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2013-08-14 Recurring

final rule

Airworthiness Directives; Revo, Incorporated Airplanes

Unsafe Condition: Fretting, cracking, or corrosion of the horizontal stabilizer attachment fitting, which could lead to structural failure of the fitting.

Effective: Jun 13, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Revo, Incorporated Airplanes

2005-12-02 Recurring

final rule

Airworthiness Directives; Revo, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

Unsafe Condition: Fatigue cracks in the horizontal stabilizer attachment fitting (part number 2-2200-21) could result in failure of the fitting, leading to loss of control of the airplane.

Effective: Jul 8, 2005 Category: aircraft Compliance: Within 12 months of the effective date (July 8, 2005)

Why matched: Airworthiness Directives; Revo, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

2002-21-05

final rule

Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 Airplanes

Unsafe Condition: Cracks in the upper and lower wing spar doublers and angles, which could lead to wing spar failure and wing separation from the airplane.

Effective: Oct 23, 2002 Category: aircraft Compliance: After the incorporation of Modification Kit B-79 or FAA-approved equivalent.

Why matched: Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 Airplanes

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

2000-10-22

final rule

Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 Airplanes

Unsafe Condition: Fatigue cracks in the wing spars, specifically at the second-most inboard wing attachment bolt hole, could result in wing separation and loss of control.

Effective: Jun 20, 2000 Category: aircraft Compliance: Within 12 months of the effective date of the AD.

Why matched: Airworthiness Directives; REVO, Incorporated Models Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, and Lake Model 250 Airplanes

Amdt-39-10524

final rule

Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

Unsafe Condition: Fatigue cracks to the horizontal and vertical stabilizer attachment fitting could result in loss of control of the airplane.

Effective: Jun 8, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

94-22-02

final rule

Airworthiness Directives; CONSOLIDATED AERONAUTICS Lake Model 250 airplanes

Unsafe Condition: Failure of the elevator autotrim to disengage could result in flight path deviations.

Effective: Nov 4, 1994 Category: aircraft Compliance: within the next 10 hours time-in-service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives; CONSOLIDATED AERONAUTICS Lake Model 250 airplanes

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

86-23-05

final rule

Airworthiness Directives; Consolidated Lake Model 250 Series Airplanes

Unsafe Condition: Possible contact of the fuel shutoff valve handle hardware and the cabin rear upholstery panel.

Effective: Dec 17, 1986 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Consolidated Lake Model 250 Series Airplanes

79-21-09 R1

final rule

Airworthiness Directives; Consolidated Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

Unsafe Condition: Burning of power wires in case of an electrical short due to anchor light or bilge pump power lines bypassing the battery relay.

Effective: Jun 8, 1981 Category: aircraft Compliance: within the next 50 hours time in service

Why matched: Airworthiness Directives; Consolidated Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

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

79-06-01

final rule

Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

Unsafe Condition: Engine mounts with cracked straps, part number 2-5400-245, could result in engine separation.

Effective: Feb 23, 1979 Category: aircraft Compliance: Prior to further flight and within the next 15 hours flight time.

Why matched: Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

78-14-05

final rule

Airworthiness Directives; Consolidated Aeronautics Model LA-4-200 Airplanes

Unsafe Condition: Flawed (material defect) wing main beam attachment fittings (steel fittings), P/N 1-3214-3, with spanwise cracks or impression stamped bar stock heat treat lot numbers 741 or 741R.

Effective: Jul 19, 1978 Category: aircraft Compliance: Prior to further flight and thereafter prior to the first flight of each day until paragraph 3 is...

Why matched: Airworthiness Directives; Consolidated Aeronautics Model LA-4-200 Airplanes

76-24-02

final rule

Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

Unsafe Condition: Engine oil cooler failures allowing rapid loss of engine oil which could result in engine stoppage.

Effective: Oct 15, 1976 Category: aircraft Compliance: Before next flight of the affected airplanes for inspection; prior to further flight for replacem...

Why matched: Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

76-12-11

final rule

Airworthiness Directives; Consolidated Aeronautics Model LA-4-200 Airplanes

Unsafe Condition: Engine power loss resulting from fuel injector contamination caused by filter housing corrosion.

Effective: Jun 29, 1976 Category: aircraft Compliance: Within the next 30 days for filters installed 60 or more days prior, or prior to the accumulation...

Why matched: Airworthiness Directives; Consolidated Aeronautics Model LA-4-200 Airplanes

76-02-01

final rule

Airworthiness Directives; Consolidated Aeronautics Models Lake LA-4 and Lake LA-4-200 Airplanes

Unsafe Condition: Engine power interruption resulting from water contamination of the fuel system due to water entering the auxiliary fuel tank sumps.

Effective: Jan 30, 1976 Category: aircraft Compliance: by the effective date of this Amendment

Why matched: Airworthiness Directives; Consolidated Aeronautics Models Lake LA-4 and Lake LA-4-200 Airplanes

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

74-26-02

final rule

Airworthiness Directives; Consolidated Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA-4P and LA-4-200 Airplanes

Unsafe Condition: Failure of the arms of the rudder bellcrank assembly (P/N's 2-7109-1, 2-7103-91 and 1-7103-1) leading to loss of rudder control.

