# Service difficulty reports: N415WN, cancelled Sep 30, 2025

A list on [N415WN, cancelled Sep 30, 2025](https://openairdocs.org/deregistered/N415WN-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 7 · 321 reports

- [SDR SWAA2025033119438](https://openairdocs.org/sdr/SWAA2025033119438.md): Bracket · broken · Mar 29, 2025 · N415WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR ESCAPE SLIDE COVER REAR GIRT BAR BRACKET BROKEN<[01] RESECURE L1 DOOR REAR GIRT BAR BRACKET PER SRM 51-40-02. OPS CK GOOD.
- [SDR SWAA2024122379809](https://openairdocs.org/sdr/SWAA2024122379809.md): Window · cracked · Dec 20, 2024 · N415WN · Boeing 7377H4 · Passenger Compartment Windows
  > PAX AND F/A'S REPORTED ROW 4 ABC WINDOW CRACKED; PRESSURIZATION NORMAL DAVE HAS ASKED FOR MCI TO SEND OLD WINDOW TO DAL FOR OUR ENGINEER TEAM TO INVESTIGATE THANKS.<[01] R&R ROW 4ABC WINDOW PER AMM 56-21-00.
- [SDR SWAA2024111859860](https://openairdocs.org/sdr/SWAA2024111859860.md): Slide · out of adjust · Nov 13, 2024 · N415WN · Boeing 7377H4 · Escape Slide
  > R2 SERVICE DOOR PULL HANDLE FLAP ADRIFT<[01] REPOSITIONED AFT SERVICE DOOR SLIDE AS REQUIRED PER AMM 25-66-01 AND MT725-61-06
- [SDR SWAA2024092742340](https://openairdocs.org/sdr/SWAA2024092742340.md): Slide · out of adjust · Sep 26, 2024 · N415WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE SLIDING OUT.<[01] REMOVED; REPACKED; AND REINSTALLED L1 DOOR SLIDE PER MT 725-61-01
- [SDR SWAA2024090330820](https://openairdocs.org/sdr/SWAA2024090330820.md): Escape Rope · misinstalled · Aug 27, 2024 · N415WN · Boeing 7377H4 · Emergency Equipment
  > PASSENGER CABIN LEFT OVER WING EMERGENCY EXIT DOOR ESCAPE LANYARD IMPROPERLY STOWED.<[01] PROPERLY SECURED AND STOWED LH OWE EXIT DOOR ESCAPE LANYARD/ROPE PER AMM 25-61-10
- [SDR SWAA2024052990773](https://openairdocs.org/sdr/SWAA2024052990773.md): Slide · loose · May 25, 2024 · N415WN · Boeing 7377H4 · Escape Slide
  > CREW REPORTED FWD ENTRY DOOR SLIDE IS SAGGING INSIDE CONTAINER. REPOSITION FWD ENTRY DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2024052889916](https://openairdocs.org/sdr/SWAA2024052889916.md): Slide · out of position · May 25, 2024 · N415WN · Boeing 7377H4 · Escape Slide
  > CREW REPORTED FWD ENTRY DOOR SLIDE IS SAGGING INSIDE CONTAINER.<[01] REPOSITION FWD ENTRY DOOR SLIDE PER MT 725-61-06.
