TM 55-2840-254-23
1-90 INSPECT ENGINE AFTER COMPRESSOR STALL (SURGE) (Continued)
1-90
(2) Inspect first stage compressor rotor
blades through inlet ducts for evidence
of erosion or foreign object damage (Ref.
(3) Determine that improper adjustment
or operation of interstage air-bleed
actuator and bleed band are not
causing surge (Ref. Task 1-47).
GO TO NEXT PAGE
1-306.1/(1-306.2 blank)
Change 4