Effective: Dec 27, 1974 Category: aircraft Compliance: Within 10 hours' time in service after the effective date of this AD and thereafter at intervals ...

Why matched: Airworthiness Directives; Consolidated Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA-4P and LA-4-200 Airplanes

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

74-25-08

final rule

Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1 and Colonial C-2 Airplanes

Unsafe Condition: Cracked or failed wing rear spar fittings or wing rear spar fittings with distorted bolt holes

Effective: Dec 18, 1974 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; Consolidated Aeronautics Model Colonial C-1 and Colonial C-2 Airplanes

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

74-09-06

final rule

Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

Unsafe Condition: The possibility of engine stoppage resulting from contamination in the fuel injector due to a flush insert in the restrictor fitting P/N 2-6750-41.

Effective: May 10, 1974 Category: aircraft Compliance: within the next twenty-five (25) hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4-200 Airplanes

72-07-11

final rule

Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes

Unsafe Condition: Failure of the rod-end bearing, P/N HM-5C, connected to the flap pushrod, P/N 2-7811-21, which could result in hazards in flight due to corrosion, cracks, or binding of the ball motion.

Effective: Jan 5, 1973 Category: aircraft Compliance: within the next 15 hours in service after the effective date of this AD, unless already accomplis...

Why matched: Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes

67-11-01

final rule

Airworthiness Directives; Colonial Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4P, Lake LA-4A, Lake LA-4

Unsafe Condition: Failure of the fuel pressure gauge instrument line could allow unrestricted fuel to enter the cabin compartment.

Effective: Aug 5, 1967 Category: aircraft Compliance: within 25 hours' time in service after April 5, 1967

Why matched: Airworthiness Directives; Colonial Aeronautics Models Colonial C-1, Colonial C-2, Lake LA-4P, Lake LA-4A, Lake LA-4

65-15-03

final rule

Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4 Aircraft

Unsafe Condition: Failure of the nose landing gear to latch in the down and locked position due to incorrect bolt installation or elongated bolt holes in the nose gear drag strut assembly.

Effective: Jul 1, 1965 Category: aircraft Compliance: within the next 25 hours' time in service after the effective date of this AD unless already acco...

Why matched: Airworthiness Directives; Consolidated Aeronautics Model Lake LA-4 Aircraft

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

64-17-05

final rule

Airworthiness Directives; Consolidated Aeronautics Models Lake LA-4, Lake LA-4A and Lake LA-4P Aircraft

Unsafe Condition: Complete breather blockage and subsequent loss of engine oil due to icing.

Effective: Aug 28, 1964 Category: aircraft Compliance: prior to September 15, 1964

Why matched: Airworthiness Directives; Consolidated Aeronautics Models Lake LA-4, Lake LA-4A and Lake LA-4P Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

60-22-01

final rule

Airworthiness Directives; Colonial Model C-2

Unsafe Condition: Failures of the engine mount bolts

Effective: Nov 29, 1960 Category: aircraft Compliance: within 100 hours' time in service after effective date of this amendment

Why matched: Airworthiness Directives; Colonial Model C-2

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

57-13-01

final rule

Airworthiness Directives; Colonial Model C-1 Aircraft

Unsafe Condition: Cracks in the weld areas of engine pylon side strut attaching fittings (P/N 3208-10) may originate across the edge, leading to structural failure.

Category: aircraft Compliance: within next 10 hours of operation or July 15, 1957, whichever occurs first, and every 100 hours' ...

Why matched: Airworthiness Directives; Colonial Model C-1 Aircraft

59-12-05

final rule

Airworthiness Directives; Colonial Models C-1 and C-2 Aircraft

Unsafe Condition: Plastic control surface hinge pin locks may crack, allowing the hinge pin to work out.

Category: aircraft Compliance: before further operation

Why matched: Airworthiness Directives; Colonial Models C-1 and C-2 Aircraft

59-17-04

final rule

Airworthiness Directives; Colonial Models C-1 and C-2 Aircraft

Unsafe Condition: Failures in service of the two AN 4 bolts attaching the wing rear spar to the hull on each side at hull Station 138.

Category: aircraft Compliance: within the next 10 hours but not later than October 15, 1959, and at each 100 hours thereafter

Why matched: Airworthiness Directives; Colonial Models C-1 and C-2 Aircraft

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

59-15-02

final rule

Airworthiness Directives; COLONIAL All Models C-1 and C-2 Aircraft

Unsafe Condition: Rivets fastening the aluminum throttle control handle to the steel bell crank have loosened and sheared.

Category: aircraft Compliance: before the next periodic inspection or December 1, 1959, whichever comes first

Why matched: Airworthiness Directives; COLONIAL All Models C-1 and C-2 Aircraft