# Service difficulty reports: N8508W A list on [N8508W](https://openairdocs.org/aircraft/N8508W.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 3 · 111 reports - [SDR SWAA2026101203797](https://openairdocs.org/sdr/SWAA2026101203797.md): Sign · missing · Oct 11, 2026 · N8508W · Boeing 7378H4 · Emergency Lighting > EXIT SIGN TO RIGHT OF AFT OVERWING EMERGENCYEXIT DOOR MISSING F/O SIDE. REPLACED OVERWING EXIT SIGN IAW AMM 33-51-01. - [SDR SWAA2026101381241](https://openairdocs.org/sdr/SWAA2026101381241.md): Battery Pack · faulty · Oct 9, 2026 · N8508W · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT LIGHTNING SYSTEM DUE TO PARTIAL EMERGENCY EXIT LIGHTING ACTIVATION ON THEN OFF AT 8-10 MINUTES. R & R POWER SUPPLY ASSY M1672 IAW AMM 33-51-06. REMOVED AND REPLACED THE BATTERY PACK AT M1672 IAW AMM 33-51-06. OPS CHECKED GOOD. - [SDR SWAA2026101282018](https://openairdocs.org/sdr/SWAA2026101282018.md): Battery Pack · intermittent · Oct 9, 2026 · N8508W · Boeing 7378H4 · Emergency Lighting > PARTIAL EMERGENCY EXIT LIGHTING ACTIVATION (ON THEN OFF) AT 8-10 MINUTE INTERVALS. OCCURS WITH THE SWITCH ARMED OR OFF. LIGHTS REMAIN ON FOR ABOUT 2 MINUTES EACH OCCURRENCE. R & R EMERGENCY LIGHTS POWER AFT SUPPLY BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026101259827](https://openairdocs.org/sdr/SWAA2026101259827.md): Slide · out of position · Oct 7, 2026 · N8508W · Boeing 7378H4 · Escape Slide > CUSTOMER WALK FINDING FSD VALANCE ON SLIDE IS HANGING TOO LOW. REPACKED FSD VALANCE ON SLIDE IAW CMM 25-60-37. - [SDR SWAA2026101275686](https://openairdocs.org/sdr/SWAA2026101275686.md): Slide · out of adjust · Oct 7, 2026 · N8508W · Boeing 7378H4 · Escape Slide > CUSTOMER WALK FINDING, AED VALANCE ON SLIDE IS HANGING TOO LOW. REPACKED AED VALLANCE ON SLIDE IAW CMM 25-60-37. - [SDR SWAA2026101274248](https://openairdocs.org/sdr/SWAA2026101274248.md): Battery Pack · inoperative · Oct 4, 2026 · N8508W · Boeing 7378H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1695 DO NOT ILLUMINATE. REMOVED, REPLACED, AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805. - [SDR SWAA2026052104932](https://openairdocs.org/sdr/SWAA2026052104932.md): Battery · inoperative · May 20, 2026 · N8508W · Boeing 7378H4 · Emergency Equipment > AFT GALLEY F/O SIDE INBOARD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD. - [SDR SWAA2026042089585](https://openairdocs.org/sdr/SWAA2026042089585.md): Handle · inoperative · Apr 15, 2026 · N8508W · Boeing 7378H4 · Passenger/Crew Doors > BOTTOM L1 DOOR HANDLE INOPERATIVE. REPLACED L1 BOTTOM DOOR ASSIST HANDLE REF AMM 52-11-31. - [SDR SWAA2025123055649](https://openairdocs.org/sdr/SWAA2025123055649.md): Light · inoperative · Dec 26, 2025 · N8508W · Boeing 7378H4 · Emergency Lighting > FWD RIGHT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-04-960-801-NG. - [SDR SWAA2025121244247](https://openairdocs.org/sdr/SWAA2025121244247.md): Battery · no test · Dec 9, 2025 · N8508W · Boeing 7378H4 · Emergency Equipment > FWD RIGHT EMERGENCY FLASHLIGHT FAILED PUSH TO TEST. R & R EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00. - [SDR SWAA2025121250361](https://openairdocs.org/sdr/SWAA2025121250361.md): Flashlight · no test · Dec 9, 2025 · N8508W · Boeing 7378H4 · Emergency Equipment > FWD RIGHT EMERGENCY LIGHT FAILS PUSH TO TEST. R & R EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. - [SDR