# Service difficulty reports: N426WN A list on [N426WN](https://openairdocs.org/aircraft/N426WN.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 · 391 reports - [SDR SWAA2025120843032](https://openairdocs.org/sdr/SWAA2025120843032.md): Glowstrip · out of adjust · Dec 5, 2025 · N426WN · Boeing 7377H4 · Emergency Equipment > CABIN FLOOR PHOTOLUMINESCENT STRIP DISPLACED 12FED. ADJUSTED DISPLACED PHOTOLUMINESCENT STRIP AT 12FED IAW AMM 33-51-15. - [SDR SWAA2025120140363](https://openairdocs.org/sdr/SWAA2025120140363.md): Handle · out of adjust · Nov 27, 2025 · N426WN · Boeing 7377H4 · Passenger/Crew Doors > L1 DOOR HANDLE SEATS IN VERTICAL POSITION. RE-SEATED DOOR HANDLE ON L1 PER AMM 52-11-00. OPS CHECKED GOOD. - [SDR SWAA2025103128965](https://openairdocs.org/sdr/SWAA2025103128965.md): Skin · cracked · Oct 27, 2025 · N426WN · Boeing 7377H4 · Passenger/Crew Doors > L1 ENTRY DOOR LOWER HINGE SKIN. BELOW SNUBBER; DENTED 2IN FROM FWD EDGE OF DOOR WITH A 1/2 INCH CRACK IN THE CENTER. SKIN DAMAGE HAS CRACK WITH DIMENSIONS OF 0.50' LENGTH AND 1.7' FROM FWD EDGE DOOR SKIN WITH A BEND / DEFLECTION L 3.3' X W 0.6'' X D 0.28. D - [SDR SWAA2025081299969](https://openairdocs.org/sdr/SWAA2025081299969.md): Tray · broken · Aug 9, 2025 · N426WN · Boeing 7377H4 · Passenger Compartment Equipment > 12F TRAY TABLE BROKEN (EM. EXIT ROW). SECURED 12F T/T PER CMM 25-21-42. - [SDR SWAA2025081198275](https://openairdocs.org/sdr/SWAA2025081198275.md): Floorbeam · cracked · Aug 5, 2025 · N426WN · Boeing 7377H4 · Fuselage Main, Floor Beam > FLOOR SUPPORT LEFT OF CENTER CRACKED AT FWD R/H CORNER ALONG FASTENER AT STA 540.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] FLOOR SUPPORT LEFT OF CENTER AT STA 540 - [SDR SWAA2025032107725](https://openairdocs.org/sdr/SWAA2025032107725.md): Girt Bar · out of adjust · Mar 19, 2025 · N426WN · Boeing 7377H4 · Emergency Equipment > FWD ENTRY DOOR SLIDE GIRT BAR STICKY <[01]. 02 - INSPECTED PER [AMM 25-66-01-200-802-NG (ESCAPE SLIDE PACK CHECK - PERMANENT)]. - [SDR SWAA2025010682174](https://openairdocs.org/sdr/SWAA2025010682174.md): Lamp · inoperative · Jan 1, 2025 · N426WN · Boeing 7377H4 · Emergency Lighting > LEFT WING EXTERNAL EMERGENCY EXIT LIGHT INOP.<[01] RELAMPED EXIT LIGHT PER AMM 33-51-04. - [SDR SWAA2024120273028](https://openairdocs.org/sdr/SWAA2024120273028.md): Light · inoperative · Dec 1, 2024 · N426WN · Boeing 7377H4 · Emergency Lighting > LEFT SIDE OVERWING EMERGENCY LIGHT INOP.<[01] REPOSITION LEFT SIDE OVERWING EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2024112671818](https://openairdocs.org/sdr/SWAA2024112671818.md): Battery Pack · inoperative · Nov 26, 2024 · N426WN · Boeing 7377H4 · Emergency Lighting > CABIN EMERGENCY LIGHTS ON LH #3 STOW BIN AND OVER WING EXIT CENTER AISLE LIGHT ARE INOP.