Canadian Aviation Service Difficulty Reports - Transports Canada

practices may affect engine reliability. In addition to this, P&WC has developed a new bolt specification for this application available since February 2012. 2 Feedback 1/2014 FIXED WING Aerospatiale ATR 42-320 SDR # 20121109009 Cargo Door Retract Actuator Frame Mount Failure SDR submitted: Maintenance reported that during a regular inspection, it was noticed that the cargo door wasn`t opening fully causing the actuator to run to its limit. During investigation, it was noticed that the cargo door seemed overly flexible and presented more sway than expected. When the cargo door interior panel was opened, a crack was found emanating from the retract actuator frame mount attachment point. The frame was repaired and the aeroplane was made serviceable. Transport Canada Comments: Through discussions with Aerospatiale Continuing Airworthiness engineering, it was determined that this condition does not impose a detrimental effect to flight safety and the repair is covered by the Structural Repair Manual (SRM) 52-31-00. Transport Canada Civil Aviation is advising all ATR 42 owners, operators and maintainers of this possible condition.@ BAE - (Raytheon), Hawker 800XP SDR # 20121120006 Fuel Crossfeed Bellcrank Lever Corrosion SDR submitted: During a routine heavy maintenance 48 month inspection for corrosion, maintenance found the fuel crossfeed bellcrank lever severely pitted and corroded beyond acceptable repair limits. The bellcrank lever was replaced with a new part in accordance with the Aircraft Maintenance Manual (AMM) 28-20-00. Total part time since new was 3900 hours and time cycles since new 2475. Transport Canada Comments: An important item to be aware of when performing a corrosion inspection on Hawker 800XP aeroplanes.@ Cargo door retract actuator supporting mount structure crack A corroded fuel crossfeed bellcrank lever Feedback 1/2014 3 Piper PA-32R-301 SDR # 20121114001 Aileron Hinge Bracket Corrosion SDR submitted: During removal of the right hand aileron for painting, the Aircraft Maintenance Engineer discovered severe corrosion on the inside hinge that reduced the bracket thickness to about 60%-70% of the original manufactured thickness. Corrosion was also found on the left-hand aileron hinge bracket. Consequently, all 4 hinge brackets were replaced on the right-hand and left-hand ailerons. Transport Canada Comments: Transport Canada Civil Aviation (TCCA) investigated further and found 1 previous Service Difficulty Report (SDR) that reported aileron hinge bracket corrosion. Additionally, the Federal Aviation Administration (FAA) have published the following Special Airworthiness Information Bulletins (SAIB) pertaining to corrosion related problems on Piper PA-28, PA-32, PA-34 and PA-44 aeroplane models. TCCA recommend that owners/operators comply with the FAA corrosion related recommendations contained within these SAIB(s): CE-11-10 (flap hinges/brackets/ribs), CE-11-12 (wing rear spar fuselage attach fittings), CE-11-13(wing front spar corrosion) and, CE-11-14 (vertical forward stab attach point).@ Beech 200 SDR # 20120510005 Rudder Pedal - Broken SDR submitted: During taxi operations, the pilot reported that the left-hand rudder pedal unit broke. The pedal was subsequently replaced with a new assembly. In addition, the left-hand rudder pedal arm shaft bracket taper pin was also found to be excessively worn and had to be replaced. As a precautionary measure, the remaining rudder pedals were inspected and as a result the right-hand rudder arm to pedal attachment point was found to have excessive play and was worn beyond specified limits. Transport Canada Comments: The rudder pedal assembly is constantly undergoing various stresses that over a short period of time can result in excessive wear and stress cracks. This is an area that requires regular attention as exemplified in the above scenario and this operator’s responsible follow-up action resulted in the following f inding: the pilot and co-pilot rudder pedal arms, part number 50-524326-33, worn to limits at the upper bushings.@ Aileron Hinge Bracket Corrosion 4 Feedback 1/2014 Beech 95 SDR # 20120809014 Rudder Trim Cables - Reversed SDR submitted: During cruise flight, the pilot attempted to centre the ball in the “Turn and Bank Indicator” by applying rudder trim, however the effect was opposite to normal (turned trim wheel left but the right rudder trim was noted to move). Soon afterwards, the pilot landed and maintenance personnel later confirmed that the rudder trim system was operating in reverse. A complete inspection revealed that the rudder trim cables exiting the rear bulkhead to nearby pulleys that direct trim cables up the vertical stabilizer were confirmed to be routed incorrectly. Maintenance rigged the trim cables correctly followed by a dual inspection check by qualified personnel. Company quality assurance investigation revealed that this aircraft was imported some 6 years ago and verified that the rudder system had not altered during the importation process nor since that time. During these last 6 years, both flight crews and maintenance personnel had missed this potentially dangerous flight control error. Proper rudder control input would be critical during an engine failure in order to assist flying with asymmetrical thrust, especially in the fire suppression role/low altitude role that this particular aircraft is engaged in. Flight training (“engine out” procedures) is conducted on a similar Baron with dual flight controls which may be one of the reasons that this rudder trim rigging error was not detected on the occurrence aircraft. Another reason could be that the cockpit rudder trim indicator is labeled “Rudder Tab” and the control wheel mechanism is labeled “Left-Rudder Tab-Right”. Most rudder trims are identified as “Nose Left or Nose Right”. Transport Canada Comments: These types of flight control errors would not have occurred if personnel following the maintenance instructions subsequently conducted dual independent inspections. Alarmingly, these types of occurrences continue to occur on both the rudder and elevator trim systems and have resulted in fatal occurrences. It is strongly recommended that dual inspections be carried out as well as conducting visual checks on the actual flight tab position to ensure it corresponds correctly with the cockpit indicated positions.@ Rudder trim cables crossed at the rear bulkhead Cables crossed Feedback 1/2014 5 Boeing 727-243 SDR # 20121122007 Slat Actuator Supporting Mount Failure SDR submitted: Upon selecting flaps down on approach, the crew noticed a hydraulic system low pressure light and corresponding loss of quantity. The crew declared an emergency and landed without incident. Maintenance discovered the #2 slat actuator had broken from its upper mount and moved aft, shearing a hydraulic line which caused the loss of the hydraulic system and damaging an anti-ice pneumatic duct. The flap actuator supporting mount was repaired, the hydraulic line and pneumatic duct replaced and the hydraulic system re-serviced, making the aeroplane serviceable. Transport Canada Comments: Upon review of the Web Service Difficulty Reporting System (WSDRS) database, additional occurrences were noted where Boeing Service Bulletin (SB) 727-57-0130 has been released to strengthen the slat actuator mount bracket.@ Bombardier CL-600-2D15 SDR # 20121109008 Insufficient Hydraulic Line Support SDR submitted: While applying take-off power at the start of the take-off roll, the #1 engine driven pump (EDP) caution message came on and the #1 hydraulic quantity went to zero. Maintenance investigation found a chaffed hydraulic line in the aft equipment bay that caused the loss of the hydraulic fluid. The line had chaffed against stringer #7 due to a broken retaining “L” bracket. The hydraulic line and “L” bracket were replaced and the damage to the stringer was repaired making the aeroplane serviceable. Transport Canada Comments: When performing service checks and walkarounds, it’s important to inspect for the serviceable condition of hydraulic line retaining brackets and clamps.