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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

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

96-18-07

final rule

Airworthiness Directives; Bellanca, Incorporated Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

Unsafe Condition: Failure of the nose landing gear (NLG), which could result in loss of control of the airplane during landing operations due to cracks or bends in the NLG drag strut brackets or corroded/worn bolts ...

Effective: Oct 25, 1996 Category: aircraft Compliance: Initially upon accumulating 500 hours time-in-service (TIS) or within the next 50 hours TIS after...

Why matched: Airworthiness Directives; Bellanca, Incorporated Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

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

Amdt-39-9731 Recurring

final rule

Airworthiness Directives; Bellanca, Incorporated Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

Unsafe Condition: Collapse of the nose landing gear (NLG) during landing due to failure of the NLG strut and brackets.

Effective: Oct 25, 1996 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bellanca, Incorporated Models 17-30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

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

96-12-22

final rule

Airworthiness Directives; Cessna Aircraft Company Engine Oil Filter Adapter Assemblies Installed on Aircraft

Unsafe Condition: Loose or separated engine oil filter adapters could cause loss of engine oil, leading to engine stoppage while in flight and loss of control of the airplane.

Effective: Jul 31, 1996 Category: appliance Compliance: Within the next 100 hours time-in-service (TIS) after the effective date or when the engine oil f...

Why matched: Airworthiness Directives; Cessna Aircraft Company Engine Oil Filter Adapter Assemblies Installed on Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

90-15-15 R1

final rule

Airworthiness Directives; AMERICAN CHAMPION AIRCRAFT (BELLANCA, CHAMPION) Model 8KCAB Airplanes

Unsafe Condition: Failure of the upper wing front spar strut fittings, part number 2-1976, could result in an in-flight separation of the wing.

Effective: May 15, 1991 Category: aircraft Compliance: Within the next 25 hours time-in-service (TIS) after the effective date of this AD or prior to th...

Why matched: Airworthiness Directives; AMERICAN CHAMPION AIRCRAFT (BELLANCA, CHAMPION) Model 8KCAB Airplanes

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

90-02-17

final rule

Airworthiness Directives; BELLANCA, INCORPORATED Models 14-19-3, 14-19-3A, 17-30, 17-31 and 17-31TC, 17-30A, 17-31A and 17-31ATC Airplanes

Unsafe Condition: Collapse of the main landing gear due to cracks, deformations, or failures in the left and right drag strut landing gear fitting assemblies, Part Number 194153-10.

Effective: Feb 5, 1990 Category: aircraft Compliance: Within 500 hours total time-in-service (TIS) or within the next 100 hours TIS after the effective...

Why matched: Airworthiness Directives; BELLANCA, INCORPORATED Models 14-19-3, 14-19-3A, 17-30, 17-31 and 17-31TC, 17-30A, 17-31A and 17-31ATC Airplanes

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

87-11-01 R1

final rule

Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

Unsafe Condition: Engine power loss due to either the accumulation of water or other contaminants in the fuel system or due to mismanagement of available fuel resources caused by lack of pilot familiarity with the a...

Effective: Aug 28, 1987 Category: aircraft Compliance: Within the next 30 days after the effective date of this AD or at the next annual inspection, whi...

Why matched: Airworthiness Directives; Bellanca Model 17- 30, 17-30A, 17-31, 17-31A, 17-31TC, and 17-31ATC Airplanes

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

86-25-06

final rule

Airworthiness Directives; Bellanca Model 17-30, 17-30A, 17-31, 17-31A, 17-31TC and 17-31ATC Airplanes

Unsafe Condition: Engine power loss due to the accumulation of water or other contaminants in the fuel system from wing main and auxiliary fuel tanks lacking an FAA approved drain valve.

Effective: Dec 22, 1986 Category: aircraft Compliance: within the next 50 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Bellanca Model 17-30, 17-30A, 17-31, 17-31A, 17-31TC and 17-31ATC Airplanes

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

81-16-04

final rule

Airworthiness Directives; BELLANCA AIRCRAFT CORPORATION Models 8KCAB, 7ECA, 7GCAA, 7GCBC and 7KCAB Airplanes

Unsafe Condition: Improper installation of the competition harness (ACRO harness) shoulder straps not passing on the forward side of the seat back could result in inadequate retention of the pilot during acrobatic m...

