Feedback 4/2011

Optional Service Bulletins A320-92-1049 and A320-92-1052 provides additional insulation for the “M” or outer harness runs. Transport Canada Civil Aviation (TCCA) is working with European Aviation Safety Agency and Airbus to address this present issue and would like to advise all A320 operators/maintainers of this possible scenario for wire raceway chaffing and available Airbus optional Service Bulletins. @ AIRBUS, A330 243 SDR # 20110413014 Wing Panel Missing SDR submitted: During a maintenance walk-around, it was discovered that a riveted panel, forward of inboard flap on right wing, was missing. The aeroplane was repaired as per the Structural Repair Manual (SRM). A new wing panel was installed and the aeroplane was made serviceable. Transport Canada Comments: European Aviation Safety Agency Airworthiness Directive 2006-0107 was issued which mandated the one-time inspection of the supporting fasteners and surrounding structure of this discrepant wing panel. Following this and due to the occurrence of more events of this nature, European Aviation Safety Agency Airworthiness Directive 2008-0002 was issued mandating the incorporation of Service Bulletin A330-57-3100, which replaces the existing blind rivets with bolted fasteners. Transport Canada Civil Aviation (TCCA) would like to advise all A330-200/300 and also applicable 340-300 operators of this possible scenario and available documentation. The accomplishment of the latest Service Bulletin is recommended to be done at the soonest possible opportunity. @ Inboard wing root Inboard flap panel Rear wing spar Raceway wiring guides Service Bulletin A320-24-1062 Missing panel area Feedback 4/2011 5 BEECH 300 SDR # 20091002006 Hydro Mechanical Unit Fuel Line - Leakage SDR submitted: The pilot noticed fuel leaking from the left-hand engine lower cowling during a walk around inspection. Maintenance personnel removed a cowling, cleaned the residual fuel but could not find the source of the fuel leakage. An engine ground run-up was carried out and it was then that a steady fuel spray was emanating from the fuel line that attached from the engine pylon to the Hydro Mechanical Unit (HMU). The fuel spray was contacting the back of one of the engine igniters, thus the engine was immediately shutdown without incident. The fuel line was replaced but did not show any evidence of damage or wear. No cause for fuel line failure was found. Transport Canada Comments: The proper maintenance of fuel lines and fittings is particularly important because of the flammability of fuel. Even a small leak in a confined area (such as the above area, igniters) can soon produce an explosive atmosphere that can be ignited by any kind of spark. The Service Difficulty Report database contains 3 previous reports of this fuel line being chaffed by the engine cowl latch. @ BOEING, 737 800 SDR # 20110316005 Flap Gimbal Bushing Excessive Wear SDR submitted: During a scheduled performance of Boeing task cards 27-144-00-01/02 to lubricate the left and right inboard flap outboard ballscrew and gimbals, it was found that the lower gimbal bushing assembly on both the left and the right inboard flaps had migrated out from their respective gimbal seats. The results of these migrated bushings were excessively worn attachment bolts, which are used to retain the bushings within the gimbal. The photo to the right shows the abnormal wear of a retaining bolt and gimbal bushing. Both gimbal bushing assemblies and retaining bolts were replaced and the aeroplane was released back to service. Transport Canada Comments: Boeing Fleet Team Digest (FTD) 737NG-FTD-27-03006 defines in detail this possible scenario which is rooted to the application of excessive high grease-gun pressures that can apply undue pressure on the gimbal bushing, forcing it to migrate out and wear into its retaining bolt. Transport Canada Civil Aviation (TCCA) would like to advise all Boeing 737-600/700/800/BBJ operators and maintainers of this available Boeing Fleet Team Digest and the precaution to take when using high-pressure grease guns. @ Worn gimbal bushing Worn Retaining Bolt 6 Feedback 4/2011 BOEING, 757 200 SDR # 20110215002 Engine Fuel Leak and Imbalance SDR submitted: During cruise, the aeroplane experienced a large fuel imbalance due to a fuel leak at the right hand engine. The aeroplane declared an emergency and diverted where upon arrival the right hand tank fuel quantity was 1500 kilogram (kg) less than the left hand tank. Maintenance personnel found an o-ring that was leaking at the right engine high-pressure fuel pump feed line. The o-ring was replaced and the aeroplane was returned to service. Six flight legs previous to this event, the right engine high-pressure fuel pump had been replaced where new o-rings were used and leak checks carried out. Transport Canada Comments: The reason behind the failure of the o-ring has not been determined but is suspected that possible damage or improper installation of the new o-ring was incurred during the pumps replacement. Transport Canada Civil Aviation (TCCA) would like to emphasize the importance for maintainers to follow all maintenance manual procedures and necessary handling precautions. @ BOEING, 767 300 SDR # 20110607014 Relay Failure SDR submitted: During flight, several system failure messages were posted where maintenance troubleshot the fault to a failing relay. It was noted that several of the connecting post studs were loose within the relay body receptacles, breaking the posts electrical continuity capability. The relay was replaced and the aeroplane was made serviceable. Transport Canada Comments: Transport Canada Civil Aviation (TCCA) would like to emphasize to all aeroplane maintainers of this relay’s possible failure scenario. @ Dislodged connecting post studs Fuel Control Unit Assembly Connecting post receptacles at the relay Leak occurred here High Pressure Fuel Pump Feedback 4/2011 7 BOMBARDIER, CRJ 200 SDR # 20110526004 Insufficient Hydraulic Line Support SDR submitted: During flight at cruise and inbound to a maintenance base, the #1 hydraulic quantity went to zero followed by the pressure going to zero and associated system low pressure caution messages. Upon maintenance investigation, it was found that the #1 hydraulic pressure line in the aft equipment bay was chaffed through, causing the complete loss of the fluid. The chaffing was a result of the hydraulic line jam-nuts at the top of the hydraulic support shelf coming loose, allowing significant movement and vibration. The hydraulic support shelf was severely worn along with several support bracket fairleads downstream the line. The hydraulic support shelf was repaired, the hydraulic line and fairlead inserts for the support brackets were replaced and the aircraft was made serviceable. Transport Canada Comments: The correct support of all hydraulic lines is essential for the continued operation of aircraft hydraulic systems. This scenario demonstrates that the worn fairlead inserts were an indicator of a more significant failure else-where in the system. Transport Canada Civil Aviation (TCCA) would like to advise all operators and maintainers of this possible scenario that may lead to a complete hydraulic system failure. @ Failed hydraulic line support clamp fairlead inserts found severely worn Failed hydraulic line Hydraulic support shelf found severely worn 8 Feedback 4/2011 BOMBARDIER, CL600 2D24 (RJ900) SDR # 20110310004 Main Landing Gear Wheel Rim Cracks SDR submitted: During a standard service check it was found that several rim spokes of the main landing gear wheel number 2 (left-hand inboard) were found cracked. The wheel assembly was replaced as per the aircraft maintenance manual and the aeroplane was made serviceable. Transport Canada Comments: The close visual inspection of all wheel assembly landing gear items is an essential task to accomplish for all pre-departure walk-around and service checks. @ DHC 8 301 SDR # 20110524008 Frayed Aileron Cable SDR submitted: During inspection, the right- hand aileron cable was found to be significantly frayed and beginning to unravel. The area of the failing cable (Wing Station (WS) 181) is located in a cable block on the aft spar where aluminum guide rollers part number FL4C6-2. This particular area of the cable is almost impossible to see when the gust lock is engaged and/or the aileron is in a neutral position because of the cable block. Transport Canada Comments: The SDR database reveals several previous reports of this nature in this general area. A reminder for personnel that during flight control cable inspection that the entire cable run must be inspected to detect these types of failures. @ 9 of the 18 wheel spokes are broken Feedback 4/2011 9 EMBRAER, ERJ 170 200 SU SDR # 20110121001 Pylon Fairing Missing Attaching Hardware SDR submitted: During a heavy maintenance “N1” check visit on the aeroplane, a left-hand pylon inspection found that the aft lower fixed fairing assembly was missing several items of attaching hardware. Within the pylon fixed fairing, both forward quick release pins had fallen out, as had one of four mid-point attach bolts. The missing hardware was found in the bottom of the fairing. The right-hand pylon was found to have the two forward quick release pins and three of four mid-point bolts also missing. The pins and two of the three missing bolts were found inside the fairing. In both cases, the four aft mounting bolts were found installed and properly torqued. Transport Canada Comments: This operator obtained the required engineering Original Equipment Manufacturer (OEM) and company approval to install a single dash length longer attaching bolt and reinstalled new quick release “pip” pins. Further investigations of the operators E170 fleet and Embraer, the Original Equipment Manufacturer (OEM), revealed that this was a fleet wide affected issue upon which a Service Newsletter (SNL) 170-54-0001 was released. Transport Canada Civil Aviation (TCCA) would like to advise all Embraer 170 operators of this Service Newsletter (SNL) and its intent to replace the discrepant hardware to increase its bolt length, final torque and to introduce a new countersunk washer. @ EMBRAER, ERJ 190 100 IGW SDR # 20110526002 Engine Driven Pump Hydraulic T-Fitting Cracks SDR submitted: During a heavy maintenance “C-check” visit, maintenance found the #1 & #2 pylon engine driven hydraulic pump pressure line T-fittings cracked and with evidence of hydraulic fluid leakage. Both pressure line T-fittings were replaced to correct the fault. Transport Canada Comments: Transport Canada Civil Aviation (TCCA) would like to advise all Embraer 190 operators and maintainers of this possible scenario. @ Crack and evidence of leakage 10 Feedback 4/2011 FAIRCHILD, SA227AC SDR # 20110614008 Metroliner Bleed Duct Failure SDR submitted: The pressurization was snagged as inoperative by the flight crew. During maintenance trouble-shooting it was noted that the engine bleed pressure would fluctuate uncontrollably and when turned to “high” only function for approximately 30 seconds. Then the eyeball vents would drop off with almost no air-flow output available. During subsequent inspection of the right-hand wing bleed air duct plumbing, maintenance found the tube assembly from the right-hand modulating valve to right- hand cooling turbine cracked in half. The tube was replaced, ground run accomplished and the aircraft returned to service. Transport Canada Comments: Transport Canada Civil Aviation (TCCA) would like to advise all Fairchild SA227 operators and maintainers of this possible bleed duct failure scenario. @ LEARJET 60 SDR # 20110608005 Cabin Temperature Control Valve Failure SDR submitted: During cruise, the cabin temperature was uncontrollable, leaving the cabin in a very warm and uncomfortable condition. Upon maintenance investigation, the cabin temperature control valve plunger body was found cracked off, shearing the plastic link arm which opens and closes the butterfly valve and rendering it uncontrollable. The valve was replaced and the aircraft made serviceable. Transport Canada Comments: Transport Canada Civil Aviation (TCCA) would like to advise all Learjet 60 operators of this possible scenario concerning the integrity of the cabin temperature control valve. @ Broken valve body and parts Feedback 4/2011 11 ROCKWELL COLLINS 609A SDR # 20110429007 Elevator Trim Servo Running Backwards SDR submitted: During annual inspection three autopilot servos and one elevator trim servo were removed and sent for 900 hour test/re-certification. The returned servos were re-installed per Maintenance Manual (MM). The Aircraft Maintenance Engineer (AME) ensured trim tab and elevator trim gauge agreed throughout the range of movement (indicated nose up corresponded with trim tab down and vice versa). Manual trim moved in the correct direction agreeing with the gauge and trim tab. What the AME didn’t notice was the direction arrows on the elevator trim switch on the control column during these checks. When pushed “up” on the electric trim switch, the system moved towards nose up rather than the correct direction of nose down. The autopilot and trim system were dual inspected and the aeroplane was sent for a test flight. During the flight, it was discovered the trim system was operating backwards and the autopilot would not hold altitude. The pilots used manual trim (which was working normally) to return to base. The trim servo was suspected and a serviceable unit was installed. The electric trim system functioned normally with the serviceable unit installed. The system was dual inspected again, sent for test flight and found airworthy. It appears the servo was assembled/rewired incorrectly by the overhaul facility although the original work order does not show rewiring. The suspect servo was returned to the overhaul facility. Transport Canada Comments: It is important to fully understand the operation of a system being worked on. It must be tested and confirmed in all modes once the work is completed. @ SAAB, SF340A SDR # 20110509004 Incorrectly Installed Fuel Line SDR submitted: During a scheduled inspection on a SAAB 340A, maintenance found a fuel line twisted on the left-hand engine lower nacelle. The line was removed, replaced and the aeroplane was made serviceable. Transport Canada Comments: Correct fuel line installation is essential to support the full range of engine operation. When installing fuel lines of any type and in particular aluminum, proper aircraft maintenance manual torque values must be followed. @ 12 Feedback 4/2011 engines AVCO LYCOMING, IO-540-AE1A5 SERVICE DIFFICULTY REPORT (SDR) # 20110317003 Connecting Rod Failure SDR submitted: The pilot reported a loud bang and subsequent engine failure. The pilot auto-rotated to an open field with no damage to the airframe during the landing. The aeroplane was removed from the field and transported to a repair facility for further investigation. Aeroplane panels were removed and a large hole in the crankcase was observed near the #3 cylinder intake lifter bore. Large pieces of crankcase debris were found on top of the engine case above the #2 cylinder area. Lycoming was advised and a field service rep came to investigate the failure on location. Initial indications were the #4 connecting rod failed just below the piston pin area and this caused the breach in the crankcase between the #3 & #4 cylinders. Transport Canada Comments: The cause of this connecting rod failure was the result of a missing wrist Pin Plug. Maintainers are reminded that all manufacturers’ instructions must be followed. @ AVCO LYCOMING, IO-360-B1B SDR # 20110322008 Incorrect Fuel Pump Fitting SDR submitted: The engine was received fresh from the overhaul facility with the engine driven fuel pump and associated fittings assembled. Post install ground runs were unable to achieve take off power. After 2300 revolutions per minute (rpm) further power lever advancement resulted in loss of revolutions per minute (rpm) and increase in manifold pressure, indicating fuel starvation. Upon inspection it was found that the inlet fitting to the fuel pump was restricted (just a pin hole) either the part was not manufactured properly (not fully drilled through) or it is an incorrect part (a restrictor fitting). In either case it does not belong on the engine. The fitting was replaced with the correct part and engine runs completed. Transport Canada Comments: Inventory control is of utmost importance. When receiving parts from stock or from a supplier, it is important to inspect for defects and that the part ordered is the part received. @ Incorrect fitting Correct fitting Feedback 4/2011 13 AVCO LYCOMING, O-320-D2J SDR # 20110329006 Sudden Engine Stoppage SDR submitted: The engine experienced a sudden stoppage in flight. Aircraft was landed and the engine was removed and shipped for inspection. Upon disassembly, it was found that the #4 cylinder failed due to a crack that progressed from near the top of the barrel almost all the way around the circumference. This failure seized the engine. This cylinder appears to be a field overhauled unit and has been sent to Transport Safety Board (TSB) for inspection. The last engine logbook entry has 488.9 hours since overhaul. The engine was last overhauled June 19, 2009 and was installed October 23, 2009. Transport Canada Comments: It is likely that this crack was almost undetectable using visual inspection technique before the catastrophic failure. Field overhauls must be completed in accordance with the manufacturer’s instruction and include any required Non-Destructive inspections carried out by an appropriately rated facility. @ PRATT & WHITNEY, PT6 A-67R SDR # 20110525010 Power Turbine Failure SDR submitted: The engine was removed subsequent to a catastrophic failure during takeoff role. The pilot reported, “engine failed on takeoff roll, audible noise, metal exiting exhaust duct, engine went to minimum flow and takeoff aborted”. During a dismantle investigation, the power section was found excessively damaged and it appeared that the failure occurred in the power turbine area. The 1st stage power turbine blades were found broken close to the platform areas. The fracture surface exhibited rough appearance with textures of brittle overloading fracture. The 2nd stage power turbine blades were found broken; the breakage varying from below shrouded the blade tip to above the blade platform. Service Bulletin (SB) 14369 was released to address a premature failure issue and Service Bulletin (SB) 14003 provides relevant life limit recommendations for pre-service bulletin 14369 2nd stage power turbine blades.