# Service difficulty reports: N912WN

A list on [N912WN](https://openairdocs.org/aircraft/N912WN.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 · 270 reports

- [SDR SWAA2026092170096](https://openairdocs.org/sdr/SWAA2026092170096.md): Slide · dislodged · Sep 17, 2026 · N912WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE FALLEN OUT OF COVER. REINSTALLED SLIDE IN COVER IAW AMM 25-66-01. OPS CHECKS GOOD.
- [SDR SWAA2026061510221](https://openairdocs.org/sdr/SWAA2026061510221.md): Isolator · cracked · Jun 9, 2026 · N912WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED. R & R AFT ENTRY DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026012965071](https://openairdocs.org/sdr/SWAA2026012965071.md): Guard · broken · Jan 28, 2026 · N912WN · Boeing 7377H4 · Emergency Lighting
  > AFT FA STATION LIGHT PANEL HAS A BROKEN SPRING ON THE EMERGENCY EXIT LIGHT COVER PLATE. R & R THE SWITCH GAURD IAW AMM 31-15-15. INSPECTED IAW CMM REPREF NOT FOUND.
- [SDR SWAA2025120442157](https://openairdocs.org/sdr/SWAA2025120442157.md): Light · inoperative · Dec 3, 2025 · N912WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY GROUND LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-04-960-801-NG.
- [SDR SWAA2025120140791](https://openairdocs.org/sdr/SWAA2025120140791.md): Pump · faulted · Nov 28, 2025 · N912WN · Boeing 7377H4 · Fuel Controlling System
  > NUMBER 1 ENGINE WOULD NOT ACCELERATE ABOVE 88 PERCENT N1, NO EMERGENCY DECLARED, NO OVERWEIGHT LANDING. R & R THE FUEL PUMP PACKAGE IAW MT 733-11-00, ON NR 1 ENGINE.
- [SDR SWAA2025092215229](https://openairdocs.org/sdr/SWAA2025092215229.md): Wedge · delaminated · Sep 16, 2025 · N912WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT INBD MAIN FLAP OTBD OF NR 3 CANOE ON TRAILING EDGE OF FLAP LOWER SIDE IS DELAMINATED TSR-2025008016. REMOVED DAMAGED TRAILING EDGE WEDGE, LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-06; INSTALLED NEW WEDGE PER SOPM 20-50-01.
- [SDR SWAA2025091715230](https://openairdocs.org/sdr/SWAA2025091715230.md): Skin · delaminated · Sep 16, 2025 · N912WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT INBD MAIN FLAP OTBD OF NR 3 CANOE ON TRAILING EDGE OF FLAP; UPPER SIDE IS DELAMINATED. ACCOMPLISHED TAP TEST ON UPPER DISCREPANCY AREA; NO DELAM NOTED. FOUND DEFORMED AND WARPED ON UPPER SKIN FROM LOWER SKIN SEPARATION. APPLIED SPEED TAPE ON LT INBD
- [SDR SWAA2025080797550](https://openairdocs.org/sdr/SWAA2025080797550.md): Fuse · inoperative · Aug 2, 2025 · N912WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT SIDE OVERWING UPPER EMERGENCY EXIT LIGHT INOPERATIVE. ] REPLACED FUSES AND PERFORMED GOOD TEST RIGHT SIDE OVERWING UPPER EMERGENCY EXIT LIGHT (M1669) IAW AMM 33-51-06-960-804.
- [SDR SWAA2025080796660](https://openairdocs.org/sdr/SWAA2025080796660.md): Flashlight · unsecure · Jul 30, 2025 · N912WN · Boeing 7377H4 · Emergency Equipment
  > FWD WINDSCREEN LOWER EMERGENCY FLASHLIGHT NOT SECURED. TIGHTEN FWD WINDSCREEN LOWER EMERGENCY FLASHLIGHT SCREWS IAW SOPM 20-50-01.
- [SDR SWAA2025080795587](https://openairdocs.org/sdr/SWAA2025080795587.md): Battery · discharged · Jul 27, 2025 · N912WN · Boeing 7377H4 · Emergency Equipment
  > FWD WINDSCREEN LOWER EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806;[02] REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806.
- [SDR SWAA2025080792535](https://openairdocs.org/sdr/SWAA2025080792535.md): Track · cracked · Jul 18, 2025 · N912WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK ON RH HORIZONTAL STAB UPPER SHARK FIN FWD SLIDING TRACK. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER SHARK FIN FWD SLIDING TRACK PER AMM 20-50-11.
- [SDR SWAA2025080791718](https://openairdocs.org/sdr/SWAA2025080791718.md): Track · cracked · Jul 16, 2025 · N912WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK ON LT HORIZONTAL STAB UPPER SHARK FIN FWD SLIDE TRACK. REMOVED AND REPLACED LT HORIZONTAL STAB UPPER SHARK FIN FWD SLIDE TRACK IAW SOPM 20-50-01 AND AMM 20-50-11-910-801.
- [SDR SWAA2025080791392](https://openairdocs.org/sdr/SWAA2025080791392.md): Panel · cracked · Jul 15, 2025 · N912WN · Boeing 7377H4 · Vertical Stabilizer
  > CRACK ON UPPER LEFT SLIDE PANEL COMMON TO 332AT. REMOVED AND REPLACED LEFT SLIDE PANEL COMMON TO 332AT PER AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.
- [SDR SWAA2025080790281](https://openairdocs.org/sdr/SWAA2025080790281.md): Floor Panel · pulled · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE, FLOOR PANEL 221FF WAS REPLACED IAW SRM 51-10-02-0G-0 PAAR 9.A (1).
- [SDR SWAA2025080790549](https://openairdocs.org/sdr/SWAA2025080790549.md): Stringer Clip · cracked · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT AFT PASSENGER COMPARTMENT BS 907; S-16R. REMOVED AND REPLACED NEW STRINGER CLIP IAW SRM 51-40-02 AND DWG 147A0020 REV:-.
- [SDR SWAA2025080790548](https://openairdocs.org/sdr/SWAA2025080790548.md): Stringer Clip · cracked · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND AT STRINGER TO FRAME CLIP. STA 727B S-4R. REMOVED AND REPLACED STRINGER CLIP AT STA 727B S-4R IAW SRM 51-40-02 AND DWG# 146A1102 ID: 0001 REV: D.
- [SDR SWAA2025080790561](https://openairdocs.org/sdr/SWAA2025080790561.md): Stringer Clip · cracked · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND AT STRINGER TO FRAME CLIP. STA 727A S-7L. REMOVED AND REPLACED STRINGER CLIP AT STA 727A S-7L IAW SRM 51-40-02 AND DWG# 146A1101 ID: 0001 REV: E.
- [SDR SWAA2025080790547](https://openairdocs.org/sdr/SWAA2025080790547.md): Service Door · corroded · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fluid Service Doors
  > CORROSION ON PANEL 145AL TOILET SERVICE DOOR AT BONDING JUMPER AREA. REMOVED AND REPLACED PANEL 145AL IAW AIPC 52-49-07-01; AMM 52-49-07-400-801 AND DWG 146A7410 REV-.
- [SDR SWAA2025080790429](https://openairdocs.org/sdr/SWAA2025080790429.md): Seal · cracked · Jul 11, 2025 · N912WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB PANEL 343AT SLIDE SEAL CRACKED. REMOVED AND REPLACED HORIZONTAL STAB PANEL 343AT SLIDE SEAL IAW SRM 51-40-02;
- [SDR SWAA2025080690282](https://openairdocs.org/sdr/SWAA2025080690282.md): Floor Panel · pulled · Jul 11, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025080790229](https://openairdocs.org/sdr/SWAA2025080790229.md): Floor Panel · delaminated · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 242XF UPPER SURFACE HAS AREAS OF DELAMINATION. DUE TO EXTENT OF DAMAGE, FLOOR PANEL 242XF WAS REPLACED IAW SRM 51-10-02-0G-0 PAAR 9.A (1).
- [SDR SWAA2025080790243](https://openairdocs.org/sdr/SWAA2025080790243.md): Shield · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > COROSSION ON FWD SHIELD AT AFT CARGO COMPARTMENT BS 778; RBL 29; WL 157. REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02 AND DWG 146A0081 ID:0025 REV: A.
- [SDR SWAA2025080790223](https://openairdocs.org/sdr/SWAA2025080790223.md): Shear Web · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR WEB AT BS986+7 RBL38; WL 208. REPAIRED PER EA#25-153-01909-WIP1.
- [SDR SWAA2025080790236](https://openairdocs.org/sdr/SWAA2025080790236.md): Attach Angle · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > COROSSION ON ATTATCH ANGLE AT AFT CARGO COMPARTMENT BS 790; RBL 27; WL 158. AFTER FURTHER INVESTIGATION AND SOLVENT CLEANING DISCREPANCIES AREA PER SOPM 20-30-03. NO CORROSION FOUND ON DISCREPANCIES AREAS PER SRM 51-10-02.
- [SDR SWAA2025080790235](https://openairdocs.org/sdr/SWAA2025080790235.md): Intercostal · cracked · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS440 LBL25 WL155. REMOVED AND REPLACED ANGLE AT FCB BS440 LBL 25 WL 155<BR>IAW SRM 51-40-02 AND DWG 143A7505 REV:-.
- [SDR SWAA2025080790242](https://openairdocs.org/sdr/SWAA2025080790242.md): Shield · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FCB BS500 -BS500A RBL23 WL156. REMOVED AND REPLACED AFT SHIELD AT FCB BS500-BS500A RBL23 IAW B737-7 SRM 51-40-02-0G-0 AND DWG: 143A8126 ID:0010 REV: A.
- [SDR SWAA2025080790233](https://openairdocs.org/sdr/SWAA2025080790233.md): Stub Frame · cracked · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; 0.6'' ABOVE EDGE OF SEAL DEPRESSOR; BETWEEN S-8R AND S-9R; LENGTH 1'. REMOVED AND REPLACED STUB FRAME P/N 141A8370U13 AT FSD UPPER CORNER FWD AREA PER SRM 51-40-02 AND DWG 141A8370 REV: D.
- [SDR SWAA2025080790239](https://openairdocs.org/sdr/SWAA2025080790239.md): Seat Track · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 25 AT BS500A+8; BS500A+17; BS500C+11; BS500D+10.. REPLACED IN CUSTOMER CARD ID: TTG8Q013R6Z6.
- [SDR SWAA2025080790248](https://openairdocs.org/sdr/SWAA2025080790248.md): Seat Track · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 AT BS480+16; BS500+7; BS500A+7. REPLACED IN CUSTOMER CARD ID: TTG8Q013R773.
- [SDR SWAA2025080790261](https://openairdocs.org/sdr/SWAA2025080790261.md): Seat Track · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 AT BS500A+17; BS500B+18; BS500D+10. REPLACED IN CUSTOMER CARD ID: TTG8Q013R773.
- [SDR SWAA2025080690226](https://openairdocs.org/sdr/SWAA2025080690226.md): Floor Panel · delaminated · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231JF HAS AREAS OF DELAMINATION ON LOWER SURFACE. FABRICATION OF NEW 231JF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025080690227](https://openairdocs.org/sdr/SWAA2025080690227.md): Floor Panel · delaminated · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF DELAMINATION. FLOOR PANEL 241UF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 146A5810-470.
- [SDR SWAA2025080690228](https://openairdocs.org/sdr/SWAA2025080690228.md): Floor Panel · delaminated · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 242VF UPPER SURFACE HAS AREAS OF DELAMINATION. REPAIRED AFT CABIN FLOOR PANEL 242VF IAW EA 25-153-01883.
- [SDR SWAA2025080690238](https://openairdocs.org/sdr/SWAA2025080690238.md): Sidewall Support · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR TO SIDE WALL SUPPORT HAS CORROSION BTW BS 727E+13 AND BS 759; RBL 29; WL 157. REMOVED AND REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT FROM BS 727+4.04 TO BS 767 IAW SRM 51-40-02 AND DWG 146A7500 ID:0001 REV: B. REFER TASK (TTG8Q013NK43).
- [SDR SWAA2025080690240](https://openairdocs.org/sdr/SWAA2025080690240.md): Sidewall Support · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR TO SIDE WALL SUPPORT HAS CORROSION BTW BS 727B+7 AND BS 727E+10; RBL 29; WL 157. REMOVED AND REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT FROM BS 727+4.04 TO BS 767 IAW SRM 51-40-02 AND DWG 146A7500 ID:0001 REV: B.
