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RULES: Bombardier,
Published: 2003-05-29
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Bombardier Model CL6002B19 series
airplanes, that currently requires repetitive eddy current inspections
for cracking of the main landing gear (MLG) main fittings, and
replacement with new or serviceable MLG main fittings if necessary.
That AD also requires
RULES: Eurocopter France,
Published: 2003-06-11
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France (Eurocopter) Model AS332 C, L, and L1 helicopters.
This action requires revising the Rotorcraft Flight Manual (RFM)
Limitations section if certain fuel control units are installed. This
AD is prompted by the discovery of an anomaly in certain fuel control
units that may
PROPOSED RULES: Eagle Aircraft (Malaysia) Sdn. Bhd.,
Published: 2003-06-23
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Eagle Aircraft (Malaysia) Sdn. Bhd.
(Eagle) Model 150B airplanes. This proposed AD would require you to
modify the canard rear spar and the rear spar attachment bracket. This proposed AD is the result of mandatory continuing
[[Page 37103]]
airworthiness
PROPOSED RULES: Bombardier,
Published: 2003-07-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Model CL6002B19
(Regional Jet Series 100 & 440) airplanes. This proposal would require
revising the airworthiness limitations section of the Instructions for
Continued Airworthiness by incorporating new structural inspection
intervals for the
PROPOSED RULES: Air Cruisers Co.,
Published: 2003-07-18
The FAA proposes to supersede an existing airworthiness
directive (AD) for a certain Air Cruisers Company Emergency Evacuation
Slide/Raft System. That AD currently requires a onetime unpacking and
subsequent repacking of the slide/raft systems, identified by basic
part number (P/N) with dash numbers, and serial numbers (SNs) listed in
the AD, and
PROPOSED RULES: Rolls-Royce plc,
Published: 2003-07-30
The FAA proposes to adopt a new airworthiness directive (AD)
for RollsRoyce plc (RR) RB21122B series, RB211524B, 524C2, 524D4,
524G2, 524G3, and 524H series, and RB211535C and 535E series
turbofan engines with high pressure compressor (HPC) stage 3 disc
assemblies, part numbers (P/Ns) LK46210, LK58278, LK67634, LK76036,
UL11706, UL15358, UL22577,
RULES: Bombardier,
Published: 2003-08-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model CL6002B19 (Regional Jet Series
100 & 440) airplanes, that requires installing new vent tube assemblies
for the main fuel tanks; and, on certain airplanes, inspecting to
measure the clearance between the vent system tubing and the applicable
wing ribs,
RULES: McDonnell Douglas,
Published: 2003-09-02
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model MD11 and MD11F
airplanes, that requires a onetime visual inspection of the circuit
breakers to determine if discrepant circuit breakers are installed, and
corrective action if necessary. This action is necessary to prevent
internal overheating
PROPOSED RULES: Boeing,
Published: 2003-09-18
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 747 series
airplanes. This proposal would require repetitive inspections of the
nacelle struttowing attachment structure, and repetitive overhaul of
the diagonal brace and spring beam load paths, to maintain damage
tolerance
RULES: Grob-Werke,
Published: 2003-09-30
The FAA adopts a new airworthiness directive (AD) for all
GROBWERKE (GROB) Model G120A airplanes. This AD requires you to modify
the flight control system operating levers. This AD is the result of
mandatory continuing airworthiness information (MCAI) issued by the
airworthiness authority for Germany. We are issuing this AD to prevent
failure of a
PROPOSED RULES: New Piper Aircraft, Inc.,
Published: 2003-10-09
The FAA proposes to adopt a new airworthiness directive (AD)
for certain The New Piper Aircraft, Inc. (Piper) Model PA46500TP
airplanes. This proposed AD would require you to replace all electronic
control modules in the airplane electrical system with newly designed
modules. This proposed AD is the result of reports of smoke in the
cockpit and
PROPOSED RULES: Rolls-Royce plc,
Published: 2003-10-27
The FAA proposes to adopt a new airworthiness directive (AD)
for RollsRoyce plc (RR) RB211524 series turbofan engines, with
certain part number (P/N) intermediate pressure (IP) compressor stage 5
discs installed. This proposed AD would establish new reduced IP
compressor stage 5 disc cyclic limits. This action would also require
removing from
PROPOSED RULES: Cessna,
Published: 2003-11-13
The FAA proposes to supersede Airworthiness Directive (AD) 86-
2604, which applies to certain Cessna Aircraft Company (Cessna) 120,
140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182,
185, A185E, 190, 195, 205, 205A, 206, P206, P206E, TP206A, TU206,
TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and T337 series
airplanes.
PROPOSED RULES: Boeing,
Published: 2003-11-25
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 777200
series airplanes. This proposal would require a onetime general visual
inspection of wire bundles routed aft of electrical disconnect panel
AC2162 to determine their installation and separation, and corrective
actions, if
RULES: McDonnell Douglas,
Published: 2003-12-23
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas airplanes, that requires a one
time inspection for damage of the power feeder cables and surrounding
structure, and repair if necessary. For certain airplanes, this
amendment requires fabricating and installing a power feeder support
bracket assembly
PROPOSED RULES: Boeing,
Published: 2003-12-08
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 737100,
200, 200C, 300, 400, and 500 series airplanes. This proposal would
require repetitive inspections for corrosion and cracking of the pivot
hinge pins of the horizontal stabilizer, certain followon inspections,
and replacement
RULES: Boeing,
Published: 2003-12-01
This amendment supersedes 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 necessary. That
RULES: Boeing,
Published: 2003-01-03
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747 series airplanes, that
currently requires a onetime inspection to identify all alloy steel
bolts on the body station 1480 bulkhead splice, and corrective action
if necessary; and provides for optional terminating action for certain
RULES: Raytheon,
Published: 2003-01-22
This amendment adopts a new airworthiness directive (AD) that
applies to certain Raytheon Aircraft Company (Raytheon) 65, 90, 99,
100, 200, and 300 series, and Model 2000 airplanes. This AD requires
you to install new exterior operating instruction placards for the
airstair door and emergency exits. This AD is the result of Raytheon
improving the
RULES: Turbomeca S.A.,
Published: 2003-01-31
This amendment adopts a new airworthiness directive (AD), that
is applicable to Turbomeca S.A. Arriel 1 A2, 1 C, 1 C1, 1 C2, 1 D, 1
D1, 1 E2, 1 K, 1 K1, 1 S, 1 S1 and Arriel 2 B, 2 B1, 2 C, 2 C1, 2 S1
series turboshaft engines. This amendment requires the insertion of a
sleeve in the attachment boss of the compressor bleed valve, and
bonding the
PROPOSED RULES: NARCO Avionics Inc.,
Published: 2003-02-20
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to certain serial
numbers (SN's) of NARCO Avionics Inc. AT150 transponders. This proposal
would require modification to the transponder by adding a resistor and
transistor to the circuit board. This proposal is prompted by reports
of
PROPOSED RULES: Boeing,
Published: 2003-03-03
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 767
series airplanes, that currently requires a onetime inspection to
detect abrasion damage and installation discrepancies of the wire
bundles located below the P37 panel, and corrective action if
necessary. For airplanes already
RULES: Bell,
Published: 2003-03-18
This amendment supersedes an existing emergency airworthiness
directive (EAD), which was sent previously to all known U.S. owners and
operators of Bell Helicopter Textron Canada (Bell) helicopters by
individual letters. That EAD requires a visual check to ensure that the
two swashplate drive link cup washers (cup washers) are installed
correctly.
RULES: Raytheon,
Published: 2003-04-03
This amendment adopts a new airworthiness directive (AD) that
applies to certain Raytheon Aircraft Company (Raytheon) Model 390
airplanes. This AD requires you to incorporate information into the
FAAapproved Airplane Flight Manual (AFM) that would add requirements
for ``Landing Performance for Operation of the Airplane with Lift Dump
PROPOSED RULES: Boeing,
Published: 2003-04-17
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747 series
airplanes. This proposal would require repetitive inspections for
discrepancies of certain areas of the forward and aft sides of the body
station 2598 bulkhead, and repair if necessary. This action is
necessary to find