@ Overload area Fatigue area 14 Feedback 4/2011 Hangar noise Aeroplane Piston Engine Operation Transport Canada Civil Aviation (TCCA) continues to receive Service Difficulty Reports (SDRs) reporting problems encountered by operators and maintainers of piston-powered aeroplanes. Some problems may be inevitable however TCCA does everything to help mitigate them. Things like following maintenance instructions, flight manual procedures and careful daily or pre-flight inspection all help to increase reliability. While the aeroplane manufacturer has the final say in how the engine must be operated, the engine manufacturer has useful resources to help operate safely and economically. Most manufacturers have online information with regard to breaking in, operating and other tips for safe continuous operation. This information can help your engine reach Time Between Overhaul (TBO) with minimal problems. One aspect often forgotten when troubleshooting or installing a new or overhauled engine is instrumentation. One cannot properly ascertain an engine’s performance without reliable data. Instrument calibration is often neglected in the interest of keeping costs to a minimum. Over the long term, what is more cost effective, an overhaul due to operating out of limits or calibrations to ensure parameters are within manufacturer recommendations? The following are some helpful links for piston engine operation: www.lycoming.textron.com/support/tips-advice/index.html http://tcmlink.com/visitors/carenfeed/index.cfm www.rotax-aircraft-engines.com/desktopdefault.aspx/tabid-49 eqUipment airWortHiness directives (ads) Transport Canada (TC) endeavours to send copies of new Airworthiness Directives (ADs), which are applicable in Canada to the registered owners of the affected products. Equipment/appliance ADs are often only distributed to our regional offices because the owners of aircraft affected by this type of AD are not generally known. Aircraft Maintenance Engineers (AMEs) and operators of the affected products are encouraged to obtain further information or a copy of the ADs from their regional TC office, their local Transport Canada Centre (TCC), their Principal Maintenance Inspector (PMI), or from the Civil Aviation AD website at: www.tc.gc.ca/cawis-swimn Manufacturer AD Number Origin Description B/E Aerospace 2011-14-08 UNITED STATES Continuous Flow Passenger Oxygen Mask Assembly Part Numbers (P/N) Timken Alcor 2011-20-51 EUROPEAN UNION Removal of affected Parts Manufacturer Approval (PMA) replacement Timken Alcor Aerospace Technologies Inc. first stage reduction sun gear and interacting planet gears from the propeller reduction gearbox assembly Feedback 4/2011 15 special airWortHiness inFormation BUlletins (saiBs) A Special Airworthiness Information Bulletin (SAIB) is an information tool that alerts, educates, and makes recommendations to the general aviation community. It is non-regulatory information and guidance that does not meet the criteria for an Airworthiness Directive (AD). SAIB Number Make/Company Subject Issue Date Federal Aviation Authority - www.faa.gov/aircraft/safety/alerts/saiB/ CE-11-41 Air Tractor, Incorporated Fuselage, Wing Attach Fittings 06-29-2011 CE-11-42 Piper Aircraft, Incorporated Flight Controls: Control Cable/Pulley Inspections 06-29-2011 NE-06-31R4 Lycoming Engines Engine Lubricating Oils 07-06-2011 CE-11-43 American Champion Aircraft Corporation Flight Controls 07-06-2011 CE-11-44 Aeronaut Instruction Research, Aerostar International, Avian Balloon, Ballonbau Worner GmbH, Ballonfabrik Augsburg, Balloon Club of America, Balony Kubicek spol s.r.o., Cameron Balloons Limited, Cameron Balloons US, Eagle Balloons Corporation, Fantasy Sky Promotions Incorporated, Head Balloons, Incorporated, Hot Air Balloons, JR Aerosports, Limited, Lindstrand Balloons Limited, Lindstrand Balloons USA Incorporated, McGrath, Michael D., National Ballooning, Sky Balloons Limited, Skypower, Ultramagic, S.A., Fuel: Cylinder Strap Installation 07-13-2011 SW-11-31R1 Honeywell MK XXII Enhanced Ground Proximity Warning System 07-18-2011 NM-11-45 ATR – GIE Avions de Transport Régional Doors: Cargo/Baggage Doors 08-01-2011 NM-11-46 Koito Industries Equipment/Furnishings: Koito Industries Passenger Seats 08-03-2011 CE-11-47 Goodyear Aviation Landing Gear, Tire Tube. Goodyear Aviation Tires, Flight Mate Butyl Inner Tube, 7.00-8.00-6. 08-09-2011 NM-11-48 Learjet Incorporated Ice and Rain Protection: Wing Transverse Duct Assembly 08-22-2011 CE-11-50 Cirrus Design Corporation Flight Controls, Flaps 08-26-2011 CE-11-49 Air Tractor, Incorporated Flight Controls, Elevator Tab Control System 08-26-2011 NM-11-51 Bombardier Incorporated Ice and Rain Protection: Wing Anti-Ice System 08-30-2011 NM-11-52 Bombardier Incorporated Flight Controls: Stabilizer Control System 08-31-2011 NM-11-53 Transport Category Airplanes Enhancements to Airworthiness Directive Processes 09-02-2011 NE-11-54 Continental Motors, Teledyne Continental Motors Propeller System 09-08-2011 CE-11-57 Air Tractor, Incorporated Powerplant, Engine Mount Section 09-14-2011 NE-11-56 American Society for Testing and Materials (ASTM) Semi-Synthetic Jet Fuel 09-14-2011 NE-11-55 American Society for Testing and Materials (ASTM) Grade 100VLL Aviation Gasoline 09-14-2011 16 Feedback 4/2011 SAIB Number Make/Company Subject Issue Date European Aviation Safety Agency - ad.easa.europa.eu/siB- docs/page-1 2011-19 AmSafe Restraint Systems - Jammed Connector in a Rotary Buckle 6/17/2011 2011-13 Mode S Transponder Loss of Detection (Complete or Intermittent) of Aircraft 7/4/2011 2011-14 Mode S Transponder Incorrect Setting of International Civil Aviation Organization 24-Bit Aircraft Address 7/4/2011 2011-15 Mode S Transponder Ground Testing 7/4/2011 2011-20 Rockwell Collins TPR-901 Mode S Transponder - Incorrect ’Downlink Aircraft Identification’ and Incorrect Operation with Airport Ground Tracking Systems 7/15/2011 2011-22 Ground and Airborne Icing 7/28/2011 2011-23 Koito Industries Seats – European Aviation Safety Agency Airworthiness Directive 2011-0098 Compliance Information 7/29/2011 2011-24 European Geostationary Navigation Overlay Service (EGNOS) Availability 8/9/2011 2011-25 Repair and/or Fabric Recovering of Rudder and Elevator 9/16/2011 Feedback 4/2011 17 service diFFicUlty reports (sdrs) JASC: Joint Aircraft System Code number defining assembly/system/components SDR No.: Transport Canada Civil Aviation (TCCA) -assigned SDR control number — please quote in any correspondence or inquiries Region (RGN): TCCA region of SDR submitter: PAC = Pacific PNR = Prairie and Northern ONT = Ontario QUE = Quebec ATL = Atlantic NCR = Ottawa (Headquarters) VAR = Various LEGEND Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN AIRCRAFT AERO COMMANDER 680F 2820 HOSE ASSEMBLY TSOC53A LEAKING 20110908005 PNR AEROSPATIALE AS 350B 7321 END EQUIPPED 350A57105300 NORMAL 20110831007 PAC AS 350B2 2120 PIPE HEATER 350A72100509 BROKEN 20110817008 PAC AS 350B2 2842 FUEL PROBE 647510033 UNSERVICEABLE 20110822010 QUE AS 350B2 2844 FUEL PRESSURE TRANSMITTER 642792002 UNSERVICEABLE 20110714009 QUE AS 350B2 2910 HYDRAULIC SYSTEM FAILED 20110909013 PNR AS 350B2 2913 BEARING 593733 LEAKING 20110902003 PNR AS 350B2 2914 MOUNT 350A35101700 CRACKED 20110803031 PAC AS 350B2 5210 NUT