Correction

In rule document 032784 beginning on page 5822 in the issue of Wednesday, February 5, 2003, make the following correction: Sec. 39.13 [Corrected]

On page 5823, in Sec. 39.13, in the table, in the second column, under the heading ``Compliance'', in the last line, ``AC'' should read, ``AD''.
[FR Doc. C32784 Filed 21303; 8:45 am]

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocoper) Model SA341G and SA342J helicopters. This action requires modifying an electric hoist (hoist) junction box (junction box). This amendment is prompted by the discovery of an anomaly affecting the resistor that is located in the junction box. The actions

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain BAE Systems (Operations) Limited Model BAe 146 series airplanes. This proposal would require modification of the flight annunciator box. This action is necessary to prevent traffic collision avoidance system (TCAS) aural messages and resolution

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to all DornierWerke G.m.b.H. (Dornier) Model Do 27 Q6 airplanes. This AD requires you to inspect the aileron and flap control cables for proper clearance from the fuel lines in the fuselage and make necessary adjustments; and inspect the fuel lines for damage and correct

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. This proposal would require inspection of the drive trunnion pins for the main landing gear (MLG) doors to determine the part number of the pins, and corrective action if necessary.

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), applicable to Dowty Aerospace Propellers Type R334/482F/13 propeller assemblies. That AD currently requires a onetime ultrasonic inspection of propeller hubs part number (P/N) 660709201 for cracks. This proposal would require initial and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to CFM International, S.A. CFM562C, 3, and 5 series turbofan engines. This proposal would require removing from service main fuel pumps with bronze bearings and installing main fuel pumps with aluminum/bronze alloy bearings. This

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters. This action requires replacing a certain elbow adapter (adapter) with an airworthy adapter. This amendment is prompted by reports of a cracked adapter on the hydraulic reservoir resulting in leakage of hydraulic fluid and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), that is applicable to Pratt & Whitney JT8D1, 1A, 1B, 7, 7A, 7B, 9, 9A, 11, 15, 15A, 17, 17A, 17R, and 17AR turbofan
engines. That AD currently requires a determination of the utilization rate and protective coating type of the 7th, 8th, 9th, 10th, 11th, and 12th stage high

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 747 series airplanes. This action requires repetitive inspections for cracking of the upper skin of the outboard and center sections of the horizontal stabilizer and the rear spar structure, hinge fittings, terminal fittings, and splice plates; and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document revises an earlier proposed airworthiness directive (AD), applicable to certain Dornier Model 328300 series airplanes, that would have required performing a check of the airplane maintenance records; inspecting the engine nacelle antiice tube for leaks, if necessary; and modifying the joint, if necessary. This new action revises the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), that is applicable to Pratt & Whitney (PW) model PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C, PW4062, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462, and PW4650 turbofan engines. That AD currently requires interim actions to

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747100, 100B, 100B SUD, 200B, 200C, 200F, 300, 400, 400D, and 400F series airplanes; and Model 747SR series airplanes. For certain airplanes, this AD requires repetitive inspections of the clevis bushings on the inboard and outboard sequence carriages of

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to certain SchemppHirth (SCHEMPPHIRTH) Flugzeugbau GmbH Model DuoDiscus gliders. This AD requires you to accomplish a onetime inspection of the bonding of the spar cap and spar web, and repair any defective bonding of the spar cap and spar web. This AD is the result of mandatory

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA is adopting a new airworthiness directive (AD) for Wytwornia Sprzetu Komunikacyjnego
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(WSK) PZL10W turboshaft engines. This AD requires a onetime inspection of the four enginetogearbox pin retaining joints for loose or improperly crimped retaining nuts and damaged bolts on certain serial number engines. This AD is prompted by

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 747400, 777 200, and 777300 series airplanes. This proposal would require, for certain airplanes, replacement of the cell stack of the flight deck humidifier with a suppliertested cell stack, or replacement with an end plate and

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the supersedure of an existing airworthiness directive (AD), applicable to McDonnell Douglas transport category airplanes listed above, that currently requires a onetime detailed inspection to determine if wire segments of the wire bundle routed through the feedthrough on the aft side of the flight engineer's station are

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A319, A320, and A321 series airplanes. This proposal would require repetitive inspections of the left and rightside main landing gear (MLG) side stay cuff lugs and downlock spring attachments for evidence of cracked or fractured

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 DC981 (MD81), DC982 (MD82), DC983 (MD83), DC987 (MD87), and MD88 airplanes. This proposal would require installing shield assemblies for power feeder cables in the forward and aft lower cargo compartments, and installing

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A319 and A320 series airplanes. This proposal would require a modification and replacement affecting the center and wing fuel tanks. All affected airplanes would require modification of the wiring of the fuel quantity indicating

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters. This action requires certain inspections of the rodend of the main rotor head damper for freedom of movement, and depending on the torque required to move the rodend, either further inspection for a crack or replacing the rod end. This

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Bombardier DHC8102, 103, 106, 201, 202, 301, 311, and 315 airplanes, that currently requires
inspections to detect breakage in the struts of the rear mount strut assemblies on the left and right engine nacelles, and replacement of any broken struts. The existing

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Dornier Model 328100 series airplanes. This proposal would require a onetime inspection of certain engine control cables to determine the batch number on the end fitting, and replacement of affected cables with new cables. This action is

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that currently requires a onetime inspection to identify all alloy steel bolts on the body station 1480 bulkhead splice, and corrective action if necessary; and provides for optional terminating action for certain

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) 65, 90, 99, 100, 200, and 300 series, and Model 2000 airplanes. This AD requires you to install new exterior operating instruction placards for the airstair door and emergency exits. This AD is the result of Raytheon improving the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration