Boeing 747-121
Service difficulty reports · 3,030
Newest first. General aviation reporting is voluntary.
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 = '747121' 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 aircraft_model_key = '747121' 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 UPS06448067Tension Tie · crackedINSPECTION TYPE:C M/D BS 900 LT SIDE TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT AFT TENSION TIE. CRACK THROUGH THICKNESS. M/D BS 900 LT SIDE TENSION TIE AFTER CHANNEL REPAIRED AS PER RS R53-25-35559. CONTINUE INSPECTION IS REQUIRED AS PER SDR UPS06448065Tension Tie · crackedRT BS 900 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT TENSION TIE AFT CHANNEL, CRACK LENGTH 0.030". BS 900 FRAME ATTACHED TENSION TIE RT AFT CHANNEL CRACKED HOLE OVERSIZED TO 0.278" BY INCREMENT AS PER EO B747-5310-23715 APP D AND BOLT INSTALLED AS SDR UPS06447905Plate · damagedINSPECTION TYPE-C, M/D LT BS 900 TENSION TIE FWD CHANNEL ATTACHED STAINLESS STEEL PLATE OVAL HOLE 1EA FOUND AT UPPER ROW COUNT FROM IB NR 4. M/D BS 900 LT TENSION TIE FWD CHANNEL ATTACHED STAINLESS STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND SDR UPS06447903Plate · damagedINSPECTION TYPE-C, M/D LT BS780 TENSION TIE FWD CHANNEL ATTACHED STANLESS STEEL PLATE 4EA HOLE OVAL AT OB AREA. M/D LT BS 780 TENSION TIE FWD CHANNEL ATTACHED STANLESS STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01PG9 AND EO B747-5310-23715 APPENDIX C.SDR UPS06447900Doubler · crackedINSPECTION TYPE-C M/D BS 820 LT SIDE TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT WEB DOUBLER. CRACK LENGTH 0.040 INCH. M/D BS820 LHS FRAME ATTACHED DOUBLER BETWEEN STR9L TO STR12L AREA REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.SDR UPS06447869Plate · damagedINSPECTION TYPE-C M/D BS860 RT TENSION TIE FWD CHANNEL 2EA HOLE OVAL AT S/STEEL PLATE OB UPR AND LWR FASTENER HOLE AREA. M/D BS860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 5246 FOR DSDR UPS06447857Plate · damagedLT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE TO FRAME CONNECTION 1 FASTENER HOLE OVAL AT LOWER (COUNT FROM O/B NR 5). LT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 5SDR UPS06448120Plate · damagedINSPECTION TYPE:C M/D BS860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B LOWER FASTENER HOLE AREA AND AT NR 12 COUNT FROM O/B UPPER ROW FASTENER HOLE. M/D BS 860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMSDR UPS06448105Plate · damagedBS 940 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B LOWER FASTENER HOLE AREA. BS 940 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35491. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35SDR UPS06448070Plate · damagedINSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPR FASTENER HOLE AREA. M/D BS 820 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35562. CONTINUE INSPECTION IS REQUIRESDR UPS06448066Plate · damagedBS 900 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER 1 HOLE AND LOWER I/B 2 HOLE AREA. BS 900 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35559. CONTINUE INSSDR UPS06447980Floorbeam · corrodedFWD CARGO COMPT RT STA600 RBL44-45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.041" BY 1" BY 1" EXCEED SRM LIMIT. FWD CARGO COMPT BS 600 FLOORBEAM UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST BETWEEN RSDR UPS06447621Battery · dischargedINSPECTION TYPE:N/A CREW ENTRY DOOR EMERGENCY LIGHT FWD (UPPER SILL) DIM. R&R EMERGENCY LIGHT BATT ASSY PER MM 33-51-07, OPS CK GOOD.SDR UPS06447493Skin · corrodedFUSE SKIN JUST RT OF AFT GALLEY DRAIN MAST PILLOWED. *S/D* REMOVED DE-ACT'D DRAIN MAST DAMAGE. FAB'D DOUBLER & FILLERS PER SRM 53-30-03. OK TO INSTALL REPAIR. COMPLETED DOUBLER & FILLERS INSTALLATION PER SRM 53-30-03. GALLEY DRAIN MAST DELETED PER EO B74SDR EIA2006158Firewall · crackedFOUND CRACK AT BS 265 AND FWD APU FIREWALL, RT VERTICAL CHORD COMMON TO FUSELAGE AT STRINGER 12. CARRIED OUT REPAIR PER MM 51-00-00 FIG 15 AND 17 AND BOEING MSG NR 1-207158630-5 (3 JUL 06).SDR EIA2006157Pressure Panel · crackedNWW PRESSURE PAN AT 400 BL 0, FOUND CRACK AT LOWER CUTOUT. TIME LIMITED REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 82. DOUBLER USED 2024-T3 0.080 PRESSURE PAN MUST BE REPLACED BEFORE 3000 FLT CYCLES CAT A. NW WELL PRESSURE PAN AT STA 400 BL 0 FOUND CRACKED AT SDR EIA2006156Cover · crackedNR 5 RT DOOR EMERGENCY EXIT LIGHT IDENTIFIER COVER FOUND CRACKED. REPLACED COVER, OPS CHECK GOOD IAW 33-51-00.SDR EIA2006155Skin · corrodedFUSELAGE SKIN AT LOWER BELLY STA 1660 TO 1680 STRINGER 49L FOUND CORROSION. REPAIR CARRIED OUT IAW BOEING MSG NR 1-203976535-5 (DATED 36 JUN 06) 2 OFF DOUBLER'S 2024-T3 0.090 FABRICATED DIMENSION 17 BY 13 & 16 BY 12 CAT A REPAIR.SDR EIA2006154Skin · dentedFUSELAGE SKIN DENTED 1.5 AND 1.5" CENTERED ON FASTENER HEAD LOCATED BETWEEN STA 160 AND 180 APPROX 11 O'CLOCK. DENTED SKIN REPAIRED IAW B747 SRM 53-30-03 FIG 1. DOUBLER USED 2024-T3 0.050, DIMENSION12 BY 8 CAT A REPAIR.SDR EIA2006153Seat Track · crackedRT OUTBD MOST TRACK AT STA 480 FOUND CRACKED AT VERTICAL FLANGE. REPAIR CARRIED OUT IAW B747 SRM 53-10-05 FIG 5, TRACK MADE FROM EXTRUSION 63B10047-389 AND REPAIR ANGLES AND 10134-1203, 7075-T6511.SDR EIA2006152Seat Track · corrodedFOUND AT RBL 76 STA 540 SEAT TRACK WITH CORROSION. SEAT TRACK REPAIRED IAW B747 SRM 53-10-05 FIG 1A, TRACK MADE FROM 63B10047-370 AND REPAIR ANGLES FROM BAC 1503-100147, 7075-T6511.SDR EIA2006151Pressure Panel · crackedSTA 400 NOSE WHEEL WELL TORQUE BOX PRESSURE