Стандарты FAA

FAA-E-2542 MODIFICATION KITS FOR ARSR LIQUID COOLING SYSTEMS FAA AD 1946-38-01 Vacuum System Tubing FAA AD 1945-04-01 24SRT Tubing FAA AD 1944-20-02 24SRT Tubing FAA AD 2013-03-17 To Prevent Failure Of The HPT Stage 1 And Stage 2 Discs FAA AD 2012-25-09 To Prevent Uncontained IP Turbine Disc Failure, Engine Failure, And Damage To T... FAA AD 2012-23-11 To Prevent Cracking In The Rotary Rudder Boom Or Pylon Due To Fatigue, Failure ... FAA AD 2011-NM-204 To Detect And Correct A Worn Or Cracked Clevis Hole FAA AD 2012-NE-33 To Prevent Failure Of The HPT Stage 1 And Stage 2 Discs FAA AD 2010-19-05 To Prevent Separation And Loss Of A Stainless Steel Ring (75 Millimeter (mm) In... FAA AD 2009-SW-34 To Prevent Separation And Loss Of A Stainless Steel Ring (75 Millimeter (mm) In... FAA AD 2009-20-13 To Ensure Replacement Of The Control Column Rod Ends With High-Strength Steel R... FAA AD 2009-15-08 To Prevent Loss Of The Fairing Panels To Be Due To Failure Of Certain Steel Gro... FAA AD 2008-NM-193 To Prevent Loss Of The Fairing Panels To Be Due To Failure Of Certain Steel Gro... FAA AD 2008-14-03 To Require Actions that are Intended to Address the Unsafe Condition that Resul... FAA AD 2006-06-10 To Detect and Correct Cracks in the Skin, Bearstrap, and Small Steel Doubler - ... FAA AD 2005-NM-105 To Detect and Correct Cracks in the Skin, Bearstrap, and Small Steel Doubler (I... FAA AD 2005-14-08 To Prevent Loss Of The Underwing Fitting Load Path Due To Missing Or Damaged Al... FAA AD 2003-21-08 Disbonding Between The Stainless Steel Protective Strip And The MRB Skin - Appl... FAA AD 2002-NM-273 Undetected Cracking Of The H-11 Steel Bolts Or Cadmium-Plated Bolts - Applicabl... FAA AD 2003-11-25 Broken H-11 Steel Bolts - Applicable to Boeing Model 747-100, 747-100B, 747-100... FAA AD 2002-SW-58 Disbonding Between The Stainless Steel Protective Strip And The MRB Skin - Appl... FAA AD 2003-05-05 Failure Of The Steel Fuselage Center-section Tie Bar - Applicable to Robert E. ... FAA AD 2001-NM-394 Broken H-11 Steel Bolts - Applicable to Boeing Model 747 Series Airplanes FAA AD 2001-16-08 Fatigue Cracking Or Fracture Of The Steel Attachment Fittings Of The Diagonal B... FAA AD 2001-15-08 Ignition of Fuel Vapors Due to the Generation of Sparks and a Potential Ignitio... FAA AD 2000-NM-302 Prevent Fatigue Cracking or Fracture of the Steel Attachment Fittings of the Di... FAA AD 2000-08-14 Prevent Cracking of the High Strength H-11 Steel Bolts on the Wing Rear Spar Si... FAA AD 1999-NM-56 Detect And Prevent Cracking Of The High Strength H-11 Steel Bolts On The Wing R... FAA AD 1999-07-02 Detect a Mislocated or Improperly Bonded Main Rotor Blade (Blade) Leading Edge ...