This amendment supersedes an existing airworthiness directive (AD), applicable to certain Airbus Model A330 and A340 series airplanes, that currently requires an inspection of the parking brake operated valve (PBOV) of the main landing gear to identify the part and serial numbers, and followon actions if necessary. That AD also provides for

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas DC910, DC920, DC930, DC 940, and DC950 series airplanes; and Model DC981 (MD81), DC982 (MD82), DC983 (MD83), DC987 (MD87), and MD88 airplanes. This amendment requires replacement of the emergency power switch knob on the overhead switch panel in the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 777 series airplanes. This action requires revising the Airplane Flight Manual to specify that the engine antiice must be ``on'' during all ground and flight operations when icing conditions exist or are anticipated. This action is necessary to

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to Turbomeca S.A. Arrius2F turboshaft engines with certain serial number (SN) Fuel Control Units (FCU's). This proposal would require adjusting the FCU maximum fuel flow mechanical stop position to a higher fuel flow setting. This

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Raytheon Model Beech 400A and 400T series airplanes. This proposal would require replacement of the lowpressure oxygen tubing located in the forward fuselage (nose avionics bay), lower forward flight deck, and lower forward cabin areas, as

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

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 for missing bolts on the inboard and outboard support of the inboard main flap, and followon inspections and corrective actions, if necessary. For certain

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment revises an existing airworthiness directive (AD) that is applicable to CFMI CFM565C series turbofan engines. That AD currently establishes new life limits for certain low pressure turbine rotor (LPTR) stage 3 disks and certain high pressure turbine rotor (HPTR) disks. This action removes the LPTR stage 3 disks and the HPTR disks

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes to adopt a new airworthiness directive (AD) that would apply to all Short Brothers and Harland Ltd. (Shorts) Models SC7 Series 2 and SC7 Series 3 airplanes. This proposed AD would require you to repetitively inspect all flight control system rods for corrosion and cracks, replace any cracked rod, and repair corrosion damage

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) AS 350B3, SA365N, N1, AS 365N2, AS 365N3, and EC 155B helicopters. This proposal would require modifying the SIREN cargo hook and inspecting the cargo hook locking catch (locking catch) for corrosion. This proposal is prompted by the discovery of

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), that is applicable to General Electric (GE) CF348C1 turbofan engines. This amendment requires replacing combustion chamber assemblies, part number (P/N) 4126T87G04, before accumulating a new reduced cyclic life limit. This amendment is prompted by stress and life analysis conducted by GE.

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that is applicable to Turbomeca S.A. Arriel 1B, 1D, and 1D1 series turboshaft engines. This amendment requires replacement of modules M03 modified to TU 204 standard with modules M03 not modified to TU 204 standard. This amendment is prompted by several reports of 2nd stage gas generator

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes superseding an existing airworthiness directive (AD) for Eurocopter Deutschland GmbH (ECD) Model EC135 P1 and EC135 T1 model 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

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Aerospatiale Model ATR42200, 300, 320, and 500 series airplanes; and Model ATR72102, 202, 212, and 212A series airplanes; that requires modification of the flight attendant's seat located in the front of the cabin, and followon actions. This action is necessary to

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters that requires performing a continuity test, temporarily repairing any unairworthy chip detector, and replacing any repaired chip detectors. This amendment is prompted by reports of poor or no continuity between the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires removing certain main servocontrols and replacing them with servocontrols that do not fall within the ``Applicability'' of this AD at specified intervals. This amendment is prompted by the discovery of an

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes to revise Airworthiness Directive (AD) 20022217, which currently requires you to repetitively inspect the inboard forward flap bellcranks for cracks and eventually replace these bellcranks on all Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 20022217 resulted from Cessna reevaluating the bellcrank life

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA proposes to adopt a new airworthiness directive (AD) for RollsRoyce Corporation (formerly Allison Engine Company) AE 3007A1, AE 3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007A1E, and AE 3007A1P turbofan engines, with 1st to 2nd stage turbine spacers, part number (P/N) 23069627, 23070989, 23072849, or 23075364 installed. This proposed AD would

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing airplane models. This proposal would require a onetime inspection to identify all H11 steel bolts installed in the latch fittings of the cargo doors, repetitive inspections for cracked or broken H11 steel bolts, and followon and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to all Aerospatiale Model ATR42200, 300, 320, and 500 series airplanes; and all Model ATR72 series airplanes; that currently requires revising the Airplane Flight Manual (AFM) to modify procedures for calculating takeoff performance when Type II or IV de icing or

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to all Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes. This AD requires you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (referred to herein as damage), and replace any damaged

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model DC8 airplanes. This proposal would require a onetime inspection of the aft fuselage skin panel at the longeron 28 skin splice for cracks; repair of any cracks detected; and reporting of the findings of the inspection to

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes to revise an existing airworthiness directive (AD), applicable to certain Bombardier Model CL6001A11 (CL 600), CL6002A12 (CL601), and CL6002B16 (CL6013A, CL6013R, and CL604) series airplanes, that currently requires repetitive inspections to find cracks of a certain bulkhead web of the fuselage at certain locations, and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France model helicopters that requires operators to either temporarily or permanently secure the electrical bonding braid (bonding braid) that is installed on the left cyclic pitch control stick base within 10 hours timeinservice (TIS) and, if temporarily

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 757200 series airplanes, that currently requires modification of the number 3 left and right emergency exit doors. This amendment requires a new, improved modification of the number 3 left and right emergency exit doors, which terminates the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA proposes to adopt a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders. This proposed AD would require you to install GTX 330/ 330D Software Upgrade Version 3.03. This proposed AD is the result of observations that the GTX 330 and GTX 330D may detect, from other aircraft, the S1

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration