GE CF34-8C5

Service difficulty reports · 772

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF348C5'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2015060900570Engine · flamed outDURING CLIMB OUT AT 296KTS AT F190 LOUD BANG RT ENG FLAME OUT, VIB N2, FOLLOWED BY ENG OIL P-199, FOLLOWED CHECK LIST. R & R RT ENG IAW 900-72-430-902 & 900-72-430-906. REFER TO 527345 NON-ROUTINE WORK CARD. EMER WAS DECLARED, ACFT LANDED SAFELY WITHOUT INCJun 9, 2015 · N919XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA150611010Engine · failed(CAN) DURING CLIMB OUT AT 296 KTS AT FL 190 LOUD BANG, RT ENGINE FLAME OUT, VIB N2, FOLLOWED BY OIL PRESSURE, FOLLOWED CHECKLIST. AN EMERGENCY WAS DECLARED, ACFT LANDED SAFELY WITHOUT INCIDENT.Jun 9, 2015 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA150604019Control Panel · malfunctioned(CAN) ON 03-JUNE-2015, THE ACFT FLIGHT CREW REPORTED TO MAINTENANCE THAT WHILE ON-GROUND, DURING TAXI, AFTER AN UNEVENTFUL FLIGHT, THE YAW DAMPER NR 2 DISENGAGED AS INDICATED BY THE EICAS STATUS MESSAGE YD 2 INOPERATIVE. ATTEMPTS TO RE-ENGAGE THE YAW DAMPER NJun 3, 2015 · Cndair CL6002D24 · Autopilot SystemSDR CA150601005Shunt · misinstalled(CAN) MAIN BATTERY CB FOUND POPPED ON TAXI INTO GATE, NO EICAS MSGS, 1D1 MAIN BATTERY INOPERATIVE. WHILE MX WAS REPLACING SSPC K100 & PERFORMING THE OPERATIONS CHECK THEY FOUND NO CURRENT INDICATION FOR MAIN BATTERY. FOUND SHUNT SENSE WIRES, PN 8406-100, PREMay 30, 2015 · Bombdr CL6002D15 · Battery/Charger SystemSDR CA150605003Tire · out of round(CAN) FLIGHT CREW REJECTED TAKE OFF DUE TO EXTENSIVE NOSE WHEEL SHIMMY. NOSE GEAR INSPECTED FOR SHIMMY AS PER 05-51-28-220-801 AND 32-21-03 ALL GAPS WITHIN LIMITS. NOSE WHEELS FOUND OUT OF ROUND BOTH WHEELS REPLACED. THIS WAS DETERMINED WITH THE AIRCRAFT BEINGMay 30, 2015 · Cndair CL6002C10 · TireSDR REXA2015052300547Plate · wornTASK CARD 900-70-430-100 LT ENG LOWER TRANS COWL BLOW OFF DOOR HINGE & LATCH PLATE WORN. R & R LT ENG LOWER TRANS COWL BLOW OFF DOOR LATCH PLATE IAW SRM'S 51-40-11, 51-42-06 & 51-42-13. BLOW OUT DOOR HINGE REPAIRED ON JC 60023 & EA CRJ954-03459.May 23, 2015 · N913XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR CA150520006Hose · ruptured(CAN) DURING APPROACH, WHEN GEAR SELECTED DOWN, NO FLUID INDICATING IN NR 2, ALSO ASSOCIATED CAUTIONS AFTER TROUBLESHOOTING MAINTENANCE FOUND THE NR 2 EDP SUCTION LINE RUPTURED. REPLACED IAW AMM 29-11-01. ENGINE RUNS CARRIED OUT WITH NO LEAKS FOUND. AFH 295May 19, 2015 · Cndair CL600* · Hydraulic System, MainSDR SWIA201541178Engine · flamed outRT ENGINE FLAME OUT DUE TO LIGHTNING STRIKE ON APPROACH. INTERROGATED MDC AND NO FAULT FOUND RELATED TO ISSUE. RAN RT ENGINE AND NO FAULTS FOUND IAW FIM. RIGHT ENGINE OPS CHECK GOOD.May 15, 2015 · N805SK · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA150515002Contactor · burned(CAN) DURING THE CLIMB THE CREW RECEIVED AN AC BUS FAIL , CAUTION MSG ALONG WITH SEVERAL OTHER ASSOCIATED CAUTION MSGS. THE FLIGHT RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. TROUBLESHOOTING FOUND THE ADG LINE CONTACTOR K153 BURNT. THE ADG May 13, 2015 · Bombdr CL6002D15 · AC Power Distribution SystemSDR CA150511008Fitting · leaking(CAN) ON GEAR DOWN SELECTION FOR