N288WN
Service difficulty reports · 272
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 = 'N288WN' 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 = 'N288WN' 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 SWAA2024092339563Battery · inoperativeFOUND L1 DOOR; ROWS 1ABC AND 2ABC EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED M01675 EMERGENCY BATTERY PACK IN FORWARD GALLEY CEILING PANEL IAW AMM 33-51-06.SDR SWAA2024080519929Panel · delaminatedRIGHT WING INBOARD TRAILING EDGE FLAP IS DELAMINATED AT O/B AFT TRAILING EDGE APPROX 240 SQ/IN.<[01] REMOVED R/H INB FLAP TRAILING EDGE WEDGE PANEL PER SRM 51-40-02.;[02] REMOVED RIGHT I/B AFT FLAP WEDGE PANEL PER CMM 57-53-09.;[03] VERIFIED MECHANIC REMOVED RSDR SWAA2024080519931Panel · delaminatedLEFT WING I/B FLAP HAS A DELAMINATED AREA ON O/B AFT WEDGE APPROXIMATELY 9.6 X 8<[01] REMOVED AND REPLACES LEFT I/ B FLAP WEDGE PANEL PER CMM57-53-09.;[02] VERIFIED REMOVED AND REPLACED LEFT I/ B FLAP WEDGE PANEL PER CMM57-53-09.;[03] PAINTED I/B FLAP WEDGE PASDR SWAA2024080219925Seat · unsecurePASSENGER CABIN SEAT ROW LOOSE IN TRACKS AT 11DEF; 16 DEF AND 23DEF.<[01] RESECURED PASSENGER CABIN SEAT ROWS AT 11DEF; 16DEF; AND 23DEF IN REF AMM 25-22-00.SDR SWAA2024073119304Stop Pin · crackedFWD GALLEY SERVICE DOOR LOWER AFT STOP PIN FITTING CRACKED; CRACK VERIFIED.<[01] REMOVED AND REPLACED FORWARD SERVICE DOOR PER AMM 52-41-00 UP TO STEP G; SUBTASK 1. DOOR STILL REQUIRES LINING INSTALL; ADJUSTMENT AND SYSTEM TEST.;[02] ADJUSTED FWD SERVICE DOOR SDR SWAA2024041173003Lamp · inoperativeEXTERIOR RH SIDE #3 EMER LIGHT INOP<[01] RELAMPED EMER LIGHT ON RH SIDE #3 POSITION PER AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SWAA2024020945633Rib · deformedRH HORIZONTAL STAB CLOSURE RIB 182A5201-4 AT STAB STA 281.81 LOWER AFT O/B RETURN FLANGE IS BENT/DEFORMED 2.5' AND HAS A 1.75' CRACK<[01] REMOVED AND REPLACED R/H STAB CLOSURE RIB 182A5201-4 AT STAB STA 281.81 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DWG 182A5SDR SWAA2023092604564Vapor Barrier · crackedFOUND CRACK EXTENDED 18 INCHES AT LEFT WHEEL WELL VAPOR BARRIER LBL 31.83 WING CENTER SECTION SPAR. PERFORMED PULSE-ECHO INSPECTION OF LAMINATED STRUCTURES TO DETECT INTERPLY DELAMINATIONS WITH ACCESS TO ONE SIDE OF PART ONLY ON THE PERMANENT REPAIR AFTER IT SDR SWAA2023072882019Vapor Barrier · crackedFOUND AN APPROXIMATELY 9IN CRACK AT LEFT WHEEL WELL VAPOR BARRIER LBL 31.83. WING CENTER SECTION REAR SPAR.