N202WN, cancelled Oct 29, 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 = 'N202WN' AND deregistration_id = 'N202WN-2024-10-29' 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 = 'N202WN' AND deregistration_id = 'N202WN-2024-10-29' 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 SWAA2024072415449Handle · brokenL1 DOOR ASSIST HANDLE BROKEN<[01] SWAPPED BROKEN L1 DOOR ASSIST HANDLE WITH SERVICEABLE HANDLE FROM THE FWD LAV PER AMM 52-11-31. OK TO CONTINUE PER MEL 25-10-01 SP# 1B AUTH# 205343;[02] INSTALLED FWD LAV ASSIST HANDLE PER CMM 25-42-39.SDR SWAA2024043080201Fseu · false indicationDURING APPROACH/LANDING PROCEDURE NO LEADING-EDGE DEVICE LIGHT ILLUMINATED. LANDED WITH 15' FLAPS EMERGENCY DECLARE.<[01] FOUND MX MSG 27-81277 TASK 834. VERIFIED PINS ON CONNECTOR D728B D2; E2; H2; AND F2. NO DEFECTS NOTED. RAR FSEU PER AMM 27-51-01. OPS CHECSDR SWAA2024041875951Lens · out of adjustEMER EXIT SIGN ON RIGHT OVERWING EXIT LOWER SIDE DETACHED.<[01] SECURED LENSE ON RIGHT LOWER OVER WING EXIT SIGN ASSEMBLY REF. 33-51-01SDR SWAA2024031159385Sign · brokenAFT ENTRY CEILING EXIT LIGHT SIGN HOUSING IS BROKEN<[01] REMOVED AND REPLACED AFT ENTRY CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802-NG. OP CHECK GOOD.;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2024031159223Pressure Blkhd · crackedCRACK INDICATION ON STA 1016 AFT PRESSURE BULKHEAD AT S-23R<[01] REMOVED DAMAGE FROM STA 1016 BULKHEAD WEB WL 244 RBL 0.50 S-23R AND REPAIRED IAW EA 24-153-00607;[02] C/W;[03] C/W<BR>AUDIT C/WSDR SWAA2024030858477Pressure Blkhd · crackedFOUND CRACK INDICATION ON 1016 AFT PRESSURE BULKHEAD AT S-23R. SEE ATTACHED PICTURES. FOUND CRACK INDICATION ON 1016 AFT PRESSURE BULK HEAD AT S-23R. SEE ATTACHED PICTURES. CRACK MEASURES APPROXIMATELY .125.<[01] REPAIRED 1016 AFT PRESSURE BULKHEAD AT S-23R IASDR SWAA2024020247028Girt Bar · out of positionFWD GALLEY ESCAPE SLIDE GIRT BAR MISALIGNED<[01] INSPECTED ESCAPE SLIDE GIRT BAR AT R1 GALLEY SERVICE DOOR IAW AMM 25-66-01. REPOSITIONED SLIDE TONGUE ON GIRT BAR. GIRT BAR ALIGNMENT IS NORMAL. A/C OK FOR SERVICE.SDR SWAA2023092905775Slide · out of adjustAFT PASS ENTRY DOOR SLIDE GAUGE NOT VISIBLE.<[01] REMOVED; REPOSITIONED; AND REINSTALLED L2 DOOR SLIDE IAW MT 725-61-06.SDR SWAA2023081487935Unknown · unknownRT FLAP SPLIT ON FINAL @ FLAPS 30 DEG. FLAP WOULD NOT RETRACT AFTER LANDING<[01] PREFORM FIM TASK 27-51 TASK 813 FOUND FAULT 27-52259 OPS CHECK OK OF SYSTEM NO FAULTS NOTED AT THIS TIMESDR SWAA2023052250093Flap · crackedLH IB AFT FLAP DENT/CRACK LH IB AFT FLAP DENT/CRACK LOWER SKIN<[01] APPLIED PERMANENT REPAIR PER SRM 57-53-01-2R-4 AND SRM 51-70-10.SDR SWAA2023030712119Lens · missingTHE MID LEVEL EMERGENCY EXIT LIGHT LENS IS MISSING AT THE RIGHT OVERWING EMERGENCY EXIT<[01] INSTALLED LENS REF AMM 33-51-01SDR SWAA2022081842869Girt Bar · looseFED AFT GRIT BAR FITTING IS LOOSE. / [01] TIGHTENED FED AFT GIRT BAR FITTING PER AMM 25-66-02-400-801 PARA: 3.D.