Boeing 737-7Q8
Service difficulty reports · 3,964
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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 = '7377Q8' 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 = '7377Q8' 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 SWAA2022060806779Fitting · corrodedFED AFT GIRT BAR FLOOR ATTACH FTG CORRODED ON UPPER SURFACE BS 344 LBL 59.5 WL 208.1 / [01] FED AFT GIRT BAR ATTACH FITTING FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS FOUND FOR THIS PART AND IT IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02;[02] RSDR SWAA2022060807043Beam · crackedCRACKED LEFT WING FIXED T/E PANEL SUPPORT AFT OF THE PYLON; ABOVE DEFLECTION RIB. MARKED. / [01] REMOVED 2 BOLTS AT UPPER CONTROL RIB COMMON TO DEFECTION CONTROL PANEL IAW SRM 51-40-02;[02] REMOVED 2 BOLTS AT UPPER SUPPORT BEAM COMMON TO DEFECTION CONTROL RIB SDR SWAA2022060807045Support · crackedLOWER BULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS271. MARKED / [01] REMOVED AND REPLACED LOWER BULB SEAL RETAINER SUPPORT AT LH WING FIXED T/E PANEL. IAW SRM 51-40-02 AND IPC 57-50-00-25.;[02] VERIFIED CORRECTISDR SWAA2022060806245Panel · pulledFWD PASSENGER PANEL P/N 141A5810-272 UPPER SKIN FWD AREA HAS PULLED STRANDS. / IDENTIFIED PANEL 141A5810-272 IAW SRM 53-00-50-0I-1 FIGURE 2; DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.B.(2) AND WILL BE REPAIRED IAW SRM 53-00-50-2R-1. SDR SWAA2022060806246Panel · pulledFWD PASSENGER PANEL P/N 141A5810-274 UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] FWD PASSENGER CABIN FLOOR PANEL P/N 141A5810-274 WITH UPPER SKIN HAVING PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNSDR SWAA2022060806247Panel · pulledFWD PASSENGER PANEL P/N 141A5810-567 UPPER SKIN O/B AREA HAS PULLED STRANDS. / [01] FWD PASSENGER CABIN FLOOR PANEL P/N 141A5810-567 WITH UPPER SKIN HAVING PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNSDR SWAA2022060806248Panel · pulledFWD PASSENGER PANEL P/N 141A5810-582 UPPER SKIN HAS AREAS OF PULLED STRANDS. / IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1SDR SWAA2022060806250Floor Panel · pulledFWD PPASSENGER CABIN FLOOR PANEL 221GF UPPER SKIN HAS PULLED STRANDS NEAR FWD EDGE. (MARKED) / [01] FWD PASSENGER CABIN FLOOR PANEL 221GF WITH UPPER SKIN HAVING PULLED STRANDS NEAR FWD EDGE AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02SDR SWAA2022060806251Floor Panel · pulledFWD PASSENGER CABIN FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS. / IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2. FOUND MULTIPLE ADDITIONAL DAMAGE LOCATIONS ON LOWER SURFACE; ALL DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SDR SWAA2022060806252Panel · pulledFWD PASSENGER PANEL P/N 141A5810-235 UPPER SKIN HAS AREAS OF PULLED STRANDS. / REMOVED ALL THROUGH AND BLIND INSERTS TO FACILITATE REPAIRS IAW SRM 53-00-50-2R-1 PARA 3.B.IDENTIFIED PANEL 141A5810-235 MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2.DAMAGED ARESDR SWAA2022060806253Floor Panel · pulledFWD PASSENGER PANEL P/N 141A5810-479 UPPER SKIN HAS AREAS OF PULLED STRANDS.DAMAGED AREAS EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B.DAMAGE IS TO BE REPAIRED IAW SRM 53-00-50-2R-1.REMOVED ALL THROUGH AND BLIND INSERTS AND REMOVED DAMAGE IN MUSDR SWAA2022060806256Intercostal · crackedCRACKED INTERCOSTAL AT STA 277+7 AND STA 