PAN (FOR NLG RETRACT ACT) FOUND CRACKED AT INBD LOWER CORNER AND UPPER OUTBD CORNER. REF SRM 53-11-20 FIG 12 SHT 12 ITEM 60. CRACKED PRESSURE PAN (3 PARTS) FABRICATED BY WORKSHOP AND INSTALLED IAW B747 SRM 51-10-01SDR EIA2006150Web · crackedAFT CARGO STA 1480 APU DUCT CUT-OUT FOUND CRACK AT LT SIDE, APPROX 2" CRACK AT 1 O'CLOCK. CRACKED WEB REPAIRED IAW SB 747-53-2309 REV 1.SDR EIA2006148Frame · crackedMAIN DECK FRAME AT BS 1760 FOUND CRACK BETWEEN S-12 AND S-13R 0.5" LONG. REPAIRED IAW B747 SRM 53-10-04 FIG 87, DOUBLER USED 7075-T6 0.063.SDR EIA2006147Support Fitting · crackedSEAT TRACK RBL 75.0 SUPPORT FITTING AT STA 1000 FOUND CRACK. CRACK SUPPORT FITTING FABRICATED BY WORKSHOP AND INSTALLED IAW B747 SRM 51-10-01 PG 9 (FAB ORDER NR 222,17208).SDR EIA2006146Frame · crackedUPPER DECK TENSION TIE LT SIDE STA 840 FOUND 1 OF THE FASTENER HOLES WITH CRACKS ON FRAME, DOUBLER AND AFT CHANNEL. FRAME AND DOUBLER REPAIRED IAW B747 SRM 53-10-04, FIG 52. CRACKED AFT CHANNEL REPAIRED IAW B747 SRM 51-40-03 FIG 3 DOUBLER USED 7075-T6 0.063,SDR EIA2006145Frame · crackedFRAME LOWER LEG AT AFT CARGO STA 1560 BETWEEN STR 41L TO 42L FOUND CRACK AND CORROSION. REPAIRED IAW B747 SRM 53-10-04 FIG 4, REPAIR ANGLE USED 7075-T6 0.063.SDR EIA2006144Frame · crackedFOUND FUSELAGE LOWER LEG AT STA 1580 STRINGER 41L TO 42 L CRACK. CRACKED FRAME REPAIRED IAW B747 SRM 53-10-04 FIG 04 REPAIR ANGLE USED 7075-T6 0.063.SDR EIA2006143Frame · crackedFUSELAGE FRAME LOWER LEG AT STA 1540 STRINGER 41 L TO 42 L FOUND CRACKED. REPAIRED IAW B747 SRM 53-10-04 FIG 4 REPAIR ANGLE USED 7075-T6 0.063.SDR EIA2006142Frame · crackedFUSELAGE FRAME WEB AT AFT CARGO STA 1600 STRINGER 44L FOUND PUNCTURED AND CRACKED. REPAIR IAW B747 SRM 53-10-04 FIG 71, DOUBLER USED 7075-T5 0.040.SDR EIA2006141Frame · crackedAFT CARGO STA 1500 LEFT, FOUND FRAME CRACK AT STRINGER 36 LEFT CUT OUT. CRACKED FRAME REPAIRED IAW B747 SRM 53-10-04 FIG 4, REPAIR ANGLE USED 7075-T60.063.SDR EIA2006139Skin · dentedNR 2 R MED EXTERIOR SKIN LOWER CENTER AREA FOUND 2 DENTS. BOTH DENTS REPLACES IAW SRM 52-00-03 FIG 3 2024-T3 0.07 REPAIR DOUBLERS USED. PERMANENT REPAIR CAT A.SDR EIA2006138Skin · dentedFUSELAGE SKIN AT STA 1960-1970 STRINGER 45L FOUND DENTED. REPAIR IAW B747 SRM 53-30-03 FIG 1. DOUBLER USED 2024-T3 0.071, DIMENSION 11 BY 8 1/2" CAT A REPAIR.SDR EIA2006137Skin · unknownFUSELAGE EXTERIOR SKIN AT BS 1600-1620 S-17LT-S-18LT. REPAIRED IAW B747 SRM 53-30-03 FIG 1 DOUBLER USED 2024-T3 0.07 SHEET METAL 12 BY 7 1/2" CAT A REPAIR.SDR EIA2006136Shear Tie · crackedAFT CARGO AREA STA 1700 STRINGER 46L TO 47L SHEAR TIE CRACK FOUND. REPAIRED IAW B747 SRM 53-10-04 FIG 3 REPAIR ANGLE USED 7075-T6 0.071.SDR EIA2006135Seat Track · wornFOUND SEAT TRACKS WORN AT RBL 34 STA 510-520. REPAIRED IAW