# N587AL: 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: 18736P22538 - Type: Hybrid lift - Engine type: Electric - Certificate issued: June 3, 2026 - Expires: June 30, 2033 - Mode S code: A78FF4 - 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=587AL - Page: https://openairdocs.org/aircraft/N587AL 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 N587AL. ## FAA accident and incident reports None matched to N587AL. ## 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 N587AL not matched to an aircraft (25) They name N587AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ALGA2012071702](https://openairdocs.org/sdr/ALGA2012071702), Jul 17, 2012: STOP. DAMAGED. ON DISASSEMBLY, DUE TO BROKEN SPRING RETAINER, FOUND HOUSING, STOP ASSY, DAMAGED BEYOND REPAIR AND WAS REPLACED. - [SDR ALGA2012051601](https://openairdocs.org/sdr/ALGA2012051601), May 16, 2012: HUB. DAMAGED. ONE SHEAR BEARING PN 407-310-101-101, SN LK13178 ELASTOMERIC SEPARATED FOUR FEATHER BEARINGS PN 407-310-102-101, SN'S LK3060, LK3654, LK5682, LK5644 WITH ELASTO - [SDR ALGA2012042702](https://openairdocs.org/sdr/ALGA2012042702), Apr 27, 2012: FRAHM. MULTIPLE FAIL. DURING COURSE OF REPAIR TO FRAHM DAMPER FOUND STOP ASSY, (407-010-165-103), & HOUSING, (407-010-152-109) DESTROYED. SEVEN SPRINGS (407-310-104-105) GOUGED. ONE - [SDR ALGA2012042604](https://openairdocs.org/sdr/ALGA2012042604), Apr 26, 2012: STRUCTURE. CRACKED. CRACKED BEARING BORE GOING OUTWARD. - [SDR ALGAR1271145515](https://openairdocs.org/sdr/ALGAR1271145515), Jan 27, 2011: MOUNT. CRACKED. FOUND CRACKING OF FWD FLANGE OF REAR SUPPORT. - [SDR ALGA122810587AL](https://openairdocs.org/sdr/ALGA122810587AL), Dec 28, 2010: BLEED AIR SYS. SMOKE. IN CRUISE FLIGHT, FRONT SEAT PASSENGER ALERTED PILOT AN ODOR OF SOMETHING BURNING THEN SAW SMOKE BY HIS FEET (HEATER VENT AREA). PILOT TURNED OFF HEATER AND RET - [SDR ALG2005F00025](https://openairdocs.org/sdr/ALG2005F00025), Apr 16, 2005: HOSE. LEAKING. AT CRUISE FLIGHT AT 2750 FT, HEADING NORTH NORTHEAST, HYDRAULIC CAUTION LIGHT ILLUMINATED AND CONTROLS BECAME STIFF. MAINTENANCE FOUND THE CASE DRAIN LINE FLEX - [SDR ALGA099111](https://openairdocs.org/sdr/ALGA099111), Jan 22, 2005: PITCH LINK. WORN. AXIAL PLAY BEYOND MAX AND RATCHETY. REPLACED WITH NEW BY FIELD MAINTENANCE. - [SDR ALG2005F00005](https://openairdocs.org/sdr/ALG2005F00005), Nov 29, 2004: MANIFOLD. DAMAGED. AFTER LANDING AT SS69 PASSENGER INFORMED THE PILOT THERE WAS OIL ALL ALONG THE SIDE OF THE AIRCRAFT. SHUTDOWN AND CHECKED THE TRANSMISSION OIL LEVEL AND THE SIG - [SDR ALGA096465](https://openairdocs.org/sdr/ALGA096465), Jul 18, 2004: DISC PACK. CRACKED. FOUND CRACKED DISC. REPLACED