N243WN
Service difficulty reports · 293
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 = 'N243WN' 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 = 'N243WN' 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 SWAA2024022244597Stub Frame · crackedCRACK ON STUB FRAME LOCATED ON CUTOUT OF FWD SERVICE DOOR LOCATED BTW BS294.5 TO BS312 AND STR8R 2024-68197 CRACK ON STUD FRAME LOCATED ON CUTOUT OF FWD SERVICE DOOR LOCATED BTW BS294.5 TO BS312 AND STR8R PASSENGER CABIN<[01] REPLACED STUB FRAME LOCATED ON CUTSDR SWAA2024022244598Bear Strap · crackedCRACK ON BEAR STRAP LOCATED BTW BS291.5 TO BS294.5 STR8R AND STR9R PASSENGER CABIN 2024-68196<[01] TOOL USED STEP 3: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24 AND DIGITAL CALIPER; P/N: 500-197-30; S/N: A21147758; DUE SDR SWAA2024022144593Frame · crackedCRACK FRAME ON BS 312 AND BTW STR5L TO STR6L FWD GALLEY AND LAV 2024-68195<[01] REPAIRED FRAME ON BS 312 AND BTW STR5L TO STR6L FWD GALLEY AND LAV IAW EA NO M-22-153-01244 REV B . SEE INDIVIDUAL SIGN-OFFS BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFSDR SWAA2024022343492Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN 2024-68073<[01] REPLACED SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CAB IAW B737-700 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 AND DWG 146A7901 REV A SHEET 66.<BR>CRACK L=0SDR SWAA2024022243490Bulkhead Web · crackedCRACK ON WEB LOCATED BS1016 UPPER POSITION LBL25 AT PASSENGER CABIN 2024-68068<[01] PERFORMED REPAIR ON WEB LOCATED BS1016 UPPER POSITION LBL25 AT PASSENGER CABIN IAW EA 24-153-00311-WIP1 AND 24-153-00311 SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1 COMSDR SWAA2024022342871Plate · crackedCRACK ON SEAL PLATE LOCATED ON FLOOR STRUCTURE BS 1016 AND RBL 38 AFT GALLEY AREA 2024-68029<[01] REPLACED SEAL PLATE LOCATED ON BS 1016 AND RBL 38 AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 140A8970 SHEET: 20 REV: B<BR>SEE INDIVIDUSDR SWAA2024022343146Bracket · corrodedCORROSION ON BRACKET LOC. STA 312 AND AT LEVEL LBL 50 FWD GALLEY AREA 2024-68036<[01] REPLACED BRACKET LOC. STA 312 AND AT LEVEL LBL 50 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED BRACKET LOC. STA 312 AND AT LEVEL LBL 50 FWDSDR SWAA2024022242864Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE LOCATED BS 986.5 AND LBL 47 AFT GALLEY AREA 2024-68021<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X11290U021704 DUE DATE: 12-MAR-24.;[02] PERFORMED PERMANENT REPAIR LOC ON FLOOR BEAM UPPER SURFACE LOCATED SDR SWAA2024022242865Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE LOCATED BS 986.5 AND RBL 45.5 AFT GALLEY AREA 2024-68022<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X11290U021704 DUE DATE: 12-MAR-24.;[02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM UPPER SURFACE LOCATED BSSDR SWAA2024022242863Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 20 INCHES FROM FRONT SPAR EDGE AT LT HORIZONTAL STABILIZER 2024-68016<[01] STEP 3 AND 4 EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N:210138003; DUE DATE: 27-MAR-24;[02] TOOL USED ON STEP 6 AND STEP 7; EDDY CURRSDR SWAA2024022242866Intercostal · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AND LBL 45.60 PASSENGER CABIN 2024-68025<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AND LBL 45.60 PASSENGER CABI IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV -<BR>SDR SWAA2024022242867Intercostal · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AND RBL 31.60 2024-68026<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AND RBL 31.60 PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 39; REV -<BR>SEE INDIVIDUAL SDR SWAA2024022242868Floor Support · crackedCRACK ON WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE BS 344 TO BS 360 AND LBL 1 AT PASSENGER CABIN 2024-68027<[01] REPLACED WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE BS 344 TO BS 360 AND LBL 1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG SDR SWAA2024022242862Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.900 INCHES 2024-68014<[01] TOOL USED ON STEP 6 EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200053402SDR SWAA2024022342847Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE SERVICE DOOR AT AFT GALLEY AREA 2024-67938<[01] REPLACED GIRT BAR FITTING HARDWARE SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(1)(G)(H)(I)(J).;[02] CORRECTIVE ACTION CERTIFIEDSDR SWAA2024022342849Fitting · deterioratedDETERIORATED GIRT BAR FITTING ENTRY DOOR HARDWARE AT AFT GALLEY AREA 2024-67941<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(1)(G)(H)(I)(J);[02] JOB COMPLETEDSDR SWAA2024022342331Nut · deterioratedDETERIORATED ENTRY DOORWAY LINNING NUT OF ASSY HANDLE AT AFT GALLEY AREA (2 EA) 2024-67893<[01] REPLACED ENTRY DOORWAY LINNING NUT OF ASSY HANDLE AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5);[02] CERTIFIED WORK PERFORMED.SDR SWAA2024022342332Nut · deterioratedDETERIORATED SERVICE DOORWAY LINNING NUT OF ASSY HANDLE AT AFT GALLEY AREA (2 EA) 2024-67894<[01] REPLACED SERVICE DOORWAY LINNING NUT OF ASSY HANDLE AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5);[02] CERTIFIED WORK PERFORMED.SDR SWAA2024022242334Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 30 STA 663 AT PASSENGER CABIN; CRACK LENGTH: 0.450 INCH. 2024-67921<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210136503; DUE DATE: 23-MAY-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NSDR SWAA2024010236701Lens · missingEMERGENCY EXIT ROW LIGHTED SIGN MISSING LENSE COVER. F.O. SIDE; SIDEWALL<[01] REPLACED LENS PER SIPSDR SWAA2023112224053Slide · partial deployAFT ENTRY DOOR SLIDE PARTIALLY OUT OF CONTAINER<[01] INSPECTED AFT ENTRY DOOR SLIDE & FOUND TO BE IN CONTAINER. REINSTALLED GIRT BAR ON HOLDER AS REQUIRED PER AMM 25-66-01. A/C OK FOR SERVICE.SDR SWAA2023112021317Light · inoperativeEMERGENCY LIGHT AT ROW 5ABC INOP<[01] RELAMPED AREA LIGHT AT ROW 5ABC PER AMM 33-51-03. OPS CHECK GOOD.SDR SWAA2023062670987Slide · looseSLIDE FELL OUT OF CASE; FWD GALLEY DOOR<[01] RE-INSTALLED SLIDE IN REF TO MT725-61-06SDR SWAA2023060255417Transmitter · lockedFLAPS LOCKED OUT AT LESS THAN 1<[01] REMOVED AND REPLACED RH FLAP POSITION TRANSMITTER REF AMM 27-58-01. SYSTEM OPS CHECK NORMAL.SDR SWAA2023051847587Scuff Plate · crackedFWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED<[01] REMOVED AND REPLACED SCUFF PLATE ON SHELF IAW SRM 51-40-02-0G-0; IPC 53-13-00-08;[02] VERIFIED STEP 1<BR>JOB COMPLETE<BR>AUDIT C/WSDR SWAA2023051846754Vapor Barrier · crackedCRACK INDICATIONS ON 2 EACH FASTENER HOLES COMMON TO CENTER TANK AT STA 663 MARKED IN BLACK<[01] OVERSIZED QTY 2 EA HOLES TO .435 IAW SRM 51-40-05-0G-0;[02] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#31823;DUE 03JAN24;[03] VERIFIED ITEMSDR SWAA2023051846475Web · crackedDURING HFEC HOLE INSPECTION; FOUND CRACK INDICATIONS IN 2 EA HOLES IN UPPER BLADDER SEAL WEB AT STA 663; RBL 47; WL 198. CIRCLED IN BLACK.<[01] REMOVED RBL 47 WL 198 STA 663 UPPER BLADDER SEAL WEB IAW SRM 51-40-02-0G-0;[02] VERIFIED MATERIAL FOR NEW UPPER BLADSDR SWAA2023051846474Angle · crackedUPPER ATTACH ANGLE AT STA 663 WL 193 RBL 33. CRACK FOUND DURING VISUAL INSPECTION OF ANGLE AT BALL VALVE INBD NUTPLATE. VERIFIED WITH HFEC; MARKED IN BLACK.<[01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1 COMPLESDR SWAA2023051946012Attach Angle · crackedCRACK FOUND ON ATTACH ANGLE STA 663 AT LBL 8 (WL 167)<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTQ8QOOKVEM5 FOR REPAIR;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2023051946004Angle · crackedDOT A24-22 LH WING I/B L/E STRUCTURE / SUPPORT RIB ANGLE FOR PANEL 195AL IS CRACKED. MARKED<[01] STARTED REMOVAL OF SUPPORT RIB ANGLE FOR PANEL 195AL I.A.W. SRM 51-40-02-0G-0;[02] C/W;[03] C/W;[04] AUDIT CWSDR SWAA2023051845875Floor Panel · pulledDOT A24-5 MID CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM SDR SWAA2023051845876Floor Panel · pulledDOT A24-6 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-SDR SWAA2023051845879Floor Panel · pulledDOT A24-9 MID CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM SDR SWAA2023051845877Floor Panel · pulledDOT A24-7 MID CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-SDR SWAA2023051845878Floor Panel · pulledDOT A24-8 MID CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-SDR SWAA2023051846003Attach Angle · crackedCRACK FOUND ON ATTACH ANGLE STA 663 AT LBL 40 (WL 167)<[01] REMOVED 663 LBL 40 WL 167 ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5;[02] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#31823; DUE 03JAN24;[03] VERIFIED ITEM 3 OF STEP 2;[04] VERSDR SWAA2023051846002Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE AT STA 663 OUTBOARD SIDE OF RBL 45 (WL 193)<[01] REMOVED THE REPAIR THAT WAS ORIGINALLY INSTALLED PER NRC E907934 AND E907935. INSTALLED A NEW REPAIR PER EA 23-157-01477 [SRM 57-10-10-2R-3 (REPAIR 3 ALTERNATE 2) AND SRM 57-10-SDR SWAA2023051945646Doubler · crackedEXTERIOR ELECTRICAL GROUND POWER RECEPTACLE LOWER SIDE FOUND CRACK ON SURROUND DOUBLER<[01] AUDIT CWSDR SWAA2022092074325None · inoperativeEMERGENCY LIGHTS OUT AT SEAT ROW 14ABC; 22FED AND 23ABC / [01] REPLACED 2 HOUSING ASSY AND ONE BULB RELAMPED REF AMM 33-51-03SDR SWAA2022080237083Circuit Breaker · poppedRT AFT EMERGENGY LIGHT CB POPPING. / [01] REMOVED AND REPLACED RT AFT EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-06 OP?S CHECK GOODSDR SWAA2022072733526Retaining Clip · out of adjustFORWARD SERVICE DOOR GIRT BAR RETAINING CLIP LOOSE. / [01] ADJUSTED R1 DOOR GIRT BAR RETAINING CLIPS PER AMM SIP.SDR SWAA2022052310337Cover · missingOVERWING EXIT ROW SIGN FO COVER MISSING / [01] INSTALLED COVER PER S I PSDR SWAA2022052309703Cover · missingOVERWING EXIT ROW SIGN FO COVER MISSING / [01] INSTALLED COVER PER S I PSDR SWAA2022031181929Web · crackedCRACK REAR SPAR WEB SUPPORT STRUCTURE ORSS 267 AT RT WING 2022-104311 / [01] REPLACED NEW WEB SUPPORT STRUCTURE ORSS 267 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND FASTENER INSTALLED 51-40-02.;[02] TASK CARD COMPLETEDSDR SWAA2022031476788Rib · crackedCRACK DORSAL FIN BRACKET RIB #8 AT VERTICAL STABILIZER 2022-104235 / [01] TOOL USED: CALIPER 0-6? P/N: 700-113-10 S/N: 0016656 DUE DATE: 11-MAY-22;[02] REPLACED BRACKET LOC. DORSAL FIN RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-174ASDR SWAA2022031176786Track · corrodedCORROSION TRACK RBBL 13.80 LOCATED BS 787 TO BS 807 AT LEVEL STR 26R AT AFT CARGO COMPARTMENT 2022-104229 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 130066401 DUE DATE: 17-JUN-22.;[02] TOOL USED PN:NORTEC 500D;SN:N500X11290U021704; DUE DATE:01-SDR SWAA2022031176789Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW. BS 747 TO BS 767 AT LEVEL STRINGER 25 R AND RBL 21 AT AFT CARGO COMPARTMENT 2022-104232 / [01] FABRICATED SUPPORT ZEE LOCATED BTW. BS 727 TO BS 767 AT LEVEL STRINGER 25 R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 5SDR SWAA2022031176785Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW. BS 767 TO BS 807 AT LEVEL STRINGER 25 L AND LBL 21 AT AFT CARGO COMPARTMENT 2022-104233 / [01] REPLACED SUPPORT ZEE LOCATED BTW. BS 767 TO BS 807 AT LEVEL STRINGER 25 L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-SDR SWAA2022031176787Shield · corrodedCORROSION FLOOR STRUCTURE PLATE LOCATED BETWEEN BS 767 TO BS 787 AT LEVEL STRINGER 25R AND RBL 21 AT AFT CARGO COMPARTMENT 2022-104234 / [01] REPLACED FLOOR STRUCTURE PLATE(SHIELD) LOCATED BETWEEN BS 767 TO BS 787 AT LEVEL STRINGER 25R AND RBL 21 AT AFT CARGO SDR SWAA2022031476362Access Panel · crackedCRACK ACCESS PANEL 661BB HOLES AT RT WING 2022-104220 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOT BONDER; P/N: HCS9200B; S/N: 15102320; DUE DATE: 16/JAN/23.;[03] SCALE; P/N: CL5000; S/N:AE-407336; DUE DATE:16/AUG
Back to N243WN