# Service difficulty reports: N256WN

A list on [N256WN](https://openairdocs.org/aircraft/N256WN.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 · 263 reports

- [SDR SWAA2026012964986](https://openairdocs.org/sdr/SWAA2026012964986.md): Smoke Detector · false activation · Jan 28, 2026 · N256WN · Boeing 7377H4 · Smoke Detection
  > AFT LAVATORY SMOKE ALARM GOING OFF. NO SMOKE OR FIRE. OK TO CONTINUE IAW MEL 26-16-01 SP 3, & SP1B. R & R THE AFT LAVATORY SMOKE DETECTOR IAW AMM 26-14-01.
- [SDR SWAA2025110631261](https://openairdocs.org/sdr/SWAA2025110631261.md): Light · inoperative · Nov 3, 2025 · N256WN · Boeing 7377H4 · Passenger Compartment Lighting
  > SIDEWALL LIGHTS INOPERATIVE FOLLOWING LOCATIONS: ROW 12 & 18 RH SIDE, ROW 14 LT SIDE. REPLACED THE LAMPS 12 AND 18 DEF AND 14 ABC SIDEWALL LIGHTS IAW AMM 33-21-00.
- [SDR SWAA2025081905554](https://openairdocs.org/sdr/SWAA2025081905554.md): Lens · detached · Aug 17, 2025 · N256WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT FLOOR LEVEL EMERGENCY EXIT LIGHT COVER FELL OFF. REPLACED EMERGENCY EXIT LIGHT LENS AT FLOOR LEVEL IAW AMM 33-51-01.
- [SDR SWAA2025031002775](https://openairdocs.org/sdr/SWAA2025031002775.md): Vapor Barrier · cracked · Mar 7, 2025 · N256WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK IN RIGHT WHEEL WELL VAPOR BARRIER OF 11 INCHES AT STATION RBL 32.0 TO RBL 54.0 <[01] 01. - REMOVED AND REPLACED PER [SRM 57-10-10-1A-2-A00592 (CRACK - STOP DRILL AND SEAL - DVI EVERY 1200 CYC - INTERIM REPAIR)].
- [SDR SWAA2025011787036](https://openairdocs.org/sdr/SWAA2025011787036.md): Sign · detached · Jan 16, 2025 · N256WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT ROW OVERHEAD SIGN DETACHED FROM CEILING.<[01] RESECURED CENTER AISLE EMERGENCY EXIT SIGN REF AMM 33-51-01. AC OK FOR SERVICE
- [SDR SWAA2024121675592](https://openairdocs.org/sdr/SWAA2024121675592.md): Girt Bar · out of adjust · Dec 10, 2024 · N256WN · Boeing 7377H4 · Escape Slide
  > L1 GIRT BAR IS LOOSE IN DISARMED POSITION<[01] ADJUSTED GIRT BAR RETAINER CLIPS ON L1 DOOR IAW AMM 25-66-01. A/C OK FOR SERVICE.
- [SDR SWAA2024103054211](https://openairdocs.org/sdr/SWAA2024103054211.md): Girt Bar · stuck · Oct 28, 2024 · N256WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY GIRT BAR STUCK IN J HOOK<[01] 04 - REPAIRED PER [AMM 25-66-02-201-NG (FLOOR-MOUNTED ESCAPE SLIDE BRACKETS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2024103153980](https://openairdocs.org/sdr/SWAA2024103153980.md): Potable Water · contaminated · Oct 27, 2024 · N256WN · Boeing 7377H4 · Potable Water System
  > POTABLE H2O HAS A STRONG CHEMICAL SMELL. GALLEY & LAV WATER SHUT OFF. POTABLE H2O HAS A STRONG CHEMICAL SMELL.<
- [SDR SWAA2024100936768](https://openairdocs.org/sdr/SWAA2024100936768.md): Web · cracked · Sep 11, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-528896<[01] INSTALLED WEB LOCATED FROM BS 291 TO BS 332.10 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8
- [SDR SWAA2024100936297](https://openairdocs.org/sdr/SWAA2024100936297.md): Support Angle · cracked · Sep 10, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 BL0 AT PASSENGER CABIN 2024-528893<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143
- [SDR SWAA2024100936298](https://openairdocs.org/sdr/SWAA2024100936298.md): Support Angle · cracked · Sep 10, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 RBL 10 AT PASSENGER CABIN 2024-528894<[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 AND SRM 51-40-02 AND DWG 143A5400 SH
- [SDR SWAA2024100936299](https://openairdocs.org/sdr/SWAA2024100936299.md): Support Angle · cracked · Sep 10, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 RBL 41 AT PASSENGER CABIN 2024-528895<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-2 AND DWG 143A5400 SHEE
- [SDR SWAA2024100934986](https://openairdocs.org/sdr/SWAA2024100934986.md): Support Angle · corroded · Sep 6, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION BILGE AREA SUPPORT ANGLE LOCATED AT BS 947.5 BTW STRG 25R AND STRG 25L AT AFT CARGO COMPARTMENT 2024-528883<[01] REPLACED SUPPORT ANGLE LOCATED AT BS 947.5 BTW STRG 25R AND STRG 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH:9 AND S
- [SDR SWAA2024100934266](https://openairdocs.org/sdr/SWAA2024100934266.md): Floor Support · cracked · Sep 4, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK STA 540 BL 0 TO RBL 24.75 2024-528872<[01] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO RBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½
