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Airworthiness Directives

NOTE - This AD note listing is intended as a guide only and should not be relied upon as conclusive evidence of AD applicability on any particular aircraft. Entire Airworthiness Directives may be accessed at:

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AD No. MAKE Condensed description of ad note
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11-1-53 Piaggio Superseded by 11-9-51
11-1-52 Schweizer Superseded by 11-12-16
11-1-51 Piaggio Superseded by 11-1-53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

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