# Service difficulty reports: N961WN

A list on [N961WN](https://openairdocs.org/aircraft/N961WN.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 4 · 187 reports

- [SDR SWAA2026101270567](https://openairdocs.org/sdr/SWAA2026101270567.md): Cover · cracked · Oct 6, 2026 · N961WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LENS COVER CRACKED FWD OF RIGHT OVERWING EXIT DOOR. R & R EMERGENCY EXIT LENS COVER FWD OF OVERWING EXIT DOOR IAW AMM 33-51-01.
- [SDR SWAA2026081057203](https://openairdocs.org/sdr/SWAA2026081057203.md): Lamp · inoperative · Aug 6, 2026 · N961WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT DECK, EMERGENCY ESCAPE SLIDE LAMP AT AFT ENTRY DOOR INOPERATIVE. R & R FLIGHT DECK EMERGENCY ESCAPE SLIDE LAMP AT AFT ENTRY DOOR IAW AMM 33-51-04.
- [SDR SWAA2026081045421](https://openairdocs.org/sdr/SWAA2026081045421.md): Light · inoperative · Aug 6, 2026 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN RT OVERWING EXIT LIGHT INOPERATIVE. R & R RT OVERWING LIGHT IAW AMM 33-21-00.
- [SDR SWAA2026081024873](https://openairdocs.org/sdr/SWAA2026081024873.md): Battery Pack · failed · Aug 6, 2026 · N961WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT DECK, EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK M1675 FAILED CAPACITY TEST. R & R THE POWER SUPPLY BATTERY PACK M1675 IAW AMM 33-51-06.
- [SDR SWAA2026032682105](https://openairdocs.org/sdr/SWAA2026032682105.md): Handle · loose · Mar 22, 2026 · N961WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31.;[02] CONFIRMED FWD SERVICE DOOR ASSIST HANDLE SECURED IAW AMM 52-41-31
- [SDR SWAA2025111735171](https://openairdocs.org/sdr/SWAA2025111735171.md): Girt Bar · out of adjust · Nov 13, 2025 · N961WN · Boeing 7377H4 · Emergency Equipment
  > SERVICE DOOR GIRT BAR IS NOT ARMING/DE-ARMING PROPERLY. SECURED GIRT BAR INTO GIRT BAR RETAINER CLIPS PER AMM 25-66-01
- [SDR SWAA2025101523873](https://openairdocs.org/sdr/SWAA2025101523873.md): Sign · inoperative · Oct 12, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT LIGHT INOPERATIVE. R & R RT OVERWING INTERIOR EXIT SIGN IAW AMM 33-51-01. R & R FUSES IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025101524697](https://openairdocs.org/sdr/SWAA2025101524697.md): Fuse · inoperative · Oct 12, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT LIGHT INOPERATIVE. R & R RT OVERWING INTERIOR EXIT SIGN IAW AMM 33-51-01. R & R FUSES IAW AMM 33-51-06 OPS CHECKED GOOD.
- [SDR SWAA2025060575495](https://openairdocs.org/sdr/SWAA2025060575495.md): Battery Pack · inoperative · May 27, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1673 WILL NOT HOLD CHARGE <[01]. REMOVED & REPLACED M1673 BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD. WN50733; [02] C/W ITEM 1. AUDIT COMPLETE.
- [SDR SWAA2025060471836](https://openairdocs.org/sdr/SWAA2025060471836.md): Floor Panel · pulled · May 16, 2025 · N961WN · Boeing 7377H4 · Fuselage Floor Panel
  > DOT#51 A-043 CABIN FLOOR PANEL 231LF HAS PULLED FIBERS <[01]. REFER TO FAULT TTG8Q010E6U4 WHERE EA 25-153-01240 WAS ADDED AS A SUBTASK.; [02] AUDIT C/W.
