# Service difficulty reports: N269WN A list on [N269WN](https://openairdocs.org/aircraft/N269WN.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 267 reports - [SDR SWAA2026092132599](https://openairdocs.org/sdr/SWAA2026092132599.md): Battery Pack · no test · Sep 15, 2026 · N269WN · Boeing 7377H4 · Emergency Lighting > RIGHT FWD EMERGENCY LIGHT SYS BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. - [SDR SWAA2026052606114](https://openairdocs.org/sdr/SWAA2026052606114.md): Battery · inoperative · May 23, 2026 · N269WN · Boeing 7377H4 · Emergency Equipment > FLIGHT ATTENDANT MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE BATTERIES IAW AMM 25-64-00. - [SDR SWAA2026011961493](https://openairdocs.org/sdr/SWAA2026011961493.md): Battery Pack · no test · Jan 15, 2026 · N269WN · Boeing 7377H4 · Emergency Lighting > BATTERY AT M1669 FAILED TIME CHECK. R & R THE BATTERY PACK AT M166 IAW AMM 33-51-06. - [SDR SWAA2026011961484](https://openairdocs.org/sdr/SWAA2026011961484.md): Panel · pulled · Jan 15, 2026 · N269WN · Boeing 7377H4 · Wing, Plate/Skin > FOUR 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. - [SDR SWAA2025041423542](https://openairdocs.org/sdr/SWAA2025041423542.md): Isolator · cracked · Apr 11, 2025 · N269WN · Boeing 7377H4 · Escape Slide > FWD 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/W - [SDR SWAA2025041423562](https://openairdocs.org/sdr/SWAA2025041423562.md): Isolator · cracked · Apr 11, 2025 · N269WN · Boeing 7377H4 · Escape Slide > AFT 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/W - [SDR SWAA2025041423561](https://openairdocs.org/sdr/SWAA2025041423561.md): Screw · worn · Apr 11, 2025 · N269WN · Boeing 7377H4 · Service Doors > FWD 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/W - [SDR SWAA2024120657274](https://openairdocs.org/sdr/SWAA2024120657274.md): Angle · cracked · Nov 6, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK 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] REPL - [SDR SWAA2024120655811](https://openairdocs.org/sdr/SWAA2024120655811.md): Angle · cracked · Nov 2, 2024 · N269WN · Boeing 7377H4 · Trailing Edge Flaps > CRACK 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:500-19 - [SDR SWAA2024120551490](https://openairdocs.org/sdr/SWAA2024120551490.md): Rib · cracked · Oct 22, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACK 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 LOCAT - [SDR SWAA2024120551162](https://openairdocs.org/sdr/SWAA2024120551162.md): Web · cracked · Oct 20, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK 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 - [SDR SWAA2024120671992](https://openairdocs.org/sdr/SWAA2024120671992.md): Angle · cracked · Oct 17, 2024 · N269WN · Boeing 7377H4 · Engine Thrust Reverser > CRACK 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 CR - [SDR SWAA2024120648420](https://openairdocs.org/sdr/SWAA2024120648420.md): Plate · cracked · Oct 14, 2024 · N269WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACK 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 US - [SDR SWAA2024120648421](https://openairdocs.org/sdr/SWAA2024120648421.md): Angle · cracked · Oct 14, 2024 · N269WN · Boeing 7377H4 · Trailing Edge Flaps > CRACK 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
REV A.;[02] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT - [SDR SWAA2024120648419](https://openairdocs.org/sdr/SWAA2024120648419.md): Angle · cracked · Oct 14, 2024 · N269WN · Boeing 7377H4 · Trailing Edge Flaps > CRACK 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 - [SDR SWAA2024120548422](https://openairdocs.org/sdr/SWAA2024120548422.md): Panel · corroded · Oct 14, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CORROSION 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
SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED
REPLACED LOWER STRUCTURA - [SDR SWAA2024120548423](https://openairdocs.org/sdr/SWAA2024120548423.md): Bear Strap · cracked · Oct 14, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK ON BEAR STRAP LOCATED BTW BS 303.9 TO BS 312 AND BTW STR 7L TO STR 8L AT FWD GALLEY AREA 2024-633815 CRACK 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 DAMA - [SDR SWAA2024120648069](https://openairdocs.org/sdr/SWAA2024120648069.md): Support Angle · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Leading Edge Devices > CRACK 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:
REPLACED SUPPORT ANGLE ON - [SDR SWAA2024120548074](https://openairdocs.org/sdr/SWAA2024120548074.md): Track · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK 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- - [SDR SWAA2024120548075](https://openairdocs.org/sdr/SWAA2024120548075.md): Support Angle · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK 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; - [SDR SWAA2024120548071](https://openairdocs.org/sdr/SWAA2024120548071.md): Track · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK TRACK RBBL 13.84 LOCATED BS 727E AFT CARGO COMPARTMENT 2024-633781<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00WDYKT
SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1
REPAIRED CARGO TRACK LOC. BTW BS727E-9 INCH TO BS767+13 INCH; AT RBL 13.8 - [SDR SWAA2024120548073](https://openairdocs.org/sdr/SWAA2024120548073.md): Track · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK 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 COMPART - [SDR SWAA2024120548072](https://openairdocs.org/sdr/SWAA2024120548072.md): Track · cracked · Oct 13, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK TRACK RBBL 13.84 LOCATED BS 747 AFT CARGO COMPARTMENT 2024-633780<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00WDYKT
SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1
