N278AL

ZIPLINE INTERNATIONAL INC P2 ZIP · Hybrid lift · 5 engines · 0 seats · Valid Registration

Registered owner: ZIPLINE INTERNATIONAL INC, CA (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.

4 reports on file, 2010-01-11 – 2011-03-12.

OTHER · 2011-03-12 Matched by certificate designator
ATA 6510

Part: NUT — CRACKED (T/R DRIVE ASSY) · airframe 7,275 hrs

DURING ROUTINE INSP, MX FOUND 2 NUTS PN MS21042L4 CRACKED. THE NUTS WERE A PART OF THE HARDWARE STACKUP ATTACHING THE TAILROTOR DRIVESHAFT FLEX COUPLINGS TO THE DRIVESHAFT. THE NUTS HAD A VENDOR STAMP MARK RESEMBLING AN "A" OR A "V" TURNED SIDEWAYS ON ONE OF THE WRENCH FLATS. FURTHER INVESTIGATION SHOWED THE THREADS ON THE "SKIRT" OR FLANGE END OF THE NUTS TO BE SUB-PAR. VISUAL INSP OF NEW HARDWARE IN STOCK REVEALED THE SAME ANOMOLIES.

Source: SDR ALGA031211278AL
FLT CONT AFFECTED · 2011-02-02 Matched by certificate designator
ATA 6340

Part: DRIVE SHAFT — SHEARED (TACH GENERATOR) · airframe 7,157 hrs

IN FLIGHT, ACFT LOST HYDRAULIC POWER. PILOT RETURNED TO BASE. MX FOUND MAIN ROTOR TACH GENERATOR DRIVESHAFT SHEARED.

Source: SDR ALGA020211278AL
OTHER · 2010-03-09 Matched by certificate designator
ATA 6210

Part: BLADE — DEBONDED (MAIN ROTOR) · airframe 5,412 hrs

FOUND MAIN ROTOR BLADE UPPER SURFACE NR 4 GRIP FINGER DOUBLER CORRODED AND DEBONDED APPROX 3.5".

Source: SDR ALGA39106254
OTHER · 2010-01-11 Matched by certificate designator
ATA 7160

Part: MOUNT — CRACKED (COMPRESSOR) · airframe 5,371 hrs

FWD FLANGE ON COMPRESSOR REAR MOUNT CRACKED.

Source: SDR ALGA0111105694