277+13; RBL 1; WL 208. CRACKED INTERCOSTAL AT STA 277+7 AND STA 277+13; RBL 1; WL 208 P/N 141A5410-3 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0GSDR SWAA2022060806257Intercostal · crackedCRACKED INTERCOSTAL AT STA 294.5+6; RBL 1; WL 208. / [01] VERIFIED APPLICABILITY PER SRM 51-10-02-0G-0<BR><BR> REMOVED DAMAGE FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[02] REMSDR SWAA2022060806260Intercostal · crackedCRACKED INTERCOSTAL AT STA 312+9;LBL 46; WL 208. CRACKED INTERCOSTAL AT STA 312+9;LBL 46; WL 208 P/N 141A5410-12 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .; REMOVED INTERCOSTSDR SWAA2022060806261Intercostal · crackedCRACKED INTERCOSTAL AT STA 328+7; LBL 46; WL 208. CRACKED INTERCOSTAL AT STA 328+7; LBL 46; WL 208 P/N 141A5410-16; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .; REMOVED INTERCOSTSDR SWAA2022060806262Intercostal · corrodedCRACKED INTERCOSTAL AT STA 312+5; RBL 31; WL 208. CRACKED INTERCOSTAL AT STA 312+5; RBL 31; WL 208 P/N 141A5410-12; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .; REMOVED INTERCOSTSDR SWAA2022060806412Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT BL 0 BS 927+4; BS 927+16. UPON FURTHER INVESTIGATION FOUND CRACK ON PASSENGER CABIN ANGLE ATTACHED TO INTERCOSTAL (CHORD P/N 147A5430-1) AT LBL 0.859 ; BS 927+4; BS AND 927+16; WL 208.10.;PASSENGER CABIN ANGLE ATTACHED SDR SWAA2022060806417Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 987 LBL43.VERIFIED APPLICABILITY OF SRM 53-70-51-01-1 FOR IDENTIFICATION AND SRM 53-70-51-1A-1 FOR ALLOWABLE LIMIT; REMOVED CORROSION FROM PASSENGER CABIN FLOOR BEAM BS 987 LBL43 WL 208.5 IN AREA OF 1.3' X 0.9' X 0SDR SWAA2022060806424Floor Panel · missingAFT CABIN FLOOR PANEL 241ABF HAS A MISSING 'BLIND' INSERT ON THE O/B EDGE. IDENTIFIED PANEL 241ADF IAW SRM 53-00-50-0I-1 TABLE 6 AND FIGURE 6. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E.(2).(B) AND WILL BE REPAIRED IAW SRM 53-00-50-2SDR SWAA2022060806644Skin · crackedCRACK IN LH HORIZ STAB LOWER SKIN. LOCATED ALONG INBD SIDE OF STAB STA 193.9 RIB; 17'FROM FRONT SPAR. CRACK VERIFIED BY HFEC. RUNS IN FWD AND AFT DIRECTION AND MEASURES .9' IN LENGTH. SRM 55-10-01-2R-11 IS APPLICABLE TO THIS REPAIR.; TRIMMED OUT THE DAMAGED PASDR SWAA2022060805961Threshold · corrodedCORROSION ON FWD CARGO BAY THRESHOLD AT RBL 27 BS 460+16. CORROSION FOUND ON FWD CARGO BAY SUB THRESHOLD WEB AT RBL 27 BS 460+16 /VERIFIED APPLICABILITY OF SRM 53-30-15-01-1 AND SRM 53-30-15-1A-1 FOR ALLOWABLE LIMIT;REMOVED CORROSION FROM FWD CARGO BAY SUBTHRESDR SWAA2022060805970Tie Down · corrodedCORROSION ON FWD CARGO BAY TIE DOWN AT LBL 18 BS 400+2; BS 400+18; BS 420+16; BS 480+16; BS 500A+18; BS 500C+16. / [01] VERIFIED THE APPLICABILITY OF SRM 53-30-53-0I-2 ; AND SRM 53-00-53-1A-2;[02] REMOVED CORROSION ON FCB TIE DOWN TRACK AT LBL 18 BETWEEN BS 40SDR SWAA2022060805971Baffle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH POINT AT LBL 24 BS 500B+1. CRACK FUND AT FWD CARGO BAY BAFFLE FLANGE LBL 24 BS 500B+1 / DAMAGE FOUND AT FCB BAFFLE FLANGE BS 500B + 1 LBL 24 MEASURED 0.3' FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 DET.4C; FIG SDR SWAA2022060805956Shield · corrodedAFT CARGO BAY DOOR CUTOUT FWD SHEILD IS CORRODED FROM BS 767+1 TO BS 794; WL 157 RBL 21 TO RBL 23 / [01] CHECK LIMITS; NO FOUND ALLOWABLE LIMITS ON SRM FOR THIS PART L=2 W= 1 MATERIAL