N505XJ, cancelled Dec 12, 2007

Service difficulty reports · 40

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N505XJ' AND deregistration_id = 'N505XJ-2007-12-12'
  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 MALA050584Bushing · failedAFTER DEPARTING LT AND RT MAIN GEAR INDICATORS DID NOT INDICATE UP AND THE GEAR INTRANSIT LIGHT REMAINED ON. RT MAIN LIGHT WENT OUT WHEN SLOWED TO 190. REPLACED BUSHINGS ON THE LT AND RT LEVER ASSY AND SHIMED LT FWD UPPER DOOR HINGE MOUNT POINT FUNCTIONAL CHEJul 19, 2005 · N505XJ · Bac AVRO146RJ85A · Landing Gear SelectorSDR MALA050420Pump · malfunctionedCREW RETURNED TO MSP AFTER DEPARTURE FOLLOWING YELLOW HYDRAULIC SYSTEM HIGH TEMPERATURE. EMERGENCY TRUCKS WERE CALLED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND AC PUMP COMING ON LINE CAUSING YELLOW HYD HIGH TEMP NOTED DURING YELLOW SYS FLT CONT OPERAApr 26, 2005 · N505XJ · Bac AVRO146RJ85A · Hydraulic Pump (Electric/Engine), MainSDR MALA050225Downlock Switch · dirtyUPON INITIAL GEAR RETRACTION L GEAR RED UNSAFE LIGHT AND GEAR HANDLE IN TRANSIT LIGHT REMAINED ON. AFTER RECYCLING GEAR THE L GEAR LIGHT WENT OUT AND THE R GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE INTRANSIT LIGHT ON. AIRCRAFT ACCELERATED NORMALLY ON CLJan 26, 2005 · N505XJ · Bac AVRO146RJ85A · Landing Gear Position and WarningSDR MALA040864Strut · dischargedAFTER TAKEOFF THE GEAR WOULD NOT RETRACT, THE AUTO SPOILER AND AUTO THROTTLES DISCONNECTED. AIR RETURN TO DTW. MAINTENANCE UPON INSPECTION NOTED RT MLG STRUT FLAT. REPLACED RT SHOCK ABSORBER IAW TASK CARD 3210-503. PERFORMED LANDING GEAR FUNCTIONAL CHECKS Dec 13, 2004 · N505XJ · Bac AVRO146RJ85A · Main Landing Gear Strut/Axle/TruckSDR MALA040771Control Switch · damagedCREW STATED OUTFLOW VALVE WOULD NOT CLOSE. AIR RETURN TO MSP. MAINTENANCE FOUND OUTFLOW VALVE MODE SWITCH OUT OF DETENTS. REPOSITIONED SWITCH AS REQUIRED, PERFORMED CONTROLLER SELF TEST, ALL CHECKED GOOD. PERFORMED CONTROLLER FUNCTIONAL TEST AMM 21-30-00 Dec 6, 2004 · N505XJ · Bac AVRO146RJ85A · Pressure Regulator/Outflow ValveSDR MALA040608Slide · unsecureAFT RIGHT SLIDE NEEDS TO BE RESECURED. MAINTENANCE RESECURED SLIDE AS REQUIRED.Oct 1, 2004 · N505XJ · Bac AVRO146RJ85A · Escape SlideSDR MALA040589Battery Pack · dischargedBATTERY PACK 61-2275-1 SN/2715 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED AND PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/14/04. REFER TO WO NR 375413 FOR ADDITIONAL INFORMATION.Sep 8, 2004 · N505XJ · Bac AVRO146RJ85A · Emergency LightingSDR MALA040564Selector Valve · malfunctionedNOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION, GREEN LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED NLG RETRACT JACK P/N 104626002, S/N ON DH-0147-98, OFF DH-0082-96 AND LANDING SELECTOR VALVE P/N HTE9490-4, S/N ON FR022BC, OFF FSep 7, 2004 · N505XJ · Bac AVRO146RJ85A · Landing Gear SelectorSDR MALA040518Torque Shaft · inoperativeMAIN DOOR WILL NOT OPERATE NORMALLY. MAINTENANCE REMOVED L-1 LOWER HINGE COVER, INSPECTED DOOR LIFTING MECHANISM, FOUND TO BE NOT OPERATING NORMALLY. INSPECTED A/C AND FOUND TO BE SAFE FOR ONE TIME FERRY FLIGHT FROM DFW TO MSP. VERIFIED SHOOT BOLTS ENGAGED.Jul 17, 2004 · N505XJ · Bac AVRO146RJ85A · Passenger/Crew DoorsSDR MALA040169Bleed Band · malfunctionedDURING FLIGHT 3674/3411, NR 4 ENGINE TEMP 613 DEGREES, NG, 7 PERCENT BELOW OTHERS ENGINE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 4 ENGINE BLEED BAND REF EO A72023 FOR DETAILS (P/N 2-161-182-18) (S/N ON 03246371277) (P/N OFF 2-161-182-01) (S/NFeb 5, 2004 · N505XJ · Bac AVRO146RJ85A · Compressor Bleed ControlSDR MALA040168Bleed Band · malfunctionedON CLIMBOUT AND LEVEL OFF THE EGT ON NR 4 ENGINE WAS CONTROLLED TO MAX CONTINUOUS POWER WITH N1 7 PERCENT LOWER THAN OTHER ENGINES INDICATIONS WERE IDENTICAL WHEN FADEC WAS TURNED OFF. N2 WAS ALSO SHOWING 3 PERCENT HIGHER. AIR RETURN TO MSP. MAINTENANCE REMFeb 4, 2004 · N505XJ · Bac AVRO146RJ85A · Compressor Bleed ControlSDR MALA030339Sensor · malfunctionedDURING FLIGHT 3581 EN ROUTE TO OMA, NR 4 ENGINE DRIVE HIGH TEMP LIGHT ILLUMINATED ON SHORT FINAL, RAN QRH LIGHT REMAINED ON. MAINTENANCE REMOVED AND REPLACED NR 4 IDG ENGINE SENSOR SWITCH PER AMM 24-12-11. OPS AND LEAKS CHECKS GOOD.Jul 12, 2003 · N505XJ · Bac AVRO146RJ85A · AC Generation SystemSDR MALA030309Floor Support · corrodedDURING C-CHECK IN CVG, FORWARD CARGO BAY FLOOR SUPPORT ANGLES AT FRAME 21, FR 22, AND FR 23 WERE CORRODED BEYOND LIMITS AND REQUIRED REPLACEMENT PER SRM. REF 409 NR 127723, 24 AND 25 FOR DETAIL.Jun 7, 2003 · N505XJ · Bac AVRO146RJ85A · Fuselage Miscellaneous StructureSDR MALA030308Frame · damagedDURING C-CHECK INSPECTION IN CVG, VERTICAL STAB FRAME ASSEMBLY ITEM NR 1 (HC553314HO138-000) AT RIB 20 WAS DAMAGED DUE TO ITS AFT BUSHING WORN AND CAUSING THE FRAME ASSEMBLY TO DROP AND CHAFE ON RUDDER HINGE ASSEMBLY AT RIB 20. REPLACEMENT OF ITEM 1 & 2 (HC55Jun 7, 2003 · N505XJ · Bac AVRO146RJ85A · Vertical StabilizerSDR MALA030247Door · tornAIRCRAFT TO BE FERRIED FROM MSP TO CVG FOR REPAIRS TO THE ABOVE MENTIONED DAMAGES (LT MLG DOOR UPPER PANEL TORN AT UPPER AFT EDGE). NR 4 ENGINE LT AND RT ATTENUATED PANELS 7 SCREWS PULLED THROUGH AND FWD CARGO BAY FWD LT AND RT BULKHEADS DAMAGED A42BR AND 141Apr 14, 2003 · N505XJ · Bac AVRO146RJ85A · Landing