RULES: Boeing,
Published: 2001-07-24
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 747 series airplanes, that
currently requires repetitive inspections to detect cracking of the
forward and aft inner chords and the splice fitting of the forward
inner chord of the station 2598 bulkhead, and repair, if necessary.
This amendment adds
RULES: Pilatus Aircraft Ltd.,
Published: 2001-11-07
This amendment adopts a new airworthiness directive (AD) that
applies to all Pilatus Aircraft Ltd. (Pilatus) Models PC12 and PC12/
45 airplanes. This AD requires you to inspect the cargo doors to
identify front and rear end frames with plain lightening holes and
install reinforcing plates on any frame with plain lightening holes.
This AD is the
RULES: Bombardier,
Published: 2001-10-30
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model CL6002B19 series airplanes,
that requires repetitive eddy current inspections for cracking of the
main landing gear (MLG) main fittings, and replacement with a new or
serviceable MLG, if necessary. This action also requires servicing the
MLG shock
RULES: Airbus; correction,
Published: 2001-01-17
This document corrects a typographical error that appeared in
airworthiness directive (AD) 20002603, which was published in the
Federal Register on December 28, 2000 (65 FR 82262). The typographical
error resulted in the misidentification of affected airplanes. This AD
is applicable to Airbus Model A310, and Model A300 B4600, A300 B4
600R, and A300
PROPOSED RULES: Airbus,
Published: 2001-10-12
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Airbus Model A330 and A340
series airplanes. This proposal would require repetitive inspections
and operational checks of the spring function of the emergency exit
door slider mechanism, and corrective action if necessary. This action
is necessary
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 and 11F series airplanes. This proposal would require replacing
the wire harness support bracket of the integrated drive generator
(IDG) of the forward engine mounts with a new support bracket, and
modifying the
