AFT FUSELAGE/TAIL ROTOR (cont)
Fuselage area above horizontal stabilizer
for cracks in paint film. Pay particular
attention to flange bend radius and vertical
face of aft bulkhead and entire adjacent aft
fuselage skin. Any signs of cracks requires
further inspection before next flight.
CHECK
Stabilizers right hand side (vertical,
horizontal and end plates)
CHECK, NO
DAMAGE ALLOWED
Tail skid CHECK
Tail rotor alignment marks CHECK
Tail rotor gearbox to aft fuselage
attachment for security and co ndition
CHECK
Chip de tector and wiring CHECK
Control push-pull rod and bellcrank CHECK
Tail rotor transmission oil level CHECK
Output shaft dust cover, retainer nut, tang
washer, and rubber bumper
CHECK
Tail rotor blades and pitch links CHECK
Tail rotor abrasion strip CHECK
CAUTION
IF POOR ABRASION STRIP BOND IS SUSPECTED, BUT
NOT CONFIRMED, INSPECT BLADE IN ACCORDANCE
WITH HMI A PPENDIX C, PRIOR TO FURTHER
OPERATION.
Visually check each tail rotor blade abrasion strip for any evidence
of paint cracking or chipping along the abrasion strip/airfoil bond
line.
Normal Procedures
Pilot's Flight Manual
Schweizer RSG, LLC.
Model 269D Helicopter
4-6
R
eissued: 16 Jan 2019
FAA Approved
Book 3.indd 94 8/4/19 1:25 PM
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