(1)(G) - (J);[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] VERIFIED MEASUREMENTS TABLE.;[04] CERTIFYSDR SWAA2022081842770Battery Pack · inoperativeEMERGENCY LIGHTS ON BIN BULLNOSE INOP AT SEATS 9CBA AND 11CBA. REPLACED EMERGENCY LIGHTS BATTERY PACK M1670 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.SDR SWAA2022081842769Light · inoperativeEMERGENCY LIGHT BULBS BURNED OUT AT R OWE EXIT SIGNS. REPLACED LAMPS AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHT RT OWE EXIT SIGNS IAW AMM 33-51-01-960-801.SDR SWAA2022081832070Baffle · crackedFWD CARGO BAY BAFFLE CRACKED BS 500 - BS 500A LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] FWD CARGO BAY BAFFLE FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 ; STEP 4C;[03] REMOVED FWD CARGO BAY BAFFLE FROM BS 500 TO BS 500A ; LBL 25 IAW SRM 51-40-0SDR SWAA2022081832069Baffle · crackedFWD CARGO BAY BAFFLE CRACKED BS 500B - BS 500C LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS ; CRACK FOUND OUT OF LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 500B TO BS 500C ; LBL 25 IAW 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BASDR SWAA2022081832068Baffle · crackedFWD CARGO BAY BAFFLE CRACKED BS 400 - BS 420 LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS ; CRACK FOUND OUT LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 400 TO BS 420 ; LBL 25 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BAFFLSDR SWAA2022080329735Light · brokenSIDEWALL PANEL 232YHW EMERGENCY EXIT LIGHT LENS COVER IS BROKEN / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS COVER ON SIDEWALL PANEL 232YHW IAW AMM 33-51-01-960-801 STEPS 2. C. (1)(A) AND (4);[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2022081928559Frame Splice · corrodedCORROSION ON PASSENGER CABIN FRAME SPLICE AT BS 277 BL 0 STRINGER 1.(MARKED) / [01] NOT ALLOWABLE LIMITS FOUND ON SRM FOR BS277 FRAME SPLICE;SRM 51-10-02-0G-0 PAR. 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] REMOVED BS277 FRAME SPLICE LBL3-RBL3 WL287 I.A.W SDR SWAA2022081828562Web · crackedCRACK ON PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H STRINGER 16.(MARKED) / [01] CLEANED PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H<BR>STRINGER 16.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-SDR SWAA2022081828561Stringer Clip · crackedCRACK ON PASSENGER CABIN FWD ENTRY DOOR CLIP AT BS 294 L/H STRINGER 13.(MARKED) / [01] REMOVED CRACKED CLIP AT BS 294 STR 13 L/H IAW SRM 51-40-02-0G-0;[02] UPDATED MEASUREMENT TABLE;[03] FABRICATED NEW CLIP FROM BAC1489-360 LOT# 1464682-1 .050' IAW DWG PL 141ASDR SWAA2022081828560Stringer Clip · crackedCRACK ON PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.(MARKED) / [01] CLEANED PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; LARGE SEVESDR SWAA2022081828557Floor Panel · frayedAFT FLOOR PANEL 242VF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>RSDR SWAA2022081828555Floor Panel · frayedAFT FLOOR PANEL 241ADF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<SDR SWAA2022081928206Seal Depressor · crackedFSD UPPER HINGE CUTOUT UPPER REVEAL IS CRACKED. / [01] LOCATED AND DRILLED NEW SEAL DEPRESSOR P/N 141A8372U1 LOT# 1485850-1 I.A.W. B737-700 SRM 51-40-05-0G-0 FIGURE 2 AND FIGURE 3 TABLE A. OK TO INSTALL NEW SEAL DEPRESSOR FORWARD SERVICE DOOR CUTOUT.;[02] VERISDR SWAA2022081927414Support Angle · corrodedCORROSION ON THRESHOLD SUPPORT ANGLE AT FWD PASSENGER CABIN BS318 TO 338 LBL59. MARKED / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED CORROSION ON THRESHOLD SUPPORT ANGLE AT FWD CABIN BS318 TO 338 LBL59 IN A 1X1.5X.010' AREA IAW SRM 51-10-02-0G-0. ORIGINAL THICSDR SWAA2022081927406Support Fitting · corrodedCORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS312 LBL9. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9.SDR SWAA2022081927415Fitting · corrodedCORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS344 LBL14. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9SDR SWAA2022081927416Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FWD CABIN BS330 LBL11. MARKED. / [01] UPDATED MEASUREMENTS LIST.;[02] DAMAGE EVALUATION; ORIGINAL THICKNESS .080. <BR>CORROSION MATERIAL LOSS MEASURES (.022) FOUND TO BE OUT OF LIMITS AS PER SRM 53-10-04-0I-1.;[03] UPDATING TO ADDSDR SWAA2022081927419Support Angle · corrodedCORROSION ON FSD THRESHOLD SUPPORT ANGLE BS305 - BS323 RBL57. MARKED. / [01] FOUND SRM 53-10-15-1A-2 IS APPLICABLE FOR CORROSION REMOVAL AT BS 305-323 RBL 57 WL 209;[02] REMOVED CORROSION IN MULTIPLE AREAS ON FSD THRESHOLD SUPPORT ANGLE AT BS 305-323; RBL 57. SDR SWAA2022081727409Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS349 BL0 WL208. / [01] LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 BL0 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1;[04] INSTALLED INTERCOSTAL IAW SRM 51-4-02 SDR SWAA2022081727410Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS353 RBL11 WL208. / [01] UPDATED STEP 1 AND VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR><BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 RBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 1SDR SWAA2022081727420Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS294+6 RBL31. MARKED. / [01] REMOVED HI-LOCKS FROM INTERCOSTAL AT FWD CABIN BS 294+6 RBL 31 <BR>IAW SRM 51-40-02-0G-0.;[02] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR>REPAIR PER REPLACEMENT PER SRMSDR SWAA2022080327411Channel · crackedCRACKED FWD ENTRY DOOR MOP SILL BS303 LBL55 WL208. MARKED. / [01] FED MOPSILL AT B.S 303 LBL55 WL208 IS CRACKED ON VERTICAL FLANGE. OUT OF LIMITS IAW SRM 53-10-15-1A-1. STARTED FASTENER REMOVAL IAW SRM 51-40-02-0G-0.;[02] UPDATED MEASUREMENT TABLE;[03] REMOVEDSDR SWAA2022080327417Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS284 BL0 WL208. MARKED. / [01] UPDATED MEASUREMENTS. CRACKED INTERCOSTAL FOUND TO BE OUT OF LIMITS AND WILL BE REPLACEMENT OF THE PART IAW SRM 51-10-02 STEP 9. REMOVED CRACKED INTERCOSTAL AT BS284 BL0 WL208 IAW SRM 51-40-02. RSDR SWAA2022080327408Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS353 LBL11 WL208. / [01] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR><BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 LBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFISDR SWAA2022082227173Floor Support · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL36 - RBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE RBL36-RBL43 WL208 7'X1' AND FOUND TO BE OUT LIMIT AT NUT PLATSDR SWAA2022081927281Bear Strap · crackedPASSENGER CABIN FSD CUTOUT BARE STRAP CRACKED BS299; 3' BELOW FWD UPPER DOOR STOP FITTING. MARKED. / LOCATED & DRILLED NEW UPPER STUB FRAME P/N 141A8370U13 LOT# 1497302-1 