# N513NA: 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: 18735P2893 - Type: Hybrid lift - Engine type: Electric - Certificate issued: November 24, 2025 - Expires: November 30, 2032 - Mode S code: A66DC1 - 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=513NA - Page: https://openairdocs.org/aircraft/N513NA 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 N513NA. ## FAA accident and incident reports None matched to N513NA. ## 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 N513NA not matched to an aircraft (28) They name N513NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ANCF200800032](https://openairdocs.org/sdr/ANCF200800032), Jan 4, 2009: LANDING GEAR. MALFUNCTIONED. AIR TURN BACK, EICAS MSG GEAR DISAGREE AND GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. LT GEAR LIGHT, GEAR AMBER LIGHT AND DOORS AMBER LIGHT ILLUMINATE. IAW AMM 3 - [SDR ANCF200800008](https://openairdocs.org/sdr/ANCF200800008), Apr 13, 2008: WARNING LIGHT. ILLUMINATED. FLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO THE RIGHT TO CENTER COLUMN. FIM PROCEDURE - [SDR ANCF200800004](https://openairdocs.org/sdr/ANCF200800004), Feb 8, 2008: AIR DUCT. LEAKING. EICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIA - [SDR ANCF200700015](https://openairdocs.org/sdr/ANCF200700015), Jun 6, 2007: FILTER. DIRTY. DURING CLIMB CROSSING FL 300 ASC TO FL 370, HAD SMOKE COMING FROM THE PEDALS IN THE COCKPIT. CHECK LIST WAS PERFORMED AND THEN DECIDED GOING TO MIA BECAUSE OF T - [SDR ANCF200600046](https://openairdocs.org/sdr/ANCF200600046), Mar 12, 2007: ENGINE. FAILED. LT ENGIINE SURGED DURING CONSTANT POWER DURING CLIMB AT 6.000 FT. ENGINE OPS NORMAL AFTER SURGE AT LOW THRUST. BOROSCOPE INSPECTION ACCOMPLISHED TO INTERMEDIATE - [SDR ANCF200600034](https://openairdocs.org/sdr/ANCF200600034), Sep 23, 2006: ACCESS PANEL. LOOSE. PILOT REPORT: RT ENG COVER UPPER SIDE SEPARATE DURING TAKE OFF. RT ENG INSPECTED. NO VISIBLE DAMAGE FOUND INTERNAL WING, EMPENNAGE AND FUSELAGE SKIN WERE INSPEC - [SDR 513NA0011](https://openairdocs.org/sdr/513NA0011), Dec 12, 2004: WARNING LIGHT. ILLUMINATED. ABORTED TAKEOFF DUE TO SPOILER MASTER CAUTION LIGHT. PERFORMED BITE PROCEDURE, RESET SYSTEM BY FIM 27-61-00. OPERATIONAL CHECK OK. NEXT FLIGHT: SPOILER OVERHEAD - [SDR 513NA0010](https://openairdocs.org/sdr/513NA0010), Oct 4, 2004: GEARBOX. VIBRATION. ON TAXI OUT, HAD EICAS MESSAGE: LT OIL FILTER. FOUND METAL ON CHIP DETECTOR FOR HIGH SPEED GEAR BOX. REPLACED MAIN OIL FILTER AND SCAVENGE FILTER AND RAN ENGINE - [SDR 513NA0009](https://openairdocs.org/sdr/513NA0009), Jul 30, 2004: BULB. BURNED OUT. EMERGENCY LIGHT OVER 11 DEF INOP. PLACED ON MEL 33-51-1. RELAMPED AND OPS CHECKED OK PER MM 33-50. - [SDR 513NA0008](https://openairdocs.org/sdr/513NA0008), Jun 28, 2004: BOLT. MISSING. DURING WALK-AROUND, FOUND NR 7 MAIN WHEEL ASSEMBLY TIE BOLT MISSING. REPLACED NR 7 MAIN WHEEL ASSEMBLY PER MM 32-45-01. - [SDR 513NA0007](https://openairdocs.org/sdr/513NA0007), Jun 7, 2004: INDICATOR. MALFUNCTIONED. ON DESCENT INTO KSFB, NO AUTO LAND DISPLAYED ON AUTO LAND STATUS INDICATOR. RESET RIGHT FCC AND RAN MCDP TEST PER MM 22-10-00. ALL AUTO PILOT ENGAGE AND FCC CHE - [SDR 513NA0006](https://openairdocs.org/sdr/513NA0006), May 6, 2004: BOLT. MISSING. NR 2 MAIN LANDING GEAR TIRE HAS TWO WHEEL BOLTS MISSING. REPLACED NO. TWO MAIN LANDING GEAR WHEEL/TIRE ASSEMBLY PER MM 32-45-01. - [SDR 513NA0005](https://openairdocs.org/sdr/513NA0005), Apr 15, 2004: BOLT. MISSING. THREE TIE BOLTS MISSING ON THE NR 5 MAIN WHEEL ASSEMBLY. REPLACED LEFT OUTBOARD TIRE ASSEMBLY PER MM 32-45-01. - [SDR 513NA0004](https://openairdocs.org/sdr/513NA0004), Apr 6, 2004: BATTERY PACK. INOPERATIVE. MID CABIN FLOOR ILLUMINATION LIGHTS AND R3 DOOR AND OVERWING EMERGENCY LIGHTS INOP. REPLACED M734 EMERGENCY LIGHT BATTERY PACK PER MM 33-51-0. - [SDR 513NA0003](https://openairdocs.org/sdr/513NA0003), Apr 1, 2004: BOLT. MISSING. NR 7 TIRE ASEMBLY MISSING 3 BOLTS. REPLACED NR 7 MAIN TIRE PER MM 32-45-01. - [SDR 513NA0002](https://openairdocs.org/sdr/513NA0002), Feb 29, 2004: BOLT. MISSING. MAIN WHEEL BOLTS MISSING. REPLACED NR 8 MAIN TIRE (WHEEL ASSEMBLY) PER MM 32-45-01. - [SDR 513NA0001](https://openairdocs.org/sdr/513NA0001), Jul 24, 2003: WINDOW. CRACKED. LEFT FWD WINDOW CRACKED. REPLACED NR 1 FWD WINDOW PER MM 56-11-01 AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-01. OPS CHECKS GOOD. - [SDR HN62003F00000](https://openairdocs.org/sdr/HN62003F00000), Jan 20, 2003: CABLE. CHAFED. NR 2 ENGINE GENERATOR FEEDER CABLES ARE CHAFING ON NR 6 SLAT INBOARD AUXILLARY TRACK. MOUNT PLATE FOR CLAMP IS MISPOSITIONED BELOW AUXILLARY TRACK. THERE ARE 2 - [SDR 02090901](https://openairdocs.org/sdr/02090901), Sep 5, 2002: HYDRAULIC LINE. BURST. Just prior to takeoff, the "R Hyd Press" EICAS Msg. came on and right hyd qty had dropped to "0.45RF". Aircraft returned to the gate. further investigation reve - [SDR 02062501](https://openairdocs.org/sdr/02062501), Jun 22, 2002: WINDOW. During climb out at 25,000 ft., heard a loud bang from back. Flt attendants said window at Row 1D cracked, Aircraft returned to base, an uneventful landing was - [SDR 2002F00241](https://openairdocs.org/sdr/2002F00241), Feb 23, 2002: DUCT. LEAKING. DURING CLIMB, PASSING THROUGH 8,000 FT MSL, LT ENGINE OVERHEAT EICAS' MESSAFE CAME ON. SECURED BLEED VALVE, RETARDED THRUST. MESSAGE EXTINGUISHED. INVESTIGATION - [SDR 02022502](https://openairdocs.org/sdr/02022502), Feb 23, 2002: DUCT. LEAKING. DURING CLIMB, PASSING THROUGH 8,000 FT MSL, LENG OVERHEAT EICAS MESSAGE CAME ON. SECURED BLEED VALVE, RETARDED THRUST; MESSAGE EXTINGUISHED. INVESTIGATION REVEA - [SDR 2001F00746](https://openairdocs.org/sdr/2001F00746), Nov 8, 2001: OIL SYSTEM. LOW. DURING CRUISE, APU OIL ADD LIGHT CAME ON, APU SHUT DOWN. ATTEMPTED RESTART TWICE WITH NO SUCCESS. RIGHT IDG PREVIOUSLY PLACED ON MEL. ACCOMPLISHED UNEVENTFUL, U - [SDR 20010430AP006](https://openairdocs.org/sdr/20010430AP006), Mar 28, 2001: WARNING SYSTEM. ACTIVATED. ON APPROACH, IN LANDING CONFIGURATION, LE SLAT DISAGREE AND TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXTENDED USING ALTERNATE EXTENSION. ACCOMPLISHED OPERATI - [SDR 20010425AP007](https://openairdocs.org/sdr/20010425AP007), Mar 8, 2001: POWER SUPPLY. INOPERATIVE. NUMEROUS ESCAPE PATH LIGHTING LIGHTS ON SEATS NOT WORKING. REPAIRED WIRING AT POWER SUPPLY AND REPLACED POWER SUPPLY. (M) - [SDR 20010112SG037](https://openairdocs.org/sdr/20010112SG037), Nov 13, 2000: CONTROL CABLE. OUT OF RIG. ON TAKEOFF, HEADING EDGE SLATS STOPPED IN INTERMEDIATE POSITION AND A SLAT DISAGREE MESSAGE WAS RECEIVED. INVESTIGATION REVEALED CABLE TO LEFT PDU OUT OF RIG. R - [SDR 20010108AP002](https://openairdocs.org/sdr/20010108AP002), Oct 5, 2000: PRESSURE SWITCH. FAILED. ON DESCENT, ENGINE NR 1 ROLLED BACK AND FLAMED OUT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. UPON INVESTIGATION TRANCIENT PRESSURE UNIT (TPU) BITE WAS ACCOMPLISH - [SDR 20010425AP001](https://openairdocs.org/sdr/20010425AP001), Aug 8, 2000: POWER SUPPLY. INOPERATIVE. NUMEROUS ESCAPE PATH LIGHTING LIGHTS ON SEATS NOT WORKING. REPAIRED WIRING AT POWER SUPPLY AND REPLACED POWER SUPPLY. (M) ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N513NA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N513NA before. - [Cancelled 2011-11-23](https://openairdocs.org/deregistered/N513NA-2011-11-23): Aerospatiale ATR42-500, S/N 0513. Exported to Colombia. Owner: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx) - [Cancelled 1995-06-05](https://openairdocs.org/deregistered/N513NA-1995-06-05): Mitsubishi MU-2B-30, S/N 513, built 1970. Owner: [Bush Field Aircraft Co](https://openairdocs.org/faa-owner/BUSH%20FIELD%20AIRCRAFT%20CO), [Augusta, GA](https://openairdocs.org/faa-place/GA/Augusta) ## 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.