N926WN
Service difficulty reports · 272
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 = 'N926WN' 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 = 'N926WN' 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 SWAA2026012753842Scuff Plate · crackedCRACKED SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026012753843Scuff Plate · crackedCRACKED SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026012853839Vapor Barrier · crackedCRACKED VAPOR BARRIER RT SIDE, RBL 40. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025111735183Girt Bar · out of adjustFWD SERVICE DOOR GIRT BAR STUCK IN BRACKET. REPOSITIONED & ADJUSTED GIRT BAR ON FWD SERVICE DOOR AS PER AMM 25-66-00SDR SWAA2025082207252Sign · looseFWD GALLEY NEAR R2 DOOR LOWER EXIT SIGN LENS CAME OFF UNABLE TO RE-SECURE. REMOVED AND REPLACED GALLEY (FWD) EXIT SIGN INDICATOR ASSEMBLY REF AMM 33-51-01. SECURED LENS AS NEEDED; OPS CHECKS NORMAL.SDR SWAA2025082207180Flashlight · inoperativeCABIN FWD BOTTOM FLASHLIGHT WILL TEST FWD BOTTOM FLASHLIGHT WILL TEST. CABIN FORWARD BOTTOM FLASHLIGHT OPS CHECK GOOD AND REPLACED BROKEN TAMPER SHIELD REF AMM 25-64-00.SDR SWAA2025051970914Lens · crackedAFT GALLEY DOOR; EMERGENCY LIGHT LENS ABOVE DOOR IS CRACKED<[01] REMOVED AND REPLACED CRACKED AFT LENS ABOVE R2 DOOR IAW AMM 33-51-01.;[02] REMOVED AND REPLACED CRACKED AFT LENS ABOVE R2 DOOR IAW AMM 33-51-01. INSPECTION C/W.SDR SWAA2025051970913Sign · inoperativeL/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] R&R EMERGENCY EXIT LIGHT PER AMM 33-51-01;[02] 02 - INSPECTED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]SDR SWAA2025051971257Fairing · cracked#2 ENGINE PYLON AFT STRUT FAIRING NAC STA. 315; 1 INCH CRACK VISIBLE IN FITTING.<[01] ADDED 'AFT STRUT FAING' TO FAULT HEADING.;[02] REPAIRED REF M-23-154-01884;[03] ENG 02) CFM56-7B24/3 ENGINE (PN: CFM56-7B24/3; SN: 802895);[04] C/W M-23-154-01884.;[05] ADDEDSDR SWAA2025033109965Actuator · damagedNOSE WHEEL LANDING GEAR UNSAFE INDICATION ON TAKEOFF (RED GEAR LIGHT). LANDING GEAR EXTENDED NORMALLY. PSEU LIGHT ILLUMINATED ON LANDING<[01] INSTALLED NLG LOCK ACTUATOR PER AMM 32-33-21. OPS CHECK GOOD. LEAK CHECK GOOD.;[02] COMPLIED WITH RII INSPECTION OF NOSDR SWAA2025011585578Handle · out of adjustCR RR L-1 DOOR ASSIST HANDLE LOOSE NEEDS SECURED.<[01] TIGHTENED CR RR L-1 DOOR ASSIST HANDLE IAW B737-700 AMM 52-11-31-400-802 STEP 3. G. (2).;[02] VERIFIED TIGHTENED CR RR L-1 DOOR ASSIST HANDLE IAW B737-700 AMM 52-11-31-400-802 STEP 3. G. (2).SDR SWAA2024112771970Handle · brokenAFT SERVICE DOOR ASSIST HANDLE BROKEN<[01] REPLACED AFT SERVICE DOOR HANDLE REF AMM 25-21-21SDR SWAA2024100745256Seat Back · out of adjustSEAT BACKS LOOSE ROW 12 ABC<[01] ADJUSTED SEAT BACK BREAKOVER REF CMM 25-21-42; AMM 25-22-00SDR SWAA2024062505179Lens · missingEMERGENCY BULLNOSE LIGHT AT 7ABC MISSING LENS COVER<[01] INSTALLED NEW EMERGENCY BULLNOSE LIGHT LENS COVER AT 7ABC REF AMM 33-51-03SDR SWAA2024061802271Fuse · failedLEFT WING SLIDE EMERGENCY LIGHT INOP<[01] RELAMPED LEFT WING SLIDE EMERGENCY LIGHT REF AMM 33-51-04; NO HELP. REPLACED FUSE ON BATTERY PACK CRADLE REF WDM 22-51-13. OPS CHECK GOOD.SDR SWAA2024050181323Flashlight · noneFWD GALLEY EMERGENCY FLASHLIGHT (LOWER) INOPERATIVE. UPON FURTHER INVESTIGATION FOUND FORWARD GALLEY EMERGENCY FLASHLIGHT TO BE FUNCTIONING NORMAL IAW AMM 25-64-00.SDR SWAA2024030657706Skirt · out of adjustR2 DOOR SLIDE SKIRT TOUCHES THE SCUFFPLATE WHEN OPENING AND CLOSING THE DOOR<[01] REPOSITION R-2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP #1SDR SWAA2024030657705Skirt · out of adjustL2 DOOR SLIDE SKIRT TOUCHES THE SCUFFPLATE WHEN OPENING AND ENGAGES WITH SCUFFPLATE WHEN CLOSING THE DOOR<[01] REPOSITION L-2 DOOR ESCAPE SLIDE SKIRT AS PEF WORK INSTRUCTION 725-61-06;[02] VERIFEID STEP #1SDR SWAA2024030657703Light · burnedL/H OVERWING EMERGENCY EXIT DOOR LOWER FWD EXIT LIGHT HAS A FEW BURNT OUT BULBS<[01] RELAMPED L/H OVERWING EMERGENCY EXIT DOOR LOWER FWD EXIT LIGHT AS PER B737 AMM 33-51-01-960-801. TEST PASSED.;[02] VERIFIED STEP 1.SDR SWAA2024030756087Scuff Plate · crackedR-1 DOOR EXT. SCUFF PLATE IS CRACKED AT AFT. CORNER.<[01] RECIEVED; VERIFIED AND OBTAINED NEW PART SCUFF PLATE. SCUFF PLATE 141A8431-3 PO# 2043476 SCUFF PLATE WILL BE INSTALLED ON TASK CARD # TTG8Q002BDCF.;[02] VERIFIED STEP 1SDR SWAA2024030753801Post · crackedFLIGHT DECK DOOR POST COVER ASSY IS CRACKED<[01] REMOVED AND REPLACED FLIGHT DECK DOOR POST END COVER ASSY IN REF SRM-51-40-02-0G-0;[02] CORRECTION: REMOVED AND REPLACED FLIGHT DECK DOOR POST END COVER ASSY IN REF SRM-51-40-02-0G-0 AND IPC 52-51-51-12;[03] VERSDR SWAA2024030752957Doubler · crackedREPLACE PREVIOUS REPAIR AT EXTERNAL POWER DOOR INNER DOUBLER CUTOUT SKIN AFT EDGE<[01] REMOVED PREVIOUS REPAIR (INNER DOUBLER CUTOUT SKIN AFT EDGE) AT EXTERNAL POWER DOOR AS PER SRM 51-40-02-0G-0 AND SRM 53-10-15-2R-4. INSTALLED INNER DOUBLER AND RUBBING BLOCKSDR SWAA2024030851269Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 331B #4 RIB CRACK COUNTING FROM I/B TO O/B<[01] REMOVED DAMAGED RIB #4 AT LEFT HORIZONTAL STAB. LEADING EDGE ACCESS PANEL 331 AND INSTALLED NEW #4 RIB AT LEFT HORIZONTAL STAB. LEADING EDGE ACCESS PANEL 331 PSDR SWAA2024030749907Rib · crackedRIGHT HORIZONTAL STAB RIB #5 HAS A CRACK ON THE FWD UPPER SIDE OF THE WEB BELOW CHORD RADIUS RIGHT HORIZONTAL STAB RIB #5 HAS A CRACK ON THE FWD LOWER SIDE OF THE WEB ABOVE CHORD RADIUS<[01] ACCOMPLISHED REPAIR AT RIGHT HORIZONTAL STAB RIB # 5 LOWER SIDE OF THSDR SWAA2024030650192Pressure Deck · crackedCRACK FOUND AT FASTENER HOLE AT FLIGHT DECK FLOOR WEB BS 250+9 RBL 9. CORRECTION ON ORIGINAL WRITE UP CRACK FOUND AT FASTENER HOLE AT FLIGHT DECK FLOOR WEB BS 253 RBL 4.2<[01] ??WORK ACCOMPLISHED PER EA 24-153-00402.';[02] VERIFIED STEP 1SDR SWAA2024030749906Stiffener · crackedR/H HORIZONTAL STAB INTERNAL SURFCE RIB 5 STIFFENER 2 CRACKED.