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 UPS05444777Pressure Panel · crackedRT NWW SIDE PANEL FOUND 2 EA CRACK BOTH APPROX 1 INCH AT BTN BS 260 AND 280, WL 150, CRACK LENGTH 1 IN. RT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 116.Jun 29, 2005 · N682UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444776Web · crackedRT NWW SIDE PANEL FOUND CRACKED AT BTN BS 260 AND 280 WL 170, CRACK LENGTH 2.5 IN. REPAIRED AS PER SRM 53-10-04 FIG 116.Jun 29, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444775Skin · corrodedINTERIM REPAIR AFT OF ELECTRICAL ACCESS DOOR. CORROSION BLEND OUT 2 BY 5 IN , SKIN INTERNAL BONDED DOUBLER CORRODED. REMOVED PER HX RS NR R53-30-35332 AND UPS EA NR 747-53-20252 AND STRAP REPLACED PER SRM 51-10-01.Jun 27, 2005 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS05444712Battery Pack · inoperativePS EMERGENCY EXIT LIGHT IN OVERHEAD FWD OF LAVATORY COMES ON ONLY MOMENTARILY THEN GOES OUT. REPLACED EMERGENCY LIGHT BATTERY PACK PER M/M 33-51-07. OPS CHECK GOOD.Jun 18, 2005 · N683UP · Boeing 747121 · Emergency LightingSDR UPS05444308Pressure Panel · crackedINSPECTION TYPE:SV NOSE W/W LEFT SIDE PANEL FROM BS 260-280 AT WL 170 CRACK INDICATED FOUND AT THE LOCATION FASTENER NR 7 TO 15. CRACK LENGTH 9 INCHES. WEB REPAIRED AS PER EO B747-5310-20502-C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444307Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 280-300 WL 170 CRACK INDICATION FOUND AT FASTENER LOCATION NR 6, 10, 12 AT WEB. CRACK LENGTH 3 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444306Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 260-280 WL 150 CRACK INDICATION FOUND BETWEEN NR 8, 13 AT WEB AREA. CRACK LENGTH 6 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444305Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 280-300 WL 160 CRACK AT NR 12 TO NR 14 & NR 16 FASTENER AREA. CRACK LENGTH 5 INCH. CRACKED SIDE PANEL REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444304Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 260 - 280 WL 170 CRACK INDICATION FOUND AT FASTENER NR 8 AT WEB AREA. CRACK LENGTH 1 INCH. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM 6 INSTRUCTION AND SRM 53-10-04 FIGURE 116.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444302Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL TOP PANEL FROM BS 300 TO 320 AT LBL 20 CRACK INDICATION FOUND AT FASTENER NR 8, 9, 14, 15 & 16. CRACK LENGTH 5 INCHES. CRACKED TOP PANEL REPAIRED AS PER HX RS R53-10-35292 & UPS EO B747-5310-22075-A.Apr 16, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444303Pressure Panel · crackedINSPECTION TYPE:SV NW-LT SIDE WALL WEB CRACK AT 4 EA HOLE LOCATION AT BS 280 - 300 WL 170 AREA. CRACK LENGTH 4 INCHES. NW-LT SIDE WALL WEB CRACK AREA REPAIR AS PER EO B747-5310-20502 APPENDIX C ITEM 6 INSTRUCTION & SRM 53-10-04 FIGURE 116.Apr 15, 2005 · N681UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS05444197Battery · dischargedINSPECTION TYPE:A CHECK EMERGENCY LIGHT IN CIRCULAR CEILING LIGHT WILL NOT TAKE A CHARGE. REPLACED BATTERY PACK EMERGENCY LIGHT, OPS CHECKS OK.Mar 25, 2005 · N683UP · Boeing 747121 · Emergency LightingSDR UPS05444208Fitting · crackedINSPECTION TYPE:C M/DECK BS 2019 RBL 60 BELOW FLOOR SUPPORT FTG FOUND CRACK AFTER BS 2020 FLOOR FTG REMOVAL, CRACK LENGTH 3/8 INCH. M/DECK BS 2019 RBL 60 INCH BELOW FLOOR SUPT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Mar 23, 2005 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS05444211Cargo Track · corrodedM/DECK BS 1720 LBL 78 INCH AND 85 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG AND PLATE REPLACED AS PER MM 20-51-01 FTG P/N: 69B62076-1, PLATE P/N: 69B62100-1.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444207Fitting · crackedM/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG FOUND CRACKED, CRACK LENGTH 3/4 INCH. M/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS05444206Cargo Track · corrodedM/DECK BS 1880 RBL 50 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, BS 1880 RBL 50 INCH TIE DOWN FTG. REEPLACED AS PER MM 20-51-01.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444180Floorbeam · crackedINSPECTION TYPE: C M/D- BS 1500 RBL 83-89 FLOORBEAM UPPER CHORD LWR SURFACE CRACKED CRACK, LENGTH .375 INCH. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS05444179Seat Track · corrodedINSPECTION TYPE:C M/D- BS 2040 - 2140 LBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444178Seat Track · corrodedINSPECTION TYPE:C M/D - BS 2040-2050 LBL 88 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444177Seat Track · corrodedINSPECTION TYPE:C M/D- BS 1800 TO 1920 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 16.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444176Seat Track · corrodedINSPECTION TYPE:C M/D- BS 1780 RBL 95 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444173Seat Track · corrodedINSPECTION TYPE:C M/D- BS 2130 TO 2140 LBL 75 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 1 INCH. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.Mar 14, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444210Cargo Track · corrodedM/DECK BS 1500 LBL 75 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG REPLACED AS PER MM 20-51-01.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444209Cargo Track · corrodedM/DECK BS 1940 AND 1960 LBL 80 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1940 LBL 80 INCH TIE DOWN FTG REPLACED AS PER MM 20-51-01.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444205Seat Track · corrodedBS 1500-1580 LBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444203Fitting · corrodedBS 1680 LBL 55 TIE DOWN FIG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FIG PLATE REPLACED AS PER MM 20-51-01.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS05444202Seat Track · corrodedBS 1700-1707 LBL 11 INCH SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444201Seat Track · corrodedBS 1564-1570 RBL 98 INCH SEAT TRACK LEFT FLANGE CORROSION. CORROSION BLEND OUT 0.035 INCH BY 1 INCH BY 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444188Shear Tie · crackedINSPECTION TYPE:C M/D- BS 2160 L BETWEEN STR 13L & 14L SHEAR TIE CRACKED, LENGTH .25 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444187Stringer Clip · crackedINSPECTION TYPE:C M/D- BS 1960 LT STR 2L TIE CLIP CRACKED, LENGTH .375 INCH. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS05444185Web · crackedINSPECTION TYPE:C M/D- STA 1220 LBL 116-118 BELOW FLOOR SUPPORT WEB CRACKED, LENGTH 2 INCHES. FLOOR SUPPORT WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444184Floor Support · crackedINSPECTION TYPE:C M/D- STA 1500 RBL 117 FLOOR SUPPORT ANGLE CRACKED, LENGTH .75 INCH. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444183Floor Support · corrodedINSPECTION TYPE:C M/D- BS 1580 - 1600 LBL 118 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT 0.035 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444182Floor Support · corrodedINSPECTION TYPE:C M/D-BS 1650 LBL 118 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444181Floorbeam · corrodedINSPECTION TYPE:C M/D- BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.060 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS05444175Seat Track · corrodedINSPECTION TYPE: C, M/D- BS 1920 - 2040 LBL 95 SEAT TRACK & FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444174Seat Track · corrodedINSPECTION TYPE:C M/D - BS 1528-1532 RBL 75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444155Stringer · crackedINSPECTION TYPE:C AREA AFT OF BULK CARGO STA 2180 S42R STRINGER END CRACKED, CRACK LENGTH .75 INCH. AFT OF BULK CARGO BS 2160 TO 2180 STR 42R REPAIRED AS PER SRM 53-10-03 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS05444212Support · corrodedAFT CARGO WALKWAY PANEL SUPPORT FOUND CORRODED BETWEEN BS 1580 AND 1600 RBL 36. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, WALKWAY PANEL SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444200Panel · crackedRT WING L/E CAVITY AT FSSI 998 L/E MOST FWD D-SECTION ATT PANEL AND UPPER EDGE CHORD FOUND CRACKED, AFT OF NR 20 VC FLAP, CRACK LENGTH 1 INCH. PANELS AND CHORD REPAIRED AS PER SRM 57-20-03 FIG 7.Mar 12, 2005 · N682UP · Boeing 747121 · Wing, Plate/SkinSDR UPS05444189Stiffener · crackedINSPECTION TYPE:C M/D- STA 1435 RBL 65 WHEEL WELL UPPER SKIN ATTACH STIFFENER FOUND CRACKED, LENGTH .375 INCH. STIFFENER REPLACED AS PER SRM 51-30-02 & SRM 51-10-01 PG 9.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444186Floor Support · corrodedINSPECTION TYPE:C M/D- BS 2350 - 2360 RBL 55 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444153Shear Tie · crackedINSPECTION TYPE:C M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444145Floor Support · crackedINSPECTION TYPE:C M/D - BS 2300 RBL 52 FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 0.5 INCH. M/D - BS 2300 RBL 52 FLOOR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS05444129Stringer · crackedINSPECTION TYPE:C, BS 1278 STR 25R END FOUND CRACKED. CRACK LENGTH .75 INCH. M/DECK BS 2170-2180 STR 25R REPAIRED AS PER SRM 53-10-03 FIG 1.Mar 12, 2005 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS05444213Frame · crackedBS 2180 STR 25R FRAME FOUND CRACKED, CRACK LENGTH 1 INCH. FRAME REPAIRED AT BS 2180 STR 25R AREA AS PER HX RS R-53-62-35275 AND UPS EO B747-5310-21972A.Mar 11, 2005 · N682UP · Boeing 747121 · Fuselage Main, FrameSDR UPS05444152Shear Tie · crackedINSPECTION TYPE:C M/D - BS 1540 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 11, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444150Shear Tie · crackedINSPECTION TYPE:C M/D - BS 1580 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 11, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444149Shear Tie · crackedINSPECTION TYPE:C M/D - BS 1560 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGHT .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 11, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting StructureSDR UPS05444147Shear Tie · crackedINSPECTION TYPE:C M/D - BS 1580 S-19R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Mar 11, 2005 · N682UP · Boeing 747121 · Fuselage Internal Mounting Structure
Back to Boeing 747-121