ASN52320BH060N BACKED/OFF 20110829005 PAC AS 350B2 6520 TAIL ROTOR GEARBOX 350A33020005 CHIPPED 20110706001 PNR AS 350B3 6420 TAIL ROTOR CONTROL LEVER 350A33152600 SERVICEABLE 20110816004 ONT AS 350BA 2435 STARTER 150SG117Q FAILED 20110714010 PNR AS 350BA 7323 CAPACITY DAMPER 366A54108800 BROKEN 20110708005 QUE AGUSTA A109S 6420 HUB 109016201107 SEIZED 20110803016 ONT AW139 6520 TAIL ROTOR GEARBOX DAMAGED 20110727001 QUE AIRBUS A310 308 2750 BEARING 551B060001 SEIZED 20110719003 QUE A319 114 2910 HYDRAULIQUE TUBE ASSEMBLY D29170060015 FAILED 20110718007 QUE A319 114 3231 BYPASS VALVE 114087005 SHEARED 20110909012 QUE A319 114 3420 AIR DATA INERTIAL REFERENCE UNIT HG2030AC11 FAILED 20110725001 QUE A320 211 2131 CABIN PRESSURE CONTROLLER 9022157021 FAILED 20110810010 QUE A320 211 2150 PLENUM HEAT EXCHANGER 749A000002 FAILED 20110725012 QUE A320 211 2497 CONNECTOR SHORTED 20110909010 QUE A320 211 2497 WING HARNESS CHAFFED 20110728006 QUE A320 211 2611 SMOKE DETECTOR CONTROL UNIT RAI2800M0706 RESET 20110708017 QUE A320 211 2611 SMOKE DETECTION FAKE WARNING 20110824003 QUE A320 211 2750 FLAP CONTROL FLAP FAILURE 20110721002 QUE A320 211 2750 FLAP CONTROL RESET 20110728003 QUE A320 211 2750 FLAP SYSTEM OUT OF RIG 20110809002 QUE A320 211 3240 BRAKES OVERHEATED 20110809001 QUE A320 211 5610 WINDSHIELD SHATTERED 20110722004 QUE A321 211 2597 EQUIPMENT WIRING NO FAULT FOUND 20110718012 QUE A321 211 2820 FUEL SYSTEM FUEL SPILL 20110809005 QUE A321 211 2842 FUEL LEVEL FUEL SPILL 20110815004 QUE A330 342 3244 TIRE 1400X530R23 BURST 20110719004 QUE 18 Feedback 4/2011 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN BAE - UK 3112 0 PICILO TUBE 1379274H25 CRACKED 20110921003 PNR BEECH 100 3210 UNIVERSAL JOINT 12269 FAILED 20110818008 PNR 200 2100 CABIN TEMPERATURE CONTROLLER HYLZ503361 BURNT CIRCUIT 20110823001 ATL 65A90 1 5520 ELEVATOR CRACKED 20110721009 ONT B100 2800 SKIN CRACKED 20110712002 QUE B200 2600 CIRCUIT BREAKER 727725 MELTED 20110719007 PNR B200 2823 FUEL SHUT OFF VALVE 1013890255 INTERMITTENT 20110902006 ONT B200 5210 UPPER AFT LATCH BOLT 504301775 SHEARED 20110825003 PNR B200 5310 FRAME 10143002611 SEVERED 20110726009 PNR B200 5310 WEB 9744001967 CRACKED 20110726011 PNR B200 5313 FRAME 1014400405 CRACKED 20110726010 PNR B200 5330 SKIN 10140001024 CRACKED 20110726008 PNR B200 7532 ETHYL VINYL ACETATE (EVA) TUBING 131823VE4 USED 20110804006 PNR B200 7540 BLEED AIR WARNING TUBE 130936P4M150 PIN HOLE 20110907005 PNR B200 7540 PRESSURE SWITCH 903800023 NEW 20110804007 PNR C90A 5210 WELD ASSEMBLY 50440014253 CRACKED 20110822008 ATL E90 5520 RIB 50610000355 CRACKED 20110802009 PNR F90 2720 RUDDER CONTROL UNSERVICEABLE 20110817003 QUE S35 5710 BOLT CORRODED 20110826006 ONT BELL TEXTRON - CAN 206B 6320 BEARING 206040038101 UNSERVICEABLE 20110808006 QUE 206B 7300 FUEL CONTROL UNIT 23070606 FAILED 20110727006 PNR 206L 1 2840 FUEL FILTER LIGHT FAULTY 20110727005 PNR 206L 4 6322 FAN 26028951 FAILED 20110718013 QUE 407 3270 TAIL SKID 206020110103 USED 20110713004 PAC 407 5330 UPPER LEFT LONGERON 206031314177 CRACKED 20110706007 QUE 407 5510 SUPPORT ANGLE 407023800129 CRACKED 20110802010 PAC 407 6220 BEARING SHEAR 407310101105 DELAMINATED 20110916008 PAC 412CF 0 DAMPER BEARING 412010187101 DELAMINATED 20110826008 PNR 429 3212 QUICK RELEASE PIN 429706069 LOOSE 20110907008 QUE 429 3246 QUICK RELEASE PIN LOOSE 20110907007 QUE BELL TEXTRON - USA 204B 6230 MAST BEARING 212040136001 UNSERVICEABLE 20110727004 PAC 205A 1 6510 HANGAR ASSEMBLY 212040600 FAILED 20110711020 PNR 205B 6340 TACH GENERATOR 32005007 INOPERATIVE 20110722007 PAC 212 0 TAIL ROTOR CONTROL TUBE 212001055101 TO BE INSPECTED 20110815017 PNR 212 2823 FUEL VALVE 233565 INTERMITTENT 20110707016 PAC 212 2913 HYDRAULIC PUMP 212076011101 LEAKING 20110707014 PAC 212 6320 FITTING ASSEMBLY 212030154101 CRACKED 20110803029 PAC 212 7311 OIL-FUEL HEATER 305330801 LEAKING 20110707012 PAC 212 7323 N2 LINEAR ACTUATOR 2040607625 SEIZED 20110707015 PAC BOEING 727 223 3231 LINE ASSEMBLY - HYDRAULIC BACH8A08NN0310T RUPTURED 20110802001 ONT 727 227 3232 LEFT-HAND GEAR DOOR ACTUATOR 731414 CRACKED 20110730001 PNR 727 243 2750 FLAP CONTROL FLAP FAILURE 20110902007 PAC 727 27C 2782 SLAT ACTUATOR 1U109592 SHEARED 20110817010 PAC 727 C 2750 FLAP SYSTEM ASSYMETRY 20110810008 PAC 737 6CT 2120 AIR DISTRIBUTION ELECTRICAL FUMES 20110901005 PNR 737 6CT 3160 DISPLAY SYSTEM 4081600930 FAILED 20110802006 PNR 737 6CT 3230 LANDING GEAR LEVER 273A33014 INTERMITTENT 20110704014 PNR 737 6CT 3310 LIGHTING 3103 BURNT 20110722009 PNR Feedback 4/2011 19 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN 737 76N 2740 STAB CONTROL INTERMITTENT 20110825005 PNR 737 76N 5610 WINDOW DRAIN NOISEY 20110711018 PNR 737 7CT 2100 RAM AIR ACTUATOR 5416744 UNSERVICEABLE 20110729007 PNR 737 7CT 2530 GALLEY EQUIPMENT ELECTRICAL ODOR 20110805006 PNR 737 7CT 2742 STAB TRIM MOTOR 6355C000101 UNSERVICEABLE 20110727007 PNR 737 7CT 3244 TIRE BLOW-OUT 20110729009 PNR 737 7CT 3244 TIRE H435X16021 FAILED 20110822012 PNR 737 7CT 3417 MODULE PITOT AIR DATA C17001BA01 FAILED 20110705004 PNR 737 7CT 3610 PRE-COOLER CONTROL VALVE 32895626 FAILED 20110830018 PNR 737 7CT 5610 R1 WINDOW 5893543150 SHATTERED 20110718016 PNR 737 81Q 3244 MAIN WHEEL ASSEMBLY 26123111 UNSERVICEABLE 20110726003 ATL 747 SPJ6 2915 RELIEF VALVE 719852 FRACTURED 20110715004 QUE 757 236 2422 STATIC INVERTER S282T0048 SMOKING 20110901002 ONT 767 333 2781 SLAT SENSOR FAILED 20110708009 QUE 767 333 2913 PACKING NAS161210 WORN 20110704010 QUE 767 333 3697 TERMINAL LUG DAMAGED 20110809003 QUE 767 33A 2130 CABIN PRESSURE CONTROL HUMAN ERROR 20110718015 QUE 767 33A 2750 POWER DISTRIBUTION UNIT S256T00411 FAILED 20110708002 QUE 767 375 5754 SLAT PANEL 114T410242 CRACKED 20110823004 QUE 767 38E 2530 COFFEE MAKER FAILED 20110831004 QUE 767 3Y0 2931 PRESSURE SWITCH S00033 FAILED 20110815008 QUE 777 333ER 2530 GALLEY OVERHEATED 20110815005 QUE 777 333ER 2597 SEAT CONTROLLER 178861101 OVERHEATED 20110708008 QUE 777 333ER 2741 PITCH TRIM RESET 20110718014 QUE BOMBARDIER BD 700 1A10 2450 CONTACTOR 59117381 BURNT 20110725009 QUE BD 700 1A10 2497 ALTERNATING CURRENT (AC) POWER FEEDER CABLE SAA0001W DAMAGED 20110826007 QUE BD 700 1A11 5610 WINDSHIELD GC331000110 CRACKED 20110913001 QUE CL600 2B19 (RJ100) 0 FLAP ACTUATOR 853D10024 SEIZED 20110916003 ATL CL600 2B19 (RJ100) 0 ROTARY VARIABLE DIFFERENTIAL TRANSFORMER (RVDT) 16735109 INOPERATIVE 20110914008 QUE CL600 2B19 (RJ100) 0 STUD BROKEN 20110921002 PNR CL600 2B19 (RJ100) 2150 AIR CYCLE MACHINE 78279015 OVERHEATED 