# Service difficulty reports: N917WN

A list on [N917WN](https://openairdocs.org/aircraft/N917WN.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 · 284 reports

- [SDR SWAA2026101277836](https://openairdocs.org/sdr/SWAA2026101277836.md): Thrust Reverser · malfunctioned · Oct 7, 2026 · N917WN · Boeing 7377H4 · Engine Thrust Reverser
  > LEFT THRUST REVERSER WOULD NOT DEPLOY, NR 1 THRUST REVERSER LIGHT ILLUMINATED. FOUND V148 & V150 FAULTS ON NR 1 ENG T/R EAU DEPLOYED NR 1 ENG T/R & CLEARED EAU FAULTS IAW FIM 78-32 TASK 814. CYCLED NR 1 ENG T/R MULTIPLE TIMES & COULD NOT DUPLICATE FAULT. OPS
- [SDR SWAA2026072091169](https://openairdocs.org/sdr/SWAA2026072091169.md): Battery Pack · no test · Jul 16, 2026 · N917WN · Boeing 7377H4 · Emergency Lighting
  > FWD LEFT EMERGENCY LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-805-NG.
- [SDR SWAA2026062916229](https://openairdocs.org/sdr/SWAA2026062916229.md): Girt Bar · loose · Jun 25, 2026 · N917WN · Boeing 7377H4 · Emergency Equipment
  > L1 GIRT BAR LOOSE. REMOVED FORWARD ENTRY ESCAPE SLIDE, REMOVED & REPLACED RIVETS FOR GIRT BAR HOOK, & REINSTALLED FORWARD ENTRY ESCAPE SLIDE IAW MT 725-61-06 & SRM 51-40-02.
- [SDR SWAA2026061612718](https://openairdocs.org/sdr/SWAA2026061612718.md): Hmu · slow · Jun 3, 2026 · N917WN · Boeing 7377H4 · Fuel Controlling System
  > NR 1 ENG SLOW TO SPEED (NR 2 AT +50% BEFORE NR 1 MOVED FROM 10%) (6-8 SECONDS BEHIND NR 2) ONCE STABILIZED ALL INDICATIONS NORMAL. RESPONDED NORMAL ONCE ABOVE 45%. REMOVED AND REPLACED NR 1 HMU IAW AMM 73-21-10 AND MT 773-21-10. PERFORMED TEST NR 8 IAW AMM 7
- [SDR SWAA2026060208012](https://openairdocs.org/sdr/SWAA2026060208012.md): Slide · partial deploy · May 30, 2026 · N917WN · Boeing 7377H4 · Escape Slide
  > SLIDE AT DOOR 1L FELL OUT OF DOOR LINER WHEN DOOR WAS OPENED. REPACKED L1 FWD ENTRY EMERGENCY SLIDE IAW MT 725-61-06.
- [SDR SWAA2026060106872](https://openairdocs.org/sdr/SWAA2026060106872.md): Girt Bar · loose · May 26, 2026 · N917WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR SLIDE GIRT BAR STOW HOOK LOOSE;NEEDS TO BE SECURED. INSPECTED GIRT BAR HOOK IAW AMM 25-66-01;GIRT BAR IS SECURED IN STOWED POSITION;OK FOR SERVICE
- [SDR SWAA2026042792550](https://openairdocs.org/sdr/SWAA2026042792550.md): Engine · no discrepancy · Apr 23, 2026 · N917WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE SLOW TO SPOOL FOR TAKE OFF. RT ENGINE AT TAKE OFF THRUST & LT ENGINE AT 45%. IAW FIM 73-05, TASK 814. PERFORMED TEST 8 ACCELERATION CHKD AMM 71-00-00. TEST PASSED; NO DEFECTS FOUND.
- [SDR SWAA2026031177887](https://openairdocs.org/sdr/SWAA2026031177887.md): Lens · unsecure · Mar 8, 2026 · N917WN · Boeing 7377H4 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT LENS WILL NOT SECURE IN PLACE. OK TO CONT IAW MEL 33-1-01 SP1. LIGHT REMAINS OPERATIONAL. NSTALLED LENSE IAW AMM 33-14-00.
- [SDR SWAA2026022372807](https://openairdocs.org/sdr/SWAA2026022372807.md): Handle · loose · Feb 21, 2026 · N917WN · Boeing 7377H4 · Service Doors
  > R1 DOOR; DOOR-ASSIST HANDLE LOOSE. ADJUSTED R1 DOOR ASSIST HANDLE IAW AMM 52-11-00.
