Bellanca Aircraft Corporation Airworthiness Directives

28 ADs indexed for Bellanca Aircraft Corporation aircraft.

Models

Recent ADs

2022-03-15

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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

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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

96-12-22

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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

81-16-04

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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

79-19-05

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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

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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

76-22-01

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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

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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

74-15-07

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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

72-20-06

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Airworthiness Directives; Bellanca Aircraft Corporation (Champion) Models 7ECA, 7GCAA, 7KCAB, 7GCBC and 8KCAB Airplanes

Unsafe Condition: Flight controls malfunction including possible loss of control due to cable failure.

Effective: Oct 5, 1972 Category: aircraft Compliance: Effective immediately for placarding and flight manual revisions; inspections required within 100...

Why matched: Airworthiness Directives; Bellanca Aircraft Corporation (Champion) Models 7ECA, 7GCAA, 7KCAB, 7GCBC and 8KCAB Airplanes

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

63-20-01

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Airworthiness Directives; Bellanca Model 14-13 Series Aircraft

Unsafe Condition: Cracks in the welds and adjacent structure where the brake-cylinder support brackets (P/N 9811-17 and -21) are attached to fuselage cross tube P/N 9802-47.

Effective: Oct 21, 1963 Category: aircraft Compliance: Within 50 hours' time in service after October 21, 1963, and every 50 hours' time in service ther...

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

63-17-01

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Airworthiness Directives; Bellanca Model 14-13 Series Aircraft

Unsafe Condition: Failure of the main landing gear retracting strut and attaching fittings due to cracks in welds and tube intersections.

Effective: Sep 13, 1963 Category: aircraft Compliance: within 50 hours' time in service after the effective date of this AD, and at intervals thereafter...

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

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

63-06-02

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Airworthiness Directives; Bellanca 14-13 Series, Downer 14-19 and 14-19-2 Aircraft

Unsafe Condition: Elongation of the control cable attachment bolt hole in the rudder bellcrank, P/N 9817, beyond maximum diameter of 0.210 inch.

Effective: Mar 19, 1963 Category: aircraft Compliance: Within the next 25 hours' time in service after the effective date of this AD, unless accomplishe...

Why matched: Airworthiness Directives; Bellanca 14-13 Series, Downer 14-19 and 14-19-2 Aircraft

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

52-17-01

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Airworthiness Directives; Bellanca Model 14-13 Series Aircraft.

Unsafe Condition: Landing gear retracting chain malfunctionings due to lack of proper chain tension and absence of a chain guard.

Category: aircraft Compliance: August 15, 1952, with chain tension inspections to be repeated at intervals not to exceed 100 hours.

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

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

48-05-03

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Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

Unsafe Condition: Failure of the trim tab bracket bolts could result in spreading of the brackets and loss of trim tab retention.

Category: aircraft Compliance: March 15, 1948

Why matched: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

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

46-41-01

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Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes

Unsafe Condition: The unsafe condition could occur if the elevator control system components are not properly installed or adjusted, which could result in improper elevator control movement and reduce the ability to...

Category: aircraft Compliance: Before the airplane is returned to service.

Why matched: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes

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

52-28-02

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Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

Unsafe Condition: Excessive pressure from the engine-driven fuel pump may create a possible hazard.

Category: aircraft Compliance: As soon as practicable, but not later than next engine overhaul after January 1, 1953.

Why matched: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

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

51-16-01

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Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

Unsafe Condition: Failure of the elevator trim tab in flight.

Category: aircraft Compliance: within the next 25 hours of operation, but not later than August 1, 1951

Why matched: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

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

49-13-02

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Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Airplanes

Unsafe Condition: Failure of the landing gear drag strut due to overstressing or insufficient fitting strength at the rear wing spar attachment.

Category: aircraft Compliance: July 1, 1949

Why matched: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Airplanes

47-07-01

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Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes

Unsafe Condition: Improper indexing of the fuel selector valve handle may result in incorrect fuel tank selection or unintended fuel flow interruption.

Category: aircraft Compliance: not later than next periodic inspection

Why matched: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes

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

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