# N627AL: 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: 18736P22623 - Type: Hybrid lift - Engine type: Electric - Certificate issued: June 3, 2026 - Expires: June 30, 2033 - Mode S code: A83049 - 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=627AL - Page: https://openairdocs.org/aircraft/N627AL 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 N627AL. ## FAA accident and incident reports None matched to N627AL. ## 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 N627AL not matched to an aircraft (50) They name N627AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ALGA2012092104](https://openairdocs.org/sdr/ALGA2012092104), Sep 21, 2012: BEARING. FAILED. ENGINE MAKING METAL, FOUND CAUSE FOR METAL IN OIL TO COME FROM NR 2 BEARING FAILURE. - [SDR ALGA111309847230](https://openairdocs.org/sdr/ALGA111309847230), Nov 13, 2009: FIRESHIELD. MISMANUFACTURED. COULD NOT FIT VERTICAL FIRESHIELD ON ENG GEARBOX. ALL FIRESHIELD MOUNT PADS WELDED OFF CENTER. - [SDR ALG2006F00028](https://openairdocs.org/sdr/ALG2006F00028), Mar 13, 2006: CHIP DETECTOR. DIRTY. UPON TAKEOFF TO HOVER, XMSN CHIP LIGHT ILLUMINATED UPON TAKEOFF TO HOVER. PILOT LANDED AC. MAINTENANCE FOUND LIGHT FUZZ ON LOWER XMSN CHIP PLUG. CLEANED CHIP PL - [SDR ALG2005F00116](https://openairdocs.org/sdr/ALG2005F00116), Nov 13, 2005: INDICATOR. UNKNOWN. ON PREFLIGHT, FOUND 5 SEPARATE DEBONDED AREAS AND A CRACK IN THE WINDSHIELD. REMOVED AND REPLACED DUAL TAC GAUGE. (K) - [SDR ALGA099112](https://openairdocs.org/sdr/ALGA099112), Jan 23, 2005: PITCH LINK. WORN. AXIAL PLAY BEYOND MAX AND ROUGH. REPLACED WITH NEW BY FIELD MAINTENANCE. - [SDR ALGA098819](https://openairdocs.org/sdr/ALGA098819), Dec 28, 2004: PITCH LINK. BINDING. ROUGH, BINDING, AXIAL PLAY BEYOND MAX. REPLACED WITH NEW BY FIELD MAINTENANCE. - [SDR ALG2004F00070](https://openairdocs.org/sdr/ALG2004F00070), Oct 25, 2004: GAUGE. OVERTORQUED. DURING TAKEOFF, TORQUE GAUGE OVERTORQUED WITH NO OTHER EXCEDENCES. THE MECHANIC DRIED THE MOISTURE FROM TORQUE TRANSMITTER, COMPLIED WITH GROUND RUN AND AIRCRAF - [SDR ALG2004F00008](https://openairdocs.org/sdr/ALG2004F00008), Feb 23, 2004: CHIP DETECTOR. CONTAMINATED. DURING TAKEOFF, TRANSMISSION LIGHT CAME ON FOR 30 SECONDS THEN IT WENT OFF. MAINTENANCE FOUND CARBON PARTICLES ON PLUG, CHANGED FILTER AND OIL GROUND RAN LEAKED - [SDR ALG2003F00061](https://openairdocs.org/sdr/ALG2003F00061), May 1, 2003: PRESSURE SWITCH. FAILED. UPON TAXING OUT, THE TRANSMISSION CHIP LIGHT ILLUMINATED. THE PILOT RETURNED TO THE PAD AND LANDED AS SOON AS POSSIBLE. ON SHUT DOWN WHILE TURNING OFF FUEL BOOS - [SDR ALGA086245](https://openairdocs.org/sdr/ALGA086245), Apr 23, 2003: BEARING. WORN. FOUND BEARING WORN AND RATCHETING. BEARING REPLACED BY (FIELD) MAINT. - [SDR ALGA086244](https://openairdocs.org/sdr/ALGA086244), Apr 23, 2003: BEARING. WORN. FOUND BEARING TO BE WORN AND RATCHETING. - [SDR ALG2003F00028](https://openairdocs.org/sdr/ALG2003F00028), Dec 14, 2002: ENGINE. FAILED. DURING CRUISE FLIGHT, ENGINE CHIP LIGHT ILLUMINATED DURING CRUISE FLIGHT. THE PILOT FOLLOWED THE EMERGENCY CHECKLIST AND UPON LANDING THE MECHANIC REMOVED AND R - [SDR ALGA081622](https://openairdocs.org/sdr/ALGA081622), Dec 11, 2002: UNIVERSAL. WORN. FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE. - [SDR ALG2002F00015](https://openairdocs.org/sdr/ALG2002F00015), Jan 20, 2002: BEARING. WORN. DURING PREVENTATIVE MAINTENANCE INSPECTION, BEARINGS ROUGH AND WORN/ BEARINGS SCRAPPED. BEARINGS SHOULD BE MOUNTED IN SELF-CENTERING HOUSING. - [SDR ALG2001F00039](https://openairdocs.org/sdr/ALG2001F00039), Oct 5, 2001: DISC PACK. CRACKED. DURING 25 HOUR AD INSPECTION, FOUND TAIL ROTOR DRIVESHAFT DISC CRACKED. - [SDR 2001F00615](https://openairdocs.org/sdr/2001F00615), Aug 20, 2001: DISC PACK. CRACKED. DURING 25 HOUR INSPECTION, COUPLING IS CRACKED, PROBABLE CAUSE IS EXCESSIVE RIGIDITY IN THE BEARING MOUNT SYSTEM. ALLOW TAILROTOR DRIVESHAFT TO FLOAT SO DISC PA - [SDR 20000912SH014](https://openairdocs.org/sdr/20000912SH014), Aug 6, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND AFT SEGMENT IS CRACKED ACROSS THE SPAN IN TWO PLACES 180 DEGREES APART. (X) - [SDR 20000807SH016](https://openairdocs.org/sdr/20000807SH016), Jul 13, 2000: BUSHING. CORRODED. DURING REPAIR FOR WORN BUSHINGS AND SPACERS, EXCESSIVE CORROSION AROUND AND UNDER BUSHINGS, PN 206-010-338-3. - [SDR 20000807SH009](https://openairdocs.org/sdr/20000807SH009), Jul 13, 2000: BUSHING. WORN. DURING REPAIR FOR WORN BUSHINGS AND SPACERS, EXCESSIVE CORROSION AROUND AND UNDER BUSHINGS, P/N 206-010-338-3. (X) - [SDR 20000807SH008](https://openairdocs.org/sdr/20000807SH008), Jul 12, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, AFT SEGMENT CRACKED ACROSS THE SPAN. (X) - [SDR 20000807SH007](https://openairdocs.org/sdr/20000807SH007), Jul 12, 2000: DISC PACK. CRACKED. DURING 25 HOUR AD INSPECTION, FORWARD SEGMENT CRACKED ACROSS THE SPAN. (X) - [SDR 20000807SH010](https://openairdocs.org/sdr/20000807SH010), Jul 7, 2000: DISC PACK. CRACKED. AFT COUPLING OF NR 2 TAILROTOR DRIVESHAFT HAS A CRACK ACROSS THE SPAN ON THE FORWARD AND AFT SEGMENTS OF THE DISC PACK. (X) - [SDR 20000807SH005](https://openairdocs.org/sdr/20000807SH005), Jul 7, 2000: SEAL. LEAKING. DURING DAILY INSPECTION, FORWARD SEAL LEAKING, CARBON PORTION PITTED. (X) - [SDR 20000807SH015](https://openairdocs.org/sdr/20000807SH015), Jun 28, 2000: PITCH HORN. CORRODED. AT FIRST OVERHAUL OF MAIN ROTOR HUB ASSEMBLY, CORROSION PITTING UNDER BUMPER PLATES. (X) - [SDR 20000807SH014](https://openairdocs.org/sdr/20000807SH014), Jun 28, 2000: PITCH HORN. CORRODED. AT FIRST OVERHAUL OF MAIN ROTOR HUB ASSEMBLY, CORROSION PITTING UNDER BUMPER PLATES. (X) - [SDR 20000807SH011](https://openairdocs.org/sdr/20000807SH011), Jun 23, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, DSIC PACK CRACKED IN TWO PLACES ACROSS THE SPAN OF THE FORWARD SEGMENT. (X) - [SDR 20000807SH013](https://openairdocs.org/sdr/20000807SH013), Jun 8, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, AFT SEGMENT CRACKED ACROSS SPAN. (X) - [SDR 20000807SH012](https://openairdocs.org/sdr/20000807SH012), Jun 6, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, AFT SEGMENT CRACKED ACROSS THE SPAN. (X) - [SDR 20000807SH006](https://openairdocs.org/sdr/20000807SH006), May 20, 2000: DUCT. CRACKED. UPON DAILY INSPECTION, CRACKS IN CORNERS CAUSED BY INHERENT VIBRATION. (X) - [SDR 20000719SH003](https://openairdocs.org/sdr/20000719SH003), Apr 27, 2000: HOUSING. CRACKED. DURING DAILY INSPECTION AND BEARING LUBRICATION, FOUND HOUSING CRACKED AND BLACK GREASE EXPELLED FROM AROUND THE SEAL DETERMINING BEARING DAMAGED. (X) - [SDR 20000719SH002](https://openairdocs.org/sdr/20000719SH002), Apr 27, 2000: HOUSING. CRACKED. DURING DAILY