SWAA2025111936392](https://openairdocs.org/sdr/SWAA2025111936392.md): Lamp · inoperative · Nov 18, 2025 · N8508W · Boeing 7378H4 · Emergency Lighting > AFT SERVICE DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPED AFT SERVICE DOOR EMERGENCY SLIDE LIGHT PER AMM 33-51-04. OPS CHECKS GOOD. - [SDR SWAA2025102221639](https://openairdocs.org/sdr/SWAA2025102221639.md): Light · broken · Oct 6, 2025 · N8508W · Boeing 7378H4 · Emergency Lighting > LH FWD OVER WING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT ASSY HAS BROKEN NUT PLATE. R & R EMERGENCY LIGHT ASSY PER AMM 33-51-04 / OPS CHECK GOOD PER AMM 33-51-00. - [SDR SWAA2025102221638](https://openairdocs.org/sdr/SWAA2025102221638.md): Light · inoperative · Oct 5, 2025 · N8508W · Boeing 7378H4 · Emergency Lighting > LH FWD EMERGENCY EXIT DOOR EXTERIOR LIGHT INOPERATIVE. LH FWD EMERGENCY EXIT DOOR EXTERIOR EMERGENCY LIGHT ASSY R&R IAW AMM 33-51-04 ON TTG8Q015JU70. - [SDR SWAA2025102219703](https://openairdocs.org/sdr/SWAA2025102219703.md): Seal · cracked · Sep 30, 2025 · N8508W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > LEFT HORIZONTAL; UPPER FORWARD SLIDING SEAL CRACKED. REMOVED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31. - [SDR SWAA2025102219704](https://openairdocs.org/sdr/SWAA2025102219704.md): Seal · cracked · Sep 30, 2025 · N8508W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > RIGHT HORIZONTAL; UPPER FORWARD SLIDING SEAL CRACKED. REMOVED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31. REPLACED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31. - [SDR SWAA2025102219054](https://openairdocs.org/sdr/SWAA2025102219054.md): Web · cracked · Sep 28, 2025 · N8508W · Boeing 7378H4 · Nacelle/Pylon, Main Frame > NUMBER 1 ENGINE INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED. REMOVED AND REPLACED WITH TTG8Q00S5H1F. - [SDR SWAA2025102218843](https://openairdocs.org/sdr/SWAA2025102218843.md): Floor Support · cracked · Sep 27, 2025 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STA. 540 LBL1 CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL AT STA 540 LBL1 IAW SRM 51-40-02. - [SDR SWAA2025102218844](https://openairdocs.org/sdr/SWAA2025102218844.md): Floor Support · cracked · Sep 27, 2025 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > INTERCOSTAL AT BS 540 RBL1 CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL AT STA 540 RBL1 IAW SRM 51-40-02. - [SDR SWAA2025102218764](https://openairdocs.org/sdr/SWAA2025102218764.md): Ring · corroded · Sep 27, 2025 · N8508W · Boeing 7378H4 · Emergency Equipment > ANCHOR ATTACH RING ON RT EMERGENCY EXIT DOOR ESCAPE STRAP IS CORRODED. R & R EMERGENCY EXIT LIFE LINE PER AMM 25-61-10. - [SDR SWAA2025102218312](https://openairdocs.org/sdr/SWAA2025102218312.md): Rib · cracked · Sep 26, 2025 · N8508W · Boeing 7378H4 · Wing, Rib/Bulkhead > LEFT WING CLIP BETWEEN VERTICAL ANGLE AND MID SPAN DEFLECTION CONTROL RIB IS CRACKED. REMOVED L/H WING CLIP BETWEEN VERTICAL ANGLE AND MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT PER SRM 51-40-02. - [SDR SWAA2025102218311](https://openairdocs.org/sdr/SWAA2025102218311.md): Angle · cracked · Sep 26, 2025 · N8508W · Boeing 7378H4 · Wing Miscellaneous Structure > LEFT WING VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB IS CRACKED. REMOVED VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT. INSTALLED A NEW ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB PER SRM 51-40-02.. REFINISH - [SDR SWAA2025102218192](https://openairdocs.org/sdr/SWAA2025102218192.md): Vapor Barrier · cracked · Sep 25, 2025 · N8508W · Boeing 7378H4 · Fuselage Main, Bulkhead > BS 663 VAPOR BARRIER HAS A CRACK INDICATION AT APPROXIMATELY RBL 9. CUT AND REMOVED CRACKED SECTION OF VAPOR BARRIER ATTACH ANGLE PER SRM 57-10-10-2R.;[02] CW INSPECTION OF STEP #1. FABRICATED REPAIR ANGLE PER SRM 57-10-10-2R-5, C/W INSPECTION OF LINE #3 FAB - [SDR SWAA2025102218305](https://openairdocs.org/sdr/SWAA2025102218305.md): Rib · damaged · Sep 25, 2025 · N8508W · Boeing 7378H4 · Wing, Rib/Bulkhead > LEFT WING TRAILING EDGE SHELF PANEL ABOVE DEFLECTION RIB HAS ELONGATED BOLT HOLES ON SERRATED PLATE AND SHELF PANEL BRACKET.<[01] REMOVED SERRATED PLATES AND HARDWARE THAT ATTACH DEFLECTION CONTROL RIB AT TAB TO UPPER BEAM.;[02] REMOVED DAMAGE ON UPPER BEAM AT - [SDR SWAA2025102218303](https://openairdocs.org/sdr/SWAA2025102218303.md): Bracket · cracked · Sep 25, 2025 · N8508W · Boeing 7378H4 · Wing Miscellaneous Structure > RIGHT WING; DEFLECTION CONTROL RIB; INBOARD FIXED TRAILING EDGE UPPER PANEL BRACKET CRACKED. (M)<[01] REMOVED CRACKED WEB ANGLE BRACKET PER SRM 51-40-02.;[02] LOCATED; DRILLED AND DEBURRED REPLACEMENT WEB ANGLE BRACKET PER SRM 51-40-05.;[03] INSPECTED WORK IN - [SDR SWAA2025081805081](https://openairdocs.org/sdr/SWAA2025081805081.md): Slide · loose · Aug 16, 2025 · N8508W · Boeing 7378H4 · Escape Slide > F/A REPORTS FWD SVC DOOR SLIDE LOOSE. ADJUSTED FWD SVC DOOR SLIDE PER AMM 25-66-00. - [SDR SWAA2025072393259](https://openairdocs.org/sdr/SWAA2025072393259.md): Sign · detached · Jul 20, 2025 · N8508W · Boeing 7378H4 · Emergency Lighting > F/A FWD CHIME LIGHTS PLASTIC COVER KEEPS FALLING OFF. R&R FWD EMERGENCY EXIT SIGN ASSEMBLY OPS OK IAW AMM 33-51-01. - [SDR SWAA2024101045225](https://openairdocs.org/sdr/SWAA2024101045225.md): Connector · inoperative · Oct 4, 2024 · N8508W · Boeing 7378H4 · Light System Wiring > FWD ENTRY DOOR INTERIOR EMERGENCY EXIT LIGHTS ARE INOP<[01] RE SEATED FORWARD ENTRY EMERGENCY BATTERY PACK CONNECTOR. OPS CHECKS GOOD PER MM 33-51-00 - [SDR SWAA2024101045223](https://openairdocs.org/sdr/SWAA2024101045223.md): Battery · inoperative · Oct 4, 2024 · N8508W · Boeing 7378H4 · Emergency Lighting > BOTH L/H OVERWING EMERGENCY EXIT HATCHES INTERIOR EMERGENCY EXIT LIGHTS ARE INOP<[01] REPLACED L/H BATTERY FWD OF EMERGENCY EXIT. REF. AMM 33-51-06. L/H OVERWING EMERGENCY EXIT HATCHES INTERIOR EMERGENCY EXIT LIGHTS OPS CHECK GOOD. REF. AMM 33-51-00.;[02] INSP - [SDR SWAA2024100944992](https://openairdocs.org/sdr/SWAA2024100944992.md): Support Bracket · cracked · Oct 3, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO JUST FWD OF L/H TOILET TANK CLOSURE PANELS VERTICAL SUPPORT BETWEEN PANELS 141QW AND 141PW LOWER AT FLOOR LINE BRACKET HAS A 2' CRACK.