N962WN
Service difficulty reports · 194
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 = 'N962WN' 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 = 'N962WN' 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 SWAA2021080295684Bulkhead Web · damagedL/H VAPOR BARRIER FASTENER ATTACH HOLES ON O/B END (APPROX. 39) ARE OVERSIZED ; / PART/MATERIAL IDENTIFIED PER SRM 57-10-10-0I-2 FIG 2 TABLE 2 ITEM 4 .<BR>30' OF THE O/B EDGE BAND OVERSIZE HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-10-10-1A-2 PARA 4 SDR SWAA2021080394625Skate Angle · chafedCHAFE DAMAGE ON THE R/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED R/H SKATE ANGLES IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U4 PO#823628 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOSDR SWAA2021080394626Skate Angle · corrodedCHAFE DAMAGE ON THE L/H VERTICAL STAB TO FUSELAGE SKATE ANGLES / [01] REMOVED LH SKATE ANGLES PER SRM 51-40-02.; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 148A8310U3 PO#829514 /1 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 148A8300 REV.A; [03] NOSDR SWAA2021080394611Floorbeam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 259.5; LBL 1; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.3' X 0.4' AREA; MAX DEPTH .005' PER SRM 51-10-02-0G-0; MEASURED WITH CAL ID: ATS2472 SN: UNKNOWN CAL DATE: 06/2021. ORIGINAL THICKNESS IS .094' PER DWG 141SDR SWAA2021080294610Beam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 259.5; LBL 5; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.2' X 0.6' AREA; MAX DEPTH OF BLENDOUT .006' PER SRM 51-10-02-0G-0; MEASURED WITH MICROMETER CAL ID: IS000461 S/N: 67126205 CAL DATE: 01/2021. ORIGINAL THICSDR SWAA2021080294621Beam · corrodedCORROSION ON FLIGHT DECK LATERAL BEAM BS 270; RBL 2.5; WL 208 (MARKED) ; / [01] REMOVED CORROSION IN A 1.5' X 0.6' AREA; MAX DEPTH .008' PER SRM 53-10-51-1A-1;FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1.; [02] REMOVED NUTPLATE AT BS 270; RBL 2.5; WL 208 PESDR SWAA2021080294609Attach Angle · damagedREJECT- L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE DAMAGE REMOVAL CUTLINE IS NOT TRIMMED AS SHOWN IN SRM 57-10-10-2R-5; FIGURE 202 REPAIR 5 ; / [01] CUT OUT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE DAMAGE IAW SRM 57-10-10-2R-5; [02] VERIFIED; [03] VERIFIEDSDR SWAA2021080394613Sidewall Support · corrodedCORROSION BS727E +6- +12 LBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED CORROSION FROM L/H ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6 MEASURED 2'L X 1'W AND 0.020' DEEP. ORIGINAL THIKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] VERIFIESDR SWAA2021080294604Plate · corrodedCORROSION BS767 RBL 24 WL157 PLATE THAT TIES TOP OF FRAME TO FWD SHIELD CORRODED / [01] REMOVED PLATE COMMON TO FRAME AT BS 767 RBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-SDR SWAA2021080294606Shield · corrodedCORROSION BS767-787 RBL24 WL157 SHIELD UPPER SURFACE / [01] REMOVED AFT CARGO BAY SHIELD BS767-787 RBL24 WL157 IAW SRM 