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PROPOSED RULES: Garmin AT and Apollo GX series global positioning system navigation units with software versions 3.0 through 3.4 inclusive,
Published: 2004-04-01
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to aircraft equipped with Garmin AT,
Apollo GX series GPS navigation units with software versions 3.0
through 3.4 inclusive. This proposal would require modification and
testing of the software for Apollo GX50/55/60/65 TSOC129a GPS
navigation units; and
PROPOSED RULES: Air Tractor, Inc.,
Published: 2004-04-09
The FAA proposes to supersede Airworthiness Directive (AD)
20021910, which applies to certain Air Tractor, Inc. (Air Tractor)
Models AT402, AT402A, AT402B, AT602, AT802, and AT802A airplanes.
AD 20021910 currently requires you to repetitively inspect the upper
longeron and upper diagonal tube on the left hand side of the aft
fuselage structure for
PROPOSED RULES: Airbus,
Published: 2004-04-22
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all
[[Page 21775]]
Airbus Model A330200 and 300 and A340200, 300, 500, and 600
series airplanes. This proposal would require a onetime inspection of
each emergency evacuation slide raft installed on Type ``A'' exit doors
equipped with regulator valves
RULES: Boeing; correction,
Published: 2004-05-03
This document corrects a typographical error that appeared in
airworthiness directive (AD) 20040722 that was published in the
Federal Register on April 7, 2004 (69 FR 18250). The typographical
error resulted in reference to an incorrect paragraph number. This AD
is applicable to all Boeing Model 747 series airplanes. This AD
requires that the
RULES: Boeing,
Published: 2004-05-11
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747400 and 747400D series
airplanes, that requires a detailed inspection of the fire
extinguishing system tube and clamp for correct installation or a
repetitive pressure test of the fire extinguishing system tube for
leakage, and corrective action, if
PROPOSED RULES: General Electric,
Published: 2004-05-18
The FAA proposes to adopt a new airworthiness directive (AD)
for GE CF343A, CF343A2, CF341A, CF343A1, CF343B, and CF343B1
series turbofan engines. This proposed AD would require removal from
service of certain high pressure compressor (HPC) forward spools, at
the first piecepart level exposure after 6,000 cycles since new (CSN),
but not later than
PROPOSED RULES: Bombardier,
Published: 2004-06-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Bombardier Model CL6002B19
(Regional Jet Series 100 & 440) airplanes. This proposal would require
repetitive inspections of the check valves and air supply ducts of the
rear bulkhead for damage, and related corrective actions. This proposal
also
PROPOSED RULES: Honeywell,
Published: 2004-06-16
The FAA proposes to adopt a new airworthiness directive (AD)
for Honeywell International Inc. (formerly AlliedSignal Inc. and
Garrett Turbine Engine Co.) TFE7312 and 3 series turbofan engines
with certain part number (P/N) low pressure turbine (LPT) stage 1 disks
installed. This proposed AD would require for TFE7312 and 2C series
engines, initial
RULES: Agusta S.p.A.,
Published: 2004-06-25
This amendment revises an existing airworthiness directive
(AD), for the Agusta S.p.A. (Agusta) Model A109C, A109E, and A109K2
helicopters, that currently requires inspecting the main rotor blade
(blade) tip cap for bonding separation and a crack, and also requires a
tap inspection of the tip cap for bonding separation in the blade bond
area and a
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2004-07-08
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Model EMB135 and 145 series airplanes. This proposed AD
would require modifying the total air temperature (TAT) sensor heating
system. This proposed AD is prompted by a report that the fully
automated digital electronic control (FADEC) unit failed to compensate
for ice
PROPOSED RULES: Airbus,
Published: 2004-07-15
The FAA proposes to supersede an existing airworthiness
directive (AD) for certain Model A310; and Model A300 B4600, A300 B4
600R, and A300 F4600R (collectively called A300600) series airplanes.
