Boeing 747-123

Service difficulty reports · 2,292

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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 = '747123'
  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 UPS05443994Rib · crackedINSPECTION TYPE:C RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE AT ROTARY ACTUATOR AFT AREA FOUND CRACKED, CRACK LENGTH .5 INCH. RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE REPAIRED AS PER HX RS R57-41-35254 WITH CRACKED AREA TRIMMED OFF & INSPECTED BY NDT.Feb 5, 2005 · N676UP · Boeing 747123 · Wing, Rib/BulkheadSDR UPS05443991Bulkhead · crackedINSPECTION TYPE: C, LT BODY L/G W/W STA 1480 BULKHEAD APU BLEED AIR DUCT CUT OUT FOUND CRACKED AT LEFT O/B SIDE LBL 100. CRACK LENGTH 2.5 INCH, LT BODY L/G W/W BS 1480 BULKHEAD APU BLEED AIR DUCT CUTOUT REPAIRED AS PER SB B747-53-2309 R1, EO B747-5310-3100-C Feb 4, 2005 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS05443804Stringer · corrodedINSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480-1, Jan 13, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443803Stringer · corrodedINSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. FLAP PEEN CARRIED OUT AS PER SRM 51-10-07 AND SOPM 20-10-03, STRINGER SEGMENT AND SPLICE ANGLE REWOJan 13, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443717Skin · corrodedINSPECTION TYPE:C, CORROSION INDICATOR REVEALED ON FUSELAGE UPPER SKIN AT BS 1820 TO BS 1825 STR 46L. CORROSION BLEND OUT 0.035 X 2 X 2 INCHES EXCEED SRM LIMIT. OVER LAPPING SKIN REPLACED AS PER SRM 53-30-03 FIG 17 AND REPAIR DOUBLER AND FILLER INSTALLED AS Jan 12, 2005 · N675UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS05443832Floor Panel · corrodedSTA 1170 TO 1250, BTN L11 AND R11 FLR METAL PNL SKIN FOUND CORR. METAL FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320- 21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPJan 9, 2005 · N675UP · Boeing 747123 · Fuselage Floor PanelSDR UPS05443802Seat Track · corrodedINSPECTION TYPE:C M/D - BS 1180 RBL 97 I/B SEAT TRACK SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH, EXCEED SRM LIMIT. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443801Seat Track · corrodedINSPECTION TYPE:C - BS 1160 - 1220 RBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. SEAT TRACK CUT OFF AT BS 1070 RBL 98 AS PER SRM 51-10-01. REPROTECTED AS PER SRM 51-10-02. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443772Web · crackedINSPECTION TYPE:C - R3 DOOR LOWER WEB CRACKED AT LOWER GATE PUSH ROD CUTOUT. LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jan 9, 2005 · N675UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS05443667Seat Track · corrodedINSPECTION TYPE:C - BS 1000 LBL 33 O/B SEAT TRACK FLANGE CORRODED. M/D BS 990 - 1000 LBL 33 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443659Floorbeam · corrodedINSPECTION TYPE:C - FLOORBEAM BS 340 LBL 11 - 39 UPPER CHORD CORRODED. REPAIR PARTS FABRICATED AS PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443654Seat Track · corrodedINSPECTION TYPE:C - BS 520 - 540 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 520 - 560 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.060 X 1 X 1 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443653Seat Track · corrodedINSPECTION TYPE:C U/D - BS 480 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 480 - 500 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.050 X 1 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443650Seat Track · corrodedBS 480 - 500 RBL 66 SEAT TRACK CORRODED AS MARKED. SEAT TRACK PART FABRICATED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.Jan 9, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443812Stringer · crackedBS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443773Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443730Stiffener · crackedINSPECTION TYPE:C - BS 1080 RBL 99 BELOW FLOOR STIFFENER FOUND CRACKED. M/D BS 1080 RBL 99 BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-01 PAGE 9.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443726Intercostal · crackedINSPECTION TYPE:C M/D - BS 1220 RBL 118 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. WEB REPAIR PER SRM 51-40-02 FIG 1.