<[01] REMOVED DAMAGED PART OF STIFFENER #2 AT RIB #5 REF. SRM 55-10-09-2R-4 AND INSTALLED REPAIR PARTS (T-SECTION; ANGLE AND SHIMS) PER REF 55-10-09-2R-4 REPAIR 4 AND SRM 51-40-02-0G-0;[02] CORRECTISDR SWAA2024030749899Link · crackedFOUND PIVOT LINK CRACKED AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 520 AND STA 540 BL 0<[01] REMOVED AND REPLACED PIVOT LINK AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 520 AND STA 540 BL 0 IAW SRM 51-40-02-0G-0 AND DWG 143A5595.;[02] VERIFIED STEP 1;[03] STEP #SDR SWAA2024030749318Angle · crackedMAIN CABIN CRACK AT PANEL BREAK ANGLE STA 540 RBL 1'<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN STA 540 RBL 1 AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1SDR SWAA2024030749319Angle · crackedMAIN CABIN CRACK AT PANEL BREAK ANGLE STA 540 LBL 1'<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN STA 540 LBL 1 AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1SDR SWAA2024030848978Seat Track · crackedMAIN CABIN FWD WET AREA LEFT INNER CHORD CRACK AT STA 303.9<[01] REMOVED AND REPLACED NEW L-1 INNER CHORD FROM STA 270 TO STA 357 LBL-56 REF USED B737-00 SRM 51-40-02-0G-0 AND DWG#141A8110 AND 142A0050;[02] VERIFIED STEP 1SDR SWAA2024030748979Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 270-294.5 BL 0' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 270 TO 294.5 BL 0' PER SRM 51-40-02-0G-0;[02] CORRECTION ON STEP #1:REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 270 TO 294.5SDR SWAA2024030748959Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 312-328 LBL 46' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 TO STA 328 AND LBL 46' IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400.;[02] VERIFIED STEP 1SDR SWAA2024030748980Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 344-328 LBL 46' CRACK<[01] REMOVED AND REPLACED NEW INTERCOSTAL BETWEEN STA 344 TO STA 328 AND LBL 46' IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400.;[02] VERIFIED STEP 1SDR SWAA2024030748929Doubler · crackedEXTERNAL POWER DOOR CUTOUT SKIN DOUBLER IS CRACK AT AFT CENTER EDGE<[01] ACCOMPLISHED TRIMOUT REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE AFT CENTER EDGE IN REF B737-700 SRM 53-10-15-2R-4 FIG 203.;[02] VERIFIED STEP 1SDR SWAA2024030748951Floorbeam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM STA 986.5 RBL 44'-47'<[01] REJECT TTG8Q00RCQT8....MEASUREMENT CHART HAS INCORRECT BUTT LINE END. STEP 1 WORK PERFORMED MISSING RBL 44 - RBL 47. GENERATED T/C TTG8Q00RPQ2F;[02] COMPLETED SME INSPECTION OF WORKMANSSDR SWAA2024030748964Floor Panel · peelingCABIN FLOOR PANEL 231BF HAS UPPER SURFACE FIBERS PEELING OFF MKD<[01] RECEIVED MAIN CABINS FLOOR PANEL 231BF AND WILL BE INSTALLED ON T/C TTG8Q00Q8H04;[02] VERIFIED STEP 1SDR SWAA2024030748965Floor Panel · peelingCABIN FLOOR PANEL 231AF UPPER SURFACE HAS FIBERS PEELING OFF MKD<[01] RECEIVED MAIN CABIN FLOOR PANEL 231 AF AND WILL BE INSTALLED ON T/C TTG8Q00Q8H06;[02] VERIFIED STEP 1SDR SWAA2024030748977Support Angle · corrodedMAIN CABIN FWD WET AREA CORROSION AT LEFT INNER CHORD SUPPORT ANGLE BETWEEN STA 312-344<[01] REMOVED AND REPLACED SUPPORT ANGLE AT MAIN CABIN FWD WET RAEA INNER CHORD REF. SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1SDR SWAA2024030748953Strap · corrodedMAIN CABIN AFT WET AREA CORROSION AT AFT PRESSURE BULKHEAD SEAL STRAP RBL 33'<[01] CLEANED AFT WET AREA AT AFT PRESSURE BULKHEAD SEAL STRAP RBL 33' REF SOPM 20-30-03 AND TREATED AND APPLIED PRIMER AFT WET AREA AT AFT PRESSURE BULKHEAD SEAL STRAP RBL 33' REF AMSDR SWAA2024030648820Pressure Deck · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB AT STA 663 RBL 41. CRACK LENGTH 0.218'<[01] ACCOMPLISHED REPAIR AT HORIZONTAL PRESSURE DECK WEB AT STA 663 RBL 41 IN REF WITH 53-40-51-2R-2;[02] VERIFIED STEP 1SDR SWAA2024030748449Stiffener · crackedR/H HORIZONTAL STAB INTERNAL SURFACE RIB #5 STIFFENER #3 CRACKED.<[01] REMOVED DAMAGE PART OF STIFFENER #3 AT RIB #5; VERIFIED CUT EDGES OF INITIAL PARTS SURFACE ROUGNESS OF 63 MICROINCHES RA REF. SRM 55-10-09-2R-4 TOOL USED B/C 172329 NO DUE DATE;<BR>LOCATED SDR SWAA2024030748684Frame · crackedCRACK - AT END OF FRAME STA 312 JUST ABOVE L-1 DR CUT-OUT FWD UPPER CORNER<[01] ACCOMPLISHED EA: M-22-153-01244/9108451.;[02] VERIFIED STEP 1SDR SWAA2024030748447Connector · damagedEMERGENCY LIGHT POWER SUPPLY M1670 CONNECTOR DAMAGED<[01] REMOVED & REPLACED EMERGENCY LIGHT POWER SUPPLY (M1670) CONNECTOR. D10716P PER B737 SWPM 20-61-00 AND WDM 33-51-13 & 33-51-11 AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT POWER SUPPLY M1670 AS SDR SWAA2024030748446Scuff Plate · crackedR-1 DOOR EXT. SCUFF PLATE IS CRACKED AT AFT. CORNER.<[01] RECIEVED; VERIFIED AND OBTAINED NEW PARTS PLATE AND SCUFF PLATE.<BR>(PLATE) 411A2219-26; BN 406072; NSI; ISSUE TAG ST1099 AND PO#: 2043476. <BR>(SCUFFPLATE) 141A8431-3; BN 407582; NSI; PO# 2043476 AND ISDR SWAA2024030748448Stiffener · crackedL/H HORIZONTAL STAB INTERNAL SURFACE RIB #5 STIFFENER#2 CRACKED.<[01] REMOVED DAMAGED PART OF STIFFENER#2 AT RIB#5;VERIFIED CUT EDGES OF INITIAL PARTS SURFACE ROUGHNESS OF 63 MICROINCHES RA REF SRM 55-10-09-2R-4 TOOL USED B/C 172329 NO DUE DATE; LOCATED AND DRSDR SWAA2024030848045Skin · cracked#2 LEADING EDGE SLAT NOSE SKIN EVIDENCE OF CRACK AT APPROX. SS322.71 #2 LEADING EDGE SLAT NOSE SKIN EVIDENCE OF CRACK AT APPROX. SS322.26<[01] ACCOMPLISHED L/E #2 SLAT NOSE SKIN REPAIR SRM 57-42-01-2R-8 AND RE-INSTALLED ACCESS PANEL 524CB; 524DB; 524EB AND FLESDR SWAA2024030747945Doubler · crackedEXTERNAL POWER DOOR CUTOUT SKIN DOUBLER IS CRACK AT AFT. LOWER EDGE.<[01] ACCOMPLISHED TRIMOUT REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE AFT LOWER EDGE IN REF B737-700 SRM 53-10-15-1A-4 FIG 104 DETAIL A.;[02] VERIFIED STEP 1SDR SWAA2023121129190Floor Panel · splitFWD. CARGO COMPARTMENT; THE AFT FLOOR PANEL IS SPLIT IN THE MIDDLE.<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT; AFT FLOOR PANEL 120CF PER AMM 25-52-10.SDR SWAA2023092604126Sign · missingWALL EXIT SIGN MISSING FROM EMER EXIT CAPT SIDE<[01] INSTALLED IAW AMM 33-51-01SDR SWAA2023083195705Support Bracket · crackedRIGHT WING TRAILING EDGE PANEL 661AB UPPER SUPPORT BRACKET CRACKED AT LOWER RADIUS. ACCOMPLISHED TEMPORARY REPAIR OF DAMAGE PER EA 23-157-02656
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