N489FE, cancelled Dec 18, 2013
Service difficulty reports · 163
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 = 'N489FE' AND deregistration_id = 'N489FE-2013-12-18' 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.
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 = 'N489FE' AND deregistration_id = 'N489FE-2013-12-18' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201212204343Unknown · smokeON SHUTDOWN OF APU DURING TAXI, ALL GB`S TRIPPED. WHILE RUNNING STABILIZERS AND QRH, NOTICED SMOKE ODOR IN COCKPIT. SUSPECTED PACK OVERHEAT. ACFT BEGAN TO ROLL DURING ATTEMPT TO START APU TO REGAIN POWER. APPLIED PNEUMATIC BRAKE TO STOP. ONCE POWER WAS BASDR FDEA201207252666Accessory Unit · malfunctionedAFTER T/O LANDING GEAR LEVER COULD NOT BE MOVED BEYOND THE "OFF" POSITION. COMPLIED WITH QRH. R & R THE LANDING GEAR ACCESSORY UNIT PER MM 32-09-121-4.PERFORMED OPS TEST REF MM 32-09-122-5. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.SDR FDEA201205261972Skin · dentedDENT IN SKIN AT BS 1129 S29L. CUT OUT DAMAGED AREA IAW SRM 53-30-3, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 1 AND SRM 53-30-2, FIG 2.SDR FDEA201205231941Skin · damagedSKIN DENTED AND GOUGED BS 1050 TO 1060 BETWEEN STRINGERS 26-28R. CUT OUT DAMAGED AREA IAW IAW SRM 53-30-3, FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-30-3, FIG 1 AND SRM 51-30-2.SDR FDEA201205221932Frame · crackedCRACK AT NR 1 CARGO DOOR AFT FRAME BS 620, S25R. CUT OUT DAMAGED AREA IAW SRM 51-40-3, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-2, FIG 3 AND SRM 51-40-2, FIG 1.SDR FDEA201205221927Web · dentedDENT ON LT AIRSTAIR TORQUE BOX WEB AT BS 1313. DENT OUT OF LIMITS IAW SRM 53-10-1, FIG 1. CUT OUT DAMAGED AREA IAW SRM 51-40-02, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, FIG 1.SDR FDEA201205221920Stringer · damagedON REMOVAL OF DAMAGED STRINGER 28L FOUND SKIN CORRODED AT BS 585. CUT OUT DAMAGED SKIN IAW SRM 51-10-1 AND EA 7-5330-143992. FABRICATED FILLER, STRUCTURAL FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3 AND EA 7-5330-143992. INSTALLED IAW SRM 51-30-2, 53-30-3 FIG SDR FDEA201205191887Frame · crackedSTATION 720 FRAME CRACKED AT SKIN ATTACH FASTENER HOLE BETWEEN STR 28L AND 27L. CUT OUT DAMAGED AREA IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991.SDR FDEA201205191886Stringer · corrodedCORROSION ON STRINGER 28L FROM BS 580 TO 600. CUT OUT CORRODED PORTION OF STRINGER IAW SRM 51-10-1. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2, REV 103.SDR FDEA201204111363Line · leakingTOTAL LOSS OF "A" SYS HYD QTY AND PRESSURE WHEN GEAR RETRACTED FOLLOWING TAKEOFF. ON POST FLIGHT DEBRIEF CREW REPORTED THAT WHEN THEY RETRACTED THE GEAR THEY LOST HYD FLUID AND PRESSURE AND THAT THEY HAD TO EXTEND THE GEAR MANUALLY. OPENED ACCESS PANEL 8505SDR FDEA201203231070Fitting · leakingNR 3 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS, CRUISING AT FL 330. NR 3 OIL QUANTITY STARTED TO DECREASE APPROX 1 QT PER 2 MINUTES. AT FIRST INDICATION OF SECONDARY CONFIRMATION COMPLETED SHUTDOWN CHECKLIST AND DIVERTED. SHUTDOWN TO LANDING WINDMILL 15 MINSDR FDEA201109203980Window · obstructedCAPT'S WINDOW WILL NOT