Effective: Jul 28, 1981 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; BELLANCA AIRCRAFT CORPORATION Models 8KCAB, 7ECA, 7GCAA, 7GCBC and 7KCAB Airplanes

80-21-06

final rule

Airworthiness Directives; BELLANCA (CHAMPION) Models 7GC, 7GCB, 7HC, 7KC, 7GCA, 7GCBA, 7ECA, 7GCAA, 7GCBC, 7KCAB, and 8KCAB Airplanes.

Unsafe Condition: Degradation of the induction system icing protection or partial engine power loss due to cracking or deterioration of the baffle installation within the muffler core and body assemblies (Bellanca (...

Effective: Oct 16, 1980 Category: aircraft Compliance: Within the next 25 hours time in service, or 60 days after the effective date of this AD, whichev...

Why matched: Airworthiness Directives; BELLANCA (CHAMPION) Models 7GC, 7GCB, 7HC, 7KC, 7GCA, 7GCBA, 7ECA, 7GCAA, 7GCBC, 7KCAB, and 8KCAB Airplanes.

47-20-01

final rule

Airworthiness Directives; Bellanca (Aeronca) Model 7AC, 7BCM, and 11AC Aircraft

Unsafe Condition: Accumulations of water and foreign matter in the metal gascolator bowl can obstruct fuel flow and lead to engine failure.

Effective: Mar 18, 1980 Category: aircraft Compliance: Compliance required as indicated below: for aircraft without quick-drain, every 25 hours of engin...

Why matched: Airworthiness Directives; Bellanca (Aeronca) Model 7AC, 7BCM, and 11AC Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

79-22-01

final rule

Airworthiness Directives; Bellanca Model 7ECA, 8KCAB and 8GCBC Aircraft

Unsafe Condition: Exhaust system cracking in the welded area between the riser tube and exhaust flange, and muffler body cracks, which could lead to exhaust leakage and potential engine failure.

Effective: Oct 29, 1979 Category: aircraft Compliance: within the next 30 days or 10 hours of aircraft time in service, whichever occurs first, after th...

Why matched: Airworthiness Directives; Bellanca Model 7ECA, 8KCAB and 8GCBC Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

79-19-05

final rule

Airworthiness Directives; Bellanca Model 14-13 Aircraft

Unsafe Condition: Reversal of aileron control system leading to incorrect operation

Effective: Sep 10, 1979 Category: aircraft Compliance: within the next 10 hours in service after the effective date of this AD

Why matched: Airworthiness Directives; Bellanca Model 14-13 Aircraft

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

79-07-02

final rule

Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979

Unsafe Condition: The Exide AC 78M and Willard W 78M batteries manufactured between December 1978 and February 1979, identified by N-8, A-9, or B-9 stamped on terminal posts, may fail due to internal short circuits ...

Effective: Apr 3, 1979 Category: appliance Compliance: before next flight

Why matched: Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979

77-22-05

final rule

Airworthiness Directives; Bellanca (Champion) Models 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBC, 7HC and 7KCAB Airplanes

Unsafe Condition: Failure to comply with airspeed restrictions and operating limitations could result in exceeding load factors or structural failure of the wing front lift struts, leading to loss of aircraft control.

Effective: Nov 7, 1977 Category: aircraft Compliance: within three (3) months after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; Bellanca (Champion) Models 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBC, 7HC and 7KCAB Airplanes

77-22-02

final rule

Airworthiness Directives; Bellanca Models 14-19-3, 14-19-3A, 17-30 and 17-30A Series Aircraft

Unsafe Condition: Cracks or tube buckling in the Bellanca Part No. 191106 and 191898 nose landing gear engine mount bed rail frame nose landing gear support structure.

Effective: Nov 2, 1977 Category: aircraft Compliance: Within the next 50 hours time in service after the effective date of the airworthiness directive ...