51-40-02; [02] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR ACB FWD SHIELD; PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02; [03] VERIFIEDSDR SWAA2021080294605Intercostal · corrodedCORROSION BS767-787 TR25R INTERCOSTAL UPPER CHORD CORRODED IN SEVERAL PLACES COMMON TO NUT PLATES / [01] REMOVED CORROSION ON INTERCOSTAL UPPER CHORD AT BS 767 TO BS 787; RBL 25 ; WL 157 ; WORK AREA IS 18.5' X 0.950' X 0.009' ; ORIGINAL THICKNESS IS 0.050' ; RSDR SWAA2021080294598Support · corrodedCORROSION BS727C+14-18 RBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727-767 RBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT AT BS 727C+14 RBL23 MEASDR SWAA2021080294617Retainer · corrodedCORROSION BS790 RBL24 WL157 ON NUT PLATE RETAINER / [01] REMOVED CORROSION ON NUT PLATE RETAINER AT BS 790 ; RBL 24 ;WL 157 ; WORK AREA IS 5.0' X 0.900' X 0.005 ; ORIGINAL THICKNESS IS 0.040 ; REMAINING THICKNESS IS 0.035 ; FOUND TO BE OUT OF LIMITS IAW SRM 53SDR SWAA2021080294599Support · corrodedCORROSION BS727C+10 LBL 24 WL157 FLOOR TO SIDEWALL SUPPORT / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 727-787 LBL 24 WL 157 PER SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT BS727C+10 LBL24 MEASURSDR SWAA2021080294607Web · corrodedCORROSION BS792-810 RBL28 WL157 UPPER SURFACE OF SUB THRESHOLD CORRODED IN SEVERAL PLACES / [01] REMOVED ACB SUBTHRESHOLD WEB BS 792-847 RBL 21-28 WL 157 PER SRM 51-40-02; [02] VERIFIED REMOVAL; [03] REMOVED CORROSION ON SUB THRESHOLD AT BS792-810 RBL28 WL157;SDR SWAA2021080293322Attach Angle · crackedL/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED LBL 40 WL 164 ; / CUT OUT DAMAGE ANGLE IAW SRM 57-10-10-2R-5 FABRICATED; LOCATED AND DRILLED REPAIR PARTS IAW SRM 57-10-2R-5. MATERIAL ID:<BR>ITEM [1] 2024T3#0.063 CLAD; LOT #1457316-1 <BR>ITEM[2] 2024T3#0.07SDR SWAA2021080293269Floor Panel · damagedFWD CARGO BAY FLOOR PNL 120AF DAMAGED ; / [01] FABRICATED NEW FCB FLOOR PANEL 120AF FROM 090 CONOLITE; LOT# 1454533-1 PER AMM 25-52-01-201-801; [02] ADDED DWG REFERENCE 453A1610; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801 AND DWG 453A1610SDR SWAA2021080293263Floor Panel · damagedAFT CARGO BAY FLOOR PNL 140AF DAMAGED ; / [01] FABRICATED NEW ACB FLOOR PANEL 140AF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801SDR SWAA2021080293264Floor Panel · damagedAFT CARGO BAY FLOOR PNL 140BF DAMAGED ; / [01] FABRICATED NEW ACB FLOOR PANEL 140BF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801SDR SWAA2021080293270Floor Panel · damagedFWD CARGO BAY FLOOR PNL 120CF DAMAGED ; / [01] FABRICATED NEW FCB FLOOR PANEL 120CF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A1610; [02] ADDED MEASUREMENT INFORMATION; [03] VERIFIED FABRICATION OF NEW PANEL PER AMM 25-52-01-201-801SDR SWAA2021080293284Floor Panel · delaminatedFLOOR PANEL 242CF - UPPER FORWARD L/H CORNER IS DELAMINATED ; / [01] IDENTIFIED FLOOR PANEL 242CF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. DUE TO THE EXTENT OF DAMAGE OPTED TSDR SWAA2021080293285Floor