- [SDR SWAA2023113026004](https://openairdocs.org/sdr/SWAA2023113026004.md): Switch · out of alignment · Nov 29, 2023 · N415WN · Boeing 7377H4 · Cabin Pressure Control System
  > CABIN WOULD NOT PRESSURIZE. MAX CABIN ALT. 12000FT. COMPLIED WITH QRH NO HELP.<[01] ACCOMPLISHED FIM 21-21 TASK 801. DCPC#2 SHOWED F/C30 LOINFL/HILEAKG. DCPC#1 AND #2 DCPC GROUND OPERATIONAL CHECK PER MM 21-31-00 OPS CHECKS GOOD. NO FAULTS. ACCOMPLISHED CABIN
- [SDR SWAA2023080782991](https://openairdocs.org/sdr/SWAA2023080782991.md): Drag Link · cracked · Jul 27, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > BS 540 DRAG LINK - RH 9MODULATION DOOR CRACKED<[01] CRACKED LBS 540 DRAG LINK - RH 9MODULATION DOOR WITH NEXT DIMENSION O/B L= 0.170' TOOL USED CALIPER<BR>ID:ATS2739<BR>S/N:A22004232<BR>DATE:11/2022<BR>DUE:11-2023 FOUND TO BE OUT<BR>DUE TO NO ALLOWABLE DAMAGE
- [SDR SWAA2023080780138](https://openairdocs.org/sdr/SWAA2023080780138.md): Stringer · cracked · Jul 18, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AFT AREA OF FOWARD CARGO BS540 STR 23R CRACKED<[01] VERIFIED APPLICABILITY SRM 53-00-03-2R-1<BR>CUT AND REMOVED THE DAMAGED AREA ON STRINGER 23R BS 540 PER SRM 53-00-03-2R-1 CUT AREA ON BS 513;[02] VERIFIED CORRECTIVE ACTION 1;[03] REQUEST HFEC EDDY CURRENT IN
- [SDR SWAA2023080780139](https://openairdocs.org/sdr/SWAA2023080780139.md): Stringer · cracked · Jul 18, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AFT AREA OF FOWARD CARGO BS540 STR 26R CRACKED<[01] VERIFIED APPLICABILITY SRM 53-00-03-2R-1<BR>CUT AND REMOVED THE DAMAGED AREA ON STRINGER 26R BS 540 PER SRM 53-00-03-2R-1 CUT AREA ON BS 511;[02] VERIFIED CORRECTIVE ACTION 1;[03] REQUEST HFEC EDDY CURRENT IN
- [SDR SWAA2023080780140](https://openairdocs.org/sdr/SWAA2023080780140.md): Stringer · cracked · Jul 18, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AFT AREA OF FOWARD CARGO BS540 STR 25L CRACKED<[01] VERIFIED APPLICABILITY SRM 53-00-03-2R-1<BR>CUT AND REMOVED THE DAMAGED AREA ON STRINGER 25L BS 540 PER SRM 53-00-03-2R-1 CUT AREA ON BS 515;[02] VERIFIED CORRECTIVE ACTION 1;[03] REQUEST HFEC EDDY CURRENT IN
- [SDR SWAA2023080779202](https://openairdocs.org/sdr/SWAA2023080779202.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4 · Wing Structure
  > R/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.<
- [SDR SWAA2023080779205](https://openairdocs.org/sdr/SWAA2023080779205.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.
- [SDR SWAA2023080779206](https://openairdocs.org/sdr/SWAA2023080779206.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > R/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.<
- [SDR SWAA2023080779201](https://openairdocs.org/sdr/SWAA2023080779201.md): Panel · pulled · Jul 16, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > R/W T/E PANEL 671AB HAS PULLED FASTENER HOLES (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.<BR><BR>JOB COMPLETE
- [SDR SWAA2023080778944](https://openairdocs.org/sdr/SWAA2023080778944.md): Panel · pulled · Jul 15, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES ON T/E (MARKED)<[01] DAMAGED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABL
- [SDR SWAA2023080778961](https://openairdocs.org/sdr/SWAA2023080778961.md): Panel · pulled · Jul 15, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLES ON T/E (MARKED)<[01] DAMAGED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABL
- [SDR SWAA2023080778930](https://openairdocs.org/sdr/SWAA2023080778930.md): Panel · pulled · Jul 15, 2023 · N415WN · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES ON T/E (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE
- [SDR SWAA2023080778923](https://openairdocs.org/sdr/SWAA2023080778923.md): Angle · cracked · Jul 14, 2023 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] ACCOMPLISHED REMOVE AND REPLACE BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE ON CUSTOMER CARD # TTG8Q00M7WFD (FUSELAGE 5026);[02] VERIFIED CORRECTIVE ACTION 1 AN
- [SDR SWAA2023080778610](https://openairdocs.org/sdr/SWAA2023080778610.md): Bulkhead · cracked · Jul 14, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL37 WL161.<[01] PARTIAL STEPS 3-6.;[02] REMOVED L/H COMPOSITE BULKHEAD (VAPOR BARRIER) AT BS663 LBL I.A.W SRM 51-40-02-0G-0.;[03] UPDATE STEP 7.;[04] UPDATE STEPS 5;6 AND 9.;[05] COMPLETED STEPS 5;6;7 AND 9;[06]
- [SDR SWAA2023080778611](https://openairdocs.org/sdr/SWAA2023080778611.md): Angle · cracked · Jul 14, 2023 · N415WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 10; W.L. 164.<[01] REMOVED BS663 UPPER ATTACH ANGLE IAW SRM 51-40-02;[02] UPDATE STEPS 2 AND 3.;[03] COMPLETED STEPS 1 AND 3.... OK TO INTALL LH BS 663 UPPER ATTACH ANGLE;[04] VERIFIED S
- [SDR SWAA2023070574403](https://openairdocs.org/sdr/SWAA2023070574403.md): Brake · smoke · Jul 1, 2023 · N415WN · Boeing 7377H4 · Landing Gear Brake System
  > AFTER PARKING; SMOKE WAS REPORTED COMING FROM THE RIGHT WHEELS. FIRE DEPARTMENT WAS CALLED AND MEASURED 800-900 DEGREES.<[01] INSPECTED RIGHT MAIN GEAR TIRES AND BRAKES ASSY. TOOK TEMP READING WITH OUR THERMOMETER. TEMP WAS AROUND 240 DEGREES. NO SMOKE NOTED.
- [SDR SWAA2023062771555](https://openairdocs.org/sdr/SWAA2023062771555.md): Sign · damaged · Jun 26, 2023 · N415WN · Boeing 7377H4 · Emergency Lighting
  > DAMAGED EXIT LOCATOR SIGN ON CEILING MID PAX CABIN<[01] R&R EXIT LOCATOR SIGN LOCATED ON CEILING MID PAX CABIN PER AMM 33-51-01
- [SDR SWAA2023060655977](https://openairdocs.org/sdr/SWAA2023060655977.md): Battery Pack · inoperative · Jun 4, 2023 · N415WN · Boeing 7377H4 · Emergency Lighting
  > FOUND MULTIPLE FWD GALLEY AREA EMERGENCY LIGHTS INOP.<[01] R+R LEFT BATTERY PACK AT STA 322 IAW AMM 33-51-06. OPC GOOD.
- [SDR SWAA2023051849026](https://openairdocs.org/sdr/SWAA2023051849026.md): Girt Bar · loose · May 16, 2023 · N415WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR GIRT BAR SUPPORT LOOSE<[01] REPLACED 1 EA RIVET AT AFT GIRT BAR SUPPORT AND REPLACED LATCH ASSY REF SRM 51-40-02 AND AMM 25-66-01
- [SDR SWAA2023051849036](https://openairdocs.org/sdr/SWAA2023051849036.md): Lens · out of adjust · May 16, 2023 · N415WN · Boeing 7377H4 · Emergency Lighting
  > RH EMERGENCY EXIT DOOR LAMP LENS IS NOT SEATED CORRECTLY.<[01] REPOSITIONED RH OVER WING EMERGENCY DOOR COVER LIGHT LENS. REF AMM 33-21-00;[02] C/W
- [SDR SWAA2023011992013](https://openairdocs.org/sdr/SWAA2023011992013.md): Strip · damaged · Jan 17, 2023 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CAP STRIP JUST FWD OF AFT CARGO DOOR HAS MISSING MATERIAL. REMOVED AND REPLACED CAP STRIP IAW AMM 25-52-10.
- [SDR SWAA2022071929950](https://openairdocs.org/sdr/SWAA2022071929950.md): Sign · missing · Jul 16, 2022 · N415WN · Boeing 7377H4 · Emergency Lighting
  > RT EMY EXIT ROW SMALL PLASTIC SIGN MISSING / [01] FOUND AND RESECURED RIGHT EMER. EXIT ROW (LENS) SIGN REF S.I.P. AND AMM 33-51-00.
- [SDR SWAA2022063023398](https://openairdocs.org/sdr/SWAA2022063023398.md): Battery · faulty · Jun 27, 2022 · N415WN · Boeing 7377H4 · Emergency Equipment
  > AFT GALLEY FLASH LIGHT RED LIGHT NOT BLINKING / [01] R & R FLASHLIGHT BATTERY IAW AMM 25-64-00
- [SDR SWAA2022061317446](https://openairdocs.org/sdr/SWAA2022061317446.md): Cover · out of position · Jun 10, 2022 · N415WN · Boeing 7377H4 · Escape Slide
  > EMERGENCY SLIDE PULL HANDLE COVER DISPLACE AFT ENTRY DOOR / [01] REPOSITION SLIDE PULL HANDLE COVER PER AMM 25-66-01-400-804
- [SDR SWAA2022052309320](https://openairdocs.org/sdr/SWAA2022052309320.md): Light · out of position · May 19, 2022 · N415WN · Boeing 7377H4 · Emergency Lighting
  > CABIN EMERGENCY EXIT LENS NOT SECURE 12F / [01] REMOVED AND REPLACED CABIN EMERGENCY EXIT LIGHT LENS IN REF TO BOEING AMM 33-52-01
- [SDR SWAA2022052309326](https://openairdocs.org/sdr/SWAA2022052309326.md): Battery Pack · failed · May 19, 2022 · N415WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVER WING BATTERY FAILED CAPACITY TEST. / [01] R&R BATTERY PACK (POWER SUPPLY) AT LOCATION M1668 PER AMM 33-51-06.;[02] R&R BATTERY PACK (POWER SUPPLY) AT LOCATION M1668 PER AMM 33-51-06.
- [SDR SWAA2023062270608](https://openairdocs.org/sdr/SWAA2023062270608.md): Landing Gear · disengaged · Jan 6, 2022 · N415WN · Boeing 7377H4 · Landing Gear System
  > ON TAKE OFF GEAR HANDLE MOVED TO UP POSITION ALL THREE GEAR RETRACTED UP AND LOCKED; WHEN HANDLE WAS PLACED TO THE OFF POSITION THE NOSE GEAR STARTED TO EXTEND. HANDLE WAS RECYCLED TO UP NOSE GEAR RET ON TAKE OFF GEAR HANDLE MOVED TO UP POSITION ALL THREE GEAR
- [SDR SWAA2021100826312](https://openairdocs.org/sdr/SWAA2021100826312.md): Light · inoperative · Oct 4, 2021 · N415WN · Boeing 7377H4 · Emergency Lighting
  > INOP EMERGENCY LIGHT FWD ENTRY DOOR AT PASSENGER CABIN (1 EA); 2021-369717 / [01] REPLACED EMERGENCY LIGHT FWD ENTRY DOOR AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-01-960-801 STEP 2.C(1)(A)3) AND 2.C(1)(C) AND 2.C(4) TEST IS OK.; [02] STEP 1 WAS CORRECTED.<
- [SDR SWAA2021100822953](https://openairdocs.org/sdr/SWAA2021100822953.md): Battery Pack · failed · Sep 24, 2021 · N415WN · Boeing 7377H4 · Emergency Lighting
  > DONT PASS OPERATIONAL TEST EMERGENCY LIGHT M1669 BATTERY PACK DO NOT CHARGE. AT PASSENGER CABIN (1 EA); 2021-369695 / [01] PERFORMED FIM 33-50 TASK 801 AND FOUND THE BATTERY PACK M1669 DO NOT WORK. MUST BE REPLACE. TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 376
- [SDR SWAA2021100818037](https://openairdocs.org/sdr/SWAA2021100818037.md): None · cracked · Sep 14, 2021 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INNER CHORD LOCATED BS 303.9 AND S-17L AT FWD GALLEY AREA; 2021-369672 / [20] REPLACED INNER CHORD AND FASTENERS LOCATED BS 270 BS 360 AT LEVEL STR 17L AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 TEM 9 AND DRAWING 142A0050 REV:- RII CERTIFIED
- [SDR SWAA2021100818036](https://openairdocs.org/sdr/SWAA2021100818036.md): None · cracked · Sep 14, 2021 · N415WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INTERNAL AREA STUD FRAME LOCATED BS 294.5 BETWEEN S-10R TO S- 5R AT UPPER FUSELAGE; 2021-369671 / [15] REPLACED STUD FRAME AND FASTENERS LOC. BS 294.5 BTW STR 10R TO STR 5R AT UPPER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 141A8370
- [SDR SWAA2021101115329](https://openairdocs.org/sdr/SWAA2021101115329.md): Angle · cracked · Sep 6, 2021 · N415WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CRACK ON ANGLE LOC BS 663.75 BTW RBL 8 TO RBL 30 VAPOR BARRIER AREA; 2021-369636 / [01] REMOVED ANGLE LOC BS 663.75 BTW RBL 8 TO RBL 30 VAPOR BARRIER AREA IAW SRM B737-700 51-40-02 DUE TO ALLOWABLE DAMAGE NOT FOUND ON SRM AND MUST BE
- [SDR SWAA2021100812544](https://openairdocs.org/sdr/SWAA2021100812544.md): Fitting · corroded · Aug 27, 2021 · N415WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CORROSION TRAILING EDGE VERTICAL FIN AFT SPAR FITTING FWD OUTBOARD LUG AT VERTICAL STABILIZER (1EA); 2021-369555 / [15] REPLACED FITTING LOC TRAILING EDGE VERTICAL FIN AFT SPAR FWD OUTBOARD LUG AT VERTICAL STABILIZER LH SIDE IAW EA 21-153-02648 SUMMARY AND EA
- [SDR SWAA2021100812543](https://openairdocs.org/sdr/SWAA2021100812543.md): None · deteriorated · Aug 26, 2021 · N415WN · Boeing 7377H4 · Escape Slide
  > DETERIORATED GIRT BAR FITTING PLATE RH FWD SIDE AT AFT GALLEY AREA; 2021-369545 / [01] REPLACED GIRT BAR FITTING PLATE RH FWD SIDE AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 STEP 3.1D ITEM (A) (B); [02] TASK COMPLETED
- [SDR SWAA2021101110602](https://openairdocs.org/sdr/SWAA2021101110602.md): None · delaminated · Aug 25, 2021 · N415WN · Boeing 7377H4 · Vertical Stabilizer
