N494WN
Service difficulty reports · 335
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 = 'N494WN' 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 = 'N494WN' 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 SWAA2022080124886Rib · crackedCRACK INSPAR RIB AT STAB STA 92.70 AND 21 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-372683 / [01] TOOL USED PN NORTEC 600D; SN. 60009161631; DUE DATE: 03-DEC-22;[02] REPAIRED INSPAR RIB 92.70 IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 LT HORIZONTAL STAB.SEE INSDR SWAA2022080124890Rib · crackedCRACK INSPAR RIB AT STAB STA 111.10 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-372686 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DSDR SWAA2022080124891Rib · crackedCRACK INSPAR RIB AT STAB STA 111.10 AND 10 INCH FROM REAR SPAR LT HORIZONTAL STAB 2022-372689 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DASDR SWAA2022061015829Duct · smokeON TAKEOFF DUCT TEMP WENT TO OVER 110 DEG AND A STRONG ACRID BURNING SMELL AND FAINT SMOKE WAS IN COCKPIT. FLIGHT ATTENDANTS ALSO SMELLED WHAT THEY THOUGHT WAS PLASTIC BURNING IN THE BACK OF THE AIRCRAFT. RETURNED TO DEPARTURE AIRPORT / [01] PERFORMED FIM TASKSDR SWAA2022032486374Light · inoperativeSIDEWALL LIGHT FOR EMERGENCY EXIT DOOR INOP RT SIDE / [01] OK TO CONTINUE PER MEL 33-2-03 SP1B MDDR #5418;[02] REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY OVER RT EMERGENCY EXIT DOOR. OPS CHECK GOOD IAW AMM 33-21-00SDR SWAA2022031680557Angle · crackedBS 663; RBL 34; WL 195; .400' CRACK IN CENTER WING BOX UPPER SKIN TO BS 663 BULKHEAD ATTACH ANGLE ON I/B SIDE OF ANGLE DRAIN HOLE; AREA MARKED IN BLACK. DOT 148-001 / [01] CUT AND REMOVED CRACK DAMAGE AT R/H SIDE INBD DRAIN HOLE AT STA 663 IAW SRM 51-10-02-0G-SDR SWAA2022031680558Angle · crackedBS 663; RBL 33.5; WL 195; .350' CRACK IN CENTER WING BOX TO BS 663 BULKHEAD ATTACH ANGLE AT FASTENER HOLE IN ANGLE. AREA MARKED IN BLACK; DOT 148-002 / [01] CUT AND REMOVED CRACK DAMAGE AT STA 663 RBL 33.5 IAW SRM 51-10-02-0G-0;[02] VERIFIED STEP 1 COMPLETE <BSDR SWAA2022031680562Panel · crackedBS 663.5; RBL 46; WL 201; CRACK IN ATTACH FASTENER HOLE IN STIFFENER ANGLE ON AFT SIDE OF BS 663 BULKHEAD; HOLE MARKED IN BLACK ON FWD SIDE OF BS 663 BULKHEAD; DOT: 148-003 / [01] PERFORMED NDT IAW B737 NDT PT. 6; 51-00-00 PROC 17. NO CRACKS NOTED ON VERTICAL SDR SWAA2022031679270Angle · crackedCRACK FOUND IN A/C BAY ON UPPER ATTACH ANGLE AT STA 663 LBL 8 / [01] REMOVED 24 FASTENERS IN REPAIR AREA OF REPAIR 5 I/A/W SRM 57-10-10-2R-5;[02] CUT AND REMOVED ATTACH ANGLE I/A/W SRM 57-10-10-2R-5 REPAIR 5 STEP 4 B AT L/H 663 LBL 8 AT A/C BAY ON UPPER ATTACHSDR SWAA2022031678945Angle · crackedCRACK FOUND ON LOWER ATTACH