N367DA
Registered owner: GLOBAL AVIATION INC, OR (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Global Aviation, Inc. (G73A) | Certificate holder | — | Matched by certificate designator |
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.
4 reports on file, 2012-04-30 – 2017-12-19.
Part: SERVO MOTOR — SHORTED (NLG STEERING) · airframe 12,478 hrs · 9,717 cycles
ON THE GROUND AT PAE, DURING TAXI OPERATIONS THE PILOT NOTICED WHEN THE NOSE WHEEL STEERING WAS USED IT WOULD POP THE CIRCUIT BREAKER, AND DISENGAGE THE NOSE WHEEL STEERING. THE PILOT MEL'D THE NOSE WHEEL STEERING IN ORDER TO RETURN HOME FOR MAINTENANCE. TECHNICIANS TROUBLESHOT THE PROBLEM AND FOUND THE NOSE WHEEL STEERING SERVO HAD FAILED, THE FAILED UNIT WAS INSTALLED ON 09/07/17 IN A REPAIRED CONDITION, FOR A 2000 HR INSPECTION. THE FAILED UNIT WAS REPLACED WITH A REPAIRED UNIT ON 12/28/17, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE REPAIR REPORT FOR THE FAILED NOSE WHEEL STEERING SERVO SHOWED THAT IT WAS DRAWING A HIGH CURRENT, UPON THE TEAR DOWN INSPECTION 2 RESISTORS WERE SHORTED OUT, AND THE MECHANICAL CLUTCH WAS OUT OF SPECS.
Part: INDICATOR — FAILED (TRIM TAB) · airframe 12,214 hrs · 9,490 cycles
NEW TRIM TAB INDICATOR FAILS TO OPERATE. OBTAINED TEAR-DOWN REPORT, FINDINGS OF NEEDLE STICKING INTERMITTENTLY, REQUIRES CLEANING AND ADJUSTMENT/OVERHAUL.
Part: BRAKE ASSY — LEAKING (NR 3) · airframe 12,078 hrs · 9,369 cycles
NR 3 BRAKE LEAKING FLUID.
Part: WIRE — DAMAGED (FIRE LOOP)
LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED ON FINAL APPROACH. ALL OTHER INDICATIONS WERE NORMAL. FOUND DAMAGED & FRAYED WIRE IN PYLON FOR AFT BODY FIRE LOOP. CUT BACK WIRE LEAD, CRIMPED NEW CONNECTOR PIN ON LEAD AND REASSEMBLED CONNECTOR. OPS CHECK OF SYS WAS NORMAL AFTER REPAIR.