# Service difficulty reports: N287WN

A list on [N287WN](https://openairdocs.org/aircraft/N287WN.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 · 245 reports

- [SDR SWAA2026073028065](https://openairdocs.org/sdr/SWAA2026073028065.md): Cover · broken · Jul 27, 2026 · N287WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT ROW LIGHT COVER LEFT SIDE BROKEN. R & R LT EX. ROW LIGHT ASSY IAW MM 33-51-01, OPS CHECK NORMAL.
- [SDR SWAA2026061510784](https://openairdocs.org/sdr/SWAA2026061510784.md): Balance Weight · corroded · Jun 10, 2026 · N287WN · Boeing 7377H4 · Rudder Miscellaneous Structure
  > RUDDER COUNTER BALANCE WEIGHT CORRODED AND ERODED. REPLACED THE RUDDER BALANCE WEIGHT IAW CMM 55-40-09.
- [SDR SWAA2026061010781](https://openairdocs.org/sdr/SWAA2026061010781.md): Battery Pack · no test · Jun 10, 2026 · N287WN · Boeing 7377H4 · Emergency Lighting
  > AFT EMERGENCY EXIT BATTERY PACK M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2026033083158](https://openairdocs.org/sdr/SWAA2026033083158.md): Extinguisher · low pressure · Mar 25, 2026 · N287WN · Boeing 7377H4 · Fire Bottle, Portable
  > COCKPIT FIRE EXTINGUISHER PRESSURE BELOW LIMITS<[01] R/R COCKPIT FIRE EXT. IAW AMM 26-26-01
- [SDR SWAA2025110430971](https://openairdocs.org/sdr/SWAA2025110430971.md): Girt Bar · out of adjust · Nov 1, 2025 · N287WN · Boeing 7377H4 · Emergency Equipment
  > GIRT BAR ON L1 DOOR HARD TO GET ON AND OFF CLIPS. RESECURED GIRT BAR ON L1 DOOR PER AMM 25-66-01.
- [SDR SWAA2025103030144](https://openairdocs.org/sdr/SWAA2025103030144.md): Girt Bar · unsecure · Oct 29, 2025 · N287WN · Boeing 7377H4 · Emergency Equipment
  > FAS REPORT L1 DOOR LEFT SIDE SLIDE GIRT BAR IS LOOSE. SECURED THE GIRT BAR TO CLIP IAW AMM 25-66-01. OPS CHKD GOOD.
- [SDR SWAA2025040220175](https://openairdocs.org/sdr/SWAA2025040220175.md): Handle · loose · Mar 31, 2025 · N287WN · Boeing 7377H4 · Passenger/Crew Doors
  > FLT ATT ASSIST HANDLE AFT OF L1 DOOR IS LOOSE 2025-168124 <[01]. CORRECTED INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5); [02] INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5).
- [SDR SWAA2025040219535](https://openairdocs.org/sdr/SWAA2025040219535.md): Support · corroded · Mar 29, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FAULT RAISED TO CAPTURE MANDATORY MEASUREMENT OF CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT ADDING RII LABOR ROW REMOVED BY ERROR ON FAULT TTG8Q00Z1GCE <[01]. REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 W
- [SDR SWAA2025040704750](https://openairdocs.org/sdr/SWAA2025040704750.md): Seat Track · cracked · Mar 12, 2025 · N287WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072<[01] REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. O
- [SDR SWAA2025040414253](https://openairdocs.org/sdr/SWAA2025040414253.md): Seat Track · cracked · Mar 12, 2025 · N287WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072 <[01]. REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LO
- [SDR SWAA2025040702662](https://openairdocs.org/sdr/SWAA2025040702662.md): Skin · corroded · Mar 6, 2025 · N287WN · Boeing 7377H4 · Wing, Plate/Skin
  > CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032<[01] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[02] TOOL USED ON STEP 5:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D
- [SDR SWAA2025040214240](https://openairdocs.org/sdr/SWAA2025040214240.md): Skin · corroded · Mar 6, 2025 · N287WN · Boeing 7377H4 · Wing, Plate/Skin
  > CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032 <[01]. TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [02] TOOL USED ON STEP 5: EDDY CURRENT FLAW DETECTOR P/N:NORTE
- [SDR SWAA2025040202312](https://openairdocs.org/sdr/SWAA2025040202312.md): Bracket · cracked · Mar 5, 2025 · N287WN · Boeing 7377H4 · Wing, Center Box
  > CRACK ON BRACKET STRUCTURE WING CENTER SECTION LOCATED BS540 AND BS578 AT LEVEL BL6 KEEL BEAM 2025-168021<[01]. REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.
- [SDR SWAA2025040202176](https://openairdocs.org/sdr/SWAA2025040202176.md): Plate · cracked · Mar 4, 2025 · N287WN · Boeing 7377H4 · Wing, Control Surfaces
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2025-168012 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMA
- [SDR SWAA2025040201604](https://openairdocs.org/sdr/SWAA2025040201604.md): Support · corroded · Mar 3, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELO
- [SDR SWAA2025040201603](https://openairdocs.org/sdr/SWAA2025040201603.md): Shield · corroded · Mar 3, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31
- [SDR SWAA2025040114234](https://openairdocs.org/sdr/SWAA2025040114234.md): Shield · corroded · Mar 3, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31
- [SDR SWAA2025040114235](https://openairdocs.org/sdr/SWAA2025040114235.md): Support · corroded · Mar 3, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELO
- [SDR SWAA2025040201442](https://openairdocs.org/sdr/SWAA2025040201442.md): Tie Clip · cracked · Mar 2, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN 2025-167974 <[01]. REPLACED NEW TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN IAW B737-700 SRM-51-40-03-0G-O AND DWG-141A1110 SHEET 17 REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [02] CERTIFIED CORRECTIVE
- [SDR SWAA2025040201091](https://openairdocs.org/sdr/SWAA2025040201091.md): Angle · cracked · Mar 1, 2025 · N287WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > CRACK ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-167865<[01] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL
- [SDR SWAA2025040201093](https://openairdocs.org/sdr/SWAA2025040201093.md): Access Panel · cracked · Mar 1, 2025 · N287WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-167870<[01] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL
- [SDR SWAA2025040700756](https://openairdocs.org/sdr/SWAA2025040700756.md): Stub Frame · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697<[01] REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A83
- [SDR SWAA2025040700760](https://openairdocs.org/sdr/SWAA2025040700760.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;
- [SDR SWAA2025040700762](https://openairdocs.org/sdr/SWAA2025040700762.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
- [SDR SWAA2025040700763](https://openairdocs.org/sdr/SWAA2025040700763.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
- [SDR SWAA2025040700922](https://openairdocs.org/sdr/SWAA2025040700922.md): Access Panel · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED H
- [SDR SWAA2025040700752](https://openairdocs.org/sdr/SWAA2025040700752.md): Web · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF
- [SDR SWAA2025040700751](https://openairdocs.org/sdr/SWAA2025040700751.md): Support Angle · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET
- [SDR SWAA2025040700754](https://openairdocs.org/sdr/SWAA2025040700754.md): Angle · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6
- [SDR SWAA2025040200919](https://openairdocs.org/sdr/SWAA2025040200919.md): Scuff Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2025-167749 <[01]. TOOL USED: DIGITAL CALIPER P/N: 8647A42 S/N: B22440130 DUE DATE: 20-SEP-25; [02] STEP 4. TOOL USING RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.; [03] REPAIRED
- [SDR SWAA2025040200761](https://openairdocs.org/sdr/SWAA2025040200761.md): Support · corroded · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA 2025-167730 <[01]. REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL S
- [SDR SWAA2025040214212](https://openairdocs.org/sdr/SWAA2025040214212.md): Stub Frame · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697 <[01]. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A
- [SDR SWAA2025040214217](https://openairdocs.org/sdr/SWAA2025040214217.md): Access Panel · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED H
- [SDR SWAA2025040214210](https://openairdocs.org/sdr/SWAA2025040214210.md): Web · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF
- [SDR SWAA2025040214211](https://openairdocs.org/sdr/SWAA2025040214211.md): Angle · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SL
- [SDR SWAA2025040214209](https://openairdocs.org/sdr/SWAA2025040214209.md): Fitting · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET
- [SDR SWAA2025040114213](https://openairdocs.org/sdr/SWAA2025040114213.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;
- [SDR SWAA2025040114215](https://openairdocs.org/sdr/SWAA2025040114215.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
- [SDR SWAA2025040114214](https://openairdocs.org/sdr/SWAA2025040114214.md): Nut Plate · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
- [SDR SWAA2025040100755](https://openairdocs.org/sdr/SWAA2025040100755.md): Floor Support · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2025-167681<[01] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40
- [SDR SWAA2025040100757](https://openairdocs.org/sdr/SWAA2025040100757.md): Floor Support · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2025-167675<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 S
- [SDR SWAA2025040100758](https://openairdocs.org/sdr/SWAA2025040100758.md): Floor Support · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV 2025-167669<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A54
- [SDR SWAA2025040100759](https://openairdocs.org/sdr/SWAA2025040100759.md): Floor Support · cracked · Feb 28, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV 2025-167671<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A54
- [SDR SWAA2025040700235](https://openairdocs.org/sdr/SWAA2025040700235.md): Stub Frame · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597<[01] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02
- [SDR SWAA2025040700577](https://openairdocs.org/sdr/SWAA2025040700577.md): Angle · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF
- [SDR SWAA2025040700579](https://openairdocs.org/sdr/SWAA2025040700579.md): Angle · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SL
- [SDR SWAA2025040214194](https://openairdocs.org/sdr/SWAA2025040214194.md): Stub Frame · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597 <[01]. REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40
- [SDR SWAA2025040214207](https://openairdocs.org/sdr/SWAA2025040214207.md): Angle · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SL
- [SDR SWAA2025040214206](https://openairdocs.org/sdr/SWAA2025040214206.md): Angle · cracked · Feb 27, 2025 · N287WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF
- [SDR SWAA2025040400226](https://openairdocs.org/sdr/SWAA2025040400226.md): Support Bracket · cracked · Feb 26, 2025 · N287WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 2

Next page: https://openairdocs.org/aircraft/N287WN/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 = 'N287WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N287WN/reports

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