# Service difficulty reports: N261WN

A list on [N261WN](https://openairdocs.org/aircraft/N261WN.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 · 241 reports

- [SDR SWAA2026061511326](https://openairdocs.org/sdr/SWAA2026061511326.md): Fire Loop · faulted · Jun 10, 2026 · N261WN · Boeing 7377H4 · Fire Detection
  > NR 2 ENG FIRE LOOP A GIVES FAULT LIGHT. OK TO CONTINUE PER MEL 26-2-01. REMOVED AND REPLACED THE NR 2 ENG FIRE LOOP A UPPER. IAW AMM 26-11-01. OPS CHECKED OK.
- [SDR SWAA2026041488197](https://openairdocs.org/sdr/SWAA2026041488197.md): Floor Panel · cracked · Apr 11, 2026 · N261WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO BIN FLOOR CRACKED. PANEL 140CF 15. OK TO CONTINUE IAW MEL 25-16-01 SP1B AUTH 314501. R & R AFT FLOOR PANEL 140CF IAW AMM25-52-10.
- [SDR SWAA2026010658063](https://openairdocs.org/sdr/SWAA2026010658063.md): Lock · loose · Jan 4, 2026 · N261WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 11D OVER RECLINES INTO EXIT ROW. SECURED RECLINE LOCK IAW CMM 25-21-42. NO FURTHER DEFECTS NOTED FOR SEAT 11D.
- [SDR SWAA2025102025128](https://openairdocs.org/sdr/SWAA2025102025128.md): Battery Pack · no test · Oct 17, 2025 · N261WN · Boeing 7377H4 · Emergency Lighting
  > L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
- [SDR SWAA2025091514592](https://openairdocs.org/sdr/SWAA2025091514592.md): Slide · out of limits · Sep 14, 2025 · N261WN · Boeing 7377H4 · Escape Slide
  > R2 SLIDE OUT OF LIMITS. REMOVED AND REPLACED THE R2 SLIDE IAW AMM 25-60 6-01.
- [SDR SWAA2025063086339](https://openairdocs.org/sdr/SWAA2025063086339.md): Shimmy Dampener · vibration · Jun 27, 2025 · N261WN · Boeing 7377H4 · Main Landing Gear
  > AT ROTATION AIRCRAFT YAWED TO THE LEFT WITH A VIBRATION FELT; AFTER ABEING AIRBORNE NO FLIGHT CONTROL DISCREPANCIES NOTICED; NO ABNORMAL ENGINE PERAMETERS NOTED; RETURNED TO AIRFIELD NORMAL SMOOTH LANDING WITH NO ABNORMAL VIBRATIONS FELT NO OVERWEIGHT LANDING
- [SDR SWAA2025042940304](https://openairdocs.org/sdr/SWAA2025042940304.md): Glowstrip · damaged · Apr 25, 2025 · N261WN · Boeing 7377H4 · Emergency Equipment
  > FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01 SP1<BR>AUTH# 248928;[02] REMOVED AND REPLACED FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP PER SIP
- [SDR SWAA2025030502296](https://openairdocs.org/sdr/SWAA2025030502296.md): Elec Connector · failed · Mar 5, 2025 · N261WN · Boeing 7377H4 · Flight Control System Wiring
  > LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONN
- [SDR SWAA2025030502292](https://openairdocs.org/sdr/SWAA2025030502292.md): Transmitter · failed · Mar 5, 2025 · N261WN · Boeing 7377H4 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONN
- [SDR SWAA2024110656273](https://openairdocs.org/sdr/SWAA2024110656273.md): Light · inoperative · Nov 3, 2024 · N261WN · Boeing 7377H4 · Emergency Lighting
  > FLOOR LIGHTING STRIP SEGMENT INOP. FRONT; FO SIDE ROW 1.<[01] R&R FLOOR LIGHTING STRIP AT ROW 1; FO?S SIDE PER AMM 25-27-31.
- [SDR SWAA2024070910031](https://openairdocs.org/sdr/SWAA2024070910031.md): Battery · faulted · Jul 6, 2024 · N261WN · Boeing 7377H4 · Emergency Lighting
  > POPPED OUT C/B LIGHTING EMER CHGR WHEN TURN THE EMER EXIT LIGHT SWITCH TO OFF POSITION<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY M1673 IAW B737-700 AMM 33-51-06-960-805; TEST IS OK.
