# Service difficulty reports: N410EA, cancelled Jun 9, 2005 A list on [N410EA, cancelled Jun 9, 2005](https://openairdocs.org/deregistered/N410EA-2005-06-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR WXOA00009](https://openairdocs.org/sdr/WXOA00009.md): Power Supply · inoperative · Sep 21, 2000 · N410EA · Doug DC951 · Emergency Lighting > FAT - DURING SCHEDULED MAINTENANCE, CABIN EMERGENCY FLOOR PATHWAY LIGHTING SYSTEM FAILED TO ILLUMINATE AT SECOND POWER SUPPLY STATION. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR WX0A00007](https://openairdocs.org/sdr/WX0A00007.md): Power Supply · failed · Aug 17, 2000 · N410EA · Doug DC951 · Emergency Lighting > FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY. TAILCONE EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR WX0A00006](https://openairdocs.org/sdr/WX0A00006.md): Bulb · failed · Aug 16, 2000 · N410EA · Doug DC951 · Emergency Lighting > LGB - DURING FAA RAMP INSPECTION, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED BULBS. TAILCONE EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR WX0A00005B](https://openairdocs.org/sdr/WX0A00005B.md): Bulb · failed · Aug 14, 2000 · N410EA · Doug DC951 · Emergency Lighting > FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED BULBS AND BATTERIES. TAILCONE EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR WX0A00005A](https://openairdocs.org/sdr/WX0A00005A.md): Battery · discharged · Aug 14, 2000 · N410EA · Doug DC951 · Emergency Lighting > FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED BULBS AND BATTERIES. TAILCONE EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR WX0A00001](https://openairdocs.org/sdr/WX0A00001.md): Spar · cracked · Jun 22, 2000 · N410EA · Doug DC951 · Wing Spar > FAT - DURING ACCOMPLISHMENT OF CARD 4027.5 INCH CRACK DETECTED AT RIGHT WING REAR SPAR LOWER CAP AT THE NR 2 FLAP HINGE ATTACH BRACKET. AIRCRAFT FERRIED TO MHV FOR REPAIRS. INSTALLED TEMPORARY REPAIR KIT IAW SB A57-146, REV 3, DATED 1-30-89, AND DRAWING J06 - [SDR TWAA9903408](https://openairdocs.org/sdr/TWAA9903408.md): Longeron · cracked · Feb 28, 1999 · N410EA · Doug DC951 · Fuselage Main, Longeron/Stringer > FOUND THE INBD FLANGE OF LONGERON 5R CRACKED.25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REPAIRED PER DC9 SRM 53-02, FIG 18 SHEET 1. CHECK-C 8-12-98 STL. - [SDR TWAA9903407](https://openairdocs.org/sdr/TWAA9903407.md): Longeron · cracked · Feb 28, 1999 · N410EA · Doug DC951 · Fuselage Main, Longeron/Stringer > FOUND THE OTBD FLANGE OF LONGERON 4L CRACKED.25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-02, FIG 18. CHECK-C 2-28-99 STL. - [SDR TWAA9813404](https://openairdocs.org/sdr/TWAA9813404.md): Fitting · corroded · Aug 12, 1998 · N410EA · Doug DC951 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND LONGERON 20R, LONGERON 21R, LONGERON 22R, HAD END FITTINGS CORRODED AT STA 1167 BULKHEAD. REPLACED END FITTINGS AT STA 1167 AND LONGERON 22R, LONGERON 20R, AND LONGERON 21R PER SRM 51-30-2. - [SDR TWAA9813403](https://openairdocs.org/sdr/TWAA9813403.md): Longeron · cracked · Aug 8, 1998 · N410EA · Doug DC951 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINT, FOUND.25 INCH CRACK IN FLANGE OF LONGERON 23L AT STA 287. CUT OUT DAMAGED SECTION OF LONGERON, AND INSTALLED NEW SECTION AND SPLICE PER SRM 53-02, FIG 18. - [SDR TWAA9813402](https://openairdocs.org/sdr/TWAA9813402.md): Longeron · cracked · Aug 8, 1998 · N410EA · Doug DC951 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINT, FOUND.25 INCH CRACK IN FLANGE OF LONGERON 24L AT STA 294. CUT OUT DAMAGED SECTION OF LONGERON AND INSTALLED NEW SECTION AND SPLICE PER SRM 53-02, FIG 18. - [SDR TWAA9813401](https://openairdocs.org/sdr/TWAA9813401.md): Beam · cracked · Aug 6, 1998 · N410EA · Doug DC951 · Service Doors > DURING CHECK-C