@ Failed flap actuator supporting bracket causing a complete hydraulic system failure and damaging an anti-ice pneumatic duct Hydraulic retaining “L” bracket broken and hydraulic line chaffing condition 6 Feedback 1/2014 Canadair CL-600-2B16 SDR # 20131230006 Bent Nose Landing Gear Centering Bracket SDR submitted: Upon selecting the landing gear up after departure, only the main landing gear retracted. The nose landing gear (NLG) stayed down and locked and the crew returned for an uneventful landing. Maintenance personnel traced the fault to the NLG centering sensor bracket which is believed to have been bent during a previous towbarless ground handling movement. It is suspected that the towbarless tugs strut strap had been mistakenly placed around the NLG strut centering bracket. The NLG centering sensor bracket was replaced and the aeroplane was returned to service. Transport Canada Comments: The use of towbarless tugs are now a common sight at airports around the world and this style of ground support equipment (GSE) provides better aeroplane controllability and maneuverability as compared to a standard towbar & tug configuration. As stated by the operator, Bombardier Advisory Wire 600T-2171 has been issued identifying the possible scenario where damage to the NLG when using a towbarless tug can occur. Transport Canada Civil Aviation is advising all owners, operators and maintainers of this possible scenario and available Bombardier documentation.@ Damaged nose landing gear centering sensor bracket Feedback 1/2014 7 DHC-8-400 SDR # 20110802002 Burnt - #2 Engine Intake Adaptor Heater SDR submitted: During descent through 6000 feet altitude, the #2 engine inlet adaptor heat caution light warning illuminated. Each time, the inlet bypass door was pressed, the circuit breaker for the #2 lip heater would “pop”. The crew continued the descent to exit the icing conditions, then proceeded to fly a normal circuit and landed with the engine intake de-icing system turned off. An investigation by line maintenance personnel revealed that the engine intake adaptor heater was severely damaged from a significant overheat event during operation. Soot evidence in the engine area indicates possible flames were generated; however the crew received no cockpit fire indication advisories. Evidence of soot damage was also found in the area of the electrical connector area for the heater. The failed intake adaptor heater was quarantined and has been sent to the manufacturer for further analysis. Transport Canada Comments: A review of the Service Difficulty Report (SDR) database has revealed previous failure events where the crew smelt a burning odor entering the aeroplane. In particular, one significant ground event (2004) reported smoke and flames coming from the engine cowling and air intake section caused by a failed intake adaptor heater (pre-mod part number (P/N) 4100S028-01). Investigation by the manufacturer (Zodiac Aerospace) of the engine inlet adaptor heater revealed that during manufacturing process, the heating element is difficult to place with the casting and as a result it can cause overheating during the manufacturing process or in the field. In the interim, it is recommended that maintainers routinely inspect for any visible damage to the engine inlet area and associated electrical connectors.@ Failed switch spot-welds Exterior damage to #2 engine intake 8 Feedback 1/2014 DHC-8-400 series SDR # 20120910001 Engine Oil Cooler Bypass Valves – Failures SDR submitted: A number of DHC-8-400 operators have reported engine shutdowns due to high oil temperature caused by the failures of oil cooler bypass valves part number (P/N) D2887-355C. This has resulted in numerous air turn-backs and a decreased level of safety. Bombardier have taken corrective action and have introduced a new configuration of valve (P/N D2887-955C) that incorporates an advanced polymer sleeve that will resist the swelling of the current internal rubber sleeve that was the root cause of this valve’s failures. Installation of the new valve P/N D2887-955C will also change the oil cooler assembly from a D2887-815A to D2887-915A Bombardier also recommends that operators apply a soft time to the air cooler thermal valve P/N D2887-355C at 3000 hours to avoid in-flight shutdowns or high oil pressure indication. Transport Canada Comments: Transport Canada Civil Aviation recommends that all operators install the new configuration P/N D2887-955C valve at the first opportunity. In the interim, please comply with the soft time of 3000 hours when using the older style P/N D2887-355C oil cooler valve. More specific information is contained within Bombardier document DH8-400-SL-71-014. Bombardier has now introduced SB 84-79-06 “Improved Engine Oil Cooler Bypass Valve”.@ Diamond DA20-A1 SDR # 20110107005 Chafed Radiator Pipe SDR submitted: During a routine inspection, it was found that the springs that hold the exhaust muffler in place were rubbing against the radiator pipe. Because this is a confined area, the pipe was removed for further inspection. It was then discovered that the radiator pipe was almost entirely chafed through. A loss of engine coolant during flight would have resulted in an in-flight shutdown with possible heat related damage to the engine. This is the 3rd time chaffing was reported in this area. Diamond has informed operators that when the flexible coolant hoses are replaced, that the aluminum radiator pipe needs to be the correct distance away from the exhaust springs. Transport Canada Comments: As with all adjacent components and parts, always ensure that adequate clearances exist. This is especially true in tightly confined, hard to access areas.@ Feedback 1/2014 9 Douglas DC3C SDR # 20130129007 Melted Pitot Static Lines SDR submitted: The flight crew reported to maintenance that the captain’s airspeed indicator was reading up to 40 knots lower than the co-pilot’s airspeed in flight. Maintenance performed a pitot static leak check and visual inspection of the aeroplane revealing that both the captain’s pitot and static plastic lines were melted from contacting a cockpit under-floor heater duct. The pitot and static plastic lines were routed adjacent to a heater duct, causing the contact and eventual melting of the pitot-static lines. The affected pitot-static lines were replaced and precaution was taken to relocate the replacement lines at a suitable distance away from the heater ducts, making the aeroplane serviceable. Transport Canada Comments: As stated by the operator, the work done to relocate the plastic lines was in accordance with Federal Aviation Administration (FAA) Advisory Circular (AC) 43.13-1B and 2B since the existing original equipment manufacturer (OEM) maintenance manual did not provide sufficient instructions to correct the problem.@ Fairchild SA227-DC SDR # 20120821006 Aileron In-Flight Jam Condition SDR submitted: The aileron system of the aeroplane temporarily jammed in flight. The system was troubleshot and the jam appeared to be coming from the copilot control wheel. At first it was thought to be faulty bearings at the control wheel so they were replaced and re shimmed as per the Aircraft Maintenance Manual (AMM). Further investigation found that the chain was binding at the control wheel sprocket area within the control column. The chain looked dry (no lube), its link rollers worn and showed evidence of wear at the link joints. There was also evidence of the chain contacting the insides of the control columns housing (slight loss of metal and primer). The chain was replaced and lubed, making the aeroplane serviceable. Transport Canada Comments: As commented by the operator and through extensive investigations from the original equipment manufacturer (OEM), M7, it’s now Melted pitot-static lines due to contact with a heater duct Aileron control wheel cable chain link roller with wear marks 10 Feedback 1/2014 understood that the aileron control wheel jam was caused by a combination of a lack of lubrication and excessive wear on the chain link rollers. With the excessive wear of the chain and a control wheel roll input applied, the chain would have a tendency to ride up the control wheel sprocket teeth and bind through contact with the inside wall of the control column housing. Also noted by the operator was an error in the AMM which omitted to include the specific lubrication of the aileron control wheel chain. M7 has produced Service Bulletins 27-001R2, 27-026R2, 27-054R2 and 27-074 to address this issue including corrections to the affected AMM.@ Honeywell, Equipment SDR # 20121115008 Corrosion In Float Aeroplane Avionics SDR submitted: The subject aeroplane was brought to an avionics repair shop with an autopilot snag. It was determined that the pitch servo had sustained water damage that resulted in corrosion and an intermittent short on the clutch engage wire. This in turn caused the failure of a transistor. To rectify the problem, the autopilot computer was repaired and the pitch servo was replaced. The aeroplane is equipped with amphibious floats and has drainage holes in the bottom fuselage. Transport Canada Comments: Corrosion in float aeroplanes is an ongoing concern. Avionics components are also subject to corrosion internally and must be considered when conducting inspections.@ Autopilot Servo With Corroded Transistor Feedback 1/2014 11 Learjet 60 SDR # 20120821008 Nose Landing Gear - Improper Servicing SDR submitted: During landing at touchdown, the aeroplane veered hard left when approaching 105 knots where full right rudder and brake was applied to counteract the uncommanded turn. Once the left engine was brought out of reverse thrust, the aeroplane responded and abruptly swung back to center line where the aeroplane taxied normally from the runway. Maintenance inspection found the nose landing gear (NLG) oleo was flat which prevented the internal NLG strut centering cam mechanism from aligning the NLG wheel prior to touch-down. The NLG showed no indication of hydraulic fluid leakage where it was confirmed that the nitrogen gas charge was underserviced, causing the NLG wheel misalignment. Transport Canada Comments: As stated by the operator, a correctly serviced NLG oleo requires only 75 PSI of nitrogen gas pressure and due to this low preset pressure, the oleo weight-on-wheels (WOW) extension is largely dependent on fuel load and aeroplane balance. This may be misleading to maintenance personnel and the flight crew when performing the pre-flight walk-around check in understanding if the NLG has proper oleo extension. The Aircraft Maintenance Manual (AMM) defines two types of procedures or methods to service the NLG strut for correct oleo extension. The “Preferred Method” requires the provisions to jack the aeroplane in order to accomplish the correct landing gear servicing while the “Alternate Method” enables the maintenance provider to service the gear while the aeroplane is on ground or WOW, but requires the aeroplane to be full of fuel. The attached figure represents the required oleo extension when referencing the “Alternate method” AMM servicing procedure. Recently, Learjet issued Service Bulletin SB 60-11-4 which provides the installation of a service instructions name plate on the NLG strut that defines the AMM “Preferred Method” servicing procedures.@ Nose Landing Gear Strut Static Deflection Nose Gear Strut - Servicing 12 Feedback 1/2014 ENGINES General Electric CF34-8C5 SDR # 20121130002 Engine High Pressure Turbine Failure SDR submitted: While climbing through 8000 feet, flight crew heard a loud noise followed by a yaw to the right. Right engine parameters indicated the engine was spooling down. Flight crew secured the engine, declared an emergency, turned back and landed without further incident. Initial inspection of the engine by local maintenance revealed no damage to the fan blades however there was significant damage to the turbines. Transport Canada Comments: Engine teardown revealed the failure was caused by high pressure turbine blade release. This is a known problem for CF34 engines and is caused by corrosion under the blade platform. Service Bulletins 72-0228 and 72-0242 introduce re-designed blades that address this issue.@ Pratt & Whitney - Canada PW123 SDR # 20130826001 Metal In Oil – A Sign of Engine Distress SDR submitted: At disassembly of the reduction gear box module (for a light overhaul due to metal in oil), three cracks were noted in the 2nd stage spur gear shaft wall. The cracks were originating from the nº 15 bearing mating face and propagating forward. The cracks were adjacent to each other approximately 1.52 mm (0.060”) apart. There was material breakout at the tooling slot corner. The separated piece of material was picked by the magnetic chip detector in-field. The missing piece is approximately 1.52 mm (0.060”) wide, 2.54 mm (0.100”) long and 1.27 mm (0.050”) deep. Transport Canada Comments: Metal found in oil systems and chip detector indication is an indicator of engine wear or distress. This can be a precursor to catastrophic failure. These conditions must be investigated further to determine the source. Manufacturer’s instructions regarding metal in oil found in maintenance manuals, Service Bulletins (SB’s) and Service Information Letters (SIL’s) should always be followed.@ High pressure turbine stage 2 blades Bull gear with clear crack indication and missing piece Feedback 1/2014 13 Garrett TFE731-2-2B SDR # 20131210001 Cracked Gearbox Housing SDR submitted: During a visual inspection of the engine gearbox, it was noted that the oil filter housing assembly lower mounting stud ear was cracked. The corrective action taken was to replace the aft gearbox housing case. Transport Canada Comments: Transport Canada Civil Aviation would like to raise awareness of this defect to operators of TFE731 engines. Due to the location of the stud (six o’clock position) and the length of the housing, the possibility of accidental damage is high. The cause in this case is not known; however it could have been the result of corrosion (or casting inclusion), a past over torque or perhaps an accidental overload or impact damage during installation or shipping. Whatever the case, maintainers are urged to be cautious when working on complex systems and always follow manufacturers instruction.@ General Electric, CF34-3B1 SDR # 20121101004 Broken Fire Loop Wiring Found, Potential In-flight Shutdown Avoided! SDR submitted: During routine maintenance, the left hand jet pipe loop “A” was found unserviceable. Troubleshooting found that the engine fire detection wiring harness was broken at the pylon connector. The fire detection and fire protection wiring harnesses were replaced. This defect, if unnoticed, might have resulted in an in-flight engine shutdown due to a false engine fire or jet pipe overheat warning. Transport Canada Comments: This was a good find by the maintenance team who were doing the inspection (in particular considering the defect’s location in the pylon). As aeroplane fleets in Canada and abroad age, there will likely be more of these issues discovered. @ Damaged Gearbox Housing Exposed fire loop wires near cannon connector 14 Feedback 1/2014 Garrett TPE331-10UGR-514H SDR # 20121107004 Cracked Engine Combustor SDR submitted: The crew reported that when the power lever was advanced, the engine could only achieve 40% torque. The take off run was aborted and the aeroplane returned to the hangar. A maintenance crew performed a quick visual inspection of the engine and performed an engine ground run with the cowlings open. Startup was noted to be longer than expected and when the engine achieved ground idle, the technician sitting in the cockpit noticed an orange glow from below the engine. Stop procedures where carried out and the engine was shutdown. A detailed visual inspection confirmed a large 25.4 to 30.48 cm (10 to 12 inch) long crack in the combustion liner. The engine was removed and replaced. Transport Canada Comments: The plenums on these engines are operated ‘on condition’. The type certificate holder (Honeywell) has issued Service Bulletin 72-2178 (Combustion Section –inspect combustion case assembly) that recommends it be accomplished at each scheduled fuel nozzle inspection and/or replacement. Transport Canada Civil Aviation recommends that operators familiarize themselves and comply with this service bulletin.