B747 SRM 53-10-05 FIG 1A REPAIR TRACK MADE FROM 63B10047-370 AND REPAIR ANGLES FROM BAC1503-1001-47 7075-T65.11SDR EIA2006134Frame · crackedFOUND BULK CARGO, FUSELAGE FRAME AT STA 2040 STR 3 LEFT FOUND CRACKED. REPAIRED IAW B747 SRM 53-10-04 FIG 90 DOUBLER USED 7075-T6 0.071STRAP 7075-T6 0.063.SDR EIA2006133Frame · crackedMAIN-DECK FRAME AT BS 1940 STR 12-R CRACKED. REPAIRED IAW B747 SRM 53-10-04 FIG 87, DOUBLER USED 7075-T6 0.063, STR USED 7075-T6 0.100.SDR EIA2006163Lens · missingEMERGENCY LIGHT LENS ASSY AT DOOR 5 NOT INSTALLED (MISSING). DOOR 5 LT EMERGENCY LIGHT LENS ASSY INSTALLED IAW B747 MM 33-51-00.SDR EIA2006162Unknown · crackedCRACK FOUND AT AFT CARGO STA 1500 RIGHT, STRINGER 35R CUTOUT. REPAIRED IAW B747 SRM 53-10-04 FIG 4, 7075-T6 0.071 REPAIR ANGLE USED.SDR EIA2006161Frame · crackedFOUND FUSELAGE FRAME STA 280 LT SIDE CRACKED AT STR 27 AT CUTOUT. REPAIRED IAW B747 SRM 53-10-04 FIG 11, 2024-T42 0.063 REPAIR DOUBLER USED.SDR EIA2006176Frame · crackedFUSELAGE FRAME B STA 940 RT FOUND CRACKED BETWEEN STR 37 & STR 38. REPAIRED IAW B747 SRM 53-10-04 FIG 52 REPAIR DOUBLER USED 7075-T6 0.063SDR EIA2006182Frame · crackedFUSELAGE FRAME B STA 960 RT FOUND CRACKED AT CUTOUT FOR STR 31 (TOP CORNER). CRACKED FRAME REPAIRED IAW B747 SRM 53-10-04 FIG 4 REPAIR ANGLE WEB 7075-T6 0.063 USED.SDR EIA2006181Frame · crackedFUSELAGE FRAME B STA 800 LT INNER CHORD FOUND CRACKED BETWEEN STR 35-36. REPAIRED IAW B747 SRM 53-10-04 FIG 52, DOUBLER 7075-T6 0.063 & STRAP 7075-T6 0.040 USED.SDR EIA2006180Frame · crackedFUSELAGE FRAME B STATION 820 LT FOUND CRACKED AT CUTOUT FOR STR 33 (TOP CORNER). REPAIRED IAW B747 SRM 53-6-04 FIG 4 7075-T6 0.071 REPAIR ANGLE USED.SDR EIA2006179Frame · crackedFUSELAGE FRAME B STATION 940 RT FOUND CRACKED AT CUTOUT FOR STR 34 (BOTTOM CORNER). REPAIR IAW B747 SRM 51-40-03 FIG 3 7075-T6 0.063, REPAIR ANGLE USED.SDR EIA2006178Frame · crackedFUSELAGE FRAME B STA 940 RT FOUND CRACKED AT CUTOUT FOR STR 31 (TOP CORNER). REPAIRED IAW B747 SRM 53-10-04 FIG 4, 7075-T6 0.071 REPAIR ANGLE USED.SDR EIA2006177Frame · crackedFUSELAGE FRAME B STA 940 RT FOUND CRACKED AT CUTOUT FOR STR 30 (TOP CORNERS). REPAIRED IAW B747 SRM 53-10-04 FIG 4 7075-T6 0.071, REPAIR ANGLE USED.SDR EIA2006175Floorbeam · crackedMAIN DECK FLOORBEAM STA 320 LEFT WEB AND LOWER CHORD, OUTBOARD OF NOSE WW TORQUE BOX VERTICAL BEAM CRACKED. REPAIRED IAW BOEING MSG 1-206083941-14 DATED 13 JUL 06. SELF FAB WEB REPAIR SEGMENT AND DOUBLER CHORD SEGMENT & SPLICES FAB'D BY WORKSHOP.SDR EIA2006174Skin · crackedNR 1 R MAIN ENTRY DOOR EXTERIOR SKIN FOUND CRACKED AT LWR COLUMN OF RIVETS AS MARKED. REPAIRED IAW B747 SRM 52-10-02 FIG 9 REPAIR DOUBLER USED 2024-T3 0.063 DIMENSIONS 11.5 X 9.25 INCHES.
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