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RULES: BAE Systems (Operations) Ltd.,
Published: 2005-06-28
The FAA is adopting a new airworthiness directive (AD) for all
BAE Systems (Operations) Limited Model BAe 146 and Avro 146RJ series
airplanes. This AD requires repetitive external eddy current
inspections of the forward fuselage skin to detect cracking due to
fatigue, and repair if necessary. This AD is prompted by evidence of
cracking due to
RULES: Airbus,
Published: 2005-07-06
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus transport category airplanes. This AD requires an
inspection to determine if suspect part numbers (P/Ns) and serial
numbers of certain Thales Avionics equipment are installed, and
replacement of any suspect part with a modified part having a new P/N.
This AD is prompted by
PROPOSED RULES: Shadin,
Published: 2005-08-17
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Shadin ADC2000 air data computers (ADC) installed on
airplanes. This proposed AD would require you to replace affected ADC
2000 units with a modified unit. This proposed AD results from reports
that certain ADC2000 units display incorrect altitude information on
the Electronic
PROPOSED RULES: Airbus,
Published: 2005-08-08
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Airbus Model A300 B4620, A310304, A310324, and A310325
airplanes. This proposed AD would require installing fused adaptors
between the external wiring harness and the intank wiring at the
connectors on the fuel tank wall of the auxiliary center tank (ACT).
This proposed AD is
PROPOSED RULES: Boeing,
Published: 2005-07-27
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 757200, 200CB, and 300 series airplanes.
This proposed AD would require repetitive detailed inspections for
proper functioning of the girt bar leaf springs for the escape slides
at passenger doors 1, 2, and 4, and corrective actions if necessary.
This proposed AD
RULES: Boeing,
Published: 2005-01-06
This amendment adopts a new airworthiness directive (AD), that
is applicable to certain Boeing Model 767300 and 767300F series
airplanes equipped with General Electric or Pratt & Whitney engines.
This AD requires reworking the wingtostrut diagonal braces and the
aft pitch load fittings of the wings, and reinstalling the diagonal
braces with new
RULES: EXTRA Flugzeugbau GmbH,
Published: 2005-01-19
The FAA adopts a new airworthiness directive (AD) to supersede
AD 980314, which applies to certain EXTRA Flugzeugbau GmbH (EXTRA)
Model EA300 and EA300/S airplanes. AD 980314 currently requires you
to inspect the upper longeron cutoutbridge for cracks, to repair any
cracks found, and to modify this area. This AD retains the actions of
AD 980314
PROPOSED RULES: Bombardier,
Published: 2005-02-01
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier Model DHC8102, 103, 106, 201, 202, 301,
311, and 315 airplanes. The subject of this proposed AD is the pilot's static system. This proposed AD would require
[[Page 5079]]
revising the airplane flight manual to include applicable procedures to
follow when the
PROPOSED RULES: Boeing,
Published: 2005-02-14
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 747 airplanes. This proposed AD would require
repetitive inspections of the dual side braces (DSBs), underwing
midspar fittings, and associated parts; other specified actions; and
corrective actions if necessary. This proposed AD also provides an
optional
PROPOSED RULES: Air Tractor, Inc.; correction,
Published: 2005-02-28
Correction
In proposed rule document 052507 beginning on page 6786 in the
issue of Wednesday February 9, 2005, make the following correction: Sec. 39.13 [Corrected]
On page 6788, in Sec. 39.13, in the third column, under the heading
What Airplanes Are Affected by This AD?, paragraph designation ``(b)''
should read paragraph designation
RULES: DG Flugzeugbau GmbH,
Published: 2005-12-28
The FAA adopts a new airworthiness directive (AD) for certain
DG Flugzeugbau GmbH Models DG800B and DG500MB sailplanes. This AD
requires you to modify the connection of the starter ring gear to the
lower drive belt pulley adapter. This AD results from mandatory
continuing airworthiness information (MCAI) issued by the airworthiness
authority for
PROPOSED RULES: McDonnell Douglas,
Published: 2005-12-20
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain McDonnell Douglas Model DC910,
20, 30, 40, and 50 series airplanes; Model DC981 (MD81), 82
(MD82), 83 (MD83), and 87 (MD87) airplanes; and Model MD88
airplanes. That proposed AD would have required repetitive inspections
and functional tests of the static
RULES: Airbus,
Published: 2005-12-14
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus transport category airplanes. This AD requires
repetitive eddy current inspections for cracks of the stiffener
