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RULES: Goodrich Avionics Systems, Inc.,
Published: 2003-06-30
This amendment adopts a new airworthiness directive (AD) that
applies to all Goodrich Avionics Systems, Inc. (Goodrich) TAWS8000
terrain awareness warning systems (TAWS) that are installed on
airplanes. This AD requires you to inspect the TAWS installation and
remove any TAWS where both the TAWS and any other device are connected
to the same baro
PROPOSED RULES: GROB-WERKE,
Published: 2003-07-15
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all GROBWERKE (GROB) Model G120A airplanes.
This proposed AD would require you to modify the flight control system
operating levers. This proposed AD is the result of mandatory
continuing airworthiness information (MCAI) issued by the airworthiness
authority for
PROPOSED RULES: Saab,
Published: 2003-07-21
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 an inspection to detect
chafing or damage to the electrical wire harnesses in the left and righthand wing fuel
[[Page 43043]]
tanks, applicable corrective action(s) if necessary,
RULES: McDonnell Douglas,
Published: 2003-08-08
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model MD11 and 11F airplanes,
that requires modifying the overhead instrument lighting by relocating
the dimmer control unit and revising the wire routing. This action is
necessary to prevent overheating and internal component failure of the
dimmer
RULES: McCauley Propeller Systems, Inc.,
Published: 2003-08-21
The FAA is superseding an existing airworthiness directive
(AD) for McCauley Systems, Inc. propellers that are installed on, but
not limited to, BAE Systems (Operations) Limited Jetstream Model 4101
airplanes. That AD currently requires a onetime fluorescent penetrant
inspection (FPI) of propeller blade retention areas for cracks. This AD
requires
PROPOSED RULES: Airbus,
Published: 2003-09-08
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A300 B4600
Series Airplanes, Model A300 B4600R Series Airplanes, Model A300 C4
605R Variant F Airplanes, and Model A300 F4605R Airplanes. This
proposal would require modification of certain components of the 115
Volts Alternating
PROPOSED RULES: Boeing,
Published: 2003-09-19
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing Model 737300, 400, and
500 series airplanes, that would have required replacement of the hinge
assemblies on certain escape slide compartments of the forward doors
with new, stronger hinge assemblies. This new action revises the
proposed rule by
RULES: General Electric Co.,
Published: 2003-10-03
The FAA is adopting a new airworthiness directive (AD) for
General Electric Company (GE) CF680E1A2 turbofan engines with forward
engine mount platforms part numbers (P/Ns) 1520M53G04 and 1846M24G15
installed. This AD requires initial and repetitive fluorescent
penetrant inspections of cast material forward engine mount platforms.
This AD is
PROPOSED RULES: McDonnell Douglas,
Published: 2003-10-15
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas
airplanes as listed above. This proposal would require modification of
the installation wiring for the electric motor operated auxiliary
hydraulic pumps in the right wheel well area of the main landing gear,
and repetitive
PROPOSED RULES: Bombardier,
Published: 2003-11-05
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier Inc. (formerly deHavilland Inc.) Model Otter DHC3 airplanes that have turbine engines
[[Page 62546]]
installed per one of three supplemental type certificates (STC). This
proposed AD would prohibit you from operating any affected airplane
with these engine and
PROPOSED RULES: Airbus,
Published: 2003-11-18
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A320
111, 211, and 231 series airplanes, that currently requires
repetitive inspections for cracking in the transition and pickup
angles in the lower part of the center fuselage area, and corrective action if
[[Page 65009]]
PROPOSED RULES: AeroSpace Technologies of Australia Pty Ltd.,
Published: 2003-12-29
The FAA proposes to adopt a new airworthiness directive (AD)
for all AeroSpace Technologies of Australia Pty Ltd Model N22B, N22S,
and N24A airplanes. This proposed AD would require you to inspect the
forward and aft face of the rear fuselage frame for cracks and to
repair or modify accordingly. This proposed AD is the result of
mandatory continuing
PROPOSED RULES: Airbus,
Published: 2003-12-17
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A300
B4 series airplanes and all Airbus Model A300600 series airplanes.
