| 11-10-13 |
Diamond |
AD to prevent in-flight loss of rear passenger door, see AD | DA-42 |
| 11-10-12 |
Eurocopter |
Replace the cup springs and fan nut, functionally testing the damping system as specified | AS350B, B1, B2, B3, BA, EC130 B4 |
| 11-10-1 |
Dassault |
Perform a functional test of the RAT heater using an approved method as specified | Falcon 7X |
| 11-1-53 |
Piaggio |
Superseded by 11-9-51 |
| 11-1-52 |
Schweizer |
Superseded by 11-12-16 |
| 11-1-51 |
Piaggio |
Superseded by 11-1-53 |
| 11-1-4 |
Embraer |
Install clamps and protection sleeves to harness W101 in cockpit area as specified | Phenom 100 |
| 11-1-10 |
Bombardier |
Relocate the No.2 and No.3 hydraulic system lines in the wing auxiliary spar area on the left side of the aircraft as specified | BD-700-1A10 / -1A11 |
| 11-1-1 |
Embraer |
Supersedes 08-13-15 | Revise the ALS of the ICA to incorporate section A2.5.2, Fuel Systems Limitations Items, of apendix 2 of the MPG as specified | EMB-135BJ |
| 10-9-9 |
Piaggio |
Incorporate Temporary Revisions No. 31 and 41 into the AFM as specified | P-180 Avanti II |
| 10-9-8 |
GE Engines |
For engines with an AFT Technologies combustion liner, please see AD | CJ610 and CF700 series |
| 10-9-4 |
Honeywell Avionics |
Results from discovery of software anomalies which can cause faulty FMS navigation, see AD | Primus EPIC and APEX FMS |
| 10-9-1 |
Eurocopter |
Disconnnect the ground wire for the hosit squib wiring and test the hoist system to assure that the squib can be electrically fired | AS350 and 355 series |
| 10-7-7 |
Socata |
Remove the foam from the towing bar stowage box following Socata's Mandatory Service Bulletins | TBM 700 |
| 10-7-6 |
Bombardier |
Insert Bombardier temporary revision TR-39 in the AFM | Challenger 300 |
| 10-7-2 |
Honeywell |
Supersedes 06-22-5 | Inspect Primus II RNZ-850/851 integrated navigation unit (INU) as specified | various aircraft |
| 10-6-8 |
Sikorsky |
Inspect the flotation system connector and if a metallic foil shunt is found, remove it as specified | S-76 |
| 10-6-7 |
Eurocopter |
Inspect for nonconformity of the servo-control cap, P/N 800137, replace as specified | multiple models |
| 10-6-3 |
Eurocopter |
Intended to remove non-conforming drive shafts from service and prevent failure of the drive shaft, see AD | AS355 series |
| 10-6-2 |
Beechcraft |
Detect and correct inadequate clearance of the brake reservoir tubing and the heater fuel pump wiring to avoid chafing and or fire | G58 |
