N268WN

Service difficulty reports · 262

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 = 'N268WN' 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 SWAA2026092274966Cover · missingAISLE OVERHEAD EXIT SIGN MISSING FORWARD FACING COVER. REPLACED AISLE FRONT FACING OVERHEAD EXIT SIGN COVER REF AMM 33-51-01-960-802. OPS CHECKS NORMAL.Sep 18, 2026 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026090870845Cover · missingEMERGENCY LIGHT ROW 14 & 15 A,B & C, COVER MISSING. INSTALLED MISSING COVER IAW AMM 33-51-03.Sep 3, 2026 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026081423387Lens · detachedEMERGENCY EXIT SIGN OVERHEAD IN CABIN FELL DOWN REINSTALLED LENS COVER REF AMM 33-51-00.Aug 10, 2026 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026080575007Floor Panel · crackedFWD CARGO FLOOR PANEL CRACKED (6 , 5.5 2 SPOT) BS 500. PERFORMED A PATCH REPAIR IAW AMM 25-52-01. NO OTHER LINER AND PANEL DAMAGE NOTED.Aug 1, 2026 · N268WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026060208207Floor Panel · splitRAMP REPORTS AFT CARGO PIT FIBERGLASS FLOOR SPLIT. SPLIT IS IN FIBERGLASS FLOOR FROM STATION 751-768. OK TO CONT PER MEL 25-16-01. REMOVED AND REPLACED AFT CARGO FLOOR PANEL PER AMM 25-52-10.May 31, 2026 · N268WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026022372823Cover · looseEMERGENCY EXIT LIGHT COVER ON F/O SIDE OVERWING EXIT FELL OFF DURING FLIGHT. SECURED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-01.Feb 21, 2026 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025082909134Light · looseRH PHOTO LUMINESCENT STRIP LOOSE AT FWD GALLEY MAT. SECURED RT PHOTOLUMINESCENT STRIP AT FWD GALLEY BALL MAT IN REF TO AMM 33-51-15.Aug 28, 2025 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025080697913Battery Pack · inoperativeFOUND FRONT LEFT EMERGENCY LIGHTS OUT. R & R FWD LT BATTERY PACK PER AMM 33-51-06 OPS GOOD.Aug 3, 2025 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2025070186477Fairing · damagedSTRUT 4 FAIRING HAS AN ENLARGED MOUNT HOLE ON TOP AFT SIDE<[01] C/W 25-172-01732Jun 28, 2025 · N268WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2024103054003Connector · damagedINOP EMERGENCY EXIT LIGHT ON CEILING PANEL AT FWD GALLEY AREA 2024-593383<[01] CONNECTED CORRECTLY ELECTRICAL CONNECTOR D3160 OF THE EMERGENCY LIGHT ON CEILING PANEL AT FORWARD GALLEY AREA IAW B737-700 WDM 33-51-12-2 AND PERFORMED EMERGENCY LIGHTS OPERATIONAL Oct 27, 2024 · N268WN · Boeing 7377H4 · Light System WiringSDR SWAA2024103045313Web · crackedCRACK ON LOWER SILL WEB LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA 2024-593316<[01] REPLACED LOWER SILL WEB (1EA) LOCATED BTW BS 291.5 TO BS 332.1 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET: 25 REV: DWG 140A9810 SHOct 5, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103042819Support Angle · crackedCRACK BODY FAIRING SUPPORT T ANGLE LOCATED BS500D; BETWEEN STRINGER 18R AND STRINGER 19R AT LOWER FUSELAGE 2024-593247<[01] REPLACED SUPPORT T ANGLE LOCATED AT BS500D; BETWEEN STRINGER 18R AND STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG 14Sep 28, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103042817Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN 2024-593237<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A.;[02] REPLACED SUPPORT BRACKET LOSep 27, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041983Lens · brokenBROKEN LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA 2024-593195<[01] REPLACED LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3. C. (6) (A) THRU 3. C. (6) (E);[02] REPLACED LENS EMERGENCY EXIT ON LAVATORY A ASep 26, 2024 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024103041726Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING 2024-593185<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFISep 25, 2024 · N268WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024103041725Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT RT WING 2024-593183<[01] REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED ORSS 269 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9;DWG 115A2930 SHEET 8 REV-;;[02] REPLACED ANGLE AND FASTENERS TRAILING EDSep 25, 2024 · N268WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024103041527Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593167<[01] TOOL USED IN STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600Sep 25, 2024 · N268WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024103041229Web · crackedCRACK ON WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-593135<[01] REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV ?<BR>SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041519Angle · crackedCRACK ANGLE AFT POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-593151<[01] REPLACED ANGLE LOCATED AFT POSITION BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-0Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041230Web · crackedCRACK ON WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2024-593132<[01] REPLACED WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV ?<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACESep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041226Plate · corrodedCORROSION ON PLATE LOCATED BS 1006 PLUS 23 INCHES RBL 3 WL 208.1 AT AFT GALLEY AREA 2024-593121<[01] TOOL USED CALIPER P/N: 500-752-20; S/N:B12037208; DUE DATE: 17-APR-25.;[02] REPLACED PLATE AND FASTENERS LOCATED BS 1006 TO BS 1040 RBL 3 WL 208.1 AT AFT GALLESep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041512Fitting · corrodedCORROSION INNER CHORD LOCATED BTW BS 303.9 TO BS 328 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593138<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG SN 130061901; DUE DATE. 12-JUN-25;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BTW BS 303.9 TO BS 360 LBL 54 WL Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041520Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-593152<[01] TRIM OUT BS 312 FRAME UPPER CHORD AT LBL 33 BETWEEN S-5L AND S-6L IAW EA# M-22-153-01244 [TTG8Q00W585E] SEE INDIVIDUAL SIGN OFF BELOW.;[02] TRIM OUT BS 312 FRAME UPPER CHORDSep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024103041522Angle · crackedCRACK ON ANGLE LOCATED FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GALLEY 2024-593153<[01] REPLACED ANGLE LOCATED ON FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GALLEY IAW B737-700 SRM 51-10-02 51-40-02 AND DRAWING 141A1311 SHEET 1 REV C MATERIAL USED BAC 1489-360Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041513Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-593140<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041515Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-593142<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041516Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-593144<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041517Plate · corrodedCORROSION ON PLATE LOCATED BS 312 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593146<[01] REPLACED PLATE LOCATED BS312 LBL54 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 DUE NOT FOUND AN ALLOWABLE DAMAGE APPLICABLE TO THIS PART IN B737-700 SRM 53-30-51-1ASep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041526Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593165<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; SSep 24, 2024 · N268WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024103041514Support · crackedCRACK SUPPORT ZEE LOCATED BTW STA 727D TO STA 727E AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-593141<[01] REPLACED SUPPORT ZEE SECTION;AND FASTENERS LOCATED ON BS 727B PLUS 10 INCH AND BS 767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103041511Stub Frame · crackedCRACK ON STUB FRAME LOCATED 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-593136<[01] STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 05-AUG-25;[02] PERFORMED PERMANENT REPAIR ON STUB FRAME LOCATED 294.5 AT LEVELSep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024103041521Stringer · crackedCRACK ON STRINGER 16L LOCATED BTW BS 294.5 TO BS 303.9 AT FWD GALLEY AREA 2024-593150<[01] ON STEP 3; TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130064101; DUE DATE: 13/DEC/24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631Sep 24, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024103040716Web · crackedCRACK SUPPORT WEB LOCATED BTW STA 847 TO STR 867 AT LEVEL LBL 24.82 CEILING AREA AT AFT CARGO COMPARTMENT 2024-593041<[01] REPLACED SUPPORT WEB AND FASTENERS LOCATED BTW STA 847 TO STA 867 AT LEVEL LBL 24.82 CEILING AREA AT AFT CARGO COMPARTMENT IAW B737-700 SSep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103040953Connector · brokenBROKEN CONNECTOR OF THE OVERWING SCAPE LOCATED BTW STA 747 TO STA 767 AND BTW STR 21L TO STR 22L AT AFT CARGO COMPARTMENT 2024-593054<[01] REPLACED CONNECTOR OF THE OVERWING SCAPE LOCATED BTW STA 747 TO STA 767 AND BTW STR 21L TO STR 22L AT AFT CARGO COMPARTMESep 23, 2024 · N268WN · Boeing 7377H4 · Equipment/Furnishings WiringSDR SWAA2024103040962Web · crackedCRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2024-593092<[01] REPLACED WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV ?<BR>SEE INDIVIDUAL SING OFF BELOW;[02] CERSep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103040721Angle · crackedCRACK ANGLE LOCATED STA 927 AT LEVEL STR 18R AT AFT CARGO COMPARTMENT 2024-593042<[01] REPAIRED ANGLE LOCATED BTW STA 900 TO STA 927 AT LEVEL STR 18R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0 FIG 201;SHEET 2 .SEE INDIVIDUAL SIGN OFF BELOW;[02] CESep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103040954Floorbeam · corrodedCORROSION LOCATED ON FLOOR BEAM 986.5 RBL 42 WL 208.1 AT AFT GALLEY AREA 2024-593056<[01] PERFORMED PERMANENT REPAIR CAT A LOCATED ON FLOOR BEAM 986.5; LBL13 TO RBL50 WL 208.1 AT AFT GALLEY AREA. I.A.W. B737-700 SRM 53-70-51-2R-4 REPAIR 4 AND 24-153-02746-WIP2Sep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024103040955Floorbeam · corrodedCORROSION LOCATED ON FLOOR BEAM 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2024_593057<[01] ET TOOL USED PN: MIZ-21C; SN:769680; DUE DATE: 28-AUG-25;[02] TOOL USED ON STEP 12:ET EQUIPMENT; P/N: NORTEC 600D; S/N:210138003; DUE DATE: 11/JUN/25;[03] PERFORMED PERMASep 23, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024103040189Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-592934<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23272676;DUE DATE:17-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1998072 ; DUE DATE : 23/JAN/25;[03] REPAIRED BY WELDISep 22, 2024 · N268WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024103040179Strip · crackedCRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (8 EA) 2024-592911<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (8 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FSep 21, 2024 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024103040180Light · crackedCRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (8 EA) 2024-592912<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (8 EA) IAW B737-700 AMM-33-51-15-400-802-NG;[02] REPLACED STRIP PHOTOLUMINESCENSep 21, 2024 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024103040169Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT RH WING LOWER SURFACE 2024-592880<[01] TOOL USED CALIPER PN: 500-196-30; SN: A193117217; DUE DATE: 16/MAY/25.;[02] TOOL USED ON ITEM 2: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 2010361Sep 21, 2024 · N268WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024103039504Skin · crackedCRACK SLAT 2 LOWER SKIN AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71 AT LT WING 2024-592769<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25.;[02] REPLACED L/E SLAT 2 LT WING Sep 19, 2024 · N268WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2024103039505Vapor Barrier · crackedCUSTOMER REQUEST CRACK VAPOR BARRIER LH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENTS 2024-592759<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189443; DUE DATE: 06-MAR-25;[02] TOOL USED SCALE P/N SPX222 S/N C410738991 DUE DATE 05/AUG/25;[03] HOT BONDER P/N: HCSep 19, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024103039503Vapor Barrier · crackedCUSTOMER REQUEST CRACK VAPOR BARRIER RH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENT 2024-592758<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18229508; DUE DATE: 14-JAN-25.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18196126 DUE DATE:03-APR-25;[03] TOOL USEDSep 19, 2024 · N268WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024060397128Tire · blown#2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11May 31, 2024 · N268WN · Boeing 7377H4 · TireSDR SWAA2024060397804Tire · blown#2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11May 31, 2024 · N268WN · Boeing 7377H4 · TireSDR SWAA2024020247465Wire · brokenLOWER LEFT EMERGENCY LIGHT ON FWD LAV INOP<[01] FOUND BROKEN WIRE ON FOR EMERGENCY LIGHT ASSY. REPAIRED WIRE IAW SWPM 20-30-12. OPS CHECK GOOD AT THIS TIME.Feb 1, 2024 · N268WN · Boeing 7377H4 · Light System WiringSDR SWAA2024013046004Cover · detachedOVER WING EXIT SIGN COVER KNOCKED OFF FWD SIDE<[01] RESECURED EMERGENCY EXIT SIGN COVER AS REQUIRED PER SIPJan 28, 2024 · N268WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023110919384Battery Pack · failedEMX BATT PACK M01670 FAILS CAPACITANCE CHECK / [01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06Nov 8, 2023 · N268WN · Boeing 7377H4 · Emergency Lighting
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