N914WN
Service difficulty reports · 256
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 = 'N914WN' 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 = 'N914WN' 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 SWAA2025050565142Light · brokenFOUND FWD L1 DOOR EMERGENCY LIGHT ASSY BROKEN<[01] REMOVED + REPLACED L1 DOOR EMERGENCY LIGHT ASSY IAW AMM 33-51-01; OPS CHECK GOOD.;[02] REMOVED + REPLACED L1 DOOR EMERGENCY LIGHT ASSY IAW AMM 33-51-01; OPS CHECK GOOD.SDR SWAA2025022498807Cover · missingOVERWING EMERGENCY EXIT SIGN FRONT COVER MISSING<[01] INSTALLEDMISSING OVERWING EMERGENCY EXIT SIGN FRONT COVER IN REFERENCE TO AMM 33-51-01SDR SWAA2024120574171Battery Pack · failedL/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2024101547450Sign · missingFWD EXIT COVER ON OVERWING EXIT SIGN MISSING<[01] INSTALLED FWD EXIT COVER ON EXIT SIGN IAW SIP.SDR SWAA2024100443953Megaphone · inoperativeAFT MEGAPHONE INOPFT<[01] R&R'D AFT MEGAPHONE PER AMM 25-64-00SDR SWAA2024090331448Control Panel · failedAFTER PARKING CHECK LIST CARGO FIRE DETECTOR FWD AND DETECTOR FAULT ILLUMINATED FOLLOWED BY SMOKE AND FUMES FROM THE DETECTOR PANEL<[01] R&R CARGO FIRE CONTROL PANLE IAW AMM 26-00-02 AND OP?S CHECK GOOD.SDR SWAA2024071211757Slide · out of positionFWD ENTRY DOOR GIRT BAR HARD TO LATCH<[01] REPOSITIONED FE ESCAPE SLIDE IAW MT 725-61-06. GIRTBAR LATCHES AND UNLATCHES NORMAL.SDR SWAA2024062404555Retainer · damagedL1 DOOR SLIDE FELL OUT OF CONTAINER<[01] FOUND GIRT BAR RETAINING CLIP DAMAGED; REPAIRED AND OK TO CONTINUE PER EA M-23-125-01839. REINSTALLED L1 DOOR SLIDE PER MT 725-61-06.SDR SWAA2024060391488Fairing · delaminated#6 CANOE FAIRING AFT CONE LOWER SECTION DELAMINATED<[01] 05 - OK TO CONTINUE PER [CDL 57-10-4 XB;RIGHT - FLAP TRACK FAIRING TAIL CONES- INBOARD FLAPS]. WITH SP 1. INSTALLED NEW AFT FAIRING TAILCONE IAW AMM 27-51-18 THIS CLEARED CDL;[03] REPLACED #6 AFT FLAP FSDR SWAA2024022956679Lamp · inoperativeRT OVERWING EXIT SIGN HAS ONE LAMP INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-01. OPS CHECK OK.SDR SWAA2023112022290Handle · out of adjustL-1 DOOR ASSIST HANDLE LOOSE NEEDS SECURED.<[01] SECURED L-1 DOOR ASSIST HANDLE AS PER B737 AMM 25-21-31-420-802;[02] VERIFIED STEP 1SDR SWAA2023112121395Battery Pack · inoperativeEME BATTERY AT LOCATION M01674 WILL NOT CHARGE<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M01674 I/A/W BOEING AMM 33-51-06-960-805; OPS CHECKS NORMAL;[02] VERIFIED STEP 1SDR SWAA2023112117164Intercostal · corrodedFOUND CORROSION AT MAIN CABIN INTERCOSTAL STABILIZER RBL 11.05; BETWEEN STA. 294.5 & STA. 312; WL 208.1.<[01] ORIGINAL THICKNESS 0.080'; REMAINING MATERIAL 0.067'; REMOVED MATERIAL 0.013'. REWORKED AREA IS OUT OF LIMITS REF SRM 53-10-51-1A-1; FIGURE 105; DETAISDR SWAA2023112117162Floor Support · corrodedFOUND CORROSION AT MAIN CABIN INTERCOSTAL STABILIZER RBL 11.05; BETWEEN STA. 312 & STA. 328; WL 208.1.