Why matched: Airworthiness Directives; Bellanca Models 14-19-3, 14-19-3A, 17-30 and 17-30A Series Aircraft

76-22-01

final rule

Airworthiness Directives; Bellanca Aircraft Corporation MODEL 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB and 8GCBC Airplanes

Unsafe Condition: Cracks and/or permanent deformation in the lower frame side tubes of the adjustable front seat due to installation per Bellanca Kit #252.

Effective: Nov 2, 1976 Category: aircraft Compliance: within the next 10 hours' time in service after the effective date of this AD, unless already acc...

Why matched: Airworthiness Directives; Bellanca Aircraft Corporation MODEL 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB and 8GCBC Airplanes

76-20-07

final rule

Airworthiness Directives; Bellanca CH, CH-300 Pacemaker, 300-W Pacemaker, CH-400 Skyrocket, E Pacemaker, F. Skyrocket, 14-9, 14-9L, 14- 12F-3, 14-13, 14-13-2, 14-3-3, 14-13-3W, 31-42 Pacemaker Aircraft

Unsafe Condition: Failure of forward or aft wing spars due to wood decay caused by water collecting in the wing.

Effective: Oct 8, 1976 Category: aircraft Compliance: Prior to the next flight after receipt of this AD unless already accomplished, and at each annual...

Why matched: Airworthiness Directives; Bellanca CH, CH-300 Pacemaker, 300-W Pacemaker, CH-400 Skyrocket, E Pacemaker, F. Skyrocket, 14-9, 14-9L, 14- 12F-3, 14-13, 14-13-2, 14-3-3, 14-13-3W, 31-42 Pacemaker Aircraft

76-08-04

final rule

Airworthiness Directives; Bellanca Model: 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31TC and 17-31ATC Airplanes

Unsafe Condition: Wood deterioration in the wing could result in structural failure.

Effective: Sep 9, 1976 Category: aircraft Compliance: Effective September 9, 1976. Compliance required as indicated.

Why matched: Airworthiness Directives; Bellanca Model: 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31TC and 17-31ATC Airplanes

75-17-16

final rule

Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

Unsafe Condition: Engine power loss due to fatigue failure of the carburetor alternate air valves.

Effective: Aug 12, 1975 Category: aircraft Compliance: Within the next 10 hours time in service after the effective date of this AD or June 25, 1975, as...

Why matched: Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

75-11-06

final rule

Airworthiness Directives; Bellanca Model 17-31, 17-31TC, 17-31A and 1731ATC Airplanes

Unsafe Condition: Failure of the check valve (P/N 19121-206) in the vapor return line could result in engine power failure due to fuel vapor lock.

Effective: Jun 25, 1975 Category: aircraft Compliance: within the next 25 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Bellanca Model 17-31, 17-31TC, 17-31A and 1731ATC Airplanes

74-23-04

final rule

Airworthiness Directives; Bellanca Model 8KCAB Aircraft

Unsafe Condition: Fatigue cracks and/or distortion of rib flanges on Bellanca Model 8KCAB aircraft wing ribs could lead to wing structural failure.

Effective: Mar 6, 1975 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; Bellanca Model 8KCAB Aircraft

75-04-12

final rule

Airworthiness Directives; Bellanca Model 8GCBC Airplanes

Unsafe Condition: Resonant vibratory conditions with McCauley Model 1A200/HFA fixed pitch propellers installed on Lycoming O-360-C2A or -C2E type engines.

Effective: Feb 21, 1975 Category: aircraft Compliance: within the next 10 hours time in service after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; Bellanca Model 8GCBC Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

74-15-07

final rule

Airworthiness Directives; Bellanca Aircraft Corporation Model 8GCBC Aircraft

Unsafe Condition: Improper indexing of the propeller to the crankshaft flange may cause bushing shoulders to be misaligned, leading to potential damage or failure of the propeller mounting components.

Effective: Jul 26, 1974 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bellanca Aircraft Corporation Model 8GCBC Aircraft