P.O. CERT# 875637 I.A.W B737-700 SRM 51-40-05-0G-0 FIGURE 2 & FIGURE 3 TABLE A. OK TO INSSDR SWAA2022081927166Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS1016 RBL6. MARKED. / [01] BEGAN REMOVING FASTENERS COMMON TO WEB BS1016-BS1031 BL0-RBL37 IAW SRM 51-40-02.;[02] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SDR SWAA2022081927168Tension Tie · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016 RBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5744U1 IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-SDR SWAA2022081927169Tension Tie · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016 - BS1028 LBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5620U3 IAW SRM 51-40-02-0G-0 AND 51-SDR SWAA2022081927170Web · corrodedCORROSION ON WEB AT AFT WET AREA BS1028 LBL4 TO LBL19. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1028 LBL4-LBL19 SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED BS1016<BR>L/H SHEAR WEB I.A.W SRSDR SWAA2022081927171Web · corrodedCORROSION ON WEB AT AFT WET AREA BS1016 LBL11; LBL34. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 L/H SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C ALL REMOVAL AND REPLACED TO BE ACCOMPLSHED ON COSTUMESDR SWAA2022081927172Floorbeam · corrodedCORROSION ON FLOORBEAM AT AFT WET AREA BS986 LBL34 - LBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE LBL34-LBL43 WL208 9'X1' AND FOUND TO BE OUT LIMIT AT NUT PLATESDR SWAA2022081827282Frame · crackedFWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283. MARKED. / [01] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IAW SRM 51-10-02.;[02] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IN AN AREA OF 1' X .2' IAW SRM 51-10-02.;[03] RSDR SWAA2022081827176Frame · crackedCRACKED FRAME AT AFT PASSENGER CABIN S-8L BS927. MARKED. / [01] REMOVED FRAME TO BIN RAIL ATTACH ANGLE BS 927; STR 8L FOR ACCESS IAW SRM 51-40-02-0G-0. NO VISUAL SIGN OF CRACK ON FRAME;[02] VERIFIED CORRECTIVE ACTION #1;[03] REQUEST NDI FOR CRACK FREE CONDITIOSDR SWAA2022080327283Bracket · looseLOOSE FASTENERS CHAFING ON INTERCOSTAL AT FWD PASSENGER CABIN BS277 3' OB OF S-2R WL282. / [01] GAINED ACCESS BY REMOVING COCKPIT DOOR POST PER SRM 51-40-02;[02] REMOVED CHAFFED BRACKET AT BS 277 ;3' OUTBD OF STR 2R; WL 282 IAW SRM 51-40-02;[03] LOCATED NEW BRSDR SWAA2022081926591Pressure Deck · crackedHORIZONTAL PRESSURE DECK CRACKED AT BS 664.5; LBL 30.5 AND 32; WL 202.5. (CRACKS CIRCLED IN RED) / CUTED AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2. PAR. 4 A;B;C (1)(2)(3).HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<SDR SWAA2022081826586Floor Panel · damagedFWD FLOOR PANEL 222DF HAS A RIPPED OUT INSERT ALONG THE O/B EDGE. (MARKED) / [01] IDENTIFIED FWD PANEL 222DF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW 53-00-50-1A-1 PARA 4.F. <BR>DAMAGE WILL BE REPAIRED IAW SRM 53-0SDR SWAA2022081826585Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SURFACE HAS AREAS OF PULLED STRANDS. / REMOVED ALL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3B<BR>REMOVED PREVIOUS REPAIR AND ALL DAMAGE NOTED AND CLEANED REPAIR AREAS IAW SRM 53-00-50-2R-1 PARA 3C-F;[02] VALIDATED AP
Back to N202WN, cancelled Oct 29, 2024