<[01] REF LOG PAGE # 2404650 FOR DUPLICATE WRITE UPSDR SWAA2023061455678Girt Bar · out of positionL1 DOOR AND R1 DOOR SLIDES GIRTS ARE NOT PROPERLY INSTALLED<[01] REPOSITIONED L1 DOOR AND R1 DOOR SLIDES GIRTS IN REF AMM 25-66-01-400-801.;[02] VERIFIED STEP 1SDR SWAA2023061459026Girt Bar · incorrectL1 DOOR AND R1 DOOR SLIDES GIRTS ARE NOT PROPERLY INSTALLED<[01] REPOSITIONED L1 DOOR AND R1 DOOR SLIDES GIRTS IN REF AMM 25-66-01-400-801.;[02] VERIFIED STEP 1SDR SWAA2023061355677Battery Pack · inoperativeSEVERAL INTERNAL AND EXTERNAL EMERGENCY LIGHTS INOP.<[01] TROUBLESHOT TO FUALTY EMERGENCY LIGHTS POWER SUPPLY BATTERY PACKS AT POSITIONS M1670 AND M1674; REMOVED AND REPLACED BATTERY PACKS M1670 AND <BR>M1674; OPS CHECK NORMAL REF B737 AMM 33-51-06 AND 33-51-0SDR SWAA2023061454734Support Angle · crackedFABRICATE ANGLE-SUPPORT P/N 141A5134-13 AT FLIGHT DECK FLOOR STRUCTURE BETWEEN STA 250 AND STA 260 AT RBL 3.6 TO RBL 15.<[01] RECEIVED AND VERIFIED NEW ANGLE SUPPORT P/N 141A5134-13 FABRICATED BY OUTSIDE VENDOR PREMIER AEROSPACE CORP. WITH AAR REPAIR ORDER #41SDR SWAA2023061451883Scuff Plate · crackedAFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIED REPAIR TO AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED AREA.SDR SWAA2023061452168Slat · crackedREPLACE #5 LEADING EDGE SLAT. FOUND CRACK TO BE OUT OF LIMITS; INSTALL NEW SLAT UPON ARRIVAL.<[01] REMOVED AND REPLACED #5 LEADING SLAT AS PER AMM 27-81-21-400-801;[02] REMOVED AND REPLACED #5 LEADING SLAT AS PER AMM 27-81-21-400-801. OPS CHECK OK; NO LEAKS NOSDR SWAA2023061451440Baffle · crackedFOUND BAFFLE CRACKED AT FWD. CARGO S-26L; BETWEEN STA. 500A - 500B.<[01] REMOVED DAMAGED BAFFLE; RECEIVED & REPAIRED NEW BAFFLE FOR ACCESS TO ROUTE WIRE BUNDLE; INSTALLED NEW REPAIRED BAFFLE AT FWD. CARGO S-26L. BETWEEN STA. 500A - 500B; AS PER DWG. 143A7505; SDR SWAA2023061451000Channel · crackedMAIN CABIN FWD WET AREA CHANNEL BETWEEN STA 360-380 BL 0 CRACKED<[01] REMOVED DAMAGED STRAP CHANNEL P/N: 143A5410-165; AT MAIN CABIN BETWEEN STA. 360-380; BL 0'; AS PER SRM 51-40-02.;[02] STEP #1: ENTERED IN ERROR.;[03] REMOVED AND REPLACED STRAP CHANNEL P/N: SDR SWAA2023061451176Panel · crackedRIGHT WING LEADING EDGE ACCESS PANEL 621VB FWD END CRACK<[01] PREPARED PANEL #621VB FOR REPAIR PER B737 SRM 51-70-04-2R-6 PARA 4.D; APPLIED REPAIR ON DAMAGE AREA; ACCESS PANEL 621VB; AS PER B737 SRM 51-70-04-2R-6. MATERIAL USED PO.1800550 AND PO.1473815; PAINTSDR SWAA2023061449910Web · crackedCRACK FOUND AT 1 EA.FASTENER HOLE UNDER FLIGHT DECK FLOOR WEB AT RBL 3.6' OF BEAM UPPER CHORD BETWEEN STA 250 - STA 260. (MARKED). CRACK FOUND AT 1 EA.FASTENER HOLE UNDER FLIGHT DECK FLOOR WEB AT RBL 3.6" OF BEAM UPPER CHORD BETWEEN STA 250 - STA 260. (MARSDR SWAA2023061450146Frame · crackedL-1 DOOR CUTOUT STA 312 BETWEEN STR 6L-5L FRAME END CRACKED<[01] ACCOMPLISH REPAIR ON EA: M-22-153-01244.; TTG8Q00L4MLS.;[02] VERIFIED STEP 1SDR SWAA2023061449379Stiffener · crackedCRACK INDICATION OBTAINED