MD Helicopters 369 Series, Manual

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CSP−HMI−2
MD Helicopters, Inc
.
MAINTENANCE MANUAL
Page 2
Revision 39
05−20−00
Form HOE005 (Rev 5/04)
Table 1. 100 − Hour or Annual Inspection (Cont.)
Registration No. Serial No.
Helicopter Hours Torque Events
Model Initial Chap/Sect Requirement
ALL Fuselage upper surfaces for:
*
Damage and condition.
* Mast base drain holes clean and free of debris (blow air thru holes to
ensure no clogging).
*
Engine air inlet fairing free from damage. No delamination noted. Bypass
door operationally checked. Seals free from damage.
*
Engine air bypass door operationally checked. Seals free from damage.
Cable system checked for smooth operation.
*
Engine access doors for proper operation of latches and closure,
distortion, damage, cracks and security.
52
53
71
52
ALL Fuselage for:
*
Damage and condition.
* Compartment fresh air vents in doors and front of canopy for easy of
operation and security.
*
Fuel cell vent fairings free of obstructions and obvious damage.
* Pilot’s and passenger/cargo compartment doors for condition of door
glass, vents and proper operation of latching and locking mechanisms.
*
Door hinges and pins for play or wear. Ensure door pin locking tab is
engaged with slot in frame.
*
No evidence of oil leakage around fuselage drain holes.
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369D/E/FF Sta. 142.0 tail rotor control bellcrank support for cracking or damage, use
bright light and mirror (Ref. Upper Fuselage and Tailboom Control Linkage
Inspection).
67 − 20 − 10
500/600N Anti − torque fan inlet for:
* Screen for cleanliness and damage.
* Attaching hardware for security.
* Interior of fan inlet for cleanliness and damage.
* Driveshaft cover for damage.
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ALL * Check for no gap between tailboom and fuselage at attach points.
* Check tailboom skin around stabilizer fittings for cracks.
* Tailboom attachment − to − fuselage for security, evidence of corrosion or
cracks, loose rivets or buckling.
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