N941WN
Service difficulty reports · 219
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 = 'N941WN' 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 = 'N941WN' 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 SWAA2021081991921Floor Panel · peelingPASSENGER CABIN FLOOR;PANEL 241ABF TOP SKIN FIBERS PEELING UP ; / [01] EVALUATED DAMAGE; TOP SKIN IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR ARE IAW B737 SRM 53-00-50-2R-1 PAR 3; STEPS A;C;SDR SWAA2021081991911Floor Panel · peelingPASSENGER CABIN FLOOR;PANEL 242UF TOP SKIN FIBERS PEELING UP ; / [01] EVALUATED AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE FACE SHEET AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1<BR><BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53SDR SWAA2021081991918Floor Panel · peelingPASSENGER CABIN FLOOR;PANEL 241AAF TOP SKIN FIBERS PEELING UP ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-5SDR SWAA2021081991909Bracket · crackedA045-006; FORWARD CARGO COMPARTMENT; GUSSET ATTACH BRACKET CRACKED AT RADIUS; FORWARD SIDE OF STA:500D; STR:19L. ; / [01] REMOVED OLD GUSSET; VERIFIED NEW PN 143A9481-6; A-TAG A62903. BOEING DWG 143A7902 SHT 209 REV-. DRIILLED UP NEW GUSSET IAW SRM 51-40-05-0GSDR SWAA2021081991923Gusset · crackedA045-007; FORWARD CARGO COMPARTMENT; GUSSET ATTACH BRACKET CRACKED AT RADIUS; FORWARD SIDE OF STA:500D; STR:19R. ; / [01] REMOVED CRACKED GUSSET ATTACH BRACKET IN FWD CARGO PIT STA 500D; STR 19R IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW GUSSET ATTACH BRACKET P/SDR SWAA2021081991424Support Angle · crackedAFT CARGO COMPARTMENT; BULKHEAD SUPPORT ANGLE AT STA 867; LBL 12; WL 155; CRACKED DOT#A-193-51 ; / [01] VERIFIED NEW PART AS P/N 149A8109-114 ATAG A02639 IAW DWG 149A8102 REV -; [02] REMOVED CRACKED ANGLE AND DRILLED NEW IAW SRM 51-40-02-0G-0; 51-40-05-G-0-; DSDR SWAA2021081991908Angle · corrodedA045-004; FORWARD PIT; RH Z-ANGLE HAS CORROSION. BS:500 TO 500D; RBL:25; WL:155. ; / [01] REMOVED DAMAGE FROM R/H Z-ANGLE IN FWD CARGO COMPARTMENT; STA 500-500D IAW SRM 51-10-02-0G-0 SECTION 15; VERIFIED WITH 10X MAGNIFICATION. VERIFIED MATERIAL LOSS ORIGINAL SDR SWAA2021081991443Angle · corrodedAFT CARGO COMPARTMENT; LH Z-ANGLE HAS CORROSION AT STA 787+11'; LBL 21; WL 156; DOT#A-193-49 ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 SECTION 15; VERIFIED WITH 10X MAGINIFICATION. VERIFIED LIMITS; ORIGINAL THICKNESS .040' LOSS.010' REMAINING .030' OUT SDR SWAA2021081991433Angle · corrodedAFT CARGO COMPARTMENT; LH Z-ANGLE HAS CORROSION AT STA 747+2'; LBL 21; WL 156; DOT#A-193-43 ; / [01] FABRICATED REPLACEMENT ZEE ANGLE BS 727-847 IAW SRM 53-00-52-2R-5 ON FAULT TTG8Q005PPNQ; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991434Angle · corrodedAFT CARGO COMPARTMENT; LH Z-ANGLE HAS CORROSION AT STA 747+15'; LBL 21; WL 156; DOT#A-193-45 ; / [01] FABRICATED