N250WN
Service difficulty reports · 274
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 = 'N250WN' 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 = 'N250WN' 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 SWAA2024052982820Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SH 8; REV -.SDR SWAA2024052982818Web · crackedCRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING. REPLACED WEB AND FASTENERS ON TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 115A 2512 SHEET 14; REV. A.SDR SWAA2024052982815Angle · crackedCRACK ANGLE TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 275 AT LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IAW SRM 51-40-02; SRM 51-10-02,ITEM 9 AND DWG 115A6200 SHEET 11 REV B. MEASURE OF CRACK IS: L 1.727.SDR SWAA2024052982819Web · crackedCRACK WEB TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING. REPLACED WEB AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 115A2512, SHEET 14, REV A. MEASURE OF CRACK ISSDR SWAA2024052982816Rib · crackedCRACK FITTING CONTROL RIB LOCATED ORSS278 AT LT WING. PERFORMED REPAIR ON DEFLECTION CONTROL RIB AREA LT WING IAW SRM 57-51-02-2R-3 REPAIR 3 & SRM 57-51-02-2R-1 REPAIR 1.SDR SWAA2024052982746Web · corrodedCORRODED WEB, FUEL INDICATOR LOCATED INTERNAL CAVITY LE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB IAW EA 24-157-01348 AND EA 24-157-01348-WIP1.SDR SWAA2024052982549Skin · crackedCRACK LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING 2024-286837<[01] ON STEP 3. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[03] PERFORMRD REPAIRSDR SWAA2024052982244Cargo Track · crackedCRACK TRACK RBBL 13.84 LOCATED STA767 AFT CARGO COMPARTMENT 2024-286835<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE:SDR SWAA2024052982240Cargo Track · crackedCRACK TRACK RBBL 13.84 LOCATED STA727E AFT CARGO COMPARTMENT 2024-286833<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATESDR SWAA2024052982241Angle · crackedCRACK ANGLE LOCATED STA947.5 AND LBL10 AFT CARGO COMPARTMENT 2024-286829<[01] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SSDR SWAA2024052982242Floorbeam · crackedCRACK ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2024-286830<[01] REPLACED ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 149A8102SDR SWAA2024052982238Strap · damagedELONGATED HOLE STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286831<[01] REPLACED STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRMSDR SWAA2024052982239Strap · damagedELONGATED HOLE STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286832<[01] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0SDR SWAA2024052982551Angle · crackedCRACK BRACKET ANGLE LOCATED BS 540 PLUS 3 INCHES LBL18 AT AIR CONDITIONING BAY. REPLACED THE BRACKET ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.367.SDR SWAA2024052981956Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-286774<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 ITEM 9;SDR SWAA2024052980773Girt Bar · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-286711<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 STEP 3.D.(1) (A) TO (J);[02] REPLACED GIRT BAR FITTSDR SWAA2024052980940Support Angle · crackedBROKEN ACCESS PANEL 551FB SUPPORT ANGLE AT LT WING. REPLACED THE SUPPORT ANGLE ON ACCESS PANEL 551FB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2710 SHEET: 7 REV -.SDR SWAA2024052981115Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, STEPS (2) & (4) TO (7).SDR SWAA2024052980602Web · crackedCRACK WEB LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA 2024-286676<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AMD DWG 141A5400 SHEET 20 REV:?.SEE INDIVIDUAL STEP SDR SWAA2024052980604Web · crackedCRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286678<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV: ?. SEE INDIVIDUALSDR SWAA2024052980606Web · crackedCRACK WEB LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286680<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV:? .SEE INDIVIDUAL SDR SWAA2024052980605Structure · crackedCRACK INNER CHORD LOCATED BS303 LBL55 AND WL208 AT FWD GALLEY AREA 2024-286679<[01] REPLACED INNER CHORD AND FASTENERS LOCATED BETWEEN BS 270 TO BS 360 LBL55 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SDR SWAA2024052980603Structure · corrodedCORROSION INNER CHORD LOCATED BETWEEN BS312 TO BS328 RBL60 AND WL208 AT FWD GALLEY AREA. REPLACED INNER CHORD INNER CHORD LOC. BTW BS 259.5 - 360; ANGLE & STRAP LOC. ON INNER CHORD IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 & DWG 141A8310 SHEET 25 REV, DWG 141SDR SWAA2024052980373Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 31 STA 663 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 INCH APPROX 2024-286661<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] TOOL USED P/N: NORTEC 500D; S/N: 500X1SDR SWAA2024052980374Floorbeam · corrodedCORROSION ON FLOOR BEAM LOCATED BS986.5 RBL43 AND WL208 AFT GALLEY AREA. PERFORMED REPAIR ON FLOOR BEAM LOCATED BS986.5 BTW RBL40 TO RBL 50 AND WL208 AFT GALLEY AREA. IAW EA 24-153-01239.SDR SWAA2024052980375Web · corrodedCORRODED WEB LOCATED BS 1016 PLUS 11INCH, LBL12 AND WL208, AFT GALLEY AREA. REPLACED WITH A NEW WEB AND FASTENERS IAW 51-40-02, SRM 51-10-02 ITEM 9, & DRAWING 147A5600 SHEET 32 REV B.SDR SWAA2024052980028Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN 2024-286610<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 2SDR SWAA2024052980029Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS695 AND RBL24.75 AT PASSENGER CABIN 2024-286612<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-SDR SWAA2024052979696Isolation Mount · deterioratedDETERIORATED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) 2024-286532<[01] REPLACED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) IAW B737-700 SRM 51-10-02-0G ITEM 9 AND B737-700 SRM 51-40-02.;[02] JOB COMPLETEDSDR SWAA2024052979441Beam · crackedCRACK INDICATION FOUND ON INBOARD RADIUS ADJACENT TO FASTENER HOLE; ON 141A6536-14 BEAM #4 ON FWD SERVICE DOOR. CRACK LENGTH = 0.860 INCHES. 2024-286507<[01] REPLACED BEAM #4 LOCATED BTW BSTA 299 TO BSTA 328. AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. SRMSDR SWAA2024052979011Seat Track · crackedCRACK ON FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) 2024-286474<[01] REPLACED FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) I.A.W B737-700 AMM-25-11?11-400-801<BR>TOOL USED: TRACK SETTING FIXTURE NG BOEING<BR>P/N: 0T900-0247<BR>S/N: AE-3SDR SWAA2024052978844Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN 2024-286467<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:SCALE PN: CR5200 SN:8342514551 DUESDR SWAA2024052978845Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN 2024-286469<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:<BR>SCALE PN: CR5200 SN:8342514551SDR SWAA2024052978414Light · inoperativeDETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA 2024-286419<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-4SDR SWAA2024052978584Wedge · debondedDEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE OB SIDE AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW SRM 57-53-01-2R-7 REPAIR 7.SDR SWAA2024030658916Floor Panel · crackedFORWARD CARGO FLOOR HAS CRACK<[01] OK TO CONT PER MEL 25-16-01 SP1B;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)]SDR SWAA2023092699513Floor Panel · pulledDOT A24-5 MID CABIN FLOOR PANEL 241BF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 RSDR SWAA2023092699514Floor Panel · pulledDOT A24-6 MID CABIN FLOOR PANEL 242AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 RSDR SWAA2023092699521Floor Panel · pulledDOT A24-7 MID CABIN FLOOR PANEL 232RF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGE TO FLOOR BOARD AND IS B.E.R. FABRICATE NEW FLOOR BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4<BRSDR SWAA2023092699520Floor Panel · pulledDOT A24-3 MID CABIN FLOOR PANEL 231XF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF ESDR SWAA2023092699512Floor Panel · pulledDOT A24-4 MID CABIN FLOOR PANEL 241AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF ESDR SWAA2023092699206Vapor Barrier · crackedRIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT EXISTING REPAIR AT APPROX RBL 32 AND RBL 57<[01] REMOVED AND REPLACED WEB 111A1151Y10 ON SHELD IAW SRM 51-40-05-0G-0DWG 111A1151 REV A;[02] VERIFIED STEP 1<BR>AUDIT C/WSDR SWAA2023092699032Light · inoperativeCABIN STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IS INOP<[01] REPLACED LAMPED STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IAW AMM 33-51-03-960-801 OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2023082291674Battery Pack · inoperativeEMERGENCY LIGHTS L1 &R1 BATTERY PACK INOP<[01] R&R BATTERY PACK FOR EMERGENCY LIGHTS R1&R2 M-01674 PER 33-51-06 .OPS CHK GOOD .SDR SWAA2023042530404Battery Pack · inoperativeAFT W4142 EMERGENCY LIGHT BATTERY PACK NEEDS TO BE REPLACED.<[01] REMOVED AND REPLACED AFT W4142 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2022080236707Battery Pack · inoperative2 FORWARD LH BULLNOSE EMERGENCY LIGHTS INOP / [01] R & R LH FWD. BULLNOSE EMERGECY LIGHT BATTERY PACK IAW AMM 33-51-06.SDR SWAA2022052510254Light · inoperativeBURNED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) 2022-228627 / [01] REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) I.A.W B737-700 AMM 33-51-01-960SDR SWAA2022052707249Bracket · elongatedELONGATE HOLE ON BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE 2022-228600 / [01] REPLACED BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART USED HINGE ASSY P/N USED: 146A7414-9 PO: 2022-12SDR SWAA2022052607248Vapor Barrier · crackedCRACK VAPOR BARRIER LOCATED ON BS 663 LBL 65 ON MAIN WHEEL WELL LH SIDE 2022-228599 / [01] TOOL USED CALIPER P/N 500-197-30; S/N A18234378; DUE DATE: 21-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9000B; S/N: 15092096; DUE DATE: 16-JAN-23;[03] TOOL USED SCALE P/SDR SWAA2022053106217Angle · cracked(CUSTOMER REQUEST) CRACK ON BRACKET LOCATED AT BS 663 BETWEEN LBL 45.64 TO LBL 54.21 L/H SIDE MAIN WHEEL WELL 2022-228593 / [01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87-5; S/N: 98740068; DUE DATE
Back to N250WN