# Service difficulty reports: N922WN

A list on [N922WN](https://openairdocs.org/aircraft/N922WN.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 · 296 reports

- [SDR SWAA2026080368997](https://openairdocs.org/sdr/SWAA2026080368997.md): Battery Pack · no test · Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT EMERGENCY LIGHT BATTERY PACK M1668 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026080310598](https://openairdocs.org/sdr/SWAA2026080310598.md): Battery Pack · no test · Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency Lighting
  > FWD LEFT ENTRY EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 C/W INSPECTION.
- [SDR SWAA2026080319518](https://openairdocs.org/sdr/SWAA2026080319518.md): Battery Pack · no test · Jul 29, 2026 · N922WN · Boeing 7377H4 · Emergency Lighting
  > ROW 20 ABC EMERGENCY BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2026061611648](https://openairdocs.org/sdr/SWAA2026061611648.md): Girt Bar · out of adjust · Jun 12, 2026 · N922WN · Boeing 7377H4 · Emergency Equipment
  > AFT SERVICE DOOR HAS A DAMAGED EVAC RELEASE STOP ON THE GIRT BAR. REMOVED AND REPLACED RELEASE STOP IAW AMM 25-66-00.
- [SDR SWAA2026022372380](https://openairdocs.org/sdr/SWAA2026022372380.md): Lamp · inoperative · Feb 20, 2026 · N922WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXIT LIGHT IS HAS A BULB OUT. REMOVED AND REPLACED BOTTOM MOST LAMP IN THE LT OVERWING EXIT SIGN JUST FORWARD OF LT OVERWING EXIT AND PERFORMED SATISFACTORY OPERATIONAL TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2026022368081](https://openairdocs.org/sdr/SWAA2026022368081.md): Scuff Plate · cracked · Feb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT ENTRY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRM 5
- [SDR SWAA2026022368082](https://openairdocs.org/sdr/SWAA2026022368082.md): Scuff Plate · cracked · Feb 5, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD GALLEY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRM
- [SDR SWAA2026022466142](https://openairdocs.org/sdr/SWAA2026022466142.md): Skin · debonded · Jan 30, 2026 · N922WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING OTBD AFT FLAP INBD AFT CORNER DISBONDED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP INBD IAW AMM 27-51-22-401.
- [SDR SWAA2026022465349](https://openairdocs.org/sdr/SWAA2026022465349.md): Retainer · cracked · Jan 28, 2026 · N922WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING AFT BULB SEAL RETAINER IS CRACKED AT THE TRANSVERSE WEB. REMOVED AND REPLACED THE AFT BULB SEAL RETAINER IAW SRM 51-40-02-OG-O.
- [SDR SWAA2026022465014](https://openairdocs.org/sdr/SWAA2026022465014.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727B, S9L. ACCOMPLISHED HFEC SURFACE SCAN OF THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED THE CRACK. REMOVED BS 727B; S-9L STRINGER CLIP IAW SRM 51-40-02, LOCATED AND DRILLED NEW STRINGER CLIP PER SR
- [SDR SWAA2026022465018](https://openairdocs.org/sdr/SWAA2026022465018.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727C, S7L. ACCOMPLISHED HFEC SURFACE SCAN OF STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED CRACKED. REMOVED BS 727C; S-7L STRINGER CLIP PER SRM 51-40-02. LOCATED AND DRILLED NEW STRINGER CLIP PER S
- [SDR SWAA2026022465019](https://openairdocs.org/sdr/SWAA2026022465019.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727D, S7R. FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01 & DWG 143A1010-1 REV C..APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW AMM 51-21-41-370-802, & AMM 51-21-72-370-804. REMOVED THE STRINGER CLIP IAW SRM 51-40-02. INS
- [SDR SWAA2026022465011](https://openairdocs.org/sdr/SWAA2026022465011.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727C, S6L. ACCOMPLISH HFEC INSPECTION OF THE STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. REMOVED THE BS 727C; STRINGER CLIP 6L IAW SRM 51-40-02, FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01, & DWG 143
- [SDR SWAA2026022465020](https://openairdocs.org/sdr/SWAA2026022465020.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 727E, S5R, HFEC INSPECTED AREA IAW NDTM, PART 6; 51-00-00, PROCEDURE 23. CRACK NOTED. REMOVED THE STRINGER CLIP IAW SRM 51-40-02, LOCATED & DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, & DWG 146A1112, REV-. FABRICATED A NEW ST
- [SDR SWAA2026022465021](https://openairdocs.org/sdr/SWAA2026022465021.md): Stringer Clip · no discrepancy · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 767, S7R. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
- [SDR SWAA2026022464680](https://openairdocs.org/sdr/SWAA2026022464680.md): Former · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Aerodynamic Fairings
  > LEFT WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN STRINGER 19L & 20L. EVALUATED CRACK ON THE WING TO BODY FAIRING, FOUND TO BE OUT LIMITS AND WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9. REMOVED AND REPLACED THE WING TO BODY FAIRING FORME
- [SDR SWAA2026022364652](https://openairdocs.org/sdr/SWAA2026022364652.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT AFT FLOOR PANEL 241UF WAS FABRICATED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026022364683](https://openairdocs.org/sdr/SWAA2026022364683.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364653](https://openairdocs.org/sdr/SWAA2026022364653.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364687](https://openairdocs.org/sdr/SWAA2026022364687.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2026022364657](https://openairdocs.org/sdr/SWAA2026022364657.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364658](https://openairdocs.org/sdr/SWAA2026022364658.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED UPPER SKIN PULLED STRANDS IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
- [SDR SWAA2026022364646](https://openairdocs.org/sdr/SWAA2026022364646.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE THE FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).
- [SDR SWAA2026022364648](https://openairdocs.org/sdr/SWAA2026022364648.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364650](https://openairdocs.org/sdr/SWAA2026022364650.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364651](https://openairdocs.org/sdr/SWAA2026022364651.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022364656](https://openairdocs.org/sdr/SWAA2026022364656.md): Floor Panel · pulled · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ACF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026022365017](https://openairdocs.org/sdr/SWAA2026022365017.md): Stringer Clip · cracked · Jan 27, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 727B, S5R. ACCOMPLISH HFEC INSPECTION ON THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00 PROCEDURE 23. LOCATED AND DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, AND DWG 146A1102 REV-. FABRICATED A NEW STRINGER CLIP IAW SR
- [SDR SWAA2026022464636](https://openairdocs.org/sdr/SWAA2026022464636.md): Floor Support · cracked · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 380-400, LBL 1, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.
- [SDR SWAA2026022464523](https://openairdocs.org/sdr/SWAA2026022464523.md): Seat Track · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON TOP & IN WELL OF PASSENGER CABIN SEAT TRACK LBL 45, BS 727C+13 - 787+6, BS 807+6, BS 847+7, BS 847+8, WL 208. REMOVED THE DAMAGED SEAT TRACK AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 146A5300, REV-.
- [SDR SWAA2026022464628](https://openairdocs.org/sdr/SWAA2026022464628.md): Skin · cracked · Jan 26, 2026 · N922WN · Boeing 7377H4 · Leading Edge Devices
  > POSSIBLE CRACK ON NR 4 SLAT NOSE SKIN AT ACTUATOR ATTACH FITTING. REPAIRED THE NR 4 SLAT NOSE SKIN IAW SRM 57-42-01-2R-8.
- [SDR SWAA2026022364644](https://openairdocs.org/sdr/SWAA2026022364644.md): Floorbeam · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER HOLE AT BS 986, LBL 47, WL 208. REMOVED AND REPAIRED THE DAMAGE OF THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.
- [SDR SWAA2026022364679](https://openairdocs.org/sdr/SWAA2026022364679.md): Support · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AROUND FASTENER HOLE, BS 986, RBL 47, WL 208. OPEN HOLE EXIST C/T INTERCOSTAL AND FLOOR PANEL SUPPORT AT BS 986 - 1006, WL 208 - WL 202 RBL38. REMOVE DAMAGED REPLACEMENT TEE ANGLE AND INSTALLED NEW REPLACEMENT -1 REPAIR IAW SRM 51-40-02-0G-0, SRM
- [SDR SWAA2026022364635](https://openairdocs.org/sdr/SWAA2026022364635.md): Floor Support · cracked · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BS 380 - 400, RBL 39, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.
- [SDR SWAA2026022364666](https://openairdocs.org/sdr/SWAA2026022364666.md): Floor Support · cracked · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BS 380 - 400, RBL 8, WL 208. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.
- [SDR SWAA2026022364677](https://openairdocs.org/sdr/SWAA2026022364677.md): Shield · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY FWD SHIELD BETWEEN BS 767 - 794, RBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A0081, REV-.
- [SDR SWAA2026022364642](https://openairdocs.org/sdr/SWAA2026022364642.md): Support · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727+4 - 847, LBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A7500, REV-.
- [SDR SWAA2026022364643](https://openairdocs.org/sdr/SWAA2026022364643.md): Support · corroded · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4 - 767, RBL 22, WL156 IAW SRM 51-40-02, DWG 146A7500, REV
- [SDR SWAA2026022364634](https://openairdocs.org/sdr/SWAA2026022364634.md): Floor Support · cracked · Jan 26, 2026 · N922WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BS 277 - 294, BL 0, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, REV -.
- [SDR SWAA2026022364418](https://openairdocs.org/sdr/SWAA2026022364418.md): Crossbeam · cracked · Jan 25, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, PASSENGER CABIN, BS 540, LBL 2, WL 208. REMOVED AND REPLACED THE CROSSBEAM, BS 540, LBL 0.0 TO LBL 24.75 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B;
- [SDR SWAA2026022364419](https://openairdocs.org/sdr/SWAA2026022364419.md): Crossbeam · cracked · Jan 25, 2026 · N922WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM AT PASSENGER CABIN, BS 540; LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540 LBL 24.75 - LBL 45.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B.
- [SDR SWAA2026022364092](https://openairdocs.org/sdr/SWAA2026022364092.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231YF HAS PULLED STRANDS. FABRICATED A NEW 231YF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026022364090](https://openairdocs.org/sdr/SWAA2026022364090.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231ZF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO THE EXTENT OF ALL OF THE DAMAGE.
- [SDR SWAA2026022364094](https://openairdocs.org/sdr/SWAA2026022364094.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026022364095](https://openairdocs.org/sdr/SWAA2026022364095.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241BF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG:144A5810 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026022364096](https://openairdocs.org/sdr/SWAA2026022364096.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026022364098](https://openairdocs.org/sdr/SWAA2026022364098.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241DF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026022364099](https://openairdocs.org/sdr/SWAA2026022364099.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241EF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND BDWG:144A5810, DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026022364097](https://openairdocs.org/sdr/SWAA2026022364097.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242CF HAS PULLED STRANDS. THE FLOOR PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0125.
- [SDR SWAA2026022364100](https://openairdocs.org/sdr/SWAA2026022364100.md): Floor Panel · pulled · Jan 23, 2026 · N922WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242DF HAS PULLED STRANDS. THE FLOOR SUPPORT REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0123.

Next page: https://openairdocs.org/aircraft/N922WN/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 = 'N922WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N922WN/reports

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