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT MAIN CABIN RBL 11.05 AND BETWEEN STA 312 TO STA 328; WL 208.1 REF SRM 51-40-02-0G-0;[02] RII; VERIFIED STEP # 1SDR SWAA2023112116215Panel · damagedINLET ACCESS #2 ENGINE LOWER NOSE COWL PANEL #422AB HAS ELONGATED FASTENER HOLES<[01] RECEIVED NEW LOWER NOSE COWL PANEL #422AB P# 314-2163-1 PO# 2028887 BN 406123. PANEL WILL BE INSTALLED ON TASK CARD # TTG8Q00P88YN;[02] VERIFIED STEP 1SDR SWAA2023112020285Panel · bulgedR/H WING LOWER MID T/E ACCESS PANEL # 661CB HAS BULGING/CRACKED FASTENER HOLES THE CORRECT PANEL NUMBER IS 661BB<[01] ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION IAW B737 NDT PART 1; 51-01-02 AND PART 4;51-00-01. NO ADDITIONAL DAMAGE NOTED OTHER SDR SWAA2023112115200Stringer · crackedFASTENER HOLE # 7 FROM AFT TO FWD ON STR 16-L FOUND CRACKED BETWEEN STA 294.5 AND 303.9<[01] REMOVED AND REPLACED DAMAGE STRINGER AT STR 16L STA 294.5-303.9 REF SRM 53-00-03-2R-1 FIGURE 205 TABLE 201 AND TABLE 202 AND DWG # 141A3120. EA # 21-153-03254-WIP1/898SDR SWAA2023112114861Floor Support · crackedCABIN FLOOR INTERCOSTAL CRACKED AT FASTENER HOLE B.S. 312+9' LBL.45' W.L.208. (51-002)<[01] APPLIED EWIS PROTECTION TO CABIN FLOOR STA 312+9 LBL 45' AS PER AMM 20-60-07-913-801; REMOVED FASTENERS FROM CABIN FLOOR INTERCOSTAL STA 312+9' LBL.45' AS PER SRM 51-40SDR SWAA2023112114862Intercostal · crackedCABIN FLOOR INTERCOSTAL CRACKED AT B.S. 277+7' RBL 1' W.L. 208. (51-003)<[01] REMOVED AND REPLACED INTERCOSTAL AT CABIN FLOOR B.S. 277+7' RBL 1' W.L. 208. AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1.SDR SWAA2023112114860Fitting · corrodedCORROSION SPOT ON L1 DOOR GIRT BAR FORWARD MOUNT FITTING B.S. 312 LBL 54' W.L 208. (51-004)<[01] REMOVED L1 DOOR GIRT BAR FWD MOUNT FITTING IAW SRM 51-40-02-0G-0. INSTALLED L1 DOOR GIRT BAR FORWARD MOUNT FITTING B.S. 312 LBL 54' W.L 208.1 IN REF WITH SRM 51-40SDR SWAA2023112114863Intercostal · crackedCABIN FLOOR INTERCOSTAL CRACKED AT FASTENER HOLE B.S. 344 + 10' BL. 0 W.L 208. (51-005)<[01] REMOVED AND REPLACE CRACKED INTERCOSTAL AT B.S 344 +10' BL. 0 AS PER SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED; STEP # 1.SDR SWAA2023112114708Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD HAS SPOTS OF CORROSION BETWEEN BS 847 & BS 887; LBBL 65. WL 208.1. MAIN CABIN CREASE BEAM INNER CHORD HAS SPOTS OF CORROSION BETWEEN BS 847 & BS 887 RBL 65. WL 208.1.<[01] ACCOMPLISHED EA: 23-153-03284.;[02] VERIFIED STEP 1SDR SWAA2023112114706Web · dentedFLIGHT DECK FLOOR WEB HAS DIMPLED FASTENER HOLE AT B.S. 259.5-5' LBL. 14' W.L.208. (51-001)<[01] ACCOMPLISHED EA: 23-153-03264.;[02] VERIFIED CORRECTIVE ACTION STEP 1; ACCOMPLISHMENT OF EA: 23-153-03264;[03] VERIFIED CORRECTIVE ACTION STEP 1; ACCOMPLISHMENT OFSDR SWAA2023112113922Stiffener · crackedLEFT HORIZONTAL STAB RIB # 6 AFT STIFFENER WAS FOUND CRACKED AFTER RIB REMOVAL<[01] REMOVED AND INSTALLED NEW STIFFENER AT LEFT HORIZONTAL STAB RIB # 6 REF 51-40-02-0G-0; DWG 182A1505 AND EA23-155-03219 (WIP 1).;[02] RII; VERIFIED STEP # 1;[03] REMOVED AND INSSDR SWAA2023112113413Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 242UF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 