<[01] REMOVED AND REPLACED ANGLE CLIP PER SRM 51-40-02;[02] PARTS INFO ADDED;[03] VERIFIED. REMOVED AND REPLACED ANG - [SDR SWAA2024101042869](https://openairdocs.org/sdr/SWAA2024101042869.md): Battery Pack · inoperative · Sep 27, 2024 · N8508W · Boeing 7378H4 · Emergency Lighting > SEVERAL BULL NOSE EMERGENCY LIGHTS INOP IN MAIN CABIN<[01] REPLACED 3 BATTERY PACKS. FWD LEFT AT SEAT 7ABC; AFT LEFT AT SEAT 20ABC AND AFT RIGHT AT SEAT 20DEF. REF. AMM 33-51-06. OPS CK GOOD REF. AMM 33-51-00.;[02] C/W INSPECTION AS REQUIRED - [SDR SWAA2024100941580](https://openairdocs.org/sdr/SWAA2024100941580.md): Doubler · corroded · Sep 24, 2024 · N8508W · Boeing 7378H4 · Fuselage Main, Plate/Skin > SIGN OF CORROSION ON THE FUSELAGE SKIN UNDER #2 VHF ANTENNA. SLIGHT EVIDENCE OF CORROSION TO #2 VHF ANTENNA DOUBLER ONLY. SEE EA AND ATTACHED PICS FOR WORK ACCOMPLISHED<[01] REMOVED DAMAGE PER SRM 51-10-01;[02] REPAIRED PER EA 24-153-02619;[03] INSPECTION OF D - [SDR SWAA2024100939338](https://openairdocs.org/sdr/SWAA2024100939338.md): Plate · corroded · Sep 19, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO R/H SIDE PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727I-727J.<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.009?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] REMOVED SECTION OF R/H SIDE PLA - [SDR SWAA2024101039047](https://openairdocs.org/sdr/SWAA2024101039047.md): Plate · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO FLOOR SIDEPLATE HAS EVIDENCE OF CORROSION FROM STA 500B TO 500D RBL 25.<[01] CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/H SIDE PLATE WILL BE REPLACED FROM STA. 500A-500I PER SRM 51-40-02. REFERENCE CARD #TTG8Q00VY - [SDR SWAA2024101039040](https://openairdocs.org/sdr/SWAA2024101039040.md): Plate · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO FLOOR SIDEPLATE HAS EVIDENCE OF CORROSION FROM STA 500D TO 500F RBL 25.<[01] CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/H SIDE PLATE WILL BE REPLACED FROM STA. 500A-500I PER SRM 51-40-02. REFERENCE CARD #TTG8Q00VY - [SDR SWAA2024101039038](https://openairdocs.org/sdr/SWAA2024101039038.md): Plate · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FORWARD CARGO FLOOR STRUCTURE SIDE PLATE AT RBL 21 HAS VARIOUS AREAS OF CORROSION AT FASTENER HOLES ON UPPER SURFACE FROM STA 500A-500B. (MARKED)<[01] CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED DAMAGED R/H SIDE PLATE - [SDR SWAA2024101039224](https://openairdocs.org/sdr/SWAA2024101039224.md): Web · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO THRESHOLD WEB CORRODED STA 793 TO 847<[01] REMOVED CORROSION AT AFT CARGO THRESHOLD WEB STA 793 TO 847 PER SRM 51-10-02. MEASURED MATERIAL REMOVED 0.019' OUT OF LIMITS IAW SRM 53-60-15-1A FIG. 103; DETAIL G.;[02] VERIFIED C.A. STEP 1 (AMT C. PAZ) THR - [SDR SWAA2024100939043](https://openairdocs.org/sdr/SWAA2024100939043.md): Plate · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO FLOOR SIDEPLATE HAS EVIDENCE OF CORROSION FROM STA 500H TO 500I RBL 25.<[01] CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/H SIDE PLATE WILL BE REPLACED FROM STA. 500A-500I PER SRM 51-40-02. REFERENCE CARD #TTG8Q00VY - [SDR SWAA2024100939037](https://openairdocs.org/sdr/SWAA2024100939037.md): Plate · corroded · Sep 18, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO FLOOR SIDEPLATE HAS EVIDENCE OF CORROSION FROM STA 500F TO 500H RBL 25.<[01] CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/H SIDE PLATE WILL BE REPLACED FROM STA. 500A-500I PER SRM 51-40-02. REFERENCE CARD #TTG8Q00VY - [SDR SWAA2024101038599](https://openairdocs.org/sdr/SWAA2024101038599.md): Scuff Plate · cracked · Sep 17, 2024 · N8508W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO FWD THRESHOLD CORNER CRACKED<[01] INSTALLED NEW FWD CARGO FWD CORNER SCUFF PLATE IAW AMM 53-11-02.;[02] VERIFIED - [SDR SWAA2024101040227](https://openairdocs.org/sdr/SWAA2024101040227.md): Placard · worn · Sep 14, 2024 · N8508W · Boeing 7378H4 · Placards and Markings > ON TOP OF THE RIGHT HAND INBD WING; THE PAINTED EXIT PATHWAY MARKINGS ARE WORN.<[01] REFINISHED WING EXIT PATHWAY PER AMM 11-24-04.;[02] INSPECTED WORK PERFORMED - [SDR SWAA2024101040226](https://openairdocs.org/sdr/SWAA2024101040226.md): Paint · worn · Sep 14, 2024 · N8508W · Boeing 7378H4 · Standard Practices/Structures > ON TOP OF THE LEFT HAND WING; THE PAINTED ESCAPE MARKINGS HAVE WEAR.<[01] REFINISHED WING EXIT PATHWAY PER AMM 11-24-04.;[02] INSPECTED WORK PERFORMED - [SDR SWAA2024090333185](https://openairdocs.org/sdr/SWAA2024090333185.md): Flashlight Assy · no test · Aug 30, 2024 · N8508W · Boeing 7378H4 · Emergency Equipment > RIGHT AFT F/A JUMPSEAT HAS 1 FLASHLIGHT THAT WON'T TEST.<[01] REMOVED AND REPLACED AFT RH FA JUMPSEAT FLASHLIGHT BRACKET IAW AMM 25-64-00. OPS CK GOOD. MEL CLEARED. - [SDR SWAA2024081325017](https://openairdocs.org/sdr/SWAA2024081325017.md): Battery Pack · inoperative · Aug 11, 2024 · N8508W · Boeing 7378H4 · Emergency Lighting > DURING WALK AROUND FOUND MULTIPLE INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP.<[01] R/R EMERGENCY EXIT LIGHT BATTERY PACK M1671 & M1676 AS PER AMM 33-51-06 OPS CK OK. NO FAULTS NOTED AT THIS TIME. - [SDR SWAA2024061401147](https://openairdocs.org/sdr/SWAA2024061401147.md): Slider · cracked · Jun 13, 2024 · N8508W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED.<[01] R&R LEFT UPPER HORIZONTAL STABILIZER SLIDER PER AMM 53-31-31-401 CONFIG 2-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT) - [SDR SWAA2024053091432](https://openairdocs.org/sdr/SWAA2024053091432.md): Flashlight · no test · May 30, 2024 · N8508W · Boeing 7378H4 · Emergency Equipment > FWD GALLEY OUTBOARD EMERGENCY FLASHLIGHT PUST TO TEST LED DOES NOT ILLUMINATE.<[01] REPLACED EMERGENCY FLASHLIGHT BATTERY REF AMM 25-64-00. OPS TEST GOOD. - [SDR SWAA2024021953032](https://openairdocs.org/sdr/SWAA2024021953032.md): Flashlight · inoperative · Feb 16, 2024 · N8508W · Boeing 7378H4 · Emergency Equipment > FLIGHT ATTENDANT D POSITION -BOTH FLASHLIGHTS ARE NOT WORKING<[01] RESEATED BOTH AFT FLASHLIGHTS FO SIDE IAW AMM 25-64-00. OPS CHECK GOOD. - [SDR SWAA2024010938078](https://openairdocs.org/sdr/SWAA2024010938078.md): Flashlight · inoperative · Jan 5, 2024 · N8508W · Boeing 7378H4 · Emergency Equipment > 2 CABIN FLASHLIGHTS AFT GALLEY INOP<[01] R&R?ED 2 EMERGENCY FLASHLIGHT BATTERIES ON AFT L/H JUMP SEAT AND REPLACED SEALS PER MM 25-64-00 - [SDR SWAA2024010939323](https://openairdocs.org/sdr/SWAA2024010939323.md): Flashlight · inoperative · Jan 5, 2024 · N8508W · Boeing 7378H4 · Emergency Equipment > 2 CABIN FLASHLIGHTS AFT GALLEY INOP<[01] R&R?ED 2 EMERGENCY FLASHLIGHT BATTERIES ON AFT L/H JUMP SEAT AND REPLACED SEALS PER MM 25-64-00 - [SDR SWAA2023091800830](https://openairdocs.org/sdr/SWAA2023091800830.md): Light · inoperative · Sep 15, 2023 · N8508W · Boeing 7378H4 · Emergency Lighting > AFT L/H ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED LAMP AT AFT L/H ENTRY DOOR EXTERIOR EMERGENCY LIGHT ASSY REF AMM 33-51-04. OPS TEST GOOD. Next page: https://openairdocs.org/aircraft/N8508W/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 = 'N8508W' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8508W/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.