# Service difficulty reports: N274WN

A list on [N274WN](https://openairdocs.org/aircraft/N274WN.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 SWAA2026100569536](https://openairdocs.org/sdr/SWAA2026100569536.md): Lens · missing · Sep 30, 2026 · N274WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY AISLE LIGHT AT SEAT 25DEF LENS MISSING. REPLACED EMERGENCY AISLE AREA LIGHT LENS AT 25DEF IAW AMM 33-51-03.
- [SDR SWAA2026092488845](https://openairdocs.org/sdr/SWAA2026092488845.md): Floor Panel · cracked · Sep 20, 2026 · N274WN · Boeing 7377H4 · Fuselage Floor Panel
  > RAMP REPORTS HOLE IN FWD CARGO FLOOR FOUND 4IN LONG CRACK ON FLOOR PANEL 120CF. REPAIRED PANEL IAW AMM 25-52-01.
- [SDR SWAA2026040987682](https://openairdocs.org/sdr/SWAA2026040987682.md): Battery Pack · failed · Apr 9, 2026 · N274WN · Boeing 7377H4 · Emergency Lighting
  > THE EMERGENCY LIGHTING BATTERY PACK AT THE R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2026040987681](https://openairdocs.org/sdr/SWAA2026040987681.md): Battery Pack · failed · Apr 9, 2026 · N274WN · Boeing 7377H4 · Emergency Lighting
  > AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2026040786322](https://openairdocs.org/sdr/SWAA2026040786322.md): Slide · out of adjust · Apr 3, 2026 · N274WN · Boeing 7377H4 · Escape Slide
  > L2 ENTRY DOOR SLIDE FELL OUT. SLIDE DID NOT DEPLOY. RE-INSTALLED L2 DOOR SLIDE IN SLIDE COMPARTMENT PER MT 725-61-06. A/C OK FOR SERVICE.
- [SDR SWAA2026040183389](https://openairdocs.org/sdr/SWAA2026040183389.md): Stringer Clip · corroded · Mar 25, 2026 · N274WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON INBD AND OTBD STRINGER CLIPS AT BS 767, STRINGER 27R. REMOVED AND REPLACED THE STRINGER CLIPS IAW SRM 51-40-02-0G AND DRAWING 146A7810, REV A.
- [SDR SWAA2026040185367](https://openairdocs.org/sdr/SWAA2026040185367.md): Stringer Clip · corroded · Mar 25, 2026 · N274WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON INBD AND OTBD STRINGER CLIPS, BS 767 STRINGER 27R. REMOVED AND REPLACED THE STRINGER CLIPS IAW SRM 51-40-02-0G AND DRAWING 146A7810, REV A.
- [SDR SWAA2026021370109](https://openairdocs.org/sdr/SWAA2026021370109.md): Floor Panel · cracked · Feb 12, 2026 · N274WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO METAL FLOOR HAS CRACK IN IT. REMOVED AND REPLACED FWD CARGO METAL FLOOR PANEL IAW AMM 25-52-10, M-22-125-02597, & M-21-125-00819.
- [SDR SWAA2025112037094](https://openairdocs.org/sdr/SWAA2025112037094.md): Battery Pack · inoperative · Nov 20, 2025 · N274WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS OUT MID CABIN. R & R BATTERY PACK AND CHARGER NEAR LT EMERGENCY WINDOW IAW AMM 33-51-06, OPS CHECKED GOOD.
- [SDR SWAA2025071791302](https://openairdocs.org/sdr/SWAA2025071791302.md): Bulb · inoperative · Jul 15, 2025 · N274WN · Boeing 7377H4 · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED R2 DOOR EMERGENCY LIGHT BULB IAW AMM 33-51-04.
- [SDR SWAA2025060376725](https://openairdocs.org/sdr/SWAA2025060376725.md): Lamp · inoperative · May 31, 2025 · N274WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVER WING EMERGENCY LIGHT INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)].
