# Service difficulty reports: N416WN, cancelled Sep 29, 2025

A list on [N416WN, cancelled Sep 29, 2025](https://openairdocs.org/deregistered/N416WN-2025-09-29.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 · 271 reports

- [SDR SWAA2025042846003](https://openairdocs.org/sdr/SWAA2025042846003.md): Lamp · inoperative · Apr 22, 2025 · N416WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 12 ABC AND 20 ABC INOP<[01] REMOVED AND REPLACE EMERGENCY LIGHT AREA LAMPS AT ROWS 12 ABC AND 20 ABC IAW AMM 33-51-03-960-801-NG. OPS CHECK GOOD.
- [SDR SWAA2025022800213](https://openairdocs.org/sdr/SWAA2025022800213.md): Slide · out of adjust · Feb 27, 2025 · N416WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE AFT ATTACH BOLT BARRELL NUT IS BROKEN <[01]. R/R FWD ENTRY DOOR SLIDE AFT BARREL NUT PER AMM 20-50-11.; [02] INSPECTION C/W.
- [SDR SWAA2025022800212](https://openairdocs.org/sdr/SWAA2025022800212.md): Seal · cracked · Feb 27, 2025 · N416WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > L/H HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED. <[01] REMOVED AND REPLACED SLIDING SEAL PER AMM 53-31-31.; [02] INSPECTED C/A 1. (TECHNICIAN); REMOVED AND REPLACED SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2024102852008](https://openairdocs.org/sdr/SWAA2024102852008.md): Battery Pack · inoperative · Oct 23, 2024 · N416WN · Boeing 7377H4 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS AT 9A AND 12A INOP<[01] R/R M1668 BATTERY PACK AND R/R M1668 BATTERY CHARGER PER AMM 33-51-06 EMERGENCY LIGHTS AT 9A AND 12A OPS CHECK GOOD
- [SDR SWAA2024102854222](https://openairdocs.org/sdr/SWAA2024102854222.md): Charger · inoperative · Oct 23, 2024 · N416WN · Boeing 7377H4 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS AT 9A AND 12A INOP<[01] R/R M1668 BATTERY PACK AND R/R M1668 BATTERY CHARGER PER AMM 33-51-06 EMERGENCY LIGHTS AT 9A AND 12A OPS CHECK GOOD
- [SDR SWAA2024040570934](https://openairdocs.org/sdr/SWAA2024040570934.md): Slide · dislodged · Apr 5, 2024 · N416WN · Boeing 7377H4 · Escape Slide
  > R1 SLIDE FALLING OUT<[01] RESECURED R1 ESCAPE SLIDE REF AMM 25-66-01. OPS CHK GOOD..
- [SDR SWAA2024040469002](https://openairdocs.org/sdr/SWAA2024040469002.md): Lens · missing · Mar 31, 2024 · N416WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD BIN LIGHT ROW 9 CAPTAINS SIDE 'COVER'<[01] REPLACED MISSING AREA EMERGENCY LIGHT LENS AS PER AMM 33-51-03.
- [SDR SWAA2024020247258](https://openairdocs.org/sdr/SWAA2024020247258.md): Lens · loose · Feb 1, 2024 · N416WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ASSEMBLE ON BULL NOSE PANEL LOOSE @ 9 CBA<[01] SECURED LENS REF AMM 33-51-03
- [SDR SWAA2023100507197](https://openairdocs.org/sdr/SWAA2023100507197.md): Light · inoperative · Oct 4, 2023 · N416WN · Boeing 7377H4 · Emergency Lighting
  > R/H OVERWING EXIT AFT EMERGENCY LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01
- [SDR SWAA2023100507196](https://openairdocs.org/sdr/SWAA2023100507196.md): Light · inoperative · Oct 4, 2023 · N416WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVERWING EXIT FWD EMERGENCY LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01
- [SDR SWAA2023052551347](https://openairdocs.org/sdr/SWAA2023052551347.md): Battery Pack · inoperative · May 23, 2023 · N416WN · Boeing 7377H4 · Emergency Lighting
  > ASD EXTERIOR EMERGENCY LIGHT IS INOP.<[01] REPLACED BATTERY PACK M1672; PERFORMED GOOD TEST OF THE RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023052544413](https://openairdocs.org/sdr/SWAA2023052544413.md): Threshold · cracked · May 3, 2023 · N416WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CAL DUE
- [SDR SWAA2023052544414](https://openairdocs.org/sdr/SWAA2023052544414.md): Threshold · cracked · May 3, 2023 · N416WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CAL DUE DATE
- [SDR SWAA2023052545197](https://openairdocs.org/sdr/SWAA2023052545197.md): Barrier · debonded · May 3, 2023 · N416WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET ARE MOISTURE BARRIER DISBONDED FROM FLOOR PANEL 8 INCHES AFT OF FWD LAV.<[01] APPLIED LS4410 SEALANT TO DAMAGE AREA AS NEEDED PER AMM 53-21-00-300-801-NG.;[02] APPLIED LS4410 SEALANT TO DAMAGE AREA AS NEEDED PER AMM 53-21-00-300-801;[03] VERIFIED CORRE
- [SDR SWAA2023053043803](https://openairdocs.org/sdr/SWAA2023053043803.md): Floor Support · cracked · May 2, 2023 · N416WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT AT STA 540; RBL 1; WL 207.8<[01] NO DAMAGE LIMITS GIVEN IN SRM; PART HAS MULTIPLE CRACKS; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9; REMOVED CRACK DAMAGED BREAK PANEL FROM BS 540 RBL 1 TO RBL 23 WL 206.5 IAW SRM 51-40
- [SDR SWAA2023053043805](https://openairdocs.org/sdr/SWAA2023053043805.md): Floor Support · cracked · May 2, 2023 · N416WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CRACKED FLOOR SUPPORT AT STA 540; LBL 1; WL 207.8<[01] NO DAMAGE LIMITS GIVEN IN SRM; PART HAS MULTIPLE CRACKS; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9; REMOVED CRACK DAMAGED BREAK PANEL ASSYEMBLY AT BS 540 LBL1 TO LBL 23 IAW SRM 51-40-0
- [SDR SWAA2023053043795](https://openairdocs.org/sdr/SWAA2023053043795.md): Bracket · broken · May 1, 2023 · N416WN · Boeing 7377H4 · Nacelle/Pylon Structure
  > #2 ENGINE STRUT O/B FIRE SEAL BRACKET (P/N 311A2683-16) UPPER FLANGE IS BROKEN<[01] REMOVED #2 ENGINE STRUT O/B FIRE SEAL BRACKET P/N 311A2683-16 IAW SRM 51-40-2-0G-0;[02] UPDATED PARTS REQUIREMENTS;[03] ADDED; AND UPDATED STEP #1;[04] INSTALLED NEW #2 ENGINE
- [SDR SWAA2023053043797](https://openairdocs.org/sdr/SWAA2023053043797.md): Support · cracked · May 1, 2023 · N416WN · Boeing 7377H4 · Trailing Edge Flaps
  > BULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED CRACKED BULB SEAL RETAINER SUPPORT CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON AND INSTALLED NEW RETAINER PART NUMBER 115A2953-1 SAME L
- [SDR SWAA2023052643681](https://openairdocs.org/sdr/SWAA2023052643681.md): Seat Track · corroded · May 1, 2023 · N416WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 BS727C+2 WL208.<[01] LOCATED AND REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 BS727C+2 WL208 PER SRM 51-10-02-0G-0 FOUND IT TO BE IN LIMITS PER SRM53-00-52-1A-1 2'.1'X.08' WELL 3'X.5'X.015' CROWN<BR>DEPTH
- [SDR SWAA2023052643684](https://openairdocs.org/sdr/SWAA2023052643684.md): Seat Track · corroded · May 1, 2023 · N416WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS540 BS610; BS608; BS633 WL208.<[01] PARTIAL UPDATE STEP 4.;[02] VERIFIED SRM 53-00-52-1A-1 IS APPLICABLE.;[03] VERIFIED CORROSION REMOVED STEPS 1;2;3;4 AND MEASUREMENT TABLE; (PARTIAL).;[04] PARTIAL UPDATE STEPS
- [SDR SWAA2023052643787](https://openairdocs.org/sdr/SWAA2023052643787.md): Seat Track · corroded · May 1, 2023 · N416WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS727C+2; 747+2; 747+15;813; 827+16; 827+28 WL208.<[01] PARTIAL COMPLETED STEPS 1-6 LOCATED AND REMOVED CORROSION.;[02] VERIFIED SRM 53-00-52-1A-1 IS APPLICABLE.;[03] VERIFIED CORROSION REMOVED STEPS 1;2;3;4;5;6; A
- [SDR SWAA2023052643788](https://openairdocs.org/sdr/SWAA2023052643788.md): Seat Track · corroded · May 1, 2023 · N416WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS385; BS380+13; BS410; BS455 WL208.<[01] VERIFIED THAT SRM 53-00-52-1A-1 IS APPLICABLE.;[02] PARTIAL UPDATE STEPS 1-4. UPDATED MEASUREMENT TABLE.;[03] VERIFIED (PARTIALS) STEPS 1;2;3;4 AND MEASUREMENT TABLE; OUTS
- [SDR SWAA2023052643790](https://openairdocs.org/sdr/SWAA2023052643790.md): Seat Track · corroded · May 1, 2023 · N416WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS540+12;613; 663+16; 693; 712; 727+15 WL208.<[01] VERIFIED THAT SRM 53-00-52-1A-1 IS APPLICABLE.;[02] PARTIAL UPDATE STEPS 1-6. UPDATED MEASUREMENT TABLE.;[03] UPDATED MEASUREMENT TABLE.;[04] VERIFIED STEP 1;2;3;4
- [SDR SWAA2023053043455](https://openairdocs.org/sdr/SWAA2023053043455.md): Angle · cracked · Apr 30, 2023 · N416WN · Boeing 7377H4 · Trailing Edge Flaps
  > RT WING FIXED TE UPPER PANEL; VERTICAL BULB SEAL RETAINER ANGLE CRACKED; DIRECTLY AFT OF THE PYLON; MARKED.<[01] THERE IS NO SRM ALLOWABLE DAMAGE FOR RT WING FIXED TE UPPER PANEL; VERTICAL BULB SEAL RETAINER ANGLE CRACK. PART TO BE REPAIRED BY REPLACEMENT IAW
- [SDR SWAA2023053042815](https://openairdocs.org/sdr/SWAA2023053042815.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > MAIN DISTRIBUTION BAY CRACK ON END OF STR 26R BS 540<REMOVED DAMAGED SECTION OF STRINGER 26R BS 500D+11'-540 IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4-B.;[04] PERFORMED GVI ON REPAIR AREA AND NO ADDITIONAL DAMAGED FOUND IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4-B(1).;[05]
- [SDR SWAA2023052542812](https://openairdocs.org/sdr/SWAA2023052542812.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > MAIN DISTRIBUTION BAY CRACK ON END OF STR 26L BS 540<[01] UPDATED MEASURING TABLE. REMOVED DAMAGED SECTION OF STRINGER 26L BS 500D+11'-540 IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4-B. PERFORMED GVI ON REPAIR AREA AND NO ADDITIONAL DAMAGED FOUND IAW SRM 53-00-03-2
- [SDR SWAA2023052542814](https://openairdocs.org/sdr/SWAA2023052542814.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > MAIN DISTRIBUTION BAY CRACK ON END OF STR 23R BS 540. PERFORMED GVI ON REPAIR AREA AND NO ADDITIONAL DAMAGE FOUND IAW EA 23-153-01413 AND SRM 53-00-03-2R-1 REP.1 PAR 4 B(1). INSTALLED ALL FASTENERS COMMON TO SKIN AND STRINGER SECTION STR-23R BS 500D+11'-54
- [SDR SWAA2023052542829](https://openairdocs.org/sdr/SWAA2023052542829.md): Fitting · loose · Apr 28, 2023 · N416WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR FWD GIRT BAR FITTING LOOSE.<[01] REMOVED CLEANED & REINSTALLED FT SERVICE DOOR FWD GIRT BAR FITTING TORQUED TO SPEC PER AMM 25-66-02-400-801; 25-66-02-000-801; 20-50-11-910-801.<BR>OPS CHECK GOOD.;[02] REMOVED CLEANED & REINSTALLED AFT SERVICE
- [SDR SWAA2023052542475](https://openairdocs.org/sdr/SWAA2023052542475.md): Web · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; LBL 33; WL 202.5. APPROXIMATE LENGTH: 1.5'<[01] DAMAGE FOUND ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; LBL 33; WL 202.5 TO BE REPAIRED IN TTG8Q00KQ86N I.A.W SRM 53-40-51-2R-2 REPAIR 2;[02] VERIFIED CORREC
- [SDR SWAA2023052542477](https://openairdocs.org/sdr/SWAA2023052542477.md): Web · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; RBL 40; WL 202.5. APPROXIMATE LENGTH:.75'<[01] DAMAGE FOUND ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; RBL 40; WL 202.5. TO BE REPAIRED IN TTG8Q00KQ8UG I.A.W SRM 53-40-51-2R-2 REPAIR 2;[02] VERIFIED CORRE
- [SDR SWAA2023052542478](https://openairdocs.org/sdr/SWAA2023052542478.md): Web · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; RBL 42.5; WL 202.5. APPROXIMATE LENGTH:.5'<[01] DAMAGE FOUND ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; RBL 42.5; WL 202.5. TO BE REPAIRED IN TTG8Q00KQ8UG I.A.W SRM 53-40-51-2R-2 REPAIR 2;[02] VERIFIED CO
- [SDR SWAA2023052542479](https://openairdocs.org/sdr/SWAA2023052542479.md): Web · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663+9.5; RBL 41; WL 202.5. APPROXIMATE LENGTH:.75'<[01] HORIZONTAL PRESSURE DECK WEB AT 663+9.5; RBL41; WL202.5 FOUND TO BE OUT LIMITS AND WILL BE REPAIR IAW SRM 53-40-51-2R-2. VERIFIED SRM 53-40-51-2R-2 IS APPLICA
- [SDR SWAA2023052542476](https://openairdocs.org/sdr/SWAA2023052542476.md): Web · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663+2; LBL 37.5; WL 202.5. APPROXIMATE LENGTH:.85'<[01] UPDATED MEASUREMENTS. HORIZONTAL PRESSURE DECK WEB AT 663+2; LBL37.5; WL202.5 FOUND TO BE OUT LIMITS AND WILL BE REPAIR IAW SRM 53-40-51-2R-2. VERIFIED SRM 53
- [SDR SWAA2023052542482](https://openairdocs.org/sdr/SWAA2023052542482.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER S-23L TERMINUS. STA 540<[01] UPDATED MEASUREMENT TABLE.[08] RECEIVED NEW STRINGER SECTION S-23L FROM OSS RO. 917127-SWA-3 IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4D AND EA 23-153-01405.;[09] VERIFIED CORRECTIVE ACTION 8.;[10] RECEIVED STRINGER SPLI
- [SDR SWAA2023052542487](https://openairdocs.org/sdr/SWAA2023052542487.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER S-25R TERMINUS. STA 540<[01] UPDATED MEASUREMENT TABLE AND STEP 1.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] ACCOMPLISHED HFEC SURFACE SCAN OF CUT EDGE IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>ACCOMPLISHED HFEC
- [SDR SWAA2023052542483](https://openairdocs.org/sdr/SWAA2023052542483.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER S-24L TERMINUS. STA 540<[01] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1 AND UPDATED OF MEASUREMENT TABLE.;[02] REMOVED DAMAGED SECTION OF STRINGER 26L BS 500D+11'-540 IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4-B.;09/2023;[07] RECEIVED NEW STR
- [SDR SWAA2023052542484](https://openairdocs.org/sdr/SWAA2023052542484.md): Stringer · cracked · Apr 28, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER S-25L TERMINUS. STA 540<[01] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1.;[02] REMOVED DAMAGED SECTION OF STRINGER 25L BS 500D+11'-540 IAW SRM 53-00-03-2R-1 REP. 1 PAR. 4-B.;[03] PERFORMED GVI ON REPAIR AREA AND NO ADDITIONAL DAMAGED FO
- [SDR SWAA2023053041772](https://openairdocs.org/sdr/SWAA2023053041772.md): Vapor Barrier · cracked · Apr 26, 2023 · N416WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK ON BS 663 VAPOR BARRIER BULKHEAD AT LBL 28 WL 151.<[01] REMOVED BS 663 VAPOR BARRIER BULKHEAD AT LBL 28 WL 151 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW LH BS663 VAPOR BARRIER BLKHD IAW SRM 51-40-05 AND DWG #111A1000.;[03] VERIFIED CORRECTIVE AC
- [SDR SWAA2023053041885](https://openairdocs.org/sdr/SWAA2023053041885.md): Skin · cracked · Apr 26, 2023 · N416WN · Boeing 7377H4 · Leading Edge Devices
  > #1 SLAT LEADING EDGE NOSE SKIN IS CRACKED JUST I/B OF ACTUATOR FITTING<CUT AND REMOVED 3EA CRACKS ON SKIN AS FOLLOWS; -O/B 2ND FWD FASTENER ON ACTUATOR RIB FITTING IAW SRM 57-42-01-2R-8 REPAIR 8 REQUIREMENTS.<BR>-O/B 1ST FASTENER ON I/B DOWN STOP RIB IAW SRM 5
- [SDR SWAA2023042630745](https://openairdocs.org/sdr/SWAA2023042630745.md): Slide · dislodged · Apr 24, 2023 · N416WN · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE LOOKS DISLODGED<[01] INSTALLED R1 DOOR SLIDE PER MT 725-61-06.
- [SDR SWAA2023022709663](https://openairdocs.org/sdr/SWAA2023022709663.md): Tail Cone · cracked · Feb 24, 2023 · N416WN · Boeing 7377H4 · Aileron Tabs
  > #8 FLAP SUPPORT FAIRING TAIL CONE CRACKED REFERENCE TTG8Q00J1YP2. INSPECTION MISSING FROM ORIGINAL FAULT.<[01] ITEM PLACED ON CDL REFERENCE TTG8Q00J1YP2 FOR ORIGINAL FAULT
- [SDR SWAA2022112975912](https://openairdocs.org/sdr/SWAA2022112975912.md): Floor Panel · cracked · Nov 28, 2022 · N416WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO AFT FLOOR PANEL CRACKED / [01] R+R FWD CARGO 120 CF FLOOR PANEL IAW AMM 25-52-10.
- [SDR SWAA2022112975913](https://openairdocs.org/sdr/SWAA2022112975913.md): Floor Panel · cracked · Nov 28, 2022 · N416WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FWD FLOOR PANEL 140BF CRACKED / [01] REMOVED AND REPLACED AFT CARGO FLOOR PANEL 140BF IAW AMM 25-52-10.
- [SDR SWAA2022102763833](https://openairdocs.org/sdr/SWAA2022102763833.md): Slide · dislodged · Oct 25, 2022 · N416WN · Boeing 7377H4 · Escape Slide
  > R1 DOOR ESCAPE SLIDE HAS EXTRA MATERIAL COMING FROM BOTTOM OF BEZEL. / [01] INSTALLED EXTRA MATERIAL REF AMM 25-66-01;[02] INSPECTED
- [SDR SWAA2022101759900](https://openairdocs.org/sdr/SWAA2022101759900.md): None · faulty · Oct 13, 2022 · N416WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > SELECTED FLAPS 5 RIGHT FLAP REMAINED UP LEFT FLAP INDICATOR STOPPED AT LESS THAN 1 / [01] REMOVED AND REPLACED #6 SKEW SENSOR PER AMM 27-59-01
- [SDR SWAA2022092683380](https://openairdocs.org/sdr/SWAA2022092683380.md): Hook · loose · Sep 20, 2022 · N416WN · Boeing 737 · Escape Slide
  > FWD L1 DOOR GIRT BAR STOW HOOK ( ON THE DOOR UNARMED POSITION) IS LOOSE AND DOES NOT STOW THE GIRT BAR PROPERLY / [01] RESECURED FWD GIRT BAR HOOK ON L1 DOOR PER BOEING DRAWING BWG416A2204-SHT14
- [SDR SWAA2022062721112](https://openairdocs.org/sdr/SWAA2022062721112.md): Handle · out of position · Jun 21, 2022 · N416WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY SLIDE HANDLE EXPOSED / [01] FOUND AFT ENTRY DOOR SLIDE HANDLE COVER TUCKED UP IN TO SLIDE-COVER. SECURED COVER PER SIP.
- [SDR SWAA2022052310307](https://openairdocs.org/sdr/SWAA2022052310307.md): Cover · missing · May 19, 2022 · N416WN · Boeing 7377H4 · Emergency Lighting
  > LEFT SIDE CABIN ROW 12 LIGHT COVER MISSING / [01] O.K. TO CONTINUE PER MEL 33-15-02 SP # 1 <BR>TR # 66943;[02] INSTALLED NEW LIGHT COVER AT ROW 12ABC IN REF. TO AMM 33-51-03.
- [SDR SWAA2022052309653](https://openairdocs.org/sdr/SWAA2022052309653.md): Cover · missing · May 19, 2022 · N416WN · Boeing 7377H4 · Emergency Lighting
  > LEFT SIDE CABIN ROW 12 LIGHT COVER MISSING / [01] O.K. TO CONTINUE PER MEL 33-15-02 SP # 1 <BR>TR # 66943;[02] INSTALLED NEW LIGHT COVER AT ROW 12ABC IN REF. TO AMM 33-51-03.
- [SDR SWAA2022041894520](https://openairdocs.org/sdr/SWAA2022041894520.md): Light · inoperative · Apr 14, 2022 · N416WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT COVER MISSING BIN ROW 12ABC / [01] REINSTALLED EMERGENCY LIGHT COVER AT BIN ROW 12ABC IAW 33-51-03

Next page: https://openairdocs.org/deregistered/N416WN-2025-09-29/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 = 'N416WN' AND deregistration_id = 'N416WN-2025-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N416WN-2025-09-29/reports

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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.