# N507AL: 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: 18736P22506
- Type: Hybrid lift
- Engine type: Electric
- Certificate issued: June 2, 2026
- Expires: June 30, 2033
- Mode S code: A653FC
- 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=507AL
- Page: https://openairdocs.org/aircraft/N507AL

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 N507AL.

## FAA accident and incident reports

None matched to N507AL.

## 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 N507AL not matched to an aircraft (18)

They name N507AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ALGA2012020100075](https://openairdocs.org/sdr/ALGA2012020100075), Feb 1, 2012: MAST. CORRODED. CORROSION FOUND ON TUNGSTEN CARBIDE AREA OF MAST POLE. SENT TO HELICOPTER FOR EVALUATION IAW ASB 407-11-94 MANUAL.
- [SDR ALGA2012012312412](https://openairdocs.org/sdr/ALGA2012012312412), Jan 23, 2012: ADAPTER. CORRODED. MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.
- [SDR ALGA2012012311412](https://openairdocs.org/sdr/ALGA2012012311412), Jan 23, 2012: ADAPTER. CORRODED. MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.
- [SDR ALGA2012012310412](https://openairdocs.org/sdr/ALGA2012012310412), Jan 23, 2012: ADAPTER. CORRODED. MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.
- [SDR ALGA2012012392412](https://openairdocs.org/sdr/ALGA2012012392412), Jan 23, 2012: ADAPTER. CORRODED. MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.
- [SDR ALGA2012012382412](https://openairdocs.org/sdr/ALGA2012012382412), Jan 23, 2012: GRIP. CORRODED. MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.
- [SDR ALGA2012012372412](https://openairdocs.org/sdr/ALGA2012012372412), Jan 23, 2012: GRIP. CORRODED. MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.
- [SDR ALGA2012012362412](https://openairdocs.org/sdr/ALGA2012012362412), Jan 23, 2012: GRIP. CORRODED. MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.
- [SDR ALGA2012012352412](https://openairdocs.org/sdr/ALGA2012012352412), Jan 23, 2012: PITCH HORN. CORRODED. MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.
- [SDR ALGA2012012342412](https://openairdocs.org/sdr/ALGA2012012342412), Jan 23, 2012: PITCH HORN. CORRODED. MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.
- [SDR ALGA2012012332412](https://openairdocs.org/sdr/ALGA2012012332412), Jan 23, 2012: PITCH HORN. CORRODED. MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.
- [SDR ALGA2012012322412](https://openairdocs.org/sdr/ALGA2012012322412), Jan 23, 2012: PITCH HORN. CORRODED. MAIN ROTOR HUB PITCH HORN HAS CORROSION BEYOND LIMITS.
- [SDR ALGA088163](https://openairdocs.org/sdr/ALGA088163), Jul 21, 2003: GEAR. SPALLED. HEAVY SPALLING ON GEAR TEETH, DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED.
- [SDR ALGA088162](https://openairdocs.org/sdr/ALGA088162), Jul 21, 2003: PINION GEAR. SPALLED. HEAVY SPALLING ON GEAR TEETH,DUE TO IMPROPER MESHING OF GEAR TEETH.
- [SDR ALGA088160](https://openairdocs.org/sdr/ALGA088160), Jul 21, 2003: GEAR. SPALLED. HEAVY SPALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED.
- [SDR ALGA088137](https://openairdocs.org/sdr/ALGA088137), Jul 9, 2003: INDICATOR. STUCK. DUAL TACH STUCK AT 120 PERCENT.
- [SDR ALG2003F00098](https://openairdocs.org/sdr/ALG2003F00098), Jun 25, 2003: INDICATOR. MALFUNCTIONED. ON TAKE OFF, DURING CLIMB THE TORQUE INDICATION WENT TO 103 PERCENT FOR 3-5 SECONDS AND (CHECK) INSTRUMENT LIGHT ILLUMINATED. TORQUE WAS REDUCED TO 93 PERCENT W
- [SDR 2000ZZZX820](https://openairdocs.org/sdr/2000ZZZX820), Feb 16, 2000: FUSEABLE PLUG. FAILED. THE AIRCRAFT WAS IN THE HANGAR AND ALL OF THE AIR LEAKED FROM THE FLOAT BOTTLE. THE FUSELAGE PLUG FAILED, DISCHARGED FLOAT BOTTLE.

## 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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