N567WN
Service difficulty reports · 225
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 = 'N567WN' 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 = 'N567WN' 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 SWAA2023030897911Seat Track · corrodedLEFT OB CABIN SEAT TRACK HAS EXFOLIATING CORROSION BS 375. 8-26<[01] REMOVED FASTENERS FOR ACCESS TO REMOVE SEAT TRACK CORROSION PER B737-700 SRM 51-40-02-0G-0.;[16] VERIFIED STEP NO15. (FINAL) REMOVED CORROSION AT LEFT O/B CABIN SEAT TRACK BS 375 PER B737-700SDR SWAA2023030897542Stiffener · crackedRIGHT HORIZONTAL STILIZER RIB 4 CRACKED AT STIFFENER 2 LOWER RADIUS.<[01] REMOVED THE DAMAGE PART OF THE RIB 4 STIFFENER 2 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] PERFORMED HFEC INSP ON REWORKED; IAW B 737 NDT PARTSDR SWAA2023030897785Barrier · crackedRT BS 663 VAPOR BARRIER CRACK RBL 45.<[01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON R/H VAPOR BARRIER AND FOUND CRACK OF 9' PER B737 NDTM 51-05-01;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF THE CRACK PER B737 SRM 57-10-10-2R-2 STEP 6.B;SDR SWAA2023030897321Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #241XF; UPPER SURFACE DELAMINATED DOT 223-PCF241XF.<[01] RECEIVED NEW PANEL 241XF; PO#2005897. PANEL WILL BE INSTALLED ON TTG8Q00H2SLP.;[02] VERIFIED AND INSPECTED STEP #1.SDR SWAA2023030896999Bracket · crackedLH VAPOR BARRIER SUPPORT BRACKET FOUND CRACKED AROUND FASTENER HOLE<[01] RECEIVED NEW BRACKET P/N 276A9183-5 AND LOCATED AND DRILL PER REF SRM 51-40-05-0G-0;[02] TREATED AND PRIME NEW FASTENER HOLES; PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03] OSDR SWAA2023030897329Channel · brokenRIGHT 'Z' CHANNEL AT FWD END B/S 727 ATTACHMENT IS BROKEN<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKAET;[02] FINAL INSPECTION; AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FSDR SWAA2023030897333Floor Panel · crackedFLOOR PNL 242SF HAS CRACK ON UPPER SURFACE. 8-25<[01] RECEIVED NEW PANEL 242SF PO#2005895. PANEL WILL BE INSTALLED ON TTG8Q00H2URQ.;[02] VERIFIED AND INSPECTED STEP #1.SDR SWAA2023030897332Channel · corrodedAFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727C-727E<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD #TTG8Q00HKAET;[02] VERIFIED STEP #1.SDR SWAA2023030897328Channel · corrodedAFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727E-767<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT Z-CHANNEL PER REF SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW R/H Z-CHANNEL FROM STA 727 TO 767 PER REF SRM 51-40-05SDR SWAA2023030897326Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 77B-727E<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.SDR SWAA2023030897325Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 727-727B<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT L/H Z CHANNEL STA 727-727B PER SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW L/H Z CHANNEL FROM STA 727- 847 PER REF SRSDR SWAA2023030897330Channel · corrodedAFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 767-807<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.SDR SWAA2023030897000Retainer · crackedLH VAPOR BARRIER SEAL RETAINER FOUND CRACKED<[01] RECIEVED; LOCATED AND DRILLED NEW L/H VAPOR BARRIER SEAL RETAINER PN: 111A1512U1 PO:1792296 PER REF SRM 51-40-05-0G-0.;[02] TREATED AND PRIMED NEW HOLES PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03SDR SWAA2023030897320Fitting · crackedRT WING TRAIL EDGE RIB WBL 201.90 HAS AFT UPPER FITTING CRACKED THRU. 8-24<[01] REMOVED AND REPLACED AFT UPPER FITTING AT RT WING TRAIL EDGE RIB WBL 201.90 PER REF SRM-51-40-02-0G-0.;[02] FINAL INSPECTION; T/E RIB REPLACED.SDR SWAA2023030896756Vapor Barrier · crackedCOMP- REPAIR LH VAPOR BARRIER CRACK<[01] MEASUREMENTS.;[02] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10SDR SWAA2023030896442Doubler · crackedEGPR INTERNAL DOUBLER CRACKED AT FWD LOWER CORNER.<[01] REMOVED PAINT BY STRIPPING AT FUSELAGE SKIN R/H SIDE EGPR AREA REF B737-700 AMM 51-21-11-150-810.; LOCATED AND DRILLED NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-05-0G-0.;[07] TREATED AND PRIMED DRISDR SWAA2023030896443Stiffener · crackedRIGHT HORIZONTAL STABILIZER RIB 4 CRACKED AT STIFFENER 3 LOWER RADIUS.(51-025)<[01] REMOVED THE DAMAGE PART OF THE RIB 4 AT STIFFENER 3 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED 1. ACCOMPLISHED GVI OF REPAIRSDR SWAA2023030896445Angle · crackedRT BS 663 VAPOR BARRIER UPPER SUPPORT ANGLE CRACKED.<[01] BEGAN REMOVED FASTENERS AT RT VAPOR BARRIER UPPER SUPPORT ANGLE BS 663 IN AS PER SRM 51-40-02-0G-0;18] COMPLETED INSTALLATION OF NEW REPAIR PARTS OF RT UPPER SUPPORT WING CENTER SECTION VAPOR BARRIER FRSDR SWAA2023030895861Panel · elongatedMID FORWARD BODY FAIRING PANEL #191D; ALL FASTENER HOLES ELONGATED OR/AND SURFACE PROTRUDING DOT 223-MFF191D.<[01] PERFORMED VISUAL INSPECTION ON PANEL #191D AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWATED MATERIAL PER B737 NDTM 51-05-01;[02] PREPAREDSDR SWAA2023030895855Angle · elongatedL/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B ATTACHED ANGLE FWD FASTENER HOLE ELONGATED AND BUSING ; BOLT ; NUT MISSING MKD DOT<[01] REMOVED DAMAGE ANGLE AT LT WING T/E LOWER PANEL 551GB I/B SIDE PER REF B737 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGSDR SWAA2023030895856Beam · elongatedL/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POINT LOCATION ' A' ELONGATED HOLES ;EXCESSIVE PLAY MKD DOTS<[01] REMOVED HARDWARE AT L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POING LOCATION 'A'AS PSDR SWAA2023030894636Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 ; 17' FROM FRONT SPAR ; I/B ROW . CRACK LENGTH : 0.75' CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 17' FROM FRONT SPAR I/B ROW .CRACK LENGTH : 0.7SDR SWAA2023012593696Tray · out of adjustROW 12C TRAY TABLE WILL NOT STAY UP & PAX UNIT LIGHT FIXTURE MOVES.<[01] ADJUSTED TRAY TABLE @ 12C PER SIP. 12C READING LIGHT ASSEMBLY FOUND TO BE SECURE; FOUND 12C AIR OUTLET TO BE DAMAGED AND LOOSE. R&R 12C PSU AIR OUTLET PER AMM 21-24-04.SDR SWAA2023012493975Seat · wrong partSEAT 11F RECLINES IN FRONT OF EXIT-SEAT 11F UNUSABLE SEAT 11F RECLINES IN FRONT OF EXIT-SEAT 11F UNUSABLE*** DO NOT CARRY ***<[01] ADJUSTED SEAT 11F HYDROLOCK TO DISABLE RECLINE IAW AMM 25-22-00. THIS CLEARS MEL.SDR SWAA2022112172556Restraint · looseFWD GALLEY MEGAPHONE RESTRAINT LOOSE / [01] R/R?D FWD GALLEY MEGAPHONE BRACKET PER S.I.PSDR SWAA2022101759540Mechanism · out of adjustFIRST OFICER'S SLIDING WINDOW FAILS EMERGENCY EXIT RELEASE HANDLE OPS CHECK. / [01] ADJUSTED FIRST OFFICERS SLIDING WINDOW EMERGENCY EXIT RELEASE MECHANISM PER M/M 56-12-11.SDR SWAA2022092724640Slide · out of positionFOWARD ENTRY DOOR ESCAPE SLIDE DISLODGED FROM IT'S CONTAINER / [01] REMOUNTED FWD DOOR ESCAPE SLIDE IAW S.I.P.SDR SWAA2022050301062None · inoperativeAFT ENTRY DOOR EMERGENCY LIGHTS INOP / [01] REPLACED THE AFT L/H EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECK GOODSDR SWAA2022030980412Light · inoperativeEMERGENCY LIGHT AFT OF L2 DOOR INOP / [01] R&R EMERGENCY LIGHT AFT OF L2 DOOR IAW AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2022011360415Light · inoperativeFWD CEILING EMERGENCY LIGHT INOP ; / [01] RELAMPED FWD CEILING AREA EMERGENCY LIGHT PER AMM 33-51-03. OPS CK GOODSDR SWAA2022010356992Strap · out of adjustFWD ENTRY DOOR UPPER STRAP NEEDS ADJUSTMENT ; / [01] REPLACED ATTACH SCREW PER SIPSDR SWAA2021122053935Slide · looseFSD ESCAPE SLIDE FELL FROM CLAM SHELL HOUSING ; FSD ESCAPE SLIDE FELL FROM CLAM SHELL HOSING / [01] REPACKED AND MOUNTED FSD ESCAPE SLIDE IAW AMM 25-66-01.SDR SWAA2021121351581Panel · crackedSUPPLEMENTAL INFORMATION: 194E PANEL HAS CRACKED AND ELONGATED HOLES / [01] REPLACED PANEL 194E PER AMM 53-51-21SDR SWAA2021121351580Panel · crackedSUPPLEMENTAL INFORMATION: 193D PANEL HAS CRACKED HOLES / [01] REPLACED PANEL 193D PER AMM 53-51-21SDR SWAA2021071995196Acm · faultedON APPROACH CABIN AIR TEMPERATURE BECAME HOT. SMELL ACCOMPANIED THAT THROUGHOUT AIRCRAFT. AFTER LANDING; LEFT PACK TRIP OFF ILLUMINATED. ; / [01] C/W FUMES CONDITIONAL INSP IAW FIM 21-00 TASK 806; FOUND LH PACK CAUSING SMELL; OK TO CONTINUE PER MEL 21-1-01 SP1SDR SWAA2021040560129Girt Bar · out of adjustFWD SERVICE DOOR SLIDE GIRT NEEDS ADJUSTMENT AND CLIP TIGHTED ADJUSTED SLIDE GIRT AND TIGHTENED CLIP ON FWD SERVICE PER AMM256601SDR SWAA2021030853350Light · brokenEMERGENCY LIGHT LENSE AND BEZEL BROKEN AT 16 D-E-F / OK TO CONTINUE PER MEL 25-10-01 SP1B TRACKING #70711SDR SWAA2021022450490Sign · missingFWD SERVICE DOOR EXIT SIGN NOT INSTALLED / R/R RIGHT ASSY PER AMM 33-51-01SDR SWAA2021021548724Door · out of adjustR1 DOOR RIDES HARD ON AFT UPPER LATCH RECEIVER WHEN CLOSING / PERFORMED R1 DOOR ADJUSTMENT PER B737 AMM 