Boeing 737-7BD
Service difficulty reports · 7,528
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 = '7377BD' 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 = '7377BD' 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 SWAA2024101647568Cover · out of adjustPAX CABIN LEFT AFT SERVICE DOOR SLIDE COVER RUBBING AGAINST TO DOOR SCUFF PLATE TO CLOSE POSITION. 2024-565673<[01] INSTALLED CORRECTLY DOOR SLIDE COVER GIRT I.A.W B737-700 AMM 25-66-01-200-802; STEP 3.B.(1).(D).;[02] CERTIFIED WORK PERFORMED.SDR SWAA2024101647700Hook · looseFWD. SVC. DOOR GIRT BAR HOOK LOOSE<[01] R&R BROKEN RIVET ON FWD. SVC. DOOR GIRT BAR STOW HOOK<BR>PER MM 25-66-00SDR SWAA2024101647567Handle · loosePAX CABIN AFT RIGHT SERVICE DOOR LINING ;ASSISTANT HANDLE LOOSE. 2024-565671<[01] INSTALLED CORRECTLY ASSISTANT HANDLE PAX CABIN AFT RIGHT SERVICE DOOR LINING IAW B737-700 AMM 25-21-25-420-801 STEP 3(B) ITEM (5);[02] INSTALLED CORRECTLY ASSISTANT HANDLE PAX CASDR SWAA2024101647581Light · inoperativeEXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT INOP 2024-565696<[01] REPLACED EXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT IAW B737-700 AMM 33-51-04-960-802 AND PERFORMED TEST IS OK .SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED EXTERSDR SWAA2024101647570Handle · loosePAX CABIN AFT ENTRY AREA AFT LEFT BULKHEAD O/B SIDE OF FA SEAT ;ASSISTANT HANDLE LOOSE 2024-565682<[01] INSTALLED CORRECTLY ASSIT HANDLE ON PAX CABIN AFT ENTRY AREA AFT LEFT BULKHEAD O/B SIDE OF FA SEAT I.A.W. YOKOHAMA CMM 25-42-76 REV 05 ASSEMBLY STEP 1.M. PASDR SWAA2024101447045Light · inoperativeL/H AFT SLIDE LIGHT OUT<[01] RELAMPED L/H AFT SLIDE LIGHT IAW AMM 33-51-04SDR SWAA2024102847594Bracket · damagedALLONGATED HOLE ON BRACKET LOCATE BS663 AND LBL53 AT LEVEL WL210 MAIN WHEEL WELL 2024-589253<[01] REPLACED BRACKET LOCATE BS663 AND LBL53 AT LEVEL WL210 MAIN WHEEL WELL IAW B737-700 SRM 51-10-02 SRM 53-40-51-2R-2 REPAIR 2 SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLSDR SWAA2024101046412Table · brokenTRAY TABLE BROKEN ROW 12F<[01] RESECURED TRAY TABLE ARM SCREW AS PER CMM 25-23-46SDR SWAA2024101644930Seat · out of adjustRECLINE SEAT 11C EMERGENCY EXIT PASSENGER SEAT 2024-565614<[01] PERFORMED ADJUSTMENT ON PASSENGER SEAT 11C EMERGENCY EXIT PASSENGER SEAT IAW CMM 25-21-45 B/E AEROSPACE REV. 5 ITEM 3. G. (3) PAGE 6005.;[02] TASK CARD COMPLETED <BR>PERFORMED ADJUSTMENT ON PASSENSDR SWAA2024100744957Battery Pack · inoperativePASSENGER CABIN; EMERGENCY LIGHT AT 6DEF INOP.<[01] R&R OVERHEAD AREA LIGHT ASSEMBLY (EMERGENCY LIGHT HOUSING) AT SEAT 6DEF REF AMM 33-51-03; R&R BATTERY PACK M1674 & ASSOCIATED POWER SUPPLY CHARGER IAW AMM 33-51-06.SDR SWAA2024100745933Charger · inoperativePASSENGER CABIN; EMERGENCY LIGHT AT 6DEF INOP.<[01] R&R OVERHEAD AREA LIGHT ASSEMBLY (EMERGENCY LIGHT HOUSING) AT SEAT 6DEF REF AMM 33-51-03; R&R BATTERY PACK M1674 & ASSOCIATED POWER SUPPLY CHARGER IAW AMM 33-51-06.SDR SWAA2024101644929Rib · crackedCRACK ON INSPAR RIB 129.50 MORE 34 INCH FROM TO FRONT SPAR RT HORIZONTAL STABILIZER 2024-565613<[01] TOOL USED ON STEP 3 AND 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] PERFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 MOSDR SWAA2024101642350Floor Support · crackedCRACK ON HOLE OF INTERCOSTAL LOCATED BS 251.6 AND LBL 16 FLIGHT DECK FLOOR 2023-565606<[01] REPLACED INTERCOSTAL LOCATED BTW BS 251.6 AND LBL 15.3 AT LBL 24.7 FLIGHT DECK FLOOR IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5100; SHEET132; REV A. SEE INDIVIDUAL SDR SWAA2024100143098Slide · out of adjustR2 WINDOW UPPER REAR NUT MISSING ON SLIDE<[01] REPLACED MISSING NUT; WASHER; AND SPACER AT F/OS SLIDING WINDOW UPPER HOUSING IAW AMM 56-12-11-220-001; OPS CHECK GOOD.SDR SWAA2024092741640Light · inoperativeAFT RECESSED CEILING EMERGENCY LIGHT INOP<[01] RELAMPED EMERGENCY LIGHT IAW AMM 33-51-03. OPS CHECK GOODSDR SWAA2024101641390Web · crackedCRACK FLOOR STRUCTURE WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R AT FWD GALLEY AREA 2024-565603<[01] REPLACED WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING 141A8310 REV:B .SEE INDIVIDUAL STEP SIGN OSDR