<[01] REMOVED EMERGENCY LIGHT BATTERY PACK M1668 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMMM 33-51-06-960-805;[02] JOB COMPLETE. - [SDR SWAA2024112671816](https://openairdocs.org/sdr/SWAA2024112671816.md): Battery Pack · inoperative · Nov 25, 2024 · N426WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 NOT OPERATING<[01] REMOVED; REPLACE; AND PERFORMED GOOD TEST OF BOTH THE BATTERY AND THE BATTERY CHARGER FOR M1670 PER AMM 33-51-06-960-805 AND 33-51-06-960-806. NOW LIGHTS WORK CORRECTLY.;[02] VERIFIED CORRECTIVE AC - [SDR SWAA2024112670549](https://openairdocs.org/sdr/SWAA2024112670549.md): Shear Tie · cracked · Nov 21, 2024 · N426WN · Boeing 7377H4 · Fuselage Internal Mounting Structure > OUTBOARD SHEAR TIE CRACKED BS 665; RBL 65; WL 204<[01] REMOVED AND REPLACED SHEAR TIE AT BS 665 RBL 65 WL 204 IAW SRM 51-40-02 AND DWG # 144A7716 REV:-;[02] VERIFIED CORRECTIVE ACTION #1 - [SDR SWAA2024112657656](https://openairdocs.org/sdr/SWAA2024112657656.md): Fitting · cracked · Nov 7, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > 1EA CRACK FOUND DURING HFEC INSPECTION OF L/H KICK FITTING I/B SIDE AT 9:00 POSITION; L: 0.15' MARKED<[01] 'REFER TO FAULT TTG8Q00WHT52 WHERE EA 24-153-02933 WAS ADDED AS A SUBTASK.';[02] JOB COMPLETE. - [SDR SWAA2024112657657](https://openairdocs.org/sdr/SWAA2024112657657.md): Fitting · cracked · Nov 7, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > 1EA CRACK FOUND DURING HFEC INSPECTION OF R/H KICK FITTING I/B SIDE AT 5:00 POSITION; L: 0.1' MARKED<[01] 'REFER TO FAULT TTG8Q00WK92L WHERE EA 24-153-02938 WAS ADDED AS A SUBTASK.';[02] JOB COMPLETE. - [SDR SWAA2024112756832](https://openairdocs.org/sdr/SWAA2024112756832.md): Web · corroded · Nov 4, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CORROSION ON BS 663 BULKHEAD WEB AT LBL55; WL190. STEP 5 OF EA 24-153-02933-WIP1 HAS US CONTACT ENGINEERING IF DISCREPANCIES ARE FOUND<[01] UPDATED MEASUREMENTS;[02] ACCOMPLISHED INSPECTIONS AND RE-WORK INSTRUCTIONS IAW EA 24-157-03091 (AD-N426WN-ATS(PAE)-REPA - [SDR SWAA2024112651408](https://openairdocs.org/sdr/SWAA2024112651408.md): Fitting · cracked · Oct 21, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > DUE TO CRACK ON LH BS 663 FITTING (PICKLE FORK); REPLACE THE RH BS 663 FITTING (PICKLE FORK) PER CUSTOMER REQUEST AND BOEING GUIDANCE.<[01] REMOVED AND REPLACED R/H PICKLE FORK FRAME FITTING IAW EA 24-153-02938 (AD-N426WN-ATS(PAE)-REPAIR-R/H BS 663.75 FRAME FI - [SDR SWAA2024112650480](https://openairdocs.org/sdr/SWAA2024112650480.md): Fitting · cracked · Oct 18, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > LEFT PICKLE FORK FRAME FITTING CRACKED AT FASTENER #6 ( L/H UPPER FITTING 2ND AFT FASTENER FROM TOP) CRACK CONFIRMED WITH HFEC.<[01] REMOVED AND REPLACED LEFT HAND PICKLE FORK FRAME FITTING IAW EA 24-153-02933 (AD-N426WN-ATS(PAE)-REPAIR-L/H BS 663.75 FRAME FIT - [SDR SWAA2024102245980](https://openairdocs.org/sdr/SWAA2024102245980.md): Battery Pack · failed · Oct 8, 2024 · N426WN · Boeing 7377H4 · Emergency Lighting > M1675 FAILED CAPACITY TEST.<[01] R&R M1675 BATTERY PACK IZW AMM 33-51-06.;[02] R&R M1675 BATTERY PACK IAW AMM 33-51-06.;[03] R&R M1675 BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2024102245981](https://openairdocs.org/sdr/SWAA2024102245981.md): Battery Pack · failed · Oct 8, 2024 · N426WN · Boeing 7377H4 · Emergency Lighting > M1673 FAILED CAPACITY TEST.<[01] R&R M1673 BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2024102245957](https://openairdocs.org/sdr/SWAA2024102245957.md): Support Bracket · cracked · Oct 8, 2024 · N426WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CENTER KEEL BEAM PANEL #192E FWD R/H HANGAR SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED CENTER KEEL BEAM PANEL 192E FWD R/H HANGER SUPPORT BRACKET IAW B737 SRM 51-40-02. - [SDR SWAA2024102245976](https://openairdocs.org/sdr/SWAA2024102245976.md): Fitting · cracked · Oct 8, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > LEFT PICKLE FORK FRAME FITTING CRACKED AT FASTENER #6 (L/H UPPER FITTING 2ND AFT FASTENER FROM TOP). CRACK CONFIRMED WITH HFEC.<[01] COMPLIED WITH EA# 24-153-02769 AND EA# 24-153-02769 WIP1; REFERENCE LOG PAGE 2500570 AND TTG8Q00WHT52 FOR NEW OPEN FAULT. - [SDR SWAA2024102245973](https://openairdocs.org/sdr/SWAA2024102245973.md): Seal · cracked · Oct 8, 2024 · N426WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > R/H HORIZONTAL STABILIZER STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] R&R RH HORIZONTAL STAB TO BODY UPPER FRONT SLIDING SEAL REF. AMM 53-31-31. - [SDR SWAA2024102245967](https://openairdocs.org/sdr/SWAA2024102245967.md): Seal · cracked · Oct 8, 2024 · N426WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > L/H HORIZONTAL STABILIZER STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED.<[01] R&R LH HORIZONTAL STAB TO BODY UPPER FRONT SLIDING SEAL REF. AMM 53-31-31. - [SDR SWAA2024101445954](https://openairdocs.org/sdr/SWAA2024101445954.md): Slide · damaged · Oct 8, 2024 · N426WN · Boeing 7377H4 · Escape Slide > L1 DOOR SLIDE COVER SLIDE INSIDE PLACARD IS DAMAGED<[01] REMOVED AND REPLACED L1 DOOR SLIDE COVER ?SLIDE INSIDE? PLACARD PER AMM 20-10-14. - [SDR SWAA2024082127382](https://openairdocs.org/sdr/SWAA2024082127382.md): Flashlight · inoperative · Aug 18, 2024 · N426WN · Boeing 7377H4 · Emergency Equipment > ONE FWD GALLEY FLASH LIGHT IS INOP<[01] OPS CKED OK PER MM 25-64-00 - [SDR SWAA2024030656092](https://openairdocs.org/sdr/SWAA2024030656092.md): Seat Back · out of adjust · Feb 25, 2024 · N426WN · Boeing 7377H4 · Passenger Compartment Equipment > ROW 12 ABC CENTER SEAT BACK FLOATS BACK AND FORTH.<[01] ADJUSTED ROW 12 ABC CENTER SEAT BACK AS PER CMM 25-21-42;[02] VERIFIED STEP 1. - [SDR SWAA2024022956101](https://openairdocs.org/sdr/SWAA2024022956101.md): Slide · low pressure · Feb 25, 2024 · N426WN · Boeing 7377H4 · Escape Slide > L1 DOOR SLIDE PRESSURE IS IN RED BAND<[01] THIS FAULT WAS OPENED IN ERROR AND IS BEING CLOSED. ALL WORK WILL BE ACCOMPLISHED ON NON-ROUTINE TASK CARD TTG8Q00RSK9L.;[02] VERIFIED STEP 1. - [SDR SWAA2024022956107](https://openairdocs.org/sdr/SWAA2024022956107.md): Slide · low pressure · Feb 25, 2024 · N426WN · Boeing 7377H4 · Escape Slide > L1 DOOR PRESSURE IS IN RED BAND. (SLIDE)<[01] REMOVED AND REPLACED L1 DOOR SLIDE REF CUSTOMER MT ON TASK CARD TTG8Q00RSKFJ.;[02] VERIFIED STEP 1 - [SDR SWAA2024030651902](https://openairdocs.org/sdr/SWAA2024030651902.md): Skin · cracked · Feb 13, 2024 · N426WN · Boeing 7377H4 · Trailing Edge Flaps > LEFT WING I/B AFT FLAP LOWER SURFACE HAS A CRACK 12.5' FROM T/E AND 11.5' FROM I/B EDGE.