- [SDR SWAA2025121539783](https://openairdocs.org/sdr/SWAA2025121539783.md): Access Panel · elongated · Nov 26, 2025 · N917WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121534579](https://openairdocs.org/sdr/SWAA2025121534579.md): Floorbeam · cracked · Nov 12, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CRACKED AT BS 540, BL 0 - LBL 24.75. REPLACED FLOORBEAM IAW SRM 51-40-02, AND DWG 143A5240, SHEET 14, REV -.
- [SDR SWAA2025121534577](https://openairdocs.org/sdr/SWAA2025121534577.md): Floor Support · cracked · Nov 12, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN, FWD WET AREA FLOOR SUPPORT CRACKED, BTW BS 312 - 328, RBL 27. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 39, REV-.
- [SDR SWAA2025121534443](https://openairdocs.org/sdr/SWAA2025121534443.md): Angle · cracked · Nov 12, 2025 · N917WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE, TRAILING EDGE ACCESS PANEL 551FB ON LT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, AND DWG 115A2710, SHEET 9, REV A.
- [SDR SWAA2025121546419](https://openairdocs.org/sdr/SWAA2025121546419.md): Web · corroded · Nov 11, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 TO BS 492.4, RBL 22, WL156 FWD CARGO BAY. REPLACED THE WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4, RBL 22, WL156 IAW SRM 51-10-02, ITEM 9 AND DWG 143A8330, SHEET 42, REV A.
- [SDR SWAA2025121534018](https://openairdocs.org/sdr/SWAA2025121534018.md): Web · corroded · Nov 11, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4, RBL 22, WL 156 IN THE FWD CARGO BAY. REPLACED WEB LOWER SILL IAW SRM 51-10-02, ITEM 9, & DWG 143A8330, SHEET 42, REV A.
- [SDR SWAA2025121234188](https://openairdocs.org/sdr/SWAA2025121234188.md): Floor Panel · delaminated · Nov 11, 2025 · N917WN · Boeing 7377H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231WF IN THE PASSENGER CABIN. REPAIRED THE FLOOR PANEL 231WF IAW SRM 53-00-50-2R-4, REPAIR 4.
- [SDR SWAA2025121533599](https://openairdocs.org/sdr/SWAA2025121533599.md): Support Bracket · cracked · Nov 10, 2025 · N917WN · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > CRACKED SUPPORT BRACKET, TRAILING EDGE MLG SUPPORT BEAM REAR SPAR UPPER AREA, LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, AND SRM-51-10-02-0G-0, ITEM 9. LENGTH OF CRACK: 0.986.
- [SDR SWAA2025121533597](https://openairdocs.org/sdr/SWAA2025121533597.md): Plate · cracked · Nov 10, 2025 · N917WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE, TRAILING EDGE ORSS 462 ON LT WING. REPLACED CORRUGATED PLATE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0. LENGTH OF CRACK: 0.528 INCHES.
- [SDR SWAA2025121234576](https://openairdocs.org/sdr/SWAA2025121234576.md): Floor Support · cracked · Nov 10, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AMAIN CABIN, FWD WET AREA FLOOR SUPPORT HAD A CRACK BTW BS 312 & 328, RBL 27.
- [SDR SWAA2025121533215](https://openairdocs.org/sdr/SWAA2025121533215.md): Support Angle · cracked · Nov 9, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BS 663.75 AND LBL 42. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5. CERTIFIED RII MAJOR REPAIR WORK PERFORMED.
- [SDR SWAA2025121546413](https://openairdocs.org/sdr/SWAA2025121546413.md): Skin · cracked · Nov 9, 2025 · N917WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STAB, LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCH REAR SPAR IN SIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED A REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.
- [SDR SWAA2025121533441](https://openairdocs.org/sdr/SWAA2025121533441.md): Skin · cracked · Nov 9, 2025 · N917WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCHES REAR SPAR INSIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.
- [SDR SWAA2025121533437](https://openairdocs.org/sdr/SWAA2025121533437.md): Angle · corroded · Nov 9, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE LOCATED ON UPPER MAIN SILL AT LEVEL BS 827, S18R, WL 200 IN THE AFT CARGO BAY. REPLACED ANGLE LOCATED ON UPPER MAIN SILL IAW SRM 51-10-02, SRM 51-40-02, AND DWG 146A8313, SHEET 2, REV-.
- [SDR SWAA2025121533439](https://openairdocs.org/sdr/SWAA2025121533439.md): Strap · corroded · Nov 9, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED BTW BS 787 - 794.3, S25R - 26R, WL 156 IN THEAFT CARGO BAY. REPLACED STRAP & FASTENERS LOCATED IAW SRM 51-40-02-0G-0, AND DWG 146A0081, SHEET 37, REV -.
- [SDR SWAA2025121533438](https://openairdocs.org/sdr/SWAA2025121533438.md): Sill Drain · corroded · Nov 9, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION LOWER SILL LOCATED BTW BS 794.3 - 847, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED LOWER SILL AND FASTENERS IAW SRM 51-40-02, & DWG 146A8340, SHEET 28, REV -.
- [SDR SWAA2025121533216](https://openairdocs.org/sdr/SWAA2025121533216.md): Plate · cracked · Nov 9, 2025 · N917WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE, TRAILING EDGE IRSS 215, RT WING. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0. LENGTH OF CRACK: 1.117 INCHES.
- [SDR SWAA2025121533213](https://openairdocs.org/sdr/SWAA2025121533213.md): Web · cracked · Nov 9, 2025 · N917WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED WEB TRAILING EDGE FIXED PANEL ORSS 271, LT WING. REPLACED THE WEB AND FASTENERS IAW SRM-51-10-02-0G-0, ITEM 9, SRM-51-40-02-0G, & DWG 115A2512, SHEET 16, REV-.
- [SDR SWAA2025121533028](https://openairdocs.org/sdr/SWAA2025121533028.md): Keelbeam · cracked · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACKED KEELBEAM, BS 727 - 727A, S27R, REPAIRED THE KEELBEAM IAW EA 25-153-03151-WIP1, EA 25-153-03151, & SRM 53-60-12-2R-1, REPAIR 1.
- [SDR SWAA2025121533027](https://openairdocs.org/sdr/SWAA2025121533027.md): Support · corroded · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION UPPER MAIN SILL LOCATED BETWEEN BS 794.3 - 847, S18R, WL 200 IN THE CARGO BAY. REPLACED UPPER MAIN SILL IAW SRM 51-40-02-0G-0, DWG 146A8110, SHEET 25, REV A, & DWG 146A8111, SHEET 16, REV -.
- [SDR SWAA2025121546411](https://openairdocs.org/sdr/SWAA2025121546411.md): Stub Frame · cracked · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON LOWER STUB FRAME LOCATED BS 294.5, S17R IN FWD GALLEY AREA. REPLACED LOWER STUB FRAME IAW SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D.
- [SDR SWAA2025121533026](https://openairdocs.org/sdr/SWAA2025121533026.md): Tie Clip · cracked · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277, STR 10R IN PASSENGER CABIN. REPLACED TIE CLIP IAW SRM 51-10-02-0G-0, STEP 9, SRM 51-40-02-0G-0, AND DWG 141A1110, SHEET 18, REV -.
- [SDR SWAA2025121533025](https://openairdocs.org/sdr/SWAA2025121533025.md): Stub Frame · cracked · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED LOWER STUB FRAME, BS 294.5, S17R IN THE FWD GALLEY AREA. REPLACED THE LOWER STUB FRAME IAW SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D.
- [SDR SWAA2025121233029](https://openairdocs.org/sdr/SWAA2025121233029.md): Support · corroded · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BS 727E - 767, RBL 22, WL 156, IN THE CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 146A7500, SHEET 13, REV-,
- [SDR SWAA2025121233031](https://openairdocs.org/sdr/SWAA2025121233031.md): Web · corroded · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB BETWEEN BS 767 - 794.3, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0081, SHEET 37, REV-.
- [SDR SWAA2025121233205](https://openairdocs.org/sdr/SWAA2025121233205.md): Strap · corroded · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED STRAP FLOOR SUPPORT LOCATED BETWEEN BS 787 - 794.3, RBL 20, WL 156 IN THE AFT CARGO BAY. TASK CARD WAS DUPLICATED; FOR RESOLUTION SEE TTG8Q018SGUS.
