N7738A
Service difficulty reports · 255
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N7738A' AND registry_match = 'registration' 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 n_number = 'N7738A' AND registry_match = 'registration' 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 SWAA2024101634460Rib · crackedCRACK INSPAR RIB 129.50 LOCATED AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-565247<[01] TOOL USED ON STEP 3:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NOSDR SWAA2024101634458Rib · crackedCRACK INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2024-565252<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[02] TOOL USED ON STEP 6 AND 7 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CSDR SWAA2024101634459Rib · crackedCRACK INSPAR RIB 120.30 LOCATED AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2024-565250<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[02] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUESDR SWAA2024101634639Stringer Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-565292<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02; DWG NO:141A1110 SHEET:18 REV: -;DWG NO:141A8380 SHEET: 21 REV: - AND IAW B737-700 SRM 51-10-SDR SWAA2024101634456Support Angle · crackedCRACK SUPPORT ANGLE LOCATED STA695 AND RBL24.75 CENTER SECTION 2024-565245<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14282005 DUE DATE 22 JAN 25; P/N P3015GOES00000 S/N 142031023 DUE DATE 22 JAN 25.;[02] REPLACED SUPPORT ANGLE AND FASTENERSSDR SWAA2024101633775Lens · brokenBROKEN LENS ASSY EMERGENCY EXIT LOWERED CEILING PANEL AFT GALLEY AREA (1EA) 2024-565221<[01] REPLACED LENS ASSY EMERGENCY EXIT LOWERED CEILING PANEL AFT GALLEY AREA (1EA) IAW B737-700 AMM-33-51-01-960-802 STEP 5.C.(A) AND (6) ITEM (A) THRU (C);[02] CORRECTED SSDR SWAA2024101634201Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA344 AND RBL31 FWD GALLEY AND LAV 2024-565236 CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL31 FWD GALLEY AND LAV<[01] REPLACED WEB - INTERCOSTAL LOC FLOOR STSDR SWAA2024101634206Bracket · corrodedCORROSION BRACKET FLOOR STRUCTURE LOCATED STA312 AND LBL54 WL208.1 AT FWD GALLEY AREA 2024-565239<[01] REPLACED BRACKET FLOOR STRUCTURE LOCATED STA312 AND LBL54 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5220 SHEET:1 REV:-;[02] JOB CSDR SWAA2024101634026Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.312 INCH 2024-565224<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 220273012; DUE DATE: 09-JAN-25.;[02] TOOL USED: EDDY CURRSDR SWAA2024101634203Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED STA294.5 AND RBL8 WL208.1 AT FWD GALLEY AREA 2024-565238<[01] TOOL USED ON STEP 8 AND 9 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :175375SDR SWAA2024101634202Floor Support · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV 2024-565235<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV IAW SRM B737-700 51-40-02; SRM 51-10SDR SWAA2024101633405Light · brokenBROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10EA) 2024-565140<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10EA) IAW B737-700 SOPM 20-50-12 REV.56 AND DWG 33500007 REV.2 SHEET 2;[02] JOB COMPLETEDSDR SWAA2024101633404Lens · inoperativeINOP LIGHT LENS ASSY EMERGENCY EXIT GALLEY 1 FWD GALLEY AREA 2024-565128<[01] REPLACED LIGHT LENS ASSY EMERGENCY EXIT GALLEY 1 FWD GALLEY AREA B737-700 AMM 33-51-01-960-802;[02] CORRECTED STEP 1<BR>REPLACED LIGHT LENS ASSY EMERGENCY EXIT GALLEY 1 FWD GALLEY ARSDR SWAA2024101632738Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN AT RT WING 2024-565024<[01] TOOL USED: CALIPER PN: 500-196-30 SN: B23272755 DUE DATE: 17/MAR/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 25/JAN/25.;[03] TSDR SWAA2024061199715Handle · unsecureAFT SERVICE DOOR ASSIST HANDLE UNSECURED. RESECURED AFT SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31. A/C OK FOR SERVICE.SDR SWAA2023121129071Slide · partial deployFWD SERVICE DOOR SLIDE BAG PARTIALLY RELEASED<[01] REMOVED & RE-INSTALLED FWD SVC DOOR SLIDE REF AMM 25-66-01& MT 725-61-06.;[02] REPLACED RIVET ON SLIDE CASE PER SRM 51-40-02 BY LANCE GWALTNEY E59819. REMOVED & RE-INSTALLED FWD SVC DOOR SLIDE REF AMM 25-66-01SDR SWAA2023092603243Tail Cone · delaminatedN0. 3 CANOE FAIRING TAIL CONE HAS 2'X2' AREA DELAMINATION ON OUTBOARD SIDE<[01] REMOVED AND REPLACED PER SRM 51-40-02;[02] C/W INSPECTION REQUIREMENT FOR REMOVAL AND INSTALLATION OF #3 CANOE FAIRING TAIL CONE PER SRM 51-54-02SDR SWAA2023070574406Cover · out of adjustEMERGENCY LIGHT LENS COVER AT PASSENGER ENTRY DOOR (FORWARD) FELL OFF<[01] R&R FWD ENTRY LOWER EXIT SIGN ASSY PER MM 33-51-01.SDR SWAA2023041126027Light · inoperativeCAPT SIDE EMERGENCY EXIT ROW LIGHT ON WALL INOP<[01] OK TO CONTINUE PER MEL 33-2-03 SP1B;[02] REMOVED AND REPLACED LH EMERGENCY EXIT ROW WALL LIGHT BALLAST. REF AMM 33-21-00. OPS NORMAL. REF LP# 2025830SDR SWAA2023021000671Seal · crackedRIGHT HORIZONTAL STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] R&R RIGHT HORIZONTAL UPPER FRONT SPAR SLIDING SEAL PER AMM 53-31-31SDR SWAA2023021000672Seal · crackedLEFT HORIZONTAL STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED L/H HORIZONAL STAB TO BODY UPPER FRONT SPAR SLIDING SEAL REF AMM 53-31-31SDR SWAA2022111570396Battery · inoperativeFWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED FWD RH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2022102061784Light · inoperativeSIDEWALL LIGHT OUT AT LH OVER WING EXIT / [01] RE-LAMPED SIDEWALL LIGHT AT LH OVER WING EXIT PER AMM 33-21-00.SDR SWAA2022092891128Connector · inoperativeL/H EXTERIOR EMERGENCY WING SLIDE LIGHT INOP. / [01] UPON TROUBLESHOOTING FOUND OPEN WIRE AT CONNECTOR D11082 POSITION 1 PER REF B737 SSM 33-51-13; AMM 33-51-04-960-801;[02] REINSTALLED CONNECTOR D11082 AND PERFORMED OPS TEST; TEST PASSED PER REF B737 AMM 33-5SDR SWAA2022091352281Connector · inoperativeL/H EXTERIOR EMERGENCY WING SLIDE LIGHT INOP. / [01] UPON TROUBLESHOOTING FOUND OPEN WIRE AT CONNECTOR D11082 POSITION 1 PER REF B737 SSM 33-51-13; AMM 33-51-04-960-801;[02] REINSTALLED CONNECTOR D11082 AND PERFORMED OPS TEST; TEST PASSED PER REF B737 AMM 33-5SDR SWAA2022092891127Lamp · inoperativeL/H OVER WING EMERGENCY LIGHT INOP / [01] REPLACED LAMP AS PER AMM REF 33-51-01-960-801. TESTED FOUND NORMAL.;[02] VERIFIED STEP #1 ABOVE.SDR SWAA2022091352279Lamp · inoperativeL/H OVER WING EMERGENCY LIGHT INOP / [01] REPLACED LAMP AS PER AMM REF 33-51-01-960-801. TESTED FOUND NORMAL.;[02] VERIFIED