FROM FASTENER HOLE ON VAPOR BARRIER STIFFENER AT LBL 51<[01] REAMED FASTENER HOLE ON VAPOR BARRIER STIFFENER AT LBL 51 TO 2ND OVERSIZE AS PER B737-700 SRM 51-40-02-0G-0 STEP 4 D.;[02] VOID STEP #1;[03] ACCOMPLISHED EA: 23-157-01649/88SDR SWAA2023061449378Angle · crackedCRACK INDICATIONS OBTAINED FROM OPEN FASTENER HOLES AT LH VAPOR BARRIER UPPER ATTACH ANGLE VERTICAL FLANGE AT LBL 7;23;24;29 30;31 & 41. ALSO; CRACK FOUND AT LBL 41. CRACK LENGTH : 0.718' CRACK INDICATIONS OBTAINED FROM OPEN FASTENER HOLES AT LH VAPOR BARRIER SDR SWAA2023061448619Panel · crackedCENTER LOWER AFT FAIRING ACCESS PANEL # 194E WITH MULTIPLE FASTENER HOLES BULGING AND CRACKED ON EDGES INNER SIDE<[01] REMOVED DAMAGED AND PREPARED AREA FOR REPAIR AS MARKED ON ACCESS PANEL #194E AS PER B737 SRM 51-70-04-2R-9; APPLIED THE GLASS FABRIC REPAIR PSDR SWAA2023061448623Panel · crackedR/T WING - LOWER LE/E ACCESS PANEL # 621GB WITH CRACKED SPRING ON LATCH (2ND FROM O/B EDGE)<[01] REMOVED AND REPLACED R/T WING - LOWER L/E ACCESS PANEL #621GB LATCH 2ND FROM O/B EDGE REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023061447920Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 380-400 RBL 12' CRACKED<[01] REMOVED & REPLACED INTERCOSTAL ANGLE AT MAIN CABIN RBL 12; BETWEEN STA. 380 - 400; AS PER SRM 51-40-02 & DWG. 143A5400.;[02] VERIFIED STEP 1SDR SWAA2023061447921Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 380-400 BL 0 CRACKED<[01] REMOVED & REPLACED INTERCOSTAL ANGLE AT MAIN CABIN BL 0; STA. 380 - 400; AS PER SRM 51-40-02 & DWG> 143A5400.;[02] (RII) VERIFIED STEP 1SDR SWAA2023061448080Gusset · crackedFWD CARGO COMP STA 500D STR 19L GUSSET CRACKED<[01] REMOVED & REPLACED GUSSET AT FWD. CARGO COMPT. STA. 500D; S-19L; AS PER SRM 51-40-02; & DWG. 143A9481.;[02] VERIFIED STEP 1SDR SWAA2023061448081Channel · crackedFWD CARGO COMP STA 500B STR 26L CLIP UNDER ZEE CHANNEL CRACKED<[01] REMOVED & REPLACED CLIP AT FWD. CARGO STA. 500B; S-26L; AS PER SRM 51-40-02 & DWG. 143A7505;[02] VERIFIED STEP 1SDR SWAA2023061448082Panel · crackedMAIN CABIN STA 540 RBL 2' PANEL BREAK CRACKED<[01] REMOVE & REPLACED PANEL BREAK AT MAIN CABIN STA. 540 RBL 2; AS PER SRM 51-40-02 & DWG. 143A0060.;[02] (RII) VERIFIED STEP 1SDR SWAA2023061448083Panel · crackedMAIN CABIN STA 540 LBL 2' PANEL BREAK CRACKED<[01] REMOVED MAIN CABIN STA 540 LBL 2' PANEL BREAK AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED MAIN CABIN STA 540 LBL 2' PANEL BREAK AS PER SRM 51-40-05-0G-0. INSTALLED MAIN CABIN STA 540 LBL 2' PANEL BREAK AS PESDR SWAA2023061448330Floor Panel · frayedMAIN CABIN FLOOR PANEL 241AEF UPPER SURFACE FRAYING AND COMPOSITE EXPOSED<[01] RECEIVED MAIN CABIN FLOOR PANELS 241AEF; PANEL WILL BE INSTALLED ON T/C