# Service difficulty reports: N963WN

A list on [N963WN](https://openairdocs.org/aircraft/N963WN.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 · 207 reports

- [SDR SWAA2026100201174](https://openairdocs.org/sdr/SWAA2026100201174.md): Light · inoperative · Sep 28, 2026 · N963WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY AREA LIGHT AT SEATS 26-27 IS INOP REMOVED AND REPLACED EMERGENCY AREA LIGHT IAW B737 AMM 33-51-03-960-801 OPS CHECK GOOD. VERIFIED REMOVED AND REPLACED EMERGENCY AREA LIGHT IAW B737 AMM 33-51-03-960-801 OPS CHECK GOOD.
- [SDR SWAA2026100116960](https://openairdocs.org/sdr/SWAA2026100116960.md): Battery Pack · inoperative · Sep 28, 2026 · N963WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT EMERGENCY LIGHT BATTERY IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1669 IAW AMM 33-51-06. OPS CHECK GOOD. OPENED AND CLOSED RETURN AIR GRILL FWD OF RT EMERGENCY EXIT DOOR IAW AMM 33-51-06.
- [SDR SWAA2026100172032](https://openairdocs.org/sdr/SWAA2026100172032.md): Light · inoperative · Sep 28, 2026 · N963WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED L2 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHECK GOOD.
- [SDR SWAA2025121551818](https://openairdocs.org/sdr/SWAA2025121551818.md): Radome · cracked · Dec 11, 2025 · N963WN · Boeing 7377H4 · Aerodynamic Fairings
  > NOSE RADOME HAS THREE CRACKS AT 9:00 POSITION, (LOOKING FWD). ALL ARE 1.5' IN LENGTH, STARTING AT AFT EDGE EXTENDING FWD. R & R NOSE RADIOMETER IAW AMM 53-52-00. R & R NOSE RADOME IAW 53-52-00..
- [SDR SWAA2025121551820](https://openairdocs.org/sdr/SWAA2025121551820.md): Guide · cracked · Dec 11, 2025 · N963WN · Boeing 7377H4 · Aerodynamic Fairings
  > RADOME ANGLE GUIDE FLANGES CRACKED AT 9:00 POSITION (LOOKING FWD). CW EA 25-153-03384.
- [SDR SWAA2025091113130](https://openairdocs.org/sdr/SWAA2025091113130.md): Slide · loose · Sep 10, 2025 · N963WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR; VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF<[01] RESECURED FWD ENTRY DOOR SLIDE PROPERLY IN REF WITH AMM 25-66-01.;[02] RESECURED FWD ENTRY DOOR SLIDE PROPERLY IN REF WITH MT 725-61-06.
- [SDR SWAA2025091113140](https://openairdocs.org/sdr/SWAA2025091113140.md): Slide · loose · Sep 10, 2025 · N963WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF<[01] RESECURED FWD SERVICE DOOR SLIDE PROPERLY IN REF WITH AMM 25-66-01.;[02] RESECURED FWD SERVICE DOOR SLIDE PROPERLY IN REF WITH MT 725-61-06.
- [SDR SWAA2025072392792](https://openairdocs.org/sdr/SWAA2025072392792.md): Baffle · cracked · Jul 18, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 500A - 500B, LBL 25 BAFFLE IS CRACKED. R & R BAFFLE IAW DWG 143A7505 REV -, & SRM 51-40-02-0G-0.
- [SDR SWAA2025072392793](https://openairdocs.org/sdr/SWAA2025072392793.md): Baffle · damaged · Jul 18, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BS 500 - 500A, LBL 25 BAFFLE. AFT FASTENER HOLE IS ELONGATED WITH NO ED. R & R BAFFLE BS 500 - 500A, LBL 25 IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025072491948](https://openairdocs.org/sdr/SWAA2025072491948.md): Baffle · cracked · Jul 16, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BS 500B TO 500C, LBL 25 BAFFLE WAS CRACKED. REMOVED AND REPLACED THE BAFFLE BS 500B - 500C, LBL 25 IAW SRM 51-40-02-0G-0 & DWG 143A7505 REV-.
- [SDR SWAA2025072490006](https://openairdocs.org/sdr/SWAA2025072490006.md): Shield · corroded · Jul 10, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD PIT DOOR CUT-OUT STRUCTURE AFT RH SHIELD CORRODED IN MULTIPLE AREAS FROM STATION 500 TROUGH 500A. REMOVED CORROSION IAW SRM 51-10-02-0G-0ITEM 15 EVALUATED REWORKED AREA WITH ORIGINAL THICKNESS 0.032'; LOSS 0.005'; REMAINING 0.027' WERE IS A MAXIMUM OF
- [SDR SWAA2025072490004](https://openairdocs.org/sdr/SWAA2025072490004.md): Angle · corroded · Jul 10, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO LEFT Z-ANGLE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES FROM BS 500+10 - 500D. REMOVED CORROSION FROM LT ZEE ANFLE BS 500+10 - 500D. EVALUATED REWORKED AREA WITH ORIGINAL THICKNESS 0.040'; LOSS 0.020'; REMAINING.020'. MAXIMUM LOSS O
- [SDR SWAA2025072490005](https://openairdocs.org/sdr/SWAA2025072490005.md): Angle · corroded · Jul 10, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT Z ANGLE HAS CORROSION AROUND SEVERAL FASTENERS HOLES, BETWEEN BS 727A+17 - 727C+4. REMOVED CORROSION & VERIFIED WITH A 10X POWER MAGNIFYING GLASS IAW SRM 53-00-53-1A-2. EVALUATED REWORKED AREA WITH ORIGINAL THICKNESS 0.040, REMAINING THICKNESS
- [SDR SWAA2025072390002](https://openairdocs.org/sdr/SWAA2025072390002.md): Angle · corroded · Jul 10, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LT ZEE ANGLE HAS CORROSION AROUND SEVERAL FASTENERS HOLES, BS 727A - 767. REMOVED CORROSION & VERIFIED WITH A 10X POWER MAGNIFYING GLASS IAW SRM 53-00-53-1A-2. EVALUATED REWORKED AREA LT BS 727A - 747+18' WITH ORIGINAL THICKNESS 0.040'; REMAINING T
- [SDR SWAA2025072390003](https://openairdocs.org/sdr/SWAA2025072390003.md): Angle · corroded · Jul 10, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT ZEE ANGLE CORRODED AROUND SEVERAL FASTENERS HOLES, BETWEEN BS 727D - 767. REMOVED CORROSION & VERIFIED WITH A 10X POWER MAGNIFYING GLASS IAW SRM 53-00-53-1A-2. EVALUATED REWORKED AREA WITH ORIGINAL THICKNESS 0.040, REMAINING THICKNESS 0.033, LO
- [SDR SWAA2025072489396](https://openairdocs.org/sdr/SWAA2025072489396.md): Shield · corroded · Jul 9, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUT OUT STRUCTURE FORWARD SHIELD IS CORRODED AROUND NUT PLATES ON LOWER SIDE. REMOVED AND REPLACED AFT CARGO DOOR CUT OUT STRUCTURE FORWARD SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081 REV A.
- [SDR SWAA2025072489394](https://openairdocs.org/sdr/SWAA2025072489394.md): Panel · delaminated · Jul 9, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT FORWARD BULKHEAD PANEL 121LW LT UPPER CORNER BENT & DELAMINATED. REPLACED ON SHELF IAW SRM 51-10-02-0G-0 STEP 9. REMOVED AND REPLACED IAW SRM 51-10-02-0G-0-A00248.
- [SDR SWAA2025072389395](https://openairdocs.org/sdr/SWAA2025072389395.md): Strap · cracked · Jul 9, 2025 · N963WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FORWARD BULKHEAD STRAP AT BS 727, RBL 24, WL 183, CRACKED. REMOVED STRAP, FABRICATED NEW, & INSTALLED NEW STRAP IAW SRM 51-40-02-0G-0, & DWG 144A2600 REV -, AND DWG 144A2617 REV B.
- [SDR SWAA2025072488020](https://openairdocs.org/sdr/SWAA2025072488020.md): Seat Track · corroded · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 706+19' TO STA 727+1' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072488022](https://openairdocs.org/sdr/SWAA2025072488022.md): Seat Track · corroded · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 727A+7.5' TO STA 727A+17' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072488013](https://openairdocs.org/sdr/SWAA2025072488013.md): Floorboard · pulled · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage Floor Panel
  > DOT (A160-18) PASSENGER CABIN FLOORBOARD 241CF HAS PULLED FIBERS. REFER TO FAULT TTG8Q013J5SY WHERE 25-153-01819 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025072488018](https://openairdocs.org/sdr/SWAA2025072488018.md): Floorboard · pulled · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage Floor Panel
  > DOT (A160-19) PASSENGER CABIN FLOORBOARD 241BF HAS PULLED FIBERS. REFER TO FAULT TTG8Q013J5SY WHERE 25-153-01819 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025072488014](https://openairdocs.org/sdr/SWAA2025072488014.md): Floorboard · pulled · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOORBOARD 242AF HAS PULLED FIBERS. REFER TO FAULT TTG8Q013J5SY WHERE 25-153-01819 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025072488139](https://openairdocs.org/sdr/SWAA2025072488139.md): Seat Track · corroded · Jul 3, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK, RBL 45, BS 500C+4 - 500D LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON SEAT TRACK IAW SRM 51-10-02-0G-0, LIMITS VERIFIED. DEPTH OF DAMAGE CLEAN UP.045, MAX CLEAN UP DEPTH ALLOWED.040. OUT OF LIMITS IAW SRM 53-0
- [SDR SWAA2025072887736](https://openairdocs.org/sdr/SWAA2025072887736.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45, BS 685+9.5 - 685+12 UPPER SIDE OF CROWN HAS EVIDENCE OF CORROSION. RESOLVED ON TTG8Q013HN6W.
- [SDR SWAA2025072487403](https://openairdocs.org/sdr/SWAA2025072487403.md): Stub Frame · cracked · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage Main, Frame
  > FWD GALLEY DOOR CUTOUT; FWD FRAME STA 294.5; UPPER STUB FRAME HAS APROX.4' CRACK AT TOP END OF SEAL DEPRESSOR. REF CARD TTG8Q00TSZYP CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS<[01] REMOVED R1 DOOR UPPER STUB FRAME IAW SRM 51-40-02-G0-0 INSTALLED R1 DOOR STUB
- [SDR SWAA2025072487718](https://openairdocs.org/sdr/SWAA2025072487718.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 500D+6' TO STA 520 LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. REPAIR OF SEAT TRACK COMPLETED IN TTG8Q013HMR6.
- [SDR SWAA2025072487721](https://openairdocs.org/sdr/SWAA2025072487721.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 540+12' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487729](https://openairdocs.org/sdr/SWAA2025072487729.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 559+9.25' TO STA 559+11.5' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT WAS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487731](https://openairdocs.org/sdr/SWAA2025072487731.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 578+5' UPPER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT WAS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487732](https://openairdocs.org/sdr/SWAA2025072487732.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 597+2' TO STA 616 LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT WAS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487726](https://openairdocs.org/sdr/SWAA2025072487726.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 685+9' TO STA 706+1' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT WAS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487739](https://openairdocs.org/sdr/SWAA2025072487739.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > (147-113) MAIN CABIN SEAT TRACK LBL 45 STA 639+23' TO STA 663.75+14' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT WAS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487737](https://openairdocs.org/sdr/SWAA2025072487737.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 663.75+1' TO STA 663.75+3' UPPER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487738](https://openairdocs.org/sdr/SWAA2025072487738.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 639+4' TO STA 639+8' LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487740](https://openairdocs.org/sdr/SWAA2025072487740.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 45 STA 639+7.5' UPPER SIDE OF CROWN HAS EVIDENCE OF CORROSION. FAULT IS RESOLVED ON FAULT TTG8Q013HN6W.
- [SDR SWAA2025072487749](https://openairdocs.org/sdr/SWAA2025072487749.md): Seal · cracked · Jul 2, 2025 · N963WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB PANEL 343AT AFT BODY SEAL CRACKED AND WORN. REPLACED AFT BODY SEAL ON HORIZONTAL STAB PANEL 343AT IAW SRM 51-40-02-0G-0; STEP 9. ATAG A337238; PN 186A3003-40; AIPC REFERENCE 55-10-52.
- [SDR SWAA2025072487746](https://openairdocs.org/sdr/SWAA2025072487746.md): Seal · cracked · Jul 2, 2025 · N963WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB PANEL 333AT AFT BODY SEAL CRACKED AND WORN. REPLACED AFT BODY SEAL ON HORIZONTAL STAB PANEL 333AT IAW SRM 51-40-02-0G-0; STEP 9. IAW AIPC 55-10-52.
- [SDR SWAA2025072487725](https://openairdocs.org/sdr/SWAA2025072487725.md): Seat Track · corroded · Jul 2, 2025 · N963WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 25, BS 685+8.5 - 706+1 LOWER SIDE OF CROWN HAS EVIDENCE OF CORROSION. CUT, & REMOVED DAMAGED PART OF THE SEAT TRACK BETWEEN BS 639+17 AND 706+10 LBL 25. INSTALLED A NEW SEAT TRACK REPAIR PART IAW SRM 53-00-52-2R-3.
- [SDR SWAA2025072487030](https://openairdocs.org/sdr/SWAA2025072487030.md): Panel · delaminated · Jul 1, 2025 · N963WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE PANEL 521DB; CORNER DELAMINATED AT ANTI-ICE DUCT CUTTOUT. REPAIRED CORNER DAMAGE TO PANEL 521DB IAW SRM 57-41-01-1A-1; SRM 51-70-08-0G-0 AND SRM 51-70-14-2R-3.
- [SDR SWAA2025072487032](https://openairdocs.org/sdr/SWAA2025072487032.md): Panel · delaminated · Jul 1, 2025 · N963WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE PANEL 521KB; 2 EACH CORNERS DELAMINATED ON FORWARD EDGE. REPAIRED LEFT WING LEADING EDGE PANEL 521KB 2EA CORNERS DELAMINATED IAW SRM 51-70-04-2R-13.
- [SDR SWAA2025072887029](https://openairdocs.org/sdr/SWAA2025072887029.md): Panel · delaminated · Jun 30, 2025 · N963WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE PANEL 621HB AFT CORNER DELAMENATED. REPAIRED CORNER DAMAGE TO PANEL 621HB IAW SRM 57-41-01-1A-1, SRM 51-70-08-0G-0, AND SRM 51-70-14-2R-3.
- [SDR SWAA2025072486799](https://openairdocs.org/sdr/SWAA2025072486799.md): Service Door · corroded · Jun 30, 2025 · N963WN · Boeing 7377H4 · Fluid Service Doors
  > F.R. WATER SERVICE DOOR (146AR) EXTERNAL SKIN CORRODED.<[01] REMOVED CORROSION AND VERIFIED WITH A 10-POWER MAGNIFYING GLASS ON WATER SERVICE DOOR (146AR) EXTERNAL SKIN I.A.W SRM 51-10-02-0G-0.<BR>EVALUATED AREA WITH ORIGINAL THICKNESS 0.140'; MATERIAL LOSS 0.
- [SDR SWAA2025072486804](https://openairdocs.org/sdr/SWAA2025072486804.md): Skin · corroded · Jun 30, 2025 · N963WN · Boeing 7377H4 · Fluid Service Doors
  > DOT A24-8 CUSTOMER REQUEST F.R. WASTE WATER SERVICE DOOR (145AL) EXTERNAL SKIN CORRODED.<[01] REMOVED AND REPLACED WASTE WATER SERVICE DOOR ASSY ON FAULT TTG8Q013G6R0;[02] VERIFIED ITEM 1<BR>AUDIT C/W
- [SDR SWAA2025072486805](https://openairdocs.org/sdr/SWAA2025072486805.md): Skin · corroded · Jun 30, 2025 · N963WN · Boeing 7377H4 · Fluid Service Doors
  > DOT A24-9 CUSTOMER REQUEST F.R. WASTE WATER SERVICE DOOR (145AL) SUSPECT INTERNAL SKIN HAS CORROSION.<[01] 01 - REMOVED AND REPLACED PER SRM 52-40-01-1A-1-A00184 (PERMANENT (NON-DENT DAMAGE TYPES)
- [SDR SWAA2024100745158](https://openairdocs.org/sdr/SWAA2024100745158.md): Sign · broken · Oct 3, 2024 · N963WN · Boeing 7377H4 · Emergency Lighting
  > MID CABIN OVERHEAD EXIT SIGN BROKE<[01] REPLACED MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPS GOOD.
- [SDR SWAA2024100744909](https://openairdocs.org/sdr/SWAA2024100744909.md): Engine · power loss · Oct 3, 2024 · N963WN · Boeing 7377H4 · Fuel Controlling System
  > #! ENGINE ROLLED BACK DURING TAKE AT 15 INDICATED. ABORTED TAKE OFF RETURNED TO GATE<[01] C/W EEC BITE; NO FAULTS FOUND; PREFORMED POWER ASSURANCE RUN NO DEFECTS NOTED IAW FIM 73-05 TASK 808
- [SDR SWAA2024042980219](https://openairdocs.org/sdr/SWAA2024042980219.md): Lens · dislodged · Apr 27, 2024 · N963WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTS MID CABIN EXIT SIGN LENS DISLODGED<[01] RESECURED LENS PER AMM 33-51-01
- [SDR SWAA2024030760068](https://openairdocs.org/sdr/SWAA2024030760068.md): Battery Pack · no test · Mar 7, 2024 · N963WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024030760067](https://openairdocs.org/sdr/SWAA2024030760067.md): Battery Pack · no test · Mar 7, 2024 · N963WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATT PACK M01673 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Next page: https://openairdocs.org/aircraft/N963WN/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 = 'N963WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N963WN/reports

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