# N905AL: Zipline International P2 ZIP

- Status: Valid registration
- Airframe: [Zipline International P2 ZIP](https://openairdocs.org/model/zipline-international-p2-zip) (registry code 06102II)
- Serial number: 18736P22657
- Type: Hybrid lift
- Engine type: Electric
- Certificate issued: June 8, 2026
- Expires: June 30, 2033
- Mode S code: AC81CA
- Registered owner: [Zipline International Inc](https://openairdocs.org/faa-owner/ZIPLINE%20INTERNATIONAL%20INC)
- Location: [S San Fran, CA](https://openairdocs.org/faa-place/CA/S%20San%20Fran)
- Owner type: Corporation
- Owner's area on the map: 37.6552° N, 122.4184° W: Placed by OpenAirDocs at the center of ZIP code 94080, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=905AL
- Page: https://openairdocs.org/aircraft/N905AL

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Zipline International P2 ZIP)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N905AL.

## FAA accident and incident reports

None matched to N905AL.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty 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 39LA2013031300004](https://openairdocs.org/sdr/39LA2013031300004), Mar 12, 2013: HOSE. COLLAPSED. AFTER 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 
- [SDR 39LA2013030800004](https://openairdocs.org/sdr/39LA2013030800004), Mar 5, 2013: ENGINE. MALFUNCTIONED. IMMEDIATLY 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 A
- [SDR P4YA2010031000001](https://openairdocs.org/sdr/P4YA2010031000001), Mar 10, 2010: LINE. CHAFED. ACFT 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

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Zipline International P2 ZIP aircraft: https://openairdocs.org/model/zipline-international-p2-zip/aircraft.md

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