- [SDR SWAA2025030601797](https://openairdocs.org/sdr/SWAA2025030601797.md): Battery Pack · no test · Mar 4, 2025 · N274WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN AND LIGHTS ABOVE THE AFT SERVICE DOOR WILL NOT ILLUMINATE.<[01] PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)] OPS CHECK SATISFACTORY.
- [SDR SWAA2024121261611](https://openairdocs.org/sdr/SWAA2024121261611.md): Web · cracked · Nov 20, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED ON BS337.2 AT LBL6.74 WL 153.5 APPROX 2024-685624<[01] REPLACED WEB LOCATED ON BS323.7 TO BS348.2 LBL6.74 WL 153.5 IAW B737-700 SRM 51-40-02-0G-0 DWG 141A8511; SHEET 11; REV ? AND DWG 141A0650; SHEET 167; REV A. SEE INDIVIDUAL SIGN OFF BEL
- [SDR SWAA2024120958680](https://openairdocs.org/sdr/SWAA2024120958680.md): Web · cracked · Nov 11, 2024 · N274WN · Boeing 7377H4 · Cargo Compartments
  > CRACK WEB - INTERCOSTAL LOCATED ON BS747 TO B767 BTW STR25R AT AFT CARGO COMPARTMENT 2024-685606<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED ON BS747 TO B767 BTW STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; DRAWING 146A7500 SH
- [SDR SWAA2024121057750](https://openairdocs.org/sdr/SWAA2024121057750.md): Plate · cracked · Nov 7, 2024 · N274WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK REAR SPAR CORRUGATED PLATE LOCATED ON IRSS 216 AT LT WING 2024-685546<[01] REPLACED CORRUGATED PLATE LOCATED ON REAR SPAR IRSS 216 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED CORRUGAT
- [SDR SWAA2024121057751](https://openairdocs.org/sdr/SWAA2024121057751.md): Plate · cracked · Nov 7, 2024 · N274WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING 2024-685547<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED I
- [SDR SWAA2024121057596](https://openairdocs.org/sdr/SWAA2024121057596.md): Angle · cracked · Nov 7, 2024 · N274WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE SLAT 6 LOCATED SLAT STATION 176 AT RT WING 2024-685545<[01] REPLACED ANGLE LOCATED ON SLAT 6 SLAT STATION 176 AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 114A5030 SHEET 14 REV B.SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED ON SLA
- [SDR SWAA2024121057079](https://openairdocs.org/sdr/SWAA2024121057079.md): Bracket · cracked · Nov 6, 2024 · N274WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK TRAILING EDGE BRACKET LOCATED DEFLECTION CONTROL RIB AREA ORSS 274 AT LT WING 2024-685535<[01] REPLACED BRACKET LOCATED ON TRAILING EDGE DEFLECTION CONTROL RIB AREA ORSS 274 AT LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0.;[02] REP
- [SDR SWAA2024121056919](https://openairdocs.org/sdr/SWAA2024121056919.md): Bracket · cracked · Nov 5, 2024 · N274WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK BODY STATION 540 LBL 7 BRACKET AT AIR CONDITIONING BAY 2024-685477<[01] REPLACED BRACKET LOCATED STATION 540 LBL 7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G.;[02] REPLACED BRACKET LOCATED STATION 540 LBL 7 AT AIR CONDITIONING BAY IAW B737-700
- [SDR SWAA2024121056920](https://openairdocs.org/sdr/SWAA2024121056920.md): Bracket · cracked · Nov 5, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BODY STATION 540 BRACKET LOCATED RBL 7 AT AIR CONDITIONING BAY 2024-685478<[01] REPLACED BRACKET LOCATED STATION 540 RBL 7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G.;[02] REPLACED BRACKET LOCATED STATION 540 RBL 7 AT AIR CONDITIONING BAY IAW B
- [SDR SWAA2024121256243](https://openairdocs.org/sdr/SWAA2024121256243.md): Web · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BTW BS344 TO BS360 BL0 AT FWD GALLEY AREA 2024-685359<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS344 TO BS360 BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND B737-700 DWG 141A5400 SHEET 32 REV ?.SEE INDIVIDUAL SIGN-OFF BELOW;[02]