REPLACEMENT ZEE ANGLE BS 727-847 IAW SRM 53-00-52-2R-5 ON FAULT TTG8Q005PPNQ; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991436Shield · corrodedAFT CARGO COMPARTMENT; RH; AFT CARGO DOOR SURROUND FWD SHIELD CORROSION AT STA 767+7'; LBL 21; WL 156; DOT#A-193-48 ; / [01] REMOVED CORROSION FRM AFT CARGO COMPARTMENT FWD SHIELD; INSPECTED WITH 10X MAG GLASS; NO DEFECTS. ORIGINAL T= .050' LOSS OF .010' REMAISDR SWAA2021081991437Angle · corrodedAFT CARGO COMPARTMENT; LH Z-ANGLE HAS CORROSION AT STA 727E+18'; LBL 21; WL 156; DOT#A-193-32 ; / [01] FABRICATED REPLACEMENT ZEE ANGLE BS 727-847 IAW SRM 53-00-52-2R-5 ON FAULT TTG8Q005PPNQ; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991442Angle · corrodedAFT CARGO COMPARTMENT; LH Z-ANGLE HAS CORROSION AT STA 747+9'; LBL 21; WL 156; DOT#A-193-44 ; / [01] FABRICATED REPLACEMENT ZEE ANGLE BS 727-847 IAW SRM 53-00-52-2R-5 ON FAULT TTG8Q005PPNQ; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991907Shield · corrodedA045-003; FORWARD PIT; RH SIDE SHIELD HAS CORROSION. BS:480+15 TO 500+11; RBL:25; WL:155. ; / [01] EVALUATED MATERIAL LOSS AND FOUND AREA TO HAVE 100% MATERIAL LOSS IAW SRM 53-00-53-1A-2; [02] RECIEVED AND VERIFIED NEW SHIELD P/N 143A8126U31ATSMRO ATAG BF3641 SDR SWAA2021081991914Crease Beam · corrodedPASSENGER CABIN FLOOR;R1 CREASE BEAM CORRODED AT SCUFF PLATE ATTACH ANGLE STA.947-967 RBL 55 WL 208 ; CORRECTING POSITION OF DEFECT: SHOULD BE R2 CREASE BEAM / [01] REMOVED CORROSION FROM PASSENGER CABIN CREASE BEAM AT SCUFF PLATE ATTACH ANGLE STA 947-967; RBLSDR SWAA2021081991915Crease Beam · corrodedPASSENGER CABIN FLOOR;R1 CREASE BEAM CORRODED AT SCUFF PLATE ATTACH ANGLE STA.967-987 RBL 55 WL 208 ; CORRECTION. SHOULD READ R2 CREASE BEAM . / [01] CREASE BEAM BEEN REPLACED ON N/R 42428/2400/0053 <BR>TTG8Q005PUYY; [02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2021081991905Floorbeam · corrodedPASSENGER CABIN FLOOR;STA 987 FLOOR BEAM CORRODED AROUND FASTNER HOLE RBL 50 WL208 ; / [01] REMOVED NUT PLATE I.A.W SRM 51-4-02-0G-0; [02] REMOVE CORROSION AND VISUALLY INSPECTED AREA WITH 10X MAGNIFIER NO DEFECTS NOTED I.A.W SRM53-70-51-1A-1; [03] VERIFIED MASDR SWAA2021071291934Beam · crackedR-1 DOOR #5 BEAM 141A6536-14 IS CRACKED IN RADIUS NEAR MOST INBD HOLE IN INSPECTION AREA. REMOVED #4 BEAM FROM R1 DOOR IAW SRM 51-40-02-0G-0. VERIFIED NEW #4 BEAM IAW EO# 5241-C-14093-NG. LOCATED AND DRILLED NEW #4 BEAM IAW SRM 51-40-02-0G-0 AND DWG'S 141A6SDR SWAA2021071291932Door · out of alignmentR1 DOOR IS SAGGING. REMOVED BODY SIDE TORQUE TUBE COVER IAW SRM 51-40-02-0G-0. REMOVED UPPER TORQUE TUBE BEARING PLATE IAW SRM 51-40-02-0G-0. REMOVED AND REPLACED WORN BEARING IN UPPER TORQUE TUBE PLATE IAW SOPM 20-50-03. VERIFIED STEP 2 OK TO INSTALL BEARINGSDR SWAA2021081991415Floorboard · peelingPASSENGER CABIN; FWD LAV FLOOR BOARD AFT OUTBD