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.

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 Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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.Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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.Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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 DAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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 5Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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 ALUMAug 9, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 R53-25-35Aug 9, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 REQUIREAug 9, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 INSAug 9, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR 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 RAug 9, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR 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.Aug 5, 2006 · N683UP · Boeing 747121 · Emergency LightingSDR 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 B74Jul 29, 2006 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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).Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, BulkheadSDR 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 Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, BulkheadSDR EIA2006156Cover · crackedNR 5 RT DOOR EMERGENCY EXIT LIGHT IDENTIFIER COVER FOUND CRACKED. REPLACED COVER, OPS CHECK GOOD IAW 33-51-00.Jul 28, 2006 · N480EV · Boeing 747121 · Emergency LightingSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR 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 51-10-01Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, BulkheadSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, BulkheadSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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).Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Miscellaneous StructureSDR 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,Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, Plate/SkinSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Internal Mounting StructureSDR 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-T65.11Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 28, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 24, 2006 · N480EV · Boeing 747121 · Emergency LightingSDR 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.Jul 24, 2006 · N480EV · Boeing 747121 · Standard Practices/StructuresSDR 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.Jul 24, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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 0.063Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Fuselage Main, Floor BeamSDR 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.Jul 23, 2006 · N480EV · Boeing 747121 · Passenger/Crew Doors
Back to Boeing 747-121