- [SDR SWAA2024121055911](https://openairdocs.org/sdr/SWAA2024121055911.md): Strip · deteriorated · Nov 3, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHPTOLUMINESCENT STRIP LT AND RT SIDE ALONG PASSENGER CABIN 2024-685353<[01] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE ALONG PASSENGER CABIN IAW B737-700 AMM 33-51-15-000-802 AND AMM 33-51-15-400-802; DWG NO.33500007 SHEET 2 REV. R;[02] REPLA
- [SDR SWAA2024121056242](https://openairdocs.org/sdr/SWAA2024121056242.md): Web · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB LOCATED BTW BS344 TO BS360 LBL12 AT FWD GALLEY AREA 2024-685358<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS344 TO BS360 LBL12 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 46 REV A.<BR>SEE INDIV
- [SDR SWAA2024121056244](https://openairdocs.org/sdr/SWAA2024121056244.md): Web · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB LOCATED BTW BS344 TO BS360 RBL34 AT FWD GALLEY AREA 2024-685360<[01] TOOL USED CALIPER P/N: 500-752-20; S/N:B21014945; DUE DATE:04-DEC-24;[02] REPLACED WEB LOCATED BTW BS344 TO BS360 RBL34 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400
- [SDR SWAA2024121056246](https://openairdocs.org/sdr/SWAA2024121056246.md): Door · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR17L AT FWD GALLEY AREA 2024-685361<[01] REPLACED INNER CHORD LOCATED BTW BS270 AND BS360 AT LEVEL STR17L AND LBL 54 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02; DWG 141A8110; SHE
- [SDR SWAA2024121056245](https://openairdocs.org/sdr/SWAA2024121056245.md): Floorbeam · corroded · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED BS328 RBL45.50 WL 208.1 AT FWD GALLEY AREA 2024-685355<[01] TOOL USED STEP 10: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 11 JUN 25.;[02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED BS328 BETWEEN LBL7
- [SDR SWAA2024121056241](https://openairdocs.org/sdr/SWAA2024121056241.md): Web · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB LOCATED BTW BS 328 TO BS344 LBL 46 AT FWD GALLEY AREA 2024-685357<[01] TOOL USED CALIPER P/N: 500-752-20; S/N:B21014945; DUE DATE:04-DEC-24;[02] REPLACED WEB AND FASTENERS LOCATED BTW BS 328 TO BS344 LBL 46 AT FWD GALLEY AREA. I.A.W. B737-700 SRM 51-
- [SDR SWAA2024121056323](https://openairdocs.org/sdr/SWAA2024121056323.md): Frame · cracked · Nov 3, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 LOCATED BTW STR5L TO STR6L FWD GALLEY AND LAV 2024-685371<[01] PERFORMED REPAIR ON FRAME LOCATED STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN IAW EA M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] PERFORMED REPAIR ON FRAME LOC
- [SDR SWAA2024121255907](https://openairdocs.org/sdr/SWAA2024121255907.md): Support Angle · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2024-685335<[01] STEP 4 TOOL USED: ULTRASONIC THICKNESS GAGE; P/N:45MG; S/N:130066701; DUE DATE: 12-JUL-25.;[02] FAULT RESOLVED ON OTHER FAULT.<BR>REPLACED SUPPORT ZEE L
- [SDR SWAA2024121055903](https://openairdocs.org/sdr/SWAA2024121055903.md): Fitting · deteriorated · Nov 2, 2024 · N274WN · Boeing 7377H4 · Escape Slide
  > DETERIORATED HARDWARE GIRT BAR FITTINGS AT AFT ENTRY DOOR (4EA) 2024-685278<[01] REPLACED HARDWARE GIRT BAR FITTINGS AT AFT ENTRY DOOR (4EA) IAW B737-700 AMM 25-66-02-400-801 STEP 3.A. THRU 3.D.(1)(G);[02] REPLACED HARDWARE GIRT BAR FITTINGS AT AFT ENTRY DOOR
