# N607AL: 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: 18736P22624 - Type: Hybrid lift - Engine type: Electric - Certificate issued: June 3, 2026 - Expires: June 30, 2033 - Mode S code: A7E14B - 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=607AL - Page: https://openairdocs.org/aircraft/N607AL 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 N607AL. ## FAA accident and incident reports None matched to N607AL. ## Reports on N607AL not matched to an aircraft (1) They name N607AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20020203021749I](https://openairdocs.org/incident/20020203021749I), Feb 3, 2002: Bell 407 (N607AL), Sabinepass, TX, Minor damage. (-23) Pilot was repositioning the helicopter on the offshore helideck, alaminos canyon-25 (AC-25), located approximately 140 NM south of sabine pass, TX, when… ## 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 N607AL not matched to an aircraft (24) They name N607AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ALGA2012051803](https://openairdocs.org/sdr/ALGA2012051803), May 18, 2012: ADAPTER. CORRODED. ADAPTER CORRODED BEYOND LIMITS. - [SDR ALGA2012051802](https://openairdocs.org/sdr/ALGA2012051802), May 18, 2012: ADAPTER. CORRODED. ADAPTER CORRODED BEYOND LIMITS. - [SDR ALGA201202070008](https://openairdocs.org/sdr/ALGA201202070008), Feb 7, 2012: CROSSTUBE. CORRODED. CROSSTUBE CORRODED BEYOND REPAIRABLE LIMITS. - [SDR ALGAR911153264](https://openairdocs.org/sdr/ALGAR911153264), Sep 1, 2011: SKID. CORRODED. SKID TUBE CORRODED BEYOND MANUFACTURER'S LIMITS. - [SDR ALGA030611607AL](https://openairdocs.org/sdr/ALGA030611607AL), Mar 6, 2011: BLADE. CRACKED. DURING DAILY SERVICE CHECK FOUND CRACKED L/E ON ORANGE MAIN ROTOR BLADE. - [SDR ALGA9110944443](https://openairdocs.org/sdr/ALGA9110944443), Sep 11, 2009: FIRESHIELD. MISALIGNED. ALL MOUNT PADS ON FIRESHIELD HAD RAISED SHEETMETAL FROM IMPROPER FIT. - [SDR ALG2004F00009](https://openairdocs.org/sdr/ALG2004F00009), Feb 27, 2004: CONNECTOR. FAILED. WHEN AIRCRAFT WAS PICKED UP TO A HOVER. AS AIRCRAFT CAME TO A HOVER, ENGINE OIL PRESSURE WENT HIGH. AIRCRAFT WAS LANDED BACK ON PAD, SHUT DOWN AND CONTACTED MAI - [SDR ALGA086242](https://openairdocs.org/sdr/ALGA086242), Apr 23, 2003: BEARING. ROUGH. FOUND BEARINGS ROUGH AND RATCHETING. - [SDR ALG2003F00022](https://openairdocs.org/sdr/ALG2003F00022), Jan 16, 2003: LINE. LEAKING. DURING POST FLIGHT. DURING POST FLIGHT PILOT NOTICED EXCESSIVE AMOUNT OF RESIDUAL OIL ON THE LEFT SIDE OF THE FUSELAGE, THE MECHANIC FOUND THE T/R HYDRAULIC RET - [SDR ALG2002F00019](https://openairdocs.org/sdr/ALG2002F00019), Mar 18, 2002: SPLINE ADAPTER. WORN. DURING OVERHAUL, FOUND SPLINE WEAR BELOW MIN. - [SDR ALG2002F00018](https://openairdocs.org/sdr/ALG2002F00018), Mar 18, 2002: SPRAG CLUTCH. WORN. DURING OVERHAUL FOUND, CAGE SLOTS WORN BEYOND MAX. LIMIT, 1 EACH SPRAG BREAKING DOWN ON INNER CAM FACE. TO PREVENT RECURRENCE: STRONGER ALLOY. - [SDR 2001F00559](https://openairdocs.org/sdr/2001F00559), Sep 3, 2001: BEARING. WORN. DURING DAILY, HIGH VIBE AND TEMP AT FORWARD BEARING, GREY GREASE. (M) - [SDR 20001219SH024](https://openairdocs.org/sdr/20001219SH024), Nov 16, 2000: SHAFT. WORN. DURING 2,500 HOUR OVERHAUL, SPLINES WERE WORN BELOW LIMITS. (X) - [SDR 20000912SH013](https://openairdocs.org/sdr/20000912SH013), Aug 9, 2000: SUN GEAR. MAKING METAL. TRANSMISSION ASSEMBLY MAKING METAL. SUN GEAR UPPER TEETH PITTED (BREAKING DOWN). SUN GEAR SCRAPPED. (X) - [SDR 20000807SH020](https://openairdocs.org/sdr/20000807SH020), Jun 19, 2000: DISC PACK. CRACKED. DURING 50-HOUR VISUAL INSPECTION, NR 3 TAILROTOR DRIVESHAFT DISC PACK IS CRACKED ON AFT SIDE. (X) - [SDR 20000719SH001](https://openairdocs.org/sdr/20000719SH001), May 1, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, TAIL ROTOR DRIVESHAFT FOUND CRACKED. (X) - [SDR 2000ZZZX435](https://openairdocs.org/sdr/2000ZZZX435), Dec 27, 1999: BEARING. DEBONDED. FOUND ON POST-FLIGHT, ELASTOMERIC BEARING DEBONDED COMPLETELY. - [SDR 2000ZZZX16](https://openairdocs.org/sdr/2000ZZZX16), Nov 30, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK CRACKED ON LAST AFT LAMINATE. (X) - [SDR 2000ZZZX15](https://openairdocs.org/sdr/2000ZZZX15), Nov 13, 1999: SUPPORT. MISINSTALLED. DURING DAILY INSPECTION, FOUND PART INSTALLED IN PRELOADED CONDITION. - [SDR 99ZZZX4563](https://openairdocs.org/sdr/99ZZZX4563), Oct 21, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION. DURING DAILY INSPECTION. DISC PACK FOUND CRACKED WITH CRACK FACING AFT TOWARDS TAIL ROTOR IN NR 3 POSITION. CAUSE NOT KNOWN. ONLY - [SDR 99ZZZX4427](https://openairdocs.org/sdr/99ZZZX4427), Oct 21, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION. DURING DAILY INSPECTION. DISC PACK FOUND CRACKED WITH CRACK FACING AFT TOWARDS TAIL ROTOR IN NR 3 POSITION, CAUSE NOT KNOWN. ONLY - [SDR 99ZZZX4599](https://openairdocs.org/sdr/99ZZZX4599), Aug 26, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND CRACK AT FORWARD SEGMENT AT THE DISC PACK, NR 3 POSITION. - [SDR 99ZZZX3527](https://openairdocs.org/sdr/99ZZZX3527), Aug 19, 1999: SUPPORT. CRACKED. SUPPORT CRACKED, THIRD FROM OUTBOARD EDGE. - [SDR 99ZZZX3213](https://openairdocs.org/sdr/99ZZZX3213), Jun 22, 1999: DISC PACK. CRACKED. DURING 25-HOUR INSPECTION, AD 97-24-17. COUPLING DISC CRACKED. ## 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.