- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18736P22896
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- June 12, 2026
- Expires
- June 30, 2033
- Mode S code
- A7CEF7
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 N602CZMatched 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 N602CZMatched 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 N602CZGeneral 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 N602CZ not matched to an aircraft · 117
They name N602CZ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR C77A2019101100001Sign · inoperativeR1 DOOR EMERGENCY LIGHT INOP - LOWER "EXIT" LIGHT. REPLACED R1 DOOR LIGHT ID SIGN PER AMM 33-50-17 OPS CHECK GOOD.SDR C77A2019010700001Rib · brokenTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH PART II OF SB 170-57-0047, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION ON THE RT WING. THIS MODIFICATION CONSISTS OF REPLACING RIB 10 AT FTE WITH A NEW REINFORCED RIB 10 P/N 170-32161-628 AND PERFORMING A COLD EXPASDR C77A2019010200003Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LT INBOARD SEAT TRACK P/N 170-86081-003 AND RT INBOARD SEAT TRACK P/N 170-86082-003. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FI
See all 117 unmatched reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.