N966WN
Service difficulty reports · 254
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 = 'N966WN' 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 = 'N966WN' 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 SWAA2023083192860Access Panel · bulgedL/H WING LOWER MID T/E ACCESS PANEL # 561CB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL #561CB AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ASDR SWAA2023083092549Panel · bulgedR/H FWD O/B ACCESSPANEL # 193CR HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL 193CR AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ANA PO#1690463SDR SWAA2023083184940Support · crackedFWD CABIN WET AREA FUS FRAME SUPPORT SMALL CRACKED @ FLANGE CUTOUT S-7L STA 312 ABOVE L-1 DOOR CUTOUT UPPER FWD MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR AT STA 312 UPPER CHORD PER ATTACHED EA # M-22-153-01244.;[02] VERIFIED; STEP # 1SDR SWAA2023083184938Attach Angle · crackedCRACK AT UPPER VAPOR BARRIER ATTACH ANGLE STA 663 LBL 8 SEEN THRU AC BAY. 8-30<[01] REMOVED AND INSTALLED NEW FABRICATED REPAIR PARTS AT UPPER VAPOR BARRIER ATTACH ANGLE AT STA 663; LBL 8 AS PER B737-700 SRM 51-40-02-0G-0; SRM 57-10-10-2R-5.;[02] (RII) FINAL ISDR SWAA2023083184780Gusset · crackedFWD CARGO COMPARTMENT RIGHT SIDE; GUSSET HAS CRACK INTERNAL AREA; AT STRINGER 19R STA 500D.<[01] REMOVED AND REPLACED GUSSET AT RIGHT SIDE FWD CARGO COMP STRINGER 19R STA 500D PER REF SRM 51-40-02-0G 0;[02] REMOVED AND REPLACED GUSSET AT RIGHT SIDE FWD CARGO CSDR SWAA2023083184767Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #242RF; UPPER SURFACE DELAMINATED DOT 223-AW242RF.<[01] RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZT2.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ONSDR SWAA2023083184612Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241ACF; UPPER SURFACE DELAMINATED DOT 223-AW241ACF.<[01] RECEIVED PANEL 241ACF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241ACF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00MSDR SWAA2023083184611Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241AEF; UPPER SURFACE DELAMINATED DOT 223-AW241AEF.<[01] RECEIVED PANEL 241AEF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241AEF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00MSDR SWAA2023083184610Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241ADF; UPPER SURFACE DELAMINATED DOT 223-AW241ADF.<[01] RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZAL.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULTSDR SWAA2023083184609Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #242WF; UPPER SURFACE DELAMINATED DOT 223-AW242WF.<[01] RECEIVED PANEL 242WF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242WF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZSS.;[02] SDR SWAA2023083184613Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #242UF; UPPER SURFACE DELAMINATED UPPER SURFACE DELAMINATED DOT 223-AW242UF.<[01] RECEIVED PANEL 242UF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242UF WILL BE COMPLETED ONSDR SWAA2023083184606Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #232SF; UPPER SURFACE DELAMINATED DOT 223-CP232SF.<[01] RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144A5810-161); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZCA.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144ASDR SWAA2023083184608Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #231ZF; UPPER SURFACE DELAMINATED DOT 223-CP231ZF.<[01] RECEIVED NEW PANEL 231ZF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZD4;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023083184607Access Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241DF; UPPER SURFACE DELAMINATED DOT 223-CP241DF.<[01] RECEIVED NEW PANEL 241DF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZAA;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023083184100Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL NO- 221EF UPPER SKIN SURFACE DELAMINATED MKD DOT<[01] RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141A5810-249); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZUJ.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141SDR SWAA2023083184101Floor Panel · corrodedFWD CABIN WET AREA FLOOR PANEL NO-221BF UPPER SURFACE SKIN BULGING ;DELAMINATED AREAS MKD DOT<[01] RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZUS;[02] FINAL INSPECTION; RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAUSDR SWAA2023083183836Channel · crackedMAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ RBL- 1 STA 540 MKD DOT<[01] REMOVED AND INSTALLED NEW FLOOR SUPPORT BREAK PANEL (CHANNEL) AT MAIN CABIN CENTER AISLE STA 540; FROM RBL 1 TO RBL 21 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 143A0060.;[02] VERISDR SWAA2023083183837Channel · crackedMAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ LBL- 1 STA 540 MKD DOT<[01] REMOVED AND INSTALLED NEW FLOOR SUPPORT BREAK ASSY CHANNEL AT STA 540 FROM LBL 1 TO LBL 21 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 143A0060.;[02] VERIFIED STEP 1 FINALSDR SWAA2023083183687Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231GF. 8-64<[01] RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZTU;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZTUSDR SWAA2023083183680Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING RF. 8-66 PANEL FLOOR 241RF<[01] RECEIVED NEW PANEL 241RF ; THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00M6Z9S;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023083183679Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 241UF. 8-67<[01] RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6YE6.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLSDR SWAA2023083183682Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231XF. 8-62<[01] RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0.SDR SWAA2023083183678Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231KF. 8-63<[01] RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZTN;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSDR SWAA2023083183677Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231DF. 8-65<[01] RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZU0.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLSDR SWAA2023090183036Panel · crackedLEFT WING LOWER MID SPAN T/E PANEL #561BB; INNER/LOWER SURFACE CRACK/DELAMINATED DOT 223-LW561BB.<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA AT LEFT WING LOWER MID SPAN T/E PANEL #561BB AS PER B737 SRM 57-51-01-2R-1; SRM 51-70-05-2R-4 PARAG 4.E AND SRM 51-7SDR SWAA2023071878444Light · inoperativeEMERGENCY LIGHT FWD OF RH AFT CARGO INOP.<[01] RELAMPED AFT R/H SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2023062972994Floorboard · crackedAFT CARGO FLOOR BOARD 140BF HAS CRACK 15 INCHES LONG; ALONG CENTER FLOOR FRAME.<[01] REMOVED AND REPLACED AFT CARGO FLOOR BOARD 140BF PER AMM 25-52-10SDR SWAA2023062059950Indicator · faultyDUE TO AHM DATA. AIRCRAFT LOGGING L/R FLAP POSITION MARGIN FAULTS. PLEASE T/S USING THE FMS MCDU AND WATCH THE MARGIN NUMBER AS YOU MOVE THE FLAPS. YOU SHOULD NOT SEE THE MARGIN NUMBER DROP BELOW 6. REMOVE INDICATOR AND IF PROBLEM GOES AWAY REPLACE THE INDICATSDR SWAA2023052552311Slide · looseJ HOOK FOR FWD ENTRY DOOR SLIDE LOOSE.<[01] TIGHTENED J HOOK FOR L1 DOOR BY USING HAND PRESSURE TO CLOSE J HOOK PER SIPSDR SWAA2023030612671Wheel · blownBLOWN #2 TIRE ON TAKEOFF ACCOMPLISHED AN OVERWEIGHT LANDING AT 132.1 K<[01] R/R #1 & #2 MLG WHEEL ASSY REF AMM 32-45-11.SDR SWAA2022111068460Megaphone · inoperativeFA AFT MEGAPHONE DOES NOT WORK / [01] REPLACED MEGAPHONE PER AMM 25-64-00. OPS CHECK GOOD.SDR SWAA2022081241037Bracket · crackedAFT GALLEY SERVICE DOOR LINER LOWER SUPPORT BRACKETS CRACKED. / [01] R&R AFT GALLEY SERVICE DOOR LINER LOWER SUPPORT BRACKET PER AMM 52-41-31SDR SWAA2022081241035Sliding Sleeve · cracked-RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / [01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER MM 53-31-31SDR SWAA2022081241036Seal Plate · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / [01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.SDR SWAA2022051106030Slide · low pressureAFT ENTRY DOOR SLIDE NEEDLE IN RED (LOW) / [01] REPLACED AFT ENTRY SLIDE PER MT725-61-06SDR SWAA2022042997842Slide · out of adjustAFT ENTRY DOOR SLIDE NEEDS TO BE ADJUSTED IN THE SLIDE BUSTLE SO THAT GREEN BAND OF PRESSURE GAUGE IS VISIBLE / [01] READJUSTED AFT ENTRY DOOR SLIDE REF M/M 25-66-01;[02] C/WSDR SWAA2021120850644None · looseSUPPLEMENTAL INFORMATION: PHOTO ILLUM STRIP NEAR ROW 9 LOOSE ; / [01] SECURED PHOTO ILLUMINATION STRIP @ ROW 9 PER SIP.SDR SWAA2021120749933Megaphone · brokenFORWARD MEGAPHONE IS BROKEN ; / [01] REMOVED AND REPLACED FORWARD MEGAPHONE IN REFERENCE TO AMM 25-64-00.SDR SWAA2021091315726Battery Pack · inoperativeM1675 EMERGENCY LIGHT BATTERY PACK INOP. ; / [01] SWAPPED KNOWN GOOD BATTERY PACK INTO CHARGER ASSEMBLY M1675 TO CONFIRM BATTERY PACK INOP PER AMM 33-51-06-960-805. KNOWN GOOD UNIT TURNS LIGHTS ON AS INTENDED; M1675 REQUIRES REPLACEMENT. RESTORED BATTERY PACKSSDR SWAA2021091315728Bulb · inoperativeL/H OVERWING EMERGENCY EXIT DOOR EXIT LOCATOR SIGN HAS 1EA BULBS INOP. ; / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF L/H OVERWING EMERGENCY EXIT DOOR LOCATOR SIGN LIGHT LAMP PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION ENTRY 1SDR SWAA2021091314262Gusset · crackedR/H GUSSET FOUND TO BE CRACKED AT BS500D STR19R WL190 / [01] REMOVED GUSSET AT BS 500D STR 19R WL 190. IAW. SRM 51-40-02; [02] EVALUATED DAMAGE ON GUSSET LOCATED AT B/S 500D STR 19R WL 190 AND NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPLACED IAW SRM 5SDR SWAA2021091314261Gusset · crackedL/H GUSSET FOUND TO BE CRACKED AT BS500D STR19L WL190 / [01] REMOVED GUSSET AT BS 500D STR 19L WL 190. IAW. SRM 51-40-02; [02] EVALUATED DAMAGE ON GUSSET LOCATED AT B/S 500D STR 19L WL 190 AND NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPLACED IAW SRM 5SDR SWAA2021091313418Strap · corrodedAFT CARGO BAY FLOOR STRAP CORODDED BS 772 RBL 21- LBL 21 WL 156 ; / [01] REMOVED AFT CARGO BAY FLOOR STRAP BS772 RBL21-LBL21 IAW SRM 51-40-02-0G-0; [02] THERE IS NO ALLOWABLE DAMAGE FOR AFT CARGO BAY FLOOR STRAP. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-1SDR SWAA2021091312220Support Angle · crackedACB WASTE TANK ENCLOSE BULKHEAD SUPPORT ANGLE CRACKED. BS867-1.5; LBL10; WL161 ; / [01] REMOVED BULKHEAD ANGLE SUPPORT AT BS867-1.5' LBL10 WL161 IAW SRM 51-40-02 NO ALLOWABLE LIMITS FOR CRACK; ANGLE IS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; [02] REMOVED BULSDR SWAA2021091312145Shield · corrodedACB FWD SHIELD CORROSION. BS767+11.5; RBL22; WL151 ; / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REP AIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [02] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REPAIR WISDR SWAA2021091312820Shield · corrodedCORROSION ON FORWARD BAY SHIELD AT B.S. 494-500A; R.B.L. 24; W.L. 154. ; / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 RECEIVED NEW BAY SHIELD ITEM HFAB53-SHD-011; LOT:1467549-1; PO NUMBER: 835449. LOCATED AND DRILLED; COSDR SWAA2021091312818Support · corrodedCORROSION ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D; L.B.L. 24 - R.B.L. 24; W.L. 154. ; / [01] ADDED MEASURMENTS; [02] NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BSSDR SWAA2021091312191Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+4; RBL22; WL151 ; / REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+4'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF SDR SWAA2021091312185Shield · corrodedACB FWD SHIELD CORROSION. BS767+3.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+3.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLASDR SWAA2021091312195Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO
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