- [SDR SWAA2025060471837](https://openairdocs.org/sdr/SWAA2025060471837.md): Floor Panel · pulled · May 16, 2025 · N961WN · Boeing 7377H4 · Fuselage Floor Panel
  > DOT#52 A-043 CABIN FLOOR PANEL 231VF HAS PULLED FIBERS IN CORNERS <[01]. REFER TO FAULT TTG8Q010E6U4 WHERE EA 25-153-01240 WAS ADDED AS A SUBTASK.;[ 02] AUDIT C/W.
- [SDR SWAA2025060471492](https://openairdocs.org/sdr/SWAA2025060471492.md): Floor Panel · pulled · May 15, 2025 · N961WN · Boeing 7377H4 · Fuselage Floor Panel
  > DOT#38 A-043 CABIN FLOOR PANEL 231UF HAS PULLED FIBERS <[01]. REFER TO FAULT TTG8Q010E6U4 WHERE EA 25-153-01240 WAS ADDED AS A SUBTASK.; [02] AUDIT C/W.
- [SDR SWAA2025060570883](https://openairdocs.org/sdr/SWAA2025060570883.md): Balance Weight · corroded · May 14, 2025 · N961WN · Boeing 7377H4 · Aileron Control System
  > DOT #114-041. RIGHT WING MOST INBOARD AILERON BALANCE BAY; INBOARD TWO WEIGHTS SHOW EVIDENCE OF CORROSION. <[01] REMOVED AND REPLACED RIGHT WING AILERON BALANCE BAY#5 BOTTOM AILERON; INBOARD TWO WEIGHTS IAW AMM 27-11-31-000-801 STEP 2. E. (1) (C) AND SRM 51-60
- [SDR SWAA2025060371105](https://openairdocs.org/sdr/SWAA2025060371105.md): Seat Track · worn · May 14, 2025 · N961WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > DOT#23 A-043 CABIN SEAT TRACK WORN ON UPPER CROWN AT STA 520 LBL 45 WL 208<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-52-2R-4-A00845 (REPAIR 4 - SECTION 43 AND 47 SEAT TRACK REPAIR FOR TITANIUM OR BAC1520-2789 ALUMINUM EXTRUSION BETWEEN FLOOR BEAMS - PERMAN
- [SDR SWAA2025060670761](https://openairdocs.org/sdr/SWAA2025060670761.md): Winglet · corroded · May 13, 2025 · N961WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > (147-22) R/H WINGLET LOWER STRAKELET HAS CORROSION AT LOWER I/B SURFACE 14.5' FROM LOWER EDGE <[01]. REMOVED AND REPLACED R/H WINGLET LOWER STRAKELET TIP CAP ON FAULT TTG8Q010E2KN; [02] VERIFIED ITEM 1. AUDIT C/W.
- [SDR SWAA2025060670759](https://openairdocs.org/sdr/SWAA2025060670759.md): Winglet · corroded · May 13, 2025 · N961WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > (147-23) R/H WINGLET LOWER STRAKELET HAS CORROSION AT LOWER I/B SURFACE 21.5' FROM LOWER EDGE <[01]. REMOVED DAMAGE AND VERIFIED WITH A 10X MAGNIFYING GLASS I.A.W SRM 51-10-02-0G-0 AND SRM 57-31-01 (AP37. 1-0632). DAMAGE FOUND TO BE OUT OF LIMITS DUE TO 100%
- [SDR SWAA2025020391278](https://openairdocs.org/sdr/SWAA2025020391278.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 11:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 11 O?CLOCK POSITION REF AMM 20-50-11.
- [SDR SWAA2025020391275](https://openairdocs.org/sdr/SWAA2025020391275.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 10:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 10 O?CLOCK POSITION REF AMM 20-50-11.
- [SDR SWAA2025020391277](https://openairdocs.org/sdr/SWAA2025020391277.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 9:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] R/R L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET AT 9 O?CLOCK POSITION REF AMM 20-50-11.
- [SDR SWAA2025020391274](https://openairdocs.org/sdr/SWAA2025020391274.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 6:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REMOVED AND REPLACED #1 ENG LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 6:00 O?CLOCK POSITION PER AMM 70-20-02.
