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RULES: Dornier,
Published: 2004-10-28
This amendment adopts a new airworthiness directive (AD),
applicable to certain Dornier Model 328100 and 300 series airplanes,
that requires inspection of the metal oxide varistor (MOV) modules and
transient absorption zener (TAZ) diodes to determine if those parts are
outside of tolerance limits, and replacement of MOV modules and TAZ
diodes with
PROPOSED RULES: Boeing,
Published: 2004-11-05
The FAA proposes to supersede an existing airworthiness
directive (AD) for certain Boeing Model 727 series airplanes. That AD
currently requires repetitive detailed inspections to detect cracking,
corrosion, and existing stopdrilled repairs of cracking in the upper
chord of the rear spar of the wing, and repair if necessary. This
proposed AD would
RULES: Airbus,
Published: 2004-11-15
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A319 and A320 series airplanes, that
requires a modification and replacement affecting all fuel tanks. All
affected airplanes require the installation of fuses in the wiring of
the fuel quantity indicating probes of all fuel tanks. Some affected
airplanes
RULES: Rolls-Royce Corp.,
Published: 2004-12-01
The FAA is adopting a new airworthiness directive (AD) for
certain RRC 250B and 250C series turboshaft and turboprop engines.
This AD requires a onetime inspection of the fuel nozzle screen for
contamination, and if contamination is found, inspection and cleaning
of the entire aircraft fuel system before further flight. This AD also
requires
PROPOSED RULES: Boeing,
Published: 2004-12-14
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 737600, 700, and 800 series airplanes. This
proposed AD would require doing a general visual inspection for sealant
at the interface of the upper spar fittings, strut side skins, and the
fittings of the thrust reverser strut fairing on the engine struts; and
PROPOSED RULES: Pratt & Whitney,
Published: 2004-12-30
The FAA proposes to adopt a new airworthiness directive (AD)
for Pratt & Whitney (PW) JT8D1, 1A, 1B, 7, 7A, 7B, 9, 9A, 11,
15, 15A, 17, 17A, 17R, 17AR, 209, 217, 217A, 217C, and 219
turbofan engines. This proposed AD would require removing affected
rotating parts overhauled by a certain repair vendor, and inspecting or
replacing the parts as
RULES: General Electric Co.; correction,
Published: 2004-01-14
This document makes a correction to Airworthiness Directive
(AD) 20032611 applicable to GE CF680E1A2 and 80E1A4 turbofan
engines with left vertical link bolts part number (P/N) 1304M26P02
installed, and pylon attachment bolts originally torqued to 450500 lb
ft. That AD was published in the Federal Register on January 6, 2004
(69 FR 494). The
RULES: McDonnell Douglas,
Published: 2004-01-30
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC981 (MD81), DC982
(MD82), DC983 (MD83), DC987 (MD87), and MD88 airplanes. This
action requires a onetime visual inspection to determine if discrepant
circuit breakers are installed, and corrective action if necessary.
This action is necessary
RULES: Boeing,
Published: 2004-02-09
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747200C and 200F series airplanes,
that requires repetitive inspections to find fatigue cracking in the
upper chord of the upper deck floor beams, and repair if necessary. For
certain airplanes, this amendment also provides an optional repair/
modification,
RULES: Boeing,
Published: 2004-02-18
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 727, 727C, 727100, and 727100C series
airplanes, that requires repetitive detailed and special detailed
inspections for cracks in the web, inner chord, and outer chord of the
forward and aft frames of the aft cargo door opening; and repair of any
crack found.
