Boeing 737-7Q8
Service difficulty reports · 3,961
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 = '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 SWAA2024041661382Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727D & 727C, WL155.5, LBL 21. THE CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.SDR SWAA2024041661383Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727D & 727C, WL155.5, RBL 21. FAULT RESOLVED ON TTG8Q00S1KR6.SDR SWAA2024041661384Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727E - 727D, WL155.5, LBL21. R & R THE CHANNEL IAW SRM 51-40-02-0G-0, & DWG 146A7500.SDR SWAA2024041661385Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727E & 727D, WL155.5, RBL21. FAULT RESOLVED ON TTG8Q00S1KR6.SDR SWAA2024041661386Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE. FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 767 & 727E, WL155.5, LBL 21. THE Z CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.SDR SWAA2024041661387Channel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 767 & 727E, WL155.5, RBL 21. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G-0, & DWG 146A7500.SDR SWAA2024041661389Channel · corrodedAFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 807 & 767 WL155.5 LBL21. THE Z CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.SDR SWAA2024041661390Shield · corrodedAFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 787 AND 767, WL155.5, RBL21. R & R THE SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081.SDR SWAA2024041661376Attach Angle · missingFWD CARGO AFT BULKHEAD SUPPORT STRUCTURE, BS 500D, STR 19R HAS AFT ATTACHED ANGLE MISSING. INSTALLED A NEW AFT ATTACHED ANGLE AT FWD CARGO AFT BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0, & DWG 143A7902. INSPECTED IAW SRM 51-40-02-0G-0-A00729.SDR SWAA2024041660508Cover · tornFORWARD GALLEY R1 DOOR GIRT BAR COVER TORN. REMOVED AND INSTALLED THE R1 SLIDE WILL BE ACCOMPLISHED ON T/C REF SA-M/MT 725-61-06.SDR SWAA2024041660522Skin · crackedR/W MOVEABLE SLAT NO-7 L/E NOSE SKIN ACTUATOR ATTACHED RIB APPEAR CRACKED @ FASTENER HEADS MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR OF DAMAGE FOUND AT RT WING SLAT #7 NOSE SKIN AT ACTUATOR ATTACHING AREA PER REF B737 SRM 57-42-01-2R-8;[02] VERIFIED STEP 1; RSDR SWAA2024041260509Floor Panel · delaminatedCABIN FLOOR PANEL #231XF DELAMINATED<[01] RECEIVED NEW PANEL 231XF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFZ04;[02] VERIFIED STEP 1SDR SWAA2024041260512Floor Panel · delaminatedCABIN FLOOR PANEL #231ZF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 231ZF ; THIS PANEL WILL BE INSTALL ON FAULT TTG8Q00RFYXXSDR SWAA2024041260513Floor Panel · delaminatedCABIN FLOOR PANEL #241DF DELAMINATED.<[01] RECEIVED NEW PANEL 241DF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFYUK;[02] VERIFIED STEP 1.SDR SWAA2024041260514Floor Panel · delaminatedCABIN FLOOR PANEL #241AF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 241AF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFYUT;[02] VERIFIED STEP 1.SDR SWAA2024041659831Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 140CF HAD A SMALL CRACK. CUT & REMOVED THE DAMAGED AREA IAW SRM 53-00-53-2R-1 & SRM 51-10-02-0G-0. COMPLETED FABRICATION OF NEW REPAIR PARTS IAW SRM 53-00-53-2R-1. INSTALLED NEW REPAIR IAW SRM 53-00-53-2R-1 & SRM 51-40-02-SDR SWAA2024031259279Battery Pack · inoperativeEMERGENCY LIGHT IS NOT COMING ON AT R2 DOOR HEADER PANEL.