242UF AND WILL BE INSTALLED ON T/C TTG8Q00NS4WB;[02] VERIFIED; RECEIVED NEW CABIN FLOOR PANEL # 242UF AND WILL BE INSTALLED ON T/C TTG8Q00NS4WBSDR SWAA2023112112452Handle · looseR-1 DOOR HANDLE STUB SHAFT LOOSE ON CAMPLATE<[01] REMOVED AND RE-TORQUED AND RE-INSTALLED NUT ON HANDLE STUB AS PER SOPM 20-50-01;[02] VERIFIED STEP 1SDR SWAA2023112112857Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL 221DF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 221DF AND WILL BE INSTALLED ON T/C TTG8Q00NS4Y3;[02] VERIFIED; STEP # 1. RECEIVED MAIN CABIN FLOOR PANEL 221DF AND WILL BE INSTALLED ON TTG8Q00NS4Y3.SDR SWAA2023112112858Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL 222DF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 222DF AND WILL BE INSTALLED ON T/C TTG8Q00NS4XF;[02] VERIFIED STEP # 1. RECEIVED MAIN CABIN FLOOR PANEL 222DF AND WILL BE INSTALLED ON TTG8Q00NS4XF.SDR SWAA2023112112859Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL 222CF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 222CF AND WILL BE INSTALLED ON T/C TTG8Q00NS4XK;[02] VERIFIED; STEP # 1. RECEIVED MAIN CABIN FLOOR PANEL 222CF AND WILL BE INSTALLED ON TTG8Q00NS4XK.SDR SWAA2023112112860Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL 222BF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANELS 222BF AND WILL BE INSTALLED ON T/C TTG8Q00NS4JF;[02] VERIFIED # 1. RECEIVED MAIN CABIN FLOOR PANEL # 222BF AND WILL BE INSTALLED ON TTG8Q00NS4JF.SDR SWAA2023112112737Intercostal · crackedINTERCOSTAL CRACKED FWD EDGE @ S-16L BETWEEN STA 294.5 AND STA 303.9 MKD DOT<[01] REMOVED AND REPLACED INTERCOSTAL;STRAP AND CLIP AT S-16L BETWEEN STA 294.5 AND STA 303.9 REF SRM 51-40-02-0G-0 AND DWG 141A8180.;[02] CORRECTION TO STEP 1. REMOVED AND INSTALLED SDR SWAA2023112112849Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241ACF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ACF AND WILL BE INSTALLED ON T/C TTG8Q00NS4PC;[02] VERIFIED; STEP # 1.SDR SWAA2023112112861Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241AAF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241AAF AND WILL BE INSTALLED ON T/C TTG8Q00NS4PH;[02] VERIFIED; STEP # 1.SDR SWAA2023112112851Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241ABF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ABF AND WILL BE INSTALLED ON T/C TTG8Q00NS4PF;[02] VERIFIED; STEP # 1.SDR SWAA2023112112852Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241XF TOP SURFACE DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241XF AND WILL BE INSTALLED ON T/C TTG8Q00NS4NL;[02] VERIFIED; STEP # 1.SDR SWAA2023112112447Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB #6 STIFFENER #3 LOWER SECTION CRACK<[01] REMOVED DAMAGE ON STIFFENER #3 LOWER SECTION AND WEB AND INSTALLED REPAIR PARTS COMMON TO STIFFENER #3 AT LEFT HORIZONTAL STABILIZER RIB #6 REF SRM 55-10-09-2R-4; FIGURE 202; DETAIL A; SRMSDR SWAA2023112111951Scuff Plate · crackedAFT CARGO COMPARTMENT CENTER SCUFF PLATE FWD CORNER CRACKED<[01] RECEIVED NEW SCUFF PLATE P/N: 146A8342-8; PO# 1578747; ISSUE TAG: WN3585. INSTALLATION OF AFT CARGO SCUFF PLATES TRANSFER TO CARD: TTG8Q002CGYV.;[02] INSTALLATION OF AFT CARGO SCUFF PLATES TRANSFSDR SWAA2023112112110Seat Track · corroded*CORROSION* CABIN SEAT TRACK STA 500D+8 LBL 45.5 WL 208.1 HAS SURFACE CORROSION AT CROWN BOTTOM. 