TTG8Q00K86F1;[02] VERIFIED STEP 1SDR SWAA2023061448311Rail · corrodedAFT CARGO DOOR CUTOUT CORROSION AT CARGO RAIL FASTENER HOLE STA 787+11' RBL 14'<[01] THIS CARGO RAIL HAS A CORROSION THAT IS OUT LIMITS ON A DIFFERENT LOCATION THEREFORE IT WILL BE REPLACED ON TASK CARD TTG8Q00L0457SDR SWAA2023061448310Rail · corrodedAFT CARGO DOOR CUTOUT CORROSION AT CARGO RAIL O/B EDGE STA 787+7' RBL 14'<[01] ACCOMPLISHED CUT OUT ON DAMAGED AFT CARGO TRACK AT STA 767+11.5' AND RBL 13.8' REF SRM 53-00-53-2R-6; ALTERNATIVE 1; FIG. 203; REMOVED AFT CARGO TRACK SECTION BETWEEN STA 767+11.5' SDR SWAA2023061448319Beam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM STA 986.5 LBL 43'<[01] REMOVED CORROSION AT FLOOR BEAM STA 986.5 LBL 43' ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.040'; REMAINING MATERIAL 0.110'; REWORKED AREA IS OUT OF LIMITS REF SRM 53-70-51-1A-1. TRIMMEDSDR SWAA2023061448321Beam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM FASTENER HOLE STA 986.5 RBL 42'<[01] REMOVED CORROSION AT FLOOR BEAM STA 986.5 RBL 42' ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.073'; REMAINING MATERIAL 0.077'; REWORKED AREA IS OUT OF LIMITS REF SRM 53-70-51SDR SWAA2023061447917Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 344-360 RBL 29' CRACKED<[01] REMOVED & REPLACED INTERCOSTAL AT STA. 344 - 360; RBL 29' AS PER SRM 51-40-02 & DWG. 141A5400.;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447916Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 344-360 RBL 12' CRACKED<[01] REMOVED & REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA. 344 - 360; RBL 12'; AS PER SRM 51-40-02; & DWG. 141A5400.;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447914Floor Panel · frayedMAIN CABIN FLOOR PANEL 222CF UPPER SURFACE FRAYING<[01] APPLIED REPAIR ON MAIN CABIN FLOOR PANEL 222CF; AS PER B737 SRM 53-00-50-2R-2 MATERIAL USED PO.1473815 AND PO.1783720;[02] VERIFIED STEP 1SDR SWAA2023061447906Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 328-344 LBL 45' CRACKED<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328-344 LBL 45' AS PER SRM 51-40-02-0G-0 AND DWG 141A5400 ID 0044.;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447909Floor Panel · frayedMAIN CABIN FLOOR PANEL 222AF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANELS 222AF PANEL WILL BE INSTALLED ON T/C TTG8Q00K86CC;[02] VERIFIED STEP 1.SDR SWAA2023061447907Floor Panel · frayedMAIN CABIN FLOOR PANEL 222DF UPPER SURFACE FRAYING<[01] REPAIRED WITH A PERMANENT REPAIR DAMAGE AREAS AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 222DF AS PER B737 SRM 53-00-50-2R-1. MATERIALS USED PO#1738579 AND PO#1783720;[02] PERFORMED TAP TEST ON RESDR