AD Number |
Effective Date |
Manufacturer |
Description |
Recurring |
 |
|
|
|
|
2008-15-05 |
08/05/2008 |
Boeing Commercial |
To detect and correct corrosion of the carriage spindle, which could result in fracture |
Y |
2008-15-01 |
08/21/2008 |
Embraer |
To prevent pitch upsets if the pitch trim actuators jam or freeze, which could result in reduced controllability,contd. |
N |
2008-14-17 |
08/21/2008 |
Airbus Industrie |
To identify and correct the loss of integrity of the upper shell structure of the fuselage between FR84 and FR87 |
N |
2008-14-16 |
08/21/2008 |
328 Support Services GmbH |
To prevent further incidents of inadvertent opening and possible detachment of a passenger door,contd. |
N |
2008-14-15 |
08/20/2008 |
International Aero Engine |
To prevent heat damage to high-pressure turbine (HPT) and low-pressure turbine (LPT) critical life limited,contd. |
N |
2008-14-14 |
08/21/2008 |
Boeing Commercial |
To prevent insufficient clearance between the wire bundle and hydraulic tube that could lead to chafing,contd. |
N |
2008-14-13 |
08/14/2008 |
Cirrus Design Corp. |
To prevent in-flight failure of the cabin door, which could result in door separation from the airplane |
N |
2008-14-12 |
08/21/2008 |
Pacific Aerospace |
To require inspections of the vertical fin for cracking, corrosion, scratches, dents, creases, and/or,contd. |
Y |
2008-14-11 |
07/23/2008 |
Boeing Commercial |
To prevent ETOPS operation with insufficient cargo fire suppression capability, which could result in an,contd. |
N |
2008-14-10 |
07/22/2008 |
Lockheed Aircraft Corp |
To prevent failure of the upper engine mount bolts, which could result in reduced structural capability,contd. |
Y |
2008-14-09 |
08/14/2008 |
Airbus Industrie |
To render manditory an inspection subsequent to accomplishment of SB A200-53-0282 or,cont'd |
Y |
2008-14-08 |
08/14/2008 |
Boeing Commercial |
To detect and correct broken or missing fasteners in the hinge segments with a single fastener row, which,contd. |
Y |
2008-14-07 |
08/14/2008 |
Lycoming Engines |
To prevent failure of the fuel injector fuel lines that would allow fuel to spray into the engine compartment,contd. |
Y |
2008-14-06 |
08/14/2008 |
Bell Helicopter |
To identify and correct manufacturing flaws on the inside surface of the upper and/or lower skin at,contd. |
N |
2008-14-05 |
08/21/2008 |
Agusta |
To extend the same mandatory corrective actions to A119 model due to its design similarity with A109E |
Y |
2008-14-04 |
08/05/2008 |
Eurocopter France |
To prevent the power drawn by the starter generators from the engines from exceding the consumption capacity at,contd. |
N |
2008-14-03 |
08/14/2008 |
Bell Helicopter |
To identify and correct an improper installation of the tailboom attachment bolt in the upper left-hand,contd. |
N |
2008-14-02 |
08/14/2008 |
Agusta |
To detect cracks in the fuselage frame structure and to prevent structural failure in this area |
Y |
2008-14-01 |
08/14/2008 |
Bell Helicopter |
To prevent interruption of the fuel supply caused by failure of the switch, which could result in loss of,contd. |
N |
2008-13-51 E |
06/13/2008 |
Eclipse Aviation Corp. |
To reduce the likelihood of the throttle position signal exceeding its maximum range, which could cause loss,contd. |
N |
2008-13-32 |
08/12/2008 |
APEX Aircraft |
To mandate revision of the AFM which introduces the corrected values for arms of front and rear fuel tanks |
N |
2008-13-31 |
08/12/2008 |
Dassault Aviation |
To secure safe closure of engine cowlings and improve the existing locking devices |
N |
2008-13-30 |