Gear DoorsSDR MALA030196Proximity Sensor · failedDURING GEAR SELECTED UP ON FLIGHT 3411, LT GEAR UNSAFE LIGHT AND INTRANSIT LIGHT WOULD NOT EXTINGUISH ON RETRACTION. AIR RETURN TO MEM. MAINTENANCE REPLACED LT MAIN GEAR DOOR UPLOCK ACTUATOR PROXIMITY SWITCH. OPS CHECK GOOD IAW AMM 32-60-17. PN ON/OFF 8-01Mar 12, 2003 · N505XJ · Bac AVRO146RJ85A · Landing Gear Position and WarningSDR MALA030193Valve · malfunctionedDURING FLIGHT 3651, WHILE HOLDING AT 240 SO. OF STL LT OUTER DEICE VALVE C/B TRIPPED PART WAY THROUGH CYCLE. AIR RETURN TO MEM. MAINTENANCE SWAPPED VALVES P/N HTE250076-1 HH11 AND HH5 C/B MX3 AND F26 P/N MS3320-3. OPS CHECK GOOD. SWAPPED, PERFORMED IAW AMMFeb 23, 2003 · N505XJ · Bac AVRO146RJ85A · Airfoil Anti/De-ice SystemSDR MALA010628Skin · damagedDURING C-CHECK IN CVG, PERFORM REPAIR TO RT STAB LOWER SKIN IAW BAE RIC HC551H9052. MAINTENANCE REMOVED DAMAGE TO RT STAB LOWER SKIN; MANUFACTURED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR PARTS FOR RT STAB IAW BAE RIL HC551H9052; SRM'S 51-20-11, 51-42-0Jun 21, 2001 · N505XJ · Bac AVRO146RJ85A · Horizontal Stabilizer, Plate/SkinSDR MALA010617Skin · crackedDURING C-CHECK IN CVG, WHILE REMOVING LT I/B LEADING EDGE NOTICED CRACK ON INNER SKIN INBOARD SIDE APPROXIMATELY 13.8 INCH FROM EDGE AND APPROXIMATELY 1 INCH LONG. MAINTENANCE REPAIRED CRACK IN LT I/B LEADING EDGE IAW RICHC579H9114 PER BAE SYSTEMS.Jun 16, 2001 · N505XJ · Bac AVRO146RJ85A · Wing, Plate/SkinSDR MALA010627Line · brokenDURING C-CHECK IN CVG, WHILE STOWING OXYGEN MASK, FOUND LINE BROKEN AT CHECK VALVE AT SEAT 8 D/E/F. MAINTENANCE REPLACED MASK ASSEMBLY P/N 174085-43, AMM 35-20-31 AT SEAT 8 D/E/F.Jun 15, 2001 · N505XJ · Bac AVRO146RJ85A · Passenger Oxygen SystemSDR MALA010626Line · brokenDURING C-CHECK IN CVG, WHILE STOWING OXYGEN MASKS FOUND LINE BROKEN AT CHECK VALVE AT SEAT 2A/B. MAINTENANCE REPLACED MASK AND LINE ASSEMBLY P/N 174085-43 AT SEAT 2A/B IAW AMM 35-20-31.Jun 15, 2001 · N505XJ · Bac AVRO146RJ85A · Passenger Oxygen SystemSDR MALA010625Skin · damagedDURING C-CHECK IN CVG, REPAIR FUSELAGE SKIN DAMAGE AT FRAME 20, STRINGER 21. MAINTENANCE PERFORMED REPAIRS IAW BAE SRM 53-00-12/201.Jun 10, 2001 · N505XJ · Bac AVRO146RJ85A · Fuselage Main, Plate/SkinSDR MALA010624Skin · damagedDURING C-CHECK IN CVG, REPAIR FUSELAGE SKIN DAMAGE AT FRAME 20 AT STRINGER 18. MAINTENANCE PERFORMED REPAIRS IAW BAE SRM 53-00-12/201.Jun 10, 2001 · N505XJ · Bac AVRO146RJ85A · Fuselage Main, Plate/SkinSDR MALA010599Hand Rail · corrodedDURING C-CHECK IN CVG, MAINTENANCE FOUND CORROSION ON O/B AIRSTAIR RAIL. CORROSION IS ENTIRE LENGTH OF RAIL AND IS EXFOLIATING BEYOND SRM LIMITS 53-00-32 101. MAINTENANCE REPLACED O/B AIRSTAIR RAIL P/N C14647 IAW BAE SRM 53-00-32.Jun 6, 2001 · N505XJ · Bac AVRO146RJ85A · Entrance StairsSDR MALA010601Sill · corrodedDURING C-CHECK IN CVG, CORROSION FOUND ON AFT Z-MEMBER 0.012 INCH DEEP BEYOND LIMITS, LT AFT DOOR SILL PLATE AREA. MAINTENANCE REPLACED SILL PLATE P/N HC53850821-0024 IAW SRM 51-43-00 AND 51-23-00.Jun 5, 2001 · N505XJ · Bac AVRO146RJ85A · Fuselage Miscellaneous StructureSDR MALA010602Sill · crackedDURING C-CHECK IN CVG, FOUND CORROSION ON FWD Z-MEMBER 0.008 INCH DEEP, ALSO CRACKED 0.075 INCH LENGTH BEYOND LIMITS. LT AFT DOOR SILL PLATE AREA. MAINTENANCE REPLACED SILL PLATE P/N HC538J0821-002U IAW SRM 51-43-00, AND 51-23-00.Jun 3, 2001 · N505XJ · Bac AVRO146RJ85A · Fuselage Miscellaneous StructureSDR MALA010623Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 4 ENGINE NOSE COWL FWD BULKHEAD HAS FOUR STIFFENERS CRACKED (3, 19, 32, 33). MAINTENANCE REMOVED AND REPLACED 4 EACH 3, 9, 32, 33 STIFFENERS P/N HC716H9025-000 IAW SRM 54-10-11.May 31, 2001 · N505XJ · Bac AVRO146RJ85A · Engine Cowling SystemSDR MALA010622StiffenerFound during C-Check, #1 Engine nose Cowl Fwd Bulkhead has one stiffenrer cracked (32). Maintenance replaced #32 Stiffener PN HC716H9025-000, #1 Engine Nose Cowl IAW BAe SRM 54-10-11.May 31, 2001 · N505XJ · Bac AVRO146RJ85A · Nacelle/Pylon, Main FrameSDR MALA010621Stiffener · crackedDURING C-CHECK IN CVG, NR 2 COWL FWD BULKHEAD HAS ELEVEN CRACKED STIFFENERS, (3, 12, 13, 14, 16, 17, 19, 27, 28, 29, 32). MAINTENANCE REMOVED AND REPLACED 11 CRACKED STIFFENERS IN NR 2 NOSE COWL FWD BULKHEAD NR 3, 12, 13, 14, 16, 17, 19, 27, 28, 29, 32 WITH BMay 31, 2001 · N505XJ · Bac AVRO146RJ85A · Engine Cowling SystemSDR MALA010620Stiffener · crackedFOUND DURING C-CHECK IN CVG, NR 3 NOSE COWL HAS FWD BULKHEAD STIFFENERS CRACKED FIVE TOTAL (4, 6, 17, 22, 33). MAINTENANCE REMOVED STIFFENER'S 4, 6, 17, 22, 33, IAW SRM 54-10-11. FABRICATED STIFFENER'S 4, 6, 17, 22, 33 AND REPLACED STIFFENERS 4, 6, 17, 22, 3May 31, 2001 · N505XJ · Bac AVRO146RJ85A · Engine Cowling SystemSDR MALA010619EngineDuring C-Check in CVG, during Tailpipe removal for Inspection, noted crack in casing 1 1/2" Aft of 4th Turbine Wheel at 1 o'clock position. Dimensions 3.500 L. Maintenance removed Engine SN LF07643, Installed new Engine SN/LF07629 refer to Task Card 7100-502 May 31, 2001 · N505XJ · Bac AVRO146RJ85A · Engine Collector/Tailpipe/NozzleSDR MALA000776Pressure Switch · malfunctionedNR 2 ENGINE INTAKE LOW PRESSURE LIGHT ILLUMINATED E NROUTE TO STL. DUE TO ICE CONDITIONS TURNED BACK TO MEM AND SWAPPED INTO A/C 518. MAINTENANCE REPLACED INTAKE LOW PRESSURE SWITCH IAW AMM 