ANGLE AT STA 663 OUTBOARD SIDE OF RBL 45 / [01] RECEIVED -1 REPLACEMENT ANGLE FABRICATED ON WORKSHOP WORK ORDER 43273-6000-0005 AND -2 SPLICE ANGLE FABRICATED ON WORKSHOP WORK ORDER 43273-6000-0006 I/A/W EA NO.22-157-00638-WIP1 STEPSDR SWAA2022031678946Angle · crackedCRACK FOUND IN A/C BAY AT STA 663 UPPER ATTACH ANGLE AT RBL 9 / [01] REMOVED FASTENERS IN REPAIR AREA FOR STEP 4A OF SRM 57-10-10-2R-5 REPAIR 5 ;AND SRM 51-40-02-0G-0;[02] CUT AND REMOVED DAMAGE SECTION OF ATTACH ANGLE AT STA 663 R/H A/C BAY UPPER ANGLE AT RBLSDR SWAA2021083010634Lamp · inoperativeLH OVERWING EXIT EMERGENCY LIGHT INOP / [01] RELAMPED PER AMM 33-51-04. OPS CHK OK.SDR SWAA2021031153696Sign · brokenPAX ENTRY DOOR EXIT SIGN BROKEN / R/R L1 ENTRY DOOR EMERGENCY LIGHT SIGN REF AMM 33-51-11; OPS CK GOODSDR SWAA2021022650898Slide · low pressureAFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE LOW / REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PER MT 725-61-06 RAR# 88949 TAG 751601 P/N OFF 5A3307-7 S/N OFF 9488 P/N ON 5A3307-7 S/N ON BNG16325SDR SWAA2021050541774Seal · crackedLH HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED / R&R LH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER MM REF 53-31-31SDR SWAA2021050541775Seal · crackedRH HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED / R&R RH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER MM REF 53-31-31SDR SWAA2021071340081Skin · delaminatedREFERENCE ORIGINAL DEFECT# 1187133. LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE SKIN SPANWISE AND 0.75' LOWER AFT EDGE SKIN CHORDWISE. / DMA# 1187133 REMOVED AND REPLACED OUTBOARD AFSDR SWAA2021071340080Skin · delaminatedREFERENCE ORIGINAL DEFECT# 1187131. LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE SKIN SPANWISE AND 0.75' FROM LOWER AFT EDGE SKIN CHORDWISE. / DMA# 0258744 REMOVED AND REPLACED OUTBOASDR SWAA2021060439963Skin · delaminatedDURING MAINTENANCE CHECK; FOUND LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE OF SKIN SPANWISE AND 0.75' FROM LOWER AFT EDGE OF SKIN CHORDWISE. / DMA# 0258743 REMOVED AND REPLACED OUTBSDR SWAA2020082609750Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE FAIRING INNER INB. # 3 &4 RIBS CRACKED AT FLANGES MKD DOTS / REMOVED AND REPLACED RIBS #3 AND 4 AT LT HORIZ. STAB. L/E STA 95.96 AND STA 105.26 PER BOEING 737-700 SRM 51-40-02-0G-0 AND DRAWING # 186A1200; 186A1303 AND 18SDR SWAA2020082708097Stiffener · crackedLT HOR. STAB. INSPAR RIB NR 5 AT STA 129.50 WITH NR 2 STIFFNER CRACKED. REPAIR THE STIFFENER IAW SRM 55-10-09-2R-4SDR SWAA2020082707512Stiffener · crackedLEFT HORIZONTAL STAB INSPAR RIB ASSY # 5; AT STA 129.50; HAS A CRACK AT STIFFENER #3 LOWER AREA. (MKD 78-12). REPAIRED STIFFENER #3 AT