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PROPOSED RULES: Raytheon,
Published: 2000-08-14
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Model BAe.125, Hawker 800
(U125A), and Hawker 800XP series airplanes. This proposal would
require removal of existing clamps, bedding tapes, and rubber
connecting sleeves at the ends of the turbine air discharge duct and
the water separator, and
RULES: Eurocopter France,
Published: 2000-06-07
This amendment supersedes an existing airworthiness directive
(AD) that applies to Eurocopter France Model SA365N1, AS365N2, and
SA366G1 helicopters and that currently requires initial and repetitive
inspections of the tail rotor blade Kevlar tiebar (Kevlar tiebar) for
cracks or delaminations. This amendment requires the same actions
required by
RULES: British Aerospace,
Published: 2000-06-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain British Aerospace BAe Model ATP airplanes, that
requires repetitive inspections to detect discrepancies of the downlock
support assembly and attachment of the nose landing gear (NLG), and of
the bulkhead and adjacent structure in the NLG bay; and corrective
action, if
RULES: McDonnell Douglas,
Published: 2000-07-31
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC10 series airplanes,
that requires a onetime detailed visual inspection of the galley power
feeder cables and fuselage structure at a certain station to detect
chafing or arcing damage to the cables and structure or to detect
arcing damage to
RULES: Mitsubishi,
Published: 2000-07-24
This amendment clarifies information contained in
Airworthiness Directive (AD) 20000915, which currently requires you
to incorporate modifications to the airplane operating systems on all
Mitsubishi Heavy Industries, Ltd. (Mitsubishi) MU2B series airplanes.
The Federal Aviation Administration (FAA) inadvertently omitted service
information from
PROPOSED RULES: Boeing,
Published: 2000-06-28
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747400
series airplanes. This proposal would require repetitive inspections to
detect fatigue cracking of the longeron splice fittings at stringer 11
on the left and right sides at body station 2598, and various followon
actions.
PROPOSED RULES: Boeing,
Published: 2000-12-29
This document proposes the adoption of a new airworthiness
directive (AD) that would apply to certain Boeing Model 737300, 737
400, 737500, 737600, 737700, 737800, 757200, 757200PF, 757200CB,
and 757300 series airplanes. This proposal would require a test of the
two electrical circuits that close the fuel shutoff valve on the wing
spar, and repair,
PROPOSED RULES: Rolls-Royce Corp.,
Published: 2000-12-12
This document proposes to adopt a new airworthiness directive
(AD), applicable to RollsRoyce Corporation, (formerly Allison Engine
Company), AE 2100 and AE 3007 series engines. This proposed AD would
require a onetime acid etch inspection of the 2nd stage high pressure
turbine (HPT) wheel for cracks. If the wheel is cracked, this proposed
AD would
RULES: Raytheon,
Published: 2000-12-04
This amendment adopts a new airworthiness directive (AD) that
applies to certain Raytheon Aircraft Company (Raytheon) Beech Model 58 [[Page 75608]]
airplanes. This AD requires you to inspect the rudder bellcrank
interconnect tube for damage; replace or refinish the interconnect
tube, if necessary; and modify the floorboard. Four reports of damage
RULES: Boeing,
Published: 2000-11-21
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 747 series airplanes. This action
requires repetitive inspections and torque checks of the hanger
fittings and strut forward bulkhead of the forward engine mount and
adjacent support structure, and corrective actions, if necessary. This
action also
RULES: British Aerospace,
Published: 2000-11-08
This amendment adopts a new airworthiness directive (AD),
applicable to all British Aerospace (Jetstream) Model 4101 airplanes,
that requires a functional check of the rudder pedals to ensure full
and free movement at all rudder pedal positions, and modification of
the forward rudder pedal boxes. The actions specified by this AD are
intended to
RULES: Raytheon,
Published: 2000-10-30
This amendment adopts a new airworthiness directive (AD),
applicable to certain Raytheon Model DH.125, Model HS.125, Model
BH.125, Model BAe.125 Series 800A, Model Hawker 800, Model Hawker
800XP, and Model Hawker 1000 series airplanes, that requires leak
checks and inspections for corrosion of the pitot/static and stall vent
drain valves, and
PROPOSED RULES: Raytheon,
Published: 2000-10-18