LANDING, CREW LOST ALL HYD QTY & PRESS ON THEIR NR 3 SYS. EXECUTED A GO-AROUND WITH GEAR DOWN & ACTIONED THEIR CHECKLIST. DECLARED AN EMER & LANDED SAFELY ON RUNWAY. AS THEY HAD NO STEERING, THEY WERE TOWED OFF THE RUNWAY TOMay 9, 2015 · Bombdr CL6002D15 · Landing Gear Steering SystemSDR CA150419001Controller · faulty(CAN) WITH POWER OFF AC FOUND THE, AC EXT, CB POPPED ON JB5. RESET BREAKER, BREAKER STILL POPS. NOTICED BUZZING FROM AFT EQUIPMENT BAY. FOUND THE APU BATTERY CAUSING CB TO POP. APU BATTERY REPLACED. CB RESET & SYS MONITORED. APU BATTERY CHARGER & ALL VOLApr 17, 2015 · Bombdr CL6002D15 · DC Power Distribution SystemSDR CA150419002Ecu · overheated(CAN) MX NOTICED AN ELECTRICAL ODOR IN AREA OF MAIN CABIN DOOR. FOUND ODOR TO BE COMING FROM E & E BAY. WHILE LOOKING FOR THE SOURCE OF SMELL, DROPPED POWER OFF OF THE ACFT & NOTICED CB CBP2-R1, FLAPS CONT CH 1, CB WAS POPPED. WITH POWER ON, ACFT COULD NOT Apr 17, 2015 · Bombdr CL6002D15 · Leading Edge Slat Control SystemSDR REXA2015040900395Rub Strip · chafedTASK CARD 900-54-430-301 LT NACELLE UPPER & LOWER FWD COWL TO CORE, COWL RUB STRIPS CHAFED. REPAIRED LT NACELLE UPPER & LOWER COWL RUB STRIPS IAW SRM 54-23-00-201-007-A01.Apr 9, 2015 · N909XJ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2015040800389Plate · wornTASK CARD 900-71-430-100 LT FWD COWL LOWER BLOW OUT DOOR HINGE & LATCH PLATE ARE WORN & THE UPPER BLOW OUT DOOR LATCH PLATE IS WORN. REMOVED LT LOWER & UPPER FWD COWL BLOW OUT DOOR LATCH PLATES IAW SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. INSTALLED Apr 8, 2015 · N909XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015040800390Block · wornTASK CARD 900-26-440-100 RT AFT CORE COWLING STANDOFF BLOCK TABS WORN. R & R RT AFT CORE COWL STANDOFF BLOCK IAW SRM 54-12-00-201-A01.Apr 8, 2015 · N909XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015040800391Channel · damagedTASK CARD 900-54-440-301 RT ENG TR ALIGNMENT PINS DAMAGED. FOUND STRUCTURE UNDER RT ENG ALIGNMENT PINS BENT & CRACKED. REMOVED OTBD EDGE CHANNEL IAW SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. INSTALLED NEW CHANNEL IAW SRM 51-42-06-001-001-A01 & 51-42-Apr 8, 2015 · N909XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2015032500368Bracket · chafedTASK CARD CRJ PANEL CARDS. LT CORE COWL STANDOFF BRACKET DOG EAR CHAFED. R & R LT CORE COWL STANDOFF BRACKET IAW SRM 54-13-00-201-002-A01 & 51-42-06-001-001-A01.Mar 25, 2015 · N908XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015032200333Valve · malfunctionedAT POWER UP FOR TAKEOFF, AFTER ABOUT 15 KTS LT TR UNSAFE CAUTION MSG CAME ON. ABORTED TAKEOFF AT 30 KTS EXITED RUNWAY, AT MX REQUEST ON TAXIWAY PUSH POWER UP TO 60%, NO MSG, THEN CYCLED TR WHEN LT TR WAS OFF, THE LT TR UNSAFE CAUTION MSG CAME ON AGAIN, THEN OMar 22, 2015 · N316PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR CA150317003Control Unit · failed(CAN) ACFT RETURNED TO GATE ON TAXI OUT AS THE RESULT OF FLIGHT CREW RECEIVED THE STEERING INOPERATIVE CAUTION MESSAGE. SEVERAL RESETS CARRIED OUT, HOWEVER, TO NO AVAIL AS MESSAGE RETURNED ABOUT 30 TO 40 SECONDS AFTER RESET.Mar 17, 2015 · Cndair CL600* · Landing Gear Steering SystemSDR CA150323012Wire · burned(CAN) DURING A HEAVY MAINTENANCE