@ Engine plenum (combustion section) with a visible 25.4 to 30.48 cm crack Feedback 1/2014 15 RotoRcRAFt Bell 212 SDR # 20130724003 Skid Failure SDR submitted: The pilot landed at a forest service lookout tower and heard a bang. He thought he had hit a rock. On landing at a local airstrip, the helicopter sat in an unusual attitude. The forward skid landing gear cross tube was found broken near a forward support. Transport Canada Comments: This cross tube is the subject of recurring Bell Helicopter Alert Service Bulletin (ASB) 212-09-132. The ASB requires a detailed inspection every 7 days. The Federal Aviation Administration (FAA) and the manufacturer have been informed and an investigation is ongoing to determine if the ASB inspection interval requirements are sufficient.@ A cross section view of the broken forward skid landing gear A forward skid landing gear cross tube broken near a forward support 16 Feedback 1/2014 Bell 212 SDR # 20130312010 Support Case Cracked SDR submitted: During a routine daily aircraft inspection, an Aircraft Maintenance Engineer (AME) was inspecting the main transmission and noticed the support case was cracked on the left hand side by the airframe attachment bolt. The transmission was removed and it was found that the support case leg was broken with the crack originating from one of the small bushing attachment screws. Transport Canada Comments: The Original Equipment Manufacturer (OEM) is currently investigating this issue. In the interim, Transport Canada Civil Aviation recommends maintenance personnel to remain vigilant while inspecting this area of the transmission.@ Bell 407 SDR # 20131129004 Oil Line Leaking Due to Fretting SDR submitted: The engine was removed from the aircraft due to a service inspection required for Bell helicopter Alert Service Bulletin (ASB) 407-13-99RA. During that time it was found that oil line part number (P/N) 70-037A0910-000 was seeping black oxide out of its internal portion. After further inspection, the steel braids were found cut. Transport Canada Comments: Transport Canada Civil Aviation reminds maintainers of the importance of keeping adequate clearance on all hydraulic, fuel and electrical lines to prevent fretting. This defect was discovered before a potential catastrophic occurrence could have occurred.@ Support case fitting crack (outer portion) Support case fitting cracked Engine oil line fretting Feedback 1/2014 17 HANGAR NoISE C&D Aerospace, Equipment SDR # 20120921002 A Surprising Cause Of Smoke In The Cabin During the interior cleaning of the aeroplane, the cabin cleaners noted a burning smell and smoke in the forward lavatory. The lead engineer of the aeroplane was immediately informed. It was found that the soap dispenser had been leaking on to the circuit breaker of the forward lavatory power outlets. The circuit breaker has open terminals on the top allowing the liquid soap to make contact and create a short. Troubleshooting showed that the soap dispenser bottle had not been properly tightened and that the circuit breaker had no protection against leaks. The circuit breaker is located directly below the bottle. The circuit breaker required replacement due to contamination and possible internal damage/short and the soap dispenser bottle was properly installed. Transport Canada Comments: Even though this incident took place on a foreign operated aeroplane, it serves as a good reminder that no matter how trivial an item may appear (such as installing a soap dispenser bottle) it can have major consequences.@ A contaminated circuit breakers 18 Feedback 1/2014 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 APICAL INDUSTRIES STC SH06-1 STC SR01535LA 2013-22-21 United States Incorrectly Installed Float Inflation Hoses EQUIPMENT 1999-01-05 United States Wing Strut Corrosion - Cracked Forks PIAGGIO D-1972-070 Germany Pilot Seats / Engine Throttle and Propeller Control System / Engine Cylinder Block Feedback 1/2014 19 FAA SPEcIAl AIRWoRtHINESS INFoRMAtIoN BUllEtINS (SAIB) A Federal Aviation Administration (FAA) 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). www.faa.gov/aircraft/safety/alerts/SAIB/ SAIB N umBer mAke/CompANy S uBjeCt ISSue DAte CE-14-09 Don Luscombe Aviation History Foundation, Inc. Luscombe Model 8A Fuel System 02/13/14 NE-13-33R2 CFM International, S.A. Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes 01/28/14 NM-14-08 Cessna Aircraft Company Fuselage: Aerodynamic Fairings 01/23/14 CE-14-07 Piper Aircraft, Inc. Wing Spar – Main Spar Lower Cap Cracks 12/12/13 SW-14-06 Rotorcraft Electrical System Assessments 12/04/13 NM-14-05 Beechcraft Corporation Wing: Ailerons 11/27/13 SW-08-03R4 Rotorcraft Recommendations for Rotorcraft During cing/Snowy Conditions 11/26/13 CE-14-04 Flight Management Computing Systems Flight Management Computing Systems; Navigation Database Updates - Data and Procedural Exclusions 11/22/13 20 Feedback 1/2014 EASA SAFEty INFoRMAtIoN BUllEtIN (SIB) European Aviation Safety Agency (EASA) SIB 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). www.ad.easa.europa.eu/sib-docs/page-1 SAIB N umBer mAke/CompANy S uBjeCt ISSue DAte 2008-59R1 Turboshaft-engine Powered Rotorcraft - Engine In-Flight Shutdown due to Ice and Snow Ingestion 02/10/14 2014-05 Hydraulic Pump Electrical Motor Connectors Incorrect Installation 02/10/14 2014-04 RNP-APCH (Required Navigation Performance Approach Procedures) with Barometric Vertical Navigation (APV/Baro-VNAV). 02/07/14 2014-03 Land and Hold Short Operations at U.S. Airports 02/04/14 2014-02 [Correction] Frequency Interference - Spurious Transmissions of Honeywell VHF Transceivers 01/17/14 UPN2014- 20130611002 General Electric CF34-10E Engines - Experimental Engine Controls (FADEC) without FAA production approval 01/15/14 2014-01 Cessna Aircraft Company Supplemental (Structural) Inspection Programmes 01/07/14 2013-23 Uncommanded Engine Loss of Power, Rotor Speed Fluctuations or In-Flight Shutdown following Electronic Engine Control Unit Failure 12/19/13 2013-22 Suspected Unapproved Parts Notification - 10 Person Life Raft part number (P/N) 6491010414, serial numbers (S/N) 0251 and 0254, and P/N 64910-10214, S/N 0249. 12/11/13 UPN2013- 20130325006 Aircraft Bolts Manufactured and Sold without FAA approval 12/09/13 2013-21 Use of Portable Electronic Devices during Commercial Air Transport Aircraft Operation 12/09/13 2011-27R1 Suspect (Bogus - Counterfeit) Electronic Components 12/05/13 SAFO13009 Hamilton Sundstrand Propeller Control Units and Adapters - Improperly Repaired or Overhauled 12/02/13 UPN2013- 20130611005 General Electric CF-34-10E Engines - Experimental Serial Numbers 994-101 and 994-103 11/22/13 2013-20 Bounced Landing Recognition and Recovery Training 11/19/13 Feedback 1/2014 21 Region (RGN): TCCA region of SDR submitter: PAC = Pacific PNR = Prairie and Northern ONT = Ontario QUE = Quebec ATL = Atlantic NCR = Ottawa (Headquarters) VAR = Various SERVIcE DIFFIcUlty REPoRtS (SDRS) LEGEND 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 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN AEROPLANE AEROSPATIALE AS 350B2 2916 HYDRAULIC RESERVOIR 350A7510350001 SERVICEABLE 20131107006 QUE AS 350B2 6510 BUSH RUBBER FA3819 MELTED 20131023011 QUE AS 350B2 6730 SERVO AC67246 SERVICEABLE 20131121003 QUE AS 350B3 7220 UPPER HOUSING 135013 NO FITTED 20131001011 ONT AS 350BA 2916 HYDRAULIC RESERVOIR 350A7510350001 SERVICEABLE 20131107004 QUE AS 350BA 2916 HYDRAULIC RESERVOIR 350A7510350001 SERVICEABLE 20131107005 QUE AS 350BA 3340 STROBE POWER SUPPLY 356H2802 UNSERVICEABLE 20131007026 PNR AS 350BA 6220 STARFLEX 350A31191800 NEW 20131107009 QUE AS 350BA 6420 ROD ACTUATING TAIL GEARBOX 350A27191003 CRACKED 20131107007 QUE AS 355NP 2913 PINION HYDRAULIC PUMP 355A32211000 SEARED 20131105012 PNR ATR 42 300 3246 BOLT WHEEL HALF MS2125006038 BROKEN 20131029002 ONT ATR 72 202 3420 ALTITUDE HEADING REFERENCE UNIT 7003360946 UNSERVICEABLE 