REMAINING .030'; PART IS REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02SDR SWAA2022060805967Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500+14; BS 500A+6. / [01] VERIFIED APPLICABILITY OF SRM 53-00-53-01-1 FOR IDENTIFICATION AND SRM 53-00-53-1A-1 FOR ALLOWABLE LIMIT;[07] REMOVED THE DAMAGED PART OF THE FLOOR TO SIDEWALL SUPPORT SDR SWAA2022060805968Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+6; BS 500A+14. / [01] VERIFIED APPLICABILITY OF SRM 53-00-53-01-1 FOR IDENTIFICATION AND SRM 53-00-53-1A-1 FOR ALLOWABLE LIMIT;[02] REMOVED CORROSION FROM FCB FLOOR TO SIDE WALL SDR SWAA2022060805969Shield · corrodedCORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 25 BS 500+2; BS 500+6; BS 500+10; BS 500+14; BS 500+18. / [01] CORROSION AT FCB AFT SHIELD FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR-9C;[02]SDR SWAA2022060805975Light · missingPASSENGER SIDEWALL PANEL 231YHW; FLOOR PROXIMITY EXIT SIGN IS MISSING A MOUNTING FASTENER. / [01] REPLACED FASTENER ON PASSANGER SIDEWALL PANEL 231YHW; FLOOR PROXIMITY EXIT SIGN IAW AMM 33-51-01-960-802; STEP 3 (C)-6 (A) (E).;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022060805683Panel · delaminatedR/W L/E PANEL 621CB DELAM ON L/E OF PANEL / [01] REMOVED 2EA. BACKUP PLATES ACCORDING TO SRM 51-40-02; PARA. 4.E02] IDENTIFIED PANEL 621CB MATERIAL ACCORDING TO SRM 57-41-01-0I-4; FIG. 5; TABLE 5; ITEM 3; AND FIG. 20; TABLE 17.<BR><BR>FOUND DAMAGE TO BE OUT OFSDR SWAA2022060805699Panel · pulledR/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 57-51-01-0I-1 FIG.3; SHT.1; TABLE 3; AND ITEM 10. FOUND SEVERAL PULLED FASTENER HOLES TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-51-01-1A-1 PAR.4SDR SWAA2022060805703Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-51-01-0I-1 FIGURES 1+3; TABLE 3; ITEM[9].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4.B (5) (B).<BR>PERMANENT REPSDR SWAA2022060805704Panel · pulledL/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 57-51-01-0I-1 FIG.3; SHT.1; TABLE 3; AND ITEM 10. FOUND SEVERAL PULLED FASTENER HOLES TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-51-01-1A-1 PAR.4SDR SWAA2022060805705Panel · delaminatedL/W L/E PANEL 521DB HAS AREA OF DELAM (MARKED) / [01] IDENTIFIED PANEL 521DB MATERIAL IAW SRM 57-41-01-0I-1 FIGURE 5 TABLE 5 ITEM 2<BR><BR>DAMAGED AREAS EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR.4 A(2)<BR><BR>DAMAGE IS REPAIRABLE IAW SRM 51-70-0SDR SWAA2022060805347Support Fitting · corrodedCORROSION ON AFT CARGO BAY FLOOR SUPPORT FITTING AT STA 887; LBL 8.5; WL 168.6. / [01] REMOVED CORROSION ON AFT CARGO BAY FLOOR SUPPORT FITTING P/N 146A9401-40 AT STA 887; LBL 8.5; WL 168.6 AREA 1.2'X.8'X.016 ; FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0.<SDR SWAA2022060805348Splice · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 867+19; AND 887+1; WL 168.6; RBL 21. / [01] PARTIAL STEP 1 AND 2.;[02] VERIFIED PARTIAL UPDATE STEP 1; 2.;[03] FABRICATED; LOCATED AND DRILLED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 887 LBLSDR SWAA2022060805350Support · corrodedCORROSION ON ACB AFT BULKHEAD SUPPORT AT STA 947.5; RBL 14.5; 181.6 AND RBL 17; WL 183. CORRECTION: CORROSION AT STA 947.5; RBL 14.5 WL 181.6 AND RBL 17 RBL 183. / [01] REMOVED CORROSION ON PART L=1.0 W=1.0 D=.011.CHECK LIMITS FOR THIS PART; NO ALLOWABLE LIMITSDR SWAA2022060805352Support · corrodedCORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT FROM STA 727B+2 TO STA 747+18; WL 156; RBL 20 TO RBL 22. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727A+4 - BS767 IAW SRM 51-40-02.<BR><BR><BR>REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORSDR SWAA2022060805353Support · corrodedCORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727+18 TO STA 787+4; WL 156; LBL 20 TO LBL 22. / [01] REMOVED CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727+18 TO STA 787+4; WL 156; LBL 20 TO LBL 22 P/N 146A7502-1 ;AREASDR SWAA2022060805354Support · corrodedCORROSION ON AFT CARGO BAY FWD BULKHEAD SUPPORT AT STA 727+5; LBL 8 TO LBL 11; WL 156. / [01] CHECK LIMITS FOR PART; NO FOUND ALLOWABLE DAMAGED ON SRM FOR THIS PART REPAIRED BY REPLACEMENT PART PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION #1.;[03] RSDR SWAA2022060805500Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE (MARKED) / [01] IDENTIFIED PANEL 661AB IAW SRM 57-51-01-0I-1 FIGURE 3; SHEET 1; TABLE 3; ITEM 5. <BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4B(5).<BR><BR>REPAIR TO BE ACSDR SWAA2022060805501Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / [01] IDENTIFIED PANEL 661BB MATERIAL IAW SRM 57-51-01-0I-1 TABLE 3 FIGURE 3 ITEM 9. DAMAGE TO MULTIPLE FASTENER HOLES AS MARKED ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARAGRAPH SDR SWAA2022051105546Lens · brokenFWD ENTRY EMERGENCY LIGHT LENS BROKEN / [01] REPLACED PER SIPSDR SWAA2022060805251Panel · pulledL/W T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES. IDENTIFIED L/W T/E PANEL 561CB IAW SRM 57-51-01-0I-1 FIGURE 3; SHEET 1; TABLE 3; ITEM 10. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4B(5).REPAIR TO BE ACCOMPLISHED IAW SRM 51SDR SWAA2022060805345Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 164. / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR.;[02] CUT AND REMOVED DAMAGE ON WING CENTER SESDR SWAA2022060804991Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.5; 3RD VERTICAL STIFFENER IS CRACKED. / REMOVED DAMAGE FROM 3RD VERTICAL STIFFENER OF THE RIB 129.5 IAW SRM 55-10-09-2R-4; STEP 4.B.(1); HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-0SDR SWAA2022050403248Water Separator · contaminatedTWO MINUTES INTO FLIGHT FAS COMPLAINED OF AN ODD SMELL IN THE CABIN. ALSO A SENSE OF HEAT FILLING THE CABIN. WE RETURNED TO DENVER AND PERFORMED AN OVER WEIGHT LANDING AT 130.2K LBS; OTHERWISE NORMAL LANDING. FAS SAID SMELL WENT AWAY DURING DECENT. NO ABNORMALSDR SWAA2022050402405Light · inoperativeEMERGENCY LIGHT BETWEEN ROWS 8 AND 9 IS OUT ROWS 8DEF-9DEF / [01] CORRECTED BY BATT PACK REPLACEMENT ON NON ROUTINE TTG8Q00C8D38. OPS CHK GOOD.SDR SWAA2022050402193Light · inoperativeEMERGENCY LIGHTS AT ROWS 6ABC-12ABC IS OUT / [01] REPLACED BATT PACK OF THE AFFECTED EMERGENCY LIGHTS PER AMM 33-51-06. OPS CHK GOOD.SDR SWAA2022041893636Light · inoperative12 ABC BULLNOSE EMERGENCY LIGHT LENS NOT SECURE / [01] REMOVED AND REPLACED EMERGENCY LIGHT LENS AT 12 ABC REF AMM 33-51-03;[02] INSPSDR SWAA2022041893525Battery Pack · faultyEMERGENCY EXIT LIGHTS AT AFT 2 LT OVHD BINS AND AFT LAV WALL COME ON THEN GO OUT. / [01] REMOVED; REPLACED AND PERFORMED GOOD OPS TEST OF M1673 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION 1.
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