INSPECTION AND BEARING LUBRICATION, FOUND HOUSING CRACKED AND BLACK GREASE EXPELLED FROM AROUND THE SEAL DETERMINING BEARING DAMAGED. (X) - [SDR 20000518SH002](https://openairdocs.org/sdr/20000518SH002), Apr 17, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 5 COUPLING CRACKED THROUGH ONE LAMINATE ON AFT FACING SIDE OF COUPLING, POSSIBLE CAUSE UNKNOWN. (X) - [SDR 20000807SH017](https://openairdocs.org/sdr/20000807SH017), Apr 4, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, ONE LAMINATE IS CRACKED (AFT LAMINATE). (X) - [SDR 20000412SH032](https://openairdocs.org/sdr/20000412SH032), Feb 26, 2000: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND CRACK AT INBOARD FORWARD SEGMENT OF DISC PACK. (X) - [SDR 2000ZZZX808](https://openairdocs.org/sdr/2000ZZZX808), Feb 9, 2000: HOUSING. CRACKED. DURING DAILY INSPECTION, BLOWER HOUSING FOUND CRACKED. - [SDR 2000ZZZX807](https://openairdocs.org/sdr/2000ZZZX807), Feb 9, 2000: BEARING. ROUGH. DURING DAILY INSPECTION, FORWARD BEARING FOUND ROUGH. BOTH FORWARD AND REAR BEARINGS FOUND ROUGH. - [SDR 2000ZZZX806](https://openairdocs.org/sdr/2000ZZZX806), Feb 9, 2000: BEARING. ROUGH. DURING DAILY INSPECTION, FORWARD BEARING FOUND ROUGH. BOTH FORWARD AND REAR BEARINGS FOUND ROUGH. - [SDR 99ZZZX4564](https://openairdocs.org/sdr/99ZZZX4564), Oct 12, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 7 TAILROTOR DISC CRACKED. - [SDR 99ZZZX4567](https://openairdocs.org/sdr/99ZZZX4567), Sep 25, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND CRACKED 1ST FORWARD SEGMENT. - [SDR 99ZZZX4080](https://openairdocs.org/sdr/99ZZZX4080), Aug 25, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 7 COUPLING CRACKED, FIRST FORWARD DISC. - [SDR 99ZZZX3532](https://openairdocs.org/sdr/99ZZZX3532), Aug 12, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK CRACKED. - [SDR 99ZZZX3531](https://openairdocs.org/sdr/99ZZZX3531), Aug 12, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 3 DISC PACK CRACKED. - [SDR 99ZZZX3529](https://openairdocs.org/sdr/99ZZZX3529), Aug 12, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, NR 7 DISC PACK CRACKED. - [SDR 99ZZZX3528](https://openairdocs.org/sdr/99ZZZX3528), Aug 12, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 3 DISC PACK CRACKED. - [SDR 99ZZZX3533](https://openairdocs.org/sdr/99ZZZX3533), Aug 6, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK HAS 2 CRACKS. - [SDR 99ZZZX3530](https://openairdocs.org/sdr/99ZZZX3530), Aug 6, 1999: DISC PACK. CRACKED. DURING 25-HOUR AD INSPECTION. NR 7 DISC PACK HAS 2 CRACKS. - [SDR 99ZZZX3349](https://openairdocs.org/sdr/99ZZZX3349), Jun 24, 1999: SUPPORT. MISINSTALLED. SUPPORT MISINSTALLED. - [SDR 99ZZZX3028](https://openairdocs.org/sdr/99ZZZX3028), Jun 22, 1999: DISC PACK. CRACKED. DURING RECURRING INSPECTION OF AD 97-24-17, ONE OUTBOARD DISC IN THE DISC PACK IS CRACKED. SUBMITTER STATED THIS IS THE SECOND CRACKED NEW STYLE DISC PACK IN 50 - [SDR 99ZZZX3029](https://openairdocs.org/sdr/99ZZZX3029), Jun 13, 1999: DISC PACK. CRACKED. DURING RECURRING INSPECTION OF AD 97-24-17, BOTH OUTBOARD DISCS IN THE DISC PACK ARE CRACKED. SUBMITTER STATED THIS IS THE FIRST OCCURRENCE WITH THE NEW STYLE D - [SDR 99ZZZX1479](https://openairdocs.org/sdr/99ZZZX1479), Feb 17, 1999: DISC PACK. CRACKED. DURING COMPLIANCE OF AD 97-24-17, FOUND DISC PACK 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.