20110727010 QUE CL600 2B19 (RJ100) 2750 BRAKE PRESSURE SENSOR UNIT (BPSU) HARNESS 601R571161 FAILED 20110808004 ATL CL600 2B19 (RJ100) 2750 ELECTRICAL WIRE DAMAGED 20110826002 ATL CL600 2B19 (RJ100) 2910 FAIRLEAD BLOCK TA3050052403 WORN OUT 20110713003 PAC CL600 2B19 (RJ100) 3230 NOSE LANDING GEAR (NLG) SELECTOR VALVE 750006000 UNSERVICEABLE 20110907003 ONT CL600 2B19 (RJ100) 3230 SOLENOID SELECTOR VALVE 750006000 FAILED 20110825007 QUE CL600 2B19 (RJ100) 3230 VALVE MAIN LANDING GEAR (MLG) SELECTOR 750005000 FAILED 20110725005 QUE CL600 2B19 (RJ100) 3230 VALVE MAIN LANDING GEAR (MLG) SELECTOR 750005000 FAILED 20110725006 QUE 20 Feedback 4/2011 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN CL600 2B19 (RJ100) 3230 VALVE MAIN LANDING GEAR (MLG) SELECTOR 750005000 FAILED 20110815014 QUE CL600 2B19 (RJ100) 3231 NOSE LANDING GEAR (NLG) AFT DOOR 6003304410 DAMAGED 20110818004 ATL CL600 2B19 (RJ100) 520 NO PARTS HARD LANDING 20110704008 QUE CL600 2B19 (RJ100) 520 WINGLET LIGHTNING STRIKE 20110822011 ATL CL600 2B19 (RJ100) 5312 ANGLE 601R3220881 CRACKED 20110812001 ATL CL600 2B19 (RJ100) 5342 HORIZONTAL STABILIZER (HSTAB) PIVOT FITTING 600210274 CORRODED 20110708011 ATL CL600 2B19 (RJ100) 5610 PILOT’S SIDE WINDOW 601R3303319 CRACKED 20110831001 ATL CL600 2B19 (RJ100) 5610 WINDOW SIDE (LEFT-HAND) NP1393221 SHATTERED 20110815002 QUE CL600 2B19 (RJ100) 5610 WINDSHIELD NP13932113 CRACKED 20110803019 ATL CL600 2B19 (RJ100) 5610 WINDSHIELD NP13932112 SHATTERED 20110824004 ATL CL600 2B19 (RJ100) 5610 WINDSHIELD (RIGHT-HAND) 601R3303318 CRACKED 20110815003 QUE CL600 2B19 (RJ100) 5712 ANGLE 601R1001113A1 CRACKED 20110824001 ATL CL600 2B19 (RJ100) 5755 SPOILER PANEL 6001060273 WORN 20110811003 ATL CL600 2C10 (RJ700) 2910 HYDRAULIC SYSTEM CHAFFED 20110725007 QUE CL600 2C10 (RJ700) 3230 GEAR SELECTOR VALVE FAILED 20110705003 QUE CL600 2C10 (RJ700) 3320 BALLAST OVERHEATED 20110727009 QUE CL600 2C10 (RJ700) 3620 BLEED LOOP FAILED 20110824002 QUE CL600 2C10 (RJ700) 5610 WINDSHIELD NP13932110 SHATTERED 20110704006 QUE CL600 2C10 (RJ701) 2810 CAP ASSEMBLY FUEL FILLER 45787221015 MISSING 20110823002 QUE CL600 2D24 (RJ900) 2530 CIRCUIT BREAKER LOOSE SCREW 20110815010 QUE CL600 2D24 (RJ900) 3251 ELECTRONIC CONTROL UNIT FAILED 20110815006 QUE CL600 2D24 (RJ900) 5610 CAPTAINS WINDSHIELD NP13932113 SHATTERED 20110704005 QUE CL600 2E25 (RJ1000) 2497 CIRCUIT BREAKER MS2536180 LOOSE TORQUE 20110829002 QUE CANADAIR CL215 1A10 0 BEARING AW12VCRPG1 CRACKED 20110915009 PNR CL215 1A10 0 BOLT AN173C6 WORN 20110915008 PNR CL215 1A10 2300 MICROPHONE SWITCHES INTERMITTENT 20110707010 PNR CL215 1A10 3233 O-RINGS MS28775225334 SPLIT 20110701003 PNR CL600 2B16(604) 2910 TUBE ASSEMBLY REAR FUSELAGE 604752383 CHAFED 20110711017 ONT CESSNA 150M 7120 ENGINE MOUNT 4511201 CRACKED 20110826011 ONT 152 5347 SPRING SEAT PLUNGER 4112652 BROKEN 20110811009 PAC Feedback 4/2011 21 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN 152 7414 DISTRIBUTOR GEAR K3008 LOOSE FINGER 20110804001 ONT 172E 2701 CONTROL WHEEL PLASTIC BROKEN 20110817005 ONT 172M 1420 CIRCUIT BREAKER SWITCH W31X2M1G25 UNSERVICEABLE 20110914005 PNR 172M 2720 RIGHT-HAND AFT RUDDER CABLE 510105307 FRAYED 20110819004 PAC 172M 3245 NOSE WHEEL TUBE DETERIORATED 20110729010 PAC 172N 3340 SWITCH S21605 JAMMED 20110810007 ONT 172P 3340 SWITCH TTGCTA201TWB JAMMED 20110810006 ONT 172S 8011 STARTER 149NLEC BURNT INTERNALLY 20110713002 PNR 180 5753 FLAP TRACK 12210107 CRACKED 20110903001 ONT 550 3210 DOOR BOND ASSEMBLY 652750153 DELAMINNATED 20110718004 ONT 560 3230 NOSE LANDING GEAR (NLG) DOWNLOCK SWITCH 1EN1186 FAILED 20110826005 PNR CONVAIR - CAN 340 2400 HEATER MOTOR RELAY 1A7S5001 BURNT 20110701001 PNR DASSAULT FALCON 7X 2133 INTEGRATED CABIN PRESSURE CONTROL SYSTEM (ICPCS) VALVE CABIN VENT 211916810 UNSERVICEABLE 20110907004 ONT FALCON 900EX 3246 WHEEL SEAL 50142921 DAMAGED 20110719009 PNR FALCON 900EX 520 PITOT-PROBE LEFT-HAND 50520 IN SERVICE 20110704011 QUE DEHAVILLAND - CAN DHC 2 MKI 2730 TRIM CABLE C2CF579A BROKEN 20110829013 ONT DHC 2 MKI 5510 STABILIZER FORWARD ATTACH BRACKET C2TP187A CRACKED 20110725015 PNR DHC 2 MKIII 1000 BUSHING CT2FS10572 NEW 20110722010 PAC DHC 3 2497 CIRCUIT BREAKER SWITCH W31XZMIG10 WON’T RESET 20110711015 ONT DHC 3 7332 FUEL FLOW TRANSMITTER FT100EI USED 20110821001 QUE DHC 6 5714 STRUCTURE ASSEMBLY - WING C6W1002 NEW 20110715006 PAC DHC 6 300 5630 WINDOW C3FS5152 BROKEN 20110804003 ATL DHC 7 102 2910 HYDRAULIC TUBE 72980010217 NEW 20110811005 ONT DHC 8 102 2197 TERMINAL BLOCK M817142DA1 CORRODED 20110803023 ATL DHC 8 102 2731 RIGHT-HAND ELEVATOR SPRING TAB 85520003009 BURN HOLES 20110908007 ATL DHC 8 102 2910 HYDRAULIC LINE AE2463510E0124 LEAKING 20110921004 PAC DHC 8 102 2910 PRESSURE LINE 82974010119 PIN HOLE 20110803020 ATL DHC 8 102 2910 UNION AN81510D CRACKED 20110915003 PNR DHC 8 102 2913 PACKING DETERIORATED 20110725010 ATL DHC 8 102 3230 PULLEY MS20219A4 SEIZED 20110830012 ATL DHC 8 311 5210 END FITTING 85210096103 FRACTURED 20110704009 ATL DHC 8 311 5413 INTERCOSTAL 85411581103 CRACKED 20110801006 PAC DHC 8 314 3230 ACTUATOR 82910016009 LEAKING 20110725014 ONT DHC 8 315 3230 NOSE LANDING GEAR (NLG) ACTUATOR FLEX HOSE DSC252B40124 FATIGUE FRACTURED 20110919003 ONT DHC 8 400 2730 CENTERING SPRING 8SC0798 BROKEN 20110711011 ONT DHC 8 400 2913 ENGINE DRIVEN HYDRAULIC PUMP 6617304 CRACKED 20110706005 ONT DHC 8 400 3020 INTAKE ADAPTOR HEATER 4100S02802 BURNT 20110802002 ONT 22 Feedback 4/2011 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN DHC 8 400 5610 LEFT-HAND WINDSHIELD 80260007 CRACKED 20110706006 ONT DHC 8 400 5610 WINDSHIELD NP15790120 CRACKED 20110922002 ONT DHC 8 402 2810 FUEL TANK METAL FILINGS 20110824006 ATL DHC 8 402 2910 TUBE ASSEMBLY 82974270003 CHAFFED 20110708018 QUE DIAMOND - AS DA 40 5210 HINGE DA452212600 CRACKED 20110708001 ATL DA 40 5210 HINGE DA452212600 CRACKED 20110708003 ATL DA 40 5210 LATCH PIN DA452107300 LOOSE 20110708013 ATL DA 42 7310 FUEL RETURN LINE 057313K003105 CHAFFED 20110727008 PNR DIAMOND - CAN DA 20 C1 0 NOSE FORK 20322008001 CRACKED 20110915004 ATL DA 20 C1 3220 FORK 2032200800 CRACKED 20110906001 ATL DA 20 C1 3220 FORK WHEELING 20322001061 CRACKED 20110815015 ATL DA 20 C1 3220 NOSE FORK TRAIN 20322001061 CRACKED 20110810012 QUE DA 20 C1 7600 THROTTLE CABLE A15500550 BROKEN 20110902005 PNR DA 20 C1 8540 REAR CASE ASSEMBLY 6538572 CHIPPED 20110718001 ATL DORNIER 228 202 2730 ELEVATOR CONTROL A332200B00C DELAMINATED 20110707005 PNR EMBRAER EMB 145LR 5554 BOLT NAS6404A26D BROKEN 20110830020 QUE