N630AX
Registered owner: AIRBORNE TACTICAL ADVANTAGE COMPANY LLC, VA (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.
8 reports on file, 2001-04-27 – 2007-06-12.
Part: MOTOR — BYPASSING (L2 DOOR) · airframe 85,518 hrs · 21,713 cycles
L-2 DOOR AIR MOTOR IS BYPASSING AIR INTERNALLY DURING OPS CHECK.
Part: DUCT — RUPTURED (NR 2 ENGINE) · airframe 80,031 hrs · 20,706 cycles
NR 2 ENGINE ON T/O LOST POWER FROM 111.5 PERCENT TO 92.1 PERCENT ENGINE FAIL LIGHT CAME ON ABORTED T/O DUE TO LOSS OF N1 POWER. INSPECTED NR 2 ENGINE FOUND 14TH STAGE HIGH PRESSURE DUCT RUPTURED. REMOVED AND REPLACED PER MM 75-20 PERFORMED HIGH POWER RUN PER JRH, OPS CHECKED NORMAL.
Part: DUCT — RUPTURED (CABIN AIR) · airframe 78,129 hrs · 20,369 cycles
THICK SMOKE IN AFT LAV'S ALONG WITH A HOT FLOOR. AFTER PACKS 2 AND 3 TURNED OFF SMOKE SEEMED TO DISSIPATE. REMOVED AND REPLACED RUPTURED DUCT IN CENTER CARGO PIT LEFT SIDE.
Part: ACM — FAILED (NR 1) · airframe 76,677 hrs · 20,118 cycles
LITTLE TO NO AIRFLOW FROM NR 1 PACK, LITTLE TO NO AIRFLOW FROM NR 2 PACK. NOTE: UNABLE TO HOLD PRESSURIZATION WITH BOTH NR 1 & 2 PACKS. REMOVED AND REPLACED NR 1 ACM. FOUND LOOSE BOLT ON NR 2 PACK TURBINE BYPASS VALVE.
Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 74,679 hrs · 19,744 cycles
EXIT LIGHTS AT L-3 AND R-3 DOOR CAME ON IN-FLIGHT AND STAYED ON.
Part: COWLING — MISSING (NR 2 ENGINE)
NR 2 ENGINE FAN COWL FOUND MISSING UPON WALK-AROUND AFTER LANDING. REPLACED LEFT ENGINE SIDE COWL AND ASSOCIATED HARDWARE, NO OTHER DAMAGE NOTED.
Part: WIRE — BROKEN (NR 2 ENGINE) · airframe 70,995 hrs · 18,959 cycles
NR 2 ENG OIL TEMP HIGH AFTER TAKEOFF, ENG SHUTDOWN. REPAIRED BROKEN WIRE AT ADEL CLAMP ON ENG IAW 20-30-01. ENGINE GROUND RUN, OPS CHECKED OK.
Part: CLAMP — LOOSE (BLEED AIR) · airframe 70,444 hrs · 18,812 cycles
AFTER TAKEOFF, NR 3 ENGINE FIRE WARNING ILLUMINATED AT CRUISE POWER. REDUCED POWER AND INDICATION CEASED. ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT ENGINE DOWN. RETURNED TO ORIGINATING AIRPORT. INSPECTED ENGINE. FOUND LOOSE CLAMP ON PNEUMATIC DUCT AT TURBINE MIDFRAME AREA. REALIGNED DUCT, RETIGHTENED CLAMP, AND SAFETIED. PERFORMED GROUND ENGINE RUN. ALL PARAMETERS NORMAL.