<[01] INSTALLED RAPAIR AT LEFT WING I/B AFT FLAP ON LOWER SURFACE PER SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR 4' DIAMETRE VERIFIED INSTALLED RAPAIR AT LEFT WING I/B - [SDR SWAA2024030652006](https://openairdocs.org/sdr/SWAA2024030652006.md): Skin · cracked · Feb 13, 2024 · N426WN · Boeing 7377H4 · Spoilers > RIGHT WING SPOILER NO.7 LOWER SURFACE HAS A CRACK 1' FROM T/E AND 37.5' FROM I/B EDGE.<[01] FINAL STATEMENT: REMOVED AND REPLACED #7 SPOILER REF AMM 27-62-12-000-801 AND AMM 27-62-12-400-801;[02] VERIFIED FINAL STATEMENT: REMOVED AND REPLACED #7 SPOILER REF AM - [SDR SWAA2024030754507](https://openairdocs.org/sdr/SWAA2024030754507.md): Panel · delaminated · Feb 11, 2024 · N426WN · Boeing 7377H4 · Wing, Plate/Skin > RIGHT WING LOWER L/E PANEL#621HB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621HB AS PER B737 SRM 51-70-04-2R-13 PARAG 4 D-G; MATERIAL USED RESIN PO#1791128; FIBERGLASS PO#1473815; EQUIPMENT USED: HOT BONDER - [SDR SWAA2024030754509](https://openairdocs.org/sdr/SWAA2024030754509.md): Panel · delaminated · Feb 11, 2024 · N426WN · Boeing 7377H4 · Wing, Plate/Skin > RIGHT WING LOWER L/E PANEL#621JB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621JB AS PER B737 SRM 51-70-04-2R-13 PARAG 4 D-G; MATERIAL USED RESIN PO#1791128; FIBERGLASS PO#1473815; EQUIPMENT USED: HOT BONDER - [SDR SWAA2024030754508](https://openairdocs.org/sdr/SWAA2024030754508.md): Panel · delaminated · Feb 11, 2024 · N426WN · Boeing 7377H4 · Wing, Plate/Skin > RIGHT WING LOWER L/E PANEL#621YB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621YB AS PER B737 SRM 57-41-01-2R-6 PARAG 4-J-M; MATERIAL USED: PO#2039275;[02] VERIFIED APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS - [SDR SWAA2024030850205](https://openairdocs.org/sdr/SWAA2024030850205.md): Deflector · cracked · Feb 8, 2024 · N426WN · Boeing 7377H4 · Wing Main, Frame Structure > LT WING T/E DEFLECTOR PNL AT WBL 201.90 HAS AFT WEDGED SHAPED RIB WEB ASSY CRACKED AT LWR BOLT HOLE. 8-31<[01] REMOVED AND REPLACED RIB WEB ASSY AT L/H WING T/E DEFLECTOR PANEL AT WBL 201.90 PER REF B737 SRM 51-40-02-0G-0 AND DWG 115A2930; DWG 115A2900.;[02] V - [SDR SWAA2024030750204](https://openairdocs.org/sdr/SWAA2024030750204.md): Angle · cracked · Feb 8, 2024 · N426WN · Boeing 7377H4 · Wing Miscellaneous Structure > LT WING TRAIL EDGE DEFLECTOR PNL RIB WBL 201.90 HAS WEB AFT EDGE FITTING ANGLE CRACKED. 8-31<[01] REMOVED AND REPLACED CRACKED EDGE FITTING ANGLE FROM LT WING TRAIL EDGE DEFLECTOR PNL RIB WBL 201.90 AS PER SRM 51-40-02-0G-0 AND DWG# 115A2930.;[02] VERIFIED REM - [SDR SWAA2024022950351](https://openairdocs.org/sdr/SWAA2024022950351.md): Beam · cracked · Feb 8, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK FOUND AT R1 DOOR STRUCTURE LOWER BEAM #4 AT PERIMETER OF I/B FASTENER HOLE. REMOVED DAMAGE BEAM #4 AT R1-DOOR IN REF B737-700 SRM 51-40-02-0G-0 AND INSTALLED NEW BEAM #4 AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0 AND DWG 141A6535 REV: F AND DWG 141A - [SDR SWAA2024022950349](https://openairdocs.org/sdr/SWAA2024022950349.md): Skin · cracked · Feb 8, 2024 · N426WN · Boeing 7377H4 · Leading Edge Devices > PANEL 623DB ON SLAT 6 CRACKED. 8-42<[01] REMOVED DAMAGE PANEL 623DB; FABRICATED NEW PANEL AND INSTALLED PER REF B737 SRM 51-40-02-0G-0 AND DWG 141A8131;[02] VERIFIED STEP 1 - [SDR SWAA2024022950209](https://openairdocs.org/sdr/SWAA2024022950209.md): Gusset · cracked · Feb 8, 2024 · N426WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD CARGO AT FRAME STA 500D GUSSET AT STRINGERS 19L CRACKED. 8-34<[01] REMOVED AND REPLACED GUSSET AT FWD CARGO; STA 500D; STRINGER 19L AS PER B737-700 SRM 51-40-02-0G-0; DWG# 143A7902.;[02] VERIFIED 1. - [SDR SWAA2024030749821](https://openairdocs.org/sdr/SWAA2024030749821.md): Angle · cracked · Feb 7, 2024 · N426WN · Boeing 7377H4 · Trailing Edge Flaps > RT WING TRAIL EDGE RIB WBL 201.90 HAS WEB AFT EDGE FITTING ANGLE CRACKED. 8-11<[01] REMOVED AND REPLACED CRACKED EDGE FITTING FROM RT WING TRAILING EDGE RIB WBL 201.90 AS PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND DWG#115A2930.;[02] VERIFIED REMOVED AND REP - [SDR SWAA2024030749823](https://openairdocs.org/sdr/SWAA2024030749823.md): Web · cracked · Feb 7, 2024 · N426WN · Boeing 7377H4 · Wing Miscellaneous Structure > RT WING T/E RIB WBL 201.90 HAS AFT WEDGED SHAPED WEB ASSY CRACKED AT LWR BOLT. 8-12<[01] REMOVED AND REPLACED AFT WEDGED SHAPED WEB AT RT WING T/E RIB WBL 201.90 PER REF B737 SRM 51-40-02-0G-0.;[02] CORRECTING STEP !REMOVED AND REPLACED AFT WEDGED SHAPED WEB A - [SDR SWAA2024022949816](https://openairdocs.org/sdr/SWAA2024022949816.md): Pressure Deck · cracked · Feb 7, 2024 · N426WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK FOUND AT HORIZONTAL PRESSURE DECK WEB AT STA 675 RBL 42. CRACK LENGTH: 0.531'.<[01] ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60 REF B737-700 SRM 53-40-51-2R-2 TABLE 201 FI - [SDR SWAA2024011841828](https://openairdocs.org/sdr/SWAA2024011841828.md): Handle · loose · Jan 17, 2024 · N426WN · Boeing 7377H4 · Service Doors > FWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] RETIGHTEN HANDLE CAM PLATE PER AMM 20-50-11.;[02] C/W INSPECTION - [SDR SWAA2023111420236](https://openairdocs.org/sdr/SWAA2023111420236.md): Light · broken · Nov 10, 2023 · N426WN · Boeing 7377H4 · Emergency Lighting > FWD ENTRY EMERGENCY FLOOR LIGHT BROKEN<[01] REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY I/A/W AMM 33-51-01 - [SDR SWAA2023062270117](https://openairdocs.org/sdr/SWAA2023062270117.md): Slide · low pressure · Jun 21, 2023 · N426WN · Boeing 7377H4 · Escape Slide > FOUND R1 DOOR ESCAPE SLIDE PRESSURE GAUGE BELOW LIMITS GAUGE PRESSURE A BIT BELOW LIMITS<[01] R AND R ESCAPE SLIDE IAW AMM 25-66-01; MT 725-61-06. - [SDR SWAA2023042429930](https://openairdocs.org/sdr/SWAA2023042429930.md): Girt Bar · out of adjust · Apr 20, 2023 · N426WN · Boeing 7377H4 · Escape Slide > FWD SERVICE DOOR SLIDE GURT BAR STRAP HANGING TO LOW<[01] REPOSITIONED GURT BAR STRAP PER M/M 25-66-01.NO DEFECTS NOTED. - [SDR SWAA2023022005157](https://openairdocs.org/sdr/SWAA2023022005157.md): Buss · fault message · Feb 16, 2023 · N426WN · Boeing 7377H4 · AC Generation System > IN CLIMB AROUND FL 180; LOST #1 GEN; TR1; AND HALF THE AIRCRAFT ELECTRICAL SYSTEM. APU AND GROUND POWER WILL NOT POWER AIRCRAFT; NUMEROUS OTHER NON NORMAL INDICATIONS THROUGHOUT COCKPIT.<[01] RAN #1; #2 ENG; AND APU PER AMM 71-00-00 AND AMM 49-11-00. CYCLED AI - [SDR SWAA2023022003800](https://openairdocs.org/sdr/SWAA2023022003800.md): Generator · fault message · Feb 16, 2023 · N426WN · Boeing 7377H4 · AC Generation System > IN CLIMB AROUND FL 180; LOST #1 GEN; TR1; AND HALF THE AIRCRAFT ELECTRICAL SYSTEM. APU AND GROUND POWER WILL NOT POWER AIRCRAFT; NUMEROUS OTHER NON NORMAL INDICATIONS THROUGHOUT COCKPIT.<[01] RAN #1; #2 ENG; AND APU PER AMM 71-00-00 AND AMM 49-11-00. CYCLED AI - [SDR SWAA2022062822171](https://openairdocs.org/sdr/SWAA2022062822171.md): Light · loose · Jun 24, 2022 · N426WN · Boeing 7377H4 · Emergency Lighting > OVER WING EXIT OVERHEAD EMERGENCY LIGHT LOOSE / [01] R&R OVER WING EXIT OVERHEAD EMERGENCY LIGHT ASSY PER MM 33-51-04 - [SDR SWAA2022031470683](https://openairdocs.org/sdr/SWAA2022031470683.md): Rib · carboned · Feb 9, 2022 · N426WN · Boeing 737* · Horizontal Stabilizer, Spar/Rib > CRACK LEADING EDGE RIB LOCATED LES114.55 RT HORIZONTAL STAB 2022-68047 / [01] REPLACED RIB AND FASTENERS LOCATED LEADING EDGE RIB LOCATED LES114.55 RT HORIZONTAL STAB I.A.W B737-700 SRM 51-40-02 AND DRAWING 186A1001 REV-A SEE INDIVIDUAL SIGN OFF BELLOW;[02] RE - [SDR SWAA2022031470682](https://openairdocs.org/sdr/SWAA2022031470682.md): Rib · cracked · Feb 9, 2022 · N426WN · Boeing 737* · Horizontal Stabilizer, Spar/Rib > CRACK LEADING EDGE RIB LOCATED LEADING EDGE STATION 105.26 RT HORIZONTAL STAB 2022-68046 / [01] REPLACED RIB AND FASTENERS LOCATED LEADING EDGE RIB LOCATED LEADING EDGE STATION 105.26 RT HORIZONTAL STAB I.A.W B737 SRM 51-40-02 AND DRAWING 186A1001 REV-A SEE IN - [SDR SWAA2022031470827](https://openairdocs.org/sdr/SWAA2022031470827.md): Angle · cracked · Feb 9, 2022 · N426WN · Boeing 737* · Wing Miscellaneous Structure > CRACK FRONT SPAR SUPPORT ANGLE LOCATED FUEL BOOST PUMP IFSS 120 APROX. AND WBL 94.24 AT RT WING 2022-68053 / [01] CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 03-DEC-22.;[02] TOOL USED: POWER PACK P/N FMK0007096 S/N PE0414/70786 DUE DATE: 23-FEB-22. MULTIM Next page: https://openairdocs.org/aircraft/N426WN/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 = 'N426WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N426WN/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.