CORNER TOP SKIN PEELING UP ; / [01] EVALUATED DAMAGE; AFT OUTBD CORNER TOP SKIN IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED REPAIR AREA; POTTED CORE IAW B737 SRM 53-00-50-2R-1 PAR 3; STEPSSDR SWAA2021081991414Fitting · corrodedPASSENGER CABIN COMP.L1 FWD GIRT BAR FITTNG CORRODED STA.312 LBL 60 WL 208 ; / [01] REMOVED AND REPLACED L1 DOOR FWD GIRT BAR FITTING TIE DOWN PLATE P/N 141A5220-2 ATAG A63447 IAW SRM 51-40-02-G-0; IPC 53-42-00-29; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021081991420Shield · corrodedA45-001; FORWARD CARGO COMPARTMENT; RIGHT HAND SIDE SHIELD HAS CORROSION; BS:420+9 TO 420+13; RBL:25; WL: 155. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 SECTION 15; VERIFIED WITH 10X MAGNIFICATION. VERIFIED LIMITS ORIGINAL THICKNESS .032' LOSS .007' REMSDR SWAA2021081991419Web · corrodedAFT CARGO DOOR CUT OUT BOTTOM WEB CORRODED STA 797 WL 156 RBL20' ; / [01] REMOVED CORROSION FROM LOWER SILL WEB ORIGINAL T= .045' LOSS OF .011' REMAINING T= .034' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103 DETAIL D TOOLING # 21461 CAL DUE 04AUG21;SDR SWAA2021081997303Scuff Plate · brokenA22-46; FWD PIT THRESHOLD; AFT SCUFF PLATE BROKEN ; / [01] FORWARD CARGO AFT CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O 42430-1400-0001 SERIAL NO. 8199403 IAW SRM 53-30-15-2R-1; [02] VERIFIED ITEM 1<BR>OK TO TREAT AND PRIME; [03] OK TO TREAT AND PRIME; [SDR SWAA2021081990860Support · crackedA-125-5 PANEL 195AR FAIRING SUPPORT CRACKED AT LOCK FASTENER. I/B OF LANDING LIGHT RIGHT SIDE. ; / [01] BEGAN REMOVAL OF FAIRING SUPPORT IAW SRM 51-40-02-0G-0; [02] COMPLETED REMOVAL OF FAIRING SUPPORT END RIB ASSY. IAW SRM 51-40-02-0G-0; [03] LOCATED AND DRILSDR SWAA2021081990859Floor Panel · corrodedA22-45; AFT PIT FLOOR PANEL 140CF; 6EA AREAS AROUND PANEL PERIMETER; CORROSION; MRK'D. (SECONDARY STRUCTURE) ; / [01] VERIFIED MATERIAL AS 2024-T3; .071 IAW AMM 25-52-01-201-801. A-TAG # A53467.; [02] VERIFIED STEP 1 C/W; [03] FABRICATED REPLACEMENT AFT PIT FLSDR SWAA2021040239097Floorboard · damagedFLOOR BOARD CREEKS AT ROW 2 3 IN ISLE WHEN WALKED ON REMOVED FLOOR BOARD AT ROW 2 3 INSPECTED AND RESECURED SCREWS PER AMM 532100.SDR SWAA2020102926119Lens · missingFWD SERVICE DOOR LOWER FWD EMERGENCY EXIT LIGHT MISSING DIRECTIONAL ARROW. REMOVED & REPLACED FWD SERVICE DOOR LOWER FWD EMERGENCY EXIT LIGHT LENS, PER AMM 33-51-01.SDR SWAA2020072201661Power Supply · inoperativeAFT RT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.SDR SWAA2020030442087Controller · faultyDIVERSION/DECLARED EMERGENCY----------------------------------------------------------CLIMBING THROUGH FL360, HEAR A LOUD BANGING NOISE BEHIND COCKPIT DOOR AND REPORTED IN FORWARD CABIN AREA BY FLT ATTND. NO ABNORMAL INDICATIONS ON ENGINES OR PRESSURIZATION NOSDR SWAA2019072435261Lens · crackedR1 EMERGENCY LIGHT LENS CRACKED. INSTALLED