Boeing 737-7L9
Service difficulty reports · 1,024
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 = '7377L9' 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 = '7377L9' 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 SWAA2022011047296Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS727B+3; BS727B+12 - BS727C; BS727C+3 - BS727C+13; BS727D - BS727D+10; BS727D+14 - BS747; BS747+5 - BS805; BS814; BS821 - BS833. ; / [01] COMPLETED STEPS 1-8; [02] VERIFIED STEPS 1 - 8 COMPLETE.; [03] STEPSDR SWAA2022011047294Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS483; BS494 - BS500+13; BS500A+7 - BS500B+2; BS500B+14; BS500C - BS500C+13; BS500D+9 - BS520; BS500D+6. ; / [01] UPDATED MEASUREMENTS; [02] ACCOMPLISHED STEPS 1 AND 2; [03] STEP 1 COMPLETE. VERIFIED PARTIASDR SWAA2022011047297Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS840; BS846 - BS861; BS876 - BS887. ; / [01] UPDATED PARAMETER VALUES; [02] ACCOMPLISHED STEPS 1 AND 2; [03] VERIFIED STEP 1 AND 2 COMPLETE; [04] STEP 3 COMPLETE.; [05] EDITED MEASUREMENT TABLE ADDED FULL SDR SWAA2022011047298Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL45 WL208.1 BS386 - BS399; BS420 - BS426; BS439 - BS458; BS474; BS465. ; / [01] BLENDED CORROSION FROM SEAT TRACK AT LBL 45.5 WL 208 BS386-399; BS420-426; BS439-458 AND BS465-474 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; [02SDR SWAA2022011047299Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK LBL45 WL208.1 BS483; BS492; BS500+6 - BS500+15; BS500A+13 - BS500B+11; BS500C - BS500C+11; BS500D+9 - BS520. ; / [01] BLENDED CORROSION FROM SEAT TRACK AT LBL45.5 WL 208 BS483-492; BS500+6-500+15; BS500A+13-500B+11; BS50SDR SWAA2022011047080Support Angle · corrodedCORROSION ON SUPPORT CLIP AT MAIN EBAY BL0 BS360. MARKED. ; / [01] REMOVED CORROSION IN AN AREA OF 1.7'X1' PER SRM 51-10-02-0G-0; [02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.; [03] UT INSPECTED DENT/BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESDR SWAA2022010647084Intercostal · corrodedCORROSION ON INTERCOSTAL IN MAIN E&E BAY BS359 S-23L. REMOVED CORROSION IAW SRM 51-10-02-0G-0, UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 2, REMOVED CORROSION IN AN AREA OF 1.5'X0.4' PER SRM 51-10-02-0G-0. REPAIRED PER EA 21-153-03572.SDR SWAA2022010647082Support Angle · corrodedCORROSION ON SUPPORT ANGLE AT MAIN EBAY BS380 S-23L. REMOVED CORROSION IN AN AREA OF 1' X 1' IAW SRM 51-10-02-0G-0. UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 2, REMAINING THICKNESS IS 0.035'. EVALUATED CORROSION ON SUPPORT ANGLE, FOUNDSDR SWAA2022011046891Angle · corrodedCORROSION FWD CARGO BAY AFT BULKHEAD L/H LOWER BULKHEAD SUPPORT ANGLE I/B END APPROX BS 500D; LBL 25; WL 153 ; / [01] WORK WILL BE PERFORMED ON FAULT. TTG8Q009FXXB; [02] DUPLICATE CARD; ALL EVALUATIONS ARE ACCOMPLISHED ON TTG8Q009FXXB; [03] INADVERTENTLY USED SDR SWAA2022010646893Cargo Track · damagedFWD CARGO BAY RAIL BS 500C+19 LBL RBL 8.5 HAS ELONGATED HOLE ; / [01] VERIFIED EWIS PROTECTION; [02] REMOVED DAMAGED SECTION OF CARGO RAIL 500C +10' TO 500D RBL 8.5 IAW SRM 53-00-53-2R-2 REP.2; [03] FABRICATED REPAIR PARTS; CHANNEL FILLER BAC1509-100146 7050-TSDR SWAA2022010646715Support Angle · crackedFLOOR SUPPORT ANGLE CRACKED BS 927+10- BS927+11 BL 0 WL 208 ; / [01] REMOVED FLOOR SUPPORT ANGLE AT BS 927+10 BL 0 WL 208 IAW SRM 51-40-02; [02] CORRECTION OF BODY STATIONS. REMOVED FLOOR SUPPORT ANGLE AT BS 927-947 BL 0 WL 208 IAW SRM 51-4-02; [03] CERTIFIED;SDR SWAA2022010546890Baffle · elongatedFWD CARGO BAY BAFFLE BS 460 - 480 LBL 25 HAS ELONGATED HOLE ; / [01] EVALUATED DAMAGED HOLES AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOSDR SWAA2022010546892Baffle · elongatedFWD CARGO BAY BAFFLE BS 440 - 460 LBL 25 HAS ELONGATED HOLE ; / [01] EVALUATED DAMAGED HOLES AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOSDR SWAA2022010546894Baffle · elongatedFWD CARGO BAY BAFFLE BS 500C-500D RBL 25 HAS ELONGATED HOLE. EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. LOCATED AND DRILLED NEW FCB BAFFLE BS500C-BS500D; RBL 25 PER DWG 143A7505 AND SRM 51-40-02-0G-0. OK TO INSTALL; [07] VERIFIED LSDR SWAA2022010446717Stringer Clip · crackedSTRINGER CLIP CRACKED BS 294.5 STRINGER 13 LT ; / [01] REMOVED STRINGER CLIP AT BS 294.5 STR. 13 L/H IAW SRM 51-40-01 PARA. 4 AND FIG 8. FABRICATED NEW STRINGER CLIP USING 7075T62 LOT #1464682-1 PER DWG. #141A1311; [02] VERIFIED CORRECTIVE ACTION 1; [03] APPLISDR SWAA2022010446719Support · crackedFLOOR SUPPORT CRACKED BS 312+10 TO 312+11 BL 0 WL 208 ; / [01] CORRECTION TO FAULT: FLOOR SUPPORT CRACKED BS 312+10 TO 312+11 LBL45 WL 208; [02] REMOVED DAMAGE FLOOR SUPPORT BS 312-328 LBL45 WL 208 IAW SRM 51-40-02-0G-0.; [03] CERTIFIED REMOVED OF DAMAGE FLOORSDR SWAA2022011146358Counterweight · corrodedRUDDER COUNTER BALANCE WEIGHT HAS CORROSION ; / [01] REMOVED AND REPLACED RUDDER COUNTER-BALANCE WEIGHT IAW CMM55-40-09 STEP 2.C.