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.

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;Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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 53Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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 53-00-5Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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 51-40-05-0GJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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/Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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-; DJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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/WJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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/WJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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' REMAIJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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/WJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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/WJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 Jul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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; RBLJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Main, StructureSDR 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/WJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Main, StructureSDR 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 MAJul 6, 2021 · N941WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR 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 141A6Jul 6, 2021 · N941WN · Boeing 7377H4 · Galley DoorsSDR 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 BEARINGJul 6, 2021 · N941WN · Boeing 7377H4 · Service DoorsSDR 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; STEPSJul 5, 2021 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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/WJul 5, 2021 · N941WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR 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' REMJul 5, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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;Jul 5, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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; [Jul 2, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 DRILJul 2, 2021 · N941WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR 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 FLJul 2, 2021 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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.Dec 31, 2020 · N941WN · Boeing 7377H4 · Fuselage Floor PanelSDR 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.Oct 27, 2020 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020072201661Power Supply · inoperativeAFT RT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.Jul 20, 2020 · N941WN · Boeing 7377H4 · Emergency LightingSDR 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 NOMar 2, 2020 · N941WN · Boeing 7377H4 · Cabin Pressure ControllerSDR SWAA2019072435261Lens · crackedR1 EMERGENCY LIGHT LENS CRACKED. INSTALLED LENS PER AMM.Jul 22, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072235207Battery Pack · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1674. R&R EMERGENCY BATTERY PACK PER AMM.Jul 16, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072235206Battery Pack · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1670. R&R EMERGENCY BATTERY PACK PER AMM.Jul 16, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072235205Fuse · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1675. R&R EMERGENCY FUSE PER AMM.Jul 16, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072235204Power Supply · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1674. R&R EMERGENCY POWER SUPPLY PER AMM.Jul 16, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR SWAA2019072235202Power Supply · failedL1 DOOR OVERHEAD LIGHT FAILED DURING EMERGENCY LIGHT TEST AT POSITION M1670. R&R EMERGENCY POWER SUPPLY PER AMM.Jul 16, 2019 · N941WN · Boeing 7377H4 · Emergency LightingSDR 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.Jul 13, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR 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.Jul 13, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019072335228Rib · crackedLT HORIZONTAL STABILIZER RIB #5 UPPER FORWARD END CRACKED. REPAIRED RIB IAW EA.Jul 8, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019071834944Rib · crackedLT HORIZONTAL STABILIZER RIB 5 LOWER FORWARD END CRACKED. REPAIRED STABILIZER AW SRM.Jul 8, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR 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; 27-81-00-820-803Jul 7, 2019 · N941WN · Boeing 7377H4 · Leading Edge DevicesSDR 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; 27-81-00-820-803Jul 7, 2019 · N941WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2019071634852Attach Angle · crackedRT HORIZONTAL STABILIZER RIB # 4 ATTACH ANGLE CRACKED AT LEADING EDGE WEB ATTACH POINT. R&R STIFFENER ANGLE IAW SRM.Jul 5, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2019071634878Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 34.5" FROM FRONT SPAR. REPAIRED RIB IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019071634851Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 34.4" FROM FRONT SPAR. REPAIRED RIB IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019071634850Rib · crackedLT HORIZONTAL STABILIZER INTERNAL RIB #5 LOWER PART OF STIFFENERS CRACKED 26.5" FROM FRONT SPAR. REPAIRED RIB IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019071234780Stiffener · crackedLT HORIZONTAL STABILIZER RIB #4 (36" AFT OF FRONT SPAR) LOWER PART OF STIFFNER CRACKED. REPAIRED STIFFENER IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2019071234779Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 4 CRACKED. REPAIRED STIFFENER IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2019071234778Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 3 CRACKED. REPAIRED STIFFENER IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2019071234777Stiffener · crackedRT HORIZONTAL STABILIZER RIB #4 (STAB STA 120.30) VERTICAL STIFFENER # 2 CRACKED. REPAIRED STIFFENER IAW SRM.Jul 3, 2019 · N941WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
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