It does not receive public funding
Editor in chief:
CLARA MOSCHINI

Facebook Twitter Youtube Instagram LinkedIn

AVIONEWS - World Aeronautical Press Agency

102,090 news found

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Washington, Usa - To detect material defects in the inboard ends of the outer skin panels of the horizontal stabilizer at Station Xh=7.234, which could lead to cracks and an associated loss of strength in the attachments, and consequent reduced structura

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-213-AD; Amendment... more

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

Washington, Usa - To prevent the failure of an emergency slide or slide/raft to fully inflate during an emergency situation, which could impede an evacuation and result in injury to passengers or airplane crewmembers

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-84-AD; Amendment... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Washington, Usa - To prevent separation of the screws in the autopilot clutch assembly of the SM-300 servo, which could result in uncommanded engagement of the autopilot servo and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-79-AD; Amendment... more

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

Usa - To find and fix fatigue cracking of structure near and common to the upper chord and splice fittings of the rear spar of the wing, which could result in loss of structural integrity of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-238-AD; Amendment... more