RULES: AeroSpace Technologies of Australia Pty Ltd.,
Published: 2004-03-03
The FAA adopts a new airworthiness directive (AD) for all
AeroSpace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N22S,
and N24A airplanes. This AD requires you to repetitively inspect wing
fittings for fatigue defects, replace or correct defective wing
fittings, and replace the stub wing front spar assembly and wing
fitting when fatigue
RULES: Boeing,
Published: 2004-03-09
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Boeing Model 737600, 700, 700C, 800, and 900
series airplanes. This action requires an inspection of the rear spar
attach pins and front spar attach bolts that attach the horizontal
stabilizers to the horizontal stabilizer center section for damage; and
followon or
PROPOSED RULES: Bombardier,
Published: 2004-03-17
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model CL600
2B19 (Regional Jet Series 100 & 440) airplanes. This proposal would
require repetitive detailed and eddy current inspections on the main
fittings of the main landing gears (MLG) to detect discrepancies, and
related
RULES: Saab,
Published: 2004-03-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain Saab Model SAAB 2000 series airplanes, that
requires measuring the torque of the adjustable pin in the rear
attachment of the intermediate strut for both engines, and retorquing
the adjustable pins to the correct torque value. This action is
necessary to prevent
PROPOSED RULES: Saab,
Published: 2004-04-01
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Saab Model SAAB SF340A and
SAAB 340B series airplanes. This proposal would require inspection of
the main landing gear's (MLG) separation bolt harness, corrective
actions if necessary, and replacement of the MLG's separation bolt
harness. For
PROPOSED RULES: de Havilland,
Published: 2004-04-12
The FAA proposes to adopt a new airworthiness directive (AD)
for all deHavilland Inc. Models DHC2 Mk. I and DHC2 Mk. II airplanes
and for all Bombardier Inc. Model (Otter) DHC3 airplanes powered by
radial engines. This proposed AD would require you to visually inspect
the firewall ignition plugs and receptacles for proper lockwire
security and
PROPOSED RULES: Short Brothers,
Published: 2004-04-22
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Short Brothers Model SD360
series airplanes. This proposal would require inspection of the welded
joints of the balance weight brackets for the left and right elevator
trim tabs for cracking; repetitive inspections, as applicable; and
corrective
RULES: Boeing,
Published: 2004-05-05
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 767 series airplanes powered
by General Electric or Pratt & Whitney engines, that currently requires
repetitive inspections to detect discrepancies of the four aftmost
fastener holes in the horizontal tangs of the midspar fitting of the
strut,
RULES: Bombardier,
Published: 2004-05-11
This amendment revises an existing airworthiness directive
(AD), applicable to certain Bombardier Model DHC8102, 103, 106,
201, 202, 301, 311, and 315 series airplanes, that currently
requires repetitive inspections for discrepancies of certain rear spar
fittings between the flex shaft of the flap secondary drive and the
wingtofuselage structure,
PROPOSED RULES: Bombardier,
Published: 2004-05-19
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model CL600
2C10 (Regional Jet Series 700 & 701) series airplanes. This proposal
would require an inspection of the thrust reverser cascades for correct
installation; removing and reinstalling the cascade in the correct
location, if
PROPOSED RULES: Short Brothers,
Published: 2004-06-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Short Brothers Model SD3
series airplanes. This proposal would require installing a new warning
annunciator light on the central warning panel and revising the Normal
Procedures Section of the Aircraft Flight Manual to provide the
flightcrew with
RULES: Boeing,
Published: 2004-06-16
This amendment revises an existing airworthiness directive
(AD), applicable to certain Boeing Model 737100, 200, 200C, 300,
400, and 500 series airplanes, that currently requires replacing
existing screw, nut, and washers that attach the latch cable assembly
to the latch block assembly of the door mounted escape slides, with
new, improved screw,
RULES: Lycoming Engines,
Published: 2004-06-28
This document makes corrections to Airworthiness Directive
(AD) 20041014, applicable to Lycoming Engines (formerly Textron
Lycoming), directdrive reciprocating engines that was published in the
Federal Register on May 21, 2004 (69 FR 29210). Some corrections to
engine models have been made by adding missing dashes, clarification to
changes in
RULES: Airbus,
Published: 2004-07-09
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Airbus Model A330, A340200, and A340300
series airplanes, that currently requires repetitive inspections to
check the play of the eyeend of the piston rod of the elevator servo
controls, and followon corrective actions if necessary. This amendment
requires the
PROPOSED RULES: Grob-Werke,
Published: 2004-07-15
The FAA proposes to adopt a new airworthiness directive (AD)
for all GROBWERKE (GROB) Model G120A airplanes. This proposed AD would
require you to repetitively inspect visually the area between the
vertical stabilizer main spar and the nearby vertical stabilizer skin
for any disbonding/crack; repair any disbonding/crack found; and
calculate weight