- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18735P2896
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- November 24, 2025
- Expires
- November 30, 2032
- Mode S code
- A658D5
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 N508NAMatched 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 N508NAMatched 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 N508NAGeneral 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 N508NA not matched to an aircraft · 12
They name N508NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 02082201Skin · gougedGouge in outer skin, STA. 755, STR. 15L. Cut out damaged area, installed fillers and doubler Per E.O. 02-0887. To be Reinspected every 12000 Flight CyclesSDR N8TA02081201Sill · corrodedCORROSION ON MOP SILL BS 1647, WL 208, LBL 57. REPLACED PER SRM 51-40-02.SDR 02080802Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 1640, RBL 52, WL 208. FLOORBEAM UPPER TEE FOUND TO BE OUT OF LIMITS AT RBL 52 PER SRM 53-00-51. FLOORBEAM REPAIRED PER SRM 53-00-51 FIG. 205, 53-00-51 PG 216, AND SRM 51-20-01. (STANDARD STRAP, ANGLE, ANF FILLER REPAIR.). AIRCRAFT
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.