200020012002200320042005200620072008
Pages:
«<2223242526
PROPOSED RULES: Boeing,
Published: 2000-09-18
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 767 series
airplanes. This proposal would require a onetime detailed visual
inspection of certain wire bundles located in the aft section of the
strut forward fairing panel of both engine struts to detect chafing
damage, and repair
PROPOSED RULES: Bell,
Published: 2000-05-03
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to Bell Helicopter Textron Canada
(BHTC) Model 430 helicopters. This proposal would require replacing arm
clamp screws (screws) in the yaw, roll, pitch, and collective syncro
resolvers, and installing a guard bracket on the yaw, roll, pitch, and
collective
PROPOSED RULES: Raytheon,
Published: 2000-05-10
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Raytheon (Beech) Model MU300,
MU30010, 400, and 400A series airplanes. This proposal would require
repetitive inspections of the bleed air supply tube assemblies for
discrepancies; and replacement of the bleed air tube assembly with a
new bleed air
PROPOSED RULES: McDonnell Douglas,
Published: 2000-05-16
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC8 series airplanes that have been converted from a passenger to a
cargocarrying (``freighter'') configuration. This proposal would
require a revision to the Airplane Flight Manual Supplement to ensure
that the main deck
PROPOSED RULES: Bombardier,
Published: 2000-08-23
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Bombardier Model
DHC8102, 103, and 301 series airplanes, that currently requires a
onetime inspection for wear and breakage of wire segments of the
individual lighting units of the ceiling and sidewall lights, and
replacement of any damaged
RULES: Bell,
Published: 2000-08-16
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron Canada (BHTC) Model 430 helicopters. This AD
requires replacing arm clamp screws (screws) in the yaw, roll, pitch,
and collective syncro resolvers, and installing a guard bracket on the
yaw, roll, pitch, and collective syncro resolvers. This AD is prompted
by an
RULES: Fokker,
Published: 2000-06-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Fokker Model F.28 Mark 1000, 2000, 3000, and 4000
series airplanes, that requires a onetime review of the maintenance
records to determine if tripping of the fuel boost pump circuit
breakers has been recorded, repetitive inspections to detect fuel
leakage from the fuel
PROPOSED RULES: Raytheon,
Published: 2000-08-08
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Model Hawker 800XP and
Hawker 800 (U125A) series airplanes. This proposal would require
inspection of the wire bundle to relay `KT' on panel `JA' for correct
routing, adequate clearance from the fuel crossfeed valve operating
lever, and the
RULES: Fokker,
Published: 2000-06-14
This amendment adopts a new airworthiness directive (AD),
applicable to certain Fokker Model F27 Mark 050, 100, 200, 300, 400,
500, 600, and 700 series airplanes, and Model F28 Mark 0070, 0100,
1000, 2000, 3000, and 4000 series airplanes, that requires a onetime
functional test to verify correct installation of the shoulder
harnesses of the
PROPOSED RULES: Eurocopter Canada Ltd.,
Published: 2000-06-19
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to Eurocopter Canada Ltd.
