- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18736P21556
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- April 26, 2026
- Expires
- April 30, 2033
- Mode S code
- A3E88F
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N351ALMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Zipline International P2 ZIP aircraft
FAA incident reports
No FAA accident or incident reports matched to N351ALMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Zipline International P2 ZIP aircraft
Service difficulty reports
No reports matched to N351ALGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Zipline International P2 ZIP aircraft
Reports on N351AL not matched to an aircraft · 7
They name N351AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ALGA105522Bearing · making metalTRANSMISSION ASSEMBLY MAKING METAL, DISASSEMBLED AND FOUND DUPLEX BEARING BREAKING DOWN. / REMOVED AND REPLACED DUPLEX BEARING P/N 206-040-032-105SDR ALG2005F00052Compressor · stalledDURING TAKEOFF AT 95 PERCENT TORQUE, OAT +34, WINDS CALM, AC HAD A COMPRESSOR STALL FOLLOWED BY A LOUD BANG, YAW, AND A DROP IN TORQUE. THE PILOT REDUCED POWER LEVELED AT 50 FT AT 70 KNOTS 50 PERCENT TORQUE, FLEW 8 MINUTES TO A LARGER PLATFORM AND LANDED. THSDR ALG2003F00062Link · inoperativeON POST FLIGHT, THE PILOT FOUND MAIN ROTOR PC LINK SN TY3241 JAM NUT LOOSE, THE MECHANIC REMOVED AND REPLACED THE PC LINK AND HE COMPLIED WITH TRACK AND BALANE AND AUTO ROTATION CHECK.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.