# N409AL: 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: 18736P21598
- Type: Hybrid lift
- Engine type: Electric
- Certificate issued: April 27, 2026
- Expires: April 30, 2033
- Mode S code: A4CE1B
- 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=409AL
- Page: https://openairdocs.org/aircraft/N409AL

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 N409AL.

## FAA accident and incident reports

None matched to N409AL.

## 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 N409AL not matched to an aircraft (15)

They name N409AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ALGA201410098303](https://openairdocs.org/sdr/ALGA201410098303), Oct 9, 2014: BEARING. DAMAGED. ENGINE CHIP LIGHT. UPON TEARDOWN NR 5 BEARING WAS FOUND TO BE DAMAGED.
- [SDR ALGA2012110729142](https://openairdocs.org/sdr/ALGA2012110729142), Nov 5, 2012: MASTER SWITCH. INOPERATIVE. AFTER START UP, THE AVIONICS MASTER SWITCH DID NOT SUPPLY POWER TO AVIONICS AFTER IT WAS TOGGLED ON. REPLACED AVIONICS MASTER SWITCH.
- [SDR ALGA2012061803](https://openairdocs.org/sdr/ALGA2012061803), Jun 18, 2012: BEARING. FAILED. ENGINE CHIP LIGHT CAUSED BY PTO AFT BEARING FAILURE.
- [SDR ALGA8411A1250](https://openairdocs.org/sdr/ALGA8411A1250), Aug 4, 2011: BLADE. CRACKED. MAIN ROTOR BLADE L/E CRACKED AT STA 90.00. TRACER STRANDS BREAKING THROUGH ON LOWER SURFACE SKIN AND TRIM TAB EARS DEBONDED.
- [SDR ALGAR72511BT410](https://openairdocs.org/sdr/ALGAR72511BT410), Jul 25, 2011: DRIVE SHAFT. CORRODED. PITTING CORROSION BEYOND LIMITS ON BOTH ADAPTER END FACES.
- [SDR ALGA106077](https://openairdocs.org/sdr/ALGA106077), Sep 11, 2005: PITCH LINK. BINDING. EXCESSIVE BINDING AND EXCESSIVE AXIAL PLAY. REPLACED WITH NEW BY FIELD MAINTENANCE.
- [SDR ALGA104430](https://openairdocs.org/sdr/ALGA104430), Jun 24, 2005: PITCH LINK. BINDING. PITCH LINK HAS EXCESSIVE AXIAL PLAY; BINDING AND RATCHETY / REPLACED WITH NEW BY FIELD MAINTENANCE.
- [SDR ALGA089096](https://openairdocs.org/sdr/ALGA089096), Sep 11, 2003: UNIVERSAL. BINDING. UNIVERSAL FOUND WORN, BINDING AND RATCHETY. REMOVED AND REPLACED BY FIELD MAINT.
- [SDR ALGA088833](https://openairdocs.org/sdr/ALGA088833), Aug 22, 2003: CHANNEL. CRACKED. CHANNEL CRACKED AT LOWER. AND MIDDLE DZUS RECEPTICALS.PROBABLE CAUSE IS ASB 407-02-54.
- [SDR ALGA088832](https://openairdocs.org/sdr/ALGA088832), Aug 22, 2003: SUPPORT. CRACKED. CHAFED AND CRACKED AT DZUS RECEPTICALS.INSTALLED DOUBLERS AT RECEPTICAL LOCATIONS,AND CHAFE TAPE ALONG LENGTH OF SUPPORT.
- [SDR ALGA086492](https://openairdocs.org/sdr/ALGA086492), May 23, 2003: UNIVERSAL. STICKING. UNIVERAL STICKING, RATCHETY AND WORN. REMOVED AND REPLACED WITH SERVICABLE PART. SUBMITTED BY: PRESTON BARZARE
- [SDR ALG2003F00073](https://openairdocs.org/sdr/ALG2003F00073), Mar 15, 2003: FIREWALL. CRACKED. DAILY. FIREWALL HAD 1.5 INCH CRACK ON FIREWALL LT LWR CORNER OF COMBUSTION CAN DEPRESSION. THICKER FIREWALL.
- [SDR ALGA081626](https://openairdocs.org/sdr/ALGA081626), Dec 11, 2002: UNIVERSAL. WORN. FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE.
- [SDR ALGA081624](https://openairdocs.org/sdr/ALGA081624), Dec 11, 2002: UNIVERSAL. WORN. FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE.
- [SDR 2002F00765](https://openairdocs.org/sdr/2002F00765), Jul 2, 2002: SUPPORT FITTING. CRACKED. TAILBOOM SUPPORT FITTING CRACKED FROM EDGE THROUGH FIRST SCREW HOLE THEN UP RIVETED FLANGE BETWEEN 3RD AND 4TH FASTENER HOLES. CRACK APPEARS TO START FROM TOOLI

## 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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