# Service difficulty reports: N495WN A list on [N495WN](https://openairdocs.org/aircraft/N495WN.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 7 · 316 reports - [SDR SWAA2026083189724](https://openairdocs.org/sdr/SWAA2026083189724.md): Exhaust Duct · fire · Aug 28, 2026 · N495WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle > NR 1 ENG. TAIL PIPE FIRE REPORTED BY ANOTHER AIRCRAFT. EXTINGUISHED AFTER ENGINE SHUTDOWN. FLAMES FOUND TO BE CANDLE FIRE PHENOMENA IN THE EXHAUST PLUG. C/W INSPECTION IAW AMM 71-00-00 NO DEFECTS NOTED. SUBSEQUENT ENGINE RUN NORMAL A/C OK FOR SERVICE.. - [SDR SWAA2026080328107](https://openairdocs.org/sdr/SWAA2026080328107.md): Bolt · loose · Jul 31, 2026 · N495WN · Boeing 7377H4 · Passenger/Crew Doors > FWD ENTRY DOOR ASSIST HANDLE WAS LOOSE. TIGHTENED BOLTS ON FED ASSIST HANDLE IAW AMM 52-11-31-400-802, STEP 3.G. (2). - [SDR SWAA2026080375433](https://openairdocs.org/sdr/SWAA2026080375433.md): Light · inoperative · Jul 21, 2026 · N495WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF AND PERFORMED GOOD OPS TEST IAW AMM 33-51-03-960-801. - [SDR SWAA2026080390865](https://openairdocs.org/sdr/SWAA2026080390865.md): Lamp · burned out · Jul 21, 2026 · N495WN · Boeing 7377H4 · Emergency Lighting > RIGHT OVERWING LOWER EMERGENCY EXIT SIGN HAS BURNED OUT BULBS. R & R RT OVERWING LOWER EMERGENCY SIGN LAMPS IAW AMM 33-51-01-960-801. - [SDR SWAA2026080433329](https://openairdocs.org/sdr/SWAA2026080433329.md): Stiffener · corroded · Jul 20, 2026 · N495WN · Boeing 7377H4 · Wing Miscellaneous Structure > CORROSION FOUND ON LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73. REMOVED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73 IAW SRM 51-40-02-0G-0. INSTALLED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OF SS 308 SS 73 IAW SRM 51-4 - [SDR SWAA2026080486563](https://openairdocs.org/sdr/SWAA2026080486563.md): Stiffener · corroded · Jul 20, 2026 · N495WN · Boeing 7377H4 · Wing Miscellaneous Structure > CORROSION WAS FOUND ON STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 [MARKED] REMOVED AND REPLACED STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 IAW SRM 51-40-02-0G-0 AND AIPC 57-40-00-17. - [SDR SWAA2026080371392](https://openairdocs.org/sdr/SWAA2026080371392.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, BS 727A, S7L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -. - [SDR SWAA2026080369769](https://openairdocs.org/sdr/SWAA2026080369769.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, BS 727A, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -. - [SDR SWAA2026080388192](https://openairdocs.org/sdr/SWAA2026080388192.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, BS 727B, S7L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -. - [SDR SWAA2026080393981](https://openairdocs.org/sdr/SWAA2026080393981.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727E, S3L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DOCUMENT NR 146A1112, DWG 0009, REV-. - [SDR SWAA2026080328655](https://openairdocs.org/sdr/SWAA2026080328655.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -. - [SDR SWAA2026080388797](https://openairdocs.org/sdr/SWAA2026080388797.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727E, S4L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1112, SHEET 09, REV -. - [SDR SWAA2026080388195](https://openairdocs.org/sdr/SWAA2026080388195.md): Stringer Clip · cracked · Jul 16, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, BS 727E, S5L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 146A1112, SHEET 09, REV -. - [SDR SWAA2026080414529](https://openairdocs.org/sdr/SWAA2026080414529.md): Strap · out of tolerance · Jul 14, 2026 · N495WN · Boeing 7377H4 · Fuselage Main, Structure > E/E COMPARTMENT, BS 328 BETWEEN S20R TO S22R, FRAME STRAP CONFIGURATION DOES NOT MATCH FIG. 15 PER EO 5311-I-17336-NG REF FAULT TTG8Q0157B6V AS PER EA 26-153-01902 THE CONFIGURATION IS ACCEPTABLE. VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2026061111332](https://openairdocs.org/sdr/SWAA2026061111332.md): Tailpipe · fire · Jun 11, 2026 · N495WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle > TAILPIPE FIRE REPORTED BY SEVERAL AIRCRAFT IN THE LEFT ENGINE WITH FLAMES VISIBLE, WHEN ENGINE WAS SHUTDOWN FLAMES DISAPPEARED BUT SMOKE STILL VISIBLE REPORTED BY FIRE DEPARTMENT; (CONT IN FAULT DESCR (CONT) UPON RETURN TO THE GATE FIRE DEPARTMENT REPORTED SM - [SDR SWAA2026051803655](https://openairdocs.org/sdr/SWAA2026051803655.md): Screw · loose · May 15, 2026 · N495WN · Boeing 7377H4 · Escape Slide > CREW REPORT L1 DOOR ESCAPE SLIDE MOUNT SCREW LOOSE. SECURED L1 DOOR ESCAPE SLIDE MOUNT SCREW IAW MT 725-61-06. - [SDR SWAA2026033082539](https://openairdocs.org/sdr/SWAA2026033082539.md): Battery Pack · failed · Mar 24, 2026 · N495WN · Boeing 7377H4 · Emergency Lighting > FWD GALLEY EMERGENCY BATTERY PACK RT M1674 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK AT M1674 PER AMM 33-51-06;[02] C/W INSPECTION - [SDR SWAA2026032380559](https://openairdocs.org/sdr/SWAA2026032380559.md): Coalescer Bag · odor · Mar 17, 2026 · N495WN · Boeing 7377H4 · Air Distribution System > FLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT COALESCED BAGS; AND REMOVED AND REPLACED CABIN RECIRCULATING AIR HEAP FILTER. PERFORMED ENG AND PA - [SDR SWAA2026032380623](https://openairdocs.org/sdr/SWAA2026032380623.md): Filter · odor · Mar 17, 2026 · N495WN · Boeing 7377H4 · Air Distribution System > FLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT COALESCED BAGS; AND REMOVED AND REPLACED CABIN RECIRCULATING AIR HEAP FILTER. PERFORMED ENG AND PA - [SDR SWAA2026032080287](https://openairdocs.org/sdr/SWAA2026032080287.md): Computer · inoperative · Mar 16, 2026 · N495WN · Boeing 7377H4 · Auto Throttle System > ENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE. PERFORMED AUTOTHROTTLE SYSTEM OPERATIONAL TEST IAW AMM 22-31-00. OPS CHECKS GOOD. NO FURTHER FAULTS NOTED. MEL CLEARED. REF LP# 3078430 FOR CAT III RECERTIFICATION - [SDR SWAA2026032081730](https://openairdocs.org/sdr/SWAA2026032081730.md): Servo · inoperative · Mar 16, 2026 · N495WN · Boeing 7377H4 · Auto Throttle System > ENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE. - [SDR SWAA2025030400992](https://openairdocs.org/sdr/SWAA2025030400992.md): Lamp · inoperative · Mar 1, 2025 · N495WN · Boeing 7377H4 · Emergency Lighting > LH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (LH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT - LAMP REPLACEMENT - PERMANENT)] - [SDR SWAA2024112670914](https://openairdocs.org/sdr/SWAA2024112670914.md): Light · loose · Nov 22, 2024 · N495WN · Boeing 7377H4 · Emergency Lighting > SIDE WALL OVERWING EXIT SIGN (FO SIDE) FELL OFF DURING DEPLANING.<[01] REATT. SIDEWALL OVERWING EXIT LIGHT REF. S.I.P. - [SDR SWAA2024093041425](https://openairdocs.org/sdr/SWAA2024093041425.md): Plate · damaged · Sep 25, 2024 · N495WN · Boeing 7377H4 · Trailing Edge Flaps > LH WING UPPER FIXED TRAILING EDGE WIGGLE PANEL COMMON TO 551CT; MOUNT TAB HOLES ELONGATED AND PULLED THRU.<[01] CW NDT INSPECTION OF CUTOUT REF NDT 51-00-00 PROCEDURE 23; NO DEFECTS NOTED AT THIS TIME.;[02] PERFORMED PERMANENT REPAIR ON LH WING FIXED TRAILING - [SDR SWAA2024092741368](https://openairdocs.org/sdr/SWAA2024092741368.md): Strap · damaged · Sep 25, 2024 · N495WN · Boeing 7377H4 · Emergency Equipment > FWD SERVICE DOOR SAFETY STRAP DETERIORATED.<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIP - [SDR SWAA2024092741369](https://openairdocs.org/sdr/SWAA2024092741369.md): Strap · deteriorated · Sep 25, 2024 · N495WN · Boeing 7377H4 · Emergency Equipment > FWD ENTRY DOOR SAFETY STRAP DETERIORATED.<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIP - [SDR SWAA2024092338657](https://openairdocs.org/sdr/SWAA2024092338657.md): Handle · loose · Sep 17, 2024 · N495WN · Boeing 7377H4 · Passenger/Crew Doors > PAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE LOOSE 2024-489434<[01] CORRECTED INSTALLED PAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE IAW B737- 700 AMM 52-11-31-400-802 STEP 3.G.(2);[02] CERTIFIED WORK PERFORMED. - [SDR SWAA2024092338663](https://openairdocs.org/sdr/SWAA2024092338663.md): Handle · loose · Sep 17, 2024 · N495WN · Boeing 7377H4 · Galley Doors > PAX CABIN AFT SERVICE RIGHT DOOR AREA; FWD CUT OUT ASSISTANT HANDLE LOOSE 2024-489451<[01] PAX CABIN AFT SERVICE RIGHT DOOR AREA FWD CUT OUT ASSISTANT HANDLE TIGHTENED IAW B737-700 AMM 25-21-25-420-801 STEP 3 B.(5);[02] CERTIFIED WORK PERFORMED - [SDR SWAA2024091930026](https://openairdocs.org/sdr/SWAA2024091930026.md): Window Frame · cracked · Aug 25, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK WINDOW 3 FRAME LT SIDE AT COCKPIT 2024-489385<[01] PERFORMED A PERMANET REPAIR ON WINDOW 3 FRAME LT SIDE AT COCKPIT IAW EA- 24-153-02350-WIP1 [TTG8Q00VGP0W]; EA-24-153-02350-WIP2 [TTG8Q00VPE70]; 24-153-02350-WIP3 [TTG8Q00VT5E5]; 24-153-02350-WIP4 [TTG8Q0 - [SDR SWAA2024092025383](https://openairdocs.org/sdr/SWAA2024092025383.md): Web · cracked · Aug 12, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON WEB LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-489315<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9;B737-700 SRM 51-40-02 - [SDR SWAA2024092025381](https://openairdocs.org/sdr/SWAA2024092025381.md): Angle · cracked · Aug 12, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT 2024-489311<[01] REPLACED ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 143A7902 S - [SDR SWAA2024091925379](https://openairdocs.org/sdr/SWAA2024091925379.md): Stringer · cracked · Aug 12, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489309<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOL USED ON STEP 9: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N:210138003; DUE DATE: 11-JUN-25.;[03] - [SDR SWAA2024091925380](https://openairdocs.org/sdr/SWAA2024091925380.md): Stringer · cracked · Aug 12, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK ON STRINGER 27L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489310<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[03] TOOL USED ON STEP 8: - [SDR SWAA2024091925382](https://openairdocs.org/sdr/SWAA2024091925382.md): Stringer · cracked · Aug 12, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK ON STR 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489314<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOLS USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATURE - [SDR SWAA2024092325378](https://openairdocs.org/sdr/SWAA2024092325378.md): Balance Arm · corroded · Aug 11, 2024 · N495WN · Boeing 7377H4 · Rudder Structure > CUSTOMER REQUESTS CORROSION ON LE OF RUDDER BALANCE ARM AT VERTICAL STABILIZER 2024-489272<[01] REPLACED RUDDER BALANCE ARM WEIGHT IAW BOEING 737 CMM 55-40-09.SEE INDIVIDUAL STEPS SIGN OFF BELOW.;[02] REPLACED RUDDER BALANCE ARM WEIGHT IAW BOEING 737 CMM 55-40 - [SDR SWAA2024092324801](https://openairdocs.org/sdr/SWAA2024092324801.md): Angle · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-489238<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02;SRM 51-40-02 AND DWG 146A7901 SHEET 58 REV -. MEASURE OF CRACK IS:L=0.035 INCH T - [SDR SWAA2024092324817](https://openairdocs.org/sdr/SWAA2024092324817.md): Stringer · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN 2024-489249<[01] REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; DWG 141A1110 SHEET 18 REV- AND DWG 141A8380 SHEET 14 REV-.
SEE INDIVIDUAL SIGN-OFF BELOW.;[0 - [SDR SWAA2024092024810](https://openairdocs.org/sdr/SWAA2024092024810.md): Access Panel · damaged · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ACCESS PANEL 123YBC AT FWD CARGO COMPARTMENT 2024-489246<[01] FABRICATED PANEL 123YBC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 6 REV:A MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FAB - [SDR SWAA2024092024815](https://openairdocs.org/sdr/SWAA2024092024815.md): Access Panel · elongated · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ACCESS PANEL 123YCC AT FWD CARGO COMPARTMENT 2024-489248<[01] FABRICATED PANEL 123YCC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 7 REV:A. MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FA - [SDR SWAA2024092024813](https://openairdocs.org/sdr/SWAA2024092024813.md): Access Panel · damaged · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ACCESS PANEL 123YAC AT FWD CARGO COMPARTMENT 2024-489251<[01] FABRICATED PANEL 123YAC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 5 REV:A. MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FA - [SDR SWAA2024092024811](https://openairdocs.org/sdr/SWAA2024092024811.md): Light · deteriorated · Aug 10, 2024 · N495WN · Boeing 7377H4 · Emergency Lighting > DETERIORATED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT PASSENGER CABIN 2024-489244<[01] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT
PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT
PASSENGER CA - [SDR SWAA2024092024807](https://openairdocs.org/sdr/SWAA2024092024807.md): Angle · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Structure (General) > CRACK ANGLE - CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT 2024-489239<[01] REPLACED CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 6 REV D.;[02] CORRECTED STEP 1 CRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-489240<[01] REPLACED ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 143A7505 SHEET 6 REV. D;[02] TASK CARD COMPLETED
REPLACED - [SDR SWAA2024091924821](https://openairdocs.org/sdr/SWAA2024091924821.md): Web · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB FRAME BS 259.5 BETWEEN S-8R TO S-9R AT PASSENGER CABIN 2024-489252<[01] ON STEP 5; TOOL USED: EDDY CURRENT INSPECTION; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 11-MAY-25;[02] PERFORMED A PERMANENT REPAIR ON WEB FRAME BS259.5 BETWEEN STR-6R TO STR- - [SDR SWAA2024091924820](https://openairdocs.org/sdr/SWAA2024091924820.md): Web · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB FRAME BS 259.5 BETWEEN S-8L TO S-9L AT PASSENGER CABIN 2024-489254<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 200053402 DUE DATE: 24-AUG-24;[02] REPAIRED FUSELAGE FRAME WEB AT BSTA 259.5 BTW WL 240 & WL 280 AND BTW LBL 20 AND LB - [SDR SWAA2024091924812](https://openairdocs.org/sdr/SWAA2024091924812.md): Stringer · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK STRINGER 7L LOCATED BS 294.5 AT PASSENGER CABIN 2024-489247<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138003; DUE DATE: 11-JUN-25.;[05] PERFORMED PERMANENT REPAIR CATEGORY B. LOCATED AT STRINGER 7L AND BTW BS277 TO BS303.9 A - [SDR SWAA2024091924798](https://openairdocs.org/sdr/SWAA2024091924798.md): Web · cracked · Aug 10, 2024 · N495WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > CRACK WEB LOCATED RIB 5 AND RIB 6 FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-489228<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED PERMANENT REPAIR ON WEB LOCATED RIB 5 AND RIB 6 FRONT SPAR AT RT HORIZONTAL STABILIZER - [SDR SWAA2024092024797](https://openairdocs.org/sdr/SWAA2024092024797.md): Angle · cracked · Aug 9, 2024 · N495WN · Boeing 7377H4 · Passenger/Crew Doors > CRACK ON FWD ENTRY DOOR AFT UPPER TARGET ANGLE 2024-489223<[01] REPLACED FWD ENTRY DOOR AFT UPPER TARGET ANGLE IAW B737-700 SRM SRM 51-40-02 AND 51-10-02 ITEM 9;[02] REPLACED FWD ENTRY DOOR AFT UPPER TARGET ANGLE IAW B737-700 SRM SRM 51-40-02 AND 51-10-02 ITEM - [SDR SWAA2024092324288](https://openairdocs.org/sdr/SWAA2024092324288.md): Strap · cracked · Aug 8, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CARGO COMPARTMENT 2024-489209<[01] REPLACED STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A8200 SHEET 44 REV -;[02] REPLACED STRAP LOCATE - [SDR SWAA2024092024283](https://openairdocs.org/sdr/SWAA2024092024283.md): Support · corroded · Aug 8, 2024 · N495WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BETWEEN STA727A TO STA767 AND RBL21 WL156 AFT CARGO COMPARTMENT 2024-489195<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN STA727 TO STA 767 AND RBL21 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND Next page: https://openairdocs.org/aircraft/N495WN/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 = 'N495WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N495WN/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.