Wires 11 6 XYZ INDEX 5 INDEX 6 Blan...

Страница 314: ......

Страница 315: ...and parts creates a component The actual fit between two or more mating parts with respect to the amount of clearance or interference between them A procedure to rapidly determine what is damaged whe...

Страница 316: ...metal structural elements Loss of metal resulting from overheating The smoothing of a metal surface by mechanical action without loss of material Generally found on plain bearing surfaces Surface dis...

Страница 317: ...materials which are consumed by usage or which have a one time usage in depot maintenance activity The inner layer of material used to construct honeycomb structural panels Surface chemical action wh...

Страница 318: ...ir technique A broad ridge or pair of ridges projecting from the edge of a structural element providing additional strength or a place for attachment FLAKING Loose particles of metal or evidence of se...

Страница 319: ...ed as a protective cover A cavity with smooth bottom or sides which can occur on rolling contact surfaces A critical examination of parts to determine their use fulness or condition The joining point...

Страница 320: ...nal Stock Identification Number NIIN A local break or notch in the edge of material Performance of a practical functional action A specific BDAR repair technique often non standard in nature The proce...

Страница 321: ...t or skin due to overstress hostile fire Very deep scratches caused by foreign particles between surfaces that are moving or between one moving and one stationary surface Scores follow the travel dire...

Страница 322: ...ent further propagation of the crack A longitudinal fore and aft structural element used in semimonocoque design which stiffens the skin Often called a stiffener As used herein the checking or operati...

Страница 323: ...ates Army Chief of Staff THOMAS F SIKORA Brigadier General United States Army The Adjutant General DISTRIBUTION To be distributed in accordance with DA Form 12 31 AVUM and AVIM Maintenance requirement...

Страница 324: ......

Страница 325: ...8 redstone army mil Subject DA Form 2028 1 From Joe Smith 2 Unit home 3 Address 4300 Park 4 City Hometown 5 St MO 6 Zip 77777 7 Date Sent 19 OCT 93 8 Pub no 55 2840 229 23 9 Pub Title TM 10 Publicatio...

Страница 326: ......

Страница 327: ...IONS EXCEPT RPSTL AND SC SM AND BLANK FORMS PUBLICATION FORM NUMBER TM 9 1005 433 24 DATE 16 Sep 2002 TITLE Organizational Direct Support And General Support Maintenance Manual for Machine Gun 50 Cali...

Страница 328: ...ISTS AND SUPPLY CATALOGS SUPPLY MANUALS PUBLICATION NUMBER DATE TITLE PAGE NO COLM NO LINE NO NATIONAL STOCK NUMBER REFERENCE NO FIGURE NO ITEM NO TOTAL NO OF MAJOR ITEMS SUPPORTED RECOMMENDED ACTION...

Страница 329: ...TION FORM NUMBER DATE TITLE ITEM NO PAGE NO PARA GRAPH LINE NO FIGURE NO TABLE NO RECOMMENDED CHANGES AND REASON Reference to line numbers within the paragraph or subparagraph TYPED NAME GRADE OR TITL...

Страница 330: ...NO OF MAJOR ITEMS SUPPORTED RECOMMENDED ACTION PART III REMARKS Any general remarks or recommendations or suggestions for improvement of publications and blank forms Additional blank sheets may be use...

Страница 331: ...yards square miles acres cubic feet cubic yards fluid ounces pints quarts gallons ounces pounds short tons pound feet pound inches To 1 cu centimeter 1000 cu millimeters 06 cu inch 1 cu decimeter 1000...

Страница 332: ...P I N 0 6 6 6 3 5 0 0 0...

Страница 333: ...it They did not even scan it Why should they get your money Why are not letting you give those free manuals to your friends I am setting this document FREE This document was made by the US Government...

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Bell OH-58 C, Техническое руководство

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