Short Brothers PLC Airworthiness Directives

130 ADs indexed for Short Brothers PLC aircraft.

Models

SD3-60 62 ADs SD3-30 60 ADs SD3-SHERPA 28 ADs SD3-60 SHERPA 27 ADs SC-7 Skyvan Series 3 14 ADs SC-7 Skyvan Series 2 4 ADs 727 Series 1 AD 727-100 Series 1 AD 727-100C Series 1 AD 727-200 Series 1 AD 727-200F Series 1 AD 727C Series 1 AD 747-100 Series 1 AD 747-100B Series 1 AD ATR42-200 1 AD ATR42-300 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 ATP 1 AD C-212-CB 1 AD C-212-CC 1 AD C-212-CD 1 AD C-212-CE 1 AD C-212-CF 1 AD C-212-DE 1 AD C-212-DF 1 AD F27 Mark 050 1 AD Jetstream Model 4101 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 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 BAC 1-11 200 Series 1 AD BAC 1-11 400 Series 1 AD DH.125 Series 1A 1 AD DH.125 Series 1A-522 1 AD DH.125 Series 1A/R-522 1 AD DH.125 Series 1A/S-522 1 AD DH.125 Series 3A 1 AD DH.125 Series 3A/R 1 AD DH.125 Series 3A/RA 1 AD DH.125 Series 400A 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 A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 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 A300 B4-605R 1 AD A300 B4-620 1 AD A300 B4-622 1 AD A300 F4-605R 1 AD A310-203 1 AD A310-204 1 AD A310-221 1 AD A310-222 1 AD A310-304 1 AD A310-324 1 AD ATP 1 AD CL-600-2A12 (CL-601) 1 AD DHC-8-101 1 AD DHC-8-102 1 AD DHC-8-103 1 AD DHC-8-106 1 AD DHC-8-201 1 AD DHC-8-202 1 AD DHC-8-301 1 AD DHC-8-311 1 AD ATR42-200 1 AD ATR42-300 1 AD ATR42-320 1 AD ATR42-500 1 AD DHC-8-101 1 AD DHC-8-102 1 AD DHC-8-103 1 AD DHC-8-106 1 AD DHC-8-201 1 AD DHC-8-202 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

Recent ADs

2015-16-04

final rule

Airworthiness Directives; Kidde Graviner

Unsafe Condition: A fire extinguisher failed to operate when the activation lever was pressed, potentially leading to failure in the event of a fire.

Effective: Sep 15, 2015 Category: aircraft Compliance: Within 12 months of the effective date (September 15, 2015).

Why matched: Airworthiness Directives; Kidde Graviner

2010-24-06

final rule

Airworthiness Directives; Short Brothers PLC Model SD3 Airplanes

Unsafe Condition: Failure modes associated with an unsafe condition in the Fuel Tank System, as identified in the systems safety analysis, could lead to an unacceptable probability of ignition risk if specific tasks...

Effective: Feb 16, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Short Brothers PLC Model SD3 Airplanes

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

2009-21-10 R1

final rule

Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes

Unsafe Condition: The rupture of a high-pressure gaseous oxygen cylinder due to insufficient strength characteristics from improper heat treatment, which could cause structural damage, rapid decompression, damage to...

Effective: Feb 4, 2010 Category: appliance Compliance: Effective February 4, 2010

Why matched: Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes

2008-16-09 R1

final rule

Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

Unsafe Condition: Cracks in the stabilizer skin at the forward spar cap due to fatigue.

Effective: Sep 16, 2009 Category: aircraft Compliance: Prior to the accumulation of 2,500 flight hours, flight cycles, or landings, whichever occurs fir...

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

2008-12-08

final rule

Airworthiness Directives; Short Brothers Model SD3-60 Airplanes Equipped with an Auxiliary Fuel Tank System Installed in Accordance With Supplemental Type Certificate SA00404AT

Unsafe Condition: Potential ignition sources inside fuel tanks, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.

Effective: Jul 15, 2008 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 Airplanes Equipped with an Auxiliary Fuel Tank System Installed in Accordance With Supplemental Type Certificate SA00404AT

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

2007-08-09

final rule

Airworthiness Directives; Short Brothers Model SD3-60 SHERPA, SD3-SHERPA, SD3-30, and SD3-60 Airplanes

Unsafe Condition: Stress corrosion cracking of SAE-AISI 303 stainless steel material in MS 21260 type cable end fittings, initiated by pitting corrosion, leading to potential failure of control cables and loss of cr...

Effective: May 8, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 SHERPA, SD3-SHERPA, SD3-30, and SD3-60 Airplanes

2003-17-05R1

final rule

Airworthiness Directives; Short Brothers & Harland Ltd. Models SC-7 Series 2 and SC-7 Series 3 Airplanes

Unsafe Condition: Failure of critical structure of the aircraft caused by fatigue.

Effective: Mar 23, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Short Brothers & Harland Ltd. Models SC-7 Series 2 and SC-7 Series 3 Airplanes

2006-03-05

final rule

Airworthiness Directives; Short Brothers Model SD3-60 SHERPA, SD3-SHERPA, and SD3-60 Airplanes

Unsafe Condition: A cracked pintle pin fork end, which could lead to stress-corrosion cracking and subsequent failure of the main landing gear (MLG).