<[01] REMOVED AND REPLACED BATTERY PACK (M1673). OPERATIONAL TEST PASSED PER REF AMM 33-51-06-960-805.PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801. TEST PASSED.;[02] CERTISDR SWAA2024031259278Battery Pack · inoperativeL2 DOOR EXTERIOR EMERGENCY LIGHT DOESN'T ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK (M1672). OPERATIONAL TEST PASSED PER REF AMM 33-51-06-960-805.PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801. TEST PASSED.;[02] CERTIFIED SDR SWAA2024030759128Battery Pack · inoperativeRIGHT SIDE INTERIOR EMERGENCY OVER WING EXIT LIGHT AND 3 FORWARD OVERHEAD BIN EXIT LIGHTS INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)] AND REPLACED BATTERY PACK REF AMM 33-51-06. OP CHESDR SWAA2024031358939Slide · tornR2 DOOR MOUNTED ESCAPE SLIDE LOWER FWD SECTION IS TORN.<[01] REMOVED AND REPLACED R-2 DOOR MOUNTED SLIDE ON JOB CARD [TTG8Q00RXW8Q].;[02] VERIFIED STEP 1 REPLACEMENT OF R-2 DOOR MOUNTED SLIDE ON JOB CARD [TTG8Q00RXW8Q].SDR SWAA2024030157367Seal · crackedTAIL - LEFT HORIZONTAL FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT UPPER FWD HORIZONTAL SLIDING SEAL IAW BOEING 737 AMM 53-31-31SDR SWAA2024030157368Seal · crackedTAIL - RIGHT HORIZONTAL FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT FWD UPPER HORIZONTAL SLIDING SEAL IAW BOEING 737 AMM 53-31-31SDR SWAA2024031355757Panel · crackedCRACKED BREAK ASSY PANEL AT MAIN CABIN CENTER SECTION STA 537.5 BETWEEN RBL 45.5 TO RBL 65<[01] REMOVED AND REPLACED BREAK PANEL ASSY AT MAIN CABIN CENTER SECTION STA 537.5 BETWEEN RBL 45.5 TO RBL 65 AS-PER SRM 51-40-02-0G-0;[02] CORRECTION TO STEP 1 SHOULD RESDR SWAA2024022655965Actuator · out of adjustSEAT 11D RECLINES INTO EXIT ROW<[01] ADJUSTED SEAT 11D RECLINE ACTUATOR PER AMM 25-22-00 OPS CHECKS GOODSDR SWAA2024031354836Scuff Plate · crackedAFT CARGO DOOR SCUFF AFT CORNER FITTING BROKEN. CORRECTION FAULT. AFT CARGO DOOR SCUFF PLATE AFT CORNER CRACK<[01] ACCOMPLISHED WELD REPAIR OF AFT CARGO DOOR SCUFF PLATE AFT CORNER BY OUTSIDE VENDOR; FAA REPAIR STATION NUMBER JLWR146K. AS PER SRM 51-60-15-2R-1SDR SWAA2024031354837Scuff Plate · crackedAFT CARGO DOOR SCUFF FWD CORNER FITTING IS CRACK. CORRECTION FAULT. AFT CARGO DOOR SCUFF PLATE FWD CORNER IS CRACK<[01] LOCATED AND DRILLED NEW AFT CARGO DOOR SCUFF PLATE FWD CORNER AS PER SRM 51-40-05-0G-0. SCUFF PLATE WILL BE INSTALLED IN THE ITEM TTG8Q003CMSDR SWAA2024031256859Access Panel · crackedLOWER FUSELAGE AFT ACCESS PANEL # 193D HAS CRACKED FASTENER HOLES<[01] ACCOMPLISHED PERMANENT REPAIR ON DAMAGED HOLES AT LOWER FUSELAGE AFT ACCESS PANEL 193D AS PER B737-700 SRM 51-70-04-2R-0 PARAGRAPH 4.N;[02] VERIFED STEP 1SDR SWAA2024022153698Girt Bar · exposedAFT ENTRY DOOR EXCESSIVE GIRT BAR EXPOSED<[01] RE-ADJUSTED SLIDE PER AMM 25-66-01SDR SWAA2024031453580Panel · elongatedRIGHT WING T/E PANEL 661BB HAS ELONGATED HOLE. MARKED WITH DOT.<[01] REPAIRED RIGHT WING T/E PANEL 661BB; AS PER SRM 51-70-04-2R-9; MATERIAL USED PO#1608196 AND PO#2040614;[02] VERIFIED STEP 1.SDR SWAA2024031452972Channel · corrodedDURING CORROSION REMOVAL FOUND AFT CARGO L/H SIDEPLATE SUPPORT ZEE WITH MULTIPLE ELONGATED HOLES AT NUTPLATES ATTACHED POINTS SECTION BETWEEN STA 747+12.5' AND STA 847 LBL 21'<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTSDR SWAA2024031452973Channel · corrodedDURING CORROSION REMOVAL FOUND AFT CARGO L/H SIDEPLATE SUPPORT ZEE WITH MULTIPLE ELONGATED HOLES AT NUTPLATES ATTACHED POINTS SECTION BETWEEN STA 727 AND STA 747+12.5' LBL 21'<[01] REMOVED AND REPLACED LH Z-CHANNEL FROM STA 727 TO 847 LBL 21 PER SRM 51-40-02-0SDR 2024F00034Packing · leakingENGINE #1 OIL QUANTITY INDICATION LOW SHOWS 11 VERSUS 16 ENGI#2 FRM 79007051. CORRECTIVE ACTION: ENGINE STARTER REMOVED AND REPLACED.SDR SWAA2024030155747Support Angle · elongatedELONGATED HOLE ANGLE - SUPPORT LOCATED BS 440 AND S-22R AT FWD CARGO COMPARTMENT 2024-77444<[01] REPLACED