Airworthiness Directive 98-34502
one-timeAirworthiness Directives; Westland Helicopters Ltd. 30 Series 100 and 100-60 Helicopters
What this AD requires
This amendment adopts a new airworthiness directive (AD) that is applicable to Westland Helicopters Ltd. (Westland) 30 Series 100 and 100-60 helicopters. This action requires the removal and replacement of conformal pinion quill shafts installed in certain main rotor gearboxes that fail to pass a magnetic drain plug inspection. This amendment is prompted by a report of a forced landing that occurred when a single conformal pinion quill shaft failed in a main rotor gearbox (MRGB). This condition, if not corrected, could result in the failure of a MRGB, and a subsequent forced landing or loss of control of the helicopter.
Which aircraft AD 98-34502 applies to
Applies when the installed main rotor gearbox (MRGB) serial number is one of: AAT4440, ABL5602, ACD2875, AAX4726, ABN8930, ACN7996, ABC9438, ABP3947, ADE6100, ABD7294, ABP9028, WAG397, ABG5056, ABT3965, WAG410, ABH5075, ABW0547, WAK525, ABJ9595, ACA3707, WAK561, ABK9484, or has a documented history of shock loading. Per Westland Helicopters SB No. W30-63-75; text describes affected aircraft as 'Westland 30 series helicopters'.
Whether AD 98-34502 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.