Boeing 737-7K9
Service difficulty reports · 794
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 = '7377K9' 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 = '7377K9' 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 SWAA2024102851327Assist Handle · looseCUSTOMER WALK - BOTH DOOR ASSIST HANDLES AT THE R1 DOOR LOOSE<[01] INSTALLED 2EA DOOR ASSIST HANDLES ON R-1 DOOR AS PER AMM 52-41-31-400-802;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102851328Assist Handle · looseCUSTOMER WALK - R2 DOOR ASSIST HANDLE LOOSE<[01] INSTALLED R2 DOOR ASSIST HANDLE AS PER AMM 52-41-31-400-802;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102848915Cover · out of positionG1 GALLEY EXIT SIGN COVER POINTING TOWARD THE COCKPIT<[01] REMOVED AND REINSTALLED G1 GALLEY EXIT SIGN COVER AS PER REF AMM 33-51-01-960-801;[02] VERIFIED STEP 1SDR SWAA2024102848179Battery Pack · inoperativeFOR TROUBLESHOOTING PURPOSES; FOUND SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED TROUBLESHOOTING AS PER B737 WDM 33-51-11; WDM 33-51-12; WDM 33-51-13; WDM 33-51-14; WDM 33-51-21; AND WDM 33-51-22. FOUND M2335 AND M1668 EMERGENCY ESDR SWAA2024103147341Web · crackedREJECT: CRACKED NEW WEB AND ELONGATED HOLES ON BRACKETS; BILGE AREA BTW BS500 TO BS500A AT LEVEL STR 26L FWD CARGO COMPARTMENT. 2024 - 597224 REJECT: CRACKED NEW WEB AND ELONGATED HOLES ON BRACKETS; BILGE AREA BTW BS500 TO BS500A AT LEVEL STR 26L FWD CARGO COMSDR SWAA2024102844043Panel · damagedLEFT WING UPPER SURFACE PANEL 571AT; I/B AFT CORNER UPPER SURFACE HOLE FASTENER ELONGATED<[01] APLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #571AT AS PER B737 51-70-04-2R-0 PARAG 4-N-2 MATERIAL USED: RESIN 3804 PO#2066573; FIBERGLASS PO#1690463 ANSDR SWAA2024110543315Tie Clip · crackedCRACK TIE CLIP LOCATED 277 AND S-10R AT PASSENGER CABIN 2024-597164<[01] REPLACED TIE CLIP LOCATED 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV - DWG 141A8380 SHEET 21 REV- SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACESDR SWAA2024110543030Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 271 LT WING 2024-597163<[01] REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930; SHEET 7; REV -.;[02] REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737SDR SWAA2024110542674Angle · crackedCRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-597135<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 66 REV A.;[02] REPLACED ANGLE LOCATED BS 867 BETWEENSDR SWAA2024110541817Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT 2024-597107<[01] MEASURE OF CRACK: 1.080 INCHES TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N: A21043111 DUE DATE:08-AUG-25. REPLACED ANGLE - SUPPORT LOCATED BS 867 AND S-26L AFT CARGO COMPARTSDR SWAA2024110541820Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2024-597108<[01] REPLACED ANGLE SUPPORT LOCATED ON BS947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 149A8103 SHEET 7 REV A. SEE INDIVIDUAL SIGN OFF BELLOW.;[02] CSDR SWAA2024103141625Hook · corrodedCORROSION EMERGENCY DOOR 833 HOOK ASSEMBLY LIFE LINE AT PASSENGER CABIN 2024-597100<[01] REPLACED EMERGENCY DOOR 833 HOOK ASSEMBLY LIFE LINE AT PASSENGER CABIN IAW BOEING SOPM 20-50-01. REFER TO INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETEDSDR SWAA2024103141626Web · crackedCRACK BILGE AREA WEB BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-597103<[01] REPLACED WEB LOC. ON BILGE AREA BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 37 REV-.SDR SWAA2024110541094Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-596989<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23046084; DUE DATE 23-MAY-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1998072 ; DUE DATE : 23/JAN/25;[03] REPAIRED AFT COSDR SWAA2024110541096Frame · crackedCRACK FRAME WEB LOCATED BS259.5 AND BTW STR8R TO STR9R AT PASSENGER CABIN 2024-597028<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 5;[02] PERFORMED A PERMANENT REPAIR ON FRAME WEB LOCATED BS 259.5 AND BTW STRG 6R TO 11R AT PSDR SWAA2024110540776Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2024-596932<[01] REPLACED STIFFENER LOC. ON FLOOR STRUCTURE BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02-0G AND DWG 143A5240 SHEET 3 REV B.;[02] COSDR SWAA2024110540775Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION 2024-596933<[01] REPLACED STIFFENER LOC. ON FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02-0G AND DWG 143A5240 SHEET 3 REV B. SEESDR SWAA2024110540412Intercostal · damagedELONGATED HOLE WEB - INTERCOSTAL LOCATED BS 500D TO BS 500C AND S-26R AT FWD CARGO COMPARTMENT 2024-596806<[01] REPLACED WEB-INTERCOSTAL LOCATED BS 500D TO BS 500C AND S-26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SHEETS 10 REV. A. SDR SWAA2024110540280Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT CUT OUT 2024-596803<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23046084; DUE DATE 23-MAY-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1998072 ; DUE DATE : 23/JAN/25;[03]SDR SWAA2024110540409Gusset · crackedCRACK GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT 2024-596804<[01] REPLACED GUSSET ANGLE LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902; SHEET 174; REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK SDR SWAA2024110540411Gusset · crackedCRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT 2024-596805<[01] REPLACED GUSSET ANGLE LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02 AND DWG 143A7902; SHEET 174 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02]SDR SWAA2024103139801Floor Panel · crackedCRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2024-596735<[01] FABRICATED FLOOR PANEL 140CF LOC. AT AFT CARGO COMPARTMENT MATERIAL USED ALUMINUM SHEET P/N: 2024-T3 0.071' IAW B737-700 SRM 51-40-05; B737-700 SRM 51-40-08 AND DWG 453A2610 SHEET 11 AND 12 REV SDR SWAA2024102839211Strip · corrodedAFT CARGO COMPARTMENT R/H CAP STRIP CORRODED P/N 453A2611-11<[01] RECEIVED NEW CAP STRIP P/N: 453A2611-11<BR>PO# 2043476<BR>INSTALLATION TO BE ACCOMPLISHED ON TASKCARD # TTG8Q00VT988;[02] VERIFIED STEP 1.SDR SWAA2024102839212Strip · corrodedAFT CARGO COMPARTMENT R/H CAP STRIP CORRODED P/N 453A2611-9<[01] RECEIVED NEW CAP STRIP P/N: 453A2611-9<BR>PO# 2012626<BR>INSTALLATION TO BE ACCOMPLISHED ON TASKCARD # TTG8Q00VT988;[02] VERIFIED STEP 1.SDR SWAA2024102839209Strip · corrodedAFT CARGO COMPARTMENT L/H CAP STRIP CORRODED P/N 453A2611-10<[01] RECEIVED NEW AFT CARGO COMPARTMENT L/H CAP STRIP P/N 453A2611-10 AND INSTALLATION TO BE ACCOMPLISH ON TASKCARD TTG8Q00VT988.;[02] VERIFIED STEP 1.SDR SWAA2024102839210Strip · corrodedAFT CARGO COMPARTMENT L/H CAP STRIP CORRODED P/N 453A2611-8<[01] RECEIVED NEW CAP STRIP P/N: 453A2611-8<BR>PO# 2012626<BR>INSTALLATION TO BE ACCOMPLISHED ON TASKCARD # TTG8Q00VT988;[02] VERIFIED STEP 1.SDR SWAA2024102838586Floor Panel · corrodedAFT/CARGO PNL.