- [SDR SWAA2024121055902](https://openairdocs.org/sdr/SWAA2024121055902.md): Nut · deteriorated · Nov 2, 2024 · N274WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED NUT ON ASSIST HANDLE AT AFT LINING ENTRY DOOR (2EA) 2024-685276<[01] REPLACED NUT ON ASSIST HANDLE AT AFT LINING ENTRY DOOR (2EA IAW BOEING SOPM 20-50-01 REV.38;[02] REPLACED NUT ON ASSIST HANDLE AT AFT LINING ENTRY DOOR (2EA IAW BOEING SOPM 20-50
- [SDR SWAA2024121055901](https://openairdocs.org/sdr/SWAA2024121055901.md): Nut · deteriorated · Nov 2, 2024 · N274WN · Boeing 7377H4 · Galley Doors
  > DETERIORATED NUT ON ASSIST HANDLE AT AFT SERVICE LINING DOOR (2EA) 2024-685275<[01] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE LINING DOOR (2EA) IAW BOEING SOPM 20-50-01 REV.38;[02] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE LINING DOOR (2EA) IAW BOEING SO
- [SDR SWAA2024121055895](https://openairdocs.org/sdr/SWAA2024121055895.md): Angle · cracked · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500B RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-685261<[01] REPLACED ANGLE-CLIP LOCATED BS500B RBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505; SHEET 82; REV -. SEE INDIVIDUAL SINGS-OFF BELOW;
- [SDR SWAA2024121055906](https://openairdocs.org/sdr/SWAA2024121055906.md): Support · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727C TO BS727E WL156 AND RBL21 AFT CARGO COMPARTMENT 2024-685334<[01] STEP 4 TOOL USED: ULTRASONIC THICKNESS GAGE; P/N:45MG; S/N:130066701; DUE DATE: 12-JUL-25.;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED ON BS727 TO
- [SDR SWAA2024121055908](https://openairdocs.org/sdr/SWAA2024121055908.md): Support · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727B TO BS727D WL156 AND LBL21 AFT CARGO COMPARTMENT 2024-685336<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130064101; DUE DATE: 13 DEC 24.;[02] FAULT WAS RESOLVED ON ANOTHER FAULT<BR>REPLACED SUPPORT ZEE
- [SDR SWAA2024121055909](https://openairdocs.org/sdr/SWAA2024121055909.md): Support · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727D TO BS747 WL156 AND LBL21 AFT CARGO COMPARTMENT 2024-685337<[01] TOOL USED ON STEP 4 ULTRASONIC THICKNESS GAUGE P/N 45MG; S/N 221860711 DUE DATE 21-NOV-24;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 WL156 AND
- [SDR SWAA2024121055910](https://openairdocs.org/sdr/SWAA2024121055910.md): Support · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS747 TO BS807 WL156 AND LBL21 AFT CARGO COMPARTMENT 2024-685338<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130064101; DUE DATE: 13 DEC 24.;[02] FAULT WAS RESOLVED ON ANOTHER FAULT<BR>REPLACED SUPPORT ZEE LO
- [SDR SWAA2024121055896](https://openairdocs.org/sdr/SWAA2024121055896.md): Structure · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE PLATE LOCATED BTW BS1016 WL208.1 AND LBL3 AT AFT GALLEY AREA 2024-685266<[01] REPLACED PLATE LOCATED ON FLOOR STRUCTURE BTW BS1016 WL208.1 AND LBL3 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 147
- [SDR SWAA2024121055897](https://openairdocs.org/sdr/SWAA2024121055897.md): Floorbeam · corroded · Nov 2, 2024 · N274WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM STRUCTURE LOCATED BS986.3 WL208.1 AND LBL43 AT AFT GALLEY AREA 2024-685267<[01] TOOL USED STEP 6 ULTRASONIC THICKNESS GAGE PN: 45MG SN: 130064101; DUE DATE: 13-DEC-24;[02] ON STEP 9: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN:
- [SDR SWAA2024120955890](https://openairdocs.org/sdr/SWAA2024120955890.md): Web · cracked · Nov 1, 2024 · N274WN · Boeing 7377H4 · Cargo Compartments