OPEN. FOUND TRIM AROUND WINDOW IS NOT INSTALLED PROPERLY. TOO MUCH OF TRIM PROTRUDING ABOVE WINDOW CHANNEL THUS NOT ENOUGH CLEARANCE FOR WINDOW TO CLEAR PANEL. LOOSENED FASTENERS AROUND TRIM PANEL BELOW L-2 WINDOW. PANEL WILL NOTSDR FDEA201001290291Floorbeam · corrodedFLOORBEAM CORRODED AT BS 1130 RBL 30 TO RBL 46. CUT OUT DAMAGED AREA, FABRICATED 2 FLOORBEAM REPAIRS, 1 STRAP, 1 FILLER, 2 ANGLES, 1 STRAP AND 1 FILLER . HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A AND INSTALLED PARTS IAW 53-10-8 SDR FDEA201001290290Floorbeam · corrodedFLOORBEAM CORRODED STA 1070, RBL 5 TO RBL 10. CUT OUT DAMAGED AREA, FABRICATED 2 FILLERS, 2 REPAIR ANGLES AND INSTALLED IAW SRM 53-10-8, 51-10-2 AND 51-30-2.SDR FDEA201001270285Floorbeam · damagedDOUBLE DRILLED HOLES IN FLOORBEAM STA 1130 LBL 47. CUT OUT DAMAGE IN FLOORBEAM DIMS 1" X 1", FABRICATED NEW ANGLE, HEAT TREATED PART TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, FILLERS AND INSTALLED IAW SRM 51-30-2, 53-10-8, AND 51-SDR FDEA201001260269Skin · bentMAIN CARGO DOOR AFT EDGE AT STR 10 LT IS BENT OUT. TRIMMED OUT DAMAGED AREA, HFEC INSPECTED CUTOUT WITH NO DEFECTS NOTED IAW NDTM 51-00-00, HFEC INSPECTED HOLES WITH NO DEFECTS NOTED NDTM 51-00-00, FABRICATED DOUBLER, TRIPLER, FILLER AND INSTALLED IAW EA 7-SDR FDEA201001230268Skin · corrodedSURFACE CORROSION UNDER BASE OF NR 2 STATIC WICK ON RT HORIZ STAB OTBD T/E. REMOVED CORROSION AND FOUND OUT OF LIMITS AND CRACKED. TRIMMED OUT DAMAGE, FABRICATED DOUBLER PLATE, TWO FILLERS AND INSTALLED IAW SRM 51-30-2, 51-10-6, 55-20-3 AND 51-80-7.SDR FDEA201001230281Beam · damagedAFTER REMOVING MAIN CARGO DOOR FWD UPPER SILL, FOUND EXISTING OPEN HOLES WITH SHORT SPACING AT STA'S 480, 490, 500 AND 520. DAMAGE REPAIR DOCUMENTED.SDR FDEA201001220253Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 620 TO 640 STR 4L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.SDR FDEA201001220252Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 640 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.SDR FDEA201001220251Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 480 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.SDR FDEA201001220226Bulkhead · crackedRT W/W FWD BULKHEAD IS CRACKED BELOW APU LOAD CONTROL VALVE AT BS 870 RBL 18. REPAIRED RT WHEEL WELL BULKHEAD APU LOAD CONTROL VALVE AREA BS 870 RBL18 IAW SRM 53-10-9 FIG 5, REV 102.SDR FDEA201001220225Hinge · wornMAIN CARGO DOOR AFT HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTION USING 5212791 PO NR 79014501 DIMS 48 1/2" LONG FOR UPPER SECTION AND 20 1/4" LONG FOR LOWER SECTION AND INSTALLED IAW DWG B27-53-070 REV B.SDR FDEA201001220224Hinge · wornMAIN CARGO DOOR FWD HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTIONS AND INSTALLED IAW DWG B27-53-070 REV B.SDR FDEA201001210213Skin · damagedL-1 DOOR UPPER AND LOWER HINGE CUTOUT DOUBLERS HAVE COUNTERSUNK FASTENERS INSTALLED. REMOVED DOUBLERS, FABRICATED 2 NEW DOUBLERS, CADMIUM PLATED DOUBLERS IAW SOPM 20-40-01 AND INSTALLED IAW EO 7-5330-7-2345 PT 2 AND SRM 51-30-2.SDR FDEA201001210208Skin · crackedLT INBD AILERON LOWER SURFACE SKIN IS CRACKED AT FWD EDGE. SKIN CRACK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 4 1/2" X 5 1/8", FABRICATED DOUBLER, FILLER AND INSTALLED IAW SRM 57-50-1, 57-50-5, 51-10-1, AND 51-30-2.SDR FDEA201001200264Seat Track · corrodedSEAT TRACK CORRODED STA 970-990 RBL 24. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 144" AND SPLICE ANGLES USING BAC1503-100122 7178-T6511 PO NR 2912649 DIMS 1SDR FDEA201001190190Seat Track · corrodedCABIN SEAT TRACK BS 950 - 950, 10" LBL 24 OB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 91" AND INSTALLED IAW SRM 51-10-SDR FDEA201001190189Stringer · crackedAFT PIT STR 27L HAS CORROSION WITH EXFOLIATION AROUND FASTENERS BTWN BS 950D-950F. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED 3 EACH STRINGER SECTIONS, FABRICATED 3 FILLERS AND 4 EACH SPLICES. INSTALLED IAW SRM 51-10-6, 53-10-2, 53-10-3, AND 51-30-2.SDR FDEA201001190187Skin · corrodedFWD PIT - CORROSION ON SKIN AT BS 660 (AFT SIDE) BETWEEN STRINGERS 28R AND 29L. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 102. FABRICATED REPAIR DOUBLER, FABRICATED FILLER, INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2. FABRICATION IAW SRM 53-30-3, FIG.SDR FDEA201001190188Seat Track · corrodedCABIN SEAT TRACK BS 640 -660 LBL 56 IB FLANGE HAS SEVERAL SPOTS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED SEAT TRACK SUPPORT FLANGE. FABRICATED NEW SEAT TRACK SUPPORT FLANGE AND INSTALLED IAW SRM 51-30-2, 51-20-1 AND 51-10-2.SDR FDEA201001160267Floorbeam · corrodedFWD LAV AREA FLOORBEAM ANGLE IS CORRODED AT BS 310 LBL 20. TRIMMED DAMAGE. FABRICATED 2 REPAIR, FABRICATED FILLER, HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, AND INSTALLED IAW DWG SR27-53-017 REV A.SDR FDEA201001160223Stringer · corrodedCORROSION AROUND FASTENERS AT AFT PIT STA 1030 TO STA 1070 STRINGER 27L. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUTOUT STRINGER DAMAGE, FABRICATED FILLER USING BAC1498-145 7075T-6 PO NR 2905741 DIMS 19" AND SPLICES USING BAC1498-131 7075T-6 PO NR 2912086 DSDR FDEA201001160191Skin · crackedFUSELAGE SKIN LWR SIDE, HAS CRACK STA 720, STR 27R. REPAIRED IAW SRM 53-10-3 FIG 3 AND REPAIRED STRINGER 27R FWD PIT BETWEEN STA 700 TO 720 IAW SRM 53-10-3 FIG 1.SDR FDEA201001150192Seat Track · corrodedCABIN SEAT TRACK BS 950, 10" - 950A LBL 24 OB UPPER FLANGE HAS CORROSION AT FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION AND SPLICE ANGLES AND ONE PLATE. INSTALLED IAW SRM 51-10-6, 53-10-SDR FDEA201001150158Frame · bentCABIN FRAME BS 580 AT STRINGER 17 RT INSIDE FLANGE IS BENT IN. CUT OUT DAMAGED SECTION. FABRICATED FRAME DOUBLER REPAIR AND FILLER, HEAT TREATED MATERIAL TO T6 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A AND INSTALLED IAW SRM 51-40-3, 51-30-5, 51-SDR FDEA201001150182Seat Track · corrodedCABIN SEAT TRACK AT STA 720B LBL 45 OUTBD FLANGE UPPER SURF. HAS CORROSION. REMOVED SEAT TRACK SECTION LBL 45 BETWEEN STA 690 TO 740 AND 1EA SPLICER IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1 TREATED AND PRIMED IAW SRM 51-10-2, SDR FDEA201001150181Seat Track · corrodedCABIN SEAT TRACK AT STA 658 LBL 45 INBD FLANGE IS CORRODED. REMOVED SEAT TRACK SECTION BETWEEN STA 650 TO 690 LBL 45 AND 1EA SPLICER IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK AND FABRICATED 1 EA SPLICER 2 EA ANGLES , AND 1 EA STRAP IAW SRM 53-10-5SDR FDEA201001150156Seat Track · corrodedCABIN FLOOR TRACK B.S. 556 BL 0 LOWER SURF. HAS A CORROSION BULGE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION AT STA 480 TO 600 BL0 AND 2 EACH SERVICEABLE SPLICER SEAT TRACKS, LOCATED AND DRILLED NEW SEAT TRACK SECTION USING BAC152SDR FDEA201001150180Seat Track · corrodedCABIN SEAT TRACK AT STA 695 RBL 24 INBD FLANGE AND SPLICE CORRODED REMOVED SEAT TRACK SECTION BETWEEN STA 690 TO 740 RBL24 AND 1 EA SPLICER IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAE 1526-729-7178 T6 511 PO NR 9006020, DIM 172" LONG IAW SRM 5SDR FDEA201001150193Seat Track · corrodedCABIN SEAT TRACK BS 960-950A RBL 24 IB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND FABRICATED SPLICE FOR 2EA ANGLES AND 1EA STRAP IAW SRM 53-10-5 FIG1. TREATED AND PRIMED ISDR FDEA201001150186Keelbeam · crackedLT KEELBEAM CRACKED BS 872 BETWEEN FASTENERS. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER, CAD PLATED DOUBLER, HEAT TREATED DOUBLER AND INSTALLED IAW EA 7-5310-137782.SDR FDEA201001150160Stringer · crackedCABIN STRINGER 15 RT BS 720B PLUS 15" HAS END CRACKED AT FASTENER. REMOVED FASTENERS AND CUTOUT DAMAGED AREA, FABRICATED REPAIR "U" CHANNEL, FILLER AND FILLER TAPER. INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-2.SDR FDEA201001150159Stringer · crackedCABIN STRINGER 15 RT B.S. 720B PLUS 4" HAS END CRACKED AT FASTENER. REMOVED FASTENERS AND CUTOUT DAMAGED AREA, FABRICATED REPAIR "U" CHANNEL, FILLER AND FILLER TAPER . INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-2.SDR FDEA201001150179Seat Track · corrodedCABIN SEAT TRACK STA 680-690 RBL 24 FLANGE AND SPLICE CORRODED. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK AND SPLICER IAW SRM 53-10-2, INSTALLED NEW SEAT TRACK AND SPLICER IAW SRM 51-30-2.SDR FDEA201001150157Floorbeam · crackedFWD LAV AREA -FLOOR SUPPORT ANGLE IS CRACKED AT FASTENER HOLE, BS 312, BL 0. TRIMMED DAMAGE. FABRICATED 2 REPAIR ANGLES, FABRICATED FILLER, HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, AND INSTALLED IAW DWG SR27-53-017 REV A.SDR FDEA201001140194Floorbeam · corrodedCABIN FLOORBEAM BS 560 LBL 24- 45 UPPER FLANGE LOWER SURF HAS CORROSION AT N/P'S. REMOVED CORROSION IAW SRM 51-10-6, UT INSPECTED AREA IAW NDTM 51-00-00 FIG 3 PART 4, FOUND OUT OF LIMITS IAW PF SRM (ER 01-049) 53-10-1 FIG 4B REV C, REMOVED STIFFENER FSDR FDEA201001140127Structure · crackedLT INBD MID-FLAP T/E LOWER CHORD CRACKED WBL106. REMOVED CRACKED ANGLES AT WBL 106 AND 146, FABRICATED NEW ANGLES AND INSTALLED AT WBL 106 AND 146 IAW SRM 51-30-2, 51-40-4, 51-10-2 AND 51-10-1.SDR FDEA201001130174Sill · crackedMAIN CARGO DOOR UPPER SILL STA 495 STR 3L CRACK ORIGINATING FROM FASTENER. REMOVED FASTENER AND VERIFIED CRACK, REMOVED MAIN CARGO DOOR UPPER SILL AT STA 480 TO 530 AND ATTACHING SUPPORTS, LOCATED AND DRILLED NEW SILL AND INSTALLED NEW SILL AND ATTACHING SUPPSDR FDEA201001110079Angle · crackedRT OTBD MID-FLAP AFT UPPER CHORD ANGLE CRACKED WS 470. FLAP REMOVED AND REPLACED DUE TO DAMAGE BEYOND REPAIR LIMITS.
Back to N489FE, cancelled Dec 18, 2013