- Registered owner
- Zipline International Inc
- Location
- S San Fran, CA
- Owner type
- Corporation
- Serial number
- 18736P22657
- Type
- Hybrid lift
- Engine
- Electric
- Certificate issued
- June 8, 2026
- Expires
- June 30, 2033
- Mode S code
- AC81CA
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 N905ALMatched 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 N905ALMatched 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 N905ALGeneral 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 N905AL not matched to an aircraft · 3
They name N905AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 39LA2013031300004Hose · collapsedAFTER DEPARTURE, FUEL LOAD WAS 2800 LBS, T/O GW 17,594, TEMP 12 DEG MAGW 20,000, CG 265.2. WHEN A POWER CHANGE WAS MADE THE NR 1 ENGINE TORQUE OSCILLATED 30 TO 40 PERCENT, FUEL PRESSURE OSCILLATING 10 TO 15 PSI, AND T5 TEMPS OSCILLATING 30 TO 40 DEGREES. NF ASDR 39LA2013030800004Engine · malfunctionedIMMEDIATLY AFTER TAKEOFF AT APPROX 97 PERCENT NG THE NR 1 NG BEGAN TO FLUCTUATE 3-4 PERCENT. NOTICED THE NR 1 NF BEGIN TO FLUCTUATE AS WELL NR 1 FUEL PRESSURE AND T5. ALL INDICATIONS ON NR 2 ENGINE WERE NORMAL. APPROXIMATE 40 PERCENT TORQUE SPLIT WAS NOTED SDR P4YA2010031000001Line · chafedACFT SUFFERED A LOSS OF ITS PRIMARY HYD SYS WHILE IT WAS ON THE GROUND BEING HOT REFUELED. INDICATIONS IN THE COCKPIT WERE MASTER CAUTION AND WARNING LIGHTS, AN INDICATED LOSS OF PRESSURE ON THE PRIMARY HYD PRESSURE GAUGE AND, SOON AFTER, THE SMELL OF HYD FLUI
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.