Martin-Marietta Corporation Airworthiness Directives

56 ADs indexed for Martin-Marietta Corporation aircraft.

Models

Recent ADs

77-17-12

final rule

Airworthiness Directives; MARTIN Martin 404 Aircraft

Unsafe Condition: Corrosion at wing spar chord splice joints at wing station 187 could lead to structural failure.

Effective: Aug 30, 1977 Category: aircraft Compliance: Within the next three months or 500 hours in service, whichever occurs first, after the effective...

Why matched: Airworthiness Directives; MARTIN Martin 404 Aircraft

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

71-09-06

final rule

Airworthiness Directives; MARTIN AIRCRAFT Models 202, 202A and 404 Airplanes

Unsafe Condition: Cracks or corrosion in the main landing gear aluminum gland nut, P/N 202SD81548 (Menasco Drawing No. 511034).

Effective: May 4, 1971 Category: aircraft Compliance: Within the next 25 hours in service after the effective date (May 4, 1971), unless already accomp...

Why matched: Airworthiness Directives; MARTIN AIRCRAFT Models 202, 202A and 404 Airplanes

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

67-19-04

final rule

Airworthiness Directives; MARTIN Models 202, 202A and 404 Airplanes

Unsafe Condition: Cracks and corrosion in the engine mounts, specifically in the tubular members and welds, which could lead to structural failure of the engine mounts.

Effective: Jun 20, 1967 Category: aircraft Compliance: Within the next 100 hours' time in service after the effective date (June 20, 1967), unless alrea...

Why matched: Airworthiness Directives; MARTIN Models 202, 202A and 404 Airplanes

67-14-06

final rule

MARTIN Models 202, 202A, and 404 Series Airplanes

Unsafe Condition: Cracks in the lower spar cap, spar web inboard of the outer panel closing rib, and vertical angle attaching the web to the outer panel closing rib in the front spars of the outer wing panels at 25%...

Effective: Apr 28, 1967 Category: aircraft Compliance: Within 15 hours' time in service after the effective date (April 28, 1967) unless already accompl...

Why matched: MARTIN Models 202, 202A, and 404 Series Airplanes

66-19-03

final rule

MARTIN Model 404 Airplanes

Unsafe Condition: Cracks in the main landing gear oleo cylinders between the jury strut attach lugs could result in structural failure of the landing gear.

Effective: Aug 19, 1966 Category: aircraft Compliance: within the next 50 hours' time in service after the effective date of this AD, unless already acc...

Why matched: MARTIN Model 404 Airplanes

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

66-08-04

final rule

Airworthiness Directives; MARTIN Models 202, 202A, and 404 Airplanes

Unsafe Condition: Cracks in the piston of the piston and fork assembly of the nose landing gear, specifically part number 202SD84483, could lead to failure of the nose landing gear assembly.

Effective: Apr 10, 1966 Category: aircraft Compliance: Compliance required as indicated in the AD, with specific timelines based on the time in service ...

Why matched: Airworthiness Directives; MARTIN Models 202, 202A, and 404 Airplanes

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

64-03-03

final rule

HAMILTON STANDARD Models All Standard Aluminum-Alloy Propellers

Unsafe Condition: Propeller blades may have undetected damage from impact with solid objects, leading to bending, twisting, or other structural failures that could result in blade separation or loss of thrust.

Effective: Mar 1, 1964 Category: appliance Compliance: before further flight

Why matched: HAMILTON STANDARD Models All Standard Aluminum-Alloy Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

63-24-02

final rule

MARTIN Models 202, 202A and 404 Aircraft

Unsafe Condition: Cracks found in the rear wing spar flange and in the Eastern Airlines P/N 304-5098-1 doubler on several aircraft.

Effective: Nov 21, 1963 Category: aircraft Compliance: within 50 hours' time in service after the effective date of this AD, unless already accomplished...

Why matched: MARTIN Models 202, 202A and 404 Aircraft

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

63-13-04

final rule

MARTIN Model 404 Aircraft

Unsafe Condition: Cracks have been found in the upper portion of the 0.250 inch radius at the junction of the axle and the piston terminal (approximately 2.4 inches from the centerline of the main gear) of main land...

