Boeing 737-73V
Service difficulty reports · 1,826
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 = '73773V' 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 = '73773V' 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 SWAA2026062213876Sign · detachedFORWARD ENTRY DOOR EXIT SIGN DETACHED. REATTACHED EXIT SIGN IAW AMM 33-51-01.SDR SWAA2026060808664Light · inoperativeCENTER AISLE AT SEAT 26ABC CEILING MOUNTED EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-03.SDR SWAA2026060808676Isolation Mount · crackedFWD SERVICE DOOR AFT ISOLATOR CRACKED. R & R FWD SERVICE DOOR AFT ISOLATOR IAW SRM 51-40-02. INSPECTION C/W R&R FWD SERVICE DOOR AFT ISOLATOR IAW SRM 51-40-02.SDR SWAA2026020566836Doubler · crackedEXTERNAL GROUND POWER RECEPTACLE DOUBLER DAMAGED. REMOVED DAMAGED SECTION OF DOOR SURROUND DOUBLER IAW SRM 53-10-15-2R-4, ZONE 2 ALTERNATIVE 2, PERFORMED HFEC SURFACE CRACK INSPECTION IAW NDT PART 6 51-00-00, P23. RREPAIRED IAW SRM 53-10-15-2R-4, ZONE 2, ALSDR SWAA2026020567948Weep Hole · blockedNR 1 ENGINE WOULD NOT SPOOL UP FOR TAKEOFF . N1 WOULD NOT SPOOL UP, N2 WOULD. FOUND NR 1 ENGINE PS3 SENSE LINE WEEP HOLE BLOCKED. CLEANED IAW AMM 72-00-00. ENGINE RUN UP NORMAL.SDR SWAA2026011961618Light · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING LIGHT IAW AMM 33-51-04.SDR SWAA2025082608019Slide · unpackedAFT RIGHT EGRESS SLIDE NEED TO BE REPACKED. REPOSITIONED SLIDE IN CONTAINER PER MT 725-61-06.SDR SWAA2025073195500Anti-Skid Valve · out of limitsANTI-SKID INOP ILLUM ON APPROACH<[01] PERFORMED ALT ANTI-SKID VALVE T/S REF FIM 32-42 TASK 805. FOUND R/H ALT ANTI-SKID VALCE OUT OF RESISTANCE. REMOVED AND REPLACED R/H ANTI-SKID VALVE REF AMM 32-42-31. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR SWAA2025070882301Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 167.<[01] REPAIRED VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 BETWEEN RBL 5 TO RBL 20 WL 167 PER SRM 57-10-10-2R-5 REPAIR 5.;[02] REPAIRED BS 663 UPPER ATTACH ANGLE AT RBL 10 WLSDR SWAA2025070882393Floorbeam · crackedCRACKED ANGLE ON FLOOR SUPPORT WING CENTER SECTION STA 685+7 LBL 23 WL 203 (MARKED)<[01] REMOVED AND REPLACED ANGLE ON FLOOR SUPPORT WING CENTER SECTION STA 685+7 LBL 23 WL 203 PER SRM 51-40-02-0G-0 AND BOEING DWG 273A9110 REV: A.;[02] VERIFIED CORRECTIVE ACTISDR SWAA2025070882120Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. RESTORED FINISHES ON INNER SURFACE PER AMM 51-21-41-370-802; AMM 51-21-72-370-804.SDR SWAA2025070782119Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED NEW FCB AFT CORNER SCUFF PLATE IAW SRM 51-40-05 AND DWG143A8331;[02] LOCATED AND DRILLED NEW FCB AFT CORNER SCUFF PLATE IAW SRM 51-40-05 AND DWG143A8331.<BR>PART WILL BE INSTALLED ON CUSTOMESDR SWAA2025070781514Threshold Web · corrodedCORROSION ON FCB DOOR CUTOUT SURROUND SUB-THRESHOLD BS460+5, RBL29, WL156. REMOVED AND REPLACED ON FCB DOOR CUTOUT SURROUND SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330 REV:A.SDR SWAA2025070880894Door · crackedL/H MLG STRUT DOOR IS CRACKED<[01] L/H MAIN LANDING GEAR STRUT DOOR REPAIRED ON WORK ORDER P007K2E9-1 JOB #583943.