20131003002 PNR AGUSTA AW139 6220 TAIL ROTOR SLIP RING 4G6420V00152 FAILED 20131118028 PNR AW139 6420 SLIP RING ASSEMBLY 4G6420V00151 FAILED 20131002009 PNR AIR TRACTOR AT 602 5342 LEFT-HAND STABILIZER STRUT ASSEMBLY 3010611 CORRODED 20131113008 PNR AT 802A 5311 TUBE TOP CROSS 110297 CRACKED 20131121006 PAC AT 802A 5730 SKIN STABILIZER BOTTOM 306661 USED 20131219020 PAC AT 802A 5730 SKIN STABILIZER BOTTOM 306661 USED 20131219021 PAC AIRBUS A310 308 3211 PIN D580601 CRACKED 20131219016 QUE A310 308 3213 HINGE PIN D580601 CRACKED 20131213008 QUE A319 114 2520 SMART VIDEO DISPLAY UNIT 179000201 FAILED 20131204005 QUE A319 114 2910 CHECK VALVE ZCV638 FAILED 20131023004 QUE A319 114 3242 TEMPERATURE MONITORING UNIT 351H51002 FAILED 20131104010 QUE 22 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN A319 114 3250 STEERING CONTROL UNIT E21327106 FAULTED 20131218007 QUE A319 114 3460 FLIGHT MANAGEMENT SYSTEM FAILED 20131030003 QUE A319 114 5610 WINDOW PANE SPSA320321 FAILED 20131028009 QUE A320 211 2120 RECIRCULATION FAN FILTER DIRTY 20131017006 QUE A320 211 2750 FLAP SYSTEM FAILED 20131216014 QUE A320 211 2820 FUEL SYSTEM SPILL 20131104011 QUE A320 211 3140 CENTRALIZED FAULT DISPLAY INTERFACE UNIT B401ACM0506 FAILED 20131212005 QUE A320 211 3200 NOSE LANDING GEAR OLEO FAILED 20131216023 QUE A320 211 3230 LEFT-HAND MAIN LANDING GEAR UPLOCK 201117013 FAILED 20131129009 QUE A320 211 3260 PIN D59880 LOOSE 20131223003 QUE A320 211 5730 UPPER WING SKIN LEFT CORRODED 20131105007 QUE A321 211 5230 PROXIMITY SWITCH FAILED 20131111020 QUE A330 243 2910 TUBE AE71112112 PIN HOLE 20131007019 QUE A330 343 5210 PASSENGER DOOR INDICATION FAILED 20131028007 QUE BAE - (RAYTHEON) BAE 125 800A 3297 CIRCUIT BOARD DISCONNECTED WIRES 20131223005 ONT BAE - UK 3112 2435 MOUNTING ADAPTER 230651430 CRACKED 20131015001 ONT BEECH 1900D 2397 PUSH TO TALK SWITCH P7500091 STUCK 20131018002 PNR 1900D 2422 MOUNTING BOLT LOOSE 20131128006 ATL 1900D 2435 ARMATURE 230781471 DUE OVERHAUL 20131121007 ATL 1900D 2750 SHAFT ASSEMBLY RIGHT-HAND OUT BOARD 1013800006 SHEARED 20131101004 PNR 1900D 2752 FLAP DRIVE 1295210502 USED 20131220003 PAC 1900D 3010 DE-ICE TUBE 131823E6D108 MELTED 20131107003 PNR 1900D 3010 LEADING EDGE 1181104717 CORROSION 20131122003 PAC 1900D 5620 WINDOW PAN/FRAME 1294300433 CRACKED 20131218014 PAC 200 5313 CROSS TIE 97430000115 CRACKED 20131104009 PNR 200 5610 FRAME 504200772 CORROSION 20131126005 PAC 3N 7120 ENGINE MOUNT CLUSTER CRACKED 20131108007 ONT 3NM 7120 ENGINE MOUNT CLUSTER CRACKED 20131108006 ONT A100 2810 RIGHT-HAND FUEL PANEL CORRODED 20131218006 QUE A100 3420 ATTITUDE INDICATOR 235010616 UNSERVICEABLE 20131103007 PNR A100 3442 RADAR 66311400 POOR DISPLAY 20131103006 PNR A100 5524 CONTROL HORN ASSEMBLY 11561001421 CRACKED 20131129005 QUE B200 2810 FUEL BLADDER 1013810021 LEAKING 20131104003 PNR B200 3060 PROPELLER OVERGREASED 20131018012 ONT Feedback 1/2014 23 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN B200 3230 CLEVIS 1018102111 CRACKED 20131219023 PNR B200 3400 NAVIGATION RECEIVER 6226137001 UNSERVICEABLE 20131104004 PNR B200 3421 GYRO 5000B41 TOPPLED 20131103002 PNR B200 3421 GYRO 1U149001 UNSERVICEABLE 20131103003 PNR B200 3421 GYRO 235010616 UNSERVICEABLE 20131103004 PNR B200 5610 WINDOW 1013840252 SHATTERED 20131103005 PNR B300 2220 VERTICAL SPEED INDICATOR 66011713104 UNSERVICEABLE 20131015005 ATL B300 2720 BEARING MS289135C CORRODED 20131022002 ATL B300 5341 FORWARD LOWER WING BOLTS 130909B175 TIME EXPIRED 20131217006 PNR B300 5730 WING SKIN 101120108XX CORRODED 20131029005 PAC B300C 2120 AIR CONDITIONING HOSE 30008721 CHAFING 20131009003 ATL B300C 5230 SWITCH MS250261 SERVICEABLE 20131212001 ATL C23 7322 CARBURETOR HEATER CRACKED 20131015003 QUE C90A 3020 BOLT ICE VANE ARM AN3H23A BROKEN 20131205002 ATL D18S 7120 ENGINE MOUNT CLUSTER CRACKED 20131108005 ONT BELL TEXTRON - CAN 206B 2140 BLOWER MOTOR UNSERVICEABLE 20131028003 PNR 206B 2435 STARTER 206062200 WORN 20131028004 PNR 206B 2913 HYDRAULIC PUMP 206076022 LEAKING 20131021021 PNR 206B 6420 PITCH HORN 206011809005 SCRAP 20131114002 QUE 206B 6420 TAIL ROTOR BLADE 2062200301 BEARING STAKED 20131114001 QUE 407 2140 JUNCTION BLOCK DT0608S BURNT 20131025006 ONT 407 6710 BEARING 206301051101 LOOSE (STAKING) 20131010011 QUE 407 6710 CLAMP 406001120107 FOWLING 20131210007 QUE 407 7920 OIL FLEX LINE 70037A090000 UNSERVICEABLE 20131129004 PAC 427 6320 LOWER CASE 427040200111 CRACK 20131031008 PAC 429 1000 SCREW 120225C08T08P NEW 20131025002 QUE 429 3160 DISPLAY UNIT 429375011107W CRACKED 20131218009 QUE 429 3420 AIR DATA/ATTITUDE/ HEADING REFERENCE SYSTEM 429075123103 MALFUNCTION 20131126012 QUE 429 5230 LOCK SET 20912205 MISSING 20131218005 QUE BELL TEXTRON - USA 205A 1 6210 MAIN ROTOR BLADE 204011250001 DELAMINATED 20131129010 ATL 205A 1 6410 TAIL ROTOR BLADE 212010750105 UNSERVICEABLE 20131009002 QUE 212 2435 STARTER/GENERATOR ASSEMBLY 23046020 WORN 20131025007 PAC 212 3210 FORWARD CROSS TUBE D212664101 USED 20131126008 PNR 212 6220 CENTREFRAME 204011307105 CRACKED 20131216016 PAC 412CF 2100 BOLT AN4H20 SHEARED 20131004007 QUE 412EP 6220 OUTBOARD CLEVIS 412018058105 CRACKED 20131118023 PAC BOEING 727 225 2897 RELAY KDAGX4F001 FAILED 20131202019 PAC 727 225 2910 MODULE HOUSING 651782114 STRIPPED 20131018009 ONT 727 227 2920 MODULAR PACK 65178213 FAILED 20131223011 PAC 727 23 5230 TUBE 65734111 SHEARED 20131115002 ONT 727 243 3020 INLET ANTI-ICE AIR TUBE 567620 CRACKED 20131120011 PAC 737 2R8C 5610 WINDOW ASSEMBLY 5717623095 CRACKED 20131004006 ONT 24 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN 737 6CT 7160 COWL ANTI-ICE 32156184 FAILED 20131216024 PNR 737 7CT 2210 PRESSURE SWITCH 211C223527 FAILED 20131126004 PNR 737 7CT 2530 COFFEE MAKER 64753001003 UNSERVICEABLE 20131010006 PNR 737 7CT 2751 FLAP POSITION TRANSMITTER 18173810 FAILED 20131224001 PNR 737 7CT 2751 FLAP POSITION TRANSMITTER 18173812 FAILED 20131120005 PNR 737 7CT 3020 VALVE COWL ANTI-ICE 32156184 FAILED 20131127002 PNR 737 7CT 3230 MANUAL EXTENSION SWITCH 002A001428 RE-RIGGED 20131120003 PNR 737 7CT 3442 WEATHER RADAR FAILED 20131015007 PNR 737 7CT 3610 PRECOOLER VALVE 32895625 FAILED 20131031002 PNR 737 7CT 3830 LAVATORY SYSTEM FAILED 20131120001 PNR 737 7CT 5610 R1 WINDOW 5893543150 SHATTERED 20131118014 PNR 737 800 5610 CAPTAIN`S #2 WINDOW PANE 58935587 UNSERVICEABLE 20131216017 PNR 737 8CT 2612 WHEEL WELL FIRE LOOP 0490010110D FAILED 20131007020 PNR 767 333 2312 VERY HIGH FREQUENCY COMMUNICATION TRANSCEIVER 8221047003 FAILED 20131021020 QUE 767 333 2530 LONG OVEN 8203170000 SMOKE 20131017001 QUE 767 333 2913 HYDRAULIC PUMP 3508806 FAILED 20131202011 QUE 767 375 2120 CABIN AIR SMELL NO FAULT FOUND 20131105008 QUE 767 375 2530 COFFEE MAKER FAILED 20131029007 QUE 767 38E 5420 FITTING ASSEMBLY-FAN COWL 311T21147 CRACKED 20131125012 QUE 777 333ER 2121 RECIRCULATION FAN 4100945A FAILED 20131007021 QUE 777 333ER 2530 GALLEY AREA CONTAMINATED 20131009009 QUE 777 333ER 2612 SMOKE WARNING INTERMITTENT 20131015002 QUE BOMBARDIER BD 100 1A10 1000 HARDWARE MIS-INSTALL 20131126002 PNR BD 100 1A10 2497 FUSE (F7) 106FU0180 FUSE OPEN 20131212006 QUE BD 100 1A10 2913 BRUSHLESS DIRECT CURRENT MOTOR 9452023 SHORTED 20131008010 QUE BD 100 1A10 3097 WINDSHIELD 1859013 MELTED 20131114006 QUE BD 100 1A10 3250 STEERING MANIFOLD 40750101 FAILED 20131127001 QUE BD 100 1A10 4900 AUXILIARY POWER UNIT 38007741 FAILED 20131112007 QUE BD 700 1A10 3150 INTEGRATED CIRCUIT-810 701730061010 UPGRADED 20131202016 QUE BD 700 1A10 3400 TRANSPONDER MODULE 7517400932 UPGRADED 20131129006 QUE BD 700 1A10 3400 TRANSPONDER MODULE 7517400932 UPGRADED 20131129007 QUE BD 700 1A10 3461 INTEGRATED CIRCUIT-810 701730061010 UPGRADED 20131114005 QUE CL600 2B19 (RJ100) 2130 CABIN PRESSURE SYSTEM FAILED 20131209010 QUE CL600 2B19 (RJ100) 2200 FLIGHT CONTROL PANEL FAILED 20131115004 QUE CL600 2B19 (RJ100) 2420 GENERATOR CONTROL UNIT 720846D FAILED 20131121004 QUE Feedback 1/2014 25 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN CL600 2B19 (RJ100) 2750 FLAP SYSTEM FAILED 20131218025 QUE CL600 2B19 (RJ100) 2752 FLAP ACTUATOR FAILED 20131209004 ATL CL600 2B19 (RJ100) 2752 FLAP ACTUATOR 854D100232425 FAILED 