VISIT, A VISUAL INSPECTION FOUND THAT WIRE FBG8398-22 SHOWED SIGNS OF OVERHEATING. NO SIGN OF CHAFING. THIS WIRE WAS FOR THE AFT GALLEY 4 OPTION, HOWEVER, THAT IS NOT INSTALLED ON THIS ACFT. WIRE WAS REPAIRED.Mar 12, 2015 · Cndair CL600* · Electrical Power System WiringSDR REXA2015031100306Structure · damagedTASK CARD 900-54-430-301 LT FWD LOWER CORE COWL DAMAGED AROUND ACOC/VENT PANEL. MECHANIC REPAIRED DAMAGE TO FIRESHIELD AROUND ACOC/VENT PANEL IAW EO R54090. OP 60008.Mar 11, 2015 · N907XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2015031100307Structure · damagedTASK CARD 900-54-440-301, NUMEROUS DINGS, DENT, SCRATCHES, AND GOUGES INSIDE LOWER FWD RT ENGINE CORE COWL. MECHANIC, ALL DAMAGE FOUND TO BE WITHIN LIMITS IAW SRM 54-23-00-101-001-A01, EXCEPT FOR 1 DENT AND 1 CHAFE. DENT AND CHAFE REPAIRED IAW EA CRJ954-033Mar 11, 2015 · N907XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2015030800303Structure · chafedTASK CARD 900-26-430-100 LT ENGINE CORE COWL CHAFING AT PYLON SEAL AREA. MECHANIC REPAIRED LT ENGINE COWL CHAFING AT PYLON SEAL AREA IAW SRM 54-13-00-201-006-A01.Mar 8, 2015 · N907XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2015030800304Structure · chafedTASK CARD 900-78-430-100, RT ENGINE CORE COWL CHAFING AT PYLON SEAL AREA. MECHANIC BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR AS REQUIRED IAW SRM 54-13-00-201-006-A01.Mar 8, 2015 · N907XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR CA150305009Bulkhead · corroded(CAN) LEVEL TWO CORROSION FOUND ON THE LOWER SIDE OF THE LT & RT BULKHEAD AT FRAME 280 NEAR FLOOR LEVEL. LT REPAIRED IAW RJ9-5311-A15038 & THE PRINCIPALS OF REO690-53-11-722. RT REPAIRED IAW REO670-53-11-0594. AC HOURS 29676 AC CYCLES 15020.Mar 2, 2015 · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR CA150305010Crossbeam · corroded(CAN) LEVEL TWO CORROSION FOUND ON FRAME 280 CROSSBEAM. REPAIRED IAW REO670-53-11-579. AC HOURS 29676 WO CYCLES 15020.Mar 2, 2015 · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR CA150310012Wire Harness · failed(CAN) AIRCRAFT RECEIVED EICAS PROXIMITY SYS FAULT 1 MSG. GEAR & FLAP ICONS STAYED ON. DURING MX RECTIFICATION, THE RT NLG HARNESS WAS REPLACED & TESTED SERVICEABLE. AIRCRAFT HOURS 28768:34, CYCLES 14941.Feb 25, 2015 · Bombdr CL6002D15 · Landing Gear System WiringSDR REXA2015022000261Cowling · chafedNUMBER 1 ENG AFT CORE COWL SHOWS CHAFING AT PYLON INTERFACE AREA. REPAIRED NR 1 ENG AFT CORE COWL IAW SRM 54-13-00-201-006-A01 & NDT MANUAL 51-20-006-250-A01.Feb 20, 2015 · N906XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA150223004Switch · shorted(CAN) DURING SCHEDULED MAINTENANCE, WHEN THE AFT CARGO FIRE BOTTLE TEST BUTTON WAS DEPRESSED, BOTH AFT CARGO FIRE EXTINGUISHERS DISCHARGED. INVESTIGATION FOUND THE Ï¿½PUSH TO DISCHARGEÏ¿½ SWITCH ON THE CARGO FIRE PANEL WAS SHORTED INTERNALLY CAUSING THE BOTTLEFeb 20, 2015 · Cndair CL600* · Extinguishing SystemSDR CA150224027Actuator · binding(CAN) ON DEPARTURE IN THE CLIMB, THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAPS WERE SELECTED FROM 8 TO 1 DEGREES. THE FLAPS FAILED AT 8 DEGREES. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT AFTER BURNING OFF FUEL TO REACH THEIR MAX LANDING WEIFeb 20, 2015 · Cndair CL600* · Trailing Edge Flap ActuatorSDR REXA2015020700221Block · chafedTASK CARD 192 LT ENG CORE COWL ALIGNMENT BLOCK WORN, CHAFED AT 3 O' CLOCK. REPAIRED LT ENG CORE COWL ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01. REPAIRED CHAFE AT 3 O'CLOCK POSITION IAW SRM 54-13-00-201-005-A01.Feb 7, 2015 · N601LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2015020700222Bracket · brokenTASK CARD 192 RT ENG CORE COWL CHAFED AT OVERLAP, ALIGNMENT BRACKET BROKEN. REPAIRED RT ENG CORE COWL CHAFE IAW SRM 54-13-00-201-005-A01. REPAIRED ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01.Feb 7, 2015 · N601LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2015020400207Rub Strip · wornTASK CARD 900-54-430-301 LT ENG UPPER & LOWER FWD CORE COWLS AFT RUB STRIPS WORN. REPLACED LT ENG UPPER & LOWER WORN SECTION OF AFT RUB STRIPS IAW SRM 54-23-00-201-007-A01.Feb 3, 2015 · N601LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2015012400095Structure · chafedTASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL PYLON INTERFACE CHAFED & OTBD FWD FLANGE CHAFED. REPAIRED NR 2 ENG AFT CORE COWL AT PYLON INTERFACE IAW SRM 54-13-00-201-006-A01 STEP 6. REPAIRED NR 2 ENG AFT CORE COWL OTBD FWD FLANGE LE WITH A REMAINING THICKJan 24, 2015 · N600LR · Cndair CL6002D24 · Engine Cowling SystemSDR CA150126002Motor · inoperative(CAN) AFTER ARRIVAL THE MAIN CABIN DOOR (MCD) WOULD ONLY OPEN HALF OF THE WAY. THE PASSENGERS WERE DEPLANED VIA THE SERVICE DOOR. THE AIRCRAFT WAS FERRIED BACK TO A MAINTENANCE MAINTENANCE REPLACED THE MCD POWER ASSIST MOTOR.Jan 24, 2015 · Cndair CL600* · Passenger/Crew DoorsSDR CA150208001Sensor · failed(CAN) FLAPS HALF SPEED STATUS MESSAGE POSTED, ADVANCED DIAGNOSTICS SHOWED A RH OB SKEW SENSOR. A NEW SKEW SENSOR WAS INSTALLED TO CORRECT THE ISSUE. THE NEW UNIT PN: 5913164 SN: A3477 WAS INSTALLED AND RIGGED, DURING THE RIGGING PROCEDURE THE RESULTS WERE UNSAJan 23, 2015 · Cndair CL6002D24 · Trailing Flap Position Indicating SystemSDR CA150915008Hinge · damaged(CAN) IN PRODUCTION, IT WAS DISCOVERED THAT IT WAS DIFFICULT TO MANIPULATE THE LOWER RELEASE PIN OF FLIGHT DECK DOOR DUE TO INTERFERENCE BETWEEN THE FLIGHT DECK DOOR HINGE PAN HEAD SCREWS AND THE FLIGHT DECK DOOR HINGE FITTING WHEN THE DOOR IS IN CLOSED POSITIJan 14, 2015 · Cndair CL6002D24 · Fuselage, Door HingeSDR CA150112001Sleeve · cracked(CAN) DURING ROUTINE MAINTENANCE INSPECTION OF THE LH MLG ASSEMBLY THE LOWER TORQUE LINK ANTI-ROTATION SLEEVE PN 49230-1 WAS FOUND CRACKED. THE ANTI-ROTATION SLEEVE TO BE REPLACED AS PER THE APPLICABLE APPROVED REFERENCE. AC HOURS: 28969 AC CYCLES:14941.Jan 12, 2015 · Cndair CL6002D24 · Main Landing Gear Strut/Axle/TruckSDR REXA2015011000039Hinge Fitting · damagedTASK CARD 900-71-440-100 RT ENG LOWER FWD CORE COWL BLOW OUT DOOR UPPER HINGE ARM DAMAGED & LATCH STRIKER PLATE CHAFED. R & R RT ENG LOWER FWD CORE COWL BLOW OUT DOOR UPPER HINGE ARM & LATCH STRIKER PLATE IAW SRM 51-40-11-001-001-A01, 51-42-10-001-001-A01, 51Jan 10, 2015 · N905XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015011000040Plate · damagedTASK CARD 900-71-440-100 RT ENG UPPER FWD CORE COWL BLOW OUT DOOR UPPER HINGE ARM DAMAGED & LATCH STRIKER PLATE CHAFED. CLEANED LATCH