88-15-6 |
Cessna |
Tie battery-to-battery contactor cable to battery box cover lock pin | 150A thru M |
88-15-2 |
Aerospatiale |
Replace main rotor head spindles before 4500 hours TIS | SA330 |
88-14-1 |
Lyc Eng |
Supersedes 87-26-10 | amends ADs 86-22-8, 87-10-10 & 87-12-11 | inspect & maintain engine lubrication sys & number 3 & 4 bearings | LTS101 |
88-13-8 |
Partenavia |
Inspect & replace engine mounting brackets | P68, B, C, TC Observer |
88-13-6 |
Falcon |
Modify main landing gear release mechanism | Falcon Jet |
88-13-3 |
Cessna |
Supersedes 86-1-2 | inspect/repair landing gear torque links | S550(SN-1 thru -79) |
88-13-11 |
deHavilland |
Supeseded by 94-8-10 |
88-13-1 |
Mitsubishi |
Standardize, verify disconnection & change limitation in the AFM of autopilot/manual electric pitch trim system disconnect-interrupt push button | MU-2B,-10,-15, -20, -25, -26, -26A, -30, -35, -36, -36A, -40, -60 |
88-12-3 |
Bell |
Inspect main rotor drag brace assembly for corrosion & cracks | 214ST |
88-12-2 |
Schweizer |
Remove tail rotor retention strap assemblies with 3540 hours or more | 269C |
88-12-12 |
Cessna |
Install control to acutate fuel strainer quick drain | 177RG |
88-12-11 |
Aerospatiale |
Supersedes 73-13-2 | inspect freewheel coupling & seal for oil leak | SA315B; SA3160; SA316B,-C; SA3180,-B,-C; SA319B |
88-12-10 |
Garrett |
Reduce 2nd stage turbine rotor from 6800 to 4800 cycles | TPE331-10,-10R,-10U,-10UF,-10UG,-10UGR,-10UR & -11U |
88-11-7 |
Cessna |
Inspect flap panels' inboard lower surface to verify 3 unobstructed holes | S550 |
88-11-6 |
Enstrom |
Supersedes 72-4-4 | inspect, repair/replace horiz. stabilizer spar & attach. | F28 |
88-10-4 |
MDHC |
Superseded by 98-9-2 |
88-10-1 |
Beech |
Replace fuel boost pump w/improved unit | A23-24; A24,-R; B24R; C24R |
88-1-12 |
BAe |
Inspect & repair plumbing near ventral fuel tank | 125-800 |
88-1-1 |
BAe |
Move 115V AC stall vane heater circuit breakers;alter EFIS power cable | 125-800 |
87-9-2 |
Bell |
Revised 4/87 | Inspect spline plate | 222 |