Boeing 747-200

Service difficulty reports · 651

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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 aircraft_model_key = '747200'
  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 L0FR200400011Wheel · crackedFAILED BOLT HOLES ON OUTER RIM IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 EDDY CURRENT PROCEDURES.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400010Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400007Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400002Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR20040004Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400003Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400009Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400008Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400001Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREANov 17, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR WRNA200400016Nut · missingAFTER TAKEOFF, CREW HEARD LOUD NOISE. DISCOVERED OVERHEAD EMERGENCY EXIT HATCH LEAKING EXCESSIVELY. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE FOUND NUT MISSING FROM EMERGENCY ESCAPE HATCH LATCH HANDLE AND BOLT LOOSE. REINSTALLED BOLT AND NUT IAW B7Nov 14, 2004 · N524UP · Boeing 747200 · Emergency ExitsSDR UPS04443461Splice · crackedINSPECTION TYPE: C, NWW BS 400 STR R44 RIGHT AFT CORNER INTERNAL CIRCUMFERENTIAL SKIN SPLICE FOUND CRACK APPROX .25 INCH LONG RUNNING AFT. THE CRACKED SPLICE REMOVED FOR STOP HOLE DRILLED. THE STOP CONFIRMED NIL CRACK BEYOND THE STOP HOLE. THE AREA REPAIREDNov 2, 2004 · N521UP · Boeing 747200 · Fuselage Main, BulkheadSDR UPS04443502Fitting · corrodedINSPECTION TYPE:C, RT BS 1241 WING REAR SPAR UPPER SPLICE PLATE AREA HOLE NR 5 FOUND CORROSION APPROX 0.040 INCH AT UPPER SPLICE FITTING. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD UW656931.Nov 1, 2004 · N521UP · Boeing 747200 · Wing, Attach FittingsSDR UPS04443488Frame · crackedINSPECTION TYPE: C, U/D-BS 500 RIGHT FRAME WEB DOUBLER (AFT FACE) FOUND CRACKED. STR-R11 BS 500 RIGHT FRAME AT STR 11 CRACKED REPAIRED PER HX RS R53-10-35214, ALL CRACK STOPPED AT THE STOP HOLES, CONFIRMED BY NDT.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443485Frame · crackedINSPECTION TYPE:C U/D- BS 360 LEFT FRAME WEB DOUBLER FOUND CRACKED AT STR L10A (AFT FACE). U/D BS 360 LEFT FRAME WEB DOUBLER REPLACE PER HX NRC 5613 FOR THE SUBJECT FRAME WEB REPLACEMENT DETAIL. REF HX RS R53-15-35211 AND UPS EO B747-5310-21306-A.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443479Support Fitting · crackedINSPECTION TYPE: C, U/D- BS 420 RIGHT FRAME STR 6 STOP SUPPORT FITTING FOUND CRACKED AS MARKED. STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS04443470Seat Track · corrodedINSPECTION TYPE:C U/D - BS 480-520 RBL 44 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO M-5100-2780-E.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS04443469Seat Track · crackedINSPECTION TYPE: C, U/D - BS 498 RBL 44 SEAT TRACK CRACKED. CRACKED SEAT TRACK REPAIRED PER SRM 53-10-05 FROM BS 480-520.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS04443467Frame · crackedINSPECTION TYPE: C, U/D - BS 460 LT FRAME O/B CHORD FOUND CRACKED BETWEEN STR-12A & STR-13. BS 460 LEFT O/B CHORD REPLACED PER SRM 51-10-01.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443466Seat Track · corrodedINSPECTION TYPE: C, U/D - BS 480-520 RBL 62 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 8 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPLIED IAW UPS EO M-510Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS04443447Stringer · crackedINSPECTION TYPE: C, U/D - BS 440-460 RIGHT STR-12 FWD END FOUND CRACKED & DEFORMED. CRACKED STRINGER REPLACED AT BS 440-460 RIGHT STR 12 PER SRM 51-10-01. P/N BAC1517-1551-2024T4.