ARM IAW SRM 51-26-00-001-001-A01 NO DAMAGE NOTED. R & R LATCH REINFORCING PLATE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-0Jan 10, 2015 · N905XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015011000041Hinge Fitting · damagedTASK CARD LT ENG FWD LOWER CORE COWL BLOW OUT DOOR LOWER HINGE ARM DAMAGED & STRIKE PLATE CHAFED. R & R HINGE ARM LEVER IAW AMM 71-12-05-000-801-A01 & 71-12-05-400-801-A01. R & R LATCH REINFORCING STRIKER PLATE IAW SRM 51-42-06-001-001-A01 & 51-42-10-001-001Jan 10, 2015 · N905XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015011000042Hinge Fitting · damagedTASK CARD 900-71-430-100 LT ENG FWD UPPER CORE COWL BLOW OUT DOOR LOWER HINGE ARM DAMAGED & LATCH STRIKE PLATE CHAFED. CLEANED HINGE ARM IAW SRM 51-26-00-001-001-A01 NO DAMAGE NOTED. R & R LATCH REINFORCING PLATE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-00Jan 10, 2015 · N905XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA150107007Connector · shorted(CAN) FIRE SYS FAULT CAUTION MESSAGE DISPLAYED AT THE GATE. RESET OK BUT CAME BACK ON WITHIN MINUTES. MAINTENANCE TROUBLESHOOTING AS FOLLOWS. CONTINUITY CHECK FOR LOOP B CARRIED OUT AT FIDEEX CANNON PLUG WITH NO FAULTS FOUND. FOUND 26VDC AT PIN 10, 11 CONNECTJan 6, 2015 · Cndair CL600* · Fire Protection System WiringSDR MASA2015010112831Engine · flamed outLEFT ENGINE FLAMED OUT ON GROUND.Jan 1, 2015 · N243LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2014123101242Compressor · stalledDURING DECENT, EXPERIENCED LT ENGINE COMPRESSOR STALL, CREW DECLARED EMERGENCY. MAINT IS TROUBLESHOOTING. ADDITIONAL INFORMATION TO BE PROVIDED. AT 23000 FT THE LEFT ENGINE STARTED POPPING AND LOSING POWER BUT WOULD INSTANTLY COME BACK. THE ITT WOULD STDec 31, 2014 · N903XJ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA141231001Bulkhead Web · corroded(CAN) AFT SIDE OF LT FLIGHT DECK BULKHEAD AT FS 280 CORRODED AT FLOOR LEVEL. REPORTED AS LEVEL 2 CORROSION. BULKHEAD WEB REPAIRED IAW REO 690-53-11-00722.Dec 31, 2014 · Cndair CL600* · Fuselage Main, BulkheadSDR CA150106011Engine · power loss(CAN) ON TAKE OFF ROLL , A/C WAS AT 81%, RIGHT ENGINE ROLLED BACK APPROX 5-8%. SPEED ABOUT 70 KNOTS. LOW SPEED, ABORTED TAKE OFF AND RETURNED TO GATE. MAINTENANCE REPLACED NR 2 ENGINE.Dec 28, 2014 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2014122001225Hinge · wornLOWER BLOWOUT DOOR HAS WORN HINGE AND LATCH PLATE. MECH REPAIRED LT LWR COWL HINGE BODY IAW EA. R & R LEVER ARM IAW SRM 51-41-02-001-001-A01. R & R LATCH PLATE IAW SRM 51-42-10-001-001-A01, FIG 51-42-10-991-804 AND SRM 51-42-06-001-001-A01.Dec 20, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2014121901223Pan · chafedLT ENGINE VENT PAN IS CHAFED LOWER COWL. MECH REPAIRED LT ENGINE VENT PAN IAW EO R54090.Dec 19, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR CA141222003Door · damaged(CAN) DURING DESCENT THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THERE WERE NO SYSTEM MALFUNCTIONS REPORTED. THE ENROUTE LIGHTNING STRIKE INSPECTION WAS CARRIED OUT IAW AMM AND THE AIRCRAFT RETURNED TO A MAINTENANCE BASE. AT THE MAINTENANCE BASE THE DETAILED LIDec 19, 2014 · Cndair CL6002D24 · Landing Gear Doors
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