NEW SUPPORT ANGLE AND FASTENERS LOCATED BS 440 AND S-22R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A8200 SHEET 43 REV-.SEE INDIVIDUAL SDR SWAA2024031451324Stiffener · crackedLOWER FUS. WING CENTER SECTION REAR SPAR STIFFENER CRACKED @ LOWEER RADIUS O/B OF L/H RAM AIR EXIT EXHAUST DUCT STA 663.75.MKD DOT<[01] REMOVED AND INSTALLED NEW STIFFENER AT LOWER FUS. WING CENTER SECTION REAR SPAR STIFFENER RAM AIR EXIT EXHAUST DUCT STA 663.SDR SWAA2024031450848Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 727 TO STA 727B LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450849Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 727B TO STA 727C LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1 FINALSDR SWAA2024031450850Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 727C TO STA 727D LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450851Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 727D TO STA 727E LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450852Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 727E TO STA 747 LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450845Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 747 TO STA 767 LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450846Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 767 TO STA 787 LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450853Channel · corrodedCORROSION FOUND AFT CARGO LH 'Z' CHANNEL FROM STA 787 TO STA 807 LBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] LH Z-CHANNEL FABRICATED FROM STA 727-847 LBL 21 WL 155.5 REFERENCE TASKCARD# TTG8Q00RLL1W;[02] VERIFIED STEP 1SDR SWAA2024031450708Support · crackedMAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN CENTER WING @ LBL 1STA 540 AS-PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.;[03] IN ADDITION TO STEP 1: REMOVED AND REPLACED FLOOR SUSDR SWAA2024031248861Doubler · crackedGROUND POWER DOOR INTERNAL DOUBLER TORN;CRACK FWD LOWER CORNER<[01] ACCOMPLISHED PERMANENT REPAIR CATEGORY B AT EXTERNAL POWER RECEPTACLE CUTOUT AS PER B737-700 SRM 53-10-15-2R-5 REPAIR 5. REF TO STEP 13 FOR FURTHER INSPECTION REQUIREMENTS.;[02] VERIFIED FINALSDR SWAA2024031148706Strap · corrodedRIGHT OVER WING ESCAPE LINE IS WET ALIGHT CORROSION. ITS HOOK LATCH LOCK FINGER IS WORN WITH SIDE PLAY.<[01] REMOVED AND REPLACED RIGHT OVER WING ESCAPE STRAP REF BOEING 737 AMM 25-61-10-000-802;25-61-10-400-802 <BR>TORQUE WRENCH B/C 175285<BR>DUE DATE 19-JUN-SDR SWAA2024031354555Panel · corrodedAREA ON PNL 192F UNDER MARKER BEACON ANTENNA HAS CORROSION.<[01] RECIEVED NEW PANEL PO#2043476; REF TASK CARD TTG8Q00QQ36V FOR PANEL INSTALLATION.;[02] VERIFIED STEP 1.SDR SWAA2024031354556Panel · corrodedAREA ON PNL 192F UNDER DME #2 ANTENNA HAS CORROSION.<[01] REF TASK CARD TTG8Q00RC9UP FOR RECIEVING NEW PANEL.;[02] VERIFIED STEP 1.SDR SWAA2024022948456Access Panel · crackedCRACK ON MARKER BEACON ANTENNA ACCESS PANEL 192F BODY STATION 616 AT KEEL BEAM. REPLACED MARKER BEACON ANTENNA PANEL 192F AT LOWER FUSELAGE I.A.W B737-700 AMM 34-32-11-401-NG; PERFORMED TEST OF THE MARKER BEACON ANTENNA; TEST IS OK.SDR SWAA2024022948454Frame · crackedCRACK FRAME ON BS 947.5 BTW STR26L TO STR27L AFT CARGO COMPARTMENT 2024-77399<[01] REPLACED FRAME AND FASTENERS LOCATED BS 947.5 BTW STR 23R TO STR 23L IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. DWG 147A1047 REV:-; DWG 147A0040 REV:A AND DWG 147A0002 REV:SDR SWAA2024022948455Fitting · crackedCRACK ON FITTING LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT. REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 6 REV-.
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