# Service difficulty reports: N267WN

A list on [N267WN](https://openairdocs.org/aircraft/N267WN.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 · 303 reports

- [SDR SWAA2026070718223](https://openairdocs.org/sdr/SWAA2026070718223.md): Battery Pack · no test · Jul 3, 2026 · N267WN · Boeing 7377H4 · Emergency Lighting
  > 20 ABC EMERGENCY BATTERY PACK AT1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026070718218](https://openairdocs.org/sdr/SWAA2026070718218.md): Battery Pack · no test · Jul 3, 2026 · N267WN · Boeing 7377H4 · Emergency Lighting
  > RT EMERGENCY EXIT EMERGENCY BATTERY. PACK AT 1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2026021169123](https://openairdocs.org/sdr/SWAA2026021169123.md): Light · inoperative · Feb 9, 2026 · N267WN · Boeing 7377H4 · Emergency Lighting
  > FIRST OFFICER`S SIDE EMERGENCY WINDOW LIGHT INOPERATIVE. R & R THE EMERGENCY WINDOW LIGHT. OPS CHECKED GOOD IAW AMM 33-21-00.
- [SDR SWAA2025102025675](https://openairdocs.org/sdr/SWAA2025102025675.md): Seal · missing · Oct 18, 2025 · N267WN · Boeing 7377H4 · Flight Compartment Windows
  > CAPTAIN L2 WOULD NOT SEAL. AIRPLANE WOULD NOT PRESSURIZE;CABIN CLIMBING AT CLIMB RATE.ON LANDING SMOOTH TOUCHDOWN WITH NO SIDE LOADING ON AIRPLANE.NOSE WHEEL TOUCHED DOWN SMOOTHLY. USED AUTO BRAKES. INSPECTED AND FOUND L2 WINDOW RUBBER TORQUE SEAL MISSING.
- [SDR SWAA2025013191498](https://openairdocs.org/sdr/SWAA2025013191498.md): Door · cracked · Jan 31, 2025 · N267WN · Boeing 7377H4 · Landing Gear Doors
  > L/H MAIN LANDING GEAR CENTER STRUT DOOR IS CRACKED ON LOWER FWD POCKET.<[01] REMOVED LG L/H CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11 OK TO CONTINUE SERVICE. PER CDL 32-10-3XC AUTHORIZATION # 235084. INSTALLED LT CENTER AND INNER DOOR PER AMM 32-13-11 O
- [SDR SWAA2024092038677](https://openairdocs.org/sdr/SWAA2024092038677.md): Bulb · burned out · Sep 18, 2024 · N267WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR HAS BURNED OUT BULBS<[01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR IAW AMM 33-51-01-960-801;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024092039086](https://openairdocs.org/sdr/SWAA2024092039086.md): Bulb · inoperative · Sep 18, 2024 · N267WN · Boeing 7377H4 · Emergency Lighting
  > LH ASD EMERGENCY EXIT LIGHT INOP<[01] REPLACED LH SLIDE EMERGENCY LIGHT BULB AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024092038676](https://openairdocs.org/sdr/SWAA2024092038676.md): Wire · disconnected · Sep 17, 2024 · N267WN · Boeing 7377H4 · Light System Wiring
  > G-1 GALLEY EMERGENCY LIGHT IS NOT CONNECTED.<[01] DISPLACED G-1 GALLEY FWD SIDE WALL; CONNECTED EMERGENCY LIGHT AND INSTALLED FWD GALLEY SIDE WALL IAW AMM 25-21-35-420-801 AND AMM 25-21-35-020-801;[02] DISPLACED G-1 GALLEY FWD SIDE WALL; CONNECTED EMERGENCY LI
- [SDR SWAA2024092038546](https://openairdocs.org/sdr/SWAA2024092038546.md): Battery Pack · failed · Sep 14, 2024 · N267WN · Boeing 7377H4 · Emergency Lighting
  > BATTERIES PACKS M1675 AND M1673 FAIL TEST<[01] REPLACED EMERGENCY BATTERIES PACKS M1673 AND M1675 PER AMM 33-51-06-960-805; STEP 4.A THRU 4.E(1-5);[02] VERIFIED ITEM 1.;[03] REPLACED EMERGENCY BATTERIES PACKS M1673 AND M1675 PER AMM 33-51-06-960-805; STEP 4.A
- [SDR SWAA2024091933592](https://openairdocs.org/sdr/SWAA2024091933592.md): Stiffener · cracked · Sep 3, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > DURING NDI HFEC INSPECTION; FOUND LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IS CRACKED; L:0.5' MARKED<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IAW SRM 55-10-09-2R-4.;[02] VERIFIED RII CORRECTIVE ACTION 1.
- [SDR SWAA2024091930070](https://openairdocs.org/sdr/SWAA2024091930070.md): Stub Frame · cracked · Aug 25, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, Frame
  > DURING HFEC OPEN HOLES INSPECTION; CRACK NOTED AT HOLE COMMON TO VERTICAL FLANGE OF MOPSILL AND STUB FRAME AT BS294.5; RBL 54; WL208.5<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] VERIFIED STEPS 4;5 COMPLETE.;[03] ACCOMPLISHED REPAIR ON VERTICAL FLANGE OF MOPSILL AN
- [SDR SWAA2024092027725](https://openairdocs.org/sdr/SWAA2024092027725.md): Web · cracked · Aug 19, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > L/H WEB AT BS 993.50 CRACKED/DAMAGED COMMON TO LAV 'B' O/B MOUNT<[01] REMOVED; REPLACED; AND INSTALLED A NEW L/H WEB AT BS 993.50; LBL33.80; WL208 IAW SRM 51-40-02; BOEING DWG 147A5600 SH 1; AND BOEING DWG 147A0004 SH 64.;[02] UPDATED FAILURE TYPE MEASUREMENTS
- [SDR SWAA2024092325858](https://openairdocs.org/sdr/SWAA2024092325858.md): Seal · cracked · Aug 14, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW RT SLIDE SEAL AND REMOVED AND REPLACED SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW SRM 51-40-02-0G-0. INSTALLATION OF SLIDE SEAL WILL BE ACCOMPLISHED ON CUST FAULT #TTG8Q00V7MNA;[02] VERIFIED CORR
- [SDR SWAA2024092325856](https://openairdocs.org/sdr/SWAA2024092325856.md): Spar Web · corroded · Aug 14, 2024 · N267WN · Boeing 7377H4 · Wing Spar
  > CORROSION ON LH WING REAR SPAR WEB AT UPPER END OF CUTOUT FOR #1 FUEL TANK AFT BOOST PUMP<[01] VERIFIED APPLICABILITY OF SRM 57-20-10-1A-3 PER STC ST00830SE;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED CORROSION ON LH WING REAR SPAR WEB AT UPPER END O
- [SDR SWAA2024092325857](https://openairdocs.org/sdr/SWAA2024092325857.md): Seal · cracked · Aug 14, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW LT SLIDE SEAL AND REMOVED AND RE-INSTALLED EXISTING SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW SRM 51-40-02-0G-0. INSTALLATION OF SLIDE SEAL WILL BE ACCOMPLISHED ON CUST FAULT #TTG8Q00V7MNA;[02]
- [SDR SWAA2024092025854](https://openairdocs.org/sdr/SWAA2024092025854.md): Shield · corroded · Aug 13, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED DAMAGED ACB SHIELD FWD OF ACD BS 767-794; RBL 22; WL 156 PER SRM 51-40-02-0G-0 AND INSTALLED NEW ACB FWD SHIELD BS 767-794; RBL 22; WL 15
- [SDR SWAA2024091925849](https://openairdocs.org/sdr/SWAA2024091925849.md): Plate · corroded · Aug 13, 2024 · N267WN · 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 DAMAGED L/H FLOOR TO SIDEWALL SUPPORT; LOCATED; DRILLED AND INSTALLED NEW ACB L/H FLOOR TO SIDEWALL SUPPORT PLATE OF PER
- [SDR SWAA2024091925850](https://openairdocs.org/sdr/SWAA2024091925850.md): Support · corroded · Aug 13, 2024 · N267WN · 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] REMOVED DAMAGED R/H FLOOR TO SIDEWALL SUPPORT; LOCATED; DRILLED AND INSTALLED NEW ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE OF
- [SDR SWAA2024092025439](https://openairdocs.org/sdr/SWAA2024092025439.md): Threshold · cracked · Aug 12, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED STEPS 5;6 COMPLETE; ALL STEPS AND MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2024092324295](https://openairdocs.org/sdr/SWAA2024092324295.md): Floor Support · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 344-360 BL 0 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 344-360 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DOCUMENT NUMBER 141A5400 TYPE: DWG ID:0032 REV:-;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024092324299](https://openairdocs.org/sdr/SWAA2024092324299.md): Frame · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED FRAME BS 312 COMMON TO STRINGER 6L.<[01] ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 7L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TTG8Q00V943A;[02] EDIT: ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 6L PER EA M-22-153-01244; DOCUMENTED ON TASK ID T
- [SDR SWAA2024092324296](https://openairdocs.org/sdr/SWAA2024092324296.md): Floor Support · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 LBL 46 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 312-328 LBL 46 WL 208 PER SRM 51-40-02 COMPLETED MEASURMENT TABLE LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 312-328 LBL 46 WL 208 PER SRM 51-40-05 AND BOEING
- [SDR SWAA2024092324308](https://openairdocs.org/sdr/SWAA2024092324308.md): Skin · debonded · Aug 8, 2024 · N267WN · Boeing 7377H4 · Spoilers
  > RH #8 FLIGHT SPOILER UPPER SURFACE HAS DISBOND 2.9' FROM O/B EDGE AND 8.3' FROM T/E.<[01] REMOVED AND REPLACED RH #8 FLIGHT SPOILER IAW AMM 27-61-11-400-801;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024092024058](https://openairdocs.org/sdr/SWAA2024092024058.md): Stub Frame · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FSD STUB FRAME. LOCATED AT BS 291.5 + 10;.7' ABOVE SEAL DEPRESSOR;.4' IN LENGTH (MARKED) CORRECTION TO FAULT NAME: CRACK FOUND ON FSD STUB FRAME<[01] INSTALLED FWD SERVICE DOOR UPPER STUB FRAME P/N 141A8371-7 I.A.W. SRM 51-40-02-0G0 DWG # 141A8370 R
- [SDR SWAA2024092024300](https://openairdocs.org/sdr/SWAA2024092024300.md): Support Angle · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SCUFF PLATE SUPPORT ANGLE FWD LOWER CORNER OF FWD ENTRY DOOR CUTOUT BS 309 WL 217.<[01] REMOVED AND REINSTALLED SCUFFPLATE SUPPORT ANGLE FWD LOWER CORNER OF FWD ENTRY DOOR CUOUT BS 309 WL 217 IAW SRM 51-00-10-0G-0 AND BOEING DOCUMENT NUMBER 141A8230 TE
- [SDR SWAA2024092024303](https://openairdocs.org/sdr/SWAA2024092024303.md): Intercostal · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL @ BS 277-294 RBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL @ BS 277-294 RBL 1 WL 208 PER DWG: 141A5400 REV: - ID: 0020 AND INSTALLED INTERCOSTAL @ BS 277-294
- [SDR SWAA2024092024304](https://openairdocs.org/sdr/SWAA2024092024304.md): Intercostal · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 328-344 LBL 46 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AT BS 328 TO 344 LBL 46 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1. OK TO INSTALL GIVEN.;
- [SDR SWAA2024092024305](https://openairdocs.org/sdr/SWAA2024092024305.md): Intercostal · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] ALL STEPS COMPLETED REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE LOCATED AND DRILLED NEW INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-05 AND BOEING DW
- [SDR SWAA2024092024297](https://openairdocs.org/sdr/SWAA2024092024297.md): Intercostal · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL TO BS 380-400 LBL 1 WL 208 PER DWG: 143A5400 ID: 0038 REV: A AND SRM 51-40-02 AND INSTALLED NEW INTER
- [SDR SWAA2024092024307](https://openairdocs.org/sdr/SWAA2024092024307.md): Intercostal · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 RBL 39 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 380-400 RBL 39 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE. LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 380-400 RBL 39 WL 208 PER SRM 51-40-05 AND BOEI
- [SDR SWAA2024091924301](https://openairdocs.org/sdr/SWAA2024091924301.md): Angle · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BS 294.5 FWD SIDE OF FRAME RBL 54 WL 208.<[01] STUB FRAME OF THE FORWARD GALLEY DOOR SURROUND STRUCTURE AT STA 296.4 REPAIR IS ACCOMPLISHED ON CUSTOMER CARD #TTG8Q00VFMWA;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024091924306](https://openairdocs.org/sdr/SWAA2024091924306.md): Floor Support · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 RBL 8 WL 208.<[01] ALL STEPS COMPLETED REMOVE INTERCOSTAL BS 380-400 RBL 8 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE. LOCATED AND DRILLED NEW REPLACEMENT INTERCOSTAL BS 380-400 RBL 8 WL 208 PER SRM 51-40-05 AND BOEING D
- [SDR SWAA2024091923881](https://openairdocs.org/sdr/SWAA2024091923881.md): Stiffener · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 ARE CRACKED IN THE LOWER RADIUS.<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 IAW SRM 55-10-09-2R-4.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024091924049](https://openairdocs.org/sdr/SWAA2024091924049.md): Skin · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.3' IN LENGTH (MARKED CORRECTION TO FAULT NAME. 26.5' FROM FWD EDGE<[01] REPAIRED PER SRM 55-10-01-2R-11;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024091924052](https://openairdocs.org/sdr/SWAA2024091924052.md): Skin · cracked · Aug 8, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.65' IN LENGTH (MARKED)<[01] REPAIR AS PER SRM 55-10-01-2R-11.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024091923837](https://openairdocs.org/sdr/SWAA2024091923837.md): Bearing · out of limits · Aug 7, 2024 · N267WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > DURING ACCOMPLISHMENT OF CUSTOMER CARD 5510-I-16685-NG (INSP-STABILIZERS-HORIZONTAL STABILIZER SPHERICAL BEARING) FOUND DIMENSION H TO BE.0825 AND OUT OF LIMITS<[01] REMOVED AND REPLACED L/H AND R/H HORIZONTAL STAB CENTER SECTION HINGE HOUSING SPHERICAL BEARI
- [SDR SWAA2024091923855](https://openairdocs.org/sdr/SWAA2024091923855.md): Support · cracked · Aug 7, 2024 · N267WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > UPPER BULB SEAL RETAINER SUPPORT IS CRACKED AT LOWER FASTENER HOLE AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED AND REPLACED UPPER BULB SEAL RETAINER SUPPORT AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON<BR>I.A.W SRM 51-40-02.<B
- [SDR SWAA2024091923365](https://openairdocs.org/sdr/SWAA2024091923365.md): Vapor Barrier · cracked · Aug 6, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > R/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024091923366](https://openairdocs.org/sdr/SWAA2024091923366.md): Vapor Barrier · cracked · Aug 6, 2024 · N267WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > L/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024092322980](https://openairdocs.org/sdr/SWAA2024092322980.md): Support · cracked · Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL TRANSVERSE SUPPORT IAW SRM 51-40-02-0G-0
- [SDR SWAA2024092322984](https://openairdocs.org/sdr/SWAA2024092322984.md): Support Fitting · cracked · Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPPER PANEL MID SUPPORT BEAM AFT END FITTING IAW SRM 51-40-02-0G-0
- [SDR SWAA2024092322981](https://openairdocs.org/sdr/SWAA2024092322981.md): Beam · cracked · Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 IAW SRM 51-40-02 AND AMM 20-50-11-910-801.;[02] CAL
- [SDR SWAA2024092322986](https://openairdocs.org/sdr/SWAA2024092322986.md): Bracket · cracked · Aug 5, 2024 · N267WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET FWD FACE HAS CRACK.<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET IAW SRM 51-40-02 AND AIPC 57-42-51-03.;[02]
- [SDR SWAA2023092501958](https://openairdocs.org/sdr/SWAA2023092501958.md): Escape Rope · out of position · Sep 19, 2023 · N267WN · Boeing 7377H4 · Emergency Equipment
  > RIGHT OVERWING EXIT ESCAPE ROPE IS NOT STOWED PROPERLY.<[01] RESECURED RIGHT OVERWING EXIT ESCAPE ROPE PER SIP
- [SDR SWAA2023091801555](https://openairdocs.org/sdr/SWAA2023091801555.md): Light · inoperative · Sep 16, 2023 · N267WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHK GOOD
- [SDR SWAA2023091398812](https://openairdocs.org/sdr/SWAA2023091398812.md): Light · inoperative · Sep 11, 2023 · N267WN · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF THE REAR ENTRY DOOR INOP<[01] INSTALLED NEW LAMP FOR EXTERIOR EMERGENCY LIGHT AFT OF REAR ENTRY DOOR IAW AMM 33-51-04
- [SDR SWAA2023022105186](https://openairdocs.org/sdr/SWAA2023022105186.md): Handle · broken · Feb 20, 2023 · N267WN · Boeing 7377H4 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR ASSIST HANDLE BROKEN. FWD LAV ASSIST HANDLE MISSING.<[01] SWAPPED FWD ENTRY HANDLE WITH FWD LAV IAW AMM 52-11-31. INSTALLED FWD LAV ASSIST HANDLE PER CMM 25-42-76.
- [SDR SWAA2023012594013](https://openairdocs.org/sdr/SWAA2023012594013.md): Lens · missing · Jan 22, 2023 · N267WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT RIGHT OVER WING EXIT DOOR MISSING LENS. INSTALLED NEW LENS AS PER M/M SIP.
- [SDR SWAA2022121481219](https://openairdocs.org/sdr/SWAA2022121481219.md): Bulb · inoperative · Dec 13, 2022 · N267WN · Boeing 7377H4 · Emergency Lighting
  > FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AFT BULB IS INOP<[01] REPLACED INOP LAMP IN FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED
- [SDR SWAA2022121478970](https://openairdocs.org/sdr/SWAA2022121478970.md): Window Frame · cracked · Dec 6, 2022 · N267WN · Boeing 7377H4 · Fuselage Main, Structure
  > CAPTAIN'S #3 WINDOW FRAME HAS A CRACK EMINATING FROM THE LWR FASTENER HOLE ON THE FWD VERTICAL FASTENER ROW.<[01] REQUEST NDI VERIFICATION OF CRACK;[27] REPAIRED PER SWA EA 22-153-03613.

Next page: https://openairdocs.org/aircraft/N267WN/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 = 'N267WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N267WN/reports

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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.