That AD currently requires a onetime high frequency eddy current
inspection to detect cracking of the splice fitting at fuselage frame
(FR) 47 between
RULES: New Piper Aircraft, Inc.,
Published: 2003-12-03
This amendment adopts a new airworthiness directive (AD) that
applies to all The New Piper Aircraft, Inc. (Piper) Models PA31, PA 31300, PA31325, PA31350, PA31P, PA31T, PA31T1, PA31T2, PA
31T3, and PA31P350 airplanes. This AD requires you to install an
inspection hole (or use for inspection the tooling hole in the rudder
bottom rib), conduct a
RULES: Air Tractor, Inc.,
Published: 2003-01-02
This amendment supersedes Airworthiness Directive (AD) 2002-
1103, which applies to certain Air Tractor, Inc. (Air Tractor) Models
AT502, AT502A, AT502B, and AT503A airplanes. AD 20021103 lowered
the safe life for the wing lower spar cap and further reduced the safe
life for airplanes that incorporate or have incorporated Marburger
Enterprises,
RULES: Saab,
Published: 2003-01-06
This amendment adopts a new airworthiness directive (AD),
applicable to all Saab Model SAAB 2000, SAAB SF340A, and SAAB 340B
series airplanes, that requires replacing the main pitot static tube on
each side of the airplane with a new improved pitot static tube, and
installing a gasket between the tube and the airplane structure. The
actions
PROPOSED RULES: Boeing,
Published: 2003-01-28
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing Model 767200, 300, and
300F series airplanes, that would have required a onetime inspection
for discrepancies of certain wire bundles in the forward cargo
compartment, and corrective actions, if necessary. This new action
revises the proposed rule
RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2003-02-07
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain EMBRAER Model EMB135 and 145 series
airplanes. This action requires replacement of the horizontal
stabilizer control units (HSCUs) with new upgraded HSCUs, and
corrective actions if necessary. This action is necessary to prevent
reversal of the pilot's pitch
PROPOSED RULES: Bell,
Published: 2003-02-26
This document proposes the supersedure of an existing
airworthiness directive (AD) that applies to specified type
certificated military surplus helicopters. That AD currently requires
visual and radiographic inspections of the Boom Station (BS) 194 skin
joint area and the vertical fin spar caps for cracks or fretting. This
action would require
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2003-03-05
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain EMBRAER Model EMB120
series airplanes. This proposal would require either revising the
Airplane Flight Manual (AFM) to require a maximum operating altitude of
25,000 feet; or modifying the flight attendant's seat, or reworking the
oxygen bottle
RULES: Hartzell Propeller Inc.,
Published: 2003-03-25
This amendment adopts a new airworthiness directive (AD), that
is applicable to certain Hartzell Propeller Inc. model HCC2Y(K,R)1BF/
F84774 propellers with TKS (Aircraft Deicing) Ltd. antiice boots
that were installed by SOCATAGroupe AEROSPATIALE, the aircraft
manufacturer, using TKS Ltd. Procedure P232, Specification for the
Attachment of
RULES: Rolls-Royce Deutschland Ltd. & Co. KG,
Published: 2003-04-11
This amendment supersedes an existing airworthiness directive
(AD), that is applicable to RollsRoyce Deutschland Ltd & Co KG (RRD)
(formerly RollsRoyce Deutschland GmbH, formerly BMW RollsRoyce GmbH)
models BR700710A110 turbofan engines with fan disc part numbers (P/
Ns) BRR18803, BRR19248, or BRR20791 installed, and BR700710A220
turbofan engines
RULES: Boeing,
Published: 2003-04-23
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Boeing Model 747100, 200B, 200F, 200C, 100B,
300, 100B SUD, 400, 400D, and 400F series airplanes; and Model 747SR
[[Page 19938]]
series airplanes. This action requires repetitive inspections to detect
discrepancies of the actuator attach fittings of the inboard and
RULES: Rolls-Royce Deutschland Ltd. & Co. KG,
Published: 2003-05-09
This document makes a correction to Airworthiness Directive
(AD) 20030711, applicable to RollsRoyce Deutschland Ltd & Co KG
(formerly RollsRoyce Deutschland GmbH, formerly BMW RollsRoyce GmbH),
models BR700710A110 and BR700710A220 turbofan engines. AD 200307
11 was published in the Federal Register on April 11, 2003 (68 FR
17727). Subsequently, a
RULES: Turbomeca S.A.,
Published: 2003-05-29
This amendment adopts a new airworthiness directive (AD), that
is applicable to Turbomeca S.A. Arrius 2F turboshaft engines with
certain serial number (SN) Fuel Control Units (FCUs). This amendment
requires adjusting the FCU maximum fuel flow mechanical stop position
to a higher fuel flow setting. This amendment is prompted by an FCU
discovered to