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, 1977Category: aircraftCompliance: Within the next three months or 500 hours in service, whichever occurs first, after the effective...
Why matched: Airworthiness Directives; MARTIN Martin 404 Aircraft
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, 1971Category: aircraftCompliance: 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
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, 1967Category: aircraftCompliance: 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
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, 1967Category: aircraftCompliance: 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
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, 1966Category: aircraftCompliance: within the next 50 hours' time in service after the effective date of this AD, unless already acc...
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, 1966Category: aircraftCompliance: 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
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, 1964Category: applianceCompliance: before further flight
Why matched: HAMILTON STANDARD Models All Standard Aluminum-Alloy Propellers
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, 1963Category: aircraftCompliance: 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
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, 1963Category: aircraftCompliance: Compliance required as indicated.
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, 1961Category: aircraftCompliance: 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
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: aircraftCompliance: not later than May 1, 1952
Unsafe Condition: Oxygen bottles located in the lower center section require relocation to eliminate high pressure lines in the bottom of the fuselage.
Category: aircraftCompliance: not later than May 1, 1952
Unsafe Condition: Unsatisfactory wing scarf splice bushing installations resulting in undesirable bending loads on the bolts due to incomplete lining of the holes.
Category: aircraftCompliance: At next overhaul but not to exceed the next 1,000 operating hours.
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: aircraftCompliance: Compliance required prior to November 1, 1954 for dome modifications and by April 1, 1954 for con...
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: aircraftCompliance: Inspections must be conducted before further flight as per the specified intervals: cabin heaters...
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: aircraftCompliance: not later than May 1, 1952
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: aircraftCompliance: As soon as practicable, but not later than January 1, 1949