08/12/2008 |
Gulfstream Aerospace LP |
To prevent failure of the attachment fasterners which could result in possible in-flight loss of a,contd. |
N |
2008-13-29 |
08/12/2008 |
McDonnell Douglas Corp. |
To detect and correct such cracking, which could sever the frame, increase the loading of adjacent,contd. |
Y |
2008-13-28 |
07/17/2008 |
Hartzell Propeller |
To prevent failure of the propeller hub, which could result in blade separation and loss of control of the,contd. |
Y |
2008-13-27 |
08/06/2008 |
Turbomeca Engine Corp. |
To prevent uncommanded shutdown of the engine, which could lead to an accident |
N |
2008-13-26 |
08/12/2008 |
Lockheed Aircraft Corp |
To prevent the loss of hydraulic pressure and steering control |
Y |
2008-13-25 |
08/12/2008 |
Boeing Commercial |
To prevent fatigue cracking in the web panel of the main wheel well pressure deck, which could result in,contd. |
N |
2008-13-24 |
08/12/2008 |
Aerospatiale |
To require the inspection [for proper hole diameter] of the aileron tab bellcrank retainer and, if necessary, the,contd. |
N |
2008-13-23 |
08/06/2008 |
328 Support Services GmbH |
To install a drain hole in the lower skin of the left and right-hand elevator horns, contd. |
N |
2008-13-22 |
08/06/2008 |
Boeing Commercial |
To prevent loss of the IDUs due to failure of all three electronic flight instrument system/engine,contd. |
N |
2008-13-21 |
08/06/2008 |
Boeing Commercial |
To prevent the in-line flow indicators of the passenger oxygen masks from fracturing and separating, which,contd. |
N |
2008-13-20 |
08/06/2008 |
Boeing Commercial |
To prevent failure of the attachment bolts and consequent separation of a thrust reverser from,contd. |
Y |
2008-13-19 |
08/06/2008 |
ATR |
To require repetitive verification of the Pitot probes' resistance and replacement of any,contd. |
Y |
2008-13-18 |
07/30/2008 |
Pilatus Aircraft Ltd. |
To prevent, on take-off or landing runs, possible hazards associated with loss of directional control |
N |
2008-13-17 |
08/06/2008 |
Hawker Beechcraft |
To prevent failure of the circuit breaker toggle switch, which could result in smoke in the cockpit and the,contd. |
N |
2008-13-16 |
07/10/2008 |
Pratt & Whitney Canada |
To inspect Low-Pressure (LP) compressor fan blades and replace any blade that is found to be under,contd. |
N |
2008-13-15 |
07/30/2008 |
Embraer |
To require the inclusion of new maintenance tasks in the Critical Design Configuration Control Limitations,contd. |
Y |
2008-13-14 |
07/30/2008 |
Embraer |
To require the inclusion of new maintenance tasks in the Critical Design Configuration Control Limitations,contd. |
Y |
2008-13-13 |
08/12/2008 |
Airbus Industrie |
To prevent the airplane from departing the runway during a CAT 2 or CAT 3 automatic landing or roll-out,contd. |
N |
2008-13-12 |
08/12/2008 |
Boeing Commercial |
To detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could,contd. |
Y |
2008-13-11 |
08/05/2008 |
Viking-Air Ltd. |
To perform the corrosion tasks (CTs) required by the corrosion prevention and control program |
Y |
2008-13-10 |
07/07/2008 |
Dassault Aviation |
To require replacement of all affected SPDB with upgraded units and, in the meantime, the implementation of,contd. |
N |
2008-13-08 |
08/06/2008 |
Dehavilland Aircraft |
To prevent potential ignition sources inside the fuel system, which could result in a fuel tank explosion |
Y |
2008-13-07 |
07/30/2008 |
Dehavilland Aircraft |
To identify and correct the installation of the elevator overload bungees, reinstallation if,contd. |
N |
2008-13-06 |
07/30/2008 |