(2)(B) PAGE302 AND STEP 2.C.(3)PAGE704. SRM 51-60-07-0G-0 STEP5.A.(6)(C)1)2)<BR>CAL TOOL:<BR>ID#4077A; S/N 0297200716; [02] VERIFIESDR SWAA2022011046357Skin · corrodedMULTIPLE AREAS OF CORROSION ON UPPER FUSELAGE SKIN UNDER DORSAL FIN; BS 847-1007; S-2L TO S-2R ; / [01] REMOVED CORROSION ON EXTERNAL FUSELAGE SKIN BS908-BS1000 BETWEEN STR3L-STR3R WL308 I.A.W SRM 51-10-02-0G-0;SRM 53-00-01-1A-1 PAR 4.A(2)(A) FIG.103/ALLOWABLESDR SWAA2022011046355Skin · crackedLEFT HAND HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK MEASURING APPROXIMATELY ONE INCH IN LENGTH AT STAB STATION 193.90 APPROXIMATELY 18.5 INCHES FROM REAR SPAR. / [01] REMOVED CRACK DAMAGE LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 APPROXIMATELSDR SWAA2021122346467Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-520672 / [01] REPLACED FLOOR PANEL 221BF AT PASSENGER CABIN IAW B737-700 AMM 52-21-00-400-801; [02] COMPLETEDSDR SWAA2021122346470Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221GF AT PASSENGER CABIN ; 2021-520674 / [01] REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN IAW B737-700 AMM 53-21-00-400-801; [02] VERIFIED TASK COMPLETESDR SWAA2022011046343Support Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT AFT CARGO BAY BS947 LBL6; RBL12; RBL14; RBL20. MARKED. ; / [01] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORROSION FOUND OUT OF LIMITS DUE TO NO LIMITS STSDR SWAA2022011046319Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS727C+17; BS747 LBL17. MARKED. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+17; FOUND 0.015 REMOVED FROM ORIG 0.071 IN A 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; SDR SWAA2022011046339Intercooler · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS788; BS787+8 RBL7. MARKED. ; / [01] EVALUATED CORROSION ON INTERCOSTAL; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION SDR SWAA2022011046336Intercostal · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS767+2 RBL7 ; / [01] EVALUATED CORROSION ON INTERCOSTAL; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] RSDR SWAA2022011046334Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727D+7 - BS767 RBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PSDR SWAA2022011045869Support Channel · corrodedCORROSION ON MULTIPLE AREAS ON TOP SURFACE OF VIEWPORT CHANNEL BS 261.5 TO BS 268.5; LBL 2.6 TO RBL 2.6; WL 207.5. ; / [01] REMOVED CORROSION ON VIEWPORT CHANNEL SUPPORT BS261.5-BS268.5 LBL3-RBL3 WL207 ON NUTPLATES HOLES LOCATION REMAINING MATERIAL THICKNESS ISDR SWAA2022011046337Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS803 - BS831 RBL26. MARKED. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 810 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-6SDR SWAA2022011046332Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727+8; BS727+12; BS727B+10; BS727B+14; BS727C+14 LBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+7' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNSDR SWAA2022011046321Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS847+9 RBL21. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORROSION FOUND OUT OF LIMITS DUE TO NO STATED LIMITS IN SRM; [03] LOCATED AND DRILLED NEW SDR SWAA2022011046335Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS807 - BS747 LBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 767 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SDR SWAA2022011046009Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER L=0.35IN X W=0.35SDR SWAA2022011046008Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STA 129.50 TO ACCESS REPAIRS IAW SRM 51-40-02-0G-0.; [02] CUT AND REMOVED CRASDR SWAA2022011046010Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER L=0.55IN X W=0.35SDR SWAA2022010546318Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R RBL22 WL153. CRACK ON STRINGER WAS FOUND TO 1.0' LENGTH AND IS OUT OF LIMITS PER SRM 53-00-03-1A-1. APPLIED PRIMER TO REPAIR PARTS IAW SRM 53-00-03-2R-1, AMM 51-21-72-370-804. VERIFIED APPLIED PRIMER TO REPASDR SWAA2021122746023Access Panel · crackedCRACK ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING ; 2021-520600 / [01] REPLACED ACCESS PANEL 532NB INDICATOR FUEL FLOAT AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11.; [02] VERIFIED TASK COMPLETESDR SWAA2022011045864Web · corrodedFWD CARGO BAY SUB THRESHOLD CORROSION; MEASURED BS440 TO AFT; BS440+14; +16; +18; +21-29; +30-31; +33; +36.5; AND +38.5 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 440+18 RBL 29 WL 156. FOUND 0.015 TO BE REMOVED FROM ORIG SDR SWAA2022011045868Support Angle · corrodedFWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT ANGLE CORROSION; LBL23; BS460+10; BS480+6; BS500-2 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 460+10 LBL 23 WL 156. FOUND 0.015 TO BE REMOVED FROM ORIG 0.040 IN 1'X1' AREAS. FOUSDR SWAA2022011045865Shield · corrodedFWD CARGO BAY AFT FLOOR TO SIDEWALL SHIELD; RBL23; BS500+2; +6; +10; +18 ; / [01] EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION 1. <BR><BR>NOSDR SWAA2022011045866Support · corrodedFWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED RBL23; BS500A+2; +4; +6; +10;+14.5; +18.5; +26.5; +43; +45.5; +47.5; ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+6 RBL 23 WL 156. FOUND 0.015 TO BE REMOVED FROM ORISDR SWAA2022011045867Support · corrodedFWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED RBL23; BS 500+50; +52 ; / [01] CORRECT LOCATION OF DAMAGE IS BS 500C+10 AND 500C+12; RBL 23 WL 156. EVALUATED CORROSION AND FOUND DEEPEST LOCATION TO BE AT BS 500C+12 IN A 1'X1' AREA REMOVED 0.015 FROM ORIG SDR SWAA2022010645682Support Fitting · crackedRIGHT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED; WL160; RBL6; BS545; AFT ATTACH POINT ; / [01] REMOVED AND REPLACED RIGHT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED;WI160;RB16;BS545;AFT ATTACH POINT PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01.; [02] SDR SWAA2022010645683Support Fitting · crackedLEFT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED; WL160; LBL6; BS545; AFT ATTACH POINT ; / [01] REMOVED AND REPLACED LEFT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED;WI160;RB16;BS545;AFT ATTACH POINT PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01.; [02] VESDR SWAA2022010645499Panel · crackedPANEL 195CL AFT EDGE RADIUS CORNER IS CRACKED. ; / FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B (6)REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 AS DIRECTED PER SRM 53-40-70-2R-1 PAR 4.B (2) AND TABLE 202;REMOVED DAMAGED SDR SWAA2022010545681Angle · brokenLOWER KEEL BEAM PANEL ATTACH ANGLE BROKEN; BS552; LBL6; WL140 ; / [01] REPLACED KEEL BEAM PANEL ATTACH ANGLE BS 552 LBL 6 IAW SRM 51-40-02-0G-0;IPC 53-12-11-25; [02] VERIFIED CORRECTIVE ACTION 2SDR SWAA2021112942921Support Bracket · corrodedCORROSION SUPPORT BRACKET LOCATED ON DOOR 315A AFT POSITION ON APU COMPARTMENT ; 2021-496960 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DASDR SWAA2021112942922Bracket · corrodedCORROSION SUPPORT BRACKET LOCATED ON DOOR 315A FWD POSITION ON APU COMPARTMENT ; 2021-496959 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DASDR SWAA2021112940701None · crackedCRACK ANGLE - SUPPORT LOCATED AT BS 807 AT LEVEL S-25R AFT CARGO COMPARTMENT ; 2021-496920 / [01] INSTALLED ANGEL-SUPPORT LOC. AT BS807 AT LEVEL STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DWG 146A8120 SHEET 10 REV A PART USED:146A8125SDR SWAA2021112940702Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AFT CARGO COMPARTMENT ; 2021-496918 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG #1SDR SWAA2021112940700Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 847 AND BS 727 S-25L AT WL 156 AFT CARGO COMPARTMENT ; 2021-496919 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 847 AND BS 727 S-25L AT WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 53-00-5
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