  > DELAMINATION FOUND ON REPAIR AREA UPPER AND LOWER ON ACCESS PANEL 322B LEADING EDGE. REMOVED REPAIR PLIES AND PREPARED REPAIR AREA IAW SRM 51-70-04-2R-10, REPAIR 10, PARAGRAPH 4. B; C. INSTALLED A NEW REPAIR IAW SRM 51-70-04-2R-10, REPAIR 10, PARAGRAPH 4. C
- [SDR SWAA2021101110598](https://openairdocs.org/sdr/SWAA2021101110598.md): Skin · corroded · Aug 24, 2021 · N415WN · Boeing 7377H4 · Wing, Plate/Skin
  > CORROSION EXTERNAL SKIN WING TIP OTBD SPAR HOLES, RT WING. AFTER REMOVED DAMAGE OF RIB 27 HOLE B AT RT WING PERFORMED DETAIL VISUAL INSPECTION AND FOUND DAMAGE ON INTERNAL FITTING. EDDY CURRENT INSPECTION DONE ON SPOT FACES IAW NDT MANUAL PART 6; 51-00-00 P
- [SDR SWAA2021082709205](https://openairdocs.org/sdr/SWAA2021082709205.md): Web · cracked · Aug 23, 2021 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOWER SILL FWD GALLEY DOOR BS 294.5 AT S-17R FWD GALLEY AREA. REMOVED WEB LOWER SILL IAW SRM 51-40-02 DUE TO ALLOWABLE DAMAGE NOT FOUND ON SRM. REPLACED WEB LOCATED LOWER SILL BS 291.50 TO BS 332.10 STR 17R FWD GALLEY AREA IAW SRM B737-700 51
- [SDR SWAA2021101109203](https://openairdocs.org/sdr/SWAA2021101109203.md): Panel · cracked · Aug 22, 2021 · N415WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ACCESS PANEL 621YB LEADING EDGE AT RT WING; 2021-369509 / [01] EVALUATED ACCESS PANEL 621YB LEADING EDGE AT RT WING AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 SRM 57-41-01-2R-1 REPAIR 1 TABLE 202 PARA 4.D CRACK DAMAGE SIZE L=0.48 W=0.16 TOOL USED CA
- [SDR SWAA2021100809194](https://openairdocs.org/sdr/SWAA2021100809194.md): Web · cracked · Aug 19, 2021 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL46 FWD GALLEY AND LAV; 2021-369464 / [01] REMOVED WEB- INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 328 AND BS 344 LBL 46 IAW SRM B737-700 51-40-02 DUE TO ALLOWABLE DAMAG
- [SDR SWAA2021100809173](https://openairdocs.org/sdr/SWAA2021100809173.md): None · cracked · Aug 19, 2021 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE INTERCOSTAL, BS 380 - 400, BL 0. REMOVED ANGLE INTERCOSTAL IAW SRM 51-40-02. DRILLED NEW ANGLE INTERCOSTAL INSTALLED NEW ANGLE INTERCOSTAL IAW SRM 51-40-05, AND SRM 51-20-01.
- [SDR SWAA2021100809172](https://openairdocs.org/sdr/SWAA2021100809172.md): None · cracked · Aug 19, 2021 · N415WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV; 2021-369462 / [10] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02-0G AND DWG #
- [SDR SWAA2021100809171](https://openairdocs.org/sdr/SWAA2021100809171.md): None · cracked · Aug 19, 2021 · N415WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 277 - 294, BL 0. REMOVED THE WEB IAW SRM 51-40-02. DRILLED HOLES ON NEW WEB IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT SRM 51-20-01-0G-0. INSTALLED THE NEW WEB IAW SRM 51-40-02-0G, AND DWG 141A5400 REV-.
- [SDR SWAA2021100809193](https://openairdocs.org/sdr/SWAA2021100809193.md): Floor Panel · missing · Aug 19, 2021 · N415WN · Boeing 7377H4 · Fuselage Floor Panel
  > MISSING MATERIAL FLOOR PANEL 222AF AT FWD GALLEY AREA; 2021-369482 / [22] REPAIRED FLOOR PANEL 222AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REP. 1; [23] TASK COMPLETED

Next page: https://openairdocs.org/deregistered/N415WN-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 = 'N415WN' AND deregistration_id = 'N415WN-2025-09-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N415WN-2025-09-30/reports

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