Israel Airworthiness Directives

75 ADs indexed for Israel aircraft.

Models

Various 19 ADs 1124 15 ADs 1121 14 ADs 1123 14 ADs 1124A 14 ADs 1121A 13 ADs 1121B 13 ADs Various 7 ADs Gulfstream G150 4 ADs Gulfstream 100 3 ADs Galaxy and Gulfstream 200 2 ADs 727-100 Series 1 AD A310-203 1 AD A310-204 1 AD A310-221 1 AD A310-222 1 AD A310-304 1 AD A310-322 1 AD A310-324 1 AD A310-325 1 AD Fluorescent lighting systems 1 AD AT-302 1 AD AT-400 1 AD BN-2 1 AD BN-2A 1 AD BN-2A-3 1 AD H.P. 137 Jetstream Mk. 1 1 AD Nord 262A Series 1 AD PA-60-600 (Aerostar 600) 1 AD PA-60-601 (Aerostar 601) 1 AD PA-60-601P (Aerostar 601P) 1 AD Auxiliary Power Units 1 AD BAC 1-11 200 Series 1 AD BAC 1-11 400 Series 1 AD DC-7 1 AD DC-7B 1 AD DC-7C 1 AD Mystere-Falcon 20 - C5 1 AD Mystere-Falcon 20 - D5 1 AD Mystere-Falcon 20 - E5 1 AD Mystere-Falcon 20 - F5 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 1 AD A300 B4-103 1 AD A300 B4-203 1 AD A300 B4-2C 1 AD A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 1 AD 525 1 AD 550 1 AD 560 1 AD Avro 146-RJ100A 1 AD BAe 146-200A 1 AD Falcon 10 1 AD Jetstream Model 4101 1 AD Mystere-Falcon 20 - C5 1 AD Mystere-Falcon 20 - D5 1 AD Mystere-Falcon 20 - E5 1 AD 172 1 AD 172A 1 AD 172B 1 AD 172C 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 407 1 AD 180 1 AD 182 1 AD 185 1 AD 188 1 AD 206 1 AD 207 1 AD 210 1 AD 310 1 AD 320 1 AD 340 1 AD 1121 1 AD 1121A 1 AD 1121B 1 AD 1123 1 AD 1124 1 AD 1124A 1 AD 1125 Westwind Astra 1 AD Astra SPX 1 AD 100 1 AD Astra SPX 1 AD G150 1 AD Galaxy and Gulfstream G150 1 AD 1124 1 AD 1124A 1 AD 1124 1 AD 1124A 1 AD 1125 Westwind Astra 1 AD 1121 1 AD 1121A 1 AD 1121B 1 AD 1329-23A 1 AD 1329-23D 1 AD 1329-23E 1 AD 1329-25 1 AD

Recent ADs

2025-24-10

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: Failure of the nose landing gear (NLG) actuator-to-strut attachment pin, part numbers 2247.0500.007 and 2247.0500.008, could result in failure of the NLG to retract and lock after takeoff or extend...

Effective: Jan 16, 2026 Category: aircraft Compliance: Within the compliance times specified in CAAI AD ISR I-32-25-01-7, unless already done.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2025-15-04

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: The unsafe condition, if not addressed, could result in failure of the nose landing gear (NLG) to retract and lock after takeoff or extend and lock before landing.

Effective: Sep 10, 2025 Category: aircraft Compliance: Within 3 months after the effective date of this AD, or at the applicable "discard" interval as s...

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2025-11-04

final rule

Airworthiness Directives; Israel Aircraft Industries Ltd. Airplanes

Unsafe Condition: deployment of a thrust reverser in flight or before landing, which could result in loss of control of the airplane.

Effective: Jun 23, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Israel Aircraft Industries Ltd. Airplanes

2023-06-09

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: flap fairing debonding and moisture intrusion that might lead to lower wing skin corrosion and cracking on both wings, and reduced structural integrity of the wings.

Effective: May 18, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2022-21-16

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: wing flap fairing debonding and corrosion were discovered at lower skin of rib 3 and rib 11 on both wings

Effective: Dec 21, 2022 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2019-03-13

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: corrosion in the solder joints of the upper and lower front relay box connectors to the printed circuit board

Effective: Apr 8, 2019 Category: aircraft Compliance: Within 36 months after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2017-21-04

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: The main entrance door (MED) opened during flight, and the 'CABIN DOOR UNLOCK' crew alerting system (CAS) message may extinguish before the handle latch pin is fully engaged.