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443720Stringer · crackedINSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443716Frame · crackedINSPECTION TYPE:C - BS 960, S8R, FRAME FOUND CRACK. FRAME REPAIRED PER SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443714Frame · crackedINSPECTION TYPE:C - FRAME BS 760 STR CUTOUT CRACKED AT S-6L AND S-7L. M/D BS 760 BETWEEN STR 6L AND STR 7L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443712Frame · crackedINSPECTION TYPE:C - BS 740, BETWEEN S7 - 8R, FRAME FOUND CRACK. M/D BS 740 BETWEEN STR 7R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443711Frame · crackedINSPECTION TYPE:C - BS 760, BETWEEN STR 5 - 8R, FRAME FOUND CRACK. M/D BS 760 BETWEEN STR 5R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443678Spar · crackedINSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH. PLS REFER ATTACH FIG. HOLE REPAIRED AS PER S/B 747-57A2314.Jan 8, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443676Splice · crackedINSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTING APPROX 0.040 INCH REFER ATTACHED SKETCH. HOLE REPAIRED AS PER SB 747-57A2314.Jan 8, 2005 · N675UP · Boeing 747123 · Wing Main, Frame StructureSDR UPS05443666Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443665Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443660Stringer · crackedINSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443658Frame · crackedINSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME WEB SURFACE FOUND CRACKED AT STA 880 BETWEEN STRINGER 37L TO STRINGER 38L. SUPPORT FRAME REPAIRED PER SRM 53-10-04 FIG 52.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, FrameSDR UPS05443657Stringer · crackedINSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443656Stringer · crackedINSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443655Stringer · crackedINSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443652Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0601428Anti-Ice System · no testDURING CREW PRE-FLIGHT, FOUND LT UPPER PITOT STATIC PROBE HEAT WOULD NOT TEST. REPLACED PITOT PROBE IAW AMM 34-11-01.Jan 7, 2005 · N858FT · Boeing 747123 · Pitot/Static Anti-Ice SystemSDR UPS05443800Attach Angle · corrodedINSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME UPPER CHORD LOWER ATTACH ANGLE SURFACE FOUND CORROSION AT STA 700 LBL 38. ANGLE REPLACED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.040 X 1 X 2 INCH.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443775Web · corrodedINSPECTION TYPE:C, AFT CARGO COMPT RT STA 1660 - 1680 STRINGER 30 WEB SUPPORT BOTTOM SURFACE CORROSION AS MARK. CORROSION BLEND OUT 0.030 X 2 X 2 INCHES EXCEED SRM LIMIT. WEB SUPPORT AND TIE CLIP REPLACED AS PER SRM 51-10-01.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443767Stringer · crackedINSPECTION TYPE:C M/D - BS 742 - 744 STR 23R, STRINGER END FOUND CRACK. M/D BS 742 TO BS 744 S-23R STRINGER END REPAIRED AS PER RS : 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443764Seat Track · corrodedINSPECTION TYPE:C - BS 1480 - 1500 RBL 11 SEAT TRACK O/B FLANGE FOUND CORRODED. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.040 X 1 X 3 INCHES EXCEED SRM LIMIT.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443733Stringer Clip · crackedINSPECTION TYPE:C M/D - BS 1040 S9R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443732Stringer Clip · crackedINSPECTION TYPE:C M/D - BS 1040 S3R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443731Stringer Clip · crackedINSPECTION TYPE:C - BS 620 S15L FRAME TIE CLIP FOUND CRACK. TIE CLIP REPLACED PER SRM 51-10-01 PG 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443728Stringer Clip · crackedBS 1060 STR 5R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1060 STR 5R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443727Stringer Clip · crackedINSPECTION TYPE:C - BS 1040 STR 1R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 1R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443725Stringer Clip · crackedINSPECTION TYPE:C - BS 1040 S2R STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 2R STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443724Stringer · crackedINSPECTION TYPE:C - LEFT BS 2658 STR 13 FOUND CRACKED. STRINGER REPLACED AS PER SRM 50-10-01.Jan 7, 2005 · N675UP · Boeing 747123 · Horizontal Stabilizer, Tab StructureSDR UPS05443713Stringer · crackedINSPECTION TYPE:C - BS 1000 TO 1020 S10R STRINGER END FOUND CRACKED. M/D BS 1000 TO BS 1030 STR 10R STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS05443691Shear Tie · crackedINSPECTION TYPE: C, FWD CARGO COMPT SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 780 STR 33 TO STR 34. SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 4.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, StructureSDR UPS05443674Spar · crackedINSPECTION TYPE:C, RT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 11 FASTENER HOLE CRACKED AT UPPER SKIN LAYER APPROX 0.060 INCH RUNNING AFT. HOLE REPAIRED AS PER SB 747-57A2314.Jan 7, 2005 · N675UP · Boeing 747123 · Wing SparSDR UPS05443664Floorbeam · corrodedINSPECTION TYPE:C M/D - BS 1500 RBL 38 FLOORBEAM FOUND CORRODED. FLOORBEAM REPAIR PARTS FABRICATED PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443663Frame · crackedINSPECTION TYPE:C M/D - BS 660, BET S25 - 26R, FRAME I/B CHORD O/B FACE FOUND CRACK. FRAME I/B CHORD REPLACED PER SRM 51-10-01 PG 9.Jan 7, 2005 · N675UP · Boeing 747123 · Fuselage Main, Frame
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