20131126006 ATL CL600 2B19 (RJ100) 2820 FUEL SHROUD CA282 CORRODED 20131011005 ATL CL600 2B19 (RJ100) 3140 FLIGHT CONTROL COMPUTER 6229815037 INOPERATIVE 20131010005 PAC CL600 2B19 (RJ100) 3220 NOSE LANDING GEAR TORQUE LINKS WORN 20131203004 QUE CL600 2B19 (RJ100) 3222 NOSE LANDING GEAR 16050115 FAILED 20131230002 ATL CL600 2B19 (RJ100) 3222 SHOCK STRUT 171008722105 DEFLATED 20131118027 QUE CL600 2B19 (RJ100) 3230 MAIN LANDING GEAR SELECTOR VALVE 750005000 FAILED 20131018003 QUE CL600 2B19 (RJ100) 5312 BULKHEAD FUSELAGE STATION 621 601R36008205 CRACKED 20131125011 QUE CL600 2B19 (RJ100) 5312 PRESSURE BULKHEAD 601R36008205 CRACKED 20131204003 QUE CL600 2B19 (RJ100) 5414 PYLON REAR ASSEMBLY 601371121016 DEPARTED 20131125006 QUE CL600 2B19 (RJ100) 5610 CO-PILOT SIDE WINDOW NP13932212 CRACKED 20131211007 ATL CL600 2B19 (RJ100) 5610 WINDSHIELD NP13932113 SHATTERED 20131125001 ATL CL600 2B19 (RJ100) 7110 EXHAUST NOZZLE PANEL DETACHED 20131101009 QUE CL600 2B19 (RJ100) 7600 THROTTLE CABLE ASSEMBLY 1603730007 FAILED 20131119006 QUE CL600 2B19 (RJ100) 7603 THROTTLE CABLE 1603730007 SEIZED 20131111013 QUE CL600 2B19 (RJ100) 7810 PANEL 22850181267 MISSING 20131008007 ATL CL600 2B19 (RJ100) 7830 PNEUMATIC DRIVE UNIT 1267587 FAILED 20131209008 QUE CL600 2C10 (RJ700) 2420 GENERATOR CONTROL UNIT 766283C FAILED 20131209005 QUE CL600 2C10 (RJ700) 2711 POWER SUPPLY PS644 FAILED 20131216018 QUE CL600 2C10 (RJ700) 2760 SPOILER SYSTEM FAULTED 20131022005 QUE CL600 2C10 (RJ700) 2780 SLAT SYSTEM FAILED 20131218024 QUE CL600 2C10 (RJ700) 2782 RIGHT-HAND #5 SLAT ACTUATOR 766385C FAILED 20131209012 QUE CL600 2C10 (RJ700) 3297 PROXIMITY SENSOR 895001FS BROKEN WIRE 20131216015 QUE 26 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN CL600 2C10 (RJ700) 5420 PYLON SEALANT INCORRECT 20131219013 QUE CL600 2D15 (705) 2460 CIRCUIT BREAKER MS220731 UNSERVICEABLE 20131028008 PNR CL600 2D15 (705) 2710 PULLEY 600908004 SEIZED 20131112010 ATL CL600 2D15 (705) 2742 HORIZONTAL STABILIZER TRIM ACTUATOR 84897 FAILED 20131128010 ATL CL600 2D15 (705) 2761 LOCKING DEVICE NAS1193E10C CRACKED 20131219012 ATL CL600 2D15 (705) 2820 FUEL COMPUTER 73811814 UNSERVICEABLE 20131216019 ATL CL600 2D15 (705) 2910 HYDRAULIC FLEX LINE AE71115275 LEAKING 20131031004 ATL CL600 2D15 (705) 3610 DUCT TELESCOPING GG670800143 FAILED 20131101008 PNR CL600 2D24 (RJ900) 3160 DISPLAY COOL FAN AE0804A04 FAILED 20131016004 QUE CL600 2D24 (RJ900) 5210 OUTER HANDLE ASSEMBLY 601R317621 SHEARED 20131219005 QUE CL600 2D24 (RJ900) 5220 OVERWING EMERGENCY DOORS SH67036600 CRACKED 20131125013 QUE CL600 2D24 (RJ900) 5610 TERMINAL BLOCK BURNT 20131120002 QUE CL600 2E25 (RJ1000) 2100 RIGHT-HAND AIR CYCLE MACHINE GG670950095 FAILED 20131216022 QUE CL600 2E25 (RJ1000) 7532 OPERATIONAL BLEED VALVE 5000728106 FAILED 20131216021 QUE CL600 2E25 (RJ1000) 8011 AIR TURBINE STARTER 35059534 FAILED 20131115003 QUE CANADAIR CL215 6B11(CL415) 2731 TRIM MOTOR 215900018 REPAIRED 20131015010 QUE CL215 6B11(CL415) 3213 SPHERICAL BEARING KSC253224V NEW 20131008002 QUE CL215 6B11(CL415) 5210 HINGE 21533027 CRACKED 20131007025 QUE CL600 2A12(601) 3210 SIDE STAY SPRING 860000065 BRISER 20131206001 QUE CL600 2B16(601 3A) 3244 TIRE 256K433 USED 20131121013 ONT CL600 2B16(601 3R) 3220 SENSOR BRACKET CSK6217 BENT 20131230006 ONT CL600 2B16(604) 3230 MAIN GEAR SELECTOR VALVE 750005000 FAILED 20131113007 QUE CL600 2B16(604) 3230 MAIN LANDING GEAR SELECTOR VALVE 750005000 FAIL 20131118016 QUE CESSNA 150M 2842 TRANSMITTER MC04265171 UNSERVICEABLE 20131111017 ONT 152 2810 STRAINER ASSEMBLY 422130 SEPARATED 20131118025 ONT 152 7322 ACCELERATOR PUMP MA3PA STIFF 20131104013 PAC 172M 2421 ALTERNATOR AL12F60 UNSERVICEABLE 20131111014 ONT 172M 2700 CONTROL TEE 5600144 CRACKED 20131023009 ONT 172M 3220 NOSE WHEEL ASSEMBLY C30174 BENT 20131114007 PNR 172M 3250 BOLT S21381 CRACKED 20131128002 ONT 172M 3250 BOLT S21381 CRACKED 20131128003 ONT 172M 6113 SPINNER BULKHEAD 5503214 CRACKED 20131018006 ONT 172M 6113 SPINNER FORWARD BULKHEAD 5503214 CRACKED 20131018010 ONT 172N 2730 ELEVATOR CABLE 510105391 FRAYED 20131003003 PNR Feedback 1/2014 27 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN 172N 3250 STEERING COLLAR 7430118 CRACKED 20131023008 ONT 172N 7322 CARBURETOR HEAT CONTROL S123017 FAILED 20131008013 PNR 172P 2752 FLAP MOTOR C3010020110 INTERMITTENT 20131111008 ONT 172R 2212 ALTITUDE ENCODER SSD12030A NUT 20131007017 PNR 172R 2420 ALTERNATOR CONTROL UNIT AC2101 FAILED 20131111001 ONT 172R 7322 FUEL SERVO 25765362 CRACKED 20131017007 PNR 172R 7334 TRANSDUCER P1655282 BOUNCING 20131111005 ONT 172S 2400 SOLENOID X610007 INTERMITTENT 20131018011 ONT 172S 2420 ALTERNATOR CONTROL UNIT AC2101 NO VOLTAGE 20131111002 ONT 172S 2842 TRANSMITTER S35941 ERRONEOUS 20131111018 ONT 172S 2842 TRANSMITTER FAULTY 20131111011 ONT 172S 6113 FORWARD SPINNER BULKHEAD 5522312 CRACKED 20131018007 ONT 172S 7714 TACH S33295 READING LOW 20131111003 ONT 182 5711 BLOCK-BEARING FUSELAGE 512122 CORROSION 20131219015 PAC 182J 3211 MAIN LANDING GEAR SUPPORT CASTING RIGHT-HAND 7416032 CRACKED 20131128009 ONT 182J 5743 MAIN LANDING GEAR SUPPORT CASTING LEFT-HAND 7416031 CRACKED 20131128008 ONT 182Q 2840 PRIMARY ENGINE INSTRUMENT EDM930 NEW 20131107010 PAC 182T 7713 ADAPTOR 02G22988 USED 20131129002 PNR 208 0 FITTING 26210092 CRACKED 20131113006 PNR 208B 2161 PRESSURE REGULATOR VALVE 1H1014 UNSERVICEABLE 20131112014 PNR 208B 2213 FLIGHT COMMAND INDICATOR 60001700 NOT RESPONDING 20131101010 PNR 208B 2213 INDICATOR 60001700 ERRATIC 20131118017 PNR 208B 2410 SPLINED COUPLING 26012663 CRACKED 20131126001 ONT 208B 2421 ALTERNATOR CONTROL UNIT 261850011RX STANDBY FAILED 20131118019 PNR 208B 2750 FLAP MOTOR CIRCUIT BREAKER MELTED 20131218008 ONT 208B 2752 ACTUATOR D14500463 GRINDING 20131102004 PNR 208B 2752 COUPLING C3010010211 UNSERVICEABLE 20131206002 PNR 208B 2822 FUEL PUMP 2C68 NOISY 20131118018 PNR 208B 3417 AIR DATA COMPUTER 110088210 UNSERVICEABLE 20131101005 PNR 208B 5270 DOOR 261705741 NOT LOCKED 20131223013 PNR 208B 7931 INDICATOR OIL PRESSURE 26060152RX UNSERVICEABLE 20131230003 PNR 401B 2397 CERAMIC CAPACITOR BURNT 20131209002 PNR 525 2913 HYDRAULIC PUMP 99123922 SEALS LEAKING 20131213007 PNR 525 5755 PRINT CIRCUIT BOARD ASSEMBLY 63183572 BURN 20131002006 QUE 525C 5755 PRINTED CIRCUIT BOARD 87189884 OVERHEATED 20131212004 ONT 550 2130 HOSE AD11341212 LOOSE 20131023005 ONT 560 2300 MANAGEMENT UNIT 7013270963 FREEZES 20131219010 PAC 28 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN 560 5210 LATCH ASSEMBLY 551124325 SERVICEABLE 20131129013 PNR 560 5510 RIB-CENTER 65320144 CRACKED 20131113009 PNR 560XL 2730 ELEVATOR HINGE BRACKET 663400359 CRACKED 20131010002 PNR 560XL 5520 ELEVATOR HINGE ASSEMBLY 663400359 CRACKED 20131002003 PNR 560XL 5520 HINGE BRACKET 633410110 CRACKED 20131120012 PNR A185F 2822 PUMP FUEL BOOST 41400017 UNSERVICEABLE 20131209014 PNR A185F 8530 HYDRAULIC LIFTER 658088 UNSERVICEABLE 20131218010 PAC T206H 2710 AILERON AND RUDDER CABLES 510303304 WORN 20131205005 PNR T206H 2823 FUEL SELECTOR 98511162 INTERNAL LEAKAGE 20131204004 ONT U206F 2421 ALTERNATOR AL12F60C UNSERVICEABLE 20131103001 PNR U206F 2424 SENSOR C5930010101 FAILED 20131118015 PNR CIRRUS SR20 6113 SPINNER BACKPLATE C22945P CRACKED 20131219014 ONT CONVAIR - CAN 340 3220 LEVER 24085571018 CRACKED 20131015004 PAC 340 5240 HOOK 34085103055 DAMAGED 20131104014 PAC DEHAVILLAND - CAN DHC 6 2750 BEARINGS STAKED 20131209009 PAC DHC 6 300 2720 RUDDER PEDAL C6CFM121028 CRACKED 20131112015 ATL DHC 6 300 2720 RUDDER PEDAL C6CFM12107 CRACKED BRACKET 20131119003 ATL DHC 6 300 2750 FLAP SELECTOR SKA1043A LEAKING 20131010001 ATL DHC 6 300 3220 TORQUE ARM UPPER 711025 CRACKED 20131209001 ATL DHC 7 102 2421 GENERATOR CONTROL UNIT U13866 FAILED 20131218012 PNR DHC 7 102 5610 WINDSCREEN 15380007 ARCHING 20131217009 PNR DHC 7 103 3220 NOSE LANDING GEAR 1610021 FAILED 20131218027 PNR DHC 7 103 3230 LOCK ACTUATOR (MAIN LANDING GEAR) 155507 FAILED 20131030005 PNR DHC 8 100 5755 FLIGHT SPOILER ACTUATOR A44700009 CRACKED HOUSING 20131008004 ONT DHC 8 102 1420 ELECTRICAL CONNECTORS OVERHEAT 20131213002 ATL DHC 8 102 2350 AUDIO CONTROL PANEL 506111 SHORTED LIGHTING 20131118022 ATL