Engine
(JT8-D)
(Online AD's at the end)
Updated
to 07 Oct 2001
70-02-02 - Sixth stage compr. rotor disc
70-11-03 - Sixth stage blade failures
70-25-08 - Seventh stage compr. rotor disc
70-26-05 - First stage compr. rotor blades
71-07-01 - Front Compressor Front Hub
71-25-07 - Fuel nozzle support assemblies
75-01-01 - Low turbine shaft spline
75-05-06 - Fuel manifolds
76-12-06 - Second stage fan blade pin
76-20-02 - Second stage fan blades
76-24-01 - Eight stage compressor disk
77-03-06 - Front compressor front hubs
77-07-11 - Intermix. of different stators
77-16-12 - low turbine shaft
78-17-02 R3 - Cracks in compressor front hubs
78-23-12 - Turbine blade retention rivets
80-15-51 - JT8D Series engines
81-08-02 R2 - Disk failure
85-19-51 R1 - Second stage turbine disk
86-02-52 R1 - Combustion chamber failure
86-08-04 R1 - Removable sleeve spacers
86-09-02 R2 - Combustion chamber liners
87-11-07 R1 - Combustion chamber case rupture
87-14-01 R1 - Second stage fan blade failure
89-05-52 - Combustion chamber case rupture
89-24-02 - Second stage fan disk fracture
89-25-11 - First stg. fan blade liberation
91-24-14 - No 4-1/2 bearing seal spacer
92-10-05 - Third stage outer airseal
94-14-16 - Fuel nozzle leakage
94-20-08 - Turbine blade or shaft
94-20-09 - Turbine blade or shaft
94-25-07 - Combustion chamber case
95-02-16 - Fuel nozzle leakage
95-26-03 - Compressor disc failure
97-19-14 - Turbine blade or shaft
99-01-08 - Prevent the failure of a high-pressure compressor disk
99-12-03 - Engine part failure
2000-21-08 Critical Life Limited
Parts
2000-22-06
Loss of Engine Throttle Control
2001-15-18
Rupture 2nd Stg Compressor Disk By P/N and S/N