Cessna Aircraft Company |
To detect and correct damaged wiring of the auto-control wing de-ice system, fuel quantity indication,contd. |
N |
2008-13-05 |
07/23/2008 |
Lindstrand Balloons |
To prevent an ignition hazard caused by defective burner hoses |
N |
2008-13-04 |
07/24/2008 |
Dassault Aviation |
To mandate replacement of the wing anti-ice flexible hoses by new ones of an improved design |
N |
2008-13-03 |
07/24/2008 |
Boeing Commercial |
To prevent an uncommanded left rudder hardover in the event of cracking in the yaw damper actuator portion of the,contd. |
Y |
2008-13-02 |
07/24/2008 |
BAE Systems (Operations) |
To prevent damaging stresses in the propeller assembly, instructing the flight crews to place the propeller,contd. |
N |
2008-13-01 |
08/01/2008 |
Fokker Aircraft B.V. |
To require a one-time inspection for improper welds |
N |
2008-12-19 |
07/24/2008 |
Dassault Aviation |
To prevent chafing between the feeder bundle and the right side partition wall separating the cabin,contd. |
N |
2008-12-18 |
07/23/2008 |
Dassault Aviation |
To inspect unflagged air data error that may lead to the computation and display on both pilot's and,contd. |
Y |
2008-12-17 |
07/23/2008 |
Lockheed Aircraft Corp |
To prevent chafing of the fuel level control switch wiring harness, which could cause arcing and result in a,contd. |
N |
2008-12-16 |
07/23/2008 |
M7 Aerospace LP |
To detect and correct chafing/arcing of electrical wires, components, and bleed air lines |
N |
2008-12-15 |
07/23/2008 |
Dassault Aviation |
To mandate the replacement of the passenger oxygen mask boxes by new-designed one [boxes] adapted to controller |
N |
2008-12-14 |
07/23/2008 |
Dassault Aviation |
To prevent failure of the wings' anti-ice valve, indications of untimely anti-icing with the,contd. |
N |
2008-12-13 |
07/23/2008 |
General Avia Costruzioni |
To repetitively inspect the structure surrounding the heads of the four bolts of the engine mount attachment,contd. |
Y |
2008-12-12 |
07/23/2008 |
Viking-Air Ltd. |
To prevent the failure of the lockwire hold in the ignition connector plug, which could lead to complete loss,contd. |
Y |
2008-12-11 |
07/01/2008 |
Agusta |
To identify and correct the unsafe condition caused by interference between the pilot or co-pilot door lower,contd. |
N |
2008-12-10 |
07/16/2008 |
Bombardier, Inc. |
To prevent a chafing condition between electrical harnesses and FQGS harness that could increase the surface,contd. |
N |
2008-12-09 |
07/16/2008 |
Bombardier, Inc. |
To detect and correct the insufficient electrical bonding between fuel tubes or insufficient current,contd. |
N |
2008-12-08 |
07/15/2008 |
Short Brothers Limited |
To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel,contd. |
N |
2008-12-07 |
07/16/2008 |
Embraer |
To prevent the fuel leakage inside the conduit used to route the clear ice detector wiring through the wing,contd. |
N |
2008-12-06 |
07/16/2008 |
Moravan A.S. |
To inspect the vortex inserts inside the carburetor heating system heat exchanger for cracks and/or loose or,contd. |
N |
2008-12-05 |
07/16/2008 |
Boeing Commercial |
To prevent the in-line flow indicators of the passenger oxygen masks from fracturing and separating, which,contd. |
N |
2008-12-04 |
07/16/2008 |
Boeing Commercial |
To detect and correct such fatigue-related cracks, which could result in the crack tips continuing to turn and,contd. |
N |
2008-12-03 |
07/09/2008 |
Boeing Commercial |
To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel,contd. |
N |
2008-12-03 |
07/09/2008 |
British Aerospace |