That AD currently requires modifying the ram air turbine (RAT) by
replacing the ejection jack. This proposed AD would require a onetime
inspection of the
PROPOSED RULES: MD Helicopters, Inc.,
Published: 2004-07-29
This document proposes adopting a new airworthiness directive
(AD) for the MD Helicopters, Inc. Model 600N helicopters. The AD would
require replacing the fuselage Station 75 control support bracket
assembly (control support bracket), reducing the life limit, and
revising the Limitations section of the applicable maintenance manual
to state the
RULES: Boeing,
Published: 2004-08-09
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 767200 and 300 series airplanes
equipped with offwing escape slides, that requires an inspection of
the dooropening actuators for the offwing slide compartment on the
right and left sides of the airplane to determine the actuator
cartridge serial number,
PROPOSED RULES: Pilatus Aircraft Ltd.,
Published: 2004-08-20
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Pilatus Aircraft Ltd. (Pilatus) Model PC7 airplanes with
any Lear Romec RR53710B type or Lear Romec RR53710K fuel booster pump
(Pilatus part number 968.84.11.401; 968.84.11.403; or 968.84.11.404)
installed. This proposed AD would require you to check the airplane
logbook to
RULES: Airbus,
Published: 2004-09-14
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Airbus Model A300 B2 and B4 series
airplanes, and Model A300 B4601, B4603, B4605R, B4620, B4622R, C4
605R Variant F, and F4605R airplanes, that currently requires a one
time inspection for cracking of the gantry lower flanges in the main
landing gear (MLG) bay
PROPOSED RULES: Boeing,
Published: 2004-09-29
The FAA proposes to supersede an existing airworthiness
directive (AD) for all Boeing Model 767200, 300, and 300F series
airplanes. That AD currently requires examination of maintenance
records to determine if Titanine JC5A (also known as Desoto 823E508)
corrosion inhibiting compound (``C.I.C.'') was ever used; inspection
for cracks or corrosion
RULES: Empresa Brasileira de Aeronautica, S.A. (EMBRAER),
Published: 2004-10-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain EMBRAER Model EMB135 and EMB145 series
airplanes, that requires inspection of the housings of the main landing
gear (MLG) leg strut bushings, and related investigative and corrective
actions, and other specified actions. The actions specified by this AD
are intended to
RULES: Eurocopter Deutschland,
Published: 2004-11-02
This amendment supersedes an existing airworthiness directive
(AD) for Eurocopter Deutschland GmbH (Eurocopter) Model EC135 P1, P2,
T1, and T2 helicopters. That AD currently requires adding the AD or a
statement to the Rotorcraft Flight Manual (RFM) informing the pilot to
reduce power and land as soon as practicable if a thumplike sound
followed
RULES: McDonnell Douglas,
Published: 2004-11-09
The FAA is adopting a new airworthiness directive (AD) for
certain McDonnell Douglas Model MD11 airplanes. This AD requires
revising the cable connection stackups for midcabin terminal strips,
replacing the terminal strips, and removing a nameplate, as applicable.
This AD also requires an inspection for arcing damage in the midcabin
area, and
RULES: McCauley Propeller Systems,
Published: 2004-11-22
The FAA is adopting a new airworthiness directive (AD) for
McCauley Propeller Systems propeller assemblies, part numbers (P/Ns)
B5JFR36C1101/114GCA0, C5JFR36C1102/L114GCA0, B5JFR36C1103/114HCA0,
and C5JFR36C1104/L114HCA0, installed on BAE Systems (Operations)
Limited Jetstream Model 4100 series airplanes. This AD requires a one
time eddycurrent
PROPOSED RULES: Boeing,
Published: 2004-12-03
The FAA proposes to supersede an existing airworthiness
directive (AD) for certain Boeing Model 747 series airplanes. That AD
currently requires a onetime inspection to determine the material type
of the stop support fittings of the main entry doors (MEDs). That AD
also currently requires repetitive detailed inspections to detect
cracks of certain
RULES: Raytheon,
Published: 2004-12-16
The FAA adopts a new airworthiness directive (AD) for certain
Raytheon Aircraft Company, Model 390, Premier 1 airplanes. This AD
requires you to inspect the routing and security of the left and right
main landing gear (MLG) squat switch wire harness installations for
damage, repair any damage or replace components, and reinstall the
squat switch
RULES: Boeing,
Published: 2004-01-07
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747 series airplanes, that requires
identification of the valves installed on the engine struts as
hydraulic supply (fire) shutoff valves for the enginedriven pump,
corrective action if necessary, and eventual replacement of discrepant
valves with
PROPOSED RULES: Saab,
Published: 2004-01-22
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Saab Model SAAB 2000
series airplanes. This proposal would require repetitive inspections of
the installation of the spoilers of the windshield wiper assemblies for
discrepancies, and replacement with new spoilers if necessary. The
proposal also
PROPOSED RULES: Boeing,
Published: 2004-02-06
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing transport category
airplanes listed above, that would have required drilling witness holes
through the cowl skin at the cowl latch locations in the lefthand side
of the cowl panel assembly of each engine. This new action revises the
proposed rule