  > CRACK ON WEB LOCATED BTW BS847 TO BS867 AND LBL23 UPPER POSITION AT AFT CARGO COMPARTMENT 2024-685230<[01] REPLACED WEB LOCATED BTW BS847 TO BS867 AND LBL23 UPPER POSITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8100 SHEET 1 REV -.;[02]
- [SDR SWAA2024121055563](https://openairdocs.org/sdr/SWAA2024121055563.md): Scuff Plate · cracked · Oct 31, 2024 · N274WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACK ON AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2024-685202<[01] TOOL USED STEP 4 PHOTOMETER RADIOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 07-DEC-24;[02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH BOEING 737-700 SRM
- [SDR SWAA2024121055106](https://openairdocs.org/sdr/SWAA2024121055106.md): Panel · debonded · Oct 30, 2024 · N274WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING. 2024-685138<[01] STEP 3 TOOL USED ULTRASOUND EQUIPMENT PN: GEIT1480179; SN:GOPLS 15100171; DUE DATE: 07-DEC-24;[02] TOOL USED ON STEP 18: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600. S
- [SDR SWAA2024120954552](https://openairdocs.org/sdr/SWAA2024120954552.md): Floor Panel · cracked · Oct 29, 2024 · N274WN · Boeing 7377H4 · Cargo Compartments
  > CRACK FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2024-685082<[01] FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1F AND DWG 453A2610 SHEET: 4 REV: C MATERIAL USED CONOLITE P/N: A90RG1W P/O:2023-231977;[02] TASK COM
- [SDR SWAA2024102148538](https://openairdocs.org/sdr/SWAA2024102148538.md): Battery Pack · inoperative · Oct 15, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT NEXT TO AFT ENTRY DOOR INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]<BR>REFF. JOB CARD [TTG8Q00WEU3H]. FOR PART.
- [SDR SWAA2024102148531](https://openairdocs.org/sdr/SWAA2024102148531.md): Battery Pack · inoperative · Oct 15, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE AFT SERVICE DOOR INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024080221168](https://openairdocs.org/sdr/SWAA2024080221168.md): Lamp · inoperative · Aug 1, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR AFT ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-04
- [SDR SWAA2024071211729](https://openairdocs.org/sdr/SWAA2024071211729.md): Light · missing · Jul 12, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > MISSING PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT STA 976 ON THE LEFT HAND SIDE<[01] INSTALLED FLOOR PROXIMITY LIGHTING ON THE LEFT HAND SIDE LOCATED AT STATION 976 IAW AMM 33-51-15
- [SDR SWAA2024051485020](https://openairdocs.org/sdr/SWAA2024051485020.md): Bulb · inoperative · May 12, 2024 · N274WN · Boeing 7377H4 · Emergency Lighting
  > RT EMERGENCY EXIT AFT LIGHT ASSEMBLY HAS ONE BULB INOP.<[01] REMOVED AND REPLAMPED (1EA) RT EMERGENCY EXIT AFT LIGHT ASSEMBLY BULB AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023092704868](https://openairdocs.org/sdr/SWAA2023092704868.md): Lens · missing · Sep 27, 2023 · N274WN · Boeing 7377H4 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHT MISSING LENS COVER<[01] REINSTALLED LH OVERWING EXIT LIGHT LENS PER AMM 33-51-01.
- [SDR SWAA2023073183469](https://openairdocs.org/sdr/SWAA2023073183469.md): Attach Bracket · cracked · Jul 29, 2023 · N274WN · Boeing 7377H4 · Wing, Attach Fittings
  > LEFT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] R&R LEFT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET IN REF TO SOPM 20-50-18.

Next page: https://openairdocs.org/aircraft/N274WN/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 = 'N274WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N274WN/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.