DHC 8 102 2421 WIRE DSC20189 CHAFED 20131022001 ATL DHC 8 102 2760 CASING FRACTURED 20131002002 ATL DHC 8 102 2761 SPOILER ACTUATOR A44700009 FRACTURED 20131126009 ATL DHC 8 102 2820 FUEL LINE 82820083003 CHAFED 20131001004 ATL DHC 8 102 2910 CASING FRACTURED 20131004005 ATL DHC 8 102 3200 MAIN LANDING GEAR DOOR HINGE ARM 85420015003 CHAFED 20131119002 ATL DHC 8 102 3200 MAIN LANDING GEAR DOOR HINGE ARM 85420015003 DEEP NICK 20131119001 ATL DHC 8 102 3210 BEARING ABY6925 SEIZED 20131108001 ATL DHC 8 102 3230 PULLEY 85410466001 SEIZED 20131011003 ATL DHC 8 102 3240 BRAKE CONTROL VALVE 53200 FAULTY 20131120008 ATL DHC 8 102 3242 BRAKE OVERHEATED 20131227003 ATL DHC 8 102 5755 SPOILER ACTUATOR A44700009 CRACKED 20131213004 ATL DHC 8 102 7312 FUEL HEATER 10839 LOOSE 20131016002 ONT Feedback 1/2014 29 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN DHC 8 102 7712 TORQUE SENSOR CONDITIONING UNIT 30005000046 INTERNAL FAILURE 20131009012 ATL DHC 8 106 3232 CYLINDER 82970015005 CRACKED 20131007027 PNR DHC 8 106 7261 GARLOC SEAL 311435001 CRACKED 20131112008 QUE DHC 8 311 2900 HYDRAULIC POWER SYSTEM NAS16126A BLOWN OUT 20131030004 ATL DHC 8 311 3230 SELECTOR VALVE 574205A FAILED 20131118021 ATL DHC 8 311 5522 SKIN 85520056011 CORRODED 20131023006 QUE DHC 8 311 5522 SKIN 85520056012 CORRODED 20131023007 QUE DHC 8 314 3220 PISTON CAP 88305 BROKEN 20131118024 PNR DHC 8 314 7530 BLEED CONTROL IMPROPERLY ASSEMBLED 20131126007 ONT DHC 8 400 3213 LEFT-HAND AXLE 461083 CORROSION 20131004003 ONT DHC 8 400 3213 RIGHT-HAND AXLE 461083 CORROSION 20131004004 ONT DHC 8 400 3250 STEERING MANIFOLD 481505 STEERING INOPERABLE 20131008005 ONT DHC 8 400 3260 PROXIMITY SENSOR 401020101 DAMAGED 20131017008 ONT DHC 8 400 5320 BAGGAGE DOOR UPPER SILL 85339453 CRACKED 20131213005 ONT DHC 8 400 5520 CRANK ARM 82760760 NEW 20131127003 PAC DHC 8 402 1420 ELECTRICAL CONNECTORS CDEL40067 OVERHEATED 20131009013 ATL DHC 8 402 1420 TERMINAL BLOCK 3706001 INTERMITTENT CONNECTION 20131030002 ONT DHC 8 402 2120 COMPRESSOR INLET DUCT 8209421 HOLE IN DUCT 20131106005 ATL DHC 8 402 2120 DUCT/BELLOWS 8215531 DAMAGED/HOLE 20131230004 ATL DHC 8 402 2497 WIRING SHORTED TO SHIELD 20131126013 ATL DHC 8 402 2721 RUDDER TRIM INDICATOR 8241060800901 UNSERVICEABLE 20131024002 ONT DHC 8 402 2913 ENGINE DRIVEN PUMP 6617303 PUNCTURED 20131107002 ONT DHC 8 402 2913 ENGINE DRIVEN PUMP 6617304 UNSERVICEABLE 20131022011 ONT DHC 8 402 2920 PRESSURE MANIFOLD 9451703 BROKEN 20131112017 ATL DHC 8 402 2930 LEVEL INDICATOR ASSEMBLY 882740107 LOOSE CABLE 20131219007 ATL DHC 8 402 3020 TIMER MONITOR UNIT 4100S01807 NEW 20131115005 PNR DHC 8 402 3040 COVER ASSEMBLY (ELECTRICAL) MS1802911S10 MELTED 20131031005 ONT DHC 8 402 3060 DEICE WIRE HARNESS 697071272 PINCHED 20131220004 ONT DHC 8 402 3234 LANDING GEAR SELECTOR 860TS09Y00 BURNT DIODES 20131129001 ATL DHC 8 402 3244 MAIN WHEEL TIRE 315731 FLAT TIRE 20131025005 ATL DHC 8 402 3246 WHEEL HALF OUTBOARD 3008641 CRACKED 20131111022 PNR DHC 8 402 3246 BEARING 29675 USED 20131220002 ONT DHC 8 402 3251 NOSE WHEEL STEERING MANIF 481509 NEW 20131122004 PNR DHC 8 402 3260 COVER NOSE LANDING GEAR WEIGHT ON WHEELS SENSOR 471423 CRACKED 20131008009 PNR DHC 8 402 3260 COVER NOSE LANDING GEAR WEIGHT ON WHEELS SENSOR 471423 UNSERVICEABLE 20131007018 PNR 30 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN DHC 8 402 3260 COVER WEIGHT ON WHEELS SENSOR 471423 BROKEN 20131009006 ATL DHC 8 402 3260 COVER WEIGHT ON WHEELS SENSOR 471423 BROKEN 20131009007 ATL DHC 8 402 3260 COVER WEIGHT ON WHEELS SENSOR 471423 BROKEN 20131009008 ATL DHC 8 402 3260 COVER NOSE LANDING GEAR WEIGHT ON WHEELS SENSOR 471423 TANGS MISSING 20131007023 PNR DHC 8 402 5210 COVER ASSEMBLY- FORWARD LATCH D191206501 NEW 20131120013 PNR DHC 8 402 5311 LONGERON/MACHINE FITTING 85360421109 GAP 20131002005 ONT DHC 8 402 7800 NOZZLE ASSEMBLY JET PIPE 87804124007 SEPERATION 20131003005 ONT DIAMOND - AS DA 42 3230 MAIN LANDING GEAR TIRE RETREAD 20131029003 ONT DA 42 3244 MAIN LANDING GEAR TIRE RETREAD 20131029006 ONT DIAMOND - CAN DA 20 C1 2410 ALTERNATOR PIVOT BOLT 2224120001 SHEARED 20131001001 ATL DA 20 C1 2823 FIREWALL SHUT-OFF 171N14 LEAKING 20131025003 ATL DA 20 C1 5514 BOLT AN311A CORRODED 20131205003 ATL DA 20 C1 5554 RUDDER MOUNT SUPPORT 2055450500 CRACKED 20131031003 ATL DA 20 C1 7310 FLEXIBLE FUEL HOSE AE366000B0084 FAILED/LEAKING 20131024007 PNR DA 20 C1 7430 IGNITION SWITCH 103572101 NOT WORKING 20131004009 ATL DA 20 C1 7600 ROD END HF3M SEIZED 20131217004 ATL DA 20 C1 7930 OIL PRESSURE GAUGE 2279301000 INACCURATE 20131004008 ATL DA 20 C1 7930 OIL PRESSURE GAUGE 2279301000 INACCURATE 20131230007 ATL DA 20 C1 7930 OIL PRESSURE GAUGE 2279301000 INACCURATE 20131125007 ATL DA 20 C1 7930 OIL PRESSURE GAUGE 2279301000 INACCURATE 20131125010 ATL DA 20 C1 7930 OIL PRESSURE GAUGE 2279301000 INACCURATE 20131203005 ATL DA 20 C1 7930 OIL PRESSURE INDICATOR 2279301000 UNDERREADING 20131104005 ATL DA 20 C1 7930 OIL PRESSURE INDICATOR 2279301000 UNDERREADING 20131106007 ATL DORNIER 328 300 3240 BRAKE UNIT AHA22276 ROTOR CLIP FAIL 20131102002 QUE DOUGLAS DC10 30F 3230 LANDING GEAR HANDLE STICKY 20131218026 PAC DC3C 2400 ELECTRICAL SYSTEM LOAD PROTECTION 20131213009 ONT EMBRAER ERJ 170 200 SU 2597 WIRE W2010532924 CHAFED 20131001005 ONT ERJ 170 200 SU 2720 TORQUE TUBE 17063448XXX CHAFED 20131125014 QUE ERJ 190 100 IGW 2120 AIR CONDITIONING SYSTEM SMELL 20131218021 QUE ERJ 190 100 IGW 2520 CIRCUIT BOARD CDSP4643501 OVERHEATED 20131007022 QUE Feedback 1/2014 31 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN ERJ 190 100 IGW 2530 OVEN FOREIGN OBJECT DAMAGE 20131030001 QUE ERJ 190 100 IGW 2710 BEARING MS2764829G CORRODED 20131205004 QUE ERJ 190 100 IGW 2750 SLAT/FLAP ACE CONTROL 1700064F FAILED 20131108003 QUE ERJ 190 100 IGW 2752 FLAP ACTUATOR C1558111 FAILED 20131111019 QUE ERJ 190 100 IGW 2780 SLAT SYSTEM FAILED 20131001009 QUE ERJ 190 100 IGW 2781 LEFT-HAND OUTBOARD SLAT SKEW SEN 1716280A FAILED 20131128007 QUE ERJ 190 100 IGW 2781 WING SLAT HARNESS W513 19019567401 FAILED 20131129008 QUE ERJ 190 100 IGW 2810 FUEL SYSTEM LEAK 20131220001 QUE ERJ 190 100 IGW 2820 FUEL FEED LINE CHAFED 20131106002 QUE ERJ 190 100 IGW 2820 FUEL FEED LINE 19004302403 CHAFED 20131106001 QUE ERJ 190 100 IGW 2820 FUEL LINE GROOVED 20131031006 QUE ERJ 190 100 IGW 2820 FUEL LINE GROOVED 20131031007 QUE ERJ 190 100 IGW 2820 PRESSURE VALVE FAILED 20131223004 QUE ERJ 190 100 IGW 2910 TUBE ASSEMBLY 19005172401 FAILED 20131108002 QUE ERJ 190 100 IGW 2913 ENGINE 1 DRIVEN PUMP 5116404 FAILED 20131217001 QUE ERJ 190 100 IGW 3140 CONTROL I/O MODULE 70265341902 FAILED 20131010003 QUE ERJ 190 100 IGW 3252 SHIMMY DAMPER NUT 22250070 LOOSE 20131125002 QUE ERJ 190 100 IGW 3610 DUCT ASSEMBLY DUCT 19006713405 CRACKED 20131125004 QUE ERJ 190 100 IGW 5220 OVERWING DOOR BAD CLOSURE 20131111021 QUE ERJ 190 100 IGW 5610 WINDSHIELD RIGHT-HAND NP18730112 SHATTERED 20131104001 QUE ERJ 190 100 IGW 7603 THROTTLE CONTROL QUADRANT 426000185 FAILED 20131010004 QUE EUROCOPTER DEUT BO105 S CDN BS 4 6230 MAST SHIELD 4638305009 TORN & SHREDDED 20131121008 ONT EC 135P2PLUS 6330 TRANSMISSION ARIS MOUNT L633M2010109 UNSERVICEABLE 20131024005 ONT EUROCOPTER FRANCE EC 130 B4 5610 LEFT-HAND WINDOW CEILING 350A25904021 CRACKED 20131218022 ONT EC 130 B4 5610 WINDSHIELD CENTER 350A25902500 CRACKED 20131205006 PAC FAIRCHILD SA227DC 2150 COOLING TURBINE 20475546 OVERHEATED 20131009011 ONT GULFSTREAM - ISRAEL GULFSTREAM 100 2782 SLAT FLEX DRIVE SHAFT 1116D10011 WORN 20131021023 ONT HAWKER SIDDELEY-UK HS 748 2A 2910 RIGHT-HAND MAIN GEAR JACK UPLINE 4Q2395 CHAFED 20131107008 ONT HUGHES 369D 1000 NUT AN3205 USED 20131119005 PAC LEARJET 35A 3230 LANDING GEAR CONTROL VALVE 48C48641 CRACKED 20131121012 ONT 36A 3246 MAIN WHEEL ASSEMBLY 95439914 FAILED 20131215001 ONT LOCKHEED 382G 5510 HORIZONTAL STABILIZER CORRODED 20131203001 PAC MITSUBISHI - USA MU 2B60 3097 WIRE P253A8 BARE WIRE 20131022007 PNR 32 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN MU 2B60 3220 RIGHT-HAND STRUT 030A393029 CRACKED 20131030006 ONT MORAVAN Z242L 2720 RUDDER CABLES Z14242260100 FRAYED 20131113001 ONT Z242L 7713 MANIFOLD PRESSURE ELBOW WORN 20131011009 ONT