# Service difficulty reports: N273WN

A list on [N273WN](https://openairdocs.org/aircraft/N273WN.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 5 · 248 reports

- [SDR SWAA2026091403252](https://openairdocs.org/sdr/SWAA2026091403252.md): Floor Panel · cracked · Sep 10, 2026 · N273WN · Boeing 7377H4 · Fuselage Floor Panel
  > RAMP REPORTS FORWARD CARGO FLOOR PANEL 120CF HAS CRACKS IN IT._ OK TO CONTINUE PER MEL 25-16-01 SP1B REMOVED CARGO FLOOR PANEL 120CF PER AMM 25-52-10 AND INSTALLED NUTPLATES PER EA M-21-153-00609. SEALANT REQURES CURE TIME. APPLIED CIC AND INSTALLED GEL TAPE P
- [SDR SWAA2026061612168](https://openairdocs.org/sdr/SWAA2026061612168.md): Cover · missing · Jun 13, 2026 · N273WN · Boeing 7377H4 · Emergency Lighting
  > OVERWING EMERGENCY EXIT SIGN MISSING F.O SIDE. INSTALLED MISSING COVER IAW AMM 33-51-01
- [SDR SWAA2026022674574](https://openairdocs.org/sdr/SWAA2026022674574.md): Wedge · delaminated · Feb 26, 2026 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP WEDGE APPEARS TO BE DELAMINATED. VERIFIED NEW REPLACEMENT WEDGE FIT CHECK GOOD IAW SRM 51-40-05. VERIFIED NEW REPLACEMENT WEDGE FIT. INSTALLED NEW FLAP WEDGE IAW AMM 27-51-12.
- [SDR SWAA2026022673942](https://openairdocs.org/sdr/SWAA2026022673942.md): Skin · delaminated · Feb 24, 2026 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP APPEARS TO BE DELAMINATED. C/W EA 26-157-00528
- [SDR SWAA2026012965235](https://openairdocs.org/sdr/SWAA2026012965235.md): Slide · dislodged · Jan 27, 2026 · N273WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY L2 DOOR SLIDE DISLODGED. REMOVED & REPLACED IAW AMM 25-66-01-400-801-NG.
- [SDR SWAA2025063085963](https://openairdocs.org/sdr/SWAA2025063085963.md): Girt Bar · out of adjust · Jun 27, 2025 · N273WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD ENTRY DOOR GRIT BAR DIFFICULT TO INSERT INTO STOWAGE HOOKS<[01] ADJUSTED FWD ENTRY DOOR GIRT BAR PER AMM 25-66-01
- [SDR SWAA2025061782283](https://openairdocs.org/sdr/SWAA2025061782283.md): Fuel Filter · leaking · Jun 16, 2025 · N273WN · Boeing 7377H4 · Fuel Controlling System
  > ENGINE #2 FUEL FILTER BYPASS LIGHT ILLUMINATED ON INITIAL CLIMB OUT; LIGHT EXTINGUISHED AT 9000 FEET. CONTRACT MX WAS DOING A RUN WITH THE CREW TO CHECK OUT THE BYPASS INDICATION IN THE PROCESS FOUND A BAD FUEL LEAK.. LIGHT DIDN'T COME BACK ON BUT WOULD REPLAC
- [SDR SWAA2024111449359](https://openairdocs.org/sdr/SWAA2024111449359.md): Vapor Barrier · cracked · Oct 16, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK VAPOR VARRIER LOCATED BS663.75 LBL47 AND WL168 AT MAIN WHEEL WELL COMPARTME 2024-634568 CRACK VAPOR BARRIER LOCATED BS663.75 LBL47 AND WL168 AT MAIN WHEEL WELL COMPARTME<[01] UT EQUIPMENT USED P/N: EPOCH 650; S/N 190984811; DUE DATE: 11-JAN-25;[02] TOOL
- [SDR SWAA2024111448839](https://openairdocs.org/sdr/SWAA2024111448839.md): Support Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL0 AT PASSENGER CABIN 2024-634544<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET: 92; R
- [SDR SWAA2024111449007](https://openairdocs.org/sdr/SWAA2024111449007.md): Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN BS663 AND LBL42 AT CENTER WING BOX 2024-634540<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25.;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 663 BTW LBL 5 TO LBL 70 AT CENTER WING BOX IAW B