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS04443446Frame · crackedINSPECTION TYPE: C, U/D - BS 360 RT FRAME WEB FOUND CRACKED AT STR-2A. THE CRACK WAS PREVIOUS REPAIRED PER SRM 54-40-02 FIG 1. THE CRACK CONFIRMED NIL ADDITIONAL CRACK BEYOND THE FASTENER HOLES.Nov 1, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443475Floorbeam · crackedINSPECTION TYPE:C, U/D BS 330 RBL 61 FLOORBEAM UPPER CHORD FOUND CRACKED AS MARKED. U/D - BS 330 RBL 58 TO MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.Oct 31, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443501Skin · crackedINSPECTION TYPE:C, RT WING - CRACK FOUND ON RT WING UPPER SKIN AT BS 1241 UPPER SPLICE PLATE AREA AT HOLE NR 11 BY APPROX 0.040 INCH LONG RUNNING FWD. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD UW653051Oct 30, 2004 · N521UP · Boeing 747200 · Wing, Plate/SkinSDR UPS04443495Web · crackedINSPECTION TYPE: C, M/D- BS 440 BETWEEN STR 13AL AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51-10-01.Oct 30, 2004 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS04443483Doubler · crackedINSPECTION TYPE: C, M/D- BS 440 BELOW STR 13L FRAME ATT DOUBLER FOUND CRACKED. BS 440 FRAME DOUBLER REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A.Oct 30, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443465Frame · crackedINSPECTION TYPE: C, M/D - BS 400, S23-24R FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. FRAME SPLICE REPLACED PER SRM 51-10-01.Oct 30, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443445Frame · crackedINSPECTION TYPE: C, M/D - BS 460 BTN STR 13L AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51-10-01.Oct 30, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443444Splice · crackedINSPECTION TYPE:C M/D - BS 400, STR 23-24L, FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. BS 400 STR 23-24L FRAME SPLICE REPLACED PER SRM 51-10-01 PG 8.Oct 30, 2004 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS04443504Rib · crackedL/E PNL SUPPORT RIB FOUND CRACKED AT WS 1420 JUST O/B OF NR 1 L/E FLAP PDU. L/E PNL SUPPORT RIB REPAIRED AS PER HX RS NR R57-41-35209 JUST AT WS 1420 O/B OF NR 1 L/E FLAP PDU. REFER UPS EO NR B747-5740-21328-AOct 29, 2004 · N521UP · Boeing 747200 · Wing, Rib/BulkheadSDR UPS04443500Doubler · crackedINSPECTION TYPE: C, M/D- BS 460, BETWEEN STR 13-14L, FRAME DOUBLER FOUND CRACK. FRAME DOUBLER REPLACED PER SRM 51-10-01 PG 8.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443491Spar · crackedINSPECTION TYPE:C, RIGHT WING - MID SPAR UPPER CHORD FASTENER 2EA EDGE FOUND CRACK BETWEEN WS 440 - WS 460. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 440 - 460.Oct 29, 2004 · N521UP · Boeing 747200 · Wing SparSDR UPS04443490Spar · crackedINSPECTION TYPE: C, RIGHT WING - MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411.Oct 29, 2004 · N521UP · Boeing 747200 · Wing SparSDR UPS04443487Doubler · crackedINSPECTION TYPE:C M/D- LEFT BS 400 FRAME S15L DOUBLER CRACKED AT STR CUTOUT. DOUBLER REPAIRED AS PER HX RS R53-10-35210 AND UPS EO B747-5310-21303-A.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443486Frame · crackedINSPECTION TYPE: C, M/D- LEFT BS 360 FRAME & DOUBLER S24AL STR CUTOUT CRACKED. M/D- LEFT BS 360 FRAME & DOUBLER REPAIRED AS PER HX RS R53-12-35213 AND UPS EO B747-5310-21311-A.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443482Frame · crackedINSPECTION TYPE: C, M/D- BS 440, BELOW STR 31L, FRAME WEB FOUND CRACK. BS 440 STR 13L FRAME WEB SECTIONAL REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS04443481Spar · crackedINSPECTION TYPE: C, LT WING MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. LEFT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411.Oct 29, 2004 · N521UP · Boeing 747200 · Wing SparSDR UPS04443468Shear Angle · crackedINSPECTION TYPE: C, M/D - BS 440, APPROX STR 16L, FRAME ATT SHEAR ANGLE FOUND CRACK. CRACKED SHEAR ANGLE REPLACED PER SRM 51-10-01.