fittings of the fuselage at frame (FR) 12A, and corrective actions if
necessary. This AD also provides a terminating action for the
inspections. This AD results
PROPOSED RULES: Boeing,
Published: 2005-03-23
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 757200 and 300 series airplanes. This
proposed AD would require inspecting for the part number, the serial
number, and the mark ``RETESTED'' on the reaction link of the main
landing gear (MLG), and replacing the reaction link of the MLG with a
retested reaction
PROPOSED RULES: Eurocopter France,
Published: 2005-12-05
This document proposes superseding an existing airworthiness
directive (AD) that currently applies to Eurocopter France (ECF) Model
SA 365N, N1, and AS 365N2 helicopters. That AD currently requires
inspecting the main gearbox (MGB) suspension diagonal crossmember
(diagonal crossmember) for cracks and replacing it with an airworthy
part if any
PROPOSED RULES: Short Brothers,
Published: 2005-04-01
This document revises an earlier proposed airworthiness
directive (AD), applicable to all Short Brothers Model SD360 series
airplanes, that would have required performing an inspection of the
shear attachment fitting for the fintofuselage front spar, and of the
shear cleat for the fin root rib at the aft spar location for
corrosion; reporting
PROPOSED RULES: BAE Systems (Operations) Ltd.,
Published: 2005-04-06
The FAA proposes to adopt a new airworthiness directive (AD)
for all BAE Systems (Operations) Limited (Jetstream) Model 4101
airplanes. This proposed AD would require the overhaul of certain
auxiliary components installed on the main landing gear (MLG) and nose
landing gear (NLG). This proposed AD is prompted by manufacturer
determination that
RULES: Boeing,
Published: 2005-04-11
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 747200F and 200C series
airplanes, that currently requires repetitive detailed inspections or a
onetime openhole high frequency eddy current inspection to detect
cracking of certain areas of the upper deck floor beams, and corrective
actions if
PROPOSED RULES: Bombardier,
Published: 2005-11-10
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier Model CL6001A11 (CL600), CL6002A12 (CL
601), and CL6002B16 (CL6013A, CL6013R, & CL604) airplanes. This
proposed AD would require modifying the rudder balance spring assembly
by installing a new adjustable balance spring, and rigging the assembly
to suit the rudder
PROPOSED RULES: Pratt & Whitney,
Published: 2005-11-02
The FAA proposes to supersede an existing airworthiness
directive (AD) for Pratt & Whitney (PW) JT9D series turbofan engines.
That AD currently requires revisions to the Airworthiness Limitations
Section (ALS) of the manufacturer's Instructions for Continued
Airworthiness (ICA) to include required enhanced inspection of selected
critical
RULES: Airbus,
Published: 2005-10-26
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Model A320111, 211, 212, and 231 airplanes. This AD
requires, for certain airplanes, modifying the cables and access holes
to the inner tank fuel pumps; and, for certain other airplanes,
inspecting the fuel pump access holes and modifying the access holes,
if necessary. This
PROPOSED RULES: Eurocopter France,
Published: 2005-10-17
This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (ECF) Model EC 155B and B1 helicopters. This
proposal would require inspecting an electrical cable bundle for wear.
If wear is present, the AD would require installing an airworthy cable
bundle and modifying the routing of the electrical cable bundles. This
PROPOSED RULES: Boeing,
Published: 2005-10-07
The FAA proposes to adopt a new airworthiness directive (AD)
for all Boeing Model 747 airplanes. This proposed AD would require the
following actions for the drive mechanism of the horizontal stabilizer:
Repetitive detailed inspections for discrepancies and loose ball
bearings; repetitive lubrication of the ballnut and ballscrew;
repetitive
RULES: General Electric,
Published: 2005-05-19
The FAA is adopting a new airworthiness directive (AD) for
General Electric (GE) CF680E1 series turbofan engines that have an
electronic control unit (ECU) with software version E.1.M. or earlier
installed. This AD requires installing improved software for the ECU.
This AD results from an uncommanded engine acceleration event caused by
a failure
PROPOSED RULES: Bombardier; Correction,
Published: 2005-09-30
The FAA is correcting a typographical error in an NPRM that
was published in the Federal Register on September 14, 2005 (70 FR
54316). The error resulted in an incorrect Docket No. The NPRM applies
to certain Bombardier Model DHC8400 series airplanes. The NPRM would
require an inspection of the laminated shims for cracks, damage, or
extrusion
