N269WN

Service difficulty reports · 267

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 = 'N269WN' 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 SWAA2026092132599Battery Pack · no testRIGHT FWD EMERGENCY LIGHT SYS BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.Sep 15, 2026 · N269WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026052606114Battery · inoperativeFLIGHT ATTENDANT MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE BATTERIES IAW AMM 25-64-00.May 23, 2026 · N269WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026011961493Battery Pack · no testBATTERY AT M1669 FAILED TIME CHECK. R & R THE BATTERY PACK AT M166 IAW AMM 33-51-06.Jan 15, 2026 · N269WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026011961484Panel · pulledFOUR FASTENERS PULLED THROUGH LOWER WING PANEL OTBD OF NR 3 FLAP TRACK FAIRING ON LT WING. REMOVED AND REPLACED FASTENERS ON LOWER WING PANEL O/B #3 FLAP TRACK FAIRING ON LEFT WING PER SRM 51-40-02.Jan 15, 2026 · N269WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2025041423542Isolator · crackedFWD GALLEY DOOR AFT UPPER SLIDE MOUNT ISOLATOR CRACKED<[01] R&R FWD GALLEY DOOR AFT UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.;[02] C/WApr 11, 2025 · N269WN · Boeing 7377H4 · Escape SlideSDR SWAA2025041423562Isolator · crackedAFT ENTRY DOOR AFT UPPER SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR AFT UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.;[02] C/WApr 11, 2025 · N269WN · Boeing 7377H4 · Escape SlideSDR SWAA2025041423561Screw · wornFWD SER DOOR HAS SEVERAL WORN SCREWS AND WORN SLIDE ATTACH HARDWARE BOLTS<[01] REPLACED WORN SCREWS AND HARDWARE BOLTS IAW AMM 52-41-00.;[02] C/WApr 11, 2025 · N269WN · Boeing 7377H4 · Service DoorsSDR SWAA2024120657274Angle · crackedCRACK ON ANGLE LOCATED AT LEVEL STR 8L AND BS 312 AT FWD GALLEY AREA 2024-633958<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] REPLNov 6, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024120655811Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB AREA LT WING 2024-633747<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB AREA LT WING.IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.TOOL USED .DIGITAL CALIPER P/N:500-19Nov 2, 2024 · N269WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024120551490Rib · crackedCRACK INSPAR RIB 120.30 LOCATED 27 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633926<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 LOCATOct 22, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2024120551162Web · crackedCRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-633925<[01] REPLACED HORIZONTAL WEB LOC. BS 294.5 TO BS 332.1 AT LEVEL STR 17R FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:141A8310 Oct 20, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024120671992Angle · crackedCRACK ON ANGLE OUTBOARD THRUST REVERSER LOCATED AFT UPPER POSITION ON ENGINE 1 2024-633879<[01] REPLACED ANGLE OUTBOARD THRUST REVERSER LOCATED AFT UPPER POSITION ON ENGINE 1 I.A.W B737-700 CMM 78-31-40; SRM 51-10-02 ITEM 9 AND SRM 51-40-02 TOOK MEASURES OF CROct 17, 2024 · N269WN · Boeing 7377H4 · Engine Thrust ReverserSDR SWAA2024120648420Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 217 RT WING 2024-633807<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 217 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2001; SHEET 45; REV - . TOOL USOct 14, 2024 · N269WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024120648421Angle · crackedCRACK ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING 2024-633808<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 115A2710<BR>REV A.;[02] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT Oct 14, 2024 · N269WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024120648419Angle · crackedCRACK ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING 2024-633809<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710; SHEET 8; REV A . TOOL USED Oct 14, 2024 · N269WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024120548422Panel · corrodedCORROSION BULKHEAD PANEL 121HW AT FWD CARGO COMPARTMENT 2024-633814<[01] REPLACED LOWER STRUCTURAL SECTION AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 153A1510 REV:H<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED LOWER STRUCTURAOct 14, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120548423Bear Strap · crackedCRACK ON BEAR STRAP LOCATED BTW BS 303.9 TO BS 312 AND BTW STR 7L TO STR 8L AT FWD GALLEY AREA 2024-633815<PERFORMED REPAIR ON BEAR STRAP FWD ENTRY DOOR BTW BS 294.5 TO BS 348 AND BTW STR 4L TO STR 16L IAW EA 24-153-03017-WIP1 [TTG8Q00WSTE9]; EA 24-153-03017-WOct 14, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024120648207Support Angle · crackedCRACK SUPPORT ANGLE I/B AUXILIARY TRACK OF SLAT 1 AT LT WING 2024-633791<[01] REPLACED SUPPORT ANGLE I.A.W B737-700 SRM 51-10-02 ITEM 9 DWG 114A5010-11 SHEET 14 REV C LOC. ON I/B AUXILIARY TRACK OF SLAT 1 AT LT WING DUE TO CRACK IS NOT PERMITTED ALLOWABLE DAMAOct 13, 2024 · N269WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2024120648069Support Angle · crackedCRACK SUPPORT ANGLE ON I/B AUXILIARY TRACK OF SLAT 8 AT RT WING 2024-633786<[01] REPLACED SUPPORT ANGLE ON I/B AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND STM 51-10-02-0G-0 ITEM 9;[02] CORRECTED STEP 1:<BR>REPLACED SUPPORT ANGLE ON Oct 13, 2024 · N269WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2024120548074Track · crackedCRACK TRACK LBBL 17.24 LOCATED BS767 AFT CARGO COMPARTMENT 2024-633782<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 200048001; CAL DUE DATE: 28-MAY-25;[02] REPAIRED CARGO TRACK LOC. BTW BS 747+11? TO BS 787-10.5? AND LBL 17.24 IAW B737-700 SRM 53-00-53-Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120548075Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2024-633785 CRACK SUPPORT ANGLE LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT<[01] TOOL USED: CALIPER P/N: 500-196-30;Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120548071Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS 727E AFT CARGO COMPARTMENT 2024-633781<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00WDYKT<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1 <BR>REPAIRED CARGO TRACK LOC. BTW BS727E-9 INCH TO BS767+13 INCH ; AT RBL 13.8Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120548073Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS 767 AFT CARGO COMPARTMENT 2024-633778<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 200048001; CAL DUE DATE: 28-MAY-25;[02] REPAIRED CARGO TRACK LOC. BTW BS727E-9 INCH TO BS767+13 INCH ; AT RBL 13.84 AT AFT CARGO COMPARTOct 13, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120548072Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS 747 AFT CARGO COMPARTMENT 2024-633780<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00WDYKT<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPAIRED CARGO TRACK LOC. BTW BS727E-9 INCH TO BS767+13 INCH ; AT RBL 13.8Oct 13, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024120647719Support Angle · crackedCRACK SUPPORT ANGLE DODY FAIRING BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE 2024-633745<[01] REPLACED SUPPORT ANGLE LOCATED BODY FAIRING BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE IAW B737-700 SRM 51-40-05; SRM 51-10-02 Ï¿½TEM 9 AND DWG #: 116A3010; SHEET:Oct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024120647624Skin Panel · 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. 2024-633682<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: 220272712; DUE DATEOct 12, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024120647625Skin Panel · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-633684<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200048001;Oct 12, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024120547909Support Angle · crackedCRACK SUPPORT ANGLE BS 695 AND BL0 RT SIDE AT CENTER SECTION 2024-633756<[01] REJECTION ELONGATED HOLE BRACKET BS 695 AND BL0 RT SIDE AT CENTER SECTION PAX CABIN AT CENTER WING BOX SEE TTG8Q00WEJFU;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N Oct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2024120547718Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-633743<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 146A7901 SHEET 19 REV.?;[02] TASK COMPLETEDOct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024120647622Rib · crackedCRACK INSPAR RIB 120.30 LOCATED 10 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633675<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 60Oct 11, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024120647620Rib · crackedCRACK INSPAR RIB 120.30 LOCATED 18 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633677<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 60Oct 11, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024120547510Web · corrodedCORROSION WEB FLOOR STRUCTURE LOCATED BS1016 AND LBL1 WL208.1 AT AFT GALLEY AREA CORROSION WEB FLOOR STRUCTURE LOCATED BS1016 AND LBL1 WL208.1 AT AFT GALLEY AREA 2024-633654<[01] REPLACED WEB FLOOR STRUCTURE LOCATED BS1016 AND LBL1 WL208.1 AT AFT GALLEY AREA IOct 11, 2024 · N269WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2024120547508Floorbeam · crackedCRACK FLOOR BEAM LOCATED BS328 AND RLB24 AT FWD GALLEY AREA 2024-633648<[01] ON STEP 6: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 14 APR 25;[02] FOR STEP 11 TOOL USED PN: XRP-3000; SERIAL: 1998072; DUE DATE: 23-JAN-25.;[Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024120547511Strap · corrodedCORROSION STRAP FLOOR STRUCTURE LOCATED BS1016 AND RBL3 AT AFT GALLEY AREA 2024-633655<[01] REPLACED STRAP FLOOR STRUCTURE LOCATED BS1006 TO BS1028 AND RBL3 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024120547512Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED STA986.5 AND RBL42 WL208.1 AT AFT GALLEY AREA 2024-633658<[01] ON STEP 7: TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 500D; SN: N500X12101V022237; DUE DATE: 28 FEB 25.;[02] ON STEP 9 AND 10; TOOL USED P/N: NORTEC 500D; S/N: N500X121Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024120547513Strap · corrodedCORROSION STRAP FLOOR STRUCTURE LOCATED STA1016 TO STA1040 AND LBL3 WL208.1 AT AFT GALLEY AREA 2024-633657<[01] REPLACED STRAP AND FASTENERS FLOOR STRUCTURE LOCATED STA1016 TO STA1040 AND LBL3 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024120647162Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2024-633618<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING I.A.W B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9.<BR>TOOK MEASURES OF CRACK: Oct 10, 2024 · N269WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024120547164Angle · crackedCRACK ANGLE LOCATED BETWEEN BS727C TO BS727D AND LBL52 CEILING AREA AFT CARGO COMPARTMENT 2024-633632<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] PERFORMED PERMANENT REPAIR ON ANGLE LOCATED BETWEEN BS727C TO BSOct 10, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120547165Web · crackedCRACK WEB LOCATED BETWEEN STA847 TO STA867 AND LBL20 CEILING AREA AT AFT CARGO COMPARTMENT 2024-633631<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN STA847 TO STA867 AND LBL20 CEILING AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02 AND DOct 10, 2024 · N269WN · Boeing 7377H4 · Cargo CompartmentsSDR SWAA2024120547151Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE LT AT AFT GALLEY AREA 2024-633594<[01] REPLACED GIRT BAR FITTING HARDWARE LT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(G) THRU 3.D.(J) THE INSTALLATION IS DOCUMENTED ON TASK CARD TTG8Q0025SZE.;[02] REOct 10, 2024 · N269WN · Boeing 7377H4 · Escape SlideSDR SWAA2024120547146Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE RT AT AFT GALLEY AREA 2024-633595<[01] REPLACED GIRT BAR FITTING HARDWARE RT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(G) THRU 3.D.(J) THE INSTALLATION IS DOCUMENTED ON TASK CARD TTG8Q0025SZE.;[02] REOct 10, 2024 · N269WN · Boeing 7377H4 · Escape SlideSDR SWAA2024120546902Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE WEB UPPER SURFACE BTW STA 663 TO STA 675; AT LEVEL LBL 30. CRACK LENGTH = 0.250 INCHES APPROX. 2024-633590<[01] TOOL USED IN STEP 5 AND 6: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631 DUE DATE: 11-MAR-Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2024120547324Stub Frame · crackedCRACK STUB FRAME ON BS 294.5 AT LEVEL STR17R AT FWD GALLEY AREA 2024-633637<[01] STEP 4. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 210138003 AND DUE DATE: 11-JUN-25.;[02] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DUEOct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024120547328Intercostal · corrodedCORROSION WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA294.5 TO STA312 AND LBL12 WL208.1 AT FWD GALLEY AREA 2024-633641<[01] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN STA294.5 TO STA312 AND LBL12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRMOct 10, 2024 · N269WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2024120546906Vapor Barrier · crackedCRACK INDICATION FOUND ON VAPOR BARRIER LOCATED BS 663 AND BTW. RBL 40 TO RBL 43 CRACK LENGTH IS 6 INCH 2024-633591<[01] TOOL USED: SCALE P/N CR5200 S/N 8343110875 DUE DATE: 28/FEB/25;[02] TOOL USED HOT BONDER P/N: HCS9200B S/N:15102320 DUE DATE:25/JAN/25;[03]Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2024120547327Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL30 FWD GALLEY AND LAV 2024-633640<[01] REPLACED INTERCOSTAL WEB LOCATED BETWEEN STA 312 TO STA 328 AND RBL 30 FWD GALLEY AREA IAW B737 SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9 AND DOct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024120547323Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2024-633633<[01] REPLACED TIE CLIP AND FASTENERS LOC. BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV - AND DWG 141A8380 SHEET 21 REV -.Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024120547325Frame · crackedCRACK FRAME LOCATED STA312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN 2024-633636<[01] REPAIRED FRAME LOCATED STA 312 BTW STR5L TO STR6L FWD GALLEY AREA IAW EA NO M-22-153-01244 REV B . SEE INDIVIDUAL SIGN-OFFS BELOW;[02] JOB COMPLETEDOct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024120547326Stringer · crackedCRACK STRINGER 16L LOCATED STA294.5 AT PASSENGER CABIN 2024-633634<[01] ON STEP 6; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 190023010; DUE DATE: 05-AUG-25;[02] PERFORMED PERMANENT REPAIR ON STRINGER 16L LOCATED BTW STA277 AND STA 294.5 AT FWD GAOct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024120546898Support Angle · crackedCRACK SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION 2024-633566<[01] REPLACED SUPPORT ANGLE LOCATED STA695 BL0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 273A9110 SHEET: 6 REV: A.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGOct 9, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame
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