# Service difficulty reports: N265WN

A list on [N265WN](https://openairdocs.org/aircraft/N265WN.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 · 258 reports

- [SDR SWAA2026081717035](https://openairdocs.org/sdr/SWAA2026081717035.md): Nut Plate · cracked · Aug 12, 2026 · N265WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR FWD LOWER NUT PLATE CRACKED ON SLIDE ISOLATOR BRACKET. R & R AFT ENTRY DOOR FWD LOWER ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026081787218](https://openairdocs.org/sdr/SWAA2026081787218.md): Rib · cracked · Aug 12, 2026 · N265WN · Boeing 7377H4 · Wing, Rib/Bulkhead
  > LEFT AFT TRAILING EDGE FLAP DEFLECTION RIB, UPPER ATTACH ANGLE CRACKED. NR 8 SPOILER ACTUATOR SHUTTERING & NR 6 SPOILER ACTUATOR BYPASSING. WORKING SRM 57-51-02-2R-3 REPAIR 3. REMOVED AND TRIMMED OUT DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB. PERFORMED H
- [SDR SWAA2026081705976](https://openairdocs.org/sdr/SWAA2026081705976.md): Lens · contaminated · Aug 12, 2026 · N265WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1DEF PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R & R CABIN PHOTOLUMINESCENT STRIP IAW AMM 33-51-15.
- [SDR SWAA2026051297824](https://openairdocs.org/sdr/SWAA2026051297824.md): Window · failed · May 11, 2026 · N265WN · Boeing 7377H4 · Flight Compartment Windows
  > L1 WINDSHIELD SHATTERED IN FLIGHT FOLLOWED QRH NO PRESSURIZATION ISSUES LANDED HEAVY WEIGHT. REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-11. OPS CHECK GOOD. COMPLIED WITH OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35 NO DEFECTS NOTED.
- [SDR SWAA2025121551847](https://openairdocs.org/sdr/SWAA2025121551847.md): Stop Pin · broken · Dec 12, 2025 · N265WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR BROKEN; PLASTIC STOP RING BROKE OFF. INSTALLED NEW STOP PINS PER AMM 25-66-01
- [SDR SWAA2025090811271](https://openairdocs.org/sdr/SWAA2025090811271.md): Plate · bulged · Sep 4, 2025 · N265WN · Boeing 7377H4 · Fuselage Main, Structure
  > DOUBLER FOR LAV SERVICE PAN ASSY HAS BULGING AROUND LOWER ROW OF FASTNERS DUE TO CORROSION FROM BS 847 - 867 JUST ABOVE S25L. THERE IS ALSO HEAVY INTERGRANULAR CORROSION ON THE METAL STRIP DOUBLER FOR LAV SERVICE PAN ASSY HAS BULGING AROUND LOWER ROW OF FASTNE
- [SDR SWAA2025052875179](https://openairdocs.org/sdr/SWAA2025052875179.md): Lamp · inoperative · May 26, 2025 · N265WN · Boeing 7377H4 · Emergency Lighting
  > L2 OUTSIDE EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2025030601742](https://openairdocs.org/sdr/SWAA2025030601742.md): Seat Back · out of adjust · Mar 4, 2025 · N265WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER SEAT 11D RECLINES INTO AN EXIT ROW<[01] LOCKED OUT RECLINE HYDROLOK PER CMM 25-22-46.;[02] INSPECTED PER CMM 25-22-46
- [SDR SWAA2025030601756](https://openairdocs.org/sdr/SWAA2025030601756.md): Mount · cracked · Mar 4, 2025 · N265WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR IAW SRM 51-40-02.;[02] INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024101645691](https://openairdocs.org/sdr/SWAA2024101645691.md): Battery Pack · inoperative · Oct 6, 2024 · N265WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1670 INOP<[01] REPLACED POWER SUPPLY - BATTERY PACK M1670 PER AMM 33-51-06-960-805. GOOD TEST.;[02] CERTIFIED CARD COMPLETED;[03] VERIFIED CORRECTIVE ACTION 1-2.
- [SDR SWAA2024101644577](https://openairdocs.org/sdr/SWAA2024101644577.md): Battery Pack · inoperative · Oct 3, 2024 · N265WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-06-960-805 & WDM 33-51-12-2;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2024101644578](https://openairdocs.org/sdr/SWAA2024101644578.md): Battery Pack · inoperative · Oct 3, 2024 · N265WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1668 INOP<[01] REPLACED BATTERY PACK M1668 PER AMM 33-51-06-960-805 & WDM 33-51-13<BR><BR>ASILE LIGHTS ON ROW 9-12 L/H STILL INOP DURING FUNCTIONAL CHECK; TROUBLESHOOTED BY RELAMPING AND RECONNECTING. BAD FUSE IS S
- [SDR SWAA2024101637510](https://openairdocs.org/sdr/SWAA2024101637510.md): Skin · corroded · Sep 13, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > WI-FI ANTENNA SKIN DOUBLER HAS SEVERAL CORROSION SPOTS (FASTENERS AND SKIN) BS 727B+12 TO BS 747+6; STR 3L TO STR 3R CROWN AREA.<[01] 'REPAIRED PER EA 24-153-02600 WITH AN INSPECTION THRESHOLD/PROGRAM DEFINED IN 24-153-02600-INSP.';[02] 'REPAIRED PER EA 24-153
- [SDR SWAA2024101637509](https://openairdocs.org/sdr/SWAA2024101637509.md): Plate · corroded · Sep 13, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PLATE UNDER PSC ANTENNA HAS CORROSION AT BS 727E+15; LBL5 AND WL 306<[01] 'REFER TO FAULT TTG8Q00VV56H.';[02] VERIFIED ITEM 1
- [SDR SWAA2024101636998](https://openairdocs.org/sdr/SWAA2024101636998.md): Frame · cracked · Sep 12, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED FRAME BS 312 COMMON TO STR 6L LBL 33 WL 282.<[01] REPAIRED FRAME BS 312 COMMON TO STR 6L; LBL33; WL 282 PER EA M-22-153-01244 CUSTOMER SYSTEM ID: TTG8Q00VWUP8.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024101636533](https://openairdocs.org/sdr/SWAA2024101636533.md): Sidewall Support · corroded · Sep 11, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACE FLOOR TO SIDEWALL SUPPORT AS PER SRM 50-40-02-0G-0; DWG 146A0061 REV. A. 146A7500 REV. A.;[02] CORRECTIVE ACT
- [SDR SWAA2024101636547](https://openairdocs.org/sdr/SWAA2024101636547.md): Splice Strap · corroded · Sep 11, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED NEW FLOOR SPLICE STRAP ON PO# 889099; AND NEW STRAP TO BE INSTALLED ON
- [SDR SWAA2024101636548](https://openairdocs.org/sdr/SWAA2024101636548.md): Support Plate · corroded · Sep 11, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATION AND REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT. LOCATED; DRILLED; APPLIED WHITE ENAMEL AND INSTALLED NEW FLOOR TO S
- [SDR SWAA2024101635622](https://openairdocs.org/sdr/SWAA2024101635622.md): Attach Angle · cracked · Sep 9, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FWD WET AREA BS294 RBL53 WL208. MARKED<[01] CRACKED ATTACH ANGLE WILL BE REPLACED ON TTG8Q00VPT1S.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024101635292](https://openairdocs.org/sdr/SWAA2024101635292.md): Web · corroded · Sep 8, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WHILE WORKING R/H OVERWING EXIT DUE TO CORROSION EVAL; REMOVED SEALANT AROUND CORRODED AREAS; AND NOTICED A DRILLED START AT BS 616+20; WL221; RBL70.<[01] COMPLETED STEPS 1 AND 2;[02] APPLICABILITY AND LIMIT STATEMENTS.;[03] BLENDED AND REMOVED DRILL START DAM
- [SDR SWAA2024101634889](https://openairdocs.org/sdr/SWAA2024101634889.md): Girt Bar · corroded · Sep 6, 2024 · N265WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION ON FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208.<[01] REMOVED & REPLACED FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5220 REV=-.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024101634890](https://openairdocs.org/sdr/SWAA2024101634890.md): Angle · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208.<[01] REMOVE AND REPLACED NEW REPAIR ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208 IAW SRM 53-10-15-2R-7 AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024101634881](https://openairdocs.org/sdr/SWAA2024101634881.md): Floor Support · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 294-297 RBL 1 WL 208.<[01] UPDATED STEP 1.;[02] UPDATED STEP 3.;[03] UPDATED STEP 3.;[04] REMOVED & REPLACED INTERCOSTAL BS 294-297 RBL 1 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV=-.;[05] VERIFIED ACTION 4.<BR>JOB COMPLETE.
- [SDR SWAA2024101634882](https://openairdocs.org/sdr/SWAA2024101634882.md): Floor Support · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 LBL 45 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS312-BS328 LBL45 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV - OK;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2024101634883](https://openairdocs.org/sdr/SWAA2024101634883.md): Floor Support · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 328-344 LBL 45 WL 208. EDIT: INTERCOSTAL IS AT BS 312-328 LBL 45 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 LBL 45 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV: - DATE 10/08/96;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024101634884](https://openairdocs.org/sdr/SWAA2024101634884.md): Floor Support · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 344-360 RBL 11 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 344-360 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 REF DWG 141A5400 NO REV; DATE 02-24-96;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024101634885](https://openairdocs.org/sdr/SWAA2024101634885.md): Floor Support · cracked · Sep 6, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208.<[01] UPDATED STEP 3.;[02] REMOVED CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208 IAW SRM 51-40-02-0G-0 AND REPLACED INTERCOSTAL AT BS 344-360 LBL 12 WL 208 PER SRM 51-40-05-0G-0 AND DWG 141A5400 REV=A.;[03] VERIFIED
- [SDR SWAA2024101634707](https://openairdocs.org/sdr/SWAA2024101634707.md): Stub Frame · cracked · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8; 0.8' ABOVE SEAL DEPRESSOR 1.2' IN LENGTH (MARKED)<[01] REMOVED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 REV. D.;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2024101634710](https://openairdocs.org/sdr/SWAA2024101634710.md): Shear Web · corroded · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT L/H SHEAR WEB BS 1016 LBL 11-LBL 22 WL 208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED AFT L/H SHEAR WEB AT BS 1016-1026 LBL 0 - LBL 38 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 REV B DATE 05/06/09;[03] VERIFIED CORRECTIVE ACTION ENTRY
- [SDR SWAA2024101634711](https://openairdocs.org/sdr/SWAA2024101634711.md): Strap · corroded · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1016-1029 LBL 2 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP AT BS 1016-1029 LBL 2 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 REV B DATE 05/06/09;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2024101634716](https://openairdocs.org/sdr/SWAA2024101634716.md): Floor Support · cracked · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 927-947 LBL 3 WL 208. CRACKED ATTACH UPPER ANGEL ON INTERCOSTAL AT BS 927-947 LBL 3 WL 208.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL BS 927-947 LBL 3 WL 208. IAW SRM 51-40-02; BOEING DWG# 147A5400 REV:-;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2024101634309](https://openairdocs.org/sdr/SWAA2024101634309.md): Door · corroded · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fluid Service Doors
  > LAV SERVICE DOOR INNER SURFACE HAS CORROSION ON AFT EDGE<[01] REMOVED AND REPLACED DAMAGED LAV SERVICE PANEL PER AMM 52-49-07-000-801; 52-49-07-400-801; AMM 20-50-11-910-801; PERFORMED A GOOD RESISTANCE CHECK ON BONDING JUMPER PER AMM 52-49-07-400-801 STEP 3.C
- [SDR SWAA2024101634713](https://openairdocs.org/sdr/SWAA2024101634713.md): Floorbeam · corroded · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208.<[01] CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AND REPAIRED IAW SRM 53-70-51-2R-6 REPAIR 6 ALT. 4.;[02] CORRECTIVE ACTION COMPLETED;
- [SDR SWAA2024101634712](https://openairdocs.org/sdr/SWAA2024101634712.md): Reinforcement · corroded · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5730 REV C DATE 02/25/08;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2024101534497](https://openairdocs.org/sdr/SWAA2024101534497.md): Floor Panel · delaminated · Sep 5, 2024 · N265WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241ABF O/B EDGE IS DELAMINATED (AS MARKED)<[01] FLOOR PANEL 241ABF O/B EDGE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-10-A00948 (REPAIR 10 - REPAIR OF DAMAGE TO THE CORE ON AN EDGE IN COMPOSITE FLOOR PANELS - PERMANENT] ATTACHED CURE SHEE
- [SDR SWAA2024101633487](https://openairdocs.org/sdr/SWAA2024101633487.md): Web · corroded · Sep 3, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON R/H OVERWING EXIT CUT-OUT SILL AT STA 616+8; 616+9M 616+14; 616+15; 616+20; WL 221; RBL 70.<[01] COMPLETED STEPS 2 AND 3;[02] REMOVED CORROSION FROM R/H OVERWING EXIT CUT-OUT LOWER SILL AT STA 616+8; 616+9; 616+14; 616+15 AND 616+20 WL 221 RBL 70
- [SDR SWAA2024101633603](https://openairdocs.org/sdr/SWAA2024101633603.md): Bulkhead · cracked · Sep 3, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL36 WL163.<[01] CRACKED LOWER R/H BULKHEAD BS663 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024101633481](https://openairdocs.org/sdr/SWAA2024101633481.md): Vapor Barrier · debonded · Sep 3, 2024 · N265WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > STA 663 VAPOR BARRIER PREVIOUS REPAIR IS DISBONDED AT WL 160; LBL 40.<[01] VAPOR BARRIER PREVIOUS REPAIR REMOVED & REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024101633473](https://openairdocs.org/sdr/SWAA2024101633473.md): Attach Angle · cracked · Sep 2, 2024 · N265WN · Boeing 7377H4 · Wing, Attach Fittings
  > (RIGHT WING) UPPER WING PANEL SUPPORT U CHANEL AT 9-INCH O/B OF FUSELAGE; ATTACH ANGLE CRACKED AT REAR SPAR ATTACH POINT<[01] REMOVED AND REPLACED ANGLE P/N 115A5582-2 AT R/WING PANEL SUPPORT U CHANEL AND REAR SPAR ATTACH POINT IAW SRM 51-40-02-0G-0.;[02] VERI
- [SDR SWAA2024101632859](https://openairdocs.org/sdr/SWAA2024101632859.md): Attach Angle · cracked · Aug 31, 2024 · N265WN · Boeing 7377H4 · Wing, Attach Fittings
  > LT WING T/E DEFLECTION CONTROL RIB I/B ATTACHED ANGLE CRACK<[01] VERIFIED;[02] VERIFIED;[03] REMOVED AND REPLACED LEFT WING T/E DEFLECTION CONTROL RIB I/B ATTACHMENT ANGLE IAW SRM 51-40-02-0G-0 PAR 4.;[04] REJECT ACTION 3: MISSING INSTALLATION DRAWING ON STATE
- [SDR SWAA2024042678968](https://openairdocs.org/sdr/SWAA2024042678968.md): Threshold · cracked · Apr 25, 2024 · N265WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FUSELAGE FORWARD CARGO CENTER THRESHOLD IS CRACKED AT AFT DOOR STOP.<[01] R/R FWD CARGO DOOR CENTER THRESHOLD PER AMM 53-11-02
- [SDR SWAA2024042578970](https://openairdocs.org/sdr/SWAA2024042578970.md): Battery Pack · no test · Apr 25, 2024 · N265WN · Boeing 7377H4 · Emergency Lighting
  > EMX LIGHT BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX LIGHT BATT PACK M01672 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2023021603460](https://openairdocs.org/sdr/SWAA2023021603460.md): Battery Pack · failed · Feb 16, 2023 · N265WN · Boeing 7377H4 · Emergency Lighting
  > AFT CABIN LH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1673 IAW AMM 33-51-06.
- [SDR SWAA2023021603454](https://openairdocs.org/sdr/SWAA2023021603454.md): Battery Pack · failed · Feb 16, 2023 · N265WN · Boeing 7377H4 · Emergency Lighting
  > MID CABIN RH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 IAW AMM 33-51-06.
- [SDR SWAA2023021603461](https://openairdocs.org/sdr/SWAA2023021603461.md): Panel · cracked · Feb 16, 2023 · N265WN · Boeing 7377H4 · Galley Doors
  > AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SERVICE DOOR LOWER PANEL 844DZ PAN REF AMM 52-41-31.
- [SDR SWAA2022101056386](https://openairdocs.org/sdr/SWAA2022101056386.md): None · inoperative · Oct 5, 2022 · N265WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK LOCATED LT SIDE AT FWD GALLEY AREA 2022-467055 / [01] REPLACED BATTERY PACK P/N AD-B717-01-100SWA S/N 41847 OFF; P/N AD-B717-01-100SWA S/N BN 265159 ON; IAW B737-700 AMM 33-51-06-960-805 TEST NEW BATTERY PACK OK.;[02] REPLACED BATTERY PACK P/
- [SDR SWAA2022101046562](https://openairdocs.org/sdr/SWAA2022101046562.md): Angle · broken · Sep 22, 2022 · N265WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE BODY FAIRING IAW B737-700 SRM 51-40-02 AND DWG# 116A3010; SHEET: 3; REV: - AND D
- [SDR SWAA2022101046563](https://openairdocs.org/sdr/SWAA2022101046563.md): Stud · broken · Sep 22, 2022 · N265WN · Boeing 7377H4 · Fuselage Main, Structure
  > BROKEN STUD RECEPTACLE ON BRACKET AE0502A E5-2 2022-467012 / [01] REPLACED STUD RECEPTACLE LOCATED ON BRACKET AE0502A E5-2 I.A.W B737-700 SRM 51-40-02-0G-0.;[02] REPLACED STUD RECEPTACLE LOCATED ON BRACKET AE0502A E5-2 I.A.W B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2022101016065](https://openairdocs.org/sdr/SWAA2022101016065.md): Support Angle · broken · Sep 22, 2022 · N265WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 /
- [SDR SWAA2022100646564](https://openairdocs.org/sdr/SWAA2022100646564.md): Strap · cracked · Sep 22, 2022 · N265WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT 2022-467013 / [01] REPLACED STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #143A7500;

Next page: https://openairdocs.org/aircraft/N265WN/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 = 'N265WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N265WN/reports

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