- [SDR SWAA2024111449009](https://openairdocs.org/sdr/SWAA2024111449009.md): Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACK ANGLE LOCATED BETWEEN BS663 AND LBL9 AT CENTER WING BOX 2024-634541<[01] REPLACEMENT ANGLE LOC. BS 663 AND BTW LBL 5 TO LBL 70 AT CENTER WING BOX WAS DOCUMENTED ON FAULT TTG8Q00WFAU7. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACEMENT ANGLE LOC. BS 663 AND
- [SDR SWAA2024111448838](https://openairdocs.org/sdr/SWAA2024111448838.md): Support Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-634542<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET 3
- [SDR SWAA2024111448836](https://openairdocs.org/sdr/SWAA2024111448836.md): Support Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-634539<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET 3
- [SDR SWAA2024111448784](https://openairdocs.org/sdr/SWAA2024111448784.md): Support Angle · corroded · Oct 15, 2024 · N273WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT RT WING 2024-634508<[01] REPLACED SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG# 115A3700 SHEET 44 AND REV -.;[02] COMPLETED
- [SDR SWAA2024111448785](https://openairdocs.org/sdr/SWAA2024111448785.md): Angle · cracked · Oct 15, 2024 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING 2024-634509<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2930 SHEET: 7 RE
- [SDR SWAA2024111448595](https://openairdocs.org/sdr/SWAA2024111448595.md): Panel · corroded · Oct 14, 2024 · N273WN · Boeing 7377H4 · Leading Edge Devices
  > CORROSION FUEL STATION PANEL LOCATED LEADING EDGE AT LEVEL OF S385 AT RT WING 2024-634505<[01] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON STEP 7 AND EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 8;[02] TASK
- [SDR SWAA2024111448431](https://openairdocs.org/sdr/SWAA2024111448431.md): Angle · cracked · Oct 14, 2024 · N273WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE LOCATED ARM SLAT 7 AT RT WING 2024-634490<[01] REPLACED ANGLE LOCATED ARM SLAT 7 AT RT WING IAW B737-700 SRM-51-10-02; CMM 57-43-02 AND MEASURE CRACK IS L:1.014 INCH. TOOL USE: DIGITAL CALIPER PN: 500-197-30 SN: B23357722 DUE DATE: 28-JAN-25;[02] R
- [SDR SWAA2024111448083](https://openairdocs.org/sdr/SWAA2024111448083.md): Support Angle · corroded · Oct 13, 2024 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > CORROSION SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING 2024-634422<[01] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A3700 SHEET: 43 REV A SEE INDIVID
- [SDR SWAA2024111448081](https://openairdocs.org/sdr/SWAA2024111448081.md): Angle · cracked · Oct 13, 2024 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IRSS271 APROX AT LT WING 2024-634426<[01] REPLACED BLADE XXX IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 186A3005-4 SHEET:2 REV:B AND MEASURES OF CRACK IS:L= 0.176? INCHES TOOL USED
- [SDR SWAA2024111348078](https://openairdocs.org/sdr/SWAA2024111348078.md): Intercostal · cracked · Oct 13, 2024 · N273WN · Boeing 7377H4 · Cargo Compartments
  > CRACK FLOOR STRUCTURE WEB LOCATED BS 947.5 STRINGER 25R AT AFT CARGO COMPARTMENT 2024-634378<[01] REPLACED WEB-INTERCOSTAL AND FASTENER LOCATED BS 927 TO BS 947.5 STRINGER 25R AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; AND D
- [SDR SWAA2024111447725](https://openairdocs.org/sdr/SWAA2024111447725.md): Frame · cracked · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 BETWEEN S-5L T S-6L FWD GALLEY AND LAV 2024-634332<[01] PERFORMED REPAIR ON FRAME BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV IAW EA M-22-153-0124 ?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] CERTIFIED CORRECTIVE ACTION STEP 1