To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel,contd. |
N |
2008-12-03 |
07/09/2008 |
McDonnell Douglas Corp. |
To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel,contd. |
N |
2008-12-02 |
07/16/2008 |
British Aerospace |
To inspect the nose landing gear to ensure that the wheels are correctly retained and depending on findings,contd. |
Y |
2008-12-01 |
07/16/2008 |
Cessna Aircraft Company |
To detect and correct missing firewall sealant between the aft firewall assembly and seal assembly, which could,contd. |
N |
2008-11-20 |
06/23/2008 |
Stemme Gmbh and Co. KG |
To reduce the potential for a fire to ignite and which could lead to loss of control of the sailplane |
N |
2008-11-19 |
06/16/2008 |
Rolls-Royce Limited |
To prevent a failure of the IP turbine disc that could result in an uncontained failure of the engine and possible,contd. |
N |
2008-11-18 |
07/07/2008 |
Cirrus Design Corp. |
To detect and correct leaks in the exhaust system, which could result in exhaust gases leaking into the cabin,contd. |
Y |
2008-11-17 |
07/07/2008 |
Air Tractor, Inc. |
To prevent the front and rear connections of the overturn skid plate to the airplane from breaking, which,contd. |
N |
2008-11-16 |
07/07/2008 |
Rolls-Royce Limited |
To prevent uncontained loss of IPC stage 1 blades, which could result in damage to the airplane |
N |
2008-11-15 |
07/03/2008 |
McDonnell Douglas Corp. |
To prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations,contd. |
N |
2008-11-14 |
07/03/2008 |
McDonnell Douglas Corp. |
To prevent the accumulation of ice on the flight control cables in the wheel wells |
N |
2008-11-13 |
07/03/2008 |
Boeing Commercial |
To prevent the potential for ignition sources inside the fuel tanks caused by latent failures, alterations,contd. |
N |
2008-11-12 |
07/03/2008 |
Fokker Aircraft B.V. |
To install autopilot disconnect units and associated wiring changes |
N |
2008-11-11 |
07/23/2008 |
Viking-Air Ltd. |
To reflect the new requirement to inspect the tailplane front spar web behind the pick-up brackets using,contd. |
Y |
2008-11-10 |
08/05/2008 |
Viking-Air Ltd. |
To mandate modification and inspection of the wing front spar adapter fitting and replacement of cracked,contd. |
Y |
2008-11-09 |
07/03/2008 |
Boeing Commercial |
To detect and correct cracking in the vinyl interlayer or damage to the structural inner glass panes of the,contd. |
Y |
2008-11-08 |
07/03/2008 |
Boeing Commercial |
To detect and correct cracking in the vinyl interlayer or damage to the structural inner glass panes of the,contd. |
Y |
2008-11-07 |
07/03/2008 |
Boeing Commercial |
To prevent center tank fuel pump operation with continuous low pressure, which could lead to friction sparks or,contd. |
N |
2008-11-06 |
07/03/2008 |
McDonnell Douglas Corp. |
To prevent interference and chafing between the potable water supply hose and/or gray water hose with the,contd. |
N |
2008-10-51 |
06/03/2008 |
AvCraft Aerospace GmbH |
To prevent structural failure of the affected wing panel, possible separation of the wing from the airplane,contd. |
Y |
2007-04-19 R1 |
05/07/2007 |
Textron Lycoming |
To prevent cylinder separation that can lead to engine failure, possible engine compartment fire, and,contd. |
N |
2007-04-19 R1 |
05/07/2007 |
Teledyne Continental |
To prevent cylinder separation that can lead to engine failure, possible engine compartment fire, and,contd. |
N |
2006-16-18 R1 |
07/18/2008 |
Sandel Avionics Inc |
To prevent a bearing error, which could lead to an airplane departing from its scheduled flight path,contd. |
N |