Panel · damagedFLOOR PANEL 242BF - LOWER AFT L/H CORNER IS DAMAGED ; / [01] IDENTIFIED FLOOR PANEL 242BF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. DUE TO THE EXTENT OF DAMAGE OPTED TO FABRICSDR SWAA2021080293286Floor Panel · pulledFLOOR PANEL 231XF - UPPER SKIN HAS MULTIPLE STRANDS PULLED STARTING FROM LEADING EDGE OF PANEL ; / [01] IDENTIFIED FLOOR PANEL 231XF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4F. SDR SWAA2021080293267Floorbeam · crackedFLOOR SUPPORT BS 540; RBL 25 - BL 0; WL 208 CRACKED AT I/B FASTENER HOLE ; / [01] REMOVED AND INSTALLED FLOOR SUPPORT AT BS 540 RBL 25 TO BL 0 WL 208 PER SRM 51-40-02 AND BOEING DWG 143A0060. FLOOR SUPPORT STILL REQUIRES MATCH DRILL OF FLOOR PANEL FASTENER HOLSDR SWAA2021080293282Floorbeam · crackedFLOOR SUPPORT BS 540; LBL 25 - BL 0; WL 208 CRACKED AT I/B FASTENER HOLE ; / [01] REMOVED AND INSTALLED FLOOR SUPPORT AT BS540 LBL 25 TO BL 0 WL 208 PER SRM 51-40-02 AND BOEING DWG 143A0060. FLOOR SUPPORT STILL REQUIRES MATCH DRILL OF FLOOR PANEL FASTENER HOLESDR SWAA2021080292521Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL35 WL149. ; / [01] DAMAGE IS OUT OF ALLOWABLE LIMITS PER SRM 57-10-10-1A-2; PAR 1.C. DAMAGE TO BE REPAIRED PER SRM 51-70-04-2R-10 AS DIRECTED BY SRM 57-10-10-2R-2; PAR 1.B AND NOTE VERIFIED INSTALLED REPAIR PLIESDR SWAA2021032257076Handle · looseFORWARD SERVICE DOOR HANDLE IS LOOSE / TIGHTENED BOLTS ON FWD SERV DOOR HANDLE IAW MM 52-41-31 OPS CKS OKSDR SWAA2020110227084Battery Pack · inoperativeEMERGENCY LIGHTS AT LT EXIT ROW INOPERABLE. REMOVED AND REPLACED BATTERY PACK AT ROW 15 ABC FOR EMERGENCY LIGHTS, IAW AMM 33-51-06.SDR SWAA2020032332187Light · inoperativeSIDEWALL LIGHT OUT AT 11 ABC (EMERGENCY EXIT). / RELAMPED PASSENGER CABIN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-11.SDR SWAA2020031942586Light · inoperativeSIDEWALL LIGHT OUT AT 11 ABC (EMERGENCY EXIT). RELAMPED PASSENGER CABIN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-11.SDR SWAA2019072435271Connector · defectiveR2 DOOR HEADER EMERGENCY EXIT LIGHT INOP AT M1673. R&R CONNECTOR D10746 IAW SWPM AND WDM.SDR SWAA2019072435262Fuse · blownR2 DOOR HEADER EMERGENCY EXIT LIGHT INOP AT M1673. R&R FUSES IAW SWPM AND WDM.SDR SWAA2022031273236Support Angle · crackedLEFT MLG WHEEL WELL STA 663 LBL25 WL 150; VERTICAL SUPPORT ANGLE IS CRACKED AT BOTTOM END. / REMOVED & REPLACED LEFT MLG WHEEL WELL STA 663 LBL 25 WL 150 VERTICAL SUPPORT STIFFENER IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 & DWG 111A1000 REV-SDR SWAA2022031173209Support Bracket · crackedPASSENGER CABIN AT R1 DOOR CUTOUT STA 306-326 RBL 60; THRESHOLD SUPPORT BRACKET IS CORRODED. / BLENDED CORROSION WITH A MATERIAL LOSS OF .012' IS FOUND TO BE 'OUT OF LIMITS' AS PER B 737-700 SRM 53-10-15-1A-2 REMOVED AND REPLACED ATTACH ANGLE AS PER B 737-700 SDR SWAA2022031173212Angle · corrodedAFT CARGO COMP.RH Z-ANGLE HAS CORROSION AROUND SEVERAL FASTNER HOLES 727-727E / REMOVED AND REPLACED RH Z ANGLE FROM STA 727-767 ON SA-M 112 #X982183 IAW SRM 51-40-02-0G-0 AND DWG 146A7502 REV. -SDR SWAA2022031173213Angle · corrodedAFT CARGO COMP.RH Z-ANGLE HAS CORROSION AROUND SEVERAL FASTNER HOLES STA.727E-767 / REMOVED AND REPLACED RH Z ANGLE FROM STA 727-767 ON SA-M 112 #X982183 IAW SRM 51-40-02-0G-0 AND DWG 146A7812 REV.