MAINT, THE FWD RT SERVICE DOOR BEAM HAD A 2 IN CRACK AT FWD END. REPLACED BEAM IN SHOP ON TICKET 836667 PER SRM 52-05, FIG 25 AND 51-10. - [SDR TWAA9719004](https://openairdocs.org/sdr/TWAA9719004.md): Csd · failed · Feb 8, 1997 · N410EA · Doug DC951 · Alternator-Generator Drive > CMH - DURING TAKEOFF NR 2 ENGINE, S/N 1718, FIREWARNING LIGHT ILLUMINATED DUE TO A FAILED CSD. REMOVED AND REPLACED CONSTANT SPEED DRIVE, MFG P/N 696233B. OPERATIONAL CHECK OF THE FIREWARNING AND CSD NORMAL. (M) - [SDR TWAA9613305](https://openairdocs.org/sdr/TWAA9613305.md): Fitting · cracked · Oct 30, 1996 · N410EA · Doug DC951 · Fuselage Miscellaneous Structure > STL - DURING SPECIAL CHECK, FOND A TWO INCH CRACK IN LONGERON 29R FITTING, STATION 732.5 FORWARD SIDE. REMOVED AND REPLACED FITTING PER SRM 51-30-5 AND TWA STANDARD PRACTICES. (M) - [SDR 96ZZZX3855](https://openairdocs.org/sdr/96ZZZX3855.md): Engine · failed · May 28, 1996 · N410EA · Doug DC951 · Engine (Turbine/Turboprop) > STL - FLT 564 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. FOUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME: 35,307 HO - [SDR 96ZZZM1042](https://openairdocs.org/sdr/96ZZZM1042.md): Turbine · damaged · May 28, 1996 · N410EA · Doug DC951 · Turbine Engine Compressor Section > STL - DURING APPROACH SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. FOUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. - [SDR 96ZZZX1240](https://openairdocs.org/sdr/96ZZZX1240.md): Actuator · failed · Jan 26, 1996 · N410EA · Doug DC951 · Autopilot System > STL - FLT 503 - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG PN 2589445-933. OPERATIONAL CHECK NORMAL. CHECK C-12 - 1-11-95 - STL. - [SDR 96ZZZM208](https://openairdocs.org/sdr/96ZZZM208.md): Actuator · failed · Jan 26, 1996 · N410EA · Doug DC951 · Autopilot System > STL - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG P/N 2589445-933. OPERATIONAL CHECK NORMAL. (M) - [SDR 96ZZZX231](https://openairdocs.org/sdr/96ZZZX231.md): Csd · failed · Dec 15, 1995 · N410EA · Doug DC951 · Alternator-Generator Drive > STL - FLT 126 - AFTER TAKEOFF, NR 2 CSD LOW PRESSURE LIGHT CAME ON. NR 2 CSD DISCONNECTED. REMOVED AND REPLACED CSD, MFG PN 696233B, OPERATIONAL AND LEAK CHECK OKAY. ENGINE TOTAL TIME: 34,358 HOURS, 32,155 CYCLES. CHECK C-12 - 1-11-95 - STL. - [SDR 96ZZZM54](https://openairdocs.org/sdr/96ZZZM54.md): Bulb · failed · Dec 2, 1995 · N410EA · Doug DC951 · Emergency Lighting > STL - FLT 124 - DURING LAYOVER, MAINTENANCE FOUND RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECK NORMAL. - [SDR 95ZZZZ251](https://openairdocs.org/sdr/95ZZZZ251.md): Coalescer · dirty · May 23, 1995 · N410EA · Doug DC951 · Humidity Control System > STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE. REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR - [SDR 95ZZZZ250](https://openairdocs.org/sdr/95ZZZZ250.md): Amplifier · malfunctioned · May 23, 1995 · N410EA · Doug DC951 · Cabin Temperature Controller > STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE. REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR - [SDR 95ZZZX1231](https://openairdocs.org/sdr/95ZZZX1231.md): Belt Ring · cracked · Jan 4, 1995 · N410EA · Doug DC951 · Fuselage Miscellaneous Structure > STL - DURING CHECK-C, FOUND.25 INCH CRACK IN BELT RING, IN TAIL COMPARTMENT, STA 1212.809, LONGERON 6L, 6R, 5R, 5L, 4R, AND 4L. REPLACED BELT RING PER SRM 51-10-4 AND SRM 51-30-0. AIRCRAFT TOTAL TIME: 38,988 HOURS, 35,341 CYCLES. ## 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 = 'N410EA' AND deregistration_id = 'N410EA-2005-06-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N410EA-2005-06-09/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, except the copies of manufacturers’ service documents, which belong to their rights holders.