GA 8 Airvan (Pty) Ltd Airworthiness Directives

234 ADs indexed for GA 8 Airvan (Pty) Ltd aircraft.

Models

GA8 9 ADs GA8-TC320 7 ADs M-100 S 2 ADs M-200 2 ADs A300 B4-601 2 ADs A300 B4-603 2 ADs A300 B4-605R 2 ADs M-100 S 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD AEIO-320-D1B 1 AD AEIO-320-D2B 1 AD AEIO-320-E1A 1 AD AEIO-320-E1B 1 AD AEIO-320-E2A 1 AD AEIO-320-E2B 1 AD AEIO-360-B1B 1 AD AEIO-360-B1D 1 AD AEIO-360-B1F 1 AD AEIO-360-B1F6 1 AD 737-100 Series 1 AD 737-200 Series 1 AD 737-200C Series 1 AD A320-111 1 AD A320-211 1 AD A320-212 1 AD A320-214 1 AD A320-231 1 AD A320-232 1 AD A320-233 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 B4-620 1 AD A300 B4-622 1 AD A300 B4-622R 1 AD A300 C4-605R Variant F 1 AD A300 F4-605R 1 AD A300 F4-622R 1 AD A310-203 1 AD 480 1 AD D-16 1 AD D-16A 1 AD Navion (Army L-17A) 1 AD Navion A (Army L-17B and L-17C) 1 AD Navion B 1 AD Navion D 1 AD Navion E 1 AD Navion F 1 AD Navion G 1 AD Navion H 1 AD 150G 1 AD 172H (USAF T-41A) 1 AD 180H 1 AD 182J 1 AD 182K 1 AD 185E 1 AD 188 1 AD 206A 1 AD 210F 1 AD 210G 1 AD 182T 1 AD 206H 1 AD DA 40 1 AD DA 40F 1 AD LC40-550FG 1 AD LC41-550FG 1 AD LC42-550FG 1 AD Servo gearbox units 1 AD T182T 1 AD T206H 1 AD Engine Gage Units 1 AD 8 1 AD 8 Airvan (Pty) Ltd 1 AD GA200 1 AD GA200C 1 AD GA8 1 AD GA8-TC320 1 AD 328-100 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD GTX 33 1 AD GTX 330 1 AD GTX 330D 1 AD GTX 33D 1 AD GPS Navigation Units 1 AD GMN-00962 GTS 825 1 AD GTS 8000 1 AD GTS 855 1 AD 112B 1 AD 112TC 1 AD 112TCA 1 AD 114 1 AD 114A 1 AD 114B 1 AD 114TC 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 172I 1 AD 172K 1 AD 172L 1 AD 172M 1 AD 172N 1 AD 172P 1 AD 172Q 1 AD 172R 1 AD 172RG 1 AD 172S 1 AD 177B 1 AD 177RG 1 AD 182E 1 AD 182F 1 AD 182G 1 AD 182H 1 AD 182J 1 AD 182K 1 AD 182L 1 AD 182M 1 AD 182N 1 AD 182P 1 AD 182Q 1 AD 182R 1 AD 182S 1 AD 182T 1 AD 19A 1 AD 206H 1 AD 210D 1 AD 210E 1 AD 210F 1 AD 210G 1 AD 210H 1 AD 210J 1 AD 210K 1 AD 210L 1 AD 210M 1 AD 210N 1 AD 35-33 1 AD 35-A33 1 AD 35-B33 1 AD 35-C33 1 AD 35-C33A 1 AD 36 1 AD A23-19 1 AD A23-24 1 AD A23A 1 AD A24 1 AD A24R 1 AD A36 1 AD A36TC 1 AD B19 1 AD B23 1 AD B24R 1 AD B36TC 1 AD C23 1 AD C24R 1 AD C35 1 AD D35 1 AD E33 1 AD E33A 1 AD E33C 1 AD E35 1 AD F172E 1 AD F172F 1 AD F172G 1 AD F172H 1 AD F172K 1 AD F172L 1 AD F172M 1 AD F172N 1 AD F172P 1 AD F177RG 1 AD F182P 1 AD F182Q 1 AD F33 1 AD F33A 1 AD F33C 1 AD F35 1 AD FR172K 1 AD FR182 1 AD G33 1 AD G35 1 AD GFC 500 1 AD H35 1 AD J35 1 AD K35 1 AD M19A 1 AD M20C 1 AD M20D 1 AD M20E 1 AD M20F 1 AD M20G 1 AD M20J 1 AD M20K 1 AD M20M 1 AD M20R 1 AD M20S 1 AD M35 1 AD N35 1 AD P172D 1 AD P206C 1 AD P206D 1 AD P206E 1 AD P35 1 AD PA-24 1 AD PA-24-250 1 AD PA-24-260 1 AD PA-28-140 1 AD PA-28-150 1 AD PA-28-151 1 AD PA-28-160 1 AD PA-28-161 1 AD PA-28-180 1 AD PA-28-181 1 AD PA-28-201T 1 AD PA-28-235 1 AD PA-28-236 1 AD PA-28R-180 1 AD PA-28R-200 1 AD PA-28R-201 1 AD PA-28R-201T 1 AD PA-28RT-201 1 AD PA-28RT-201T 1 AD PA-30 1 AD PA-32-260 1 AD PA-32-300 1 AD PA-32-301 1 AD PA-32-301FT 1 AD PA-32-301T 1 AD PA-32-301XTC 1 AD PA-32R-300 1 AD PA-32R-301 (HP) 1 AD PA-32R-301 (SP) 1 AD PA-32R-301T 1 AD PA-32RT-300 1 AD PA-32RT-300T 1 AD PA-39 1 AD R172K 1 AD R182 1 AD S35 1 AD T182 1 AD T182T 1 AD T206H 1 AD T210F 1 AD T210G 1 AD T210H 1 AD T210J 1 AD T210K 1 AD T210L 1 AD T210M 1 AD T210N 1 AD TB 20 1 AD TB 21 1 AD TP206C 1 AD TP206D 1 AD TP206E 1 AD TR182 1 AD TU206C 1 AD TU206D 1 AD TU206E 1 AD TU206F 1 AD TU206G 1 AD U206C 1 AD U206D 1 AD U206E 1 AD U206F 1 AD U206G 1 AD V35 1 AD V35A 1 AD V35B 1 AD Emergency Locator Transmitter 1 AD Auxiliary Power Units 1 AD 305A 1 AD 707-100 Long Body 1 AD 707-100B Long Body 1 AD 707-100B Short Body 1 AD 707-200 1 AD 707-300 Series 1 AD 707-300B Series 1 AD 707-300C Series 1 AD 707-400 Series 1 AD 727-100 Series 1 AD 727-100C Series 1 AD D.H.82A Tiger Moth 1 AD D.H.83 Fox Moth 1 AD DH 82A 1 AD D.H.82A Tiger Moth 1 AD D.H.83 Fox Moth 1 AD DH 82A 1 AD

