The FAA is adopting a new airworthiness directive (AD) for certain serial numbers (SNs) of RollsRoyce Deutschland Ltd. & Co KG (RRD) Model Tay 65015 turbofan engines. This action requires initial and repetitive visual inspections of low pressure (LP) turbine stage 2 rotor discs and LP turbine stage 3 rotor discs on certain SNs of engines, for

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD9030 airplanes, that requires a onetime inspection for chafing of the RDB wire bundle against the No. 2 automatic direction finder (ADF) receiver located at the aft end of the forward right radio rack; repair or replacement, if necessary; and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Dornier Luftfahrt GMBH (Dornier) Models 228100, 228101, 228200, 228201, 228202, and 228212
airplanes that have electrical cabin/cockpit heater option P05 or option P09 installed. This proposed AD would require you to modify the cockpit and cabin

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes 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 airplanes that are

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document revises an earlier proposed airworthiness directive (AD), applicable to certain Airbus Model A300 B2 and B4 series airplanes; Model A300 B4600, A300 B4600R, and A300 F4600R series airplanes (collectively called A300600); Model A310 series airplanes; Model A319, A320, and A321 series airplanes; Model A330301, 321, 322, 341, and 342

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that is applicable to RollsRoyce plc (RR) RB21122B series turbofan engines with intermediate pressure (IP) compressor stage 6 to 7 rotor shaft assembly part number (P/N) UL37094 installed. This amendment requires removal from service of IP compressor stage 6 to 7 rotor shaft assemblies P/N

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

Correction

In rule document 039690 beginning on page 19940 in the issue of Wednesday, April 23, 2003 make the following corrections:

Sec. 39.13 [Corrected]

1. On page 19944, in the first column, in Sec. 39.13, in the second table, the heading, ``Table 5 Compliance Time for TLMCs'' should read ``TableCompliance Time for TLMCs''.

2. On

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain Boeing Model 737 100, 200, and 200C series airplanes, that currently requires repetitive inspections to detect discrepancies in the upper and lower skins of the fuselage lap joint, and repair if necessary. This action would add new inspections,

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 747 series airplanes equipped with General Electric CF645 and CF650 series engines. This amendment requires an inspection to detect chafing of the fuel line or incorrect clearance between the fuel line and pneumatic duct insulation blanket; a fuel leak check

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to certain Mitsubishi Heavy Industries, Ltd. (Mitsubishi) MU2B series airplanes. This AD requires you to repetitively inspect the cockpit windshield and cabin window surfaces for damage (damage is defined as crazing, scratches, and cracks). If any of the windshield or window

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

Correction

In rule document 0321519 beginning on page 50462 in the issue of Thursday, August 21, 2003, make the following correction:

Sec. 39.13 [Corrected]

On page 50464, in Sec. 39.13(o), in the table the heading should read Table 3Incorporation by Reference.
[FR Doc. C321519 Filed 9503; 8:45 am]
BILLING CODE 150501D

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A300 B4622R and A300 F4622R airplanes, and Model A310324 and 325 series airplanes, that are equipped with Pratt & Whitney PW4000 series engines. This proposal would require replacement of the existing flexible hose assembly that

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to a McDonnell Douglas Model DC915 airplane. This proposal would require an inspection to detect chafing or overheat damage of the electrical wires located at fuselage station Y=110.000 bulkhead of the lower nose left tunnel; and corrective actions, if

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA supersedes Airworthiness Directive (AD) 94-18-04 [[Page 59107]]
R1, which currently applies to all Univair Aircraft Corporation (Univair) Models Alon A2 and A2A; ERCO 415C, 415CD, 415D, 415E, and 415G; Forney F1 and F1A; and Mooney M10 airplanes. AD 941804 R1 requires installing inspection openings in the outer wing panels, inspecting

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A300 B2 and B4 series airplanes; Model A300 B4600, B4600R, and F4600R
(collectively called A300600) series airplanes; and Model A310 series airplanes. This proposal would require various modifications and repetitive inspections of

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A320111, 211, 212, and 231 series airplanes. This proposal would require repetitive inspections for fatigue cracking around the fasteners attaching the pressure panel to the flexible bracket at frame 36, adjacent to the longitudinal

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas airplane models. This proposal would require inspection of the captain's and first officer's seat locking pins for minimum engagement with the detent holes in the seat tracks; inspection of the seat lockpins for excessive wear;

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 777200 and 777300 series airplanes, that requires application of hightemperature sealant in designated areas of the strut aft dry bay. The actions specified by this AD are intended to prevent leakage of hydraulic fluid into the strut aft dry bay, where high

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain Bombardier Model CL2151A10 and CL2156B11 series airplanes, that currently requires repetitive inspections to detect cracking of main landing gear (MLG) axles that have been reworked by chromium plating, and replacement of cracked axles with

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Raytheon airplanes. This proposal would require inspection of the main landing gear (MLG) wheels to determine the part numbers of the tiebolt nuts, and replacement of nuts that have the incorrect part number with nuts that have the correct part

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS350B3 helicopters. This proposal would require inspecting the ASU No. 2 printed circuit board (PCB) to determine if the resistor R8 is installed, and if it is not installed, replacing the PCB with an airworthy PCB with that resistor

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to all MORAVAN a.s. (Moravan) Model Z242L airplanes. This AD establishes a technical service life for these airplanes by restricting Acrobatic and Utility category operations and requiring replacement of the wings after a certain operational time period. This AD is the result of

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to various transport category airplanes manufactured by McDonnell Douglas. This proposal would require a onetime test of the fire extinguishers for the engine and auxiliary power unit (APU) to determine the capability of the firex electrical circuits to

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 revising the Airworthiness Limitations Section of the Maintenance Planning Data (MPD) Document (767 Airworthiness Limitations Instructions (ALI)). The revision incorporates into the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document revises an earlier proposed airworthiness directive (AD), applicable to certain McDonnell Douglas airplanes, that would have required inspections of the linear variable differential transducers (LVDTs) of the autopilot for discrepancies, and followon actions, if necessary. This new action revises the proposed rule by expanding the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration