# Service difficulty reports: N951WN

A list on [N951WN](https://openairdocs.org/aircraft/N951WN.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 · 178 reports

- [SDR SWAA2026061712911](https://openairdocs.org/sdr/SWAA2026061712911.md): Light · inoperative · Jun 17, 2026 · N951WN · Boeing 7377H4 · Emergency Lighting
  > INOP EXTERIOR EMERGENCY EXIT LIGHT AT LT SIDE WING TO BODY FAIRING AREA BS 767. REMOVED AND REPLACED EXTERIOR EMERGENCY EXIT LIGHT AT LT SIDE WING TO BODY FAIRING AREA BS 767 IAW AMM 33-51-04-960-801. TESTED OK.
- [SDR SWAA2026062212552](https://openairdocs.org/sdr/SWAA2026062212552.md): Battery Pack · inoperative · Jun 16, 2026 · N951WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT ON STOWAGE BIN 2 AND 3 RT. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR SWAA2026062212550](https://openairdocs.org/sdr/SWAA2026062212550.md): Battery Pack · inoperative · Jun 16, 2026 · N951WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT IN FWD GALLEY 1. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
- [SDR SWAA2026062208737](https://openairdocs.org/sdr/SWAA2026062208737.md): Web · cracked · Jun 3, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED DOUBLER WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RBL 31.83. REPLACED WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RBL 31.83 IAW SRM 51-40-02; SRM 51-10-02, AND DWG 111A1001 SHEET 504, REV -.
- [SDR SWAA2026062208736](https://openairdocs.org/sdr/SWAA2026062208736.md): Access Panel · damaged · Jun 3, 2026 · N951WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELONGATED HOLES ON ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.
- [SDR SWAA2026062208128](https://openairdocs.org/sdr/SWAA2026062208128.md): Stringer · cracked · May 31, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR CATEGORY A ON STRINGER 23L BETWEEN BS 500D - 540 AT FWD CARGO BAY IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026062208039](https://openairdocs.org/sdr/SWAA2026062208039.md): Angle · cracked · May 31, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 947.5, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 149A8103, SHEET 8, REV -.
- [SDR SWAA2026062208044](https://openairdocs.org/sdr/SWAA2026062208044.md): Angle · cracked · May 31, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 149A8102, REV A.
- [SDR SWAA2026062207959](https://openairdocs.org/sdr/SWAA2026062207959.md): Bracket · damaged · May 31, 2026 · N951WN · Boeing 7377H4 · Elevator Structure
  > ELONGATED HOLE ON FWD BRACKET FRONT SPAR HORIZONTAL STAB RT SIDE. REPLACED FWD BRACKET FRONT SPAR HORIZONTAL STABILIZER RT SIDE IAW SRM 51-40-02. REPLACED FWD BRACKET FRONT SPAR HORIZONTAL STAB RT SIDE IAW SRM 51-10-02 AND SRM 51-40-02.
- [SDR SWAA2026062207958](https://openairdocs.org/sdr/SWAA2026062207958.md): Support Angle · cracked · May 30, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE, BS 867, STR 3R IN THE PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026062207613](https://openairdocs.org/sdr/SWAA2026062207613.md): Angle · cracked · May 29, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED UPPER ANGLE BS 694, BL 0. REPLACED THE UPPER ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026062207731](https://openairdocs.org/sdr/SWAA2026062207731.md): Crossbeam · cracked · May 29, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON BREAK PANEL LOCATED BS 540, BL 0 - LBL 24.75. REPLACED THE BREAK PANEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026062207612](https://openairdocs.org/sdr/SWAA2026062207612.md): Angle · cracked · May 29, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED LOWER ANGLE, BS 694, BL 0. REPLACED LOWER ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026062207730](https://openairdocs.org/sdr/SWAA2026062207730.md): Crossbeam · cracked · May 29, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED BREAK PANEL, BS 540, BL 0 - RBL 24.75. REPLACED BREAK PANEL IAW SRM 51-40-02.
- [SDR SWAA2026062207295](https://openairdocs.org/sdr/SWAA2026062207295.md): Vapor Barrier · cracked · May 28, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK ON VAPOR BARRIER RT SIDE BS 663.75 AT MAIN WHELL WELL. EVALUATED CRACK LOC. ON VAPOR BARRIER RT SIDE BS663.75 AT MAIN WHEEL WELL AND FOUND OUT LIMIT DUE TO THE DAMAGE EXCEED ALLOWABLE DAMAGE LIMITS IAW AMM 57-10-10-1A-2 ALLOWABLE DAMAGE 2, VAPOR BARRIE
- [SDR SWAA2026062207301](https://openairdocs.org/sdr/SWAA2026062207301.md): Web · cracked · May 28, 2026 · N951WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED WEB INBD FAN COWL INTERNAL AREA ON ENGINE 1. REPLACED WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW 71-13-30, PAGE 10092 AND SRM 51-10-02, ITEM 9.
- [SDR SWAA2026062207276](https://openairdocs.org/sdr/SWAA2026062207276.md): Pressure Deck · cracked · May 27, 2026 · N951WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO 675, RBL 42. PERFORMED A PERMANENT REPAIR ON THEHORIZONTAL PRESSURE DECK BTW RBL30 TO RBL60 AND BTW BS 663 - 675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2026062207275](https://openairdocs.org/sdr/SWAA2026062207275.md): Access Panel · damaged · May 27, 2026 · N951WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2026062206713](https://openairdocs.org/sdr/SWAA2026062206713.md): Scuff Plate · cracked · May 26, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FWD CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE OF FWD CARGO BAY IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026062206397](https://openairdocs.org/sdr/SWAA2026062206397.md): Light · deteriorated · May 26, 2026 · N951WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM-33-51-15-400-802. INSTALLATION COMPLETE
- [SDR SWAA2026062206541](https://openairdocs.org/sdr/SWAA2026062206541.md): Access Panel · damaged · May 26, 2026 · N951WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELONGATED HOLE ON ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-8 REPAIR 8.
- [SDR SWAA2026062206215](https://openairdocs.org/sdr/SWAA2026062206215.md): Fitting · cracked · May 24, 2026 · N951WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACKED LOWER SURFACE AROUND FASTENER ON LEFT WING ACTUATOR FITTING SLAT 4. PERFORMED A PERMANENT REPAIR ON THE NOSE SKIN SLAT 4, LT WING IAW SRM 57-42-01-2R-8, REPAIR 8, & SRM 51-40-02.
- [SDR SWAA2026051803287](https://openairdocs.org/sdr/SWAA2026051803287.md): Battery Pack · no test · May 15, 2026 · N951WN · Boeing 7377H4 · Emergency Lighting
  > M1670 FAILED CAPACITY CHECK. R/R M1670 BATTERY PACK PER AMM 33-51-06
- [SDR SWAA2025121143796](https://openairdocs.org/sdr/SWAA2025121143796.md): Tray · out of adjust · Dec 7, 2025 · N951WN · Boeing 7377H4 · Passenger Compartment Equipment
  > TRAY TABLE EXIT ROW (FO SIDE) WONT STAY LOCKED UPRIGHT. OK TO CONTINUE PER MEL 25-10-01. SP-1B. FOUND MISSING SET SCREW INSTALLED NEW SET SCREW ADJUSTED, OPS CHECK GOOD. OKAY FOR SERVICE IAW CMM 25-21-45.
- [SDR SWAA2025091213608](https://openairdocs.org/sdr/SWAA2025091213608.md): Battery Pack · failed · Sep 11, 2025 · N951WN · Boeing 7377H4 · Emergency Lighting
  > L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025080697911](https://openairdocs.org/sdr/SWAA2025080697911.md): Lamp · inoperative · Aug 3, 2025 · N951WN · Boeing 7377H4 · Emergency Lighting
  > SIDEWALL LIGHTS INOP AT ROWS 2DEF;6DEF 16ABC 22DEF;24DEF;23 ABC SIDEWALL LIGHTS INOP AT ROWS 2DEF 6DEF 16ABC 22DEF24DEF23 ABC. RELAMPED CABIN SIDEWALL LIGHTS IAW 33-21-00 AT ROWS 2DEF;6DEF 16ABC 22DEF;24DEF;23 ABC. OPS CHECKS GOOD.
- [SDR SWAA2024120974494](https://openairdocs.org/sdr/SWAA2024120974494.md): Skin · delaminated · Dec 6, 2024 · N951WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED(MARKED).<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSPECTION
- [SDR SWAA2024111157199](https://openairdocs.org/sdr/SWAA2024111157199.md): Inlet · damaged · Nov 6, 2024 · N951WN · Boeing 7377H4 · Engine Air Intake System
  > #1 ENGINE INLET COWL LIPSKIN HAS A APPROX. 9IN. CREASE AT THE 11 O'CLOCK POSITION.<[01] R & R?D #1 ENGINE INLET PER AMM 71-11-01.
- [SDR SWAA2024072913774](https://openairdocs.org/sdr/SWAA2024072913774.md): Access Panel · deteriorated · Jul 17, 2024 · N951WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT WING LOWER I/B FIXED T/E ACCESS PANEL #551GB; SEAL DETERIORATED/BROKEN<[01] REMOVED AND REPLACED L/W LOWER I/B FIXED T/E ACCESS PANEL 551GB SEAL IN REF TO SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2024072612065](https://openairdocs.org/sdr/SWAA2024072612065.md): Channel · corroded · Jul 13, 2024 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H 'Z' CHANNEL FROM STA 727C TO 727D HAS 1 SPOT WITH CORROSION. (MARKED)<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AREA; TREATED; PRIMED AND APPLIED TOPCOAT TO AFT CARGO R/H Z CHANNEL FROM STA 727C TO 727D
- [SDR SWAA2024072910521](https://openairdocs.org/sdr/SWAA2024072910521.md): Ceiling Panel · cracked · Jul 8, 2024 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING 141YBC WITH FRAYED/CRACKED EDGES.<[01] FABRICATED AFT CARGO CEILING PANEL 141YBC AS PER AMM 25-52-01-201-801;[02] VERIFIED STEP 1.
- [SDR SWAA2024072910220](https://openairdocs.org/sdr/SWAA2024072910220.md): Duct · corroded · Jul 7, 2024 · N951WN · Boeing 7377H4 · Engine Thrust Reverser
  > #2 ENGINE IB TR C-DUCT AFT EXHAUST AREA INNER SURFACE WITH PITTING CORROSION.<[01] REMOVED PITTING CORROSION AT #2 ENGINE IB TR C-DUCT AFT EXHAUST INNER SURFACE AS PER SRM 51-10-02-0G-0 AND RESTORATION TO AREA WAS ACCOMPLISHED ON 24-178-02008-WIP1 [TTG8Q00USYZ
- [SDR SWAA2024072909595](https://openairdocs.org/sdr/SWAA2024072909595.md): Support Beam · cracked · Jul 5, 2024 · N951WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RT WING T/E; LOWER PANEL 661AB SUPPORT BEAM CRACKED AT I/B END.<[01] REMOVED SUPPORT BEAM AT R/W T/E ON LOWER PANEL 661AB AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BEAM ASSY AS PER SRM 51-40-05-0G-0. INSTALLED NEW NUT PLATES ON NEW BEAM ASSY AS PER SRM
- [SDR SWAA2024072509612](https://openairdocs.org/sdr/SWAA2024072509612.md): Floor Panel · cracked · Jul 5, 2024 · N951WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 140BF HAS CRACK<[01] REMOVED AND FABRICATED NEW PANEL 140BF PER SRM 51-40-02-0G-0 AND AMM 25-52-01-201-801 INSTALLATION TO BE ACCOMPLISHED ON TASKCARD # TTG8Q00UF1S8;[02] VERIFIED STEP 1.<BR><BR>REFER TO FAULT TTG8Q00UF1S8 FOR INSTALLATIO
- [SDR SWAA2024072909167](https://openairdocs.org/sdr/SWAA2024072909167.md): Doubler · cracked · Jul 3, 2024 · N951WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16' FROM LEADING EDGE;I/B ROW. CRACK LENGTH: 1'. CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16' FROM LEADING EDGE I/B ROW. CRACK LENGTH: 1'.<[01] REMOVED FAST
- [SDR SWAA2024031463332](https://openairdocs.org/sdr/SWAA2024031463332.md): Sign · detached · Mar 13, 2024 · N951WN · Boeing 7377H4 · Emergency Lighting
  > RT OVERAWING EMERGENCY DOOR EXIT SIGN OFF<[01] INSTALLED RT. OVERAWING DOOR EXIT SIGN IAW AMM 33-51-04
- [SDR SWAA2024021552049](https://openairdocs.org/sdr/SWAA2024021552049.md): Girt Bar · loose · Feb 14, 2024 · N951WN · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE AFT GIRT BAR HANGER LOOSE.<[01] TIGHTENED GIRT BAR RIVETS PER SRM 51-40-02
- [SDR SWAA2024021552048](https://openairdocs.org/sdr/SWAA2024021552048.md): Seal · cracked · Feb 14, 2024 · N951WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > R/H HORIZONTAL STAB AFT LOWER SLIDING SEAL CRACKED<[01] R&R RH HORIZONTAL STAB AFT LOWER SLIDING SEAL REF. SRM 51-40-02.
- [SDR SWAA2024011139740](https://openairdocs.org/sdr/SWAA2024011139740.md): Handle · out of adjust · Jan 10, 2024 · N951WN · Boeing 7377H4 · Service Doors
  > AFT ENTRY DOOR HANDLE WILL NOT FULLY STOW<[01] INSPECTED AFT ENTRY DOOR AND HANDLE; OPEN AND CLOSED DOOR SEVERAL TIMES REF AMM 52-13-00. DOOR OPS NORMAL AC OK FOR SERVICE
- [SDR SWAA2023101109341](https://openairdocs.org/sdr/SWAA2023101109341.md): Unknown · unknown · Oct 10, 2023 · N951WN · Boeing 7377H4 · Landing Gear Position and Warning
  > LANDING GEAR DISAGREE (RIGHT MAIN GEAR). RAN QRH AND LANDED NORMALLY<[01] COMPLETED BITE CHECK ON PSEU. NO FAULTS FOUND. CLEANED ALL SENSORS AND CHECKED THE READINGS FROM LEFT GEAR TO RIGHT GEAR WITH NO OUT OF RANGE READINGS. PER FIM TASK; FAULT WAS INTERMITTE
- [SDR SWAA2023100406151](https://openairdocs.org/sdr/SWAA2023100406151.md): Panel · delaminated · Oct 1, 2023 · N951WN · Boeing 7377H4 · Aerodynamic Fairings
  > WTB PANEL 193B HAS SMALL AREA OF EROSION AND DELAMINATION AT L/E R/H CORNER (MARKED).<[01] R & R WTB PANEL 193B PER SRM 51-40-02
- [SDR SWAA2023081689699](https://openairdocs.org/sdr/SWAA2023081689699.md): Light · missing · Aug 14, 2023 · N951WN · Boeing 7377H4 · Emergency Lighting
  > F/A REPORTS ONE STRIP OF PHOTOLUMESCENT FLOOR LIGHTING MISSING PRIOR TO AFT GALLEY LEFT HAND<[01] REPLACE MISSING PHOTO LUMINESCENT STRIP PER MM 33-51-15
- [SDR SWAA2023072883328](https://openairdocs.org/sdr/SWAA2023072883328.md): Lamp · inoperative · Jul 28, 2023 · N951WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVERWING EMERGENCY LIGHT INOP<[01] REPLACED LAMP REF AMM 33-51-04 OPS CHECK GOOD A/C OK TO CONTINUE
- [SDR SWAA2023070573359](https://openairdocs.org/sdr/SWAA2023070573359.md): Lock · out of adjust · Jun 30, 2023 · N951WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER SEAT 11B; 11C RECLINE INTO EMERGENCY EXIT ROW<[01] ADJUSTED HYDRO-LOCKS PER AMM 25-22-00
- [SDR SWAA2023050343316](https://openairdocs.org/sdr/SWAA2023050343316.md): Panel · elongated · Apr 29, 2023 · N951WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193B HAS SEVERAL ELONGATED; OVERSIZED FASTENER HOLES AND DAMAGED COUNTERSINKS.<[01] LOCATED HOLES IN NEW PANEL PER SRM 51-40-05;[02] REMOVED AND REPLACED 193BB PANEL PER AMM 53-51-21
- [SDR SWAA2023040422890](https://openairdocs.org/sdr/SWAA2023040422890.md): Strip · broken · Apr 1, 2023 · N951WN · Boeing 7377H4 · Emergency Lighting
  > LIGHT STRIP ON FLOOR NEAR AFT GALLEY BROKE OFF<[01] SECURED EGRESS LIGHT STRIP PER M/M 33-51-15
- [SDR SWAA2023010989162](https://openairdocs.org/sdr/SWAA2023010989162.md): Lamp · inoperative · Jan 7, 2023 · N951WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXIT WINDOW LIGHT INOP.<[01] RELAMPED LEFT OVERWING EXIT WINDOW LIGHT; SATISFACTORY OP CK REF AMM 33-21-00.
- [SDR SWAA2022090649761](https://openairdocs.org/sdr/SWAA2022090649761.md): None · inoperative · Sep 3, 2022 · N951WN · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / [01] RELAMPED FWD SERVICE DOOR SLIDE EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2022081131838](https://openairdocs.org/sdr/SWAA2022081131838.md): Attach Angle · cracked · Jul 21, 2022 · N951WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > R/H HORIZ STAB INSPAR STA 120.30 RIB FWD ATTACH ANGLE CRACKED / [01] REMOVED AND REPLACED R/H HORIZ. STAB. INSPAR RIB ASSY. STAB. STA. 120.30 FWD ATTACH ANGLE IAW SRM 51-40-02-0G-0 PARA. 4. AND DWG.# 182A2401; REV:-;[02] COMPLETED PARTS USAGE;[03] RII VERIFIED
- [SDR SWAA2022081029350](https://openairdocs.org/sdr/SWAA2022081029350.md): Panel · debonded · Jul 14, 2022 · N951WN · Boeing 7377H4 · Leading Edge Devices
  > R/W L/E PANEL 621YB CONER METAL STRIP DISBONDED / [01] IDENTIFIED PANEL 621YB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 2; SHEET1; TABLE 2; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D <BR><BR>R

Next page: https://openairdocs.org/aircraft/N951WN/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 = 'N951WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N951WN/reports

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