# 140CF UPPER SIDE AT OUTTER PERIMITER SHOWS AREAS WITH LITE CORROSION BEGININGS.<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS FOUND OUT OF LIMITS AND ORDERED NEW AFT CARGO FLOOR PANEL 140CF PER SRM 51-10-02-0-0G AND SDR SWAA2024102838590Floor Support · crackedDURING INTERNAL GVI AFT OF FWD CARGO LOOKING UP AND NOTICED CABIN FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540 WATER LINE 208.1 MKD DOT<[01] PARTIALLY INSTALLED CABIN FLOOR SUPPORT BREAK LBL 1 STA 540 WATER LINE 208.1.;[02] CORRECTION TO STEP 1: REMOVED AND REPSDR SWAA2024102838591Floor Support · crackedDURING INTERNAL GVI AFT OF FWD CARGO LOOKING UP AND NOTICED CABIN FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 WATER LINE 208.1 MKD DOT<[01] REMOVED AND REPLACED NEW SUPPORT BREAK PART NO. 143A5240 P.O. NO.2074280 AT CABIN FLOOR STA. 540 RBL 1'' REF SRM 51-40-0SDR SWAA2024102838340Angle · crackedLEFT HORIZONTAL STABILIZERFRONT SPAR INTERNAL RIB # 5 REAR LOWER ANGLE CRACKED MKD DOT LEFT HORIZONTAL STABILIZERFRONT SPAR INTERNAL RIB # 5 STA 129.50 REAR LOWER ANGLE CRACKED MKD DOT<[01] ACCOMPLISHED REPAIR OF LEFT HORIZONTAL STABILIZER FRONT SPAR INTERNAL SDR SWAA2024102838082Floor Support · corrodedCORROSION AFT CARGO SIDE FLOOR SUPPORT SHIELD S-25R STA 847 TO STA 867 MKD<[01] FAULT RESOLVED ON OTHER FAULT. REF. TTG8Q00VV8NZ;[02] VERIFIED STEP 1.SDR SWAA2024102838083Floor Support · corrodedCORROSION AFT CARGO SIDE FLOOR SUPPORT SHIELD S-25R STA 767 TO STA 787 MKD<[01] FAULT RESOLVED ON OTHER FAULT.REF. TTG8Q00VV8MV;[02] VERIFIED STEP 1.SDR SWAA2024102838084Plate · corrodedCORROSION AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB PLATE<[01] AFT CARGO DOOR CUTOUT LOWER SILL WEB IS BEING REPLACED ON TASKCARD TTG8Q00VV97Z.;[02] VERIFIED STEP 1.SDR SWAA2024102537964Attach Angle · crackedFLIGHT DECK R/H AFT BULHEAD INB COMPARTMENT LOWER ATTACHED ANGLE EDGE CRACKED I/B FLOOR PANEL # 211AF MKD DOT<[01] ACCOMPLISHED REMOVAL AND REPLACEMENT OF CRACKED ANGLE AT FLIGHT DECK R/H AFT BULKHEAD I/B COMPARTMENT LOWER POSITION; ADDITIONALLY RESTORED DISTUSDR SWAA2024102837586Bracket · crackedAFT CARGO STA 727 BULKHEAD LOWER CENTER BRACKET CRACK.<[01] REMOVED AND REPLACED AFT CARGO STA 727 BULKHEAD LOWER CENTER BRACKET PER REF SRM 51-40-02-0G.;[02] VERIFIED STEP 1.SDR SWAA2024102837589Angle · crackedAFT CARGO FLOOR STRUCTURE AT STA 867 LBL 10 WL 155.5 ANGLE BRACKET CRACK.