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CLARA MOSCHINI

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Civil aviation

11,436 news found

Civil aviationFAA AD on McDonnell Douglas model MD-11 and -11F airplanes

Washington, Usa - To prevent corrosion of the barrel nut holes of the upper spar caps and skin panel of the horizontal stabilizer, which could result in structural damage and consequent reduced controllability of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-06-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 and CL-600-2D24 series airplanes

Washington, Usa - To prevent failure of the lower panel of the main landing gear (MLG) door, the lower panel's departure from the airplane, and consequent damage to airplane structure, which could adversely affect the airplane's continued safe flight and

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-209-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model AS-350B, B1, B2, B3, BA, C, D, D1, and AS-355E, F, F1, F2, and N helicopters

Washington, Usa - To prevent separation of the control rod outboard spherical bearing (bearing) ball from its outer race, rubbing of the body of the control rod against the tail rotor blade pitch horn clevis, failure of the control rod, and subsequent lo

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-SW-12-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model AS-332C, AS-332L, AS-332L1, and AS-332L2 helicopters

Washington, Usa - To detect disbonding between the stainless steel protective strip and the MRB skin, which could cause loss of the protective strip, an out-of-balance condition, and subsequent loss of control of the helicopter

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-58-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas several models aircraft

Washington, Usa - To detect and correct cracking of the lower inboard auxiliary spar cap, which could cause excessive loads to the structure attaching the support fitting of the main landing gear (MLG) to the wing, and result in loss of the MLG

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-184-AD; Amendment... more

Civil aviationFAA AD on General Electric Company CF34-3A1, -3B, and -3B1 turbofan engines

Washington, Usa - To prevent B-sump scavenge screen blockage due to coking, which could result in ignition of B-sump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-21-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747SP, 747SR, 747-100, 747-200, and 747-300 series airplanes; equipped with Pratt & Whitney model JT9D-3, -7, and -7Q series engines and model JT9D-7R4G2 engines

Washington, Usa - To ensure the integrity of the fail-safe features of the thrust reverser system by preventing possible failure modes in the thrust reverser control system that can result in inadvertent deployment of a thrust reverser during flight

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NM-67-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model AS-350B3, SA-365N, N1, AS-365N2, AS 365N3, and EC-155B helicopters

Washington, Usa - To detect internal corrosion of the Siren cargo hook locking catch, which can cause the locking catch to return to an incomplete locking position, undetectable by the operator, and result in an unexpected cargo load release

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-17-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-400, -500, -600, -700, and -800 series airplanes

Washington, Usa - To prevent a reduction in flight crew visibility due to stalled wiper motors during heavy precipitation and a period of substantial crew workload, which could result in damage to the airplane structure and injury to flight crew,

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-326-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes

Usa - To detect and correct, in a timely manner, fatigue cracks in the vertical beams of the pressure bulkheads at fuselage stations 409+128 and 559, which could result in the reduced structural integrity of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-143-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747SP and 747SR; 747-100B, -200B, -200C, -200F, -300, -400, and -400D; and 767-200 and -300 series airplanes

Washington, Usa - To prevent detachment of the shoulder restraint harness of the attendant or observer seat from its mounting bracket during service, which could result in injury to the occupant of the seat

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-106-AD; Amendment... more

Civil aviationFAA AD on Saab model SAAB 2000 series airplanes

To prevent chafing damage to the electrical wire harnesses in the left and right wing fuel tanks, which could cause misleading data and erroneous fuel pump cautions to be displayed to the flightcrew, and could result in electrical arcing with consequent

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-372-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-31 and DC- 9-32 airplanes

Washington, Usa - To prevent fatigue cracking of the internal doublers and frame structure of the fuselage skin of the cockpit enclosure window sill, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-61-AD; Amendment... more