N267WN

Service difficulty reports · 303

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 = 'N267WN' 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 SWAA2026070718223Battery Pack · no test20 ABC EMERGENCY BATTERY PACK AT1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.Jul 3, 2026 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026070718218Battery Pack · no testRT EMERGENCY EXIT EMERGENCY BATTERY. PACK AT 1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06Jul 3, 2026 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026021169123Light · inoperativeFIRST OFFICER`S SIDE EMERGENCY WINDOW LIGHT INOPERATIVE. R & R THE EMERGENCY WINDOW LIGHT . OPS CHECKED GOOD IAW AMM 33-21-00.Feb 9, 2026 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025102025675Seal · missingCAPTAIN L2 WOULD NOT SEAL. AIRPLANE WOULD NOT PRESSURIZE;CABIN CLIMBING AT CLIMB RATE.ON LANDING SMOOTH TOUCHDOWN WITH NO SIDE LOADING ON AIRPLANE.NOSE WHEEL TOUCHED DOWN SMOOTHLY. USED AUTO BRAKES. INSPECTED AND FOUND L2 WINDOW RUBBER TORQUE SEAL MISSING. Oct 18, 2025 · N267WN · Boeing 7377H4 · Flight Compartment WindowsSDR SWAA2025013191498Door · crackedL/H MAIN LANDING GEAR CENTER STRUT DOOR IS CRACKED ON LOWER FWD POCKET .<[01] REMOVED LG L/H CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11 OK TO CONTINUE SERVICE. PER CDL 32-10-3XC AUTHORIZATION # 235084. INSTALLED LT CENTER AND INNER DOOR PER AMM 32-13-11 OJan 31, 2025 · N267WN · Boeing 7377H4 · Landing Gear DoorsSDR SWAA2024092038677Bulb · burned outEMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR HAS BURNED OUT BULBS<[01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR IAW AMM 33-51-01-960-801;[02] VERIFIED CORRECTIVE ACTION STEP 1.Sep 18, 2024 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024092039086Bulb · inoperativeLH ASD EMERGENCY EXIT LIGHT INOP<[01] REPLACED LH SLIDE EMERGENCY LIGHT BULB AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.Sep 18, 2024 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024092038676Wire · disconnectedG-1 GALLEY EMERGENCY LIGHT IS NOT CONNECTED.<[01] DISPLACED G-1 GALLEY FWD SIDE WALL; CONNECTED EMERGENCY LIGHT AND INSTALLED FWD GALLEY SIDE WALL IAW AMM 25-21-35-420-801 AND AMM 25-21-35-020-801;[02] DISPLACED G-1 GALLEY FWD SIDE WALL; CONNECTED EMERGENCY LISep 17, 2024 · N267WN · Boeing 7377H4 · Light System WiringSDR SWAA2024092038546Battery Pack · failedBATTERIES PACKS M1675 AND M1673 FAIL TEST<[01] REPLACED EMERGENCY BATTERIES PACKS M1673 AND M1675 PER AMM 33-51-06-960-805; STEP 4.A THRU 4.E(1-5);[02] VERIFIED ITEM 1.;[03] REPLACED EMERGENCY BATTERIES PACKS M1673 AND M1675 PER AMM 33-51-06-960-805; STEP 4.A Sep 14, 2024 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024091933592Stiffener · crackedDURING NDI HFEC INSPECTION; FOUND LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IS CRACKED; L:0.5' MARKED<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IAW SRM 55-10-09-2R-4.;[02] VERIFIED RII CORRECTIVE ACTION 1.Sep 3, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024091930070Stub Frame · crackedDURING HFEC OPEN HOLES INSPECTION; CRACK NOTED AT HOLE COMMON TO VERTICAL FLANGE OF MOPSILL AND STUB FRAME AT BS294.5; RBL 54; WL208.5<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] VERIFIED STEPS 4;5 COMPLETE.;[03] ACCOMPLISHED REPAIR ON VERTICAL FLANGE OF MOPSILL ANAug 25, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024092027725Web · crackedL/H WEB AT BS 993.50 CRACKED/DAMAGED COMMON TO LAV 'B' O/B MOUNT<[01] REMOVED; REPLACED; AND INSTALLED A NEW L/H WEB AT BS 993.50; LBL33.80; WL208 IAW SRM 51-40-02; BOEING DWG 147A5600 SH 1; AND BOEING DWG 147A0004 SH 64.;[02] UPDATED FAILURE TYPE MEASUREMENTSAug 19, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092325858Seal · crackedRT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW RT SLIDE SEAL AND REMOVED AND REPLACED SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW SRM 51-40-02-0G-0. INSTALLATION OF SLIDE SEAL WILL BE ACCOMPLISHED ON CUST FAULT #TTG8Q00V7MNA;[02] VERIFIED CORRAug 14, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024092325856Spar Web · corrodedCORROSION ON LH WING REAR SPAR WEB AT UPPER END OF CUTOUT FOR #1 FUEL TANK AFT BOOST PUMP<[01] VERIFIED APPLICABILITY OF SRM 57-20-10-1A-3 PER STC ST00830SE;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED CORROSION ON LH WING REAR SPAR WEB AT UPPER END OAug 14, 2024 · N267WN · Boeing 7377H4 · Wing SparSDR SWAA2024092325857Seal · crackedLT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW LT SLIDE SEAL AND REMOVED AND RE-INSTALLED EXISTING SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW SRM 51-40-02-0G-0. INSTALLATION OF SLIDE SEAL WILL BE ACCOMPLISHED ON CUST