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Civil aviation

7,931 news found

Civil aviationFAA AD on Boeing model 757-200, -200CB, and - 200PF series airplanes

Washington, Usa - To prevent separations in the drive system for the inboard trailing edge flaps, which could cause a flap skew condition that could result in damage to the flaps or fuselage, and consequent reduced controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-329-AD; Amendment 39-13109; AD 2003-07-13] RIN... more

Civil aviationFAA AD on Eurocopter France model AS-350B3 helicopters

Washington, Usa - To prevent malfunction of the electrical circuits controlling the "BATT. TEMP." red warning light, the "ENGINE CHIP" amber caution and the rotor revolutions-per-minute (RPM) signal output to the vehicle engine management display

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-05-AD; Amendment 39-13116; AD 2003-08-05] RIN... more

Civil aviationFAA AD on Boeing model 757-200, 757-200CB, and 757-200PF series airplanes

Washington, Usa - To detect and correct migration of shims at the joint of the mid-bulkhead and the upper link fittings, which could result in cracking of the strut and consequent loss of the strut and engine

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-315-AD; Amendment 39-13104; AD 2003-07-08] RIN... more

Civil aviationFAA AD on Raytheon airplanes

Washington, Usa - To prevent separation of a main landing gear (MLG) wheel due to loose or missing tie-bolts or tie-bolt nuts, with consequent damage to airplane structure or systems, decompression, loss of full braking ability, or injury to personnel on

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-268-AD; Amendment 39-13103; AD 2003-07-07] RIN... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4 series airplanes; and A-300 B4-600, B4-600R, and F4-600R series airplanes

Washington, Usa - To detect and correct fatigue cracking of the upper radius of the forward fitting of fuselage frame 47, which could result in propagation of the cracking to the rear fitting and reduced structural integrity of frame 47

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-378-AD; Amendment 39-13091; AD 2003-06-04] RIN... more

Civil aviationFAA AD on Saab model Saab SF-340A series airplanes

Washington, Usa - To prevent incidents of smoke or a burning smell in the cabin during flight caused by incorrect brush insulation in the motors of the air recirculation fans that provide air to the flight compartment and the passenger compartment

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-420-AD; Amendment 39-13092; AD 2003-06-05] RIN... more

Civil aviationFAA AD on Raytheon model Hawker 800XP and 800 airplanes

Washington, Usa - To prevent failure of certain attachment bolts due to manufacturing discrepancies, which could result in reduced structural integrity of the airplane, and loss of system function for flaps, controls, and landing gear

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-18-AD; Amendment 39-13093; AD 2003-06-06] RIN... more

Civil aviationFAA AD on CFM International (CFMI) CFM56-5C series turbofan engines

Washington, Usa - To prevent low cycle fatigue (LCF) failure of the high pressure turbine rotor (HPTR) front shaft, HPTR front air seal, and booster spool, which could result in an uncontained failure and damage to the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 95-ANE-64-AD; Amendment 39-13094; AD 97-09-02R2] RIN... more

Civil aviationFAA AD on General Electric Aircraft Engines CT7 series turboprop engines

Washington, Usa - To prevent separation of PGB left-hand and right-hand idler gears, which could result in uncontained PGB failure and internal bulkhead damage, possibly prohibiting the auxiliary feathering system from fully feathering the propeller on

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-48-AD; Amendment 39-13090; AD 2003-06-03] RIN... more