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all Raytheon Aircraft Company (Raytheon) Beech
Models 35C33A, E33A, E33C, F33A, F33C, S35, V35, V35A, V35B, 36, and
A36 airplanes that incorporate a certain Teledyne Continental engine
configuration. The proposed AD would require you to repetitively
replace the
RULES: Agusta S.p.A.,
Published: 2000-10-02
This amendment adopts a new airworthiness directive (AD) for
Agusta S.p.A. (Agusta) Model A109K2 and A109E helicopters. This AD
requires replacing a certain main transmission aft support fitting (aft
support fitting) with an airworthy aft support fitting within specified
time intervals and establishes a retirement life for certain aft
support
PROPOSED RULES: Empresa Brasileira de Aeronautica, S.A.,
Published: 2000-09-20
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all EMBRAER Model EMB120
series airplanes, that currently requires revising the Airplane Flight
Manual (AFM) to include requirements for activation of the ice
protection systems and to add information regarding operation in icing
conditions;
RULES: Raytheon,
Published: 2000-09-18
This amendment adopts a new airworthiness directive (AD) that
applies to certain Raytheon Aircraft Company (Raytheon) Beech Models
1900C, 1900C (C12J), and 1900D airplanes. This AD requires you to
install a spiral wrap around the wing fuel quantity wiring harness and
apply an adhesive sealant to the Wiggins couplings on the internal fuel
tank
PROPOSED RULES: Agusta S.p.A.,
Published: 2000-05-03
This document proposes the adoption of a new airworthiness
directive (AD) applicable to Agusta S.p.A. Model A109A and A109A II
helicopters. This proposal would require radiographic inspection of the
internal surface of each main rotor blade spar (spar) for corrosion.
This proposal is prompted by the discovery of corrosion on the internal
surfaces
PROPOSED RULES: McDonnell Douglas,
Published: 2000-05-10
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC1010, 15, 30, 30F (KC10A military), and 40 series airplanes.
This proposal would require performing repetitive ultrasonic
inspections of the attaching bolts on the inboard and outboard support
on the inboard and
PROPOSED RULES: British Aerospace,
Published: 2000-08-29
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain British Aerospace
(Jetstream) Model 4101 airplanes. This proposal would require
inspection of certain components, and corrective action, if necessary.
This action is necessary to prevent loosening of the locknut holding
the main landing gear
PROPOSED RULES: Airbus,
Published: 2000-08-23
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Airbus Industrie Model A300,
A310, and A300600 series airplanes, that would have superseded an
existing AD that currently requires repetitive deployment tests of the
ram air turbine (RAT) and checks of the adjustment of the locking rod.
The proposed AD
RULES: Airbus,
Published: 2000-08-16
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Airbus Industrie Model A300 B2 and B4
series airplanes, that currently requires inspection of the fuselage
longitudinal lap joints and circumferential joints, and of the
stringers and doublers for bonding delamination and cracks; and
repairs, as necessary.
PROPOSED RULES: Boeing,
Published: 2000-08-10
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 727 series
airplanes. This proposal would require repetitive inspections of the
bearing support fitting of the forward trunnion on the main landing
gear (MLG) to detect corrosion and cracking; followon actions, if
necessary; and rework
PROPOSED RULES: Raytheon,
Published: 2000-08-08
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Raytheon Model Hawker 800A
(U125A) and Hawker 800XP series airplanes. This proposal would require
inspecting the roller clearance in the nose landing gear drag stay and
making any necessary adjustments. The proposal is prompted by reports
RULES: Eurocopter France,
Published: 2000-06-14
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France Model AS332L2 helicopters. This AD requires
inspecting for interference between the transmission flexible mounting
plate (plate) and the forward and aft shims (shims), replacing shims
and repairing the plate if interference is found, and inspecting the
plate for a
Part II: Department of Transportation, Federal Aviation Administration,
Published: 2000-07-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 series airplanes. This proposal would require modification of the
insulation blankets in the area surrounding the main external power
ground studs. This action is necessary to prevent smoke and fire in the
forward