N781WN, cancelled Sep 16, 2024
Service difficulty reports · 314
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 = 'N781WN' AND deregistration_id = 'N781WN-2024-09-16' 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 = 'N781WN' AND deregistration_id = 'N781WN-2024-09-16' 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 SWAA2023051248009Cover · missingAFT SERVICE DOOR EMERGENCY EXIT LENSE COVER MISSING<[01] REPLACED LANES PER MM 33-51-01SDR SWAA2023042028968Circuit Breaker · popped'INFO ONLY' AFTER POWER TRANSFER TO GROUND FOUND EMERGENCY LIGHTING AND FASTEN SEAT BELTS PO-CB POPPED RESET PER MOC(ROBERT). BOTH SYSTEMS OPERATE NORMALLY NO 10 DAY HISTORY.<[01] INFO NOTED BY MX.SDR SWAA2023030711829Sign · looseCABIN CEILING OVERWING EMERGENCY EXIT SIGN IS LOOSE<[01] RE-SECURED CABIN CEILING OVERWING EMERGENCY EXIT SIGN; PER AMM 33-51-01SDR SWAA2023030711801Girt Bar · out of adjustAFT ENTRY DOOR GIRT BAR RETAINING CLIPS REQUIRE ADJUSTMENT<[01] ADJUSTED AFT ENTRY DOOR GIRT BAR RETAINING CLIPS PER AMM 25-66-01SDR SWAA2023030711799Girt Bar · out of adjustAFT SERVICE DOOR SLIDE GIRT AND GIRT BAR CLIPS REQUIRES ADJUSTMENT<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT AND GIRT BAR CLIPS PER MT 725-61-06;[02] REF TECHNICIAN 1. FOR WORK ACCOMPLISHEDSDR SWAA2023030711810Panel · crackedR/H WING TE SHELF PANEL 651FB WEDGE FAIRING CRACKED/DAMAGED.<[01] ADJUSTED R/H WING TE SHELF PANEL 651FB PER AMM 27-51-11.;[02] PERFORMED R/H MAIN LANDING GEAR WHEEL WELL STRUT DOOR ADJUSTMENT PER AMM 32-13-11. NO DEFECTS NOTED.;[03] ADJUSTED R/H WING TE SHELFSDR SWAA2022112173757Floor Panel · splitAFT CARGO BIN FLOOR HAS A SPLIT / [01] FOUND AFT CARGO FLOOR PANEL 140BF WITH 2 CRACKS 15? AND 9?. OK TO CONTINUE PER MEL25-16-01 SP1B. AUTH 104453;[02] WORKING MEL 25-16-01. R+R AFT CARGO BIN FLOOR IAW AMM 25-52-10. THIS CLEARS MEL 25-16-01.SDR SWAA2022101459576None · deterioratedLEFT WING OB AFT FLAP SEPARATED AT TE APPROX 4 AT IB END. LEFT WING OB AFT FLAP SEPARATED AT TE APPROX 4 AT IB END. / [01] DISBOND MEASURES AT 5' INBD TO OTBD AND 3.5'FORE AND AFT APPLIED SEALANT 5-95 TO VOID AND APPLIED SPEED TAPE TO AFFECTED AREASDR SWAA2022092949079Module · damagedEMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WITH SWITCH OFF / [01] REMOVED AND REPLACED AFT ATTENDANT PNL LIGHTING MODULE REF AMM 25-25-11. PERFORMED EMERGENCY LIGHT OPS CHECK FOUND WORKING NORMAL PER AMM 33-51-00.SDR SWAA2022092930901Module · faultedEMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WITH SWITCH OFF / [01] REMOVED AND REPLACED AFT ATTENDANT PNL LIGHTING MODULE REF AMM 25-25-11. PERFORMED EMERGENCY LIGHT OPS CHECK FOUND WORKING NORMAL PER AMM 33-51-00.SDR SWAA2022092616197Holder · looseFORWARD SERVICE DOOR EMERGENCY SLIDE BRACKET IS LOOSE. / [01] RE-SECURED SLIDE GIRT BAR HOLDER REF. SIP.SDR SWAA2022090851132Panel · elongatedSEVERAL 193B PANEL FASTENER HOLES ARE ELONGATED AND HAS WORN THROUGH THE COMPOSITE MATERIAL. / [01] R&R 193 PANELSDR SWAA2022070725295Light · inoperativeRIGHT WING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED RT WING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOODSDR SWAA2022021471116Panel · elongatedWING TO BODY 194E PANEL HAS SEVERAL ELONGATED FASTENER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 194E PER AMM 53-51-21 FIG 1SDR SWAA2022021471119Panel · crackedWING TO BODY 194E PANEL HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY 194E PANEL PER A AMM.53-51-21. FIG 1SDR SWAA2022021471117Panel · crackedWING TO BODY 193D PANEL HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY 193D PANEL PER AMM 53-51-21 FIG 1SDR SWAA2022021471118Panel · elongatedWING TO BODY 193D PANEL HAS SEVERAL ELONGATED FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED 193D PANEL PER AMM 53-51-21 FIG 1SDR SWAA2021120348701Panel · delaminatedL/H LOWER WING TO BODY PANEL AFT OF L/H MAIN GEAR W/W PANEL 193CL IS DELAMINATED ; DELAM DIMENSIONS ARE APPROXIMATELY 12? Y 9.5? / [01] REPLACED PANEL PER MM 53-51-21SDR SWAA2021102231008Girt Bar · looseSUPPLEMENTAL INFORMATION: AFT ENTRY DOOR GIRT BAR LOOSE ; / [01] RESECURED AFT ENTRY GIRT BAR PER SIPSDR SWAA2021092220570Door · out of adjustAFT SERVICE DOOR HANDLE RAISES UP 4 FEW INCHES WHEN THE AIRCRAFT PRESSURIZES ; / [01] FOUND AFT GALLEY SERVICE DOOR HORIZONTAL CONTOL ROD OUT OF RIG. ADJUSTED CENTER CONTROL ROD I/A/W AMM 52-41-00. PREFORMED ADJUSTMENT TEST. I/A/W AMM 52-13-00. PRESSURIZED AIRSDR SWAA2021081707235Panel · crackedLEADING EDGE PANEL 621YB HAS 1IN CRACK ALONG OUTBD FWD EDGE. CRACK IS ALONG THE INBD-AFT EDGE. OK TO CONTINUE ON MX NOTE PER MPM 53-05-09A. REINSPECT EVERY 3 DAYS, WITH PERMANENT REPAIR WITHIN 20 DAYS. AUTHORIZATION CODE 22789. R&R PAL REF AMM 57-41-02.SDR SWAA2021062380201Angle · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD LWR TRANSITION ANGLE;SHOW SIGNS OF SURFACE CORROSION IN SEVERA AREAS ; / PART REPLACED WITH NEW TRANSITION ANGLE P/N 143A9485-35 INSTALLATION WILL BE ACCOMPLISH T/C TTG8Q004EBSC; VERIFIED 1SDR SWAA2021062479693Cap · corrodedFOUND SEVERAL EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS FROM STA 847 THROUGH STA 947.5 ; / LOCATED AND DRILLED CAP STRIP PER B737-700 SRM 51-40-05-0G-0.;PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.038SDR SWAA2021062479687Cap · corrodedFOUND EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS RT SIDE FROM STA 727+4 THROUGH STA 787 ; / PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.039'<BR>TOOL USED MG27 BC:172139;REMOVED CORROSION AT AFT CARGO CSDR SWAA2021062479688Cap · corrodedFOUND SEVERAL EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS LT SIDE FROM STA 727+4 THROUGH STA 847. ; / PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.041'<BR>TOOL USED MG27 BC:172139;REMOVED CORROSION FROM SDR SWAA2021062379260Bonding Jumper · missingAFT ENTRY DOOR SLIDE COMPARTMENT MISSING FWD AND AFT BONDING JUMPERS AND STUDS ON BACKING PAN / AFT ENTRY DOOR SLIDE COMPARTMENT P/N 416A2200-11A WAS MODIFIED ON AIRCRAFT PER ACO 6933-25 TO REMOVE BONDING JUMPERS AND STUDS.; VERIFIED STEP 1SDR SWAA2021062378225Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241DF DELAMINATED AT UPPER SURFACE ; / STEP 2 COMPLIED WITH RII INSPECTION;COMPLETE;VERIFIED 1 AND 2;COMPLETE;PREPARED FOR REPAIR DAMAGED AREA TA FLOOR PANEL #241DF PER B737SRM 54-00-50-2R-1;REPAIRED DAMAGED AREA AT FLOOR PANEL #241DF PESDR SWAA2021062378207Floor Panel · damagedFLIGHT COMPARTMENT FLOOR PANEL 211AF ONE ENLONGATED FASTENER'S HOLE ; / APPLIED TOPCOAT TO FLOOR PANEL 211AF AS PER B737-700 AMM 51-21-73-370-804;LOCATED AND DRILLED NEW FLOOR PANLEL 141A5133U15 AS PER B737-700 SRM 51-40-05-0G-0.;RECIEVED FLOOR PANEL 211AF P/NSDR SWAA2021062378205Sign · crackedMAIN CABIN SEAT ROW 10 L/H EXIT SING CRACK ; / REMOVED AND REPLACED MAIN CABIN SEAT ROW #10 L/H EXIT SIGN AS PER B-737-700 AMM 33-51- 01-960-802.; VERIFIED 1SDR SWAA2021062377026Floor Panel · deterioratedAFT CARGO COMPARTMENT FLOOR PANEL 140BF IS DETERIORATED. [200-011] ; / AFT