-SDR SWAA2022031173214Strap · corrodedAFT CARGO COMP.FLOOR BOARD STRAP CORRODED AROUND FASTNER HOLES STA. 767 / REMOVED AND REPLACED AFT CARGO FLOOR BOARD STRAP ASSEMBLY AT STA 767 IAW SRM 51-40-02-0G-0 AND DWG 146A 7500 RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802 PN: 146A9401-4 ATAG: SDR SWAA2022031173226Floor Panel · crackedFLOOR PANEL 242XF CRACKED / INSTALLED NEW FLOOR PANEL; WORK ACCOMPLISHED ON J.PANEL CARD - 241-CLOSESDR SWAA2019071935135Threshold · corrodedAFT CARGO COMPARTMENT THRESHOLD WEB CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 794 TO BS. 847, BETWEEN RBL 20 TO RBL 24. R&R WEB IAW SRM, AMM & DWG.SDR SWAA2019071835038Crease Beam · corrodedL2 DOOR CUTOUT CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 965 TO BS. 985, LBL 53. R&R CREASE BEAM INNER CHORD IAW DWG AND SRM.SDR SWAA2019071835037Crease Beam · corrodedR2 DOOR CUTOUT CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 960 TO BS. 985, RBL 53. R&R INNER CHORD IAW SRM AND DWG.SDR SWAA2019071834946Floorboard · damagedPASSENGER CABIN FLOORBOARD 221EF HAS UPPER PLY DAMAGED, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD PANEL IAW SRM.SDR SWAA2019071834948Crease Beam · corrodedL1 DOOR INNER CREASE BEAM ANGLE CORRODED ON UPPER SURFACE AT BS. 303.9, LBL 53. R&R L1 DOOR INNER CHORD (CREASE BEAM) PER SRM AND DWG.SDR SWAA2019071834945Floorboard · damagedPASSENGER CABIN FLOORBOARD 221DF HAD UPPER PLY AND INSERT DAMAGE BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD IAW SRM.SDR SWAA2019071634928Floor Support · crackedLONGITUDINAL FLOOR SUPPORT CRACKED AT BS. 312+4.5, RBL 33.5. R&R FLOOR SUPPORT ANGLE IAW SRM & DWG.SDR SWAA2019071634927Floor Support · crackedLONGITUDINAL FLOOR SUPPORT CRACKED AT BS. 277+7.5, BL 0. R&R FLOOR SUPPORT IAW DWG, SRM, & AMM.SDR SWAA2019071634926Floorboard · damagedAFT CABIN FLOORBOARD 242RF HAD UPPER PLY DAMAGE, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOORBOARD 242RF IAW SRM.SDR SWAA2019071634925Floorboard · damagedPASSENGER CABIN FLOOR BOARD 221BF HAD UPPER PLY DAMAGE, BETWEEN BS. 270 TO BS. 420. REPAIRED UPPER FACE SHEET IAW SRM.SDR SWAA2022031173194Seal · crackedRIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IS CRACKED / REMOVED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL AND FWD AND AFT CENTER TRACK STRIP IAW 737 AMM 53-31-31-000-802 RECEIVED AND VERIFIED NEW PART P/N 181A8025-2 IAW IPC 53-31-31-03 INSSDR SWAA2022031173196Seal · crackedLH HORIZONTAL STAB; UPPER FWD SLIDING SEAL IS CRAKED AT FWD SIDE ALONG GUIDE TRACK / REMOVED CRACKED LH HORIZONTAL STAB UPPER FORWARD SLIDING SEAL IAW 737 SRM 51-40-02-0G-0 AND 737 AMM 53-31-000-802. RECEIVED AND VERIFIED NEW SLIDING SEAL IAW 737 IPC 53-31-31-
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