<BR>REMOVED AND REINSTALLED L/H MLG STRUT 'CENTER' DOOR IAW AMM 32-13-11;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2025061180307Battery Pack · failedR/H FWD. EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED & REPLACED R/H FWD EMERGENCY LIGHTING BATTERY PACK PER AMM 33-51-06.SDR SWAA2025060376794Cover · missing9C EMER LIGHT LENS COVER MISSING <[01]. OK TO CONTINUE PER MEL 33-15-02 SP1 SECURED WITH TAPE; [02] INSTALLED EMERGENCY LIGHT COVER AT SEAT 9C PER SIP.SDR SWAA2025060275376Lamp · inoperativeL/H EMERGENCY EXIT LIGHT INOP<[01] RELAMPED EMERGENCY EXIT LIGHT IAW AMM 33-51-01. OPS CKD GOOD.SDR SWAA2025051971617Floor Panel · crackedRAMP REPORTED AFT CARGO FLOOR PANEL CRACK<[01] OK TO CONTINUE PER MEL 25-16-01; SP#1B. AUTH#252257;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)]SDR SWAA2025050164931Doubler · crackedTRANSFERRING WORK FROM FAULT TTG8Q01034TE: EXTERNAL POWER CUTOUT CRACK FOUND ON AFT SECTION OF CUTOUT.<[01] REMOVED -1 DOUBLER AND -2 FILLER FROM PREVIOUSLY ACCOMPLISHED SRM 53-10-15-2R-4 REPAIR FROM AFT SECTION OF EXTERNAL POWER CUTOUT PER SRM 51-40-02.;[02] SDR SWAA2025050164932Doubler · crackedEXTERNAL POWER CUTOUT CRACK FOUND ON LOWER SECTION OF CUTOUT.<[01] RR?D REPAIR DOUBLER PER SRM 53-10-15-2R-4SDR SWAA2025043064609Doubler · damagedEXTERNAL POWER CUTOUT LOWER AND AFT SECTION HAS SHARP EDGES<[01] REMOVED -1 DOUBLER AND -2 FILLER FROM PREVIOUSLY ACCOMPLISHED SRM 53-10-15-2R-4 REPAIR PER SRM 51-40-02.SDR SWAA2025043064610Doubler · crackedFOUND CRACK ON EGPR SURROUND DOUBLER FWD SIDE UNDER LOWER HINGE<[01] REPAIRED PER EA 25-153-01072; REF TTG8Q0103QYZ AND TTG8Q01048AL FOR WORK ACCOMPLISHED;[02] REPAIRED PER EA 25-153-01072; REF TTG8Q0103QYZ AND TTG8Q01048AL FOR WORK ACCOMPLISHEDSDR SWAA2025013091376Girt Bar · looseFLIGHT ATTENDANT REPORTS THAT THE AFT ENTRY DOOR GIRT BAR IS LOOSE<[01] SECURED AFT ENTRY DOOR GIRT BAR PER S.I.P.SDR SWAA2025011685446Light · inoperativeEMERGENCY LIGHT ON THE AFT RECESSED PANEL IS INOP<[01] RELAMPED EMERGENCY LIGHT ON THE AFT RECESSED PANEL; PERFORMED GOOD TEST PER AMM 33-51-03-960-801.<BR>TASK CARD COMPLETED;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025011685544Bulb · inoperativePASSENGER CABIN RH OVERWING EMERGENCY EXIT LIGHT INOP.<[01] RELAMPED INOP BULBS IN R/H OWE OVERHEAD SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED INSTALLATION. AND OPS CHECK.SDR SWAA2025011679949Angle · crackedL-CLIP CRACKED ON FWD EDGE OF PANEL 651FB CRACKED; 29' FROM O/B EDGE OF PANEL<[01] REMOVED AND REPLACED L-CLIP ON FWD EDGE OF PANEL 651FB; 29' FROM O/B EDGE IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025011579953Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF TOP SURFACE DELAMINATED<[01] FLOOR PANEL 241AF WITH TOP SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0008;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025011579951Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231XF TOP SURFACE DELAMINATED<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025011579952Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241DF TOP SURFACE DELAMINATED<[01] FLOOR PANEL 241DF WITH TOP SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND 144A5810 ID:0009;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025011579958Floor Panel · delaminatedPANEL 241EF HAS DELAMINATION ON FRONT EDGE AND OUTBOARD AFT EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] PANEL 241EF HAD DELAMINATION ON FRONT EDGE AND OUTBOARD AFT EDGE CORNER TOP PLY FIBERGLASS REPAIRED IAW SRM 53-00-50-2R-0 ALONG WITH DWG: 1445810 SHEET: 23SDR SWAA2025011582995Floor Panel · damagedPANEL 242AF HAS FRAYED TOP PLY FIBERGLASS (MARKED)<[01] ATTACHED PLACARDS TO FWD AND AFT UPPER SURFACE AREAS USING BAC27DCA854 LOT # 1589317-1 IAW BOEING DWG: 144A5810 ID: 0189.