- [SDR SWAA2025080690241](https://openairdocs.org/sdr/SWAA2025080690241.md): Support · corroded · Jul 10, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS480 - BS500B LBL23 WL156. REMOVED AND REPLACED SIDEWALL SUPPORT BS396 TO BS500D LBL23 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV: -;[02] REJECTION OF STEP 4 ITEM 4: FWD BULKHEAD LOWER SUPPORT INSTALLED WI
- [SDR SWAA2025080689845](https://openairdocs.org/sdr/SWAA2025080689845.md): Floorbeam · corroded · Jul 9, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANGE OF BS 986 FLOORBEAM AT RBL 43 NUTPLATE HOLE; WL 208. REPAIRED BS 986 FLOORBEAM UPPER FLANGE RBL 43 IAW SRM 53-70-51-2R-6 REPAIR 6.
- [SDR SWAA2025080689844](https://openairdocs.org/sdr/SWAA2025080689844.md): Floorbeam · damaged · Jul 9, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > ELONGATED FASTENER HOLE ON PREVIOUS REPAIR UPPER FLANGE OF BS 986 FLOORBEAM AT LBL 43 NUTPLATE HOLE; WL 208. REMOVED AND REPLACED BS 986 FLOOR BEAM UPPER FLANGE LBL 43 PREVIOUS REPAIR FILLER IAW 53-70-51-2R-6 REPAIR 6.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025080789494](https://openairdocs.org/sdr/SWAA2025080789494.md): Attach Angle · cracked · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ATTACH ANGLE AT PASSENGER COMPARTMENT BS 691; RBL 2; WL 208. REMOVED AND REPLACED ATTACH ANGLE AT PASSENGER COMPARTMENT BS 691; RBL 2; WL 208 I.A.W SRM 51-40-02-0G-0 AND DWG 273A9111.
- [SDR SWAA2025080789496](https://openairdocs.org/sdr/SWAA2025080789496.md): Floorbeam · cracked · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 44; WL 208. REMOVED CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 44; WL 208 IAW SRM 51-40-02 AND REPLACED FOR NEW PANEL BRAKE P/N 143A5240-40; LOTE:1601360-1 BN 51; IAW SRM 51-40-05 AND DWG
- [SDR SWAA2025080789502](https://openairdocs.org/sdr/SWAA2025080789502.md): Floorbeam · cracked · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 27; WL 208. REMOVED AND REPLACED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 27; WL 208; IAW SRM 51-40-05 AND DWG 143A0060 REV: -.
- [SDR SWAA2025080689499](https://openairdocs.org/sdr/SWAA2025080689499.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231ZF HAS AREAS OF DELAMINATION ON UPPER SKIN. PASSENGER CABIN FLOOR PANEL 231ZF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.
- [SDR SWAA2025080689492](https://openairdocs.org/sdr/SWAA2025080689492.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232SF HAS AREAS OF DELAMINATION ON UPPER SKIN. PASSENGER CABIN FLOOR PANEL 232SF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.
- [SDR SWAA2025080689500](https://openairdocs.org/sdr/SWAA2025080689500.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241AF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-127.
- [SDR SWAA2025080689493](https://openairdocs.org/sdr/SWAA2025080689493.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241BF HAS AREA OF DELAMINATION ON LOWER SKIN. FABRICATION OF NEW 241BF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025080689501](https://openairdocs.org/sdr/SWAA2025080689501.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025080689497](https://openairdocs.org/sdr/SWAA2025080689497.md): Floor Panel · pulled · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242CF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242CF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025080689498](https://openairdocs.org/sdr/SWAA2025080689498.md): Floor Panel · delaminated · Jul 8, 2025 · N912WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER SRM 53-00-50-2R-0-A00938.
- [SDR SWAA2025080689505](https://openairdocs.org/sdr/SWAA2025080689505.md): Skin · cracked · Jul 8, 2025 · N912WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90; 18' FROM FWD EDGE; L:0.3'. REPAIRED PER EA 25-155-01939 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 25-155-01939-INSP.
- [SDR SWAA2025051470322](https://openairdocs.org/sdr/SWAA2025051470322.md): Megaphone · broken · May 12, 2025 · N912WN · Boeing 7377H4 · Emergency Equipment
  > AFT FLIGHT ATTENDANT MEGAPHONE HANDLE IS BROKEN<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-SWA-804-NG-01 (REMOVE AND REPLACE MEGAPHONE - PERMANENT)]

Next page: https://openairdocs.org/aircraft/N912WN/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 = 'N912WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N912WN/reports

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