- [SDR SWAA2025020391273](https://openairdocs.org/sdr/SWAA2025020391273.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 5:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REPLACED L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 5:00 O?CLOCK POSITION; FORWARD FLANGE PER AMM 2
- [SDR SWAA2025020391276](https://openairdocs.org/sdr/SWAA2025020391276.md): Angle · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Turbine Section
  > L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 4:00 OCLOCK POSITION; FORWARD FLANGE IS CRACKED.<[01] REPLACED L/H ENGINE LOW PRESSURE TURBINE COOLING AIR TUBE SUPPORT ANGLE BRACKET; AT 4:00 O?CLOCK POSITION; FORWARD FLANGE PER AMM 2
- [SDR SWAA2025020390874](https://openairdocs.org/sdr/SWAA2025020390874.md): Bracket · cracked · Jan 29, 2025 · N961WN · Boeing 7377H4 · Passenger/Crew Doors
  > PASSENGER CABIN FWD ENTRY DOOR SWITCH TARGET BRACKET CRACKED AFT SIDE L1 DOOR <[01] R/R PASSENGER CABIN FWD ENTRY DOOR SWITCH TARGET BRACKET AFT SIDE REF SRM 51-40-02; OPS CHECK OF DOOR SWITCH TARGET GOOD REF AMM 52-71-11.
- [SDR SWAA2025013090886](https://openairdocs.org/sdr/SWAA2025013090886.md): Battery Pack · failed · Jan 29, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN BATTERY PACK M1672 FAILED CAPACITY TEST.<[01] R/R M1672 BATTERY PACK PER AMM 33-21-06;[02] R/R M1672 BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2025013090885](https://openairdocs.org/sdr/SWAA2025013090885.md): Battery Pack · failed · Jan 29, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN BATTERY PACK M1673 FAILED CAPACITY TEST.<[01] R/R M1673 BATTERY PACK PER AMM 33-51-06;[02] R/R M1673 BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2025013090884](https://openairdocs.org/sdr/SWAA2025013090884.md): Battery Pack · failed · Jan 29, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN BATTERY PACK M1669 FAILED CAPACITY TEST.<[01] R/R M1669 BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2025013090883](https://openairdocs.org/sdr/SWAA2025013090883.md): Battery Pack · failed · Jan 29, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN BATTERY PACK M1668 FAILED CAPACITY TEST. <[01] R/R M1668 BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2025013090877](https://openairdocs.org/sdr/SWAA2025013090877.md): Battery Pack · failed · Jan 29, 2025 · N961WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN BATTERY PACK M1670 FAILED CAPACITY TEST.<[01] R/R M1670 BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2024111257957](https://openairdocs.org/sdr/SWAA2024111257957.md): Girt Bar · unsecure · Nov 8, 2024 · N961WN · Boeing 7377H4 · Emergency Equipment
  > AFT SERVICE DOOR ON CAPT SIDE GERT BAR DOES NOT STAY SECURE.<[01] 02 - INSPECTED PER [AMM 25-66-01-000-804-NG (ESCAPE SLIDE GIRT BAR INSTALLATION - PERMANENT)]
- [SDR SWAA2024090533847](https://openairdocs.org/sdr/SWAA2024090533847.md): Floor Panel · cracked · Sep 4, 2024 · N961WN · Boeing 7377H4 · Fuselage Floor Panel
  > 2 CRACKS ON FWD FLOOR PANEL IN AFT CARGO<[01] PERFORMED REPAIR ON CRACKS REF 25-52-01
- [SDR SWAA2024090533848](https://openairdocs.org/sdr/SWAA2024090533848.md): Floor Panel · cracked · Sep 4, 2024 · N961WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACK ON SECOND FLOOR PANEL FROM THE FRON IN AFT CARGO<[01] PERFORMED CRACK REPAIR ON SECOND FLOOR PANEL FROM THE FROM THE FRONT IN AFT CARGO REF AMM 25-52-01
- [SDR SWAA2024072515692](https://openairdocs.org/sdr/SWAA2024072515692.md): Seat · unsecure · Jul 23, 2024 · N961WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 11B EXIT ROW SEAT RECLINES. SHOULD BE LOCKED IN UP POSITION.<[01] R&R HYDROLOCK AT SEAT 11B PER CMM 25-21-45 & LOCKED IN UPRIGHT POSITION.
