1 RULES: Fokker,
This amendment adopts a new airworthiness directive (AD), applicable to all Fokker Model F.28 Mark 0070 and 0100 series airplanes, that requires measurement of the overcenter force of the thrust reverser operating levers, a functional test of the secondary lock solenoid of the thrust reversers, and corrective actions if necessary. The actions
2 PROPOSED RULES: Raytheon,
This document proposes to revise Airworthiness Directive (AD) 942004 R1, which currently requires ruddervator inspections and modifications on certain Raytheon Aircraft Company (Raytheon) Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, and V35B airplanes. This proposed AD is the result of the need to add a
3 RULES: Pratt & Whitney Canada,
This amendment adopts a new airworthiness directive (AD) that is applicable to Pratt & Whitney Canada (PWC) PW500 series turbofan engines. This action requires a onetime visual inspection and re marking, or in lieu of inspection, replacement of certain part numbers (P/N's) of the flexible fuel tube located between the fuel/oil heat exchanger and
4 PROPOSED RULES: McDonnell Douglas,
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model 717200 airplanes. This proposal would require modification of certain attachment holes in the rear spar of the left and right wings. This action is necessary to prevent fatigue cracking of the rear spar of the wings,
5 PROPOSED RULES: Boeing,
This document proposes the supersedure of an existing airworthiness directive (AD), applicable to all Boeing Model 737100, 200, 200C, 300, 400, and 500 series airplanes, that currently requires repetitive inspections to find cracks, fractures, or corrosion of each carriage spindle of the left and right outboard midflaps; and corrective action, if
6 RULES: Boeing,
This document corrects a typographical error that appeared in airworthiness directive (AD) 20020616 that was published in the Federal Register on April 2, 2002 (67 FR 15468). The typographical error resulted in reference to an incorrect STC number. This AD is applicable to certain Boeing Model 767300 airplanes. This AD requires removing each
7 RULES: Pilatus Aircraft Ltd.,
This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC12 and PC 12/45 airplanes. This AD requires you to replace certain push switch caps on the electrical power management overhead panel with parts of improved design. This AD is the result of mandatory continuing airworthiness
8 PROPOSED RULES: Eurocopter France,
This document revises an earlier proposed airworthiness directive (AD) for the specified Eurocopter France (ECF) model helicopters that proposed a daily inspection of the tail rotor pitch control rod (control rod) outboard spherical bearing (bearing), a radial and axial play limit, a revised AD compliance interval, and adding the ECF Model AS350B3
9 RULES: Raytheon,
This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Model 1900D airplanes. This AD requires you to accomplish a onetime inspection for missing rivets on certain areas of the airplane and, if necessary, install rivets. This AD is the result of Raytheon identifying several instances
10 RULES: McDonnell Douglas,
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas airplanes, that requires inspections of the linear variable differential transducers (LVDTs) of the autopilot for discrepancies, and followon actions if necessary. This amendment is prompted by information from the manufacturer advising that certain
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