124-001<[01] THIS DAMAGE WILL BE RESOLVED ON OTHER FAULT : TTG8Q00P35DN. (REPAIR OF SEAT TRACK LBL 45.50 FROM STA. 520 TO 500C +10'.);[02] THIS DAMAGE WILL BE RESOSDR SWAA2023112012107Scuff Plate · corrodedAFT CARGO DOOR CUTOUT FWD PLATE-SCUFF EXFOLIATION CORROSION P/N 453A2611-1<[01] RECEIVED NEW AFT CARGO COMPT DOOR CUTOUT FWD PLATE-SCUFF; PN: 453A2611-1 PO: 2033887. PLATE-SCUFF WILL BE INSTALLED PER TASK CARD TTG8Q002CGYV.;[02] VERIFIED STEP 1SDR SWAA2023112012108Scuff Plate · corrodedAFT CARGO DOOR CUTOUT AFT PLATE-SCUFF EXFOLIATION CORROSION P/N 453A2611-2<[01] RECEIVED NEW AFT CARGO COMPT DOOR CUTOUT AFT PLATE-SCUFF; PN: 453A2611-2 PO: 2042531. PLATE-SCUFF WILL BE INSTALLED PER TASK CARD TTG8Q002CGYV.;[02] VERIFIED STEP 1SDR SWAA2023112012112Strip · corrodedAFT CARGO COMP CAP STRIP CORRODED BETWEEN STA 847-947.5 RBL 21'<[01] RECEIVED NEW AFT CAROG COMPT CAP STRIP STA 847 TO STA 947.5 RBL 21; PN: 453A2611Y3 PO: 2028887. CAP STRIP WILL BE INSTALLED PER TASK CARD TTG8Q00P3774;[02] VERIFIED STEP # 1; CAP STRIP WILL BSDR SWAA2023092604173Megaphone · failedAFT EMERGENCY EQUIPMENT COMPARTMENT MAKING AN AUDIBLE CHIRPING SOUND DURING CRUISE.<[01] REMOVED AND REPLACED AFT EMERGENCY COMPT MEGAPHONE REF AMM 25-64-00.SDR SWAA2023091499901Sign · missingOVERWING EXIT SIGN (ABOVE AISLE) MISSING FRONT FACEPLATE<[01] INSTALLED NEW FACEPLATE ON OVERWING EXIT CEILING SIGN IAW SIP.SDR SWAA2023062771877Light · inoperativeR/H OVERWING EXIT SIDEWALL LIGHT INOP<[01] REPLACED FUSE AND RELAMPED PER AMM 33-51-01SDR SWAA2023062670749Lamp · inoperativeRIGHT EMERGENCY EXIT SIDEWALL LIGHT INOP<[01] REMOVED AND REPLACED R/H EMERGENCY EXIT SIDEWALL LAMP PER AMM 33-51-01SDR SWAA2023040423015Sign · brokenAFT GALLEY LH LOWER EXIT SIGN BROKEN<[01] R&R EXIT SIGN LT ASSY AFT GALLEY LH LOWER PER MM 33-51-01SDR SWAA2022072030210Girt Bar · out of adjustFLIGHT ATTENDANT REPORTS FORWARD SERVICE DOOR GIRT BAR IS DIFFICULT TO INSTALL AND REMOVE. / [01] ADJUSTED GIRT BAR PER SIP. OPS CHECK GOOD.SDR SWAA2022041191976Rope · missingLH OVERWING EMERGENCY EXIT GUIDE ROPE NOT INSTALLED / STOWED PROPERLY / [01] RE-STOWED LH OVERWING EMERGENCY EXIT GUIDE ROPE; PER AMM 25-61-10.SDR SWAA2021120850631Sign · inoperativeSUPPLEMENTAL INFORMATION: EMERGENCY EXIT SIGNS FWD OF R/H OWE (IN CABIN) & ON G4 GALLEY HAVE BULBS OUT. ; / [01] REMOVED AND REPLACED EMERGENCY EXIT SIGNS LIGHTS FWD OF R/H OWE ; (IN CABIN) AND IN G4 GALLEY. PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT SSDR SWAA2021120647369Scuff Plate · crackedAFT CARGO COMPARTMENT FWD SCUFF PLATE CRACKED. ; / [01] ACB FWD SCUFF PLATE FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.<BR><BR>LOCATED AND DRILLED NEW ACB FWD SCUFF PLATE P/N
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