SWAA2024101639384Vapor Barrier · crackedCRACK INDICATION FOUND ON VAPOR BARRIER LOWER WEB AT BS 663 AND LBL 50 CRACK LENGTH IS 5 INCH 2024-565593<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A24028535; DUE DATE: 06-JUN-25.;[02] TOOL USED= HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 15-FEB-25SDR SWAA2024102839335Floorbeam · crackedCRACK ON BREAK PANEL LOCATED BS 663.7 AND BTW RBL 45.5 AND RBL 60 AT PASSENGER CABIN 2024-589232<[01] REPLACED BREAK PANEL LOCATED BS 663.7 AND BTW RBL 45.5 AND RBL 60 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; 51-10-02; ITEM 9 AND DWG 144A5701 SHEET 1 REV SDR SWAA2024092039310Slide · dislodgedCUSTOMER WALK: R1 SLIDE GUSSET OUT OF SLIDE COVER.<[01] FAULT ACCOMPLISHED ON TTG8Q00VYUCB;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024102839218Floorbeam · cracked(CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-589223<[01] REPLACED SUPPORT AND FASTENERS LOCATED BS540 BL0 RBL 24.75 IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DRAWING D143A5240-36. SEE INDIVSDR SWAA2024102839213Light · crackedCRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION (10 EA) 2024-589219<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-960-801;[02] CERTIFIED TASK COMPLETE <SDR SWAA2024102839214Floorbeam · cracked(CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-589224<[01] FAULT RESOLVED ON FAULT TTG8Q00VRD6P;[02] FAULT RESOLVED ON FAULT TTG8Q00VRD6PSDR SWAA2024102839026Web · crackedCRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-589217<[01] REPLACED HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 141A8310 SHEET 25 RESDR SWAA2024092039060Bottle · low pressureL1 DOOR SLIDE GAUGE IS IN THE RED<[01] INSPECTED L1 DOOR SLIDE PER AMM 25-66-01. L1 DOOR SLIDE IS IN SERVICEABLE CONDITION.SDR SWAA2024102838597Angle · crackedCRACK ANGLE LOCATE ON WEB INTERCOSTAL LOCATED BTW BS380 TO BS400 BL0 PASSENGER CABIN 2024-589207<[01] REPLACED ANGLE ON WEB INTERCOSTAL LOCATED BTW BS380 TO BS400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG#143A5400 SHEET 91 REV. - SEE INDISDR SWAA2024102838085Angle · crackedCRACK ANGLE LOCATED BS540 AND RBL 6 AT CENTER WING BOX 2024-589181<[01] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED IAW SRM 51-40-02. CRACK LENGHT IS: 0.5' TOOL USED CALIPER P/N: 500-196-30; S/N: AE2SDR SWAA2024102838086Angle · crackedCRACK ANGLE LOCATED BS 540 AND LBL 6 AT CENTER WING BOX 2024-589179<[01] REPLACED ANGLE LOCATED BS 540 AND LBL 6 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK LENGHT IS: 0.753' TOOL USED CALIPER P/N: 500-752-20; S/N: B21014939 AND DUESDR SWAA2024102837871Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 216 AT LT WING 2024-572291<[01] REPLACED ANGLE ON TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02; DWG 115A5552 SHEET 1 REV A SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPLACED ANGLE ON TRAILINSDR SWAA2024102837360Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2024-572219<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; SDR SWAA2024102837599Rib · crackedCRACK INSPAR RIB LOCATED STAB STA101.90 AND 9 INCHES FROM REAR SPAR AT RT HORIZONTAL STABILIZER 2024-572240<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 10-JUN-25;[02] TOOL USED STEP 6: EDDY CURRENT EQUIPMENT; P/N: NORSDR SWAA2024102837600Rib · crackedCRACK INSPAR RIB LOCATED STAB STA129.50 AND 9 INCHES FROM REAR SPAR LT HORIZONTAL STAB 2024-572241<[01] STEP 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:210138503; DUE DATE: 05-AUG-25;[02] REPAIRED INSPAR RIB LOCATED STAB STA129.50 AND 9 INCHESDR SWAA2024102837596Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS140 AT RT WING 2024-572231<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 115A2000 SHEET 22 REV A. MEASURE OF CRACK IS 1.328? TOOL USED DIGITAL CALIPSDR SWAA2024102837597Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 224 AT LT WING 2024-572236<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 224 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02; DWG # 115A2001 SHEET 136 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02]SDR SWAA2024091637223Lens · looseR1 DOOR