- [SDR SWAA2024070809479](https://openairdocs.org/sdr/SWAA2024070809479.md): Lens · missing · Jul 5, 2024 · N961WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MISSING @ RH EMERGENCY EXIT ROW.<[01] REPLACED EMERGENCY EXIT SIGN LENS @ RH EMERGENCY EXIT ROW. REF AMM 33-51-01.
- [SDR SWAA2024041875728](https://openairdocs.org/sdr/SWAA2024041875728.md): Isolator · cracked · Apr 17, 2024 · N961WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR AFT SLIDE ISOLATOR IS CRACKED<[01] REMOVED & REPLACED FWD SERVICE DOOR AFT SLIDE ISOLATOR. I.A.W. SRM 51-40-02;[02] C/W INSPECTION
- [SDR SWAA2023083094913](https://openairdocs.org/sdr/SWAA2023083094913.md): Gasket · failed · Aug 29, 2023 · N961WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > FAILURE #2 ENGINE ON CLIMBOUT OUT OF DEN #2 ENGINE; N1 AND N2 ROLLED BACK WITH EVENTUAL ENG FAIL AMBER LIGHT ON #2 EGT GAUGE<[01] PERFORMED RII IDLE LEAK CHECK OF THE DRIVE PAD WITH NO LEAKS NOTED;[02] REPLACED DEFECTIVE GASKET ON HMU INLET FROM FUEL FLOW XMIT
- [SDR SWAA2023060153112](https://openairdocs.org/sdr/SWAA2023060153112.md): Bulb · inoperative · May 28, 2023 · N961WN · Boeing 7377H4 · Emergency Lighting
  > LH OWE DOOR IDENTIFIER HAS 1 BULB OUT. (MARKED)<[01] REMOVED AND REPLACED LH OWE DOOR IDENTIFIER BULB PER AMM 33-51-04-960-801;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
- [SDR SWAA2023060152278](https://openairdocs.org/sdr/SWAA2023060152278.md): Battery Pack · inoperative · May 24, 2023 · N961WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE AFT ENTRY DOOR AND ON AFT GALLEY ARE INOP (L1076 & L1191)<[01] REPLACED BURNED OUT FUSE IN POWER SUPPLY M1672 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-804. EMERGENCY LIGHTS L1076 AND L1191 ARE NOW OPERATIVE.;[02] VERIFIED CORREC
- [SDR SWAA2023060152277](https://openairdocs.org/sdr/SWAA2023060152277.md): Battery Pack · inoperative · May 24, 2023 · N961WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1674 ARE INOP<[01] REPLACED BATTERY PACK M1674 EMERGENCY EXIT LIGHTS AND GOOD FUNCTIONAL TEST PER 33-51-00-710-801;[02] UPDATED PART USED ON ACTION 1;[03] VERIFIED ACTION 4;[04] VERIFIED CORRECTIVE ACTION 3
- [SDR SWAA2023060150770](https://openairdocs.org/sdr/SWAA2023060150770.md): Scuff Plate · cracked · May 20, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON RADIUS OF AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARA 4.B.(2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583 CALIBRA
- [SDR SWAA2023060148092](https://openairdocs.org/sdr/SWAA2023060148092.md): Strap · cracked · May 12, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND IN STRAP AT BS727B WL207 RBL 45.5 FASTENER HOLE LOCATION A<[01] VERIFIED APPLICABILITY OF SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 - SEAT TRACKS;[02] REMOVED STRAP COMMON TO SEAT-TRACK STA-727B RBL-45 WL207 IAW SRM 51-40-02-0G-0.;[03] LOCATED AND DRILL
