# N605CZ: 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: 18736P22723 - Type: Hybrid lift - Engine type: Electric - Certificate issued: September 29, 2026 - Expires: September 30, 2033 - Mode S code: A7DA1C - 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=605CZ - Page: https://openairdocs.org/aircraft/N605CZ 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 N605CZ. ## FAA accident and incident reports None matched to N605CZ. ## 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 N605CZ not matched to an aircraft (91, newest 50) They name N605CZ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR C77A2019022600002](https://openairdocs.org/sdr/C77A2019022600002), Feb 26, 2019: SEAT TRACK. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE LH IB SEAT TRA - [SDR C77A2019022600001](https://openairdocs.org/sdr/C77A2019022600001), Feb 26, 2019: CROSSBEAM. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE - [SDR C77A2019022500001](https://openairdocs.org/sdr/C77A2019022500001), Feb 26, 2019: RIB. CRACKED. THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH THE INSTRUCTIONS SPECIFIC TO THE LH HORIZONTAL STABILIZER FROM SB 170-55-0014, WHICH ACCOMPLISHES A STRUCTURAL MODI - [SDR C77A2020030400011](https://openairdocs.org/sdr/C77A2020030400011), Feb 24, 2019: DOUBLER. CORRODED. PANEL 192 BL HAS LIGHT SURFACE CORROSION AROUND SCREW HOLES WORK ORDER 2473505619 - [SDR C77A2020030400010](https://openairdocs.org/sdr/C77A2020030400010), Feb 24, 2019: DOUBLER. CORRODED. PANEL 192 CR POSSIBLE CORROSION ON DOUBLER AS MARKED.WORK ORDER 2473505616 - [SDR C77A2020030400009](https://openairdocs.org/sdr/C77A2020030400009), Feb 24, 2019: FLOORBEAM. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-136 - [SDR C77A2020030400008](https://openairdocs.org/sdr/C77A2020030400008), Feb 24, 2019: DOOR SILL. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-136 - [SDR C77A2020030400007](https://openairdocs.org/sdr/C77A2020030400007), Feb 24, 2019: FLOOR SUPPORT. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-136 - [SDR C77A2020030400006](https://openairdocs.org/sdr/C77A2020030400006), Feb 24, 2019: DOOR SILL. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-136 - [SDR C77A2020030400005](https://openairdocs.org/sdr/C77A2020030400005), Feb 24, 2019: FLOOR SPLICE. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRU - [SDR C77A2020030400004](https://openairdocs.org/sdr/C77A2020030400004), Feb 24, 2019: DOOR SILL. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRU - [SDR C77A2020030400003](https://openairdocs.org/sdr/C77A2020030400003), Feb 24, 2019: DOUBLER. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRU - [SDR C77A2020030400002](https://openairdocs.org/sdr/C77A2020030400002), Feb 24, 2019: UPPER SHEET. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTUR - [SDR C77A2020030400001](https://openairdocs.org/sdr/C77A2020030400001), Feb 24, 2019: PANEL SUPPORT. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTUR - [SDR C77A2018062100001](https://openairdocs.org/sdr/C77A2018062100001), Jun 17, 2018: ACTUATOR. FAILED. CREW RECEIVED A NR 2 ENGINE CONTROL FAULT MESSAGE DURING DESCENT. DECLARED AN EMERGENCY. ENGINE PULL BACK TO IDLE FOR LANDING. LANDED SAFELY AND TAXIIED OFF RUN - [SDR C77A20170502002](https://openairdocs.org/sdr/C77A20170502002), Apr 29, 2017: ENGINE. FAULTED. DURING LANDING, THE CREW SLOWED TO 210KTS, CAUSING THRUST TO REDUCE TO IDLE, ONCE AT IDLE A NR 2 ENGINE CONTROL FAULT MESSAGE APPEARED. THE CREW RAN THE QRH AND - [SDR C77A20170414008](https://openairdocs.org/sdr/C77A20170414008), Apr 14, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I RT LATERAL SEAT TRACK P/N 170-92568-005 AND THE - [SDR C77A20170414007](https://openairdocs.org/sdr/C77A20170414007), Apr 14, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I RT LATERAL SEAT TRACK P/N 170-92568-005 AND THE - [SDR C77A20170414006](https://openairdocs.org/sdr/C77A20170414006), Apr 14, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE - [SDR C77A20170414005](https://openairdocs.org/sdr/C77A20170414005), Apr 14, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE - [SDR C77A20170414004](https://openairdocs.org/sdr/C77A20170414004), Apr 14, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE - [SDR C77A20170414002](https://openairdocs.org/sdr/C77A20170414002), Apr 14, 2017: RIB. CRACKED. CRACKED ON THE UPPER FLANGE OF RIB 12A IN THE RT HORIZONTAL STABILIZER. REPAIRED IAW ETD2017-170-031205A FIGURE 1 - [SDR C77A20170414001](https://openairdocs.org/sdr/C77A20170414001), Apr 14, 2017: SKIN. DAMAGED. LH HORIZONTAL STABILIZER UPPER SKIN PANEL, REAR AND MID SPAR BETWEEN RIBS 8-14, AND STRINGERS 4 AND 8 DAMAGED. REPAIRED IAW ETD2017-170-031190, FIGURES 1 THROUG - [SDR C77A2017041102](https://openairdocs.org/sdr/C77A2017041102), Apr 11, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIRS OF CORROSION AND GOUGE DAMAGE TO THE CENTER FUSELAGE I FLOOR STRUCTURE LT INBOAR - [SDR C77A20170411001](https://openairdocs.org/sdr/C77A20170411001), Apr 11, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIRS OF CORROSION AND GOUGE DAMAGE TO THE CENTER FUSELAGE I FLOOR STRUCTURE LT INBOAR - [SDR C77A20170406004](https://openairdocs.org/sdr/C77A20170406004), Apr 6, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE III LT LATERAL SEAT TRACK P/N 170-6591 - [SDR C77A20170406003](https://openairdocs.org/sdr/C77A20170406003), Apr 6, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE III LT LATERAL SEAT TRACK P/N 170-6591 - [SDR C77A20170406002](https://openairdocs.org/sdr/C77A20170406002), Apr 6, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE I FIRST CLASS SEAT TRACKS P/N 171-0173 - [SDR C77A20170406001](https://openairdocs.org/sdr/C77A20170406001), Apr 6, 2017: SEAT TRACK. GOUGED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE I FIRST CLASS SEAT TRACKS P/N 171-0173 - [SDR C77A20161122001](https://openairdocs.org/sdr/C77A20161122001), Nov 22, 2016: BATTERY. INOPERATIVE. R1 FA JUMPSEAT FLASHLIGHT INOPERATIVE. R & R THE BATTERY IAW AMM 31-51-01. OPS CHECKED GOOD. OK FOR SERVICE. - [SDR C77A20161108001](https://openairdocs.org/sdr/C77A20161108001), Nov 7, 2016: MOTOR. SHORTED. DURING