PILATUS - SW PC 12 45 2750 ARM ASSEMBLY FLAP DRIVE LEFT-HAND 5275212153 CRACKED 20131223010 ONT PC 12 45 2750 FLAP ARM 5275212153 CRACKED 20131223006 ONT PC 12 45 2750 FLAP ARM 5275212153 CRACKED 20131223007 ONT PC 12 45 2750 FLAP ARM 5275212153 CRACKED 20131223008 ONT PC 12 45 3418 ANGLE OF ATTACK TRANSMITTER 975442142 UNRESPONSIVE 20131104008 ONT PC 12 45 6197 CONNECTOR PLUG MS3116F84S WORN 20131205008 ONT PC 12 47E 3260 SWITCH PROXIMITY 9733033113 INTERMITTENT 20131125016 PAC PIPER PA15 X 3222 LOWER SHOCK STRUT 1180300 BROKE 20131028002 PNR PA28 140 1410 HOSE ASSEMBLY FUEL 6390115 DETERIORATED 20131118026 ONT PA28 161 2810 FUEL TANK FOREIGN OBJECT DAMAGE 20131111015 ONT PA31 2730 ELEVATOR CABLE 41942000 FRAYED 20131120009 PNR PA31 2750 FLAP 1202001 BURNT 20131021022 PNR PA31 7313 FUEL INJECTION SERVO 252416315 UNSERVICEABLE 20131120010 PNR PA31 350 2197 AIR CONTROL NIL WIRE BURN 20131011004 ATL PA31 350 2922 O`RING MS2877816 NEW 20131011002 QUE PA34 200T 3220 SPRING ASSEMBLY 6801400 BROKEN SHAFT 20131121009 PNR PA44 180 3020 CARBURETOR HEAT VALVE 87327003 BROKEN 20131025004 ATL PA44 180 3230 HYDRAULIC PUMP HYC5005 OVERHAULED 20131123001 ATL PA44 180 8520 CRANKCASE LW16818 CRACKED 20131227004 ATL ROBINSON R22 BETA 6520 TAIL ROTOR GEARBOX B0211 SERVICEABLE 20131025001 ONT R44 II 2435 STARTER 14924HTH INTERMITTENT 20131112012 PNR R44 II 2435 STARTER BC3151004 WORN 20131120007 PNR R44 II 2562 EMERGENCY LOCATOR TRANSMITTER BATTERY S182050601 LOW VOLTAGE 20131017003 PNR R44 II 2916 RESERVOIR D2112 VENTING 20131007016 PNR R44 II 2916 RESERVOIR D2112 VENTING 20131024003 PNR R44 II 6220 CLAMP LOOSE 20131216025 ONT R44 II 6510 BEARING D2242 UNSERVICEABLE 20131121005 PNR R44 II 7314 FUEL PUMP LW15473 LEAKING 20131031001 PNR R44 II 7322 GOVERNOR D2782 WORN 20131202018 PNR R44 II 7414 MAGNETO 1060064620 LEAKING 20131120006 PNR R66 6230 SWASHPLATE ASSEMBLY C0176 DAMAGED 20131022003 QUE SIKORSKY S76C 6320 OUTPUT HOUSING ASSEMBLY 7635109016041 CRACKED 20131212003 PAC S92A 0 FLAME DETECTOR 9231004802 WORN AND FRETTED 20131113003 ATL S92A 0 FLAME DETECTOR WIRING INTERMITTENT FAULT 20131113005 ATL VIKING CANADA DHC 6 400 3160 DISPLAY UNIT 66012020101 NEW 20131017012 PAC Feedback 1/2014 33 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN ENGINE ALLISON 250-C20B 7321 FUEL CONTROL UNIT 230706060 UNSERVICEABLE 20131112013 PAC AVCO LYCOMING IO-540-AE1A5 7414 BLOCK 10357426 BUSHING LOOSE 20131024004 PNR LTIO-540-J2BD 8520 CRANKCASE 11F20022D3 USED 20131219009 ONT LTIO-540-J2BD 8530 PLUNGER ASSEMBLY 78290 IN SERVICE 20131017013 QUE LTS-101-700D-2 7250 RIVET 414118206 LOOSE 20131101003 QUE O-235-L2CM 8550 FRONT SEAL LW13792 LEAKING 20131218023 PNR TIO-540-J2BD 8520 CRANKCASE 11F20022D3 USED 20131219008 ONT GARRETT TFE731-2-2B 7314 ENGINE FUEL PUMP 307085059 DAMAGED 20131230001 PAC TFE731-2-2B 8300 AFT GEARBOX CASE 30713213 CRACKED 20131210001 PAC TPE331-10UGR 7261 TUBE ASSEMBLY 31080711 SERVICEABLE 20131218020 ONT TPE331-11 8300 BEARING 31035851 FAILED 20131126010 ONT TPE331-11U-612G 7321 FUEL CONTROL UNIT 8978014 UNRESPONSIVE 20131211002 ONT TPE331-12UHR 7240 COMBUSTION PLENUM 310166812 CRACKED 20131202017 ONT GENERAL ELECTRIC CF34-10E5A1 7200 CENTER VENT TUBE FLATTENED 20131128004 QUE CF34-10E5A1 7230 ROTAR BLADE 2050M38P02 CRACKED 20131219006 QUE CF34-3B1 7200 COMPRESSOR DENTED 20131004001 ATL CF34-8C5 7170 DRAIN LINE CN6278035001 CHAFED 20131101002 ATL CF34-8C5 7230 OUTBOARD VERTICAL GYRO ACTUATOR 4120T02P03 SHEARED 20131216013 QUE CF34-8C5B1 7250 STUD 4125T20P01 FRACTURED 20131002001 PNR CT58-140-2 7261 FORWARD FRAME ACCESSORY DRIVE BEARING SUPPORT 37D400200P109 UNSERVICEABLE 20131022008 PAC PRATT & WHITNEY-CAN PT6A-114A 7250 SEGMENT 3035673 SHIFTED 20131113002 PNR PT6A-34 7230 COMPRESSOR TURBINE DISK 424934 CRACKED 20131219017 PAC PT6A-41 7310 FUEL LINE 3026779 NEW 20131125015 PNR PT6A-45A 1400 NUT-SPANNER MS9951XX VISUAL DEVIATION 20131128001 QUE PT6A-61 7321 FUEL CONTROL UNIT 8061310 UNSERVICEABLE 20131121014 PAC PT6A-67D 7250 DISC-TURBINE COMPRESSOR 305374001 LIFECYCLE EXCEED 20131213001 QUE PT6T-3D 7250 BEARING 310163501 WORN 20131104006 PAC PW120A 6120 PROPELLER CONTROLS OVERTORQUE 20131218018 ATL PW120A 7200 ENGINE OVERTORQUE 20131202010 ATL PW120A 7261 SEAL 311859701 LEAKING 20131111007 ATL PW120A 7261 TRANSFER TUBE 310541601 LEAKING 20131018004 ATL PW123 7200 ENGINE OVERTORQUE 20131218016 ATL PW545A 1220 ENGINE PW545A LEAKING OIL 20131023003 ONT PRATT & WHITNEY-USA JT8D-17 7250 VORTEX DISSIPATER TUBE 6577432216 FRACTURED 20131017005 ONT JT8D-9A 7500 6TH STAGE DUCT MANIFOLD 652245031 CRACKED 20131204007 PAC R-985-AN-14B 8530 EXHAUST SEAT 20786 EXCESSIVE WEAR 20131016001 PAC ROLLS ROYCE - GY BR700-710A2-20 7830 DOOR ACTUATOR P471A0001 ROD EYE BROKEN 20131213010 QUE 34 Feedback 1/2014 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN SPEY 7250 HIGH PRESSURE STAGE 1 TURBINE DISC JR30351 FIRTREE CRACKED 20131008008 QUE TAY 651-54 7200 INTERMEDIATE CASE JR34963A CORROSION 20131107001 ONT TELEDYNE CONTINENTAL IO-240-B 7322 THROTTLE BODY 653891A19 OVERHAULED 20131112009 ATL IO-240-B 7322 THROTTLE BODY 6538481A19 WORN LOOSE 20131106006 ATL IO-520-D 7414 ROTOR 1052948 CRACKED 20131025008 PAC IO-520-D 8530 CYLINDER ASSEMBLY AEC631397 CRACKED 20131104012 ONT IO-550-N 7921 OIL COOLER 8000440 NEW 20131008014 PNR IO-550-N 8520 BEARING 634503 CRACKED 20131218017 PNR TURBOMECA ARRIEL 2B 7310 ADJUSTED VALVE 2925807 OVERHAULED 20131210006 PNR ARRIEL 2B 7310 ADJUSTED VALVE 292950090 USED 20131210004 PNR ARRIEL 2B 7310 ADJUSTED VALVE ASSEMBLY 29258070 USED 20131210005 PNR ARRIEL 2B 7321 HYDRO MECHANICAL UNIT/FUEL CONTROL UNIT 292860750 USED 20131210003 PNR PROPELLER HARTZELL HC-E4A-3D 6120 PROPELLER CONTROLS A3074 WORN PAST LIMITS 20131121011 ONT MCCAULEY 4HFR34C652 6114 HUB 3A32C406 MACHINED 20131112016 ONT EQUIPMENT AIR TRACTOR 804321 2551 FORWARD HOPPER 804321 CRACKED 20131219018 PAC 2551 AFT HOPPER ASSEMBLY 804331 CRACKED 20131219019 PAC AIRFASCO MS210424 1000 NUT MS210424 CRACKED 20131024001 ONT ARTEX 4535002 2562 G-SWITCH UNSERVICEABLE 20131119004 PNR B/E AEROSPACE 11900311 2560 EMERGENCY EQUIPMENT 11900311 UNSERVICEABLE 20131017004 PNR 804331 51305631 2730 BRACKET 51305631 CRACKED 20131002007 ONT LW12892 8530 THRUST BUTTON LW12892 BROKEN 20131010009 ONT LW12892 8530 THRUST BUTTON LW12892 BROKEN 20131010010 ONT CHAMPION 4381 7414 DISTRIBUTOR GEAR M3008 DESTROYED 20131009010 PNR K3822 7414 BEARING OVERSIZED 20131210008 PAC DART AEROSPACE D350794121 2810 TANK ASSEMBLY D4464041 CRACKED 20131010008 ONT DEHAVILLAND - CAN DHC2 2721 TRIM CABLE C2CF1443 SEPARATED 20131004002 ONT EROS MC1015107 1410 HOSE 407460 OVERHAULED 20131203003 PNR GENERAL ELECTRIC A44700009 2761 MAIN HOUSING ASSEMBLY A447037 CRACKED 20131105009 NCR HARTZELL ENGINE TECH MHB4016R 8011 STARTER MHB4016R OVERHAULED 20131121002 ONT HONEYWELL Feedback 1/2014 35 Make/Model Jasc Part Name Part Number Part Condition SDR No. RGN 36150F2M 4900 AUXILIARY POWER UNIT 38005482 UNSERVICEABLE 20131126011 QUE 701730061010 3425 INTEGRATED CIRCUIT-810 701730061010 UPGRADED 20131029004 QUE PRATT & WHITNEY-CAN PT6A67B 7930 OIL TEMPERATURE SENSOR MS280341 INTERMITTENT 20131020001 ONT ROCKWELL COLLINS 8222332100 3160 ADAPTIVE FLIGHT DISPLAY-6520 8222332100 GOOD 20131106004 QUE AN410 1400 BOLT AN410 SHEARED 20131022004 ONT SIGMA 235010311 3421 CO-PILOTS ATTITUDE INDICATOR 235010311 REPAIRED 20131202014 PNR UNIVAIR U110325 2000 TAIL SPRING U-BOLT U110325 NEW 20131022006 PNR UNAPPROVED PART UNIVAIR U110325 2000 TAIL SPRING U-BOLT U110325 NEW 20131022006 PNR HEADQUARtERS Transport Canada (AARDG) Place de Ville, Tower C Ottawa, ON K1A 0N8 Tel: 1-800-305-2059 REGIoNAl oFFIcES Atlantic Transport Canada 95 Foundry St., 6th Floor Moncton, NB E1C 5H7 Tel: 1-800-305-2059 Prairie and Northern Transport Canada 344 Edmonton Street Winnipeg, MB R3C 0P6 Tel: 1-800-305-2059 Ontario Transport Canada 4900 Yonge St., Suite 400 Toronto, ON M2N 6A5 Tel: 1-800-305-2059 Quebec Transport Canada 700 Leigh Capreol Dorval, QC H4Y 1G7 Tel: 1-800-305-2059 Pacific Transport Canada 800 Burrard St., Suite 620 Vancouver, BC V6Z 2J8 Tel: 1-800-305-2059 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