RIB ASSY #5 STA 129.50 AS PER REF B737-700 SRM 55-10-09-2R-4SDR SWAA2020082707513Stiffener · crackedLEFT HORIZ STAB INSPAR RIB ASSY #5; AT STA 129.50; HAS A CRACK AT STIFFENER # 4 LOWER AREA. (MKD 78-13). REPAIRED STIFFENER #4 AT RIB #5 STA 129.50 AS PER REF B737-700 SRM 55-10-09-2R-4SDR SWAA2021072807413Support Angle · crackedFWD CARGO COMPMT. BILGE SUPPORT CLIP CRACKED AT S-27R AND STA 500 MKD DOT 60-022 / REMOVED AND REPLACED SUPPORT CLIP AT FWD CARGO STA 500 S-27R AS REF B737-700 SRM 51-40-02-0G-0SDR SWAA2021071507426Floor Support · corrodedCORROSION AFT OF AFT CARGO COMPMT. BILGE FLOOR SUPPORT ANGLE FASTENER HOLES BETWEEN STA 927 & 947.5 RBL-13.8 WL155.5 MKD DOT 60-028 / FOUND DEEP CORROSION AROUND FASTENERS OUT OF LIMITS AT AFT CARGO FLOOR SUPPORT ANGLE (TRACK) STA 927 TO 947 AS PER REF. B737-7SDR SWAA2021052607060Gusset · crackedFWD CARGO COMPARTMENT; FWD OF (AFT BULKHEAD) STA 500D; S20L ANGLE NOTED CRACKED. / REMOVED AND INSTALLED NEW GUSSET (ANGLE) AS PER B737-700 SRM 51-40-02-0G-0.SDR SWAA2021040807430Channel · corrodedCORROSION AFT CARGO COMPMT. BILGE FLOOR SIDE Z CHANNEL FROM STA 727E + 10 TO STA 847 S-26L WL 155.5 MKD DOT 60-032 / REMOVED DAMAGED Z CHANNEL AND REPLACED AT AFT CARGO L/H STA 727E TO STA 847 AS PER B737-700 SRM 51-40-02-0G-0 AND DWG # 146A7502. FOUND DEEP COSDR SWAA2021081208850Skin · debondedAPU COMPARMRNT DOOR SKIN EDGE DISBOUNDED AREA AFT OF FWD HINGE MKD DOT / RESECURED DISBOUNDED AREA AT AFT OF FWD HINGE OF APU COMPARTMENT DOOR AS REF B737-700 SRM 51-40-02-0G-0 AMM 51-31-00-390-810SDR SWAA2021072207056Floor Panel · crackedBELOW CABIN FLOOR WING CENTER SECTION STA 540 RBL 1 LATERAL FLOOR SUPPORT PANEL BREAK IS CRACKED. [DOT 124-021] / REMOVED AND REINSTALLED FLOOR PANEL #231UF AS PER AMM 53-21-00-000-801. REMOVED AND REPLACED FLOOR SUPPORT BRACKET STA 540RBL 1' AS PER SRM 51-40-SDR SWAA2021072207055Floorbeam · crackedBELOW CABIN FLOOR WING CENTER SECTION STA 540 LBL 1 LATERAL FLOOR SUPPORT PANEL BREAK IS CRACKED. [DOT 124-020] / REMOVED LATERAL FLOOR SUPPORT CRACKED STA 540LBL 1' AND INSTERTED NEW FLOOR SUPPORT AS PER SRM 51-40-02-0G-0SDR SWAA2021072207509Strap · corrodedCORROSION AFT CARGO COMPMT. BILGE FLOOR SUPPORT STRAP AT STA 767+6 LBL 21 TO RBL 21 AND WL 155.5 MKD DOT 60-034. / FOUND DEEP CORROSION AROUND FASTNERS AT AFT CARGO BILGE FLOOR SUPPORT STRAP STA 767+6; LBL-21 TO RBL-21 AND WL 155.5 AS PER REF. B737-700 SRM 53SDR SWAA2021040507043Floor Panel · damagedAFT CARGO FLOOR PANEL 140BF HAS DAMAGE / FABRICATED NEW FLOOR PANEL AT AFT CARGO COMP # 140BF PER B737-700 AMM 25-52-01-201-801SDR SWAA2021040507042Floor Panel · damagedAFT CARGO FLOOR PANEL 140AF HAS DAMAGE / FABRICATED NEW FLOOR PANEL AT AFT CARGO COMP # 140AF PER B737-700 