N410EA
Registered owner: AVIATION STRATEGIES LLC, ID (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
23 reports on file, 1995-01-04 – 2000-09-21.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
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)
Part: POWER SUPPLY — FAILED (TAILCONE)
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)
Part: BULB — FAILED (TAILCONE)
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)
Part: BATTERY — DISCHARGED (TAILCONE)
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)
Part: BULB — FAILED (TAILCONE)
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)
Part: SPAR — CRACKED (RIGHT WING)
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 J060271, REV M, DATED 1-22-97. ALL WORK GENERATED BY EXISTING AD 88-01-04. AIRCRAFT RETURNED TO SERVICE. (X)
Earlier reports · 1995–1999 · 17 reports
1999
Part: LONGERON — CRACKED (BS 794)
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.
Part: LONGERON — CRACKED (BS 794)
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.
1998
Part: FITTING — CORRODED (BS 1167)
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.
Part: LONGERON — CRACKED (BS 287)
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.
Part: LONGERON — CRACKED (BS 294)
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.
Part: BEAM — CRACKED (SERVICE DOOR)
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.
1997
Part: CSD — FAILED (NR 2 ENGINE)
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)
1996
Part: FITTING — CRACKED (BS 732.5)
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)
Part: TURBINE — DAMAGED (NR 2 ENGINE)
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.
Part: ENGINE — FAILED (NR 2)
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 HOURS; 32,872 CYCLES. CHECK C-12 - 3-20-96 - STL. INVESTIGATION OF NR 2 ENGINE, S/N 1722, SHUTDOWN REVEALED ONE EACH VANE CRACKED AT INNER SHROUD AND RELEASED, PRODUCING DAMAGE TO THE HIGH PRESSURE COMPRESSOR AND TURBINE. THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE.
Part: ACTUATOR — FAILED (YAW DAMPER)
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.
Part: ACTUATOR — FAILED (YAW DAMPER)
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)
1995
Part: CSD — FAILED (NR 2 ENGINE)
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.
Part: BULB — FAILED (CABIN)
STL - FLT 124 - DURING LAYOVER, MAINTENANCE FOUND RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECK NORMAL.
Part: AMPLIFIER — MALFUNCTIONED (RT PACK)
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 COALESCER, (P/N 179460-8-1). AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-12 - 1-11-95 - STL. REF 95ZZZZ251.
Part: COALESCER — DIRTY (RT PACK)
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 COALESCER, (P/N 179460-8-1). AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-12 - 1-11-95 - STL. REF 95ZZZZ250.
Part: BELT RING — CRACKED (FS 1212.809)
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.