Effective: Mar 14, 2006 Category: aircraft Compliance: Within 3 months after the effective date of this AD for the initial inspection. If sealant is app...

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 SHERPA, SD3-SHERPA, and SD3-60 Airplanes

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

2005-19-18

final rule

Airworthiness Directives; Short Brothers Model SD3 Airplanes

Unsafe Condition: Reports of individuals experiencing fire extinguishant blowback when the extinguishant discharges through the fire extinguishing point adapters.

Effective: Oct 26, 2005 Category: aircraft Compliance: Within 6 months after June 8, 1998, for actions required by AD 98-09-28. Before further flight fo...

Why matched: Airworthiness Directives; Short Brothers Model SD3 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

2005-17-13

final rule

Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

Unsafe Condition: Fatigue cracking found on the rudder horn spar could lead to detachment of the mass balance weight of the rudder, which could jam or restrict the movement of the rudder, resulting in reduced contro...

Effective: Sep 12, 2005 Category: aircraft Compliance: Before further flight if any crack is detected in the rudder horn spar.

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

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

2005-13-31 Recurring

final rule

Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

Unsafe Condition: Corrosion in the area of the main spar web fittings of the vertical stabilizer could result in reduced structural integrity of the vertical stabilizer.

Effective: Aug 2, 2005 Category: aircraft Compliance: Within 4,800 flight hours or 90 days after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

2004-25-13 Recurring

final rule

Airworthiness Directives; Short Brothers Model SD3-60, SD3-SHERPA, and SD3-60 SHERPA Series Airplanes

Unsafe Condition: Failure of the aluminum alloy gland nut on the main landing gear (MLG) shock absorber, which could cause the MLG to collapse.

Effective: Jan 20, 2005 Category: aircraft Compliance: Within the compliance times specified in the AD, unless the actions have already been done.

Why matched: Airworthiness Directives; Short Brothers Model SD3-60, SD3-SHERPA, and SD3-60 SHERPA Series Airplanes

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

2004-16-02

final rule

Airworthiness Directives; Short Brothers Model SD3 Series Airplanes

Unsafe Condition: Engine shut-down in icing conditions, which could result in loss of control of the airplane and consequent injury to flightcrew and passengers.

Effective: Sep 14, 2004 Category: aircraft Compliance: Within five months after the effective date of this AD.

Why matched: Airworthiness Directives; Short Brothers Model SD3 Series Airplanes

2004-16-04

final rule

Airworthiness Directives; Short Brothers Model SD3 Series Airplanes

Unsafe Condition: Corrosion and deterioration of the aft pintle pin bushings of the main landing gear (MLG), which could result in the MLG not extending fully during landing, with consequent damage to the airplane s...

Effective: Sep 14, 2004 Category: aircraft Compliance: Within 24 months after the effective date

Why matched: Airworthiness Directives; Short Brothers Model SD3 Series Airplanes

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

2004-13-21 Recurring

final rule

Airworthiness Directives; Short Brothers Model SD3-60 SHERPA Series Airplanes

Unsafe Condition: Loose bolts that attach the vertical stabilizer to the horizontal stabilizer, and pulled or loose rivets in the upper shear angles, which could result in reduced structural integrity of the vertica...

Effective: Aug 3, 2004 Category: aircraft Compliance: Within 2 months after the effective date of this AD, or prior to the accumulation of 1,500 total ...

Why matched: Airworthiness Directives; Short Brothers Model SD3-60 SHERPA Series Airplanes

2004-13-04 Recurring

final rule

Airworthiness Directives; Short Brothers Model SD3-SHERPA Series Airplanes

Unsafe Condition: Corrosion and abnormal wear to the top and bottom shear decks, which could result in damage to the main landing gear (MLG) and consequent reduced controllability of the airplane on landing.

Effective: Jul 29, 2004 Category: aircraft Compliance: Within 6 months after the effective date of this AD, and continuing at intervals not to exceed 6 ...

Why matched: Airworthiness Directives; Short Brothers Model SD3-SHERPA Series Airplanes

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

2003-13-07 Recurring

final rule

Airworthiness Directives; Short Brothers and Harland Ltd. Models SC-7 Series 2 and SC-7 Series 3 Airplanes

Unsafe Condition: Failure of any flight control system rod caused by cracks or corrosion, which could lead to complete failure of the flight control system with consequent loss of control of the airplane.

Effective: Aug 11, 2003 Category: aircraft Compliance: Initially inspect within the next 3 months after August 11, 2003, or within 24 months after the l...

Why matched: Airworthiness Directives; Short Brothers and Harland Ltd. Models SC-7 Series 2 and SC-7 Series 3 Airplanes

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

2002-06-06

final rule

Airworthiness Directives; Rockwell Collins, Inc. TDR-94 and TDR-94D Mode S Transponders

Unsafe Condition: Erroneous altitude reporting from Rockwell Collins TDR-94 and TDR-94D Mode S transponders when deriving altitude information from a Gillham (gray code) encoded pressure altitude source, which could...

Effective: May 3, 2002 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Rockwell Collins, Inc. TDR-94 and TDR-94D Mode S Transponders

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