N257WN
Service difficulty reports · 305
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 = 'N257WN' 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 = 'N257WN' 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 SWAA2024081309101Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK IN THE WELL LBL45 BS727; BS727A+12 WL208.<[01] COMPLETED STEPS 1; 2 AND 3.;[02] COMPLETED STEP 5;[03] REMOVED AND REPLACED PASSENGER CABIN SEAT TRACK FROM LBL 45 BS 540 TO BS 727B WL 208 PER SRM 51-40-02-0G-0 AND BOEING SDR SWAA2024081308771Panel · crackedL/W L/E PANEL 521TB CORNER IS CRACKED<[01] L/W L/E PANEL 521TB CORNER WITH CRACKED WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024080908760Skin · crackedCRACK FOUND DURING HFEC INSPECTION OF LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 18' FROM FWD EDGE; L: 0.5' MARKED<[01] REPAIRED DAMAGE TO LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.9; 18' FROM FWD EDGE; L: 0.5' IAW SRM 55-10-01-2R-11.;[0SDR SWAA2024080908576Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241YF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0077.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024080908577Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ABF AFT FLOOR PANEL UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0088.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024080908571Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREA OF PULLED STRANDS ON UPPER SKIN AND DAMAGED AREA FOUND ON LOWER SKIN ON AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024080908574Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 242UF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0095.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.;[03] RII INSPECTSDR SWAA2024080908578Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 242VF AFT FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0350.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024080908569Stiffener · crackedRIGHT HORIZONTAL STAB RIB #4 STIFFENERS 2 & 3 ARE CRACKED IN THE LOWER RADIUS.<[01] REPAIRED R/ HOR. STAB. RIB #4; STIFFENER 2 IAW SRM 55-10-09-2R-4 REPAIR 4; FIG. 202; DETAIL A AND SRM 51-40-05-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND STEPS; CARD COSDR SWAA2024080908566Floor Panel · debondedCABIN FLOOR PANEL 241BF UPPER SKIN HAS A LARGE DISBOND NEAR CENTER OF PANEL.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW CABIN FLOOR PANEL 241BF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0189;[02] VERIFIED COMPLETESDR SWAA2024080908575Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024080909107Floor Panel · deformedCABIN FLOOR PANEL 241CF LOWER SKIN HAS AN IMBEDDED SCREW. (MARKED)<[01] FABRICATION OF NEW 241CF FLOOR PANEL WAS ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0130.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024081307803Support Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+5;21 INCH AFT OF REAR SPAR; SUPPORT BRACKET REAR FACE HAS CRACK.<[01] REMOVED AN REPLACED SUPPORT BRACKET AT R/WING TE ORRS 261+5;21 INCH AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081307807Attach Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+11;15 INCH AFT OF REAR SPAR; O/B ATTACH BRACKET HAS CRACK.<[01] REMOVED AND REPLACED BRACKET AT R/WING TE; ORRS 261 + 11.15 INCH AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081308032Support Bracket · crackedLH WING TE: DEFLECTION CONTROL RIB AT ORRS 261; 18 INCHES AFT OF REAR SPAR; SUPPORT BRACKET FRONT FACE HAS CRACK.<[01] TASK COMPLETE: <BR>REMOVED CRACKED BRACKET AND REPLACED WITH NEW (PN: 115A2953-1 LOT: 238381/039685) IAW SRM 51-40-02-0G-0 4.B.;[02] VERIFIEDSDR SWAA2024081308033Support Bracket · crackedLH WING TE: DEFLECTION CONTROL RIB AT ORRS 261+8; 17 INCHES AFT OF REAR SPAR; SUPPORT BRACKET AFT FACE HAS CRACK.<[01] TASK COMPLETE: <BR>REMOVED CRACKED BRACKET AND REPLACED WITH NEW (PN: 115A298291 LOT: 234768/033958) IAW SRM 51-40-02-0G-0 4.B.;[02] VERIFIEDSDR SWAA2024081307802Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+5; 19 INCHES AFT OF REAR SPAR; SUPPORT BRACKET FRONT FACE HAS CRACK.<[01] TASK COMPLETE:<BR>CRACKED SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETESDR SWAA2024081307806Support · crackedRH WING TE: DEFLECTION CONTROL RIB ORRS 261+11;18 INCH AFT OF REAR SPAR; REAR SUPPORT ATTACH POINT HAS CRACK.<[01] REMOVED AND REPLACED SUPPORT AT R/WING TE; ORRS 261 + 11.18 AFT OF REAR SPAR IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081308035Skin · corroded#1 ENGINE INLET COWL HAS CORROSION ON BARREL SKIN 1 INCH AFT OF THE INLET LIP AT 12 O'CLOCK POSITION. MARKED<[01] #1 ENGINE INLET COWL REPLACED (FAULT WAS RESOLVED ON ANOTHER FAULT) TTG8Q00S70S4;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024081307180Scuff Plate · crackedAFT CARGO BAY DOORWAY CENTER SCUFF PLATE CRACKED<[01] RECEIVED NEW AFT CARGO BAY CENTER SCUFF PLATE FROM STORES; PART IS TO BE INSTALLED ON CUSTOMER CARD TTG8Q00UCAET;[02] VERIFIED ITEM 1AND TASK CARD COMPLETED.SDR SWAA2024060497499Lens · brokenCAPT SIDE SMALL RECTANGULAR EXIT (LIGHTED) PLACARD ON OVER WING EXIT BROKEN OFF<[01] INSTALLED NEW LENS PER AMM 33-51-01 OPS CHECK GOODSDR SWAA2024022254801Slide · low pressureR1 PACK SLIDE INDICATES IN THE RED<[01] REMOVED AND REPLACED R1 ESCAPE SLIDE PER AMM 25-66-01 AND MT 725-61-06SDR SWAA2024020547793Lens · brokenRIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LENS BROKEN<[01] REMOVED AND REPLACED RIGHT OVER WING EXTERIOR EMERGENCY EXIT LIGHT LENS REF AMM 33-51-04SDR SWAA2023111520940Megaphone · inoperativeAFT MEGA PHONE INOP<[01] REPLACED AFT MEGAPHONE BATTERIES ;OPS CHECK GOOD REF AMM 25-64-00SDR SWAA2023021502182Bolt · faultySEAT 11F IS RECLINING INTO THE EXIT ROW<[01] REMOVED AND REPLACED SEAT 11F BREAKOVER BOLT AND NUT PER CMM 25-21-42. OPS CHECK GOOD.SDR SWAA2022110165272Bracket · brokenKEEL BEAM PANEL 192E FWD INBD MOUNT BRACKET BROKEN / [01] C/W EA 22-153-03209SDR SWAA2022071117371Frame · crackedCRACK FRAME BS 312 BTW STR 5L TO STR 6L AT PASSENGER CABIN 2022-307380 / [01] REPAIRED FRAME UPPER CHORD ON BS 312 AT LBL 33 LOCATED BETWEEN STRINGERS 5L AND 6L I.A.W EA: M-22-153-01244;[02] CORRECTED STEP 1. REPAIRED FRAME UPPER CHORD ON BS 312 AT LBL 33 LOCASDR SWAA2022071117496Rib · crackedCRACK ON FRONT SPAR LOWER AREA OF INSPAR RIB STAB STA 129.50 AT LT HORIZONTAL STABILIZER 2022-307381 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N:38DL PLUS; S/N:120398603; CAL DUE DATE: 18-OCT-22;[02] REPAIRED IAW EA# 22-155-01950; AND EA# 22-155-01950-WIPSDR SWAA2022071116145Rib · crackedCRACK ACCESS PANEL 321A RIB # 8 VERTICAL STABILIZER (1 EA) 2022-307348 / [01] REPLACED RIB # 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 174A0103 REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] CERTIFIED WORK PERSDR SWAA2022071115594Bracket · corrodedCORROSION DORSAL FIN DRAG BRACE LT SIDE AT VERTICAL STABILIZER (1 EA) 2022 307311 / [01] REPLACED DORSAL FIN DRAG BRACE LT SIDE AT VERTICAL STABILIZER IAW. SRM B 737 -700 51-40-02; 51-10-02 ITEM 9 AND DWG #148A8200 REV B SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPSDR SWAA2022071115496Access Panel · crackedCRACK ACCESS PANEL 195CL AT LOWER FUSELAGE 2022-307299 / [01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED HOTBONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE: 16 JAN 23.;[03] TOOL USED SCALE P/N:CL5000 S/N:AE-39882 DUE DATE: 2SDR SWAA2022071115498Cargo Track · crackedCRACK CARGO TRACK LOCATED BS767 RBL13 AND WL156 AT AFT CARGO COMPARTMENT 2022-307279 / [01] PERFOMED REPAIR ON CARGO TRACK LOCATED BS 727D AND BS 787 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND B737-700 SRM 53-00-53-2R-3 REPAIR 3; SEE INDIVIDUAL SIGSDR SWAA2022071115509Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11INCH RBL12 AND WL156 AFT CARGO COMPARTMENT 2022-307307 / [01] REPLACED ANGLE - SUPPORT LOCATED BS907 PLUS 11INCH RBL12 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 147A7221 SHEET 24 SDR SWAA2022071115592Bracket · crackedCRACK BRACKET LOCATED BS947 LBL10 AND WL156 AT AFT CARGO COMPARTMENT 2022-307309 / [01] REPLACED BRACKET LOCATED BS947 LBL10 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 149A8103 REV D;[02] REPLACED BRACKET LOCATED BS947 LBL10 SDR SWAA2022071115508Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BS767 RBL6 AND WL151 AFT CARGO COMPARTMENT 2022-307305 / [01] TOOL USED ULTRASONIC GAGE P/N: 45MG; S/N: 130061901; DUE DATE: 08-APR-23.;[02] INSTALLED WEB AND ANGLES 3 EA