- [SDR SWAA2024111447726](https://openairdocs.org/sdr/SWAA2024111447726.md): Web · cracked · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN 2024-634334<[01] REPLACED WEB-INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AND S-16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 141A8180 SHEET:27 REV:C. SEE INDIVI
- [SDR SWAA2024111447724](https://openairdocs.org/sdr/SWAA2024111447724.md): Angle · cracked · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ANGLE LOCATED BS 291.5 TO BS 294.5 AND S-17R AT FWD GALLEY AREA 2024-634333<[01] REPLACED ANGLE (CLIP) LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02-0G; SRM-51-10-02-0G-0 Ï¿½TEM 9 AND DWG:141A8310 SHEET:25 REV
- [SDR SWAA2024111447921](https://openairdocs.org/sdr/SWAA2024111447921.md): Strap · corroded · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ON STRAP LOCATED BETWEEN BS 787 AND BS 793.5; STRINGER 25; WL 156 AFT CARGO COMPARTMENT 2024-634339<[01] TOOL USED: MULTIMETER P/N: FLUKE-289 S/N:61180136 DUE DATE: 10-JUL-25; TOOL USED: THERMOMETER P/N: FLUKE 566 S/N: 65900104WS DUE DATE: 17-OCT-25
- [SDR SWAA2024111447922](https://openairdocs.org/sdr/SWAA2024111447922.md): Angle · corroded · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT 2024-634340<[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 14
- [SDR SWAA2024111447923](https://openairdocs.org/sdr/SWAA2024111447923.md): Support · corroded · Oct 12, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B AND BS 727D STRINGER 25L WL 156 AFT CARGO COMPARTMENT 2024-634341<[01] REPLACED SUPPORT ZEE; [2] SPLICE SIDE PLATE (3 E/A) AND FASTENERS LOCATED BETWEEN BS 727 TO BS 847 STRINGER 25L WL 156 AFT CARGO COMPARTMENT IA
- [SDR SWAA2024111347920](https://openairdocs.org/sdr/SWAA2024111347920.md): Web · corroded · Oct 12, 2024 · N273WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R AFT CARGO COMPARTMENT 2024-634338 CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 787 STRINGER 25R WL 155.5 AFT CARGO COMPARTMENT<[01] REPLACED WEB - INTERCOSTAL AND FASTENER
- [SDR SWAA2024111347630](https://openairdocs.org/sdr/SWAA2024111347630.md): Girt Bar · out of adjust · Oct 12, 2024 · N273WN · Boeing 7377H4 · Escape Slide
  > DETERIORATED HARDWARE ON GIRT BAR FITTING FWD ENTRY AND SERVICE DOOR A T PASSENGER CABIN 2024-634328<[01] REPLACED HARDWARE ON GIRT BAR FITTING FWD ENTRY AND SERVICE DOOR AT PASSENGER CABIN I.A.W B737-700 AMM 25-66-02-400-801 THE INSTALLATION WILL BE DOCUMENTE
- [SDR SWAA2024111447333](https://openairdocs.org/sdr/SWAA2024111447333.md): Scuff Plate · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Cargo Compartments
  > CRACK ON AFT CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT 2024-634300<[01] TOOL USED: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1998072; DUE DATE: 23-JAN-25;[02] REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT IAW BOEING 737
- [SDR SWAA2024111447334](https://openairdocs.org/sdr/SWAA2024111447334.md): Scuff Plate · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Cargo Compartments
  > CRACK ON FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT 2024-634299<[01] TOOL USED: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1998072; DUE DATE: 23-JAN-25;[02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT I. A. W. BOEIN
- [SDR SWAA2024111447516](https://openairdocs.org/sdr/SWAA2024111447516.md): Intercostal · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-634311<[01] REPLACED WEB AND FASTENERS BTW BS 270 TO BS 294.5 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G AND DWG 141A540
