19 ADs indexed for Swift Museum Foundation, Inc. aircraft.
Airworthiness Directives; Universal Model GC-1B Aircraft
Unsafe Condition: Failure through internal corrosion of the upper left and right hand members of the engine mount assembly, occurring just above the weld junction with the horizontal members, which could result in l...
Why matched: Airworthiness Directives; Universal Model GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Failure to crank the landing gear emergency extension crank back to the full up position before retraction could damage the retraction system.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Temco Models GC-1A and GC-1B Aircraft
Unsafe Condition: Looseness in the horizontal stabilizer front spar attachment to the fuselage bulkhead due to deformation or elongation of the AN 3 bolt holes.
Why matched: Airworthiness Directives; Temco Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: The rivet seam attaching the upper skin of the outer wing panels to the main spar has insufficient reinforcement due to an inadvertent error in manufacture, risking structural failure.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: The tubular (deeply inserted) type battery vent plugs of the Reading Model R-24L battery can cause acid spillage leading to corrosion on the firewall and fuselage.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Temco Models GC-1A and GC-1B Airplanes
Unsafe Condition: Pieces of asbestos from the carburetor heat muff entering the carburetor can cause engine malfunctioning.
Why matched: Airworthiness Directives; Temco Models GC-1A and GC-1B Airplanes
Airworthiness Directives; Temco Models GC-1A and GC-1B Aircraft
Unsafe Condition: The two most forward AN 3-4 bolts in each flange of reinforcement P/N 11-213-5074 interfere with the tailwheel shock strut cylinder at the upper extreme of its travel, potentially causing damage to...
Why matched: Airworthiness Directives; Temco Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Installation of steel sleeve Continental P/N 25206 at the forward end of the engine's left oil gallery outlet port may prevent positive lubrication to the No. 6 cylinder connecting rod bearing.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Temco Models GC-1A and GC-1B
Unsafe Condition: Worn bushings in landing gear pivot points could allow excessive fore and aft travel of the main landing gear exceeding 3/8-inch, leading to potential structural failure or improper operation.
Why matched: Airworthiness Directives; Temco Models GC-1A and GC-1B
Airworthiness Directives; Universal Models GC-1A and GC-1B Aircraft
Unsafe Condition: Failure of the stop ring brazed to the inner piston strut, resulting in the piston sliding out of the strut and the torque knees assuming a straight position, which precludes gear retraction into t...
Why matched: Airworthiness Directives; Universal Models GC-1A and GC-1B Aircraft
Airworthiness Directives; GLOBE Models GC-1A and GC-1B Aircraft.
Unsafe Condition: The main landing gear retraction system may have improper adjustments in the side brace down stop position, down lock plunger clearance, limit switch plunger depression, and emergency extension cab...
Why matched: Airworthiness Directives; GLOBE Models GC-1A and GC-1B Aircraft.
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: The aluminum alloy cabin heater valve assembly may not provide a complete firewall material barrier.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Fouling of the elevator cable links with the control wheel shafts
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Collapsing of the carburetor flexible air duct when the carburetor air heater is used.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Temco GC-1A and GC-1B Aircraft
Unsafe Condition: Cracks are occurring in the last bulkhead (Station 185) of the fuselage at the bottom rudder hinge and stop fitting.
Why matched: Airworthiness Directives; Temco GC-1A and GC-1B Aircraft
Airworthiness Directives; Universal (Globe) Models GC-1A and GC-1B Aircraft
Unsafe Condition: Failure of the aluminum alloy torque knees on E.L.I. type landing gear assemblies, which do not provide the required extension stop (P/N 64A31), leading to loss of landing gear and damage to the ai...
Why matched: Airworthiness Directives; Universal (Globe) Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: The AN 960-616 washers under the nuts at the attachment of the main landing gear retraction links to the shock struts may not properly retain the bushings in the retraction links.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Clogging of the engine breather line due to ice formation during cold weather operation or entry of foreign matter caused by propeller blast.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
Unsafe Condition: Cracks originating at the joggles in the flange outboard of the stabilizer attachment points on the upper bulkhead at fuselage Station 167 may form, potentially extending into the web of the bulkhead.
Why matched: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft