# Service difficulty reports: N417WN, cancelled Sep 29, 2025

A list on [N417WN, cancelled Sep 29, 2025](https://openairdocs.org/deregistered/N417WN-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 7 · 318 reports

- [SDR SWAA2025050566699](https://openairdocs.org/sdr/SWAA2025050566699.md): Inlet · pulled · May 2, 2025 · N417WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > #2 ENGINE INLET HAS 17 FASTENERS PULLED THRU ON OUTBOARD SIDE 3OCLOCK POSITION.<[01] REMOVED #2 ENGINE INLET REF AMM 71-11-01;[02] 01 - REMOVED AND REPLACED PER [AMM 71-11-01-401-NG (INLET COWL - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2025041524243](https://openairdocs.org/sdr/SWAA2025041524243.md): Skin · debonded · Apr 13, 2025 · N417WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE<[01] REMOVED LH OTBD TRAILING EDGE FLAP PER M/M 27-51-22;[02] INSTALLED LH OB TRAILING EDGE FLAP REF MM 27-51-22
- [SDR SWAA2025041424037](https://openairdocs.org/sdr/SWAA2025041424037.md): Slide · loose · Apr 12, 2025 · N417WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE LOOSE<[01] FOUND GIRT ASSY UNFOLDED. C/W ESCAPE SLIDE PACK CHECK AND FOLDED GIRT ASSY IAW AMM 25-66-01
- [SDR SWAA2025041423226](https://openairdocs.org/sdr/SWAA2025041423226.md): Skin · debonded · Apr 10, 2025 · N417WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE.<[01] PERFORMED EA- 25-157-00935;[02] VERIFIED THAT MAINTENANCE ACTIONS HAVE BEEN COMPLIED WITH IAW EA 25-157-00935;[03] VE
- [SDR SWAA2024112060963](https://openairdocs.org/sdr/SWAA2024112060963.md): Lens · out of adjust · Nov 17, 2024 · N417WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY EMERY LIGHT LENS<[01] REINSTALLED FWD ENTRY EMERG LIGHT LENS PER AMM 33-51-00
- [SDR SWAA2024111358293](https://openairdocs.org/sdr/SWAA2024111358293.md): Battery Pack · inoperative · Nov 10, 2024 · N417WN · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY EMERGENCY EXIT SIGNS LIGHTS INOP.<[01] REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT LIGHTS BATTERY PACKS PER AMM 33-51-06.
- [SDR SWAA2024091236152](https://openairdocs.org/sdr/SWAA2024091236152.md): Slide · bulged · Sep 11, 2024 · N417WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE BULGING OUT ON AFT LOWER SIDE<[01] REMOVED AND REPLACED FWD ENTRY DOOR SLIDE REF AMM 25-66-01 AND TASK CARD 25-66-01. REFERENCE TTG8Q00VSP6G FOR TASK CARD AND SIDE PARTS INFORMATION.
- [SDR SWAA2024083032419](https://openairdocs.org/sdr/SWAA2024083032419.md): Slide · out of adjust · Aug 29, 2024 · N417WN · Boeing 7377H4 · Escape Slide
  > F/A REPORTS RT FORWARD SERVICE DOOR SLIDE EXTENDS FROM BOTTOM FURTHER THEN NORMAL<[01] RESCURED SLIDE PER AMM 25-66-00
- [SDR SWAA2024061400443](https://openairdocs.org/sdr/SWAA2024061400443.md): Skin · pulled · Jun 11, 2024 · N417WN · Boeing 7377H4 · Engine Air Intake System
  > #2 ENGINE INLET COWL HAS MULTIPLE RIVETS PULLED THROUGH INLET SKIN. FWD AND AFT EDGES<[01] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW AMM 71-11-01. OPS CHECK GOOD
- [SDR SWAA2024052288194](https://openairdocs.org/sdr/SWAA2024052288194.md): Slide · dislodged · May 20, 2024 · N417WN · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE PARTIALLY DISLODGED<[01] SECURED SLIDE PER MT 725-61-06
- [SDR SWAA2024031462578](https://openairdocs.org/sdr/SWAA2024031462578.md): Seal · cracked · Mar 13, 2024 · N417WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STABILIZER FWD LOWER SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-000-803-NG (STABILIZER-TO-BODY LOWER FRONT SPAR SLIDING SEAL REMOVAL - PERMANENT)] AT LH HORIZONTAL STAB;[02] C/W INSPECTION
- [SDR SWAA2024031362566](https://openairdocs.org/sdr/SWAA2024031362566.md): Battery Pack · no test · Mar 13, 2024 · N417WN · Boeing 7377H4 · Emergency Lighting
  > EMX LIGHT BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031362565](https://openairdocs.org/sdr/SWAA2024031362565.md): Battery Pack · no test · Mar 13, 2024 · N417WN · Boeing 7377H4 · Emergency Lighting
  > EMX LIGHT BATT PACK M01668 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01668 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024022053492](https://openairdocs.org/sdr/SWAA2024022053492.md): Slide · low pressure · Feb 17, 2024 · N417WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE PRESSURE OUT OF RANGE<[01] R/R FWD SERVICE DOOR SLIDE PER MT 725-61-06FS
- [SDR SWAA2023112223910](https://openairdocs.org/sdr/SWAA2023112223910.md): Light · damaged · Nov 22, 2023 · N417WN · Boeing 7377H4 · Emergency Lighting
  > ROW 1ABC PHOTOLUMINESENT STRIP HAS MOISTURE IN IT.<[01] R/R ROW 1ABC PHOTOLUMINESCENT STRIP IAW AMM 33-51-15
- [SDR SWAA2023103015501](https://openairdocs.org/sdr/SWAA2023103015501.md): Lamp · inoperative · Oct 28, 2023 · N417WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EXIT WINDOW LIGHT INOP. RELAMPED IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2023082391898](https://openairdocs.org/sdr/SWAA2023082391898.md): Lens · broken · Aug 20, 2023 · N417WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTS; L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS FELL OFF / BROKEN<[01] R&R?D L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS IN REF. TO AMM 33-51-01. LIGHT OPS CHECK GOOD @ THIS TIME.
- [SDR SWAA2023072080367](https://openairdocs.org/sdr/SWAA2023072080367.md): Slide · out of position · Jul 19, 2023 · N417WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE INSPECTION STICKER BLOCKS NEEDLE HARD TO READ<[01] FOUND AFT ENTRY DOOR SLIDE INSPECTION DECAL MISPOSITIONED; REPLACED DOOR SLIDE DECAL PER SIP. C/W M/T 725-61-06
- [SDR SWAA2023071174613](https://openairdocs.org/sdr/SWAA2023071174613.md): Battery Pack · inoperative · Jul 4, 2023 · N417WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] COMPLETED STEP 1.;[02] REPLACED M1670 EMERGENCY LIGHTS BATTERY AND TESTED PER AMM 33-51-06-960-805; NO DEFECTS NOTED.;[03] VERIFIED CORRECTIVE ACTION 2; AND STEP 1.;[04] MAINTENANCE COMPLETE; DE
- [SDR SWAA2023071761688](https://openairdocs.org/sdr/SWAA2023071761688.md): Stiffener · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER RIB 2ND STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS
- [SDR SWAA2023071761681](https://openairdocs.org/sdr/SWAA2023071761681.md): Stringer · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23R<[01] REMOVED EXISTING REPAIR AT FCB STA-500D TO STA-540 STR-23R IAW SRM 51-40-02-0G-0;[02] UPDATE PARTIAL STEP 1-2;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENERS
- [SDR SWAA2023071761683](https://openairdocs.org/sdr/SWAA2023071761683.md): Stringer · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-26R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] PARTIAL UPDATE STEP 1;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENERS;[
- [SDR SWAA2023071761684](https://openairdocs.org/sdr/SWAA2023071761684.md): Stringer · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 500D+7 TO BS 538 STR 23L IAW SRM 51-10-02-0G-0;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN H
- [SDR SWAA2023071761685](https://openairdocs.org/sdr/SWAA2023071761685.md): Stringer · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R BS 540 STR 26L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 500D+7 TO BS 538 STR 26L IAW SRM 51-10-02-0G-0;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND
- [SDR SWAA2023071261682](https://openairdocs.org/sdr/SWAA2023071261682.md): Stringer · cracked · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 25R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-25R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] UPDATE PARTIAL STEPS 1-5;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENER
- [SDR SWAA2023071161686](https://openairdocs.org/sdr/SWAA2023071161686.md): Threshold · corroded · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Structure
  > AFT CARGO BAY SUBTHRESHOLD IS CORRODED. CORROSION IS MEASURED FROM FWD EDGE OF PART AND IS MARKED ACCORDINGLY. (+8 TO+14); (+14 TO +16); (+17 TO+19); (+23 TO +25); (29 TO +32); (+33 TO +35)<[01] PARTIALLY STEPS 1;2;3.;[02] AFT CARGO BAY SUB THRESHOLD MUST BE R
- [SDR SWAA2023071161703](https://openairdocs.org/sdr/SWAA2023071161703.md): Threshold · corroded · Jun 20, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Structure
  > AFT CARGO BAY SUB THRESHOLD CORRODED. CORROSION MEASURED FROMFWD EDGE AND IS MARKED ACCORDINGLY. (+36 TO +37); (+39); (+41 TO +42); (+44)<[01] REMOVED CORROSION ON AFT CARGO BAY SUBTHRESHOLD BETWEEN BS 827+12' RBL 28; WL.156 IAW SRM 51-10-02.<BR> MEASURE MAX.
- [SDR SWAA2023071760761](https://openairdocs.org/sdr/SWAA2023071760761.md): Panel · cracked · Jun 19, 2023 · N417WN · Boeing 7377H4 · Vertical Stabilizer, Plate/Skin
  > VERTICAL FIN PANEL 324AL LOWER CLIP IS CRACKED<[01] CRACKED ON VERTICAL FIN PANEL 324AL LOWER CLIP WITH NEXT DIMENSION L=3.220 TOOL USED CALIPER 2738; DUE:04/2024; DATE:04/2023 FOUND TO BE OUT LIMITS I.A.W SRM 55-30-01-0L-3 FOR IDENTIFICATION AND DUE TO NO ALL
- [SDR SWAA2023071760757](https://openairdocs.org/sdr/SWAA2023071760757.md): Skin · corroded · Jun 19, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > SPOTTY SKIN CORROSION; BS1050 -1088; BETWEEN SKATE ANGLE AND AFT LEFT VERTICAL FIN FWD SUPPORT ANGLE<[01] SEVERAL AREAS OF CORROSION ON THE ANGLE AT BS 1036 FROM STR2R-STR2L FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE IAW SRM 51-10-02 PAR 9C;[02]
- [SDR SWAA2023071760668](https://openairdocs.org/sdr/SWAA2023071760668.md): Plate · cracked · Jun 19, 2023 · N417WN · Boeing 7377H4 · Wing Structure
  > LEFT WING LOWER T/E WIGGLE PLATE IS CRACKED AND LOOSE JUST I/B OF #1 PYLON<[01] REMOVED AND REPLACED LEFT WING LOWER T/E WIGGLE PLATE I/B OF #1 PYLON<BR>IAW SRM 51-40-02-0G-0;[02] UPDATED PARTS;[03] VERIFIED CORRECTION ACTION ITEM 1;2; CARD COMPLETE.
- [SDR SWAA2023071260663](https://openairdocs.org/sdr/SWAA2023071260663.md): Floor Panel · pulled · Jun 19, 2023 · N417WN · Boeing 7377H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 242CF HAS A PULLED THROUGH INSERT<[01] IDENTIFIED FLOOR PANEL 242CF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 AND BWG DWG 144A5810 ID: 0006.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><
- [SDR SWAA2023071159999](https://openairdocs.org/sdr/SWAA2023071159999.md): Scuff Plate · cracked · Jun 18, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED; INCLUDNG ACROSS PREVIOUS WELD REPAIR<[01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PARTS DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT;[02] RECEIVED NEW SCUFF PLATE P/N654A0004-97 LOT#14934
- [SDR SWAA2023071759983](https://openairdocs.org/sdr/SWAA2023071759983.md): Stiffener · cracked · Jun 17, 2023 · N417WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER RIB 3RD STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[10] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511
- [SDR SWAA2023071759980](https://openairdocs.org/sdr/SWAA2023071759980.md): Web · cracked · Jun 16, 2023 · N417WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > BS 663 LH SIDE VAPOR BARRIER WEB HAS CRACKS AND A TEMPORARY REPAIR; LBL 6 TO LBL 15.<[01] IDENTIFIED IAW SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR.4 D(1)<BR><BR>DAMAGE TO BE REPAIRED IAW S
- [SDR SWAA2023071759572](https://openairdocs.org/sdr/SWAA2023071759572.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > R/W L/E PANEL 621PB HAS PULLED FASTENER HOLE (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-41-01-0I-4 FIGURES 1+3; TABLE 3; ITEM [1].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR 4.A (5).<BR>A PERMANENT REPAIR WILL BE
- [SDR SWAA2023071759574](https://openairdocs.org/sdr/SWAA2023071759574.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 621HB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621HB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 4; SHEET1; TABLE 4; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C.
- [SDR SWAA2023071759577](https://openairdocs.org/sdr/SWAA2023071759577.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > R/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621SB MATERIAL IAW SRM 57-41-01-0I-4 TABLE 3 FIGURE 3 ITEM 1. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A(5). DAMAGE IS REPAIRABL
- [SDR SWAA2023071759970](https://openairdocs.org/sdr/SWAA2023071759970.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521TB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521TB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-
- [SDR SWAA2023071759974](https://openairdocs.org/sdr/SWAA2023071759974.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521JB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 4 TABLE 4 ITEM 1.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED
- [SDR SWAA2023071759973](https://openairdocs.org/sdr/SWAA2023071759973.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521MB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 521MB IAW SRM 57-41-01-0I-4 FIGURE 4 ITEM [1]; DAMAGE TO THE PANEL IS BEYOND THE ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A.(4).(C) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-
- [SDR SWAA2023071759972](https://openairdocs.org/sdr/SWAA2023071759972.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521QB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521QB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-
- [SDR SWAA2023071759971](https://openairdocs.org/sdr/SWAA2023071759971.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521WB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521WB PANEL IAW SRM 57-41-01-0I-4 FIGURE 2; ITEM 1; TABLE 2<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-
- [SDR SWAA2023071759976](https://openairdocs.org/sdr/SWAA2023071759976.md): Panel · pulled · Jun 16, 2023 · N417WN · Boeing 7377H4 · Wing Main, Frame Structure
  > L/W L/E PANEL 521CB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 3.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED
- [SDR SWAA2023061659140](https://openairdocs.org/sdr/SWAA2023061659140.md): Spar Cap · corroded · Jun 14, 2023 · N417WN · Boeing 7377H4 · Wing Spar
  > RT WING LOWER FWD SPAR CAP SHOWS EVIDENCE OF CORROSION UNDER PANEL 621DB APPROX WS 293.0. EVALUATED EXFOLIATION CORROSION ON LOWER CHORD RT WING LOWER FWD SPAR CAP, FOUND OUT OF LIMITS 100% EXFOLIATION LOWER CHORD IAW SRM 57-20-10-1A-1 4.A. TRIMED OUT DAMAG
- [SDR SWAA2023030611235](https://openairdocs.org/sdr/SWAA2023030611235.md): Handle · loose · Feb 28, 2023 · N417WN · Boeing 7377H4 · Passenger/Crew Doors
  > FLIGHT ATTENDANT REPORTS AFT ENTRY DOOR HANDLE IS LOOSE<[01] SECURED AFT ENTRY DOOR HANDLE IAW M/M 52-13-31
- [SDR SWAA2023030110978](https://openairdocs.org/sdr/SWAA2023030110978.md): Slide · missing · Feb 28, 2023 · N417WN · Boeing 7377H4 · Escape Slide
  > FORWARD SERVICE DOOR SLIDE IS MISSING VELCRO MANUAL HANDLE COVER<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE PER MT 725-61-06
- [SDR SWAA2023020800065](https://openairdocs.org/sdr/SWAA2023020800065.md): Slide · out of position · Feb 6, 2023 · N417WN · Boeing 7377H4 · Escape Slide
  > L2 SLIDE APPEARS DISLODGED<[01] REPOSITIONED L2 SLIDE IN CASE IAW AMM 25-66-01 OK FOR SERVICE
- [SDR SWAA2023011791756](https://openairdocs.org/sdr/SWAA2023011791756.md): Lamp · inoperative · Jan 15, 2023 · N417WN · Boeing 7377H4 · Emergency Lighting
  > LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.
- [SDR SWAA2022113076657](https://openairdocs.org/sdr/SWAA2022113076657.md): Battery Pack · no test · Nov 30, 2022 · N417WN · Boeing 7377H4 · Emergency Lighting
  > FORWARD RT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2022111170118](https://openairdocs.org/sdr/SWAA2022111170118.md): Gauge · obstructed · Nov 10, 2022 · N417WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE PRESSURE GAUGE NEEDLE COVERED BY INSPECTION STICKER. REMOVED SLIDE AND UNCOVERED NEEDLE AND REINSTALLED SLIDE PER MT 725-61-06.

Next page: https://openairdocs.org/deregistered/N417WN-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 = 'N417WN' AND deregistration_id = 'N417WN-2025-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N417WN-2025-09-29/reports

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