EMERGENCY SLIDE GAUGE LENS LOOSE<[01] RESECURED R1 DOOR EMERGENCY SLIDE WINDOW REF M/M 25-66-01SDR SWAA2024102837056Floorbeam · corrodedCORROSION EXISTING REPAIR ON FLOOR BEAM LOCATED STA 986.5 BTW RBL 44 TO LBL 44 WL 208.1 AT AFT GALLEY AREA 2024-572200<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200048001; DUE DATE: 28-MAY-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOSDR SWAA2024102837059Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA294.5 AND RBL52 WL208.1 AT FWD GALLEY AREA 2024-572203<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] TOOL USED RADIOMETER/PHOTOMSDR SWAA2024102837068Intercostal · crackedCRACK WEB INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA 2024-572212<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] REPAIRED SDR SWAA2024102837069Frame · crackedCRACK FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN 2024-572213<[01] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-153-01244.;[02] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-15SDR SWAA2024102837359Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.800 INCH. APPROX. 2024-572217<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; SDR SWAA2024102837060Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV 2024-572204<[01] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV . IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A5400 SSDR SWAA2024102837062Floor Support · corrodedCORROSION INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL10 WL208.1 FWD GALLEY AND LAV 2024-572206<[01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA 312 TO STA 328 AND RBL10 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02;SDR SWAA2024102837065Structure · crackedCRACK INNER CHORD LOCATED STA 303.9 AND LBL 53 AT FWD GALLEY AREA 2024-572208<[01] REPLACED INNER CHORD LOCATED STA 277 TO STA 360 AND LBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A8110 SHEET 9 REV. A; DWG#142A0050 SHEET 15 REV. - ANDSDR SWAA2024102837067Stringer Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-572211<[01] REPLACED TIE CLIP AND FASTENERS LOCATED ON STA 277 AND STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;AND DWG 141A1110 SHEET 18 REV -;DWG 141A8380 SHEET 14 REV-;SRM 51-10-02; ITSDR SWAA2024102537058Strap · corrodedCORROSION STRAP FLOOR STRUCTURE LOCATED BETWEEN STA1006 TO STA1016 PLUS 25 INCHES AND RBL3 WL208.1 AT AFT GALLEY AREA 2024-572201<[01] REPLACED STRAP AND FASTENERS LOCATED ON FLOOR STRUCTURE BETWEEN STA1006 TO STA1016 PLUS 25 INCHES AND RBL3 WL208.1 AT AFT GALSDR SWAA2024102537066Stub Frame · crackedCRACK STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-572210<[01] TOOL USED ON STEP 5 AND 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] REPAIRED STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-SDR SWAA2024102437061Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL30 FWD GALLEY AND LAV 2024-572205<[01] REPLACED WEB-INTERCOSTAL LOC.BTW STA312 TO STA328 AND RBL30 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 39 REV.- SEE INDIVIDUAL SDR SWAA2024102437064Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BTW STA 344 TO STA 360 AND RBL 33 FWD GALLEY AND LAV 2024-572207<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE AND FASTENERS BTW STA 344 TO STA 360 AND RBL 33 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND INSSDR SWAA2024101637137Floor Support · corrodedAAI-INSPECTION AFT CARGO COMPARTMENT; FLOOR SUPPORT BRACKET HAS CORROSION BWT STA 847 & STA 867; STR 25R 2024-565563<[01] REPLACED SUPPORT BRACKET AND FASTENER LOCATED BTW STA847 AND STA867 STR25R IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 146A8320 REV-: SEESDR SWAA2024101637138Floorbeam · crackedAAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-565565<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 TO RBL 24.75 AND FASTENERS IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFSDR SWAA2024101637139Floor Support · crackedAAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-565566<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02]
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