STEP #1 ABOVE.SDR SWAA2022092891126Seat Track · elongatedSEAT TRACK FASTENER HOLE ELONGATED AT BS 727B - LBL 45.50 POSITION 'B' / [01] MEASURED ELONGATED DAMAGE AT UPPER AREA OF HOLE 'B' AT SEAT TRACK BS 727B; LBL 45.50 : 0.314'<BR>DIAMETER OF BORE HOLE IS: 0.268'. TOOL USED: B/C 170964; DUE DATE: 29-JUN-23. FOUND OSDR SWAA2022091249601Seat Track · elongatedSEAT TRACK FASTENER HOLE ELONGATED AT BS 727B - LBL 45.50 POSITION 'B'<[01] MEASURED ELONGATED DAMAGE AT UPPER AREA OF HOLE 'B' AT SEAT TRACK BS 727B; LBL 45.50 : 0.314'<BR>DIAMETER OF BORE HOLE IS: 0.268'. FOUND OUT OF LIMITS AS PER EA: 22-153-02647-WIP1/859SDR SWAA2022092802980Door · corrodedWASTE SERVICE DR 142AL CORRODED AT BASE BONDING WIRE WASTE SERVCE DR 145AL CORRODED AT BASE / [01] REMOVED WASTE SERVICE DR PER REF.52-49-07-000-801.;[02] FOUND EXFOLIATING CORROSION AROUND BONDING WIRE BASE THAT IS OUT OF LIMITS. DOOR NEEDS REPLACEMENT;[03] VSDR SWAA2022091547252Door · corrodedWASTE SERVICE DR 142AL CORRODED AT BASE BONDING WIRE WASTE SERVCE DR 145AL CORRODED AT BASE / [01] REMOVED WASTE SERVICE DR PER REF.52-49-07-000-801.;[02] FOUND EXFOLIATING CORROSION AROUND BONDING WIRE BASE THAT IS OUT OF LIMITS. DOOR NEEDS REPLACEMENT;[03] VSDR SWAA2022092802978Strap · corrodedAFT CARGO COMP STA 787+2 RBL 19' STRAP UNDER FLOOR SUPPORT CORRODED / [01] REMOVED STRAP FOR ACCESS AT AFT CARGO COMP STA 787+2 RBL 19' UNDER FLOOR SUPPORT REF B737-700 SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY IVAN HERNANDEZ #35699;[02] REMOVED CORROSION ON STRASDR SWAA2022092802979None · crackedAFT CARGO COMP STA 867 LBL 11' CLIP CRACKED / [01] REMOVED CRACKED CLIP AT AFT CARGO COMP STA 867 LBL 11'REF B737-700 REF 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP REF B737-700 SRM 51-40-05-0G-0 WORK ACCOMPLISHED BY INVAN HERNANDEZ#35699;[03] SRM 51-40-0SDR SWAA2022091542950None · crackedAFT CARGO COMP STA 867 LBL 11' CLIP CRACKED / [01] REMOVED CRACKED CLIP AT AFT CARGO COMP STA 867 LBL 11'REF B737-700 REF 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP REF B737-700 SRM 51-40-05-0G-0 WORK ACCOMPLISHED BY INVAN HERNANDEZ#35699;[03] SRM 51-40-0SDR SWAA2022091542947Strap · corrodedAFT CARGO COMP STA 787+2 RBL 19' STRAP UNDER FLOOR SUPPORT CORRODED / [01] REMOVED STRAP FOR ACCESS AT AFT CARGO COMP STA 787+2 RBL 19' UNDER FLOOR SUPPORT REF B737-700 SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY IVAN HERNANDEZ #35699;[02] REMOVED CORROSION ON STRASDR SWAA2022092943421Stringer · corroded(CORROSION) AT STRINGER 25R TO BULKHEAD CONNECTION AT BS 540. (CORRECTION) TO ORIGINAL DISCREPANCY(CORROSION) AT STRINGER 25R TO BULKHEAD FRAME CONNECTION AT BS 540 / [01] REMOVED CORROSION AT STRINGER 24R BS 540; AS PER B737-7; SRM 51-10-02.[31] INSTALLED STRSDR SWAA2022092943426None · cracked#2 ENGINE INBOARD COWL ASSY-FAN 423 FWD HOLD OPEN ROD BRACKET CRACKED / [01] REMOVED AND REPLACED #2 ENGINE INBOARD COWL ASSY-FAN 423 FWD HOLD OPEN ROD REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022092802972Stringer · corroded(CORROSION) AT STRINGER 23L TO BULKHEAD FRAME CONNECTION AT BS 540. (CORRECTION TO ORIGINAL DISCREPANCY).