N39081, cancelled Jan 17, 2003
Service difficulty reports · 87
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 = 'N39081' AND deregistration_id = 'N39081-2003-01-17' 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 = 'N39081' AND deregistration_id = 'N39081-2003-01-17' 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 CALA0100826Restrictor Valve · failedTHE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM NRT. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETURNED TO NRT WHERE IT LANDED WITHOUT INCIDENT. THE LT MLG RETRACT CYLINDER WAS REMOVED AND REPLACED, BUT THE PROBLEM REMAINED. MAINTENANCE SDR CALA0100457Bottle · dischargedDOOR R-4 WAS HARD TO OPERATE. THE R-4 DOOR N2 BOTTLE WAS RESERVICED IAW MM 52-12-16.SDR CALA0001692Duct · blownTHE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING TAKEOFF FROM IAH. THE NR 1 NACELLE TEMP WENT TO 300 DEGREES AND THE NR 1 THRUST REVERSER VALVE OPEN LIGHT CAME ON. POWER WAS REDUCED TO JUST ABOVE IDLE AND THE FIRE WARNING LIGHT EXTINGUISHED. FUESDR CALA0001407Spar Cap · corrodedINSPECTION FOUND CORROSION ON CENTER WING FORWARD LOWER SPAR CAP AT XCW 0.0. THE SPAR CAP WAS REPAIRED IAW ECRA 5311-01104 AND FLS DRAWING 90-53-1071.SDR CALA0001372Longeron · corrodedINSPECTION FOUND LONGERON 48L CORRODED AROUND FASTENERS IN CENTER CARGO BAY AT STA 1521. THE END CAP WAS REMOVED AND A NEW END CAP WAS INSTALLED IAW SRM 51-00-01.SDR CALA0001371Shear Tie · corrodedINSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1903 FROM L48R-49R, 50R-51R, AND 50L-52L. THE SHEAR CLIPS WERE REMOVED AND REPLACED IAW SRM 53-30-00.SDR CALA0001370Angle · corrodedINSPECTION FOUND STIFFENER ANGLES CORRODED AT FRAME STA 1997 ABOVE L49L TO L49R. THE STIFFENER ANGLES WERE REPLACED IAW SRM 51-00-01.SDR CALA0001369Shear Tie · corrodedINSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1941 L49R - 52L, STA 1959 L50L - L52L, AND STA 1975 L50L - L50R. THE SHEAR CLIPS WERE REPLACED IAW SRM 53-30-00, 53-00-01, AND 51-21-02.SDR CALA0001298Beam · corrodedINSPECTION FOUND G1A -G5 LT SUPPORT BEAM CORRODED AT STA 800. THE SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.SDR CALA0001286Beam · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM BENEATH LAV D CORRODED AT STA 836 - 880. THE INNER SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.SDR CALA0001285Beam · corrodedINSPECTION FOUND RT SUPPORT BEAM CORRODED AT STA 840. THE BEAM WAS REPLACED IAW SRM 53-70-00 AND GMM 10-900-01.SDR CALA0001284Floorbeam · corrodedINSPECTION FOUND O/B FLOORBEAM CORRODED AT GALLEY 2. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.SDR CALA0001283Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 392 ADJACENT TO R-1 DOOR. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.SDR CALA0001282Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT ADJACENT TO GALLEY G-1 CORRODED. REPAIRED IAW SRM 53-00-00 AND GMM 10-900-01.SDR CALA0001266Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 836 AND 804, X42 TO X-42. THE CORRODED SECTIONS OF FLOOR SUPPORT BEAM WERE REPLACED IAW GMM 10-900-01.SDR CALA0000572Engine · failedNUMBER ONE ENGINE FAILED (UNCONTAINED) AT TAKEOFF. ENGINE BEING REMOVED AND FORWARDED TO SHOP FOR FAILURE ANALYSIS. THIS SDR TO REMAIN OPEN PENDING TEARDOWN AND ANALYSIS.SDR CALA9901085Wire · damagedTHE EXIT IDENTIFIER AT LAV C FAILED TO ILLUMINATE. INSPECTION FOUND CABLES DAMAGED. THE CABLES WERE REPAIRED AND OPERATION CHECKED IAW MM 33-50-00.SDR CALA9901084Wire · chafedINSPECTION FOUND THE EMERGENCY PATH LIGHTING SYSTEM BATTERY POWER SUPPLY BLOWING FUSES AT L-3 DOOR. MAINTENANCE FOUND CHAFED WIRE AT SIDEWALL FORWARD OF LT OVERWING EXIT. REPAIRED IAW MM 20-00-00 AND OPERATION CHECKED GOOD IAW MM 33-50-00.SDR CALA9901083Charger · inopINSPECTION FOUND L-2 DOOR EMERGENCY LIGHTS BATTERY CHARGER UNIT BATTERY DISCONNECT PLUG CABLE BROKEN AT PLUG. THE CHARGER UNIT WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.SDR CALA9901082Skin · corrodedINSPECTION FOUND LT WING NR 8 SLAT CORRODED ON LEADING EDGE AT TRACK. THE NR 8 SLAT WAS REMOVED AND REPLACED IAW MM 27-80-01.SDR CALA9901079End Cap · corrodedINSPECTION FOUND FORWARD CARGO BAY STRINGER 44R END CAP CORRODED AT STA 889. THE END CAP WAS REPAIRED IAW SRM 53-30-00.SDR CALA9901071Floor · delaminatedINSPECTION FOUND FLOOR PANEL 283KF DELAMINATED WITH CORRODED FERRULES. A NEW FLOOR PANEL WAS INSTALLED IAW GMM 10-100-01.SDR CALA9901052Support · corrodedINSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1838-1873, X= 3R. THE CORRODED SECTION OF SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-100-01.SDR CALA9901051Support · corrodedINSPECTION FOUND THE LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1990-1996, X= 22R. REPAIRED IAW SRM 53-70-00, FIGURE 13 AND 14.SDR CALA9901050Support · corrodedINSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT Y= 1887, X= 3R TO 70R AND AT Y= 1887, X= 3L TO 70L, J CAPPING STRIP. THE CORRODED SECTIONS OF CAPPING STRIP WERE