30-21-14. (P/N HTE690041) (S/N ON FRTR096) IAW, (S/N OFF FRTR049AX)Dec 26, 2000 · N505XJ · Bac AVRO146RJ85A · Engine Pressure Ratio (EPR)SDR MALA000658Pickup · failedNR 4 ENGINE N1 GAUGE IS INOP, CREW REPORTED THE NR 4 ENGINE N1 GAUGE WAS READING ZERO OR DASHES. AIR TURNBACK TO MSP. MAINTENANCE INSTALLED NEW N1 PICKUP, P/N 2-313-053-01, S/N OFF 001936018265, S/N ON 001936019832, CHECED ALL CANNON PLUGS SECURE RAN ENGINE Nov 5, 2000 · N505XJ · Bac AVRO146RJ85A · Power Indicating SystemSDR MALA000340Strut · damagedCREW HAD TO USE GEAR OVERRIDE TO RETRACT LANDING GEAR. MX REPLACED RT STRUT (P/N 201106001), GEAR SWINGS GOOD.May 21, 2000 · N505XJ · Bac AVRO146RJ85A · Main Landing Gear Strut/Axle/TruckSDR MALA000244Lever · dirtyAFTER TAKEOFF GEAR LEVER COULD NOT BE RAISED UP. CREW USED MANUAL OVERRIDE TO SELECT GEAR UP. AUTOTHROTTLE BECAME INOPERATIVE, AND THE FLIGHT DIRECTORS DROPPED OFF LINE. CYCLED FD SWITCHES OFF THEN ON AND THEY CAME BACK. MX INSPECTED, NOTED RT GEAR FAULMar 29, 2000 · N505XJ · Bac AVRO146RJ85A · Landing Gear SelectorSDR MALA976632Indication · malfunctionedAFTER TAKEOFF MAIN CABIN DOOR AND GALLEY SERVICE DOOR BECAME DISARMED. RETURNED TO RDU. MAINTENANCE PERFROMED OPS TEST ON CABIN DOOR AND GALLEY SERVICE DOOR IAW 52-11-00. FOUND NO DEFECT WITH DOOR RIGGING ON DOORS. PASSED ALL OPERATION CHECKS. NO DISCREPANov 7, 1999 · N505XJ · Bac AVRO146RJ85A · Door Warning SystemSDR MALA976290Actuator · iced upLEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS SELECTED UP. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND LEFT WHEEL WELL WITH LARGE ICE ACCUMALATION AROUND GEAR DOOR UPLOCK ACTUATOR. REMOVED ICE AND CLEANED CANNON PLUGS, ALL CHECKS GOOD.Jan 9, 1999 · N505XJ · Bac AVRO146RJ85A · Landing Gear Retraction/Extension SystemSDR MALA976205Irs Syst · trippedWHEN FLAPS WERE RETRACTED AFTER TAKE OFF FTC AND EL TRIM ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE CYCLED AVIONICS MASTER SWITCHES, ALIGNED IRS SYSTEM AND TESTED EL TRIM SYSTEM AND FLAPS, ALL SYSTEMS CHECK OK.Oct 4, 1998 · N505XJ · Bac AVRO146RJ85A · Attitude and Direction Data SystemSDR MALA976145Light · brokenDURING INSPECTION, EMERGENCY LIGHT SOCKET BROKE AT ROW 2 ON THE OVERHEAD PANEL. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 2, ALL CHECKS GOOD.Jun 17, 1998 · N505XJ · Bac AVRO146RJ85A · Emergency LightingSDR MALA975643Actuator · failedFLT 3523 - DURING CRUISE FLIGHT, THE NR 4 ENGINE WAS RUNNING HOT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED BLEED BOND ACTUATOR. OPS CHECK GOOD. (X)Sep 11, 1997 · N505XJ · Bac AVRO146RJ85A · Compressor Bleed Control
Back to N505XJ, cancelled Dec 12, 2007