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 condition
CHECK
Chip detector 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
W I T H H M I A P P E N D I X C , P R I O R T O F U R T H E R
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
Reissued:
16
Jan 2019
FAA Approved
Book 3.indd 94
8/4/19 1:25 PM