EMB 145LR 5711 WING LOWER SPAR CAP 14566091001 CRACKED 20110711013 QUE ERJ 170 200 SU 2530 GALLEY OVEN BURN SMELL 20110822004 QUE ERJ 170 200 SU 2780 SKEW SENSOR 1702286B FAILED 20110729006 QUE ERJ 170 200 SU 2780 SLAT CONTROL RESET NO FAULT 20110712001 QUE ERJ 170 200 SU 2781 RIGHT-HAND SLAT POSITION SENSOR 5912847 FAILED 20110708004 QUE ERJ 170 200 SU 2781 SLAT SKEW SENSOR 1702286B FAILED 20110728001 QUE ERJ 170 200 SU 2781 SLAT SKEW SENSOR 1702288B FAILED 20110728002 QUE ERJ 170 200 SU 3242 #4 BRAKE 900005832PR FAILED 20110729003 QUE ERJ 170 200 SU 3242 BRAKE 900005832PR FAILED 20110729004 QUE ERJ 170 200 SU 3242 BRAKE ASSEMBLY 900005832PR FAILED 20110707011 QUE ERJ 170 200 SU 3600 POWER SUPPLY MODULE 59130164 BLEED FAIL 20110722003 QUE ERJ 170 200 SU 5210 DOOR DEFLECTOR FAILED 20110822002 QUE ERJ 170 200 SU 7600 ENGINE CONTROL RESET 20110808002 QUE ERJ 190 100 IGW 2150 AIR CYCLE MACHINE (ACM) 10007004 PACK FAILURE 20110721004 QUE ERJ 190 100 IGW 2350 NETWORK INTERFACE MODULE 7517964917 UNSERVICEABLE 20110805001 QUE ERJ 190 100 IGW 2420 RAM AIR TURBINE (RAT) FAILED TO DEPLOY 20110705005 QUE ERJ 190 100 IGW 2421 GENERATOR CONTROL UNIT (GCU) 1701321D FAILED 20110725004 QUE ERJ 190 100 IGW 2450 NETWORK INTERFACE CARD (NIC) 1 FAILED 20110718006 QUE ERJ 190 100 IGW 2530 COFFEE MAKER OVERHEATED 20110816001 QUE ERJ 190 100 IGW 2530 GALLEY OVENS BURN SMELL 20110822003 QUE ERJ 190 100 IGW 2750 FLAP ACTUATOR C1558111 FAILED 20110718009 QUE ERJ 190 100 IGW 2750 FLAPS RESET 20110718011 QUE ERJ 190 100 IGW 2750 FLAPS RESET 20110708012 QUE ERJ 190 100 IGW 2782 SLAT ACTUATOR TYPE E 1703911A FAILED 20110708015 QUE ERJ 190 100 IGW 3010 CLAMP 6299210200 LOOSE 20110805003 QUE ERJ 190 100 IGW 3230 MAIN LANDING GEAR (MLG) FAILED 20110908006 QUE ERJ 190 100 IGW 3411 AIR DATA SMART (ADS) PROBE BEE STRIKE 20110816002 QUE ERJ 190 100 IGW 3600 PNEUMATIC SYSTEM BLEED FAILURE 20110721003 QUE ERJ 190 100 IGW 3620 PNEUMATIC INDICATOR OVERPRESSURE 20110808001 QUE Feedback 4/2011 23 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN ERJ 190 100 IGW 3620 PRE-COOLER GASKET FAILED 20110725003 QUE ERJ 190 100 IGW 5210 DOOR DEFLECTOR 17068153401 FAILED 20110816003 QUE ERJ 190 100 IGW 5210 PAX DOOR DEFLECTOR FAILED 20110815007 QUE ERJ 190 100 IGW 5610 WINDSHIELD NP18730112 CRACKED 20110708014 QUE EUROCOPTER FRANCE AS 355 6230 GUIDE SWASHPLATE 350A37118101 SCRAPPED 20110711014 ONT EC 120 B 2300 PANEL C523S3200203 LOST 20110829001 PNR EC 130 B4 2435 STARTER GENERATOR 150SG122Q SERVICEABLE 20110822017 ONT EC 130 B4 5610 WINDSHIELD CENTRAL 350A25902500 CRACKED 20110816006 ONT FAIRCHILD SA227AC 2497 RIGHT-HAND CONTINUOUS ALCOHOL-WATER INJECTION (CAWI) RELAY J62A FAILED 20110802004 ONT SA227AC 2750 FLAP VALVE 246003 INTERMITTENT 20110829014 ONT SA227AC 3222 CENTERING ARM 54510443 UNAPPROVED PART 20110829011 PNR SA227AC 3230 O-RING FAILED 20110901001 ONT SA227CC 3120 TORQUE INDICATOR 2719158007 INTERMITTENT 20110830013 ONT SA227DC 2497 HOSE ASSEMBLY 3284301125 BURNT 20110829016 ONT SA227DC 3230 UPLOCK ROLLER BOLT NAS660421 SHEARED 20110802005 ONT FOUND BROTHERS FBA 2C1 0 FUEL VENT VALVE 342700 NEW 20110919004 PAC FBA 2C1 3246 BEARING 13889 DESTROYED 20110707007 PAC GROB-WERKE G 120A 0 AIR CONDITIONING HOSE TEGR101008 WORN 20110920010 PNR G 120A 7314 ENGINE DRIVEN FUEL PUMP RG9570K1M USED 20110811007 PAC GULFSTREAM - ISRAEL GULFSTREAM 100 2130 WORM GEAR CLAMP LOOSE 20110822016 ONT HAWKER SIDDELEY-UK HS 748 2A 2910 HYDRAULIC CUT OUT VALVE AIR41916 CRACKED 20110803022 ONT HUGHES 369D 6320 ROLLER BEARING 369D25146 CRACKED 20110810011 PAC 369D 7200 CHIP ON 20110913002 PAC LEARJET 45 2433 DIRECT CURRENT (DC) CONVERTER LT71 FAILED 20110801001 QUE 45 2700 CABLE ASSEMBLY 7627102004001 WORN 20110713001 QUE 45 2820 FLEX HOSE ASSEMBLY 244224151152 DETERIORATED 20110831003 ONT LOCKHEED 382G 5330 PLATE/SKIN CRACKED 20110818006 PAC MITSUBISHI - USA MU 2B60 2510 ADEL CLAMP MS91919WDG8 WORN 20110805002 ONT MOONEY M20F 5753 FLAP SWITCH - MICRO 2TL7510 USED 20110829008 PNR PILATUS - SW PC 12 45 2742 ALTERNATIVE/ AUTOMATIC TRIM MOTOR 9787314203 INOPERATIVE 20110822005 ONT PC 12 45 7110 LEVER AND LINK ASSEMBLY 5711009072 STRIPPED 20110706009 ONT 24 Feedback 4/2011 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN PIPER PA23 250 2730 SCREW STABILATOR TRIM 2080203 USED 20110808007 PAC PA23 250 3222 NOSE GEAR LOCK LINK 1666700 BROKEN 20110822006 ONT PA28 140 2750 FLAP RETURN SPRING 6282000 UNSERVICEABLE 20110726015 PAC PA31 350 2822 FUEL BOOST PUMP 2B663 OVERHAULED 20110803032 PNR PA31 350 2822 FUEL BOOST PUMP 2B663 USED 20110717001 PNR PA31 350 3221 NOSE LANDING GEAR (NLG) RIGHT- HAND DRAG LINK 4033600 CRACKED 20110707006 PAC PA31 350 3230 WIRE BROKEN 20110912001 ATL PA31 350 5711 LEFT & RIGHT WING MAIN SPAR 447400203 WEB BUCKLED 20110726014 PAC PA34 220T 2730 TRIM CABLE 62701073 FRAYED 20110805004 PAC PA44 180 7800 MUFFLER 86299007AWL BROKEN 20110826010 ATL ROBINSON R44 II 2421 ALTERNATOR ALU8521 FAILED 20110706008 PNR R44 II 2822 FUEL PUMP D7434 FAILED 20110829012 PNR R44 II 2822 FUEL PUMP LW15473 LEAKING 20110829007 PNR R44 II 2916 RESERVOIR D2112 VENTING 20110829004 PNR R44 II 5610 BUBBLE WINDOW D044713014 DEFORMED 20110823005 PNR R44 II 6210 MAIN ROTOR BLADES C0165 USED 20110714006 ONT R44 II 6230 RETAINER C2061 SCORING 20110725013 PNR R44 II 6310 ACTUATOR C0512 FAILED 20110902004 PNR R44 II 6310 CLUTCH C1883 SCRAPPED 20110809004 ONT R44 II 7314 FUEL PUMP FAULTY 20110803021 PNR R44 II 7314 FUEL PUMP LW15473 LEAKING 20110829010 PNR R44 II 7800 LEFT-HAND EXHAUST COLLECTOR C1695 CRACKED 20110908002 PAC R44 II 7800 MUFFLER C16932 USED 20110714007 ONT R44 II 7921 FANSHAFT C0075 CORRODED 20110729002 PNR SAAB 340B 2897 TUBE ASSEMBLY 7228306561 PIN HOLE 20110901003 PNR SIKORSKY S61L 2820 HOSE S613062150003 CONTAMINATED 20110721010 PAC S76C 7931 ENGINE OIL PUMP 292005310 FAILED 20110830019 PAC SWEARINGEN SA226TC 5341 FITTING HALF 2722123 CRACKED 20110812003 PNR SA226TC 5741 FITTING HALF 2722121 CRACKED 20110812004 PNR VIKING CANADA DHC 6 400 5313 STRUCTURE ASSEMBLY SIDE FUSELAGE C6FS2402 NEW 20110715007 PAC DHC 6 400 7300 TUBE ASSEMBLY- BOOSTER PUMP C6PF10761 NEW 20110808005 PAC ENGINE ALLISON 250-C20B 2435 SPRING/SCREW/ WASHER BURNT 20110714008 ATL 250-C47B 7240 OUTER COMBUSTION CASE 23030911 CRACKED 20110725016 PAC AVCO LYCOMING IO-540-C1B5 8530 CYLINDER LW12425 CRACKED 20110802003 PNR LTIO-540-J2BD 7322 FUEL SERVO 25245009RSH INTERMITTENT 20110722006 PNR LTIO-540-J2BD 8120 SUPPORT ASSEMBLY LW18302 FRACTURED 20110722008 PAC LTS-101-750B-1 7200 ENGINE 400100025 