<[01] REMOVED AND REPLACED AFT CARGO FLOOR STRUCTURE AT STA 867 LBL 10 WL 155.5 NEW ANGLE BRACKET PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2024102837582Shield · corrodedCORROSION FOUND AFT CARGO RH FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION; CHECKED LIMITS; FOUND OUT OF LIMITS; REMOVED SHIELD; LOCATED AND DRILLED HOLES ON NEW SHIELD; TREATED; PRIMED; APPLIED BMS SDR SWAA2024102837748Scuff Plate · crackedFOUND FWD CARGO FWD SCUFFPLATE CRACKED<[01] RECIEVED FWD CARGO SCUFFPLATE FROM JL WELDING; INC; INSTALLATION WILL BE ACCOMPLISH ON TTG8Q002FEVM;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102837749Scuff Plate · crackedFOUND AFT CARGO AFT SCUFFPLATE CRACK<[01] RECEIVED REPAIRED AFT CARGO SCUFFPLATE <BR>P/N: 146A8341-9<BR>PO# 2074280;[02] VERIFIED STEP 1.;[03] CORRECTED CHART;[04] FINAL INSPECTION; VERIFIED CORRECTION STEP #3.SDR SWAA2024102837588Web · corrodedCORROSION FOUND AFT CARGO DOOR CUTOUT LOWER WEB HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS FOUND OUT OF LIMITS ON AFT CARGO DOOR CUTOUT LOWER WEB; REMOVED WEB; DRILLED HOLES ON NEW WEB; TREATED ANSDR SWAA2024102837054Strip · elongatedFWD CARGO ALL CAPSTRIPS HAS HOLES ELONGATED<[01] INSTALLED FWD CARGO FLOOR CAP STRIPS; AMM 25-52-06-400-801-NG;[02] VERIFIED STEP 1SDR SWAA2024102836404Stiffener · crackedLH HORIZONTAL STAB RIB #5 STIFFENER 3 CRACK.<[01] REMOVED (2) DAMAGED INSTALLED REPAIR KIT PARTS # 55100003-01 AND ANGLE PART # 1490-7075-T6 P.O # 2018518 AT LH HORIZONTAL STAB RIB # 5 STIFFENER 3 REF. SRM 55-10-09-2R-5;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102836408Stiffener · crackedRH HORIZONTAL STAB RIB 3 STIFFENER 3 CRACK.<[01] CUT OUT DAMAGED INSTALLED REPAIR T SECTION; ANGLE; AND SHIMS AT RH HORIZONTAL STAB RIB 3 STIFFENER 3 REF. SRM 55-10-09-2R-4;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102836407Stiffener · crackedRH HORIZONTAL STAB RIB 3 STIFFENER 4 CRACK.<[01] CUT OUT DAMAGED INSTALLED REPAIR T SECTION; ANGLE; AND SHIMS AT RH HORIZONTAL STAB RIB 3 STIFFENER 4 REF SRM 55-10-09-2R-4;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102836862Scuff Plate · crackedR1 DOOR SCUFF PLATE IS CRACKED FWD AND AFT OF THE EDGE BEND.<[01] RECEIVED NEW SCUFF PLATE PART NUMBER 141A8431-3. PO#2074280 INSTALLATION WILL BE ACCOMPLISHED ON N/R TTG8Q002FJXM. STEP 10;[02] VERIFIED STEP 1SDR SWAA2024102541746Access Panel · crackedR/H FLIGHT COMPARTMENT CONSOLE ACCESS PANEL # 212CW CRACKED AT UPPER CORNER<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #212CW AS PER B 737 AMM 25-00-00-300-801; MATERIAL USED: PO#2039827; PO#1738579 AND APPLIED TOPCOAT ON PANEL #212CW AS PSDR SWAA2024102835636Floor Panel · corrodedFWD CARGO COMPT FLOOR PANEL 120CF HAS SURFACE CORROSION AT R/H SIDE<[01] REMOVED AND REPLACED FLOOR PANEL 120CF AMM.25-52-01-201-801;[02] CORRECTION TO STEP 1: REMOVED AND FABRICATED FLOOR PANEL 120CF AS PER AMM 25-52-01-201-801.;[03] VERIFIED; STEP # 2SDR SWAA2024102837324Vapor Barrier · crackedACCOMPLISH LEFT VAPOR BARRIER REPAIR<[01] .APPLIED REPAIR AT L/H VAPOR BARRIER ON BOTH SIDES AS PER B737 SRM 51-70-04-2R-10 PARAG 4-F AND B737 SRM 51-70-04-2R-0 PARAG 4-N-2; MATERIAL USED RESIN EY 3804 PO#1759622; FIBERGLASS PO#1473815 AND TOOL USED: TEMPERATUSDR SWAA2024102835343Web · crackedCENTER WING REAR SPAR LEFT HAND VAPOR WEB HAS CRACK<[01] REPAIR WAS ACCOMPLISHED ON TTG8Q00VQUSM;[02] VERIFIED REPAIR ACCOMPLISHED ON TTG8Q00VQUSMSDR SWAA2024090433269Slide · looseAFT ENTRY DOOR EMERGENCY SLIDE LOOSE IN BUSTLE<[01] SECURED SLIDE C/W T/C 725-61-06.
Back to Boeing 737-7K9