Recent ADs

2024-14-03

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: an un-commanded automatic pitch trim runaway when the autopilot was first engaged, which could result in un-commanded automatic pitch trim runaway and loss of control of the airplane.

Effective: Aug 20, 2024 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; Various Airplanes

2024-08-09

final rule

Airworthiness Directives; GA8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: insufficient electrical bonding of the solenoid (relay) box assembly that could result in degraded performance, errors, or intermittent failures of equipment connected to electrical Bus 1, Bus 2, a...

Effective: Jul 16, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; GA8 Airvan (Pty) Ltd Airplanes

2024-07-07

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: excessive wear in the forward slide of the cargo door may result in the cargo door separating from the airplane in flight with potentially catastrophic results

Effective: Jun 3, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

2023-21-05

final rule

Airworthiness Directives; Thales AVS France SAS Flight Management Computer Navigation Modules

Unsafe Condition: Due to software issues, certain FMC2 NAVM navigation modules provide erroneous data to the flight management computer, compromising safe flight of the airplane.

Effective: Dec 12, 2023 Category: aircraft Compliance: Within 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Thales AVS France SAS Flight Management Computer Navigation Modules

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2021-08-15

final rule

Airworthiness Directives; Garmin International GMN-00962 GTS Processor Units

Unsafe Condition: The GTS Processor software potentially calculates incorrect range rates, resulting in traffic advisories or RAs being generated when targets are greater than 10 nautical miles (NM) away. This can l...