LENS PER AMM.SDR SWAA2019072235207Battery Pack · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1674. R&R EMERGENCY BATTERY PACK PER AMM.SDR SWAA2019072235206Battery Pack · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1670. R&R EMERGENCY BATTERY PACK PER AMM.SDR SWAA2019072235205Fuse · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1675. R&R EMERGENCY FUSE PER AMM.SDR SWAA2019072235204Power Supply · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1674. R&R EMERGENCY POWER SUPPLY PER AMM.SDR SWAA2019072235202Power Supply · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1670. R&R EMERGENCY POWER SUPPLY PER AMM.SDR SWAA2019072335230Structure · crackedFOUND CRACKED 1EA. FASTENER HOLE AT LT HORIZONTAL STABILIZER UPPER CHORD INBOARD FLANGE, 29.0" FROM FRONT SPAR (BETWEEN STIFFENERS # 3 & 4) RIB #5. REPAIRED UPPER CHORD IAW EA.SDR SWAA2019072335229Rib · crackedFASTENER HOLE AT L/H HORIZONTAL STABILIZER RIB #5 CRACKED UPPER CHORD INBOARD FLANGE,19.0" FROM FRONT SPAR (BETWEEN STIFFENERS 2 & 3). REPAIRED UPPER CHORD IAW EA.SDR SWAA2019072335228Rib · crackedLT HORIZONTAL STABILIZER RIB #5 UPPER FORWARD END CRACKED. REPAIRED RIB IAW EA.SDR SWAA2019071834944Rib · crackedLT HORIZONTAL STABILIZER RIB 5 LOWER FORWARD END CRACKED. REPAIRED STABILIZER AW SRM.SDR SWAA2022031167090Skin · crackedLEFT WING MOVEABLE LEADING EDGE SLAT # 1 CRACKS AT NOSE SKIN ACTUATOR ATTACHMENT POINT. / REMOVED AND REPLACED #1 SLAT ASSY; PERFORMED ADJUSTMENT FOUND OK; REF B737-700 MM 27-81-21-400-801; 27-81-00-820-803SDR SWAA2022031167091Skin · crackedLEFT WING MOVEABLE L/E SLAT # 2 CRACKS AT NOSE SKIN ACTUATOR ATTACHMENT POINT MKD DOT 60-043 / REMOVED AND REPLACED #2 SLAT ASSY; PERFORMED ADJUSTMENT FOUND OK; REF B737-700 MM 27-81-21-400-801; 27-81-00-820-803SDR SWAA2019071634852Attach Angle · crackedRT HORIZONTAL STABILIZER RIB # 4 ATTACH ANGLE CRACKED AT LEADING EDGE WEB ATTACH POINT. R&R STIFFENER ANGLE IAW SRM.SDR SWAA2019071634878Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 34.5" FROM FRONT SPAR. REPAIRED RIB IAW SRM.SDR SWAA2019071634851Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 34.4" FROM FRONT SPAR. REPAIRED RIB IAW SRM.SDR SWAA2019071634850Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 26.5" FROM FRONT SPAR. REPAIRED RIB IAW SRM.SDR SWAA2019071234780Stiffener · crackedLT HORIZONTAL STABILIZER RIB #4 (36" AFT OF FRONT SPAR) LOWER PART OF STIFFNER CRACKED. REPAIRED STIFFENER IAW SRM.SDR SWAA2019071234779Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 4 CRACKED. REPAIRED STIFFENER IAW SRM.SDR SWAA2019071234778Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 3 CRACKED. REPAIRED STIFFENER IAW SRM.SDR SWAA2019071234777Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 2 CRACKED. REPAIRED STIFFENER IAW SRM.
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