- [SDR SWAA2024100934267](https://openairdocs.org/sdr/SWAA2024100934267.md): Floor Support · cracked · Sep 4, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK STA 540 BL 0 TO LBL 24.75 2024-528873<[01] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO LBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½
- [SDR SWAA2024100933292](https://openairdocs.org/sdr/SWAA2024100933292.md): Rib · cracked · Sep 2, 2024 · N256WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON RIB 151.75 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER 2024-528854<[01] REPLACED RIB 151.75 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER I.A.W B737-700 DWG 186A1001 SHEET 10 REV. A SRM 51-40-02-0G-0. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] REPLACED R
- [SDR SWAA2024100932829](https://openairdocs.org/sdr/SWAA2024100932829.md): Bracket · elongated · Sep 1, 2024 · N256WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ON BRACKET ACCESS PANEL 651GB TRAILING EDGE AT RT WING 2024-528847<[01] REPLACED BRACKET LOCATED ON ACCESS PANEL 651GB TRAILING EDGE AT RT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 115A2714 SHEET: 8 REV: -;[02]
- [SDR SWAA2024100932832](https://openairdocs.org/sdr/SWAA2024100932832.md): Angle · cracked · Sep 1, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA 663.75 LBL54.21 AT AIR CONDITIONING BAY 2024-528851<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25;[02]
- [SDR SWAA2024100944022](https://openairdocs.org/sdr/SWAA2024100944022.md): Bracket · corroded · Aug 31, 2024 · N256WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION ON BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS144 AT LT WING (2E/A) 2024-528820<[01] REPLACED BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS 144 AT LT WING (2 E/A). IAW B737-700 AMM AMM 28-22-41-400-801.;[02] CORRECTED STEP 1.<BR>REPLA
- [SDR SWAA2024100932826](https://openairdocs.org/sdr/SWAA2024100932826.md): Web · cracked · Aug 31, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2024-528790<[01] REPLACED WEB AND FASTENERS LOC. BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 141A8180 SHEET 27;28
- [SDR SWAA2024100932519](https://openairdocs.org/sdr/SWAA2024100932519.md): Stub Frame · broken · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > BROKEN STUB FRAME LOWER AREA ON BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528710<[01] TOOL USED ON STEP 6 AND 7:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] PERFORMED REPAIR ON STUB FRAME LOWER AREA ON BS 294.5 AT
- [SDR SWAA2024100932517](https://openairdocs.org/sdr/SWAA2024100932517.md): Support Angle · broken · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > BROKEN ANGLE - SUPPORT BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528709<[01] REMOVED AND DISCARDED ANGLE SUPPORT(CLIP) 141A8312-3 IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.B DUE TO STUB FRAME REPAIR. SEE TTG8Q00VKGYW.<BR>SEE I
- [SDR SWAA2024100932518](https://openairdocs.org/sdr/SWAA2024100932518.md): Tie Clip · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP ON BS 270 AT STR 10R AT PASSENGER CABIN 2024-528708 CRACK TIE CLIP ON BS 277 AT STR 10R AT PASSENGER CABIN<[01] REPLACED TIE CLIP AND FASTENERS LOCATED ON BS 277 AT STRINGER 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 SRM 5
- [SDR SWAA2024100932520](https://openairdocs.org/sdr/SWAA2024100932520.md): Frame · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-528711<[01] PERFORMED TRIM OUT ON FRAME LOCATED AT BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE INDIVIDUAL SIGNOFFS BELOW;[02] PERFORMED TRIM OUT ON FRAME LOCATED AT
- [SDR SWAA2024100932808](https://openairdocs.org/sdr/SWAA2024100932808.md): Tee Angle · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING 2024-528751<[01] REPLACED T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG: 115A3700 SHEET:3 REV: B. MEASURED CRACK IS L: 2.221? TOOL U
- [SDR SWAA2024100932809](https://openairdocs.org/sdr/SWAA2024100932809.md): Angle · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK T-ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING 2024-528756<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. MEASURED CRACK IS L: 0.832? TOOL USED CALIPER P/N: 500-197-
