RIGHT SIDE - FUSELAGE AND LANDING GEAR
Cabin doors for general condition, and proper operation of vent and
door latching and locking mechanism.
Door hinge pins properly installed and secured.
Exterior of fuselage skin, rivets, fasteners and structure for damage
and security. No evidence of buckling noted.
Landing gear for condition of skid tubes and fairings.
Forward and rear landing gear damper for condition, by observing
stance of helicopter. Visually check damper for leakage; replace
damper if leakage is obvious, or if extension is unusual.
Passenger steps secure and free from damage.
Pylon clean and free from damage.
No evidence of oil leakage around fuselage drain hole.
Engine exhaust duct secure, free from cracks or distortion.
Scavenge oil filter for extended bypass indicator.
Right hand static port free of obstruction.
Access, inspection and compartment panels/covers for secure
closure.
AFT FUSELAGE
CAUTION
The following special check applies to 269D3300-1 Aft
Fuselage Assemblies only. S/N 63 & subsequent are factory
equipped with the 269D3300-35 aft fusealage assembly, and do
not require that the following check be conducted. Cracks in
the paint film alone may indicate internal structure damage
and this requires further maintenance action before further
flight.
Handling, Servicing & Maint.
Pilot's Flight Manual
Schweizer RSG, LLC.
Model
269D
Helicopter
7-4
Reissued:
16
Jan 2019
Book 3.indd 166
8/4/19 1:25 PM