FAULT #TTG8Q00V7MNA;[02] Aug 14, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024092025854Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED DAMAGED ACB SHIELD FWD OF ACD BS 767-794; RBL 22; WL 156 PER SRM 51-40-02-0G-0 AND INSTALLED NEW ACB FWD SHIELD BS 767-794; RBL 22; WL 15Aug 13, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024091925849Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED DAMAGED L/H FLOOR TO SIDEWALL SUPPORT; LOCATED; DRILLED AND INSTALLED NEW ACB L/H FLOOR TO SIDEWALL SUPPORT PLATE OF PER Aug 13, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024091925850Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVED DAMAGED R/H FLOOR TO SIDEWALL SUPPORT; LOCATED; DRILLED AND INSTALLED NEW ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE OF Aug 13, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092025439Threshold · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED STEPS 5;6 COMPLETE; ALL STEPS AND MEASUREMENT FIELD COMPLETE; CARD COMPLETE.Aug 12, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092324295Floor Support · crackedCRACKED INTERCOSTAL BS 344-360 BL 0 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 344-360 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DOCUMENT NUMBER 141A5400 TYPE: DWG ID:0032 REV:-;[02] VERIFIED CORRECTIVE ACTION #1Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092324299Frame · crackedCRACKED FRAME BS 312 COMMON TO STRINGER 6L.<[01] ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 7L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TTG8Q00V943A;[02] EDIT: ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 6L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024092324296Floor Support · crackedCRACKED INTERCOSTAL BS 312-328 LBL 46 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 312-328 LBL 46 WL 208 PER SRM 51-40-02 COMPLETED MEASURMENT TABLE LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 312-328 LBL 46 WL 208 PER SRM 51-40-05 AND BOEINGAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092324308Skin · debondedRH #8 FLIGHT SPOILER UPPER SURFACE HAS DISBOND 2.9' FROM O/B EDGE AND 8.3' FROM T/E.<[01] REMOVED AND REPLACED RH #8 FLIGHT SPOILER IAW AMM 27-61-11-400-801;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Aug 8, 2024 · N267WN · Boeing 7377H4 · SpoilersSDR SWAA2024092024058Stub Frame · crackedCRACK ON FSD STUB FRAME. LOCATED AT BS 291.5 + 10; .7' ABOVE SEAL DEPRESSOR; .4' IN LENGTH (MARKED) CORRECTION TO FAULT NAME: CRACK FOUND ON FSD STUB FRAME<[01] INSTALLED FWD SERVICE DOOR UPPER STUB FRAME P/N 141A8371-7 I.A.W. SRM 51-40-02-0G0 DWG # 141A8370 RAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024092024300Support Angle · crackedCRACKED SCUFF PLATE SUPPORT ANGLE FWD LOWER CORNER OF FWD ENTRY DOOR CUTOUT BS 309 WL 217.<[01] REMOVED AND REINSTALLED SCUFFPLATE SUPPORT ANGLE FWD LOWER CORNER OF FWD ENTRY DOOR CUOUT BS 309 WL 217 IAW SRM 51-00-10-0G-0 AND BOEING DOCUMENT NUMBER 141A8230 TEAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092024303Intercostal · crackedCRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL @ BS 277-294 RBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL @ BS 277-294 RBL 1 WL 208 PER DWG: 141A5400 REV: - ID: 0020 AND INSTALLED INTERCOSTAL @ BS 277-294 Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092024304Intercostal · crackedCRACKED INTERCOSTAL BS 328-344 LBL 46 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AT BS 328 TO 344 LBL 46 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1. OK TO INSTALL GIVEN.;Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092024305Intercostal · crackedCRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] ALL STEPS COMPLETED REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE LOCATED AND DRILLED NEW INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-05 AND BOEING DWAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092024297Intercostal · crackedCRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL TO BS 380-400 LBL 1 WL 208 PER DWG: 143A5400 ID: 0038 REV: A AND SRM 51-40-02 AND INSTALLED NEW INTERAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024092024307Intercostal · crackedCRACKED INTERCOSTAL BS 380-400 RBL 39 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 380-400 RBL 39 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE. LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 380-400 RBL 39 WL 208 PER SRM 51-40-05 AND BOEIAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024091924301Angle · crackedCRACKED ANGLE BS 294.5 FWD SIDE OF FRAME RBL 54 WL 208.