<BR><BR>FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SDR SWAA2025011582996Floor Panel · damagedPANEL 241BF HAS FRAYED TOP PLY FIBERGLASS (MARKED)<[01] ATTACHED PLACARDS TO FWD AND AFT UPPER SURFACE AREAS USING BAC27DCA854 LOT # 1589317-1 IAW BOEING DWG: 144A5810 ID: 0189.<BR><BR>FABRICATION OF NEW 241BF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SDR SWAA2025011579957Floor Panel · delaminatedPANEL 242AF HAS DELAMINATION ON FRONT EDGE AND OUTBOARD FWD EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] FLOOR PANEL 242AF NEW PANEL FABRICATION ACCOMPLISHED ON FAULT TTG8Q00XRELR;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025011579959Floor Panel · delaminatedPANEL 241FF HAS DELAMINATION ON FWD INBOARD EDGE CORNER TOP PLY FIBERGLASS (MARKED)<[01] DAMAGE TO PANEL 241FF WAS FOUND TO BE OUT OF ECONOMICAL REPAIR; NEW FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED JOB COMPLETESDR SWAA2025011679649Scuff Plate · crackedACB CRACKED AFT CORNER SCUFF PLATE<[01] REPAIRED ACB AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. REFERRED TO BAC5975. EQUIPMENT USED: WELDING MACHINE ID# 10583; CAL DUE 01/2025. APPLIED CHEMICAL CONVERSION COATING AND TWO LAYERS OF PRIMER PER SOPM 20-43-03; SDR SWAA2025011679650Door · crackedLEFT HAND MAIN LANDING GEAR CENTER DOOR IS CRACKED (MARKED)<[01] REMOVED LEFT HAND MAIN LANDING GEAR CENTER DOOR IAW AMM 32-13-11-000-804;[02] UPDATED STEP 1;[03] UPDATED STEP 1;[04] COMPLETED STEP 1;[05] UPDATED PARTS;[06] COMPLETED STEP 2.;[07] SUMMARY STATESDR SWAA2025011679645Scuff Plate · crackedFCB FWD SCUFF PLATE CRACKED<[01] REMOVED ALL THE COATINGS FROM THE CORNER SCUFF PLATE APPROXIMATELY 1 INCH AWAY FROM THE WELD AREA PER SRM 53-30-15-2R-1 PARA 4.B.(2). REFERRED TO SOPM 20-30-02. WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1SDR SWAA2025011679646Web · corrodedFWD CARGO DOOR CUTOUT SURROUND; CORROSION ON TRESHOLD WEB (AS MARKED)<[01] REMOVED AND REPLACED FCB SUB-THRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330 REV:A;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025011679648Scuff Plate · crackedACB CRACKED FWD CORNER SCUFF PLATE<[01] REPAIRED ACB CRACKED FWD CORNER SCUFF PLATE PER SRM WELDED THE ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1. REFERRED TO BAC5975 EQUIPMENT USED: WELDING MACHINE ID# 10583; SDR SWAA2025012079276Panel · crackedCRACKED AFT DOOR SURROUND PANEL FSD (MARKED)<[01] REPAIRED AFT DOOR SURROUND PANEL FSD IAW CMM 25-00-66 PG. 601-602 REPAIR 1-2 SECT. 2.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024120968444Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968445Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968446Tank Unit · out of limitsSUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROSDR SWAA2024120968447Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968448Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968449Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968450Tank Unit · out of limitsMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLESDR SWAA2024120968451Tank Unit · out of limitsSUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROSDR SWAA2024120968452Tank Unit · out of limitsSUPPLEMENTAL INFORMATION: MID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROSDR SWAA2024120974349Fuel Tank · abnormalMID FLIGHT NOTICED ABNORMAL FUEL DECREASING. NOTICED UP TO 700 LBS FUEL IMBALANCE. NO TRANSFER OF FUEL FROM TANK TO TANK. NO 1 TANK LOW. PHX PERFORMED COMPARISON CHECK & VERIFIED #1 TANK IS 700 LBS LOW. NEEDS THE BOX HOOKED UP FOR TROUBLESHOTING. AFTER TROUBLE
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