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR UPS04443443Floorbeam · crackedINSPECTION TYPE: C, U/D BS 330, BET STR 13-14R, APPROX RBL 70-75 FLOORBEAM WEB FOUND CRACK. U/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443438Longeron · crackedINSPECTION TYPE: C, MAIN E/E COMPT LOWER FUSELAGE INTERIOR STRINGER FOUND CRACKED AT STA 440 TO STA 460 STR 37L. STA 440 TO STA 460 STR 37L REPAIRED AS PER SRM 53-10-03 FIG 3.Oct 29, 2004 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS04443489Floorbeam · crackedINSPECTION TYPE:C RIGHT BS 360 UPPER DECK FLOORBEAM ONE FASTENER HOLE CRACK FOUND AT FRAME WEB BS 360, WL 280 TO 320. BS 360 RT FRAME WEB CRACKED AREA REPAIRED PER HX RS R53-15-35211 BY CRACKED FRAME WEB DOUBLER REPLACED & FRAME WEB REINFORCEMENT PER THE HX ROct 28, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443484Floorbeam · crackedINSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM WEB AND FRAME WEB DOUBLER LAYER FOR DETAILS BS 360, WL 280 TO 320. LEFT BS 360 FLOORBEAM WEB & FRAME WEB CRACK REPAIRED AND FLOORBEAM WEB SECTIONAL REPLACED PEOct 28, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443480Floorbeam · crackedINSPECTION TYPE: C, RIGHT BS 340 UPPER DECK FLOORBEAM, ONE HOLE CRACK FOUND AT FRAME WEB. ONE HOLE CRACK FOUND AT FLOORBEAM WEB BS 340 WL 280 TO 320. RIGHT BS 340 UPPER DECK FLOORBEAM WEB & FRAME WEB REPAIRED AS PER HX RS R53-15-35211 AND UPS EO B747-5310-21Oct 28, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443460Floorbeam · crackedINSPECTION TYPE:C, LT BS 340 WL 280-320 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM UPPER CHORD AND STRAP LAYER. FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23 PLUS SB 747-53A2459 REV 1 PART 3 MODIFICATION.Oct 28, 2004 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS04443459Support · corrodedINSPECTION TYPE: C, FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1480 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 3 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. PANEL SUPOct 28, 2004 · N521UP · Boeing 747200 · Fuselage Main, KeelSDR UPS04443499Panel · crackedINSPECTION TYPE:C, LT WLG W/W FWD CANTED BULKHEAD LOWER AREA CRACKED AT STA 1241, LBL 94 AS MARKED (CLOSEOUT PANEL). CANTED BULKHEAD LT CLOSEOUT PANEL REPLACED AS PER UPS EO B747-5310-2758-E APPENDIX E.Oct 26, 2004 · N521UP · Boeing 747200 · Fuselage Main, StructureSDR ASAA0410435Skin · dentedOKC - AFT CARGO PIT DOOR EDGE DENTED A=1.0, Y=0.120, A/Y=8.3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.Oct 19, 2004 · N747AS · Boeing 747200 · Cargo/Baggage DoorsSDR UPS04443233Skin · crackedINSPECTION TYPE: AD, NR 2 PYLON UPPER LINK ATTACH LUG AREA, 1EA FASTENER HOLE CRACK FOUND ON NR 2ND LAYER, APPROX 0.060 INCH IN LENGTH, RUNNING O/B AS MARKED (BS 221 TO 221, WBL L470 TO L470). TEMPORARY REPAIR CARRIED OUT PER EO NR B747-5430-21111-A. STOP HOSep 28, 2004 · N523UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS04443235Skin · crackedINSPECTION TYPE:AD, NR 3 PYLON UNDER THE PREVIOUS REPAIRED CAP SKIN, CRACKED I/B OF UPPER LINK ATTACHMENT LUG AREA AS RED MARKED, NSTA 221 TO 221, WBL R470-R470. SKIN CRACK ENG STOP HOLE DRILLED, NDT CONFIRM CRACK FREE AS PER CUSTOMER INFO NR 3 PYLON WAS PREVSep 27, 2004 · N523UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS04443234Skin · crackedINSPECTION TYPE:AD, NR 2 PYLON UPPER LINK ATTACHMENT LUG AREA TOP SKIN 1 OFF CRACK FROM RIVET HOLE TOWARDS REAR AS RED MARKED (BS 221-221, WBL L470-L470). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. TSep 27, 2004 · N523UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS04443232Skin · crackedINSPECTION TYPE: AD, NR 1 PYLON UPPER LINK ATTACHMENT LUG AREA TOP 2ND LAYER SKIN CRACKED AS RED MARKED (BS 221, WBL L834 TO L834). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE.Sep 27, 2004 · N523UP · Boeing 747200 · Nacelle/Pylon, Plate/Skin
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