REPAIRED CARGO TRACK LOC. BTW BS727E-9 INCH TO BS767+13 INCH; AT RBL 13.8 - [SDR SWAA2024120647719](https://openairdocs.org/sdr/SWAA2024120647719.md): Support Angle · cracked · Oct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK 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: - [SDR SWAA2024120647624](https://openairdocs.org/sdr/SWAA2024120647624.md): Skin Panel · cracked · Oct 12, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK 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 DATE - [SDR SWAA2024120647625](https://openairdocs.org/sdr/SWAA2024120647625.md): Skin Panel · cracked · Oct 12, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK 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; - [SDR SWAA2024120547909](https://openairdocs.org/sdr/SWAA2024120547909.md): Support Angle · cracked · Oct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Keel > CRACK 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 - [SDR SWAA2024120547718](https://openairdocs.org/sdr/SWAA2024120547718.md): Support Bracket · cracked · Oct 12, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK 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 COMPLETED - [SDR SWAA2024120647622](https://openairdocs.org/sdr/SWAA2024120647622.md): Rib · cracked · Oct 11, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK 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 60 - [SDR SWAA2024120647620](https://openairdocs.org/sdr/SWAA2024120647620.md): Rib · cracked · Oct 11, 2024 · N269WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK 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 60 - [SDR SWAA2024120547510](https://openairdocs.org/sdr/SWAA2024120547510.md): Web · corroded · Oct 11, 2024 · N269WN · Boeing 7377H4 · Passenger Compartment Equipment > CORROSION 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 I - [SDR SWAA2024120547508](https://openairdocs.org/sdr/SWAA2024120547508.md): Floorbeam · cracked · Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACK 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.;[ - [SDR SWAA2024120547511](https://openairdocs.org/sdr/SWAA2024120547511.md): Strap · corroded · Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 51 - [SDR SWAA2024120547512](https://openairdocs.org/sdr/SWAA2024120547512.md): Floorbeam · corroded · Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION 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: N500X121 - [SDR SWAA2024120547513](https://openairdocs.org/sdr/SWAA2024120547513.md): Strap · corroded · Oct 11, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION 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 - [SDR SWAA2024120647162](https://openairdocs.org/sdr/SWAA2024120647162.md): Angle · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Trailing Edge Flaps > CRACK 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.
TOOK MEASURES OF CRACK: - [SDR SWAA2024120547164](https://openairdocs.org/sdr/SWAA2024120547164.md): Angle · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK 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 BS - [SDR SWAA2024120547165](https://openairdocs.org/sdr/SWAA2024120547165.md): Web · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Cargo Compartments > CRACK 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 D - [SDR SWAA2024120547151](https://openairdocs.org/sdr/SWAA2024120547151.md): Fitting · deteriorated · Oct 10, 2024 · N269WN · Boeing 7377H4 · Escape Slide > DETERIORATED 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] RE - [SDR SWAA2024120547146](https://openairdocs.org/sdr/SWAA2024120547146.md): Fitting · deteriorated · Oct 10, 2024 · N269WN · Boeing 7377H4 · Escape Slide > DETERIORATED 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] RE - [SDR SWAA2024120546902](https://openairdocs.org/sdr/SWAA2024120546902.md): Pressure Deck · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Keel > CRACK 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- - [SDR SWAA2024120547324](https://openairdocs.org/sdr/SWAA2024120547324.md): Stub Frame · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK 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; DUE - [SDR SWAA2024120547328](https://openairdocs.org/sdr/SWAA2024120547328.md): Intercostal · corroded · Oct 10, 2024 · N269WN · Boeing 7377H4 · Passenger Compartment Equipment > CORROSION 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 SRM - [SDR SWAA2024120546906](https://openairdocs.org/sdr/SWAA2024120546906.md): Vapor Barrier · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Keel > CRACK 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] - [SDR SWAA2024120547327](https://openairdocs.org/sdr/SWAA2024120547327.md): Intercostal · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK 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 D - [SDR SWAA2024120547323](https://openairdocs.org/sdr/SWAA2024120547323.md): Tie Clip · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK 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 -. - [SDR SWAA2024120547325](https://openairdocs.org/sdr/SWAA2024120547325.md): Frame · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK 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 COMPLETED - [SDR SWAA2024120547326](https://openairdocs.org/sdr/SWAA2024120547326.md): Stringer · cracked · Oct 10, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK 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 GA - [SDR SWAA2024120546898](https://openairdocs.org/sdr/SWAA2024120546898.md): Support Angle · cracked · Oct 9, 2024 · N269WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK 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.
REPLACED SUPPORT ANG Next page: https://openairdocs.org/aircraft/N269WN/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N269WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.