W/NEW PART BY FIELD MAINT. - [SDR ALGA088105](https://openairdocs.org/sdr/ALGA088105), Jul 15, 2003: GEAR. SPALLED. REMOVED GEAR FOR EXCESSIVE SPALLING ON GEAR TEETH. REMOVED FOR WARRANTY CREDIT. - [SDR ALGA088104](https://openairdocs.org/sdr/ALGA088104), Jul 15, 2003: GEAR. SPALLED. REMOVED GEAR FOR EXCESSIVE SPALLING ON GEAR TEETH. - [SDR ALGA086247](https://openairdocs.org/sdr/ALGA086247), Apr 23, 2003: BEARING. WORN. FOUND UNIVERSAL BEARING WORN AND ROUGH. - [SDR ALG2002F00065](https://openairdocs.org/sdr/ALG2002F00065), Aug 28, 2002: SHAFT. WORN. SHAFT ON FREEWHEEL UNIT HAS WORN SPLINES BEYOND LIMITS. - [SDR ALG2002F00029](https://openairdocs.org/sdr/ALG2002F00029), Mar 11, 2002: COWLING. CORRODED. REBUILD. EXCESSIVE CORROSION, CRACKING AND WEAR ON COWLING AND INTAKE SHELF. - [SDR ALG2002F00024](https://openairdocs.org/sdr/ALG2002F00024), Feb 17, 2002: TURBINE WHEEL. CORRODED. TURBINE WAS RECEIVED IN SHOP FOR LOW POWER. FOUND AFTER REMOVAL OF COMBUSTION SECTION FOUND SULPHADATION ON 1ST STAGE WHEEL. - [SDR ALG2002F00009](https://openairdocs.org/sdr/ALG2002F00009), Jan 19, 2002: BEARING. FAILED. DURING PREVENTATIVE MAINTENANCE INSPECTION, BEARING FAILED COMPLETELY, PART SCRAPPED. - [SDR ALG2001F00036](https://openairdocs.org/sdr/ALG2001F00036), Oct 9, 2001: RING. CORRODED. DURING PHASE INSPECTION. CORROSION BEYOND MAXIMUM LIMITS. - [SDR 2001F00613](https://openairdocs.org/sdr/2001F00613), Aug 24, 2001: BEARING. DISINTEGRATED. DURING DAILY, BEARING ON THE SHAFT WAS DISINTEGRATED DUE TO LOSS OF GREASE. BEARING WAS SCRAPPED AND C/W ASB 407-01-44. (M) - [SDR 20001206SH007](https://openairdocs.org/sdr/20001206SH007), Aug 8, 2000: HOUSING. CRACKED. DURING DAILY INSPECTION, FOUND OCB HOUSING CRACKED DUE TO VIBRATION. (X) - [SDR 20000912SH006](https://openairdocs.org/sdr/20000912SH006), Aug 8, 2000: DUCT. CRACKED. DURING DAILY INSPECTION, FOUND A CRACK IN THE CORNER. (X) - [SDR 20000912SH018](https://openairdocs.org/sdr/20000912SH018), Jul 31, 2000: SLEEVE. BINDING. PILOT REPORTED AN INTERMITTENT BIND. INTERMITTENT BIND IN SERVO ACTUATOR. (X) - [SDR 20000807SH003](https://openairdocs.org/sdr/20000807SH003), May 22, 2000: DUCT. CRACKED. UPON DAILY INSPECTION, CRACKS IN CORNERS CAUSED BY INHERENT VIBRATIONS. (X) - [SDR 99ZZZX3351](https://openairdocs.org/sdr/99ZZZX3351), Jun 22, 1999: CROSSTUBE. CORRODED. CORROSION FOUND UNDER SUPPORT AND CLAMPS DUE POSSIBLY TO IMPROPER TREATMENT DURING MANUFACTURING AND/OR MATERIAL DEFECT. - [SDR 98ZZZX3517](https://openairdocs.org/sdr/98ZZZX3517), Aug 5, 1998: BOLT. LOOSE. DURING DAILY SERVICE CHECK, FOUND UPPER AND LOWER AFT BOLTS TO HAVE LOST TORQUE. ## 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.