<[01] STUB FRAME OF THE FORWARD GALLEY DOOR SURROUND STRUCTURE AT STA 296.4 REPAIR IS ACCOMPLISHED ON CUSTOMER CARD #TTG8Q00VFMWA;[02] VERIFIED CORRECTIVE ACTION #1Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024091924306Floor Support · crackedCRACKED INTERCOSTAL BS 380-400 RBL 8 WL 208.<[01] ALL STEPS COMPLETED REMOVE INTERCOSTAL BS 380-400 RBL 8 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE. LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 380-400 RBL 8 WL 208 PER SRM 51-40-05 AND BOEING DAug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024091923881Stiffener · crackedLEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 ARE CRACKED IN THE LOWER RADIUS.<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 IAW SRM 55-10-09-2R-4.;[02] VERIFIED CORRECTIVE ACTION 1.Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024091924049Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .3' IN LENGTH (MARKED CORRECTION TO FAULT NAME. 26.5' FROM FWD EDGE<[01] REPAIRED PER SRM 55-10-01-2R-11;[02] VERIFIED CORRECTIVE ACTION #1Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024091924052Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .65' IN LENGTH (MARKED)<[01] REPAIR AS PER SRM 55-10-01-2R-11.;[02] VERIFIED CORRECTIVE ACTION #1Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024091923837Bearing · out of limitsDURING ACCOMPLISHMENT OF CUSTOMER CARD 5510-I-16685-NG (INSP-STABILIZERS-HORIZONTAL STABILIZER SPHERICAL BEARING) FOUND DIMENSION H TO BE .0825 AND OUT OF LIMITS<[01] REMOVED AND REPLACED L/H AND R/H HORIZONTAL STAB CENTER SECTION HINGE HOUSING SPHERICAL BEARIAug 7, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024091923855Support · crackedUPPER BULB SEAL RETAINER SUPPORT IS CRACKED AT LOWER FASTENER HOLE AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED AND REPLACED UPPER BULB SEAL RETAINER SUPPORT AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON<BR>I.A.W SRM 51-40-02.<BAug 7, 2024 · N267WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024091923365Vapor Barrier · crackedR/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1Aug 6, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024091923366Vapor Barrier · crackedL/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1Aug 6, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024092322980Support · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL TRANSVERSE SUPPORT IAW SRM 51-40-02-0G-0Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2024092322984Support Fitting · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL MID SUPPORT BEAM AFT END FITTING IAW SRM 51-40-02-0G-0Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2024092322981Beam · crackedRH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 IAW SRM 51-40-02 AND AMM 20-50-11-910-801.;[02] CAL Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2024092322986Bracket · crackedRH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET FWD FACE HAS CRACK.<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET IAW SRM 51-40-02 AND AIPC 57-42-51-03.;[02] Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2023092501958Escape Rope · out of positionRIGHT OVERWING EXIT ESCAPE ROPE IS NOT STOWED PROPERLY.<[01] RESECURED RIGHT OVERWING EXIT ESCAPE ROPE PER SIPSep 19, 2023 · N267WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023091801555Light · inoperativeAFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHK GOODSep 16, 2023 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023091398812Light · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF THE REAR ENTRY DOOR INOP<[01] INSTALLED NEW LAMP FOR EXTERIOR EMERGENCY LIGHT AFT OF REAR ENTRY DOOR IAW AMM 33-51-04Sep 11, 2023 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023022105186Handle · brokenFORWARD ENTRY DOOR ASSIST HANDLE BROKEN. FWD LAV ASSIST HANDLE MISSING.<[01] SWAPPED FWD ENTRY HANDLE WITH FWD LAV IAW AMM 52-11-31. INSTALLED FWD LAV ASSIST HANDLE PER CMM 25-42-76.Feb 20, 2023 · N267WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023012594013Lens · missingEMERGENCY EXIT SIGN AT RIGHT OVER WING EXIT DOOR MISSING LENS. INSTALLED NEW LENS AS PER M/M SIP.Jan 22, 2023 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022121481219Bulb · inoperativeFORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AFT BULB IS INOP<[01] REPLACED INOP LAMP IN FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIEDDec 13, 2022 · N267WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022121478970Window Frame · crackedCAPTAIN'S #3 WINDOW FRAME HAS A CRACK EMINATING FROM THE LWR FASTENER HOLE ON THE FWD VERTICAL FASTENER ROW.<[01] REQUEST NDI VERIFICATION OF CRACK;[27] REPAIRED PER SWA EA 22-153-03613.Dec 6, 2022 · N267WN · Boeing 7377H4 · Fuselage Main, Structure
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