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

Facebook Twitter Youtube Instagram LinkedIn

Security

5,161 news found

SecurityFAA AD on Allied Ag Cat Productions, Inc. G-164 series airplanes (2007-17-02)

Washington, Usa - To prevent turning the fuel shut-off valve clockwise past the "ON'' position stop which could allow the fuel valve to be rotated to an unplacarded "OFF'' position and lead to reduced fuel flow

Airworthiness Directive Federal Register Information [Federal Register: (Volume 72, Number 156)] [Page 45312-45314] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Taylorcraft A, B, and F series airplanes (2007-16-14)

Washington, Usa - To detect and correct corrosion or cracks in the right and left wing front and aft lift struts and could result in failure and lead to in-flight separation of the wing with consequent loss of control

Airworthiness Directive Federal Register Information [Federal Register: (Volume 72, Number 155)] [Page 45153-45156] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Fokker model F-27 Mark 050 airplanes equipped with Dowty Type R.352 or R.410 series propellers (2007-16-11)

Washington, Usa - To detect and correct boots attached with defective adhesive, which could result in separation of a boot from the airplane, consequent reduced structural integrity of the airplane, and possible injury

Airworthiness Directive Federal Register Information [Federal Register: (Volume 72, Number 153)] [Page 44746-44748] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes (2007-16-08)

Washington, Usa - To detect and correct fatigue cracks that could extend and fully sever the frame, which could result in development of skin cracks that could lead to rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: August 9, 2007 (Volume 72, Number 153)] [Page 44728-44731] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Enstrom Helicopter Corporation model F-28, F-28A, F-28C, F-28C-2, F-28C-2R, F-28F, F-28F-R, 280, 280C, 280F, 280FX, TH-28, 480, and 480B helicopters (2007-16-01)

Washington, Usa - To prevent failure of a retention pin, separation of a main rotor blade from the helicopter, and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: July 31, 2007 (Volume 72, Number 146)] [Page 41615-41618] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Boeing model 747-100, 747-100B, 747- 200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes (2007-15-07)

Washington, Usa - To detect and correct fatigue cracking of the fuselage skin near stringer 5. Cracks in this area could join together and result in in-flight depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 30, 2007 (Volume 72, Number 145)] [Page 41433-41436] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Airbus model A-318, A-319, A-320, and A-321 airplanes (2007-15-06)

Washington, Usa - To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 24, 2007 (Volume 72, Number 141)] [Page 40222-40224] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on BAE Systems (Operations) Limited model ATP airplanes (2007-15-08)

Washington, Usa - To prevent and correct fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 24, 2007 (Volume 72, Number 141)] [Page 40230-40233] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on McDonnell Douglas model DC-10-10 and DC-10-10F, DC-10-15, DC-10-30 and DC- 10-30F, DC-10-40 and DC-10-40F, MD-10-10F and MD-10-30F, MD-11 and MD-11F airplanes (2007-15-05)

Washington, Usa - To prevent continued arcing following a short circuit of the fuel pump housing electrical connector, which could create an ignition source inside the fuel tank with explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 24, 2007 (Volume 72, Number 141)] [Page 40216-40222] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Airbus model A-310 and A-300/600 series airplanes (2007-14-05)

Washington, Usa - To prevent safety-significant latent failures that would result in a hazardous or catastrophic failure condition of avionics, hydraulic systems, fire detection systems, fuel systems or other critical systems

Federal Aviation Administration Airworthiness Directive Federal Register Information [Federal Register: July 18, 2007 (Volume 72, Number 137)] [Page 39307-39310] Header Information DEPARTMENT... more

SecurityFAA AD on Bombardier model CL-600-1A11, CL-600-2A12, CL-600-2B16 airplanes (2007-14-02)

Washington, Usa - To prevent internal leakage of the selector valve, which could result in an uncommanded retraction of the NLG with consequent damage to the airplane and possible serious injury to ground personnel

Airworthiness Directive Federal Register Information [Federal Register: July 12, 2007 (Volume 72, Number 133)] [Page 38004-38006] Header Information DEPARTMENT OF TRANSPORTATION Federal... more