Effective: Jul 15, 1963 Category: aircraft Compliance: Compliance required as indicated.

Why matched: MARTIN Model 404 Aircraft

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

61-01-02

final rule

MARTIN Models 202, 202A and 404 Aircraft

Unsafe Condition: Failures of Model 404 main landing gear torque arms have occurred in the lower attachment point where the torque scissors attach to the strut, and a failure was found in the apex (upper to lower to...

Effective: Jan 6, 1961 Category: aircraft Compliance: within the next 225 hours' time in service, unless already accomplished within the last 225 hours...

Why matched: MARTIN Models 202, 202A and 404 Aircraft

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

52-04-06

final rule

MARTIN Models 202 and 202A Aircraft

Unsafe Condition: The cabin heater lights and switch are not located in the cockpit, which could lead to inadequate monitoring and potential heater system failures.

Category: aircraft Compliance: not later than May 1, 1952

Why matched: MARTIN Models 202 and 202A Aircraft

51-24-02

final rule

Martin Model 202 Aircraft

Unsafe Condition: The fin-to-fuselage attachments may contain structural defects or fretting corrosion, which could lead to fin separation.

Category: aircraft Compliance: at the 3,000-hour period following the modification of the fin attachments per Martin 202 Service...

Why matched: Martin Model 202 Aircraft

52-02-03

final rule

Martin Models 202 and 202A Aircraft

Unsafe Condition: Oxygen bottles located in the lower center section require relocation to eliminate high pressure lines in the bottom of the fuselage.

Category: aircraft Compliance: not later than May 1, 1952

Why matched: Martin Models 202 and 202A Aircraft

54-06-02

final rule

MARTIN Model 202 Aircraft

Unsafe Condition: Unsatisfactory wing scarf splice bushing installations resulting in undesirable bending loads on the bolts due to incomplete lining of the holes.

Category: aircraft Compliance: At next overhaul but not to exceed the next 1,000 operating hours.

Why matched: MARTIN Model 202 Aircraft

53-20-01

final rule

MARTIN Models 202 and 202A Airplanes

Unsafe Condition: With the reverse pitch stop ring relocated to act as a low pitch stop, inadvertent energization of the reverse solenoid valve can cause the stop ring to fail under extreme loads from high oil press...

Category: aircraft Compliance: Compliance required prior to November 1, 1954 for dome modifications and by April 1, 1954 for con...

Why matched: MARTIN Models 202 and 202A Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

50-48-01

final rule

Martin Models 202 and 202A Aircraft

Unsafe Condition: Nose gear centering cam failures which result in the inability to extend the nose landing gear.

Category: aircraft Compliance: not later than February 1, 1951

Why matched: Martin Models 202 and 202A Aircraft

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

47-47-05

final rule

Martin Model 202 Aircraft

Unsafe Condition: Cracks at combustion chamber and heat exchanger end plates on Stewart-Warner 921-B heaters in cabin and wing systems may lead to heater failure.

Category: aircraft Compliance: Inspections must be conducted before further flight as per the specified intervals: cabin heaters...

Why matched: Martin Model 202 Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

52-04-01

final rule

Martin Models 202 Aircraft

Unsafe Condition: The throttling valve vent in the cabin heater fuel supply line lacks adequate drain, which could lead to fuel leakage and potential fire hazard.

Category: aircraft Compliance: not later than May 1, 1952

Why matched: Martin Models 202 Aircraft

51-25-02

final rule

Martin Models 202 and 202A Airplanes

Unsafe Condition: Inadvertent shorting between the "MAIN" and "CONTROL" terminals of the D7231-125 inverter remote reset circuit breaker.

Category: aircraft Compliance: January 1, 1952

Why matched: Martin Models 202 and 202A Airplanes

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

48-43-01

final rule

Martin Model 202 Aircraft

Unsafe Condition: Excessive hydraulic fluid leakage from system emergency and flap synchronizer bypass valves, nose gear steer-valve, hydraulic test outlet dustcaps, main and landing gear pressure relief valves, 24S...

Category: aircraft Compliance: As soon as practicable, but not later than January 1, 1949

Why matched: Martin Model 202 Aircraft

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

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