- [SDR SWAA2025121233030](https://openairdocs.org/sdr/SWAA2025121233030.md): Support · corroded · Nov 8, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, LOCATED BETWEEN BS 727C - 787, LBL 22, WL156 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ZEE BS 727 - 847, LBL 22, WL156 IAW SRM 53-00-53-2R-5, REPAIR 5, SRM 51-10-02, ITEM 9, DWG 146A7500, SHEET 113, REV -, & DWG: 146A7502, SHEET 27,
- [SDR SWAA2025121533006](https://openairdocs.org/sdr/SWAA2025121533006.md): Intercostal · corroded · Nov 7, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON LATERAL INTERCOSTAL, BS 269, BL0, WL 208.1. PERFORMED REPAIR ON LATERAL INTERCOSTAL IAW EA 25-153-03197-WIP1, AND EA 25-153-03197.
- [SDR SWAA2025121532683](https://openairdocs.org/sdr/SWAA2025121532683.md): Bear Strap · cracked · Nov 7, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK INDICATION FOUND LOCATED AT BS 291.5 PLUS 10 INCHES, S7R BELOW 4.200 INCHES. PERFORMED REPAIR ON BEAR STRAP HOLE IAW EA 25-153-03090-WIP1, & 25-153-03090-WIP2.
- [SDR SWAA2025121532857](https://openairdocs.org/sdr/SWAA2025121532857.md): Angle · cracked · Nov 7, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, LOCATED BS 500C, S26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV -.
- [SDR SWAA2025121532845](https://openairdocs.org/sdr/SWAA2025121532845.md): Support Beam · cracked · Nov 7, 2025 · N917WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED SUPPORT BEAM, TRAILING EDGE ORSS 280 ON LT WING. REPLACED THE SUPPORT BEAM IAW SRM 51-10-02-0G-0, 51-40-02, & DWG 115A3712, SHEET 5, REV -.
- [SDR SWAA2025121232847](https://openairdocs.org/sdr/SWAA2025121232847.md): Web · corroded · Nov 7, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB, BETWEEN BS 492.4 - 500A, RBL 22, WL 156 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 143A0080, SHEET 23, REV -.
- [SDR SWAA2025121532668](https://openairdocs.org/sdr/SWAA2025121532668.md): Floorbeam · corroded · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM LOWER FLANGE, BS 986.5, RBL 40, WL 208.5. REPAIRED THE FLOORBEAM IAW EA 25-153-03177-WIP1, EA 25-153-03177, AND SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.
- [SDR SWAA2025121532426](https://openairdocs.org/sdr/SWAA2025121532426.md): Web · cracked · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB FLOOR STRUCTURE, BETWEEN BS 328 - 344, LBL 45 IN THE FWD GALLEY AND LAVATORY. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, & DWG 141A5400, SHEET 44, REV -.
- [SDR SWAA2025121532679](https://openairdocs.org/sdr/SWAA2025121532679.md): Support Beam · cracked · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BEAM NR 4, LOCATED FOR THE FWD GALLEY DOOR. REPLACED SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A6516, SHEET 102, REV B.
- [SDR SWAA2025121532423](https://openairdocs.org/sdr/SWAA2025121532423.md): Floor Support · cracked · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BTW BS 344 - 360, BL 0, IN THE FWD GALLEY AND LAV. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, AND DWG 141A5400, SHEET 32, REV-.
- [SDR SWAA2025121532422](https://openairdocs.org/sdr/SWAA2025121532422.md): Floor Support · cracked · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPPORT BTW BS 277 - 294.5, BL 0, IN THE FWD GALLEY & LAV. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, SHEET 20, REV -.
- [SDR SWAA2025121532424](https://openairdocs.org/sdr/SWAA2025121532424.md): Angle · corroded · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED ZEE ANGLE, BS 312, LBL 55, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE ZEE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025121546385](https://openairdocs.org/sdr/SWAA2025121546385.md): Angle · corroded · Nov 6, 2025 · N917WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED ZEE ANGLE, BS 312, LBL 55, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE ZEE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025121532658](https://openairdocs.org/sdr/SWAA2025121532658.md): Access Panel · damaged · Nov 6, 2025 · N917WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE ON RT WING. REPAIRED THE ACCESS PANEL 661CB TRAILING EDGE IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121532659](https://openairdocs.org/sdr/SWAA2025121532659.md): Access Panel · damaged · Nov 6, 2025 · N917WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661AB ON RT WING. REPAIRED ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.

Next page: https://openairdocs.org/aircraft/N917WN/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 = 'N917WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N917WN/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.