(CORROSION) AT STRINGER 23L TO BULKHEAD FRAME CONNECTION AT BS 540. / [01] REMOVED CORROSION AT STRINGER 22L BS 540; AS PER B737-7; SRM 51-10-02.;[21] -FABSDR SWAA2022092802971Stringer · corroded(CORROSION) AT STRINGER 23R TO BULKHEAD FRAME CONNECTION AT BS 540. (CORRECTION TO ORIGINAL DISCREPANCY) (CORROSION) AT STRINGER 23R TO BULKHEAD FRAME CONNECTION AT BS 540. / [01] REMOVED CORROSION AT STRINGER 22R BS 540; AS PER B737-7; SRM 51-10-02.;[27] -PARSDR SWAA2022092802977Shield · corrodedAFT CARGO COMP ;DOOR CUTOUT FWD SHIELD CORRODED / [01] REMOVED CORROSION AT AFT CARGO COMP ;DOOR CUTOUT FWD SHIELD PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW B737 NDT PART 4; 51-00-00; PROCEDSDR SWAA2022092802975None · crackedFWD CARGO COMP STA 500B STR 26L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO COMP STA 500B STR 26L REF B737-7 SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500B STR 26L REF 737-7 SRM 5SDR SWAA2022092802976None · crackedFWD CARGO COMP STA 500C STR 26L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO COMP STA 500C STR 26L REF B737-7 SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500C STR 26L REF 737-7 SRM 5SDR SWAA2022092802973Gusset · crackedFWD CARGO COMP STA 500D SRT 19L GUSSET CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19L; AS PER B737-7 SRM 51-40-02.;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET P/N 143A9483-6;[03] INSTALLED NEW GUSSET AT FWD CARGO COMP STA 500D SRTSDR SWAA2022092802974Gusset · crackedFWD CARGO COMP STA 500D SRT 19R GUSSET APPEARED CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19R; AS PER B737-7 SRM 51-40-02.;[02] OK TO INSTALL NEW GUSSET;[03] LATE ENTRY VERIFIED STEP 1;[04] INSTALLED NEW GUSSET AT FWD CARGO COMP STASDR SWAA2022091542520Shield · corrodedAFT CARGO COMP ;DOOR CUTOUT FWD SHIELD CORRODED / [01] REMOVED CORROSION AT AFT CARGO COMP ;DOOR CUTOUT FWD SHIELD PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW B737 NDT PART 4; 51-00-00; PROCEDSDR SWAA2022091542515None · crackedFWD CARGO COMP STA 500C STR 26L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO COMP STA 500C STR 26L REF B737-7 SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500C STR 26L REF 737-7 SRM 5SDR SWAA2022091542514Stringer Clip · crackedFWD CARGO COMP STA 500B STR 26L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO COMP STA 500B STR 26L REF B737-7 SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500B STR 26L REF 737-7 SRM 5SDR SWAA2022091542513Gusset · crackedFWD CARGO COMP STA 500D SRT 19R GUSSET APPEARED CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19R; AS PER B737-7 SRM 51-40-02.;[02] OK TO INSTALL NEW GUSSET;[03] LATE ENTRY VERIFIED STEP 1;[04] INSTALLED NEW GUSSET AT FWD CARGO COMP STASDR SWAA2022091542512Gusset · crackedFWD CARGO COMP STA 500D SRT 19L GUSSET CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19L; AS PER B737-7 SRM 51-40-02.;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET P/N 143A9483-6;[03] INSTALLED NEW GUSSET AT FWD CARGO COMP STA 500D SRTSDR SWAA2022091542168Stringer · corrodedCORROSION AT STRINGER 23L TO BULKHEAD FRAME CONNECTION AT BS 540. OUT OF LIMITS IAW SRM 53-00-03-1A-1 TABLE 101. CUT OUT DAMAGED AREA AT END OF STRINGER 23L BS 540; DIMENSION OF CUT: 0.900' X 1.000'; IAW SRM 51-10-02. FABRICATED REPLACEMENT STRINGER IAW SRM
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