# Service difficulty reports: N412WN, cancelled Sep 30, 2025

A list on [N412WN, cancelled Sep 30, 2025](https://openairdocs.org/deregistered/N412WN-2025-09-30.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 8 · 359 reports

- [SDR SWAA2025041524221](https://openairdocs.org/sdr/SWAA2025041524221.md): Light · inoperative · Apr 13, 2025 · N412WN · Boeing 7377H4 · Emergency Lighting
  > LH AFT EXTERIOR EMERGENCY LIGHT INOP <[01]. RELAMPED LH AFT EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025031704756](https://openairdocs.org/sdr/SWAA2025031704756.md): Handle · loose · Mar 13, 2025 · N412WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR INTERIOR HANDLE LOOSE <[01.] TIGHTENED L1 DOOR INTERIOR HANDLE PER AMM 53-13-11.
- [SDR SWAA2025031704755](https://openairdocs.org/sdr/SWAA2025031704755.md): Handle · loose · Mar 13, 2025 · N412WN · Boeing 7377H4 · Service Doors
  > R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.
- [SDR SWAA2024071010270](https://openairdocs.org/sdr/SWAA2024071010270.md): Sign · missing · Jul 7, 2024 · N412WN · Boeing 7377H4 · Emergency Lighting
  > OVERWING EXIT SIGN COVER MISSING RT SIDE<[01] INSTALLED MISSING EXIT SIGN IN REFERENCE TO AMM 33-51-01
- [SDR SWAA2024062002980](https://openairdocs.org/sdr/SWAA2024062002980.md): Sensor · faulted · Jun 18, 2024 · N412WN · Boeing 7377H4 · Landing Gear Position and Warning
  > AFTER TAKEOFF GEAR HANDLE IN THE UP POSITION; NOSE GEAR DISAGREE LIGHT ILLUMINATED ON FORWARD PANEL WITH GREEN NOSE GEAR LIGHT ILLUMINATED ON OVERHEAD PANEL. AFTER SELECTING GEAR DOWN RECEIVED THREE GREEN DOWN LIGHTS ON FORWARD AND OVERHEAD PANEL. ON LANDING R
- [SDR SWAA2024052889482](https://openairdocs.org/sdr/SWAA2024052889482.md): Battery Pack · inoperative · May 24, 2024 · N412WN · Boeing 7377H4 · Emergency Lighting
  > FOUND 5 EACH EMERGENCY LIGHT IN AFT LEFT CABIN WONT TURN ON.<[01] R/R AFT L/H EMERGENCY BATTERY PACK PER AMM 33-51-06 AND OPS CHECK GOOD.
- [SDR SWAA2024050983337](https://openairdocs.org/sdr/SWAA2024050983337.md): Slide · unsecure · May 7, 2024 · N412WN · Boeing 7377H4 · Escape Slide
  > FLIGHT ATTENDANT REPORTS L1 DOOR SLIDE NOT SECURED IN CONTAINER<[01] RE-INSTALLED L1 DOOR SLIDE IN THE CONTAINER IAW AMM 25-66-01 AND MT 725-61-06
- [SDR SWAA2024040971555](https://openairdocs.org/sdr/SWAA2024040971555.md): Glowstrip · unsecure · Apr 6, 2024 · N412WN · Boeing 7377H4 · Emergency Equipment
  > GLOW STRIP NEAR FWD GALLEY; FO SIDE PULLING UP FROM FLOOR.<[01] RESECURED PHOTOLUMINESCENT STRIP; NEAR FWD GALLEY FO SIDE REF AMM 33-51-15.
- [SDR SWAA2024032567050](https://openairdocs.org/sdr/SWAA2024032567050.md): Transmitter · split · Mar 23, 2024 · N412WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > ON APPROACH FLAP SPLIT BETWEEN UP AND 1.<[01] REMOVED AND REPLACED LH FLAP POSITION TRANSMITTER PER AMM 27-58-01. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024032166259](https://openairdocs.org/sdr/SWAA2024032166259.md): Slide · out of adjust · Mar 21, 2024 · N412WN · Boeing 7377H4 · Escape Slide
  > EMERGENCY SLIDE F/O'S SIDE REAR IS HANGING INCORRECTLY<[01] ACCOMPLISHED MT# 725-61-06; SLIDE REMOVAL AND INSTALLATION; FOR POSITION AND SECURITY VERIFICATION.
- [SDR SWAA2024012242687](https://openairdocs.org/sdr/SWAA2024012242687.md): Seal · cracked · Jan 19, 2024 · N412WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL HAS A 3' CRACK ON THE FORWARD LOWER SIDE WHERE IT MEETS THE SLIDING SEAL TRACK.<[01] R&R RH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2023103015901](https://openairdocs.org/sdr/SWAA2023103015901.md): Slide · out of adjust · Oct 28, 2023 · N412WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE IS HANGING DOWN<[01] ADJUSTED FWD ENTRY DOOR SLIDE PER MT 725-61-06. OK TO CONTINUE
- [SDR SWAA2023092002544](https://openairdocs.org/sdr/SWAA2023092002544.md): Module · faulty · Sep 19, 2023 · N412WN · Boeing 7377H4 · Flight Environment Data
  > AFTER TAKEOFF CAME ON THREE DIFFERENT TIMES. 20KTS SPLIT BETWEEN CA AND F.O. INDICATORS. AFTER VERIFYING AIRSPEED WITH STAY IT WAS THE CAPTAINS SIDE THAT WAS OFF<[01] R&R'D LEFT PITOT AIR DATA MODULE PER MM 34-21-04 OPS CKS GOOD AND C/W LEFT PITOT SYSTEM LEAK
- [SDR SWAA2023061558608](https://openairdocs.org/sdr/SWAA2023061558608.md): Sign · detached · Jun 13, 2023 · N412WN · Boeing 7377H4 · Emergency Lighting
  > THE EMERGENCY EXIT ROW SIGN IS DETACHED FROM THE CEILING<[01] R/R EMERGENCY EXIT OVERHEAD SIGN IAW MM 33-51-03. OP?S CK NORMAL
- [SDR SWAA2023052451656](https://openairdocs.org/sdr/SWAA2023052451656.md): Battery Pack · failed · May 24, 2023 · N412WN · Boeing 7377H4 · Emergency Lighting
  > CABIN FWD GALLEY AREA; ONE EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST<[01] REMOVED & REPLACED ONE EMERGENCY BATTERY PACK (M01675); AT FWD GALLEY AREA; PER AMM 33-51-06
- [SDR SWAA2023042730902](https://openairdocs.org/sdr/SWAA2023042730902.md): Girt Bar · loose · Apr 24, 2023 · N412WN · Boeing 7377H4 · Escape Slide
  > FED AFT GIRT BAR FITTING IS LOOSE<[01] TIGHTENED FED AFT GIRT BAR FITTING; PERFORMED INSTALLATION TEST CHECKS GOOD PER AMM 25-66-02-400-801;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION. JOB COMPLETE.
- [SDR SWAA2023042827531](https://openairdocs.org/sdr/SWAA2023042827531.md): Rib · cracked · Apr 14, 2023 · N412WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND ON THE RH HORIZONTAL RIB LOWER FLANGE AT STAB STA 193.9; 25' FROM THE LE.<REMOVED DAMAGED IN AN AREA OF 1.8' X 0.8' PER SRM 55-10-09-2R-5 REP 5.; FABRICATED; LOCATED; DRILLED; AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 55-10-09-2R-5
- [SDR SWAA2023042725491](https://openairdocs.org/sdr/SWAA2023042725491.md): Light · inoperative · Apr 10, 2023 · N412WN · Boeing 7377H4 · Emergency Lighting
  > FWD EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT IS INOP<[01] RELAMPED IAW AMM 33-51-01-960-801;[02] RELAMPED AND GOOD OP-CHECK IAW AMM 33-51-01-960-801 AND AMM 33-51-00-710-801.;[03] CERTIFIED ACTION 1 AND 2.;[04] FINAL INSPECTION. JOB COMPLETE.
- [SDR SWAA2023042824466](https://openairdocs.org/sdr/SWAA2023042824466.md): Skin · cracked · Apr 6, 2023 · N412WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND RH STAB STA 193.9 25' FROM FWD EDGE 0.4'L<REMOVED DAMAGED SKIN ON R/H HORZ STAB LOWER SKIN STA 193.9 25' FROM FWD EDGE IN AN AREA OF 2.6' X 1.7' IAW SRM 55-10-01-2R-11 REP.11.; FABRICATED; LOCATED; DRILLED; AND APPLIED CHEMICAL CONVERSION COATING A
- [SDR SWAA2023042824467](https://openairdocs.org/sdr/SWAA2023042824467.md): Skin · cracked · Apr 6, 2023 · N412WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND LH HORZ STAB LOWER SKIN STA 193.9 17' FROM FWD EDGE.8'L<REMOVED DAMAGED SKIN ON LH HORZ STAB LOWER SKIN STA 193.9 17' FROM FWD EDGE IAW SRM 55-10-01-2R-11 REP.11 STEP 4.B.1.; IN AN AREA OF 1.5' X 2.7'FABRICATED; LOCATED; DRILLED; AND APPLIED CHEMI
- [SDR SWAA2023042724461](https://openairdocs.org/sdr/SWAA2023042724461.md): Stringer Clip · cracked · Apr 6, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON PASSENGER CABIN STRINGER CLIP AT BS 727D STRINGER 4R.<[01] DISPLACED INSULATION BLANKETS AT STRINGER CLIP AT BS 727D STR 4R TO FOM AS PER M/M 25-80-00-000-801;[02] NO ALLOWABLE DAMAGED ON STRINGER CLIP AND WILL BE REPLACE IAW SRM 51-10-02 STEP 9. REMO
- [SDR SWAA2023042823693](https://openairdocs.org/sdr/SWAA2023042823693.md): Angle · corroded · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE AT MID CABIN BS663+29 RBL66 WL203.<[01] NO ALLOWABLE LIMITS FOUND DAMAGE TO BE REMOVED I.A.W SRM 51-10-02-0G-0 AND SUBMITTED ENGINEERING FOR FURTHER INSTRUCTION.;[02] REMOVED CORROSION ON ANGLE SURFACE AT MID CABIN BS692 RBL64-RBL65 WL203 1'
- [SDR SWAA2023042823696](https://openairdocs.org/sdr/SWAA2023042823696.md): Attach Angle · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID CABIN BS663+28 LBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 LBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPARABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2023042823697](https://openairdocs.org/sdr/SWAA2023042823697.md): Attach Angle · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID CABIN BS663+28 RBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 RBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC.9 REMOVED ATTACH ANGLE AT BS 663
- [SDR SWAA2023042823699](https://openairdocs.org/sdr/SWAA2023042823699.md): Attach Angle · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID CABIN BS663+29 LBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGEL AT MID CABIN BS 663+29 LBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO DAMAGE LIMITS GIVEN IN SRM PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED C
- [SDR SWAA2023042823552](https://openairdocs.org/sdr/SWAA2023042823552.md): Angle · corroded · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE AT MID CABIN BS719 LBL67 WL203.<[01] NO ALLOWABLE LIMITS FOUND DAMAGE TO BE REMOVED I.A.W SRM 51-10-02-0G-0 AND SUBMITTED ENGINEERING FOR FURTHER INSTRUCTION.;[02] REMOVED 1EA RIVET TO REMOVED CORROSION ON ANGLE SURFACE I.A.W SRM 51-40-02-0G
- [SDR SWAA2023042823553](https://openairdocs.org/sdr/SWAA2023042823553.md): Angle · corroded · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE AT MID CABIN BS713 LBL63; LBL65 WL203.< REMOVED FOR ACCESS 2EA RIVET AT MID CABIN BS713 LBL63; LBL65 TO REMOVED CORROSION ON ANGLE SURFACE I.A.W SRM 51-40-02-0G-0;[03] REMOVED CORROSION ON ANGLE SURFACE AT MID CABIN BS713 LBL63 1'X1' AREA AN
- [SDR SWAA2023042823698](https://openairdocs.org/sdr/SWAA2023042823698.md): Attach Angle · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID CABIN BS663+29 RBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT MID CABIN BS 663+29 RBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPARABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED CORRE
- [SDR SWAA2023042823700](https://openairdocs.org/sdr/SWAA2023042823700.md): Floor Support · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT IS CRACKED BS540 LBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] LOCATED AND DRILLED NEW PANEL BREAK BS540 LBL1-LBL24 WL208 I.A.W BOEIN
- [SDR SWAA2023042823701](https://openairdocs.org/sdr/SWAA2023042823701.md): Floor Support · cracked · Apr 4, 2023 · N412WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT IS CRACKED BS540 RBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] LOCATED AND DRILLED NEW PANEL BREAK BS540 RBL1-RBL24 WL208 I.A.W BOEIN
- [SDR SWAA2023042823364](https://openairdocs.org/sdr/SWAA2023042823364.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<REMOVED DAMAGED SECTION OF S-23R BETWEEN BS 500D TO 540; RECEIVED STRINGER SECTION FROM OSS R.O # 913326-SWA IAW SRM 53-00-03-2R-1 REP.1 PAR.D;[08] VERIFIED CORRECTIVE ACTION #7;[09] RECEIVED STRING
- [SDR SWAA2023042823363](https://openairdocs.org/sdr/SWAA2023042823363.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<REMOVED DAMAGED SECTION OF S-26L BETWEEN BS 500D TO 540 RECEIVED STRINGER SECTION FROM OSS R.O # 913325-SWA IAW SRM 53-00-03-2R-1 REP.1 PAR.D;[08] VERIFIED CORRECTIVE ACTION STEP 7.;[09] RECEIVED ST
- [SDR SWAA2023042823360](https://openairdocs.org/sdr/SWAA2023042823360.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. MARKED<REMOVED DAMAGED SECTION OF S-23L BETWEEN BS 500D TO 540 RECEIVED STRINGER SECTION FROM OSS R.O # 913318-SWA IAW SRM 53-00-03-2R-1 REP.1 PAR.D;[08] VERIFIED CORRECTIVE ACTION STEP 7.;[09] RECEIVED ST
- [SDR SWAA2023042823365](https://openairdocs.org/sdr/SWAA2023042823365.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<REMOVED DAMAGED SECTION OF S-26R BETWEEN BS 500D TO 540; PERFORMED DVI ON REPAIR AREA AND NO ADDITIONAL DAMAGE FOUND IAW SRM 53-00-03-2R-1 REP.1 PAR. 4 A-B.;[04] REQUIRED NDI HFEC CRACK FREE CUT OUT
- [SDR SWAA2023042823366](https://openairdocs.org/sdr/SWAA2023042823366.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<REMOVED DAMAGED SECTION OF S-27R BETWEEN BS 500D TO 540; PERFORMED DVI ON REPAIR AREA AND NO ADDITIONAL DAMAGE FOUND IAW SRM 53-00-03-2R-1 REP.1 PAR. 4 A-BRECEIVED STRINGER SECTION FROM OSS R.O # 91
- [SDR SWAA2023042823223](https://openairdocs.org/sdr/SWAA2023042823223.md): Spar · corroded · Apr 3, 2023 · N412WN · Boeing 7377H4 · Wing Spar
  > ***CORROSION*** ON LEFT WING REAR SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IRSS145.<REMOVED CORROSION ON LEFT WING REAR SPAR WEB AROUND BOOST PUMP UPPER BONDING JUMPER IRSS145 IAW SRM 57-20-10-1A-3. ALLOWABLE DAMAGE 3 STEP 2.B.(1 - 3) ON BLENDED AREA NOTED
- [SDR SWAA2023042823224](https://openairdocs.org/sdr/SWAA2023042823224.md): Spar · corroded · Apr 3, 2023 · N412WN · Boeing 7377H4 · Wing Spar
  > ***CORROSION*** ON LEFT WING REAR SPAR AROUND BOOST PUMP LOWER BONDING JUMPER IRSS145.<REMOVED CORROSION ON LEFT WING REAR SPAR WEB AROUND BOOST PUMP LOWER BONDING JUMPER IRSS145 IAW SRM 57-20-10-1A-3. ALLOWABLE DAMAGE 3 STEP 2.B.(1 - 3) CORROSION NOTED WITHIN
- [SDR SWAA2023042723362](https://openairdocs.org/sdr/SWAA2023042723362.md): Stringer · cracked · Apr 3, 2023 · N412WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25L WL155. MARKED<[01] NO ALLOWABLE DAMAGED FOUND ON SRM FOR CRACK ON FCB BS535 S-25L WL164; VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1 FOR STR-25L REPAIR.[07] RECEIVED STRINGER SECTION FROM OSS R.O # 913323-S
- [SDR SWAA2023010386699](https://openairdocs.org/sdr/SWAA2023010386699.md): Power Supply · inoperative · Dec 31, 2022 · N412WN · Boeing 7377H4 · Emergency Lighting
  > LH EMERGENCY EXIT LIGHTS ARE ALL OUT. REPLACED LH EMERGENCY EXIT POWER SUPPLY PER AMM 33-51-06 OPS CHECK GOOD FOR ALL APPLICABLE LIGHTS
- [SDR SWAA2022102863757](https://openairdocs.org/sdr/SWAA2022102863757.md): Seal · cracked · Oct 25, 2022 · N412WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STAB FORWARD UPPER SLIDING SEAL IS CRACKED / [01] R&R R/H HORIZONTAL STAB FORWARD UPPER SLIDING SEAL. IAW AMM 53-31-31
- [SDR SWAA2022102763766](https://openairdocs.org/sdr/SWAA2022102763766.md): Angle · cracked · Oct 25, 2022 · N412WN · Boeing 7377H4 · Galley Doors
  > AFT GALLEY DOOR LINER LOWER SUPPORT ASSY ANGLE CRACKED AFT SIDE / [01] R&R AFT GALLEY DOOR LINER LOWER SUPPORT ASSY ANGLE PER AMM 52-41-31
- [SDR SWAA2022031481351](https://openairdocs.org/sdr/SWAA2022031481351.md): Plate · cracked · Mar 9, 2022 · N412WN · Boeing 737* · Wing, Control Surfaces
  > R/H WING LOWER TRAILING EDGE SHELF PANEL; JUST OUTBOARD OF THE #6 FLAP TRACK FAIRING HAS A WAFFLE PLATE CRACKED OUT WITH A MISSING NUT PLATE AT ORSS 263; JUST ABOVE THE #2 PYLON AFT FAIRING. / [01] R/R WAFFLE PANEL REF SRM 51-40-02. INSTALLED ONLY 4 OUT 5 FAST
- [SDR SWAA2022022275459](https://openairdocs.org/sdr/SWAA2022022275459.md): Light · inoperative · Feb 19, 2022 · N412WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVER WING EXIT LIGHT INOP. / [01] RE-LAMPED L/H OVER WING EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2022022173744](https://openairdocs.org/sdr/SWAA2022022173744.md): Sign · loose · Feb 17, 2022 · N412WN · Boeing 737* · Emergency Lighting
  > EMERGENCY EXIT SIGN IN AFT GALLET NEAR SERVICE DOOR LOOSE / [01] R/R'D AFT GALLEY SERVICE DOOR EMERGENCY EXIT ASSY AS PER AMM 33-51-01
- [SDR SWAA2022012562987](https://openairdocs.org/sdr/SWAA2022012562987.md): Light · broken · Jan 21, 2022 · N412WN · Boeing 7377H4 · Emergency Lighting
  > R/H OVERWING EXIT SIGN COVER BROKEN; / [01] R AND R'D EXIT SIGN ASSY PER AMM-33-51-01<BR>OPS NORMAL.
- [SDR SWAA2022010557434](https://openairdocs.org/sdr/SWAA2022010557434.md): Dome · delaminated · Jan 1, 2022 · N412WN · Boeing 737 · Fuselage Main, Structure
  > SUPPLEMENTAL INFORMATION: 4 HOLE AND DELAMINATION ON RADAR DOME; NOTED 4 HOLES AND DELAMINATION ON RADAR DOME / [01] TEMP REPAIRED PER SRM53-10-72; [02] CONFIRMED SRM REFERENCE 53-10-72-1A-1 IS THE CORRECT REFERENCE FOR THIS INTERIM REPAIR.
- [SDR SWAA2021121351544](https://openairdocs.org/sdr/SWAA2021121351544.md): Sign · loose · Dec 9, 2021 · N412WN · Boeing 737 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION: R/H OVERWING EXIT SIGN FELL OFF; / [01] RESECURED R/H OVERWING EXIT SIGN IAW AMM 33-51-01. A/C OK FOR SERVICE
- [SDR SWAA2021110133339](https://openairdocs.org/sdr/SWAA2021110133339.md): Panel · elongated · Oct 26, 2021 · N412WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193D HAS SEVERAL ELONGATED FASTENER HOLES.; / [01] LOCATED HOLE IN NEW PANEL PER EO 5351-I-14642-NG; [02] REMOVED AND REPLACED PANEL PER SRM 51-10-02 AND 51-40-02.; [03] C/W
- [SDR SWAA2021091316281](https://openairdocs.org/sdr/SWAA2021091316281.md): Handle · inoperative · Sep 9, 2021 · N412WN · Boeing 7377H4 · Escape Slide
  > COVER FOR AFT SERVICE DOOR SLIDE MANUAL INFLATION HANDLE NOT INSTALLED; / [01] UNTUCKED MANUAL SLIDE INFLATION HANDLE COVER IAW SIP ON AFT SERVICE DOOR (R2)
- [SDR SWAA2021082409132](https://openairdocs.org/sdr/SWAA2021082409132.md): Slide · out of position · Aug 22, 2021 · N412WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE FELL OUT OF THE COVER.; / [01] REINSTALLED/REPOSITIONED AFT ENTRY DOOR SIDE IN THE COVER PER AMM 25-66-01. A/C OK FOR SERIVCE.

Next page: https://openairdocs.org/deregistered/N412WN-2025-09-30/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 = 'N412WN' AND deregistration_id = 'N412WN-2025-09-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N412WN-2025-09-30/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.