- [SDR SWAA2023060245660](https://openairdocs.org/sdr/SWAA2023060245660.md): Seal · cracked · May 4, 2023 · N961WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED; WITH SERVICEABLE PART. RT. HORIZONAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023060245882](https://openairdocs.org/sdr/SWAA2023060245882.md): Seal · cracked · May 4, 2023 · N961WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LT. STAB UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED; WITH SERVICEABLE PART; LT. STAB UPPER FWD SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-402.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023060144359](https://openairdocs.org/sdr/SWAA2023060144359.md): Support Bracket · cracked · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8. MARKED<[01] REMOVED RH DUCT SUPPORT BRACKET PN#212A1116-1 IAW SRM 51-40-02;[02] INSTALLED NEW/SERVICABLE RIGHT ECS BAY DUCT SUPPORT BRACKET P/N:212A1116 PER SOPM#20-50-0
- [SDR SWAA2023060144356](https://openairdocs.org/sdr/SWAA2023060144356.md): Support Bracket · cracked · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8. MARKED<[01] REMOVED LH DUCT SUPPORT BRACKET PN#212A1116-1 IAW SRM 51-40-02;[02] INSTALLED NEW/SERVICABLE LEFT ECS BAY DUCT SUPPORT BRACKET P/N:212A1116 PER SOPM#20-50-01;
- [SDR SWAA2023060144176](https://openairdocs.org/sdr/SWAA2023060144176.md): Shield · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA 500+10; 500+12.5 TO 500+15.5; AND 500+12; RBL 24 WL 156.<[01] FOUND TO BE OUT OF LIMITS PER B 737-700 SRM 53-30-15-1A-1;[02] B 737-700 SRM 53-30-15-1A-1 IS APPLICABLE REFERENCE;[03] VERIFIED CORRECTIVE
- [SDR SWAA2023060144177](https://openairdocs.org/sdr/SWAA2023060144177.md): Support · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 400+18; RBL 24; WL 156.<[01] REMOVED CORROSION ORIGINAL MATERIAL THICKNESS.040 MATERIAL LOSS.008 FOUND TO OUT OF LIMITS PER SRM 53-00-53-1A-2 TOOL # ATS 1737 DUE DATE 08/2022;[02] VERIFIED CORRECTIVE ACTION 1 AND
- [SDR SWAA2023060144178](https://openairdocs.org/sdr/SWAA2023060144178.md): Support · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 400+14; 460+10; 460+14; 480+6; 480+10; 480+12; 480+14; 480+14; 480+15; 480+18; LBL 24; WL 156.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT LBL 24 WL 156 IAW SRM 53-00-53
- [SDR SWAA2023060144182](https://openairdocs.org/sdr/SWAA2023060144182.md): Support · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 500+15; 500A+12; LBL 24; WL 158.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT LBL 24 WL 158 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] STEP #1-2 COMPLETED;[03] COMPLE
- [SDR SWAA2023060144179](https://openairdocs.org/sdr/SWAA2023060144179.md): Support · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 500A+2; 500A+6.5; 500A+10.5; 500A+13.5; 500A+14.5; 500A+19; 500B+6; 500B+10; 500C+10; 500C+14; RBL 24; WL 156.<[01] COMPLETED STEPS 1 THRU 10;[02] USED CALIBRATED TOOL # ATS 1737 DUE DATE 08/2022;[03] VERIFIED CORR
- [SDR SWAA2023060144180](https://openairdocs.org/sdr/SWAA2023060144180.md): Support · corroded · May 2, 2023 · N961WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CORROSION ON FORWARD CARGO BAY AFT BULKHEAD SUPPORT AT STA 500D; RBL 15 & 23; WL 156.<[01] FOUND TO NO ALLOWABLE LIMITS PER B 737-700 SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED BULKHEAD SUPPORT PER 51-40-02;[04] AFTER FURTHER INVESTIGATI

Next page: https://openairdocs.org/aircraft/N961WN/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 = 'N961WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N961WN/reports

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