- [SDR SWAA2024111447629](https://openairdocs.org/sdr/SWAA2024111447629.md): Vapor Barrier · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 35 AT MAIN WHEEL WELL COMPARTMENT 2024-634324 CRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 35 WL 166 AT MAIN WHEEL WELL COMPARTMENT<[01] TOOL USED SCALE P/N CR5200 S/N 8343110774 DUE DATE 28-FEB-25;[02] TOOL USED HO
- [SDR SWAA2024111447520](https://openairdocs.org/sdr/SWAA2024111447520.md): Angle · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ANGLE LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-634319<[01] REPLACED ANGLE (BRACKET) AND FASTENERS LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G AND DWG: 146A7901 SHEET:66
- [SDR SWAA2024111347517](https://openairdocs.org/sdr/SWAA2024111347517.md): Intercostal · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 13 FWD GALLEY AND LAV 2024-634312 CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 11.05 FWD GALLEY AND LAV<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE AND FAS
- [SDR SWAA2024111347518](https://openairdocs.org/sdr/SWAA2024111347518.md): Web · cracked · Oct 11, 2024 · N273WN · Boeing 7377H4 · Cargo Compartments
  > CRACK WEB LOCATED BS 847 TO BS 867 AND LBL 23 UPPER POSITION AT AFT CARGO COMPARTMENT 2024-634313<[01] REPLACED WEB AND FASTENERS LOCATED BS 847 TO BS 867 AND LBL 23 UPPER POSITION AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG# 149
- [SDR SWAA2024111346252](https://openairdocs.org/sdr/SWAA2024111346252.md): Light · deteriorated · Oct 8, 2024 · N273WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP (10 FT) AT PASSENGER CABIN 2024-634173<[01] REPLACED PHOTOLUMINESCENT STRIP (10 FT) AT PASSENGER CABIN I.A.W SOPM 20-50-12 REV. 56;[02] COMPLETED JOB
- [SDR SWAA2024111446251](https://openairdocs.org/sdr/SWAA2024111446251.md): Flap · debonded · Oct 7, 2024 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING 2024-634151<[01] TOOL USED; CALIPER PN: 8647A42; SN/ A22356048; DUE DATE: 25-JUL-25;[02] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190859705; DU
- [SDR SWAA2024111446250](https://openairdocs.org/sdr/SWAA2024111446250.md): Flap · debonded · Oct 7, 2024 · N273WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING 2024-634150<[01] TOOL USED; CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25-JUL-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 15-FE
- [SDR SWAA2024100344499](https://openairdocs.org/sdr/SWAA2024100344499.md): Overheat Loop · false activation · Oct 1, 2024 · N273WN · Boeing 7377H4 · Detection System
  > WHEEL WELL FIRE WARNIG INDICATION AFTER GEAR RETRACTION ON TAKEOFF<[01] OK TO CONTINUE PER MEL 26-4-01 SP 1 AND SP 3 C/W ATH 216807;[02] REMOVED AND REPLACED WHEEL WELL. OVERHEAT DETECTOR ELEMENT PER AMM 26-18-02
- [SDR SWAA2024090534148](https://openairdocs.org/sdr/SWAA2024090534148.md): Door · cracked · Sep 5, 2024 · N273WN · Boeing 7377H4 · Landing Gear Doors
  > RMLG MIDDLE DOOR CRACKED AT LWR FWD CUTOUT.<[01] OK TO CONTINUE SERVICE PER AUTH# 212644. REMOVED R/H MLG CTR & INNER DOOR. I.A.W. AMM 32-13-11
- [SDR SWAA2024090433095](https://openairdocs.org/sdr/SWAA2024090433095.md): Floor Panel · cracked · Sep 2, 2024 · N273WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 120CF CRACKED<[01] R&R CARGO PANEL PER AMM 25-52-10 AND ATTACHED EA
- [SDR SWAA2024051484690](https://openairdocs.org/sdr/SWAA2024051484690.md): Girt Bar · damaged · May 11, 2024 · N273WN · Boeing 7377H4 · Emergency Equipment
  > CREW REPORTS FWD SERVICE DOOR GIRT BAR (AFT) CLIP IS BENT<[01] STRAIGHTENED OUT FWD SERVICE DOOR GIRT BAR CLIP PER S.I.P.