Effective: May 17, 2021 Category: aircraft Compliance: Within 24 months of the effective date

Why matched: Airworthiness Directives; Garmin International GMN-00962 GTS Processor Units

2020-17-09

final rule

Airworthiness Directives; GA8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: A design change to the fuselage strut pick up ribs No. 5 and 6 that requires a reduced life limit.

Effective: Sep 29, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; GA8 Airvan (Pty) Ltd Airplanes

2019-07-08

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: A manufacturing quality escape has resulted in wing strut fittings in the effective serial number range to be manufactured with incorrect grain orientation. The fatigue implications of the incorrec...

Effective: May 23, 2019 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

2018-05-08

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: The fuel system integral sump tank does not meet FAA regulations due to inadequate ventilation and drainage.

Effective: Apr 12, 2018 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2016-07-02

final rule

Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Unsafe Condition: Certain interstage turbine transition (ITT) ducts failing to meet containment capability requirements.

Effective: May 5, 2016 Category: engine Compliance: Within 2,600 hours time-in-service after the effective date of this AD.

Why matched: Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2015-27438

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: Omission of engine mount fire seal washers during assembly, which could reduce engine retention capability in the event of a fire.

Effective: Dec 3, 2015 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2015-06-02 R2

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: The omission of steel washers at each isolator mount location could reduce the engine retention capability in the event of a fire.

Effective: Dec 3, 2015 Category: aircraft Compliance: before further flight (AD 2015-06-02 R2)

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

2015-17193

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: Missing required engine mount fire seal washers, which could reduce the engine retention capability in the event of a fire.

Effective: Aug 20, 2015 Category: engine Compliance: Within 300 hours time-in-service after April 24, 2015, or within 12 months after April 24, 2015, ...

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2015-06-02

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: Missing required engine mount fire seal washers, which could reduce the engine retention capability in the event of a fire.

Effective: Apr 24, 2015 Category: engine Compliance: Within 300 hours time-in-service or 12 months after April 24, 2015, whichever occurs first.

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2014-24-01 Recurring

final rule

Airworthiness Directives; Various de Havilland Airplanes

Unsafe Condition: Structural failure of the attachment of the wing to the fuselage that resulted from failed lateral fuselage tie rods.

Effective: Jan 6, 2015 Category: aircraft Compliance: Within the compliance times specified in the AD, unless already done.

Why matched: Airworthiness Directives; Various de Havilland Airplanes

2014-17-09

final rule

Airworthiness Directives; Various de Havilland Airplanes

Unsafe Condition: Structural failure of the attachment of the wing to the fuselage resulting from failed lateral fuselage tie rods.

Effective: Sep 18, 2014 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various de Havilland Airplanes

2014-12-52

final rule

Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

Unsafe Condition: Reports of LPT2 blade separations indicate the presence of casting anomalies at or near the root of the LPT2 blade, which could result in LPT2 blade failure, multiple engine in-flight shutdowns, an...

Effective: Jul 28, 2014 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc., Garrett Turbine Engine Company) Turbofan Engines

2013-19-12

final rule

Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Unsafe Condition: The fuel system integral sump tank does not meet FAA regulations, as the compartments adjacent to the Mk II sump tank are not suitably ventilated and drained to prevent the accumulation of flammabl...

Effective: Oct 15, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Amdt-39-17294

final rule

Airworthiness Directives; GA200 (Pty) Ltd Airplanes

Unsafe Condition: Failure of the wing strut bolt through the main spar.

Effective: Jan 31, 2013 Category: aircraft Compliance: Within 10 hours time-in-service after September 14, 2012, for the initial inspection. Repetitive ...

Why matched: Airworthiness Directives; GA200 (Pty) Ltd Airplanes

2012-18-10 R1

final rule

Airworthiness Directives; GA200 (Pty) Ltd Airplanes

Unsafe Condition: Failure of the wing strut bolt through the main spar, which may result in wing structural failure.

Effective: Jan 31, 2013 Category: aircraft Compliance: Initial inspection within 10 hours time-in-service, and repetitive inspections at intervals of 50...

Why matched: Airworthiness Directives; GA200 (Pty) Ltd Airplanes

View all GA 8 Airvan (Pty) Ltd ADs →