LOCATED BS767 RBL6 AND WL151 AFT CARGO COMPARTMENT IASDR SWAA2022071115593Support Angle · corrodedCORROSION ANGLE - SUPPORT LOCATED BS907 PLUS 7INCH RBL16 AND WL156 AFT CARGO COMPARTMENT 2022-307308 / [01] REPLACED ANGLE - SUPPORT LOCATED BS907 PLUS 7INCH RBL16 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 147A7221 SHEET 2SDR SWAA2022071115506Support · corrodedCORROSION SUPPORT ZEE LOCATED BS727C PLUS 10INCH RBL21 AND WL156 AFT CARGO COMPARTMENT 2022-307303 / [01] REPLACED SUPPORT ZEE LOCATED BS727C PLUS 10INCH RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7502 SHEET 2 REV A SEE INDIVIDSDR SWAA2022071115507Web · corrodedCORROSION WEB LOCATED BS767 PLUS 11INCH RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2022-307304 / [01] REPLACED WEB LOCATED BS767 PLUS 11INCH RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02; DWG 146A0081 SHEET 31 REV:- SEE INDISDR SWAA2022071115500Rib · crackedCRACK INSPAR RIB 129.50 AT 16.5 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2022-307287 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE 08-SEP-22 WAS USED;[02] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 16.5 INCHES FROM FRONT SPAR AT LT HORIZONTALSDR SWAA2022071115501Rib · crackedCRACK INSPAR RIB 129.50 AT 25 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2022-307288 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE 08-SEP-22 WAS USED;[02] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 25 INCHES FROM FRONT SPAR AT LT HORIZONTAL STASDR SWAA2022071115504Rib · crackedCUSTOMER REQUEST CRACK INTERNAL CAVITY ON UPPER STRINGER U13 LOCATED BETWEEN INSPAR RIB 24 AND 25 FUEL TANK AT RT WING 2022-307306 / [01] REPAIRED RH WING - UPPER STRINGER LOCATED BTW RIB 24 & RIB 25 AT U-13 IAW EA# 22-157-01834-WIP1; EA# 22-157-01834-WIP2 ANDSDR SWAA2022071115497Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SKIN AT LT WING 2022-307300 / [01] TOOL USED; CALIPER PN: 500-464; SN: 15331926; DUE DATE: 28/SEP/22.;[02] TOOL USED; CALIPER PN: 500-197-30; SN: A21143429; DUE DATE: 11/OCT/22.;[03] TOOL USED: AUDIBLESDR SWAA2022071115153Battery Pack · inoperativeINOP EMERGENCY LIGHT BATTERY PACK M01670 LH SIDE AT PASSENGER CABIN (1 EA) 2022-307192 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK M01670 LH SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805;[02] CORRECTED STEP 1. REPLACED EMERGENCY LIGHTSDR SWAA2022071115169Light · brokenBROKEN SERVICE DOOR LENS ASSY DOWNLIGHT ON HEADER PANEL AT AFT GALLEY AREA (1 EA) 2022-307215 / [01] REPLACED SERVICE DOOR LENS DOWNLIGHT ASSY ON HEADER PANEL AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802;[02] REPLACED SERVICE DOOR LENS DOWNLIGHTSDR SWAA2022071115170Light · brokenBROKEN ENTRY DOOR LENS ASSY DOWNLIGHT ON HEADER PANEL AT AFT GALLEY AREA (1 EA) 2022-307216 / [01] REPLACED ENTRY DOOR LENS AND DOWNLIGHT ASSY ON HEADER PANEL AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802;[02] REPLACED ENTRY DOOR LENS AND DOWNLIGSDR SWAA2022071115173Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-307247 / [01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 143A7902 REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] REPLACED GUSSSDR SWAA2022071115174Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2022-307249 / [01] REPLACED GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DWG#143A7902 SHEET:174 REV: -. SEE INDIVIDUALS SIGN OFF BELOW;[SDR SWAA2022071115139Support Bracket · crackedCRACK SUPPORT BRACKET ASSY LOCATED BS540 AT RBL24.75 TO RBL45.5 AT CENTER WING BOX 2022-307110 / [01] REPLACED SUPPORT BRACKET ASSY LOCATED BS540 AT RBL24.75 TO RBL45.5 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DRAWING 142A0060 SHEET 46 REV -;[02] REPLASDR SWAA2022071115140Angle · crackedCRACK ANGLE LOCATED BS695 AND RBL24.75 AT CENTER WING BOX (1 EA) 2022-307107 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[0SDR SWAA2022071115141Support Bracket · crackedCRACK SUPPORT BRACKET ASSY LOCATED BS540 AT BL0 AND RBL24.75 AT CENTER WING BOX 2022-307109 / [01] REPLACED BRACKET ASSY LOCATED BS540 AT BL0 AND RBL24.75 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 AND DWG 143A5240-36 SHEET 14 REV:-.;[02] CORRECTED CORRECTIV
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