MAKING METAL 20110811008 PNR O-235-L2C 7600 CARBURETOR HEAT CONTROL S123019 SEPARATED 20110811006 ONT Feedback 4/2011 25 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN O-320-D2J 7600 CARBURETOR HEAT CONTROL S123015 SEPARATED 20110823003 ONT GARRETT TFE731-20AR-1B 7931 OIL PUMP 30607852 OVERHAULED 20110701002 PAC TPE331-11U 8300 CASE 408188265 CRACKED 20110802007 ONT TPE331-11U- 612G 0 AFT PROPELLER SHAFT BEARING 3583605 DAMAGED 20110915001 PNR GENERAL ELECTRIC CF34-10E5A1 7100 STAGE 4 LOW PRESSURE TURBINE BLADE 266M13P01 MISSING 20110908004 QUE CF34-3A1 7230 COMPRESSOR SPOOL STAGE 3-8 6078T56P05 PARTS MISSING 20110704004 ATL HONEYWELL AS907-1-1A 7261 O-RING - OIL FILL CAP DAMAGED 20110713005 QUE TFE731-20AR 0 CARBON BUSHING 7410024 NEW 20110707009 ATL PRATT & WHITNEY-CAN PT6A-21 7261 OIL FILTER 307097601 CRACKED 20110722002 ONT PT6A-21 7321 FUEL CONTROL UNIT (FCU) BEARING FAILED 20110826004 ATL PT6A-42 7261 SEAL 3022375 LEAKING 20110826012 PNR PT6A-42 7261 SEAL 3022375 LEAKING 20110826013 PNR PT6T-3 0 LINE 3028325 BROKEN 20110921007 PAC PW123B 7530 HIGH PRESSURE SHUT- OFF VALVE (HPSOV) 7786863 SOLENOID CORRODED 20110801002 ONT PW123E 0 OIL TRANSMITTER APT761000100DW INTERNAL FAILURE 20110919001 ONT PW306C 7200 CARBON SEAL 30B589801 FAILED 20110721008 PAC PRATT & WHITNEY-USA R-1340-S3H1-G 8530 CYLINDER 399352 CRACKED 20110809006 QUE R-1340-S3H1-G 8530 CYLINDER 399352 CRACKED 20110817009 QUE R-985 7414 SEAL 383021 SHRUNK 20110804004 PAC R-985-AN-14B 8520 MASTEROD 39787 BROKEN 20110815016 ONT R-985-AN-14B 8530 ALUMINUM CYLINDER HEAD 399353 SCRAP 20110804005 PAC ROLLS ROYCE - UK RB211 TRENT 772B-60 7230 HIGH PERFORMANCE COMPUTING (HPC) 5 AND 6 BLADE DAMAGED 20110707001 QUE RB211 TRENT 772B-60 7280 HOUSING MAGNETIC CHIP DETECTOR (MCD) PLUG VA3509 BROKEN 20110721007 QUE TELEDYNE CONTINENTAL IO-360-G 7310 FUEL INJECTOR LINE 630662 CRACKED 20110707004 ATL IO-520-D 8520 THRUBOLT 641931981 CRACKED 20110817002 ATL O-200-A 0 CYLINDER AE65314 STUCK OPEN 20110915006 ONT TURBOMECA ARRIEL 1D1 7100 ENGINE 292005220 SEIZED 20110909009 PNR ARRIEL 1D1 7532 BLEED VALVE 9550161210 UNSERVICEABLE 20110705006 QUE ARRIEL 1D1 8012 INJECTOR TUBE ASSEMBLY 301008030 CRACKED 20110712006 PAC PROPELLER AEROPRODUCTS A6441FN-606A 0 PROPELLER MASTER GEAR A6441FN606 DAMAGED 20110916002 PAC HAMILTON STANDARD 14SF-7 0 PROPELLER BLADE SFA13M1ROAD OVERHAULED 20110915007 PAC 26 Feedback 4/2011 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN HARTZELL HC-E3YR-2ALTF 6120 PROPELLER CONTROL CABLE 2489417 BROKEN 20110707008 PAC PHC-C3YF-1RF 6110 BLADES FORK F76632RB3252 CRACKED 20110906002 PNR MCCAULEY 1C172/TM7653 0 PROPELLER BLADE 1C172TM7653 BROKEN 20110914006 QUE 3AF34C92 6110 LATCH PINS B4324 CRACKED 20110804002 PAC 4HFR34C771 6140 TACHOMETER GENERATOR 503890571 USED 20110804008 PNR EQUIPMENT AERO DESIGN 8270601 5300 STEP BRACKET 8273301 CRACKED 20110729008 QUE AIR TRACTOR EQUIPMENT 5330 EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA 145621 SERVICEABLE 20110727011 PAC ARTEX 4535002 2562 G SWITCH UNSERVICEABLE 20110822007 PNR B/E AEROSPACE 17640177 3500 VALVE - SHUT OFF NORMAL 20110831006 PNR BAE SYSTEMS 4916405 2000 INTERFACE ASSEMBLY 77430025803 UNSERVICEABLE 20110721006 QUE BELL TEXTRON - CAN 2660162401 7230 IMPELLER 2660162401 NEW 20110706002 PAC BOSCH AMERICAN SB9RU3 7414 SPRING SHORT- CIRCUITING SP52109 CORRODED 20110816007 PAC BRUCE BC10066003 3320 LIGHT SOCKET BC10066003 UNSERVICEABLE 20110715003 PNR CESSNA 991026928 7300 LEFT-HAND MIXTURE CONTROL 991026928 INCORRECT ASSEMBLY 20110827001 PNR DEHAVILLAND - CAN DHC 6 200 0 PORTABLE FIRE EXTINGUISHER 100-9750N EMPTY 20110922005 ONT DHC6 1430 RIVET SOLID MS20470AD325 NEW 20110819005 PNR MS276454 2000 FLIGHT CONTROL BEARING MS276454 NEW 20110704012 PAC GOODYEAR 302246401 3245 TUBE 302246401 DAMAGED 20110706003 ONT HAMILTON SUNDSTRAND T62T405 4920 COMBUSTOR HOUSING ASSEMBLY 118012100 UNSERVICEABLE 20110711019 PNR HARTZELL F848L 6120 PROPELLER GOVERNOR F848L LEAKING 20110712005 PNR KANNAD 406AFCOMPACT 2562 ‘D’ SUB CONNECTOR S182051403 NEW 20110810009 ONT LORD MFG LM82710 7120 ENGINE ISOLATOR LM82710 SEPARATED 20110817004 PNR MEGGITT SAFETY SYS 50105201 0 BUSHING 5013566 UNSERVICEABLE 20110916006 PNR PIPER 587779 0 POTENTIOMETER 587977 BURNT 20110916004 PAC Feedback 4/2011 27 Make/Model Jasc Part Name Part Number (No.) Part Condition SDR No. RGN PRATT & WHITNEY-CAN PT6A27 7261 OIL FILTER 7579522AM NEW 20110705002 PNR ROCKWELL COLLINS 8220868087 0 #1 FLIGHT MANAGEMENT SYSTEM (FMS) INPUT/OUTPUT OPERATIONS PER SECOND (IOPS) CARD 8220868087 BATTERY FAILED 20110913006 PNR 8220868087 0 #2 FLIGHT MANAGEMENT COMPUTER (FMC) INPUT/OUTPUT OPERATIONS PER SECOND (IOPS) CARD 8220868087 BATTERY FAILED 20110913005 PNR 8221987006 0 MAINTENANCE DIAGNOSTIC COMPUTER (MDC) INPUT/OUTPUT OPERATIONS PER SECOND (IOPS) CARD 8221987006 BATTERY FAILED 20110913007 PNR TELEDYNE BENDIX 105005561 7414 DISTRIBUTOR BLOCK 10357426 SEPARATED 20110805005 PAC UNISON 4370 7414 IMPULSE COUPLING M3100 WORN 20110803027 ONT VICKERS 3031749001 0 PUMP HYDRAULIC 3031749001 WEEPING 20110914012 PNR EQUIPMENT 2590 SEAL CUT 20110811004 PAC WIPAIRE 3A07000001 3230 LINK-PISTON ROD 3A07094001 BROKEN 20110823006 PNR UNAPPROVED PART BAE SYSTEMS 4916405 2000 INTERFACE ASSEMBLY 77430025803 UNSERVICEABLE 20110721006 QUE CESSNA 991026928 2000 LEFT-HAND MIXTURE CONTROL 991026928 INCORRECT ASSY 20110827001 PNR DEHAVILLAND - CAN MS276454 2000 FLIGHT CONTROL BEARING MS276454 NEW 20110704012 PAC HeadqUarters Transport Canada (AARDG) Place de Ville, Tower C Ottawa ON K1A 0N8 Tel: 613-952-4357 regional oFFices Atlantic Transport Canada 95 Foundry St., 6th Floor Moncton, NB E1C 5H7 Tel: 1-800-387-4999 Prairie and Northern Transport Canada 344 Edmonton Street Winnipeg, MB R3C 0P6 Tel: 204-983-3152 1-888-463-0521 Ontario Transport Canada 4900 Yonge St., Suite 400 Toronto, ON M2N 6A5 Tel: 416-952-0230 Quebec Transport Canada 700 Leigh Capreol Dorval, QC H4Y 1G7 Tel: 514-633-3319 Pacific Transport Canada 800 Burrard St., Suite 620 Vancouver, BC V6Z 2J8 Tel: 604-666-3518 civil aviation internet sites Civil Aviation Homepage www.tc.gc.ca/eng/civilaviation/menu.htm Continuing Airworthiness www.tc.gc.ca/eng/civilaviation/certification/ continuing-menu-1432.htm Canadian Aviation Regulations (CARs) www.tc.gc.ca/eng/civilaviation/regserv/cars/menu.htm Airworthiness Directive www.tc.gc.ca/cawis-swimn Civil Aviation Safety Alerts (CASA) www.tc.gc.ca/civil-aviation-safety-alert Web Service Difficulty Reporting System (WSDRS) www.tc.gc.ca/wsdrs