- [SDR SWAA2024100932806](https://openairdocs.org/sdr/SWAA2024100932806.md): Angle · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS287 AT RT WING 2024-528748<[01] REPLACED ANGLE TRAILING EDGE AND FASTENERS LOCATED AT LEVEL ORSS287 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A3712 SHEET 7 REV. A. SEE INDIVIDUAL SIGN OF
- [SDR SWAA2024100932801](https://openairdocs.org/sdr/SWAA2024100932801.md): Bracket · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATE BS540 AND RBL7 AT CENTER WING BOX 2024-528723<[01] OK TO INSTALL NEW BRACKET AND FASTENERS LOCATED BS 540 AND RBL 7 CENTER WING BOX;[02] CORRECTED STEP 1<BR>INSTALLED NEW SUPPORT BRACKET LOCATE BS540 AND RBL7 AT CENTER WING BOX AND
- [SDR SWAA2024100932802](https://openairdocs.org/sdr/SWAA2024100932802.md): Bracket · cracked · Aug 30, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX 2024-528725<[01] OK TO INSTALL NEW BRACKET AND FASTENERS BS 540 AND LBL 7 CENTER WING BOX;[02] CORRECTED STEP 1<BR>INSTALLED NEW SUPPORT BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX AND FASTE
- [SDR SWAA2024100932158](https://openairdocs.org/sdr/SWAA2024100932158.md): Floorbeam · corroded · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA 2024-528652 CORROSION FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA<[01] ET TOOL USED PN: NORTEC 500D; SN:00X12101V022233; DUE DATE: 15-OCT-24<BR><BR>UT TOOL US
- [SDR SWAA2024100931978](https://openairdocs.org/sdr/SWAA2024100931978.md): Web · cracked · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB BTW BS 312 TO BS 328 AT RBL 31 AT FWD GALLEY AREA 2024-528618<[01] REPLACED WEB AND FASTENERS BTW BS 312 TO BS 328 AT RBL 31 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:39 REV:-. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLE
- [SDR SWAA2024100931981](https://openairdocs.org/sdr/SWAA2024100931981.md): Web · cracked · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB BTW BS 270 TO BS 294.5 AT BL 0 AT FWD GALLEY AREA 2024-528620<[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 AND DWG 141A5400 SHEET:20 REV:-. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLE
- [SDR SWAA2024100931980](https://openairdocs.org/sdr/SWAA2024100931980.md): Floor Support · corroded · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE STIFFENER LOCATED BTW BS 294.5 TO BS 312 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA 2024-528619<[01] REPLACED FLOOR STRUCTURE INTERCOSTAL; HARD POINT (1E/A) AND FASTENERS LOCATED BTW BS 294.5 TO BS 312 AT LEVEL STR 17L AND LBL 13
- [SDR SWAA2024100932156](https://openairdocs.org/sdr/SWAA2024100932156.md): Web · cracked · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA 2024-528623<[01] REPLACED WEB AND FASTENERS BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:32 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AN
- [SDR SWAA2024100931979](https://openairdocs.org/sdr/SWAA2024100931979.md): Stiffener · corroded · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE STIFFENER LOCATED BTW BS 263 TO BS 270 AT LEVEL STR 17L AND LBL 12 AT FWD GALLEY AREA 2024-528621<[01] REPLACED STIFFENER LOCATED BETWEEN BS 263 TO BS 270 AT LEVEL STRINGER 17L AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;
- [SDR SWAA2024100932157](https://openairdocs.org/sdr/SWAA2024100932157.md): Support Angle · corroded · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE Z ANGLE BTW BS 312 TO BS 344 AT LEVEL STR 17L AND LBL 60 AT FWD GALLEY AREA 2024-528649<[01] REPLACED Z ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE AREA BETWEEN BS 312 TO BS 344 AT LEVEL STR 17L AND LBL 60 AT FWD GALLEY IAW BOEING 737
- [SDR SWAA2024100932155](https://openairdocs.org/sdr/SWAA2024100932155.md): Stiffener · corroded · Aug 29, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE STIFFENER BTW BS 312 TO BS 328 AT LEVEL STR 17L AND LBL 12 AT FWD GALLEY AREA 2024-528622<[01] REPLACED STRUCTURE STIFFENER AND FASTENERS LOCATED BETWEEN BS 312 TO BS 328 AT LEVEL STRINGER 17L AND LBL 12 AT FWD GALLEY AREA IAW B737-70
- [SDR SWAA2024100931734](https://openairdocs.org/sdr/SWAA2024100931734.md): Floorbeam · corroded · Aug 28, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED BS986.5 LBL42 WL208.1 AT AFT GALLEY AREA 2024-528596<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 220272512; DUE DATE: 08-JAN-25.;[02] STEP 9 TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:22027