REMOVED. NEW SECTIONS OF CAPPING STRIP WERE INSTALLED IAW GMM 10-100-01.SDR CALA9801233Light · inoperativeINSPECTION FOUND EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED.SDR CALA9800387Filter Case · brokenTHE NR 3 HYDRAULIC SYSTEM LOST FLUID ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC SYSTEM ELEVATOR OFF LIGHT WHILE EN ROUTE FROM FCO TO EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO CDG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGISDR CALA9701791Actuator · inoperativeTHE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM LGW. APPROPRIATE CHECKLISTS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR ACTUATOR SLOW TO OPERATE AND THE GEAR CONTACTED THE OUTER DOOSDR CALA9701228Bulkhead · buckledINSPECTION FOUND TAIL CONE BULKHEAD AT FS 2163, STRINGER 51L BUCKLED. THE BUCKLED AREA WAS REMOVED AND A REPAIR WAS INSTALLED USING DOUBLER AND FILLER IAW SRM 53-00-1 FIGURE 4 SHEET 2.SDR CALA9701088Floor Panel · corrodedINSPECTION FOUND FLOOR PANELS 291AF, 291EF, 292BF, 292DF, 292EF, 293BF, 293CF, AND 293DF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-21-00, AND 53-60-00.SDR CALA9701087Floor Panel · corrodedINSPECTION FOUND FLOOR PANELS 241EF, 241FF, 242BF, 242FF, AND 261BF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.SDR CALA9701085Floorboard · corrodedINSPECTION FOUND FLOORBOARD PANEL 227AF CORRODED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-60-00.SDR CALA9701074Support · corrodedINSPECTION FOUND FLOOR SUPPORT AND MOUNT FITTING CORRODED AT STA 459 TO 501, RBL 14. THE MOUNT FITTING WAS REMOVED AND REPLACED IAW SRM 51-31-01. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 AND 53-00-01.SDR CALA9701075Skin · corrodedINSPECTION FOUND LT WING INBOARD FLAP CORRODED. THE LT INBOARD TRAILING EDGE FLAP SKIN WAS REMOVED AND NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 57-52-01.SDR CALA9701020Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 475, RBL 38. THE UPPER FLANGE OF FLOOR SUPPORT WAS TRIMMED OFF AND REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5310-03505.SDR CALA9701017Skin · dentedINSPECTION FOUND A DENT AND CREASE IN LT AFT FUSELAGE SKIN AT STA 1841 BETWEEN LONGERON 40L AND 41L. THE DENT AND CREASE WERE REWORKED IAW SRM 53-20-00, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-20-00 AND ECRA 5330-02532.SDR CALA9701016Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1501, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-21-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02524.SDR CALA9701084Web · elongated holesINSPECTION FOUND SEVERAL ELONGATED FASTENER HOLES IN NR 3 PYLON FRONT SPAR WEB. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW EA 5410-01109 AND SRM 51-30-00.SDR CALA9701082Angle · corrodedINSPECTION ATTACH CHANNEL CORRODED AT STA 595, LONGERON 45L. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-12-01.SDR CALA9701070Floor · crackedINSPECTION FOUND AN 8 INCH CRACK AT LIGHTENING HOLE OF FLOOR UNDER FLIGHT ENGINEER'S SEAT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-11-01 AND 51-31-01.SDR CALA9701069Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1901 TO 2007, LBL 57. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-31-01, AND 51-21-01.SDR CALA9701086Floor Panel · corrodedINSPECTION FOUND CABIN FLOOR PANELS 231CF, 232AF, 232CF, 233AF, AND 233CF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.SDR CALA9701081Angle · corrodedINSPECTION FOUND CENTER CARGO AFT BILGE FORWARD FRAME WEB SUMP PANEL ATTACH ANGLE CORRODED AT STA 1781, RBL 1 TO RBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-31-01, AND 53-15-01.SDR CALA9701073Skin · gougedINSPECTION FOUND RT FUSELAGE SKIN GOUGED AT STA 735, LONGERON 28R. THE GOUGED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-20-00.SDR CALA9701018Floor Panel · corrodedINSPECTION FOUND FLOOR PANEL CORRODED AT STA 840-899, RBL 72. THE PANEL WAS REMOVED AND REPLACED IAW SRM 53-00-01.SDR CALA9701083Web · crackedINSPECTION FOUND A 1.125 INCH CRACK AT CORNER ACCESS HOLE WEB FRAME STA 1256, LONGERON 27R. A 1 INCH CRACK WAS FOUND ON LT SIDE AS WELL, AT LONGERON 27L. THE CRACKS WERE STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, SDR CALA9701080Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, LBL 28 TO 33. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.SDR CALA9701076Frame · crackedINSPECTION FOUND A .075 INCH CRACK IN FRAME AT FORWARD LOWER CORNER OF ACCESS HOLE WEB, STA 1305, LONGERON 27L. A .5 INCH CRACK WAS FOUND ON THE RT SIDE AT LONGERON 27R. THE CRACKS WERE STOP DRILLED, DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-0SDR CALA9701071Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, RBL 4 TO 21. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-16-01.SDR CALA9701067Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 840 TO 899. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-13-01, 51-21-01, AND 51-30-01.
Back to N39081, cancelled Jan 17, 2003