Model BO 105 LS A3 helicopters. That AD currently requires, before
further flight, creating a component log card or equivalent record, and
determining the calendar age and number of flights on each tension
torsion (TT) strap, and
PROPOSED RULES: Bell,
Published: 2000-07-20
This document proposes the adoption of a new airworthiness
directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 407
helicopters. This proposal would require inspecting the brackets that
attach each horizontal stabilizer slat (slat) to the stabilizer for a
crack and replacing the slat assembly if a crack is found. Installing
airworthy
RULES: Saab,
Published: 2000-07-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain Saab Model SAAB SF340A and SAAB 340B series
airplanes, that requires replacing the smoke detectors in the cargo
compartment with new, improved smoke detectors. This amendment is
prompted by issuance of mandatory continuing airworthiness information
by a foreign civil
PROPOSED RULES: Boeing,
Published: 2000-12-22
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 767 series
airplanes. For certain airplanes this proposal would require rework of
the bonding jumper assemblies. For certain other airplanes, this
proposal would require repetitive inspections of the drain tube
assemblies of the
PROPOSED RULES: British Aerospace,
Published: 2000-12-05
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all British Aerospace
(Jetstream) Model 4101 airplanes, that currently requires repetitive
inspections to detect loose or migrated levers of the elevator cable
tension regulators, and replacement of the regulator assembly with a
new assembly, if
RULES: Boeing,
Published: 2000-11-28
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 777 series airplanes, that
currently requires repetitive testing of the engine fire shutoff switch
(EFSS) to determine if the override mechanism and the switch handle are
operational, and replacement of the EFSS, if necessary. That AD also
requires,
RULES: Bell,
Published: 2000-11-15
This document publishes in the Federal Register an amendment
adopting superseding Airworthiness Directive (AD) 20001851 which was
sent previously to all known U.S. owners and operators of Bell
Helicopter Textron, Inc. (BHTI) Model 47B, 47B3, 47D, 47D1, 47G, 47G
2, 47G2A, 47G2A1, 47G3, 47G3B, 47G3B1, 47G3B2, 47G3B2A, 47G
4, 47G4A, 47G5, 47G5A, 47H1,
PROPOSED RULES: Airbus,
Published: 2000-11-03
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Airbus Model A319, A320, and
A321 series airplanes. This proposal would require revising the
Airworthiness Limitations Section of the Instructions for Continued
Airworthiness to incorporate service life limits for certain items and
inspections to
RULES: Pratt & Whitney,
Published: 2000-10-24
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Pratt & Whitney JT8D200 series turbofan
engines, that currently requires revisions to the Time Limits Section
(TLS) of the JT8D200 Turbofan Engine Manual to include required
enhanced inspection of selected critical lifelimited parts at each
piecepart
PROPOSED RULES: Bombardier,
Published: 2000-10-12
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC7
100, 101, 102, and 103 series airplanes. This proposal would require
inspecting the endcaps of the main landing gear selector valve for
leaks of hydraulic oil and, if leaks are detected, replacing the
leaking endcaps or the
PROPOSED RULES: Airbus,
Published: 2000-09-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A330 and A340
series airplanes. This proposal would require modification of the rib
1/wing center spar attachment. This action is necessary to prevent
fatigue cracking at the rib 1/center spar angle and bottom corner
fitting, which
PROPOSED RULES: Boeing,
Published: 2000-04-28
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 737
100, 200, 300, 400, and 500 series airplanes. That AD currently
requires inspection of the fueling float switch wiring in the center
fuel tank to detect discrepancies, accomplishment of corrective
actions, and installation of
PROPOSED RULES: Airbus,
Published: 2000-09-08
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Airbus Model A300 and A300600
series airplanes. This proposal would require verifying the correct
location of the labels of the hydraulic pipes supplying the strut
unlocking actuator of the lefthand main landing gear (MLG), and of the
pipes of the
PROPOSED RULES: Cessna; withdrawn,
Published: 2000-08-31
This document withdraws a notice of proposed rulemaking (NPRM)
that would have applied to all Cessna Aircraft Company (Cessna) Models
425 and 441 airplanes. The proposed AD would have required you to
revise the Airplane Flight Manual (AFM) to include requirements for
activation of the airframe pneumatic deicing boots. The proposed AD was
the
PROPOSED RULES: Bell,
Published: 2000-05-17
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to Bell Helicopter Textron
Canada (BHTC) Model 407 helicopters, that currently requires installing
a tail rotor pitchlimiting leftpedal stop (pedal stop), installing an
airspeed limitation placard, marking a neverexceed velocity (Vne)
placard on all
RULES: Boeing,
Published: 2000-08-21
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 777200 series airplanes, that
currently requires a onetime inspection to determine the serial
numbers of various switch modules on the overhead panel and control
stand, and replacement of certain switch modules with new, improved
modules. That AD