- [SDR SWAA2024070809527](https://openairdocs.org/sdr/SWAA2024070809527.md): Slide · out of position · Jul 6, 2024 · N261WN · Boeing 7377H4 · Escape Slide
  > PAX CABIN AFT LEFT ENTRY DOOR SLIDE LOWER COVER IS CHAFFING AGAINST WITH SCUFF PLATE WHEN TO CLOSE THE DOOR 2024-361966<[01] PERFORMED REPOSITION OF SLIDE IN THE SLIDE COMPARTMENT AT AFT ENTRY DOOR I.A.W. B737-700 AMM 25-66-01-400-803 AND MT 725-61-06 (TTG8Q00
- [SDR SWAA2024070806972](https://openairdocs.org/sdr/SWAA2024070806972.md): Scuff Plate · cracked · Jun 28, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA 2024-361946<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A23217720;DUE DATE:14-FEB-25.;[02]. TOOL USED; RADIOMETER/PHOTOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24/JUL/24;[03] REPA
- [SDR SWAA2024070999413](https://openairdocs.org/sdr/SWAA2024070999413.md): Support Bracket · cracked · Jun 7, 2024 · N261WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACK BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM 2024-361808<[01] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND BOEING 737-700 SRM 51-40-02-0G-0 STEP 9;[02] REPLA
- [SDR SWAA2024070999412](https://openairdocs.org/sdr/SWAA2024070999412.md): Support Bracket · cracked · Jun 7, 2024 · N261WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK SLAT 1 AUXILIARY TRACK ON SUPPORT BRACKET LOCATED LEADING EDGE AREA INTERNAL CAVITY AT LT WING 2024-361803<[01] REPLACED SUPPORT BRACKET LOCATED SLAT 1 AUXILIARY TRACK ON LEADING EDGE AREA INTERNAL CAVITY AT LT WING I.A.W. B737-700 SRM 51-40-02-0G-0 AND
- [SDR SWAA2024070899084](https://openairdocs.org/sdr/SWAA2024070899084.md): Fitting · deteriorated · Jun 7, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA 2024-361788<[01] REPLACED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA IAW B737-700- AMM 25-66-02-400-801;[02] JOB COMPLETED
- [SDR SWAA2024070899086](https://openairdocs.org/sdr/SWAA2024070899086.md): Fitting · deteriorated · Jun 7, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY AREA 2024-361792<[01] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY ARE I.A.W B737-700 SOPM-20-50-01;[02] REPLACED HARDWARE GRIT BAR FITTING ON
- [SDR SWAA2024070999077](https://openairdocs.org/sdr/SWAA2024070999077.md): Support · corroded · Jun 6, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS787 WL156 LBL21 AT AFT CARGO COMPARTMENT 2024-361772<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPAIRED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT
- [SDR SWAA2024070999076](https://openairdocs.org/sdr/SWAA2024070999076.md): Support · corroded · Jun 6, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-361770<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21
- [SDR SWAA2024070999074](https://openairdocs.org/sdr/SWAA2024070999074.md): Cargo Track · cracked · Jun 6, 2024 · N261WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 AT LEVEL OF BS 767 AFT CARGO COMPARTMENT 2024-361768<[01] TOOL USED ON STEP 4 AND 5: EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030457 DUE DATE: 15 OCT 24.;[02] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS767 AND WL156 AFT CARGO
- [SDR SWAA2024070999075](https://openairdocs.org/sdr/SWAA2024070999075.md): Cargo Track · cracked · Jun 6, 2024 · N261WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 AT LEVEL OF BS 727E AFT CARGO COMPARTMENT 2024-361771<[01] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 12 INCHES TO BS 767 PLUS 12 INCHES SEE TTG8Q00TT1W8;[02] FAULT WAS RESOLVED ON ANOTHER FAULT DUE
- [SDR SWAA2024070999072](https://openairdocs.org/sdr/SWAA2024070999072.md): Access Panel · cracked · Jun 6, 2024 · N261WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2024-361769<[01] REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND TOOK MEASURE OF CRACK IS L: 0.437 INCH TOOL USED DIGITA
- [SDR SWAA2024070998561](https://openairdocs.org/sdr/SWAA2024070998561.md): Support · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BILGE AREA SUPPORT ZEE LOCATED BETWEEN STA 500B TO STA 500C RH SIDE AT FWD CARGO COMPARTMENT 2024-361692<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500A TO STA 500D RH SIDE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND SRM 51-10-02 PARA
- [SDR SWAA2024070998756](https://openairdocs.org/sdr/SWAA2024070998756.md): Fitting · deteriorated · Jun 5, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA (4EA) 2024-361723<[01] REPLACED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA IAW B737-700 SRM 53-00-50-2
- [SDR SWAA2024070998415](https://openairdocs.org/sdr/SWAA2024070998415.md): Stiffener · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON STIFFENER LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-361678<[01] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1.<BR>REPLACED STIFFENER
- [SDR SWAA2024070898757](https://openairdocs.org/sdr/SWAA2024070898757.md): Scuff Plate · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-361725<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189516;DUE DATE:17-JAN-25.;[02] TOOL USED IN STEP 4: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24-JUL-24.;[03] REPAIRED S
- [SDR SWAA2024070898560](https://openairdocs.org/sdr/SWAA2024070898560.md): Intercostal · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH
- [SDR SWAA2024070810380](https://openairdocs.org/sdr/SWAA2024070810380.md): Intercostal · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH
- [SDR SWAA2024070898565](https://openairdocs.org/sdr/SWAA2024070898565.md): Support Angle · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ENTRY DOOR CUT OUT SUPPORT ANGLE LOCATED AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA 2024-361700<[01] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR CUT OUT AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM
- [SDR SWAA2024070898563](https://openairdocs.org/sdr/SWAA2024070898563.md): Tie Clip · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND
- [SDR SWAA2024070810381](https://openairdocs.org/sdr/SWAA2024070810381.md): Tie Clip · cracked · Jun 5, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND
- [SDR SWAA2024070898411](https://openairdocs.org/sdr/SWAA2024070898411.md): Structure · cracked · Jun 4, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INNER CHORD AT STA 312 AND AT LEVEL S-17L AT FWD GALLEY AREA 2024-361648<[01] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8110 SHEET: 11 REV:-. AND DWG 141A5220 SHEET: 1 R
- [SDR SWAA2024070998038](https://openairdocs.org/sdr/SWAA2024070998038.md): Floorbeam · cracked · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM LOCATED STA 328 RBL 20 AT FWD GALLEY AREA 2024-361601<[01] TOOL USED EDDY CURRENT HIGH FREQUENCY INSPECTION P/N: NORTEC600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DAT
- [SDR SWAA2024070998041](https://openairdocs.org/sdr/SWAA2024070998041.md): Floor Support · cracked · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 AND LBL 45 FWD GALLEY AND LAV 2024-361600<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEI
- [SDR SWAA2024070998043](https://openairdocs.org/sdr/SWAA2024070998043.md): Floorbeam · corroded · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361607<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE D
- [SDR SWAA2024070898045](https://openairdocs.org/sdr/SWAA2024070898045.md): Floorbeam · corroded · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361606<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE D
- [SDR SWAA2024070898042](https://openairdocs.org/sdr/SWAA2024070898042.md): Floor Support · cracked · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV 2024-361603<[01] REPLACED WEB - INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02; SRM 51-10-02
- [SDR SWAA2024070898044](https://openairdocs.org/sdr/SWAA2024070898044.md): Intercostal · cracked · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02;
- [SDR SWAA2024070810383](https://openairdocs.org/sdr/SWAA2024070810383.md): Web · cracked · Jun 3, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02;
- [SDR SWAA2024070997363](https://openairdocs.org/sdr/SWAA2024070997363.md): Vapor Barrier · cracked · Jun 2, 2024 · N261WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 LH SIDE AT WING CENTER SECTION. 2024- 361522<[01] CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 07-SEP-24.;[02] TOOL USED CALIPER P/N: 500-752-20 S/N: B16101265; DUE DATE: 06-DEC-24.;[03] TOOL USED.
- [SDR SWAA2024070997678](https://openairdocs.org/sdr/SWAA2024070997678.md): Support Bracket · cracked · Jun 2, 2024 · N261WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2024-361560<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9.<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[02] CORRECTED ST
- [SDR SWAA2024070997671](https://openairdocs.org/sdr/SWAA2024070997671.md): Angle · cracked · Jun 2, 2024 · N261WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2024-361555<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.;[02] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W
- [SDR SWAA2024070906492](https://openairdocs.org/sdr/SWAA2024070906492.md): Support Beam · worn · Jun 2, 2024 · N261WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > WEAR ON DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING 2024-361557. POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 16-SEP-25. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1
- [SDR SWAA2024070897673](https://openairdocs.org/sdr/SWAA2024070897673.md): Support Angle · cracked · Jun 2, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[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.
- [SDR SWAA2024070810382](https://openairdocs.org/sdr/SWAA2024070810382.md): Support Angle · cracked · Jun 2, 2024 · N261WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[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.
- [SDR SWAA2024070997361](https://openairdocs.org/sdr/SWAA2024070997361.md): Access Panel · delaminated · Jun 1, 2024 · N261WN · Boeing 7377H4 · Aerodynamic Fairings
  > DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE 2024-361518<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: SCALE P/N: CR5200
- [SDR SWAA2024070897048](https://openairdocs.org/sdr/SWAA2024070897048.md): Handle · deteriorated · Jun 1, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR (4 EA) 2024-361511<[01] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G(2);[02] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B7
- [SDR SWAA2024042578730](https://openairdocs.org/sdr/SWAA2024042578730.md): Holder · loose · Apr 23, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > R2 GIRT BAR DOES NOT STAY SECURE WHEN DOOR IS OPENED<[01] INCREASE CLIP PRESSURE PER SIP
- [SDR SWAA2024041172760](https://openairdocs.org/sdr/SWAA2024041172760.md): Girt Bar · damaged · Apr 10, 2024 · N261WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR SKIRT FLAP RUBBER DISBONDED. R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06. INSPECTION C/W R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06.
- [SDR SWAA2024041172752](https://openairdocs.org/sdr/SWAA2024041172752.md): Isolator · cracked · Apr 10, 2024 · N261WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR CRACKED. R & R AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR IAW SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N261WN/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 = 'N261WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N261WN/reports

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