Alexandria Aircraft, LLC Airworthiness Directives

20 ADs indexed for Alexandria Aircraft, LLC aircraft.

Models

Recent ADs

2008-05-11

final rule

Airworthiness Directives; Alexandria Aircraft, LLC Models 17-30, 17-31, 17-30A, 17-31A, and 17-31ATC Airplanes

Unsafe Condition: Cracks in the exhaust system could result in heat damage to magneto electrical wiring and smoke in the cockpit, leading to loss of engine power and/or a fire in the engine compartment.

Effective: Apr 8, 2008 Category: aircraft Compliance: Within the applicable inspection interval as specified in the AD.

Why matched: Airworthiness Directives; Alexandria Aircraft, LLC Models 17-30, 17-31, 17-30A, 17-31A, and 17-31ATC Airplanes

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

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

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

82-22-03

final rule

Airworthiness Directives; Eagle Model DW-1 Airplanes

Unsafe Condition: Loss of elevator control due to failure of the aft elevator push tube.

Effective: Nov 1, 1982 Category: aircraft Compliance: Within 25 hours after the effective date of this AD on airplanes having 400 or more hours time-in...

Why matched: Airworthiness Directives; Eagle Model DW-1 Airplanes

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

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

76-08-04

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

75-11-06

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

73-05-02

final rule

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

Unsafe Condition: Failure of the rudder control system due to cracks or other failures in the rudder pedal shaft assemblies with .049" thick horizontal tube walls.

Effective: Mar 7, 1973 Category: aircraft Compliance: Within the next 10 hours time in service after the effective date for initial inspection, and the...

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

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

73-03-03

final rule

Airworthiness Directives; Bellanca Model 17-30A Airplanes

Unsafe Condition: Bolt failures and subsequent washer ingestion into the engine due to AN4H-17A bolts attaching the air induction box to the throttle body.

Effective: Feb 7, 1973 Category: aircraft Compliance: Within 10 hours time in service after the effective date of this AD for paragraph a, and within 5...

Why matched: Airworthiness Directives; Bellanca Model 17-30A Airplanes

72-13-03

final rule

Airworthiness Directives; Bellanca Model 17-30 Airplanes

Unsafe Condition: Failure of the fuel boost pump circuit could lead to engine flooding when using the fuel boost pump, potentially causing loss of engine power.

Effective: Jun 20, 1972 Category: aircraft Compliance: Within 50 hours' time in service after June 26, 1971, or within 10 hours' time in service after S...

Why matched: Airworthiness Directives; Bellanca Model 17-30 Airplanes

72-01-03

final rule

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

Unsafe Condition: Loss of engine power due to fuel starvation caused by the use of Aeroquip P/N 359-8D-0153 hose between the firewall and engine driven fuel pump.

Effective: Jan 5, 1972 Category: aircraft Compliance: Prior to next flight

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

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

72-01-01

final rule

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

Unsafe Condition: Leakage of flammable fluids from flexible hose assemblies in the engine compartment due to potential failure of Aeroquip 601 series or Stratoflex 156 series hoses.

Effective: Dec 31, 1971 Category: aircraft Compliance: Within 50 hours' time in service after December 31, 1971, and thereafter every 100 hours' time in...

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

71-10-01

final rule

Airworthiness Directives; Bellanca Model 17-30 Airplanes

Unsafe Condition: Hazardous fuel leakage due to inadequate sealing in the electric fuel pump seal chamber.

Effective: May 8, 1971 Category: aircraft Compliance: Within 50 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Bellanca Model 17-30 Airplanes

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

69-12-04

final rule

Airworthiness Directives; Bellanca Model 14-19-3A and 17-30 Airplanes

Unsafe Condition: Failures of the stabilizer rear strut clevises

Effective: Jun 13, 1969 Category: aircraft Compliance: Within 25 hours' time-in-service after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; Bellanca Model 14-19-3A and 17-30 Airplanes

68-23-08

final rule

Airworthiness Directives; Bellanca Model 14-19-3A and Model 17-30 Airplanes

Unsafe Condition: Vibration of the horizontal tail surfaces and inaccurate airspeed indication

Effective: Nov 22, 1968 Category: aircraft Compliance: On or before November 22, 1969 for elevator trim tab modifications; within 25 hours' time-in-serv...

Why matched: Airworthiness Directives; Bellanca Model 14-19-3A and Model 17-30 Airplanes

63-06-02

final rule

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

51-16-02

final rule

Airworthiness Directives; Bellanca Model 14-19 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 14-19 Airplanes

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

53-16-01

final rule

Airworthiness Directives; Bellanca Model 14-19 Series Airplanes

Unsafe Condition: Elevator trim tab system looseness due to excessive free play of the trim tab trailing edge exceeding 0.20 inch at maximum chord, which may result from excessively worn parts or loose adjustments.

Category: aircraft Compliance: prior to September 15, 1953, and to be repeated at intervals not to exceed 100 hours flight time

Why matched: Airworthiness Directives; Bellanca Model 14-19 Series Airplanes

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

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