CARGO FLOOR PANEL 140BF WILL BE INSTALLED ON TASK CARD TTG8Q004EYM2.;FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140BF PER B737-700 AMM 25-52-01-201-801.;REMOVED PANEL 140BF;REMOVED PASDR SWAA2021062377025Floor Panel · deterioratedAFT CARGO COMPARTMENT FLOOR PANEL 140AF IS DETERIORATED. [200-010] ; / AFT CARGO FLOOR PANEL 140AF WILL BE INSTALLED ON TASK CARD TTG8Q004EYM2.;FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140AF PER B737-700 AMM 25-52-01-201-801.;REMOVED PANEL 140AF;REMOVED PASDR SWAA2021062377015Floor Panel · crackedFWD CARGO COMP FLOOR PANEL 120CF CRACKED ; / FABRICATED FLOOR PANEL #120CF AS PER REF B737-700 AMM 25-52-01-201-801;FLOOR PANEL INSTALLATION WILL BE ACCOMPLISH ON T/C TTG8Q004EBSC;VERIFIED STEPS 1 TO 3;REMOVED FLOOR PANEL PER AMM25-52-01-201-801SDR SWAA2021062376693Door · out of rigR-2 DOOR OUT OF RIG (HITTING ON BOTH FWD LATCH CRANKS) ; / FINALIZED R-2 DOOR ADJUSTMENT IN REF B737 AMM 52-41-00-820-801.;PERFORMED (R2) GALLEY SERVICE DOOR ADJUSTMENT CHECK UP TO AND INCLUDING STEP 2.M.(3)(C)(4) PG.12 IN REF B737 AMM 52-41-00-820-801;RE-INSTSDR SWAA2021042665875Battery Pack · no testBATTERY PACKS POWER SUPPLIES FAILED CAPACITY TEST AT FOLLOWING LOCATIONS M1673;M1672;M1675 M1674. R AND R 'D BATTERY PACKS POWER SUPPLIES AT FOLLOWING LOCATIONS M1673;M1672;M1675; M1674 PER AMM335106SDR SWAA2021030151956Rib · crackedR/H HORIZONTAL STAB; RIB AT STATION 101.9 CRACKED AT 4TH VERTICAL STIFFNER AFT OF FRONT SPAR HFEC VERIFIED PER 737 NDT PART 6 PROCEDURE 23 / REMOVED CRACKED RIB. THEN REPAIRED AND REINSTALLED SERVICEABLE RIB IAW SRM 55-10-09-2R & SRM 51-40-02SDR SWAA2021030151958Rib · crackedRIB AT STAB STA. 78.29 CRACKED / REMOVED AND REPLACED RIB AT STA. 78.29 PER SRM 51-40-02SDR SWAA2021030151959Rib · crackedRIVET PULLED AT RIB STAB STA. 114.55 LOWER SIDE AND RIB CRACKED. / REMOVED AND REPLACED RIB AT STA 119.55 PER SRM 51-40-02SDR SWAA2021081879958Plate · crackedAFT CARGO DOOR AFT LWR BEARING PLATE CRACKED / REMOVED AND REPLACED PER AMM 52-31-00.SDR SWAA2021052511390Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING LOWER INBD HAT SIDE LUG SHOWS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511389Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBOARD HAT SIDE LUG SHOWS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511388Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511387Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B_LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER WA 1-A57-3246 REV 11SDR SWAA2021052511384Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING; LOWER I/B LUG BORE EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511386Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING UPPER I/B LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511383Trunnion · corrodedL/H MLG FWD TRUNNION_SUPPORT FITTING UPPER I/B LUG EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511385Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING; UPPER O/B_LUG FACE EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511382Trunnion · corrodedLEFT WING MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511379Trunnion · corrodedLEFT WING MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511381Trunnion · corrodedLEFT WING MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11SDR SWAA2021052511380Trunnion · corrodedLEFT WING MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11
Back to N781WN, cancelled Sep 16, 2024