# N346AL: 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: 18736P21559
- Type: Hybrid lift
- Engine type: Electric
- Certificate issued: April 26, 2026
- Expires: April 30, 2033
- Mode S code: A3D3A3
- 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=346AL
- Page: https://openairdocs.org/aircraft/N346AL

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 N346AL.

## FAA accident and incident reports

None matched to N346AL.

## 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 N346AL not matched to an aircraft (8)

They name N346AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR EOPA033011346AL](https://openairdocs.org/sdr/EOPA033011346AL), Mar 30, 2011: STIFFENER. CRACKED. CRACK IN STIFFENER NEAR TOP OF "BROOM CLOSET".
- [SDR 97ZZZX940](https://openairdocs.org/sdr/97ZZZX940), Dec 19, 1996: FRAME. CRACKED. AT MAJOR INSPECTION FOUND CRACK AT BOLT ATTACH ON FRAME P/N 206-032-308-103. SUBMITTER STATED T.B. 206L-94-169 WAS ISSUED TO REDUCE CRACKING OF FRAME P/N 206-03
- [SDR 95ZZZX6880](https://openairdocs.org/sdr/95ZZZX6880), Nov 8, 1995: LINK IDLER. WORN. DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2
- [SDR 95ZZZX6879](https://openairdocs.org/sdr/95ZZZX6879), Nov 8, 1995: LEVER ASSY. WORN. DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2
- [SDR 96ZZZX743](https://openairdocs.org/sdr/96ZZZX743), Sep 29, 1995: HOUSING. UNBONDED. UPON DISASSEMBLY OF THE ENGINE, FOUND BRONZE PLATING UNBONDING AT COMP. BORE. ALSO, FOUND T/M HELICOIL DAMAGED. THE CAUSE FOR BRONZE PLATING UNBONDING IS DUE TO
- [SDR 95ZZZX3351](https://openairdocs.org/sdr/95ZZZX3351), Jun 15, 1995: BULKHEAD. CRACKED. AFTER REMOVAL OF SHIM TO COMPLY WITH TB 206L-94-169. FORWARD BULKHEAD FOUND CRACKED AT RT UPPER AND RT LOWER ATTACH FITTING AREAS. SUSPECT DUE TO STRESS FROM WO
- [SDR 95ZZZX2770](https://openairdocs.org/sdr/95ZZZX2770), May 22, 1995: LINK IDLER. WORN. DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2
- [SDR 95ZZZX2769](https://openairdocs.org/sdr/95ZZZX2769), May 22, 1995: LINK ASSY. WORN. DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2

## 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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