- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18736P23095
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- June 16, 2026
- Expires
- June 30, 2033
- Mode S code
- A2E49E
From the FAA registry file of October 22, 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 N286DPMatched 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 N286DPMatched 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 N286DPGeneral 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 N286DP not matched to an aircraft · 5
They name N286DP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 7GMB201680800001Generator · faultyTHE CREW REPORTED THAT NR 1 AND NR 3 MAIN GENERATORS ON LT ENGINE WERE NOT SHARING THE LOAD AND THERE WERE 50 AMP SPLIT BETWEEN THE 2 GENERATORS. IT WAS OBSERVED BOTH ON THE GROUND AND DURING IN FLIGHT. TROUBLESHOT BY SWAPPING GENERATOR CONTROL UNIT, GCU ANDSDR 7GMB20160218001Display · failedDISPLAY UNIT 4 FAN FAIL EICAS MSG DISPLAYED IN FLIGHT. THE CREW NOTICED ELEC BURNING SMELL 7 DEACTIVATED THE MFD 2 BY PULLING THE CB. THE ACFT LANDED SAFETY AT THE DESTINATION. REPLACEMENT DISPLAY UNIT WAS ORDERED, THE CB WAS SECURED & THE ACFT WAS RELEASEDSDR 7GMB2014102911781Shuttle Valve · failedAFTER LANDING & TAXING INTO RAMP, HYD 1 LO QTY EICAS INDICATION DISPLAYED & HYD SYS QTY INDICATION ON MFD SHOWS AMBER. TROUBLE SHOT & FOUND NR 1, LT OTBD BRAKE, SHUTTLE VLV WAS BYPASSING HYD FLUID TO NR 2 HYD SYS. OBSERVED HYD FLUID FLOWING FROM NR 2 HYD RES
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.