- [SDR SWAA2024050782990](https://openairdocs.org/sdr/SWAA2024050782990.md): Girt Bar · loose · May 6, 2024 · N273WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR AFT GIRT BAR CLIP IS LOOSE<[01] INSPECTED GIRT BAR AND CLIPS AT FWD SERVICE DOOR IAW AMM 25-66-01. ALL FASTENERS ARE INSTALLED AND GIRT BAR SECURITY IS SATISFACTORY. A/C OK FOR SERVICE.
- [SDR SWAA2024020648522](https://openairdocs.org/sdr/SWAA2024020648522.md): Battery Pack · inoperative · Feb 4, 2024 · N273WN · Boeing 7377H4 · Emergency Lighting
  > L/H EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED EMERG BATTERY PACK<BR>PERFORMED OPS CHECK NO FAULTS NOTED <BR>IN REF TO AMM 33-51-06
- [SDR SWAA2024010837173](https://openairdocs.org/sdr/SWAA2024010837173.md): Panel · cracked · Jan 3, 2024 · N273WN · Boeing 7377H4 · Wing Structure
  > PANEL 621PB CRACKED AT AFT INBD EDGE<[01] REMOVED PANEL 621PB FROM A/C TO FOM;[02] C/W EA 24-157-00026 AS REQ INSTALLED PANEL;[03] C/W
- [SDR SWAA2024010437166](https://openairdocs.org/sdr/SWAA2024010437166.md): Lens · out of adjust · Jan 3, 2024 · N273WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN EMERGENCY EXIT LIGHT NOT SECURE AT 22FED.<[01] SECURED 22FED PASSENGER CABIN EMERGENCY EXIT LIGHT LENS ASSY IN REF AMM 33-51-03.
- [SDR SWAA2023092704653](https://openairdocs.org/sdr/SWAA2023092704653.md): Slide · dislodged · Sep 26, 2023 · N273WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE DISLODGED<[01] RE-PACKED SLIDE IAW AMM MT 725-61-06
- [SDR SWAA2023050131235](https://openairdocs.org/sdr/SWAA2023050131235.md): Battery Pack · inoperative · Apr 25, 2023 · N273WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER AFT SERVICE DOOR AND LAST 4 CABIN LIGHTS CAME ON AND OFF DURING FLIGHT<[01] R&R LEFT AFT EMERG LIGHT BATTER AND CHARGER IRW AMM 33-51-06; OPS TEST GOOD
- [SDR SWAA2023012391039](https://openairdocs.org/sdr/SWAA2023012391039.md): Shield · corroded · Jan 12, 2023 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 787 RBL 21 AND WL 156.5 AT AFT CARGO COMPARTMENT 2022-701136<[01] REPLACED NEW SHIELD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 21 AND WL 156.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 Ï¿½TEM
- [SDR SWAA2023011990269](https://openairdocs.org/sdr/SWAA2023011990269.md): Web · cracked · Jan 10, 2023 · N273WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 500B - 500C, S25 - 26L IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, AND DWG 143A7505, SHEET 81, REV-.

Next page: https://openairdocs.org/aircraft/N273WN/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 = 'N273WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N273WN/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.