# N508NA: 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: 18735P2896 - Type: Hybrid lift - Engine type: Electric - Certificate issued: November 24, 2025 - Expires: November 30, 2032 - Mode S code: A658D5 - 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=508NA - Page: https://openairdocs.org/aircraft/N508NA 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 N508NA. ## FAA accident and incident reports None matched to N508NA. ## 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 N508NA not matched to an aircraft (12) They name N508NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 02082201](https://openairdocs.org/sdr/02082201), Aug 19, 2002: SKIN. GOUGED. Gouge in outer skin, STA. 755, STR. 15L. Cut out damaged area, installed fillers and doubler Per E.O. 02-0887. To be Reinspected every 12000 Flight Cycles - [SDR N8TA02081201](https://openairdocs.org/sdr/N8TA02081201), Aug 10, 2002: SILL. CORRODED. CORROSION ON MOP SILL BS 1647, WL 208, LBL 57. REPLACED PER SRM 51-40-02. - [SDR 02080802](https://openairdocs.org/sdr/02080802), Aug 1, 2002: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT BS 1640, RBL 52, WL 208. FLOORBEAM UPPER TEE FOUND TO BE OUT OF LIMITS AT RBL 52 PER SRM 53-00-51. FLOORBEAM REPAIRED PER SRM 53-00-51 - [SDR N8TA02080801](https://openairdocs.org/sdr/N8TA02080801), Aug 1, 2002: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM BODY STATION 377.7, LBL 17, WL 208. FLOORBEAM UPPER CHORD FOUND TO BE CORRODED OUT OF LIMITS AT LBL 6, LBL 11, AND LBL 17 PER SRM 53-00-5 - [SDR N8TA02081901](https://openairdocs.org/sdr/N8TA02081901), Jul 29, 2002: SKIN. GOUGED. GOUGE IN OUTER SKIN STA 758, 2 INCHES ABOVE STR 16L. AFTER BLEND, GOUGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. INTERIM REPAIR DOUBLER, DETAILED PER ER 02-0 - [SDR 2002F00234](https://openairdocs.org/sdr/2002F00234), Feb 5, 2002: CHILLER. SMOKE. SMOKE IN CABIN FROM AFT GALLEY REFRIGERATOR. FLIGHT ATTENDANT PULLED ALL CIRCUIT BREAKERS FOR AFT GALLEY. SMOKE CONTROLLED AND DISSIPATED. AN UNEVENTFUL, UNSCHE - [SDR 2001F00364](https://openairdocs.org/sdr/2001F00364), Aug 14, 2001: DEFLECTOR. DEPARTED. AFTER DEPARTURE OF AIRCRAFT A PORTION OF THE THRUST REVERSER DEFLECTOR BOX ASSEMBLY WAS FOUND ON RUNWAY. INVESTIGATION UPON ARRIVAL OF AIRCRAFT AT NEXT STATION - [SDR 20010409SG004](https://openairdocs.org/sdr/20010409SG004), Feb 8, 2001: TUBE. CRACKED. BLOW OUT GRILL AFT CARGO COMPARTMENT RIGHT WALL, CRACKED AND BENT. REPLACED DAMAGED TUBES IAW BOEING DRAWING 453N1625. (M) - [SDR 20010409SG005](https://openairdocs.org/sdr/20010409SG005), Feb 2, 2001: FITTING. CORRODED. FOUND SURFACE CORROSION IN AREA OF NET TIE DOWN .050 INCH BY 1.5 INCH BY 1 NICH, BS 1442, RBL 22. REPLACED CARGO TIE DOWN FITTING. (M) - [SDR 20010409SG003](https://openairdocs.org/sdr/20010409SG003), Jan 31, 2001: SKIN. DELAMINATED. RIGHT AILERON UPPER SURFACE DELAMINATED 40 INCHES INBOARD OF OUTBOARD END 6 INCHES FORWARD OF TRAILING EDGE. REPAIRED IAW SRM. (M) - [SDR 20010112SG001](https://openairdocs.org/sdr/20010112SG001), Oct 17, 2000: OVEN. DIRTY. DURING CLIMB-OUT, FLIGHT ATTTENDANT REPORTED SMOKE IN AFT CABIN. RETURNED TO DEPARTURE STATION AND MADE AN UNEVENTFUL LANDING. INVESTIGATION REVEALED NR 2 OVEN - [SDR N8TA00010702](https://openairdocs.org/sdr/N8TA00010702), Jan 7, 2000: ENGINE. VIBRATION. DURING TAKEOFF, CREW OBSERVED VIBRATION. ENGINE VIBRATION INDICATED .5. RETURNED TO STATION. INSPECTED ENTIRE EXTERIOR OF AC CHECKED GEAR DOORS, RUDDER, FLAPS S ## 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.