- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18735P2893
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- November 24, 2025
- Expires
- November 30, 2032
- Mode S code
- A66DC1
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 N513NAMatched 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 N513NAMatched 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 N513NAGeneral 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 N513NA not matched to an aircraft · 28
They name N513NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ANCF200800032Landing Gear · malfunctionedAIR TURN BACK, EICAS MSG GEAR DISAGREE AND GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. LT GEAR LIGHT, GEAR AMBER LIGHT AND DOORS AMBER LIGHT ILLUMINATE. IAW AMM 32-20-09 FIM PROCEDURE THE PSBU BITE TEST WAS PERFOMED AND NO FAULT CODE AND MAIN NLG PINS WERE REMOSDR ANCF200800008Warning Light · illuminatedFLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO THE RIGHT TO CENTER COLUMN. FIM PROCEDURE 27-81-00 FIG 105 WAS ACCOMPLISHED. IN ACCORDANCE AMM 27-51-01/201 FLAP SLAT ELECTRONIC UNIT NR 1 ASDR ANCF200800004Air Duct · leakingEICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIALLY AFTER THRUST REDUCTION BUT AFTER FEW SECONDS IT ILLUMINATED AGAIN). PERFORM FIM 26-11-00 AND F
See all 28 unmatched reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.
Earlier aircraft with this N-number · 2
These aircraft carried N513NA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.