- [SDR SWAA2024100931740](https://openairdocs.org/sdr/SWAA2024100931740.md): Floorbeam · cracked · Aug 28, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM LOCATED BS328 RBL20 AT FWD GALLEY AREA 2024-528603<[01] STEP 7. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 220272712 AND DUE DATE: 28-NOV-24.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:1753759; DUE DATE: 07/DEC/24;[0
- [SDR SWAA2024100931739](https://openairdocs.org/sdr/SWAA2024100931739.md): Floorbeam · corroded · Aug 28, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED BS294.5 BL0 WL208.1 AT FWD GALLEY AREA 2024-528605<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] TOOL
- [SDR SWAA2024100931741](https://openairdocs.org/sdr/SWAA2024100931741.md): Floorbeam · cracked · Aug 28, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM LOCATED BS294.5 RBL53 AT FWD GALLEY AREA 2024-528602<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] TOOL USED ON ST
- [SDR SWAA2024100931737](https://openairdocs.org/sdr/SWAA2024100931737.md): Floorbeam · corroded · Aug 28, 2024 · N256WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED BS986.5 BTW RBL35 TO RBL44 WL208.1 AT AFT GALLEY AREA 2024-528597<[01] TOOL USED ON STEPS 8; 9 AND 10 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] TOOLS USED: POWER PACK P/N: FMK0012180; S/N: PE0423-
- [SDR SWAA2024100931738](https://openairdocs.org/sdr/SWAA2024100931738.md): Rib · cracked · Aug 28, 2024 · N256WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB 120.30 LOCATED AT 28.5 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER 2024-528600<[01] STEPS 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25 AND ELECTRONIC CALIPER P/N: 500-196-30; S/N: A2234
- [SDR SWAA2024100931736](https://openairdocs.org/sdr/SWAA2024100931736.md): Rib · cracked · Aug 28, 2024 · N256WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER 2024-528601<[01] STEPS 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25;[02] CORRECTED STEP 1 TOOL USED EDDY CURRENT EQUIPME
- [SDR SWAA2024100931359](https://openairdocs.org/sdr/SWAA2024100931359.md): Web · corroded · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL21 WL156 AT AFT CARGO COMPARTMENT 2024-528552<[01] REPLACED WEB LOCATED BTW BS747 TO BS767 RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; AND DWG: 146A7500 SHEET:
- [SDR SWAA2024100931356](https://openairdocs.org/sdr/SWAA2024100931356.md): Cargo Track · cracked · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2024-528547<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25;[02] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7;[03]
- [SDR SWAA2024100931358](https://openairdocs.org/sdr/SWAA2024100931358.md): Intercostal · corroded · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS787 RBL7 WL156 AT AFT CARGO COMPARTMENT 2024-528553<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 767 TO BS 787 RBL 7; WL 156 AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 7
- [SDR SWAA2024100931357](https://openairdocs.org/sdr/SWAA2024100931357.md): Web · corroded · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW BS767 TO BS794.3 RBL 21 WL156 AT AFT CARGO COMPARTMENT 2024-528554<[01] REPLACED WEB LOCATED BTW BS767 TO BS794.3 RBL 21 WL156 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 146A0081 S
- [SDR SWAA2024100931128](https://openairdocs.org/sdr/SWAA2024100931128.md): Angle · cracked · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS 400 LBL24 FWD CARGO COMPARTMENT 2024-528526<[01] REPLACED ANGLE - CLIP LOCATED BS 400 LBL24 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 143A7505 SHEET 81 REV -. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] TASK COMPLETED <BR>SE
- [SDR SWAA2024100931131](https://openairdocs.org/sdr/SWAA2024100931131.md): Angle · cracked · Aug 27, 2024 · N256WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT 2024-528533<[01] ANGLE-CLIP AND FASTENERS LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT IAW B737-700 DWG:143A7505 SHEET:82 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9. SEE

Next page: https://openairdocs.org/aircraft/N256WN/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 = 'N256WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N256WN/reports

---
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.