SWAA2023061447703Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 312-328 RBL 31' CRACKED<[01] REMOVED MAIN CABIN INTERCOSTAL BETWEEN STA 312-328 RBL 31'; LOCATED AND DRILLED NEW INTERCOSTAL; AND INSTALLED INTERCOSTAL. REF SRM 51-40-02-0G-0 AND DWG #141A5400;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447702Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 277-294.5 BL 0 CRACKED<[01] REMOVED MAIN CABIN INTERCOSTAL BETWEEN STA 277-294.5 BL 0; LOCATED AND DRILLED NEW INTERCOSTAL; AND INSTALLED INTERCOSTAL. REF SRM 51-40-02-0G-0 AND DWG #141A5400;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447693Mount · corrodedMAIN CABIN FWD WET AREA CORROSION AT L-1 DOOR CUTOUT FWD SLIDE MOUNT STA 312 LBL 54'<[01] REMOVED AND REPLACED MAIN CABIN FWD WET AREA AT L-1 DOOR CUTOUT FWD SLIDE MOUNT FITTING AT STA 312 LBL 54' AS PER SRM 51-40-02-0G-0 AND DWG 141A5220.;[02] VERIFIED INSTALSDR SWAA2023061447698Angle · corrodedMAIN CABIN FWD WET AREA CORROSION AT PANEL BREAK ANGLE BETWEEN STA 312-328 RBL 9'<[01] REMOVED CORROSION AT MAIN CABIN FWD WET AREA AT PANEL BREAK ANGLE BETWEEN STA 312-328 RBL 9' AS PER SRM 51-10-02-0G-0. FOUND OUT OF LIMITS AS PER SRM 53-10-51-1A-1. <BR>REMOSDR SWAA2023061347905Intercostal · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 312-328 LBL 45' CRACKED<[01] REMOVED MAIN CABIN INTERCOSTAL BETWEEN STA 312-328 LBL 45'; LOCATED AND DRILLED NEW INTERCOSTAL; AND INSTALLED INTERCOSTAL. REF SRM 51-40-02-0G-0 AND DWG #141A5400;[02] (RII) VERIFIED STEP 1SDR SWAA2023061447570Bracket · cracked#2 ENGINE I/B FAN COWL AFT HOLD OPEN ROD BRACKET CRACKED<[01] REMOVED #2 ENGINE I/B FAN COWL AFT HOLD OPEN ROD BRACKET AS PER SRM 51-40-02-0G-0. INSTALLED #2 ENGINE I/B FAN COWL AFT HOLD OPEN ROD BRACKET AS PER SRM 51-40-02-0G-0.;[02] REMOVED #2 ENGINE I/B FANSDR SWAA2023061447567Bracket · crackedLEFT WING TRAILING EDGE DEFLECTOR PANEL LOWER CENTER BRACKET CRACKED AT O/B AROUND THE RIVET<[01] REMOVED & INSTALLED NEW BRACKET ANGLE AT LW TRAILING EDGE DEFLECTOR PANEL LOWER CENTER IN REF. SRM 51-40-02-0G -0 & DWG. 115A2156.;[02] VERIFIED STEP 1SDR SWAA2023061447568Bracket · crackedLEFT WING TRAILING EDGE DEFLECTOR PANEL LOWER CENTER FWD BRACKET CRACKED<[01] REMOVED AND REPLACED FWD. BRACKET AT LEFT WING TRAILING EDGE DEFLECTOR PANEL PER; REF. 51-40-02-0G-0;[02] CORRECTION: REMOVED AND REPLACED FWD. BRACKET AT LEFT WING TRAILING EDGE DEFSDR SWAA2023061447565Bracket · crackedRIGHT WING TRAILING EDGE DEFLECTOR PANEL FWD CENTER BRACKET CRACKED<[01] REMOVED AND REPLACED BRACKET AT RIGHT WING TRAILING EDGE DEFLECTOR PANEL AS PER SRM 51-40-02-0G-0.;[02] CORRECTION: REMOVED AND REPLACED BRACKET AT RIGHT WING TRAILING EDGE DEFLECTOR PANE
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