Effective: Nov 27, 2017 Category: aircraft Compliance: Within 12 months after the effective date of this AD.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2017-21-03

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: The main entrance door (MED) opened during flight, and the 'CABIN DOOR UNLOCK' crew alerting system (CAS) message may extinguish before the handle latch pin is fully engaged.

Effective: Nov 27, 2017 Category: aircraft Compliance: Within 12 months after the effective date of this AD.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2014-15-19

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: Use of published, non-conservative data in the AFM could result in the inability to meet required takeoff performance, leading to a hazard during performance-limited takeoff operations.

Effective: Oct 14, 2014 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2013-14-10

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: Incomplete closure of the main entry door (MED), which may result in the door opening in flight and possible separation of the door, causing damage to the airplane structure and left engine by flyi...

Effective: Sep 10, 2013 Category: aircraft Compliance: Within 250 flight hours after June 25, 2010.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2013-03-23

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: The runway slope and anti-ice corrections to V1 and take-off distances in the Gulfstream G150 Airplane Flight Manual (AFM) were presented in a non-conservative manner, which could result in the ina...

Effective: Mar 26, 2013 Category: aircraft Compliance: Within 60 days after the effective date of this AD (March 26, 2013).

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2012-15-06

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: Sponge rubber padding was found between wheel well fuel lines and electrical harnesses, which is not approved and can cause corrosion of the fuel lines. This could result in fuel leakage and possib...

Effective: Sep 4, 2012 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2012-13-51

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: An inboard vent tube hole was completely covered with sealant, which blocked airflow through the vent. Under these conditions, the rise of internal pressure during pressure fueling or due to therma...

Effective: Aug 13, 2012 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

2011-23-07

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Unsafe Condition: A broken aileron servo actuator centering spring rod was discovered on a model G100 aircraft. This latent failure, if not detected and corrected, in conjunction with the disconnection of the normal...

Effective: Dec 15, 2011 Category: aircraft Compliance: Within 12 months after the effective date of this AD.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2010-20-04

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Galaxy and Gulfstream 200 Airplanes

Unsafe Condition: Extension of airbrakes above 360 KIAS/0.79 M<INF>i</INF> results in aerodynamic driven vibration of the airbrake, leading to high cycle fatigue failure of the airbrake in-board hinge, which can res...

Effective: Oct 28, 2010 Category: aircraft Compliance: Within 60 days after the effective date of this AD.

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Galaxy and Gulfstream 200 Airplanes

2010-11-02

final rule

Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Unsafe Condition: Incomplete closure of the Main Entry Door (MED) may be followed by in-flight opening of the door. As a result, the MED and the adjacent fuselage structure may be damaged during opening and landing ...

Effective: Jun 25, 2010 Category: aircraft Compliance: Within 10 days after February 15, 2007 (the effective date of AD 2007-03-05).

Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream 100 Airplanes, and Model Astra SPX and 1125 Westwind Astra Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2006-16-18 R1

final rule

Airworthiness Directives; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/ RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

Unsafe Condition: A bearing error in the Sandel Avionics Incorporated Model ST3400 TAWS/RMI unit configured to receive bearing information from a VOR receiver interface via a composite video signal, due to a combina...

Effective: Jul 18, 2008 Category: appliance Compliance: Effective July 18, 2008

Why matched: Airworthiness Directives; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/ RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes

2005-18-20

final rule

Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.

Effective: Oct 14, 2005 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-18-13

final rule

Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1124 and 1124A Airplanes

Unsafe Condition: Chafing of the electrical bundles in the overhead circuit breaker panel, which could result in a short circuit and consequent fire and smoke in the airplane.

Effective: Sep 22, 2005 Category: aircraft Compliance: Within 60 days

Why matched: Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1124 and 1124A Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2004-14-14

final rule

Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes

Unsafe Condition: Cracking of the skins of the rudder assembly, which could result in reduced structural capability of the rudder and reduced controllability of the airplane.

Effective: Aug 13, 2004 Category: aircraft Compliance: Within 50 flight hours after the effective date

Why matched: Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

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