AMM 25-52-01-201-801SDR SWAA2020082708844Floor Skin · dentedCOCKPIT FLOOR UNDER 2ND. OBSERVER SEAT APPROX. STA. 260 IS DENTED; WL 207.54; LBL 14 TO RBL ACCOMPLISHED PERMANENT REPAIR AT COCKPIT FLOOR WEB APPROX STA 260; WL 207.54 FROM LBL 20 TO RBL 5 PER EA 1-A53-33179 REV1 FIG.1.SDR SWAA2020032634201Light · looseEXIT SIGN HANGING OFF CEILING / R&R LIGHT ASSY ; RESECURED AND OPS CHECK PER M/M 33-51-04 & 33-51-00SDR SWAA2020012040542Sign · detachedOVERWING EXIT SIGN DETACHED, WAS HANGING BY WIRES. SECURED SIGN PER MM.SDR SWAA2022032160253Bracket · crackedLH FWD UPPER WING TO BODY FAIRING AFT SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02SDR SWAA2022032160256Skin · corrodedEVIDENCE OF CORROSION UNDER LOWER ATC ANTENNA ON FUSELAGE SKIN. STATION 354 BL 0. / REMOVED CORROSION, BLENDED SKIN AND REAPPLIED PROTECTIVE FINISH IAW EA 1-753-35640.SDR SWAA2018090424743Structure · crackedR1 DOOR UPPER HINGE BOX ASSEMBLY CRACKED ON THE PRODUCTION BEVELED EDGE. REPAIRED BOX ASSEMBLY PER EA AND ER. IRSDR SWAA2018082824655Plate · crackedRT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE IAW SRM.SDR SWAA2022021760501Scuff Plate · crackedSUPPLEMENTAL INFORMATION: AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE PER EA# 1-A53-2076 REV 11SDR SWAA2022021760500Scuff Plate · crackedSUPPLEMENTAL INFORMATION: AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE PER EA# 1-A53-2076 REV 11; UPON INSTALLATION SCUFF PLATE CRACKED REMOVED AND REPLACED WITH NEW FWD CORNER SCUFF PLATE I.A.W AMM 53-11-02-0SDR SWAA2022021760504Web · crackedRT WING UPPER T/E PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB IS CRACKED ON FWD FLANGE / REMOVED AND REPLACED RIGHT WING UPPER TRAILING EDGE SUPPORT WEB ABOVE PYLON AFT TIP IAW SRM 51-40-02-0G-0 STEP 4 AND SRM 51-40-05-0G-0.SDR SWAA2018090424742Beam · crackedR1 DOOR NR 4 LOWER BEAM INBOARD SIDE OF RADIUS CRACKED. R&R DOOR PER AMM.SDR SWAA2018090424732Seat Track · corrodedSEAT TRACK CORRODED BETWEEN BS 500D+9 TO BS 520, LBL 45. REPAIRED SEAT TRACK IAW ER AND EA.SDR SWAA2018082924674Skin · corrodedFUSELAGE SKIN CORRODED AT BS 887, STR 25R. R&R SKIN IAW SRM.SDR SWAA2018082824654Support Angle · crackedRT WING TRAILING EDGE SUPPORT ANGLE ATTACHED TO DEFLECTION CONTROL RIB AND TRANSVERSE WEB CRACKED. R&R WEB IAW SRM.SDR SWAA2022021760497Web · crackedNOTED CRACK COMMON TO THE L/H SPAR VERTICAL PRESSURE WEB STA.663 WL. 200 LBL 29 / REPAIRED PER EA 1-757-15464 REV. IR AND ER 18-03794 REV. IR.SDR SWAA2018083024698Lens · crackedRT OVERHEAD BIN EMERGENCY LIGHT LENSES CRACKED. R&R LENS IAW AMM.SDR SWAA2018083024697Lens · crackedLT OVERHEAD BIN EMERGENCY LIGHT LENSES CRACKED. R&R LENS IAW AMM.
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