52-41-00-820-801 ALL OPS NORMAL PERFORMED PRESSURIZATIONAL LEAK TEST OF R1 DOOR REF B737 AMM 25-51-91-790-801; NO LEAKS FOUNDSDR SWAA2021021548485Skirt · out of adjustQA WALK*** R2 DOOR ESCAPE SLIDE SKIRT RUB SCUFF PLATE WHEN CLOSING. / ADJUSTED R2 DOOR SLIDE SKIRT RUB AS PER TASK CARD 8725-61-06SDR SWAA2021021646754Angle · crackedVERT STAB HAS ANGLE CRACKED ABOVE AND ON AFT SIDE OF FWD LEFT ATTACH LUG. / REMOVED AND REPLACED VERTICAL STAB LWR ANGLE ON FWD SIDE OF ATTACH LUG REF B737-700 SRM 51-40-02-0G-0 AND DWG #176A3101SDR SWAA2021041945681Bulkhead · damagedAFT CARGO COMPARTMENT; SHROUD 142NWA FOUND DAMAGED DURING INSPECTION. / RECEIVED NEW SHROUD 142NWA FROM STOCK .INSTALLATION WILL BE COMPLETED CUSTOMER CARD # JPANEL-141-CLOSE .SDR SWAA2021021546653Floor Panel · delaminatedCABIN PANEL 241 RF IS DELAMINATED AT AFT RIGHT HAND CORNER. / ACCOMPLISHED PERMANENT REPAIR AT CABIN FLOOR PANEL 241RF AFT RIGHT HAND CORNER PER REF B737 SRM 53-00-50-2R-9SDR SWAA2021021644734Skin · corrodedCORROSION***ON LWR SURFACE OF LWR CTR WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541. / ACCOMPLISHED REPAIR OF CORROSION FOUND ON LWR SURFACE OF WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541 PER INSTRUCTIONS ON AAR RES-WI 2016690-11 REV IR AND SOUTHWEST EA 21-157-002SDR SWAA2021021544411Support · crackedFWD CARGO COMPARTMENT;GUSSET SUPPORT IS CRACKED AT STA 500D S-19LH. / REMOVED AND REPLACED GUSSET SUPPORT AT FWD CARGO COMP. AT STA 500D S-19LH AND TREATED ASS FASTENERS HOLES WITH ALODINE AND PRIME IN REF B737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG# 143SDR SWAA2021070744995Seat Track · crackedCOCKPIT; CAPTIANS RACEWAYFOUND CRACKED. / REMOVED AND REPLACED COCKPIT; CAPTAINS RACEWAY WITH NEW RACEWAY AS PER REF B737-7 SRM 51-40-02-0G-0SDR SWAA2021021544220Bracket · crackedFWD CARGO COMPARTMENT HAS CRACKED BRACKET AFT SIDE OF FRAME BS 500C S-26L. / REMOVED AND REPLACED BRACKET AT FWD CARGO COMP AT BS 500C; S-26L AND TREATED ALL FASTNERS HOLES WITH ALODINE AND PRIMER IN REF BB 737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG # 14SDR SWAA2021071442583Bushing · out of toleranceFUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHT ATTACHMENT HAS BUSHING OUT OF LIMITS. [0.8840'] [MAX ALLOWED 0.8835' TASK 55-30-00-200-801] / REMOVED AND REPLACED BUSHING AT FUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHSDR SWAA2021021642585Rib · crackedRT WING UPPER T/E PNL AFT OF PYLON HAS CTR AFT RIB CRACKED AT FWD LWR BOLT HOLE. / REMOVED AND REPLACED CENTER AFT RIB AT RT. WING AFT OF PYLON IAW SRM 51-40-02-0G-0SDR SWAA2021021542587Structure · crackedCABIN HAS CHORD CRACKED AT END RADIUS BS 312 S5L-S6L. / CUT OUT DAMAGE AT CABIN CHORD AT END RADIUS BS 312 S5L-S6L; PERFORMED HFEC AND ROTO INSP NO CRACK NOTE AS PER NTM PART 6 51-00-00 PROCEDURE 23; FABRICATED ANGLE REPAIR MAT USED 7075-0 0.063 CLAD PO #16680
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