FLIGHT (ABOUT 15 MINUTES FROM SEA) THE CREW RECEIVED A STAB LOCK FAULT EICAS MESSAGE. THEY HAVE DECLARED AN EMERGENCY AND WILL BE LANDING IN PDX. PDX HAS - [SDR C77A20161024001](https://openairdocs.org/sdr/C77A20161024001), Oct 21, 2016: BATTERY PACK. INOPERATIVE. FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 33-51-01. OPS CHECKED GOOD. - [SDR C77A20160108002](https://openairdocs.org/sdr/C77A20160108002), Jan 9, 2016: OUTFLOW VALVE. MALFUNCTIONED. PRESN AUTO FAIL. CABIN PRESS DROP. COMPLIED WITH QRH, MSG CLEARED. PRESS RETURNED TO NORM, IN DESCENT. DEFERED IAW MEL 21-31-01-1A. TRANSFERRED TO SDI & PLACARD - [SDR C77A20150515006](https://openairdocs.org/sdr/C77A20150515006), May 14, 2015: WIRE. BROKEN. CAPTAINS FLASHLIGHT LED IS NOT ILLUMINATING. DEFERRED CAPTAINS FLASHLIGHT IAW MEL 25-62-07-1. TRANSFERRED TO SDI AS DMI DM1907904 & PLACARD INSTALLED, OK FOR SE - [SDR C77A20150505019](https://openairdocs.org/sdr/C77A20150505019), May 3, 2015: FLOOR SUPPORT. CORRODED. FORWARD MAIN CABIN LT FLOOR ANGLE PN 170-14731-001 HAS CORROSION AT FRAME 14 , X= 4270 Y= -736.6. R & R LT FLOOR PANEL ANGLE SUPPORT IAW SRM 51-41-01 & 51-43-01 - [SDR C77A20150505018](https://openairdocs.org/sdr/C77A20150505018), May 3, 2015: DOOR SILL. CORRODED. FORWARD MAIN CABIN FLOOR LT FWD SILL PN 170-03275-005 HAS CORROSION AT FRAME 16, X= 4711 Y=-1219.2. R & R RT FWD FLOOR SILL IAW SRM 51-41-01 & 51-43-01 ON WO 14 - [SDR C77A20150505017](https://openairdocs.org/sdr/C77A20150505017), May 3, 2015: DOUBLER. CORRODED. FORWARD MAIN CABIN FLOOR LT FWD DOUBLER PN 170-12118-001 HAS CORROSION AT FRAME 16, X= 4711 BETWEEN Y=-330.2 - -914.4. R & R RT FLOOR DOUBLER IAW SRM 51-41-01 & - [SDR C77A20150505016](https://openairdocs.org/sdr/C77A20150505016), May 3, 2015: FLOOR SUPPORT. CORRODED. FORWARD MAIN CABIN RT FLOOR PANEL SUPPORT PN 170-13939-001 HAS CORROSION AT FRAME 14, X= 4270, Y= 736.6. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-0 - [SDR C77A20150505015](https://openairdocs.org/sdr/C77A20150505015), May 3, 2015: FLOOR SUPPORT. CORRODED. AFT CABIN RT FLOOR SUPPORT PN 170-66797-001 HAS CORROSION AT FRAME 87, RBL 28, X= 23865 Y= 863. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 1 - [SDR C77A20150505014](https://openairdocs.org/sdr/C77A20150505014), May 3, 2015: FLOOR SUPPORT. CORRODED. AFT CABIN RT PANEL SUPPORT PN 170-92908-001 HAS CORROSION AT FRAME 84, RBL 35 - 46, X= 22847 Y= 943-116. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-0 - [SDR C77A20150505013](https://openairdocs.org/sdr/C77A20150505013), May 3, 2015: DOOR SILL. CORRODED. AFT CABIN LT AFT PANEL SUPPORT, SILL, PN 170-86139-005 HAS CORROSION BETWEEN FRAME 88 & 90, LBL 41". X= 24048 - 24868, Y= -947. R & R LT FLOOR PANEL SUPPORT IAW - [SDR C77A20150505012](https://openairdocs.org/sdr/C77A20150505012), May 3, 2015: SUPPORT ANGLE. CORRODED. AFT CABIN RT FLOOR SUPPORT ANGLE PN 170-60287-002 HAS CORROSION 4 INCHES AFT OF FRAME 90, RBL11, X= 24560, Y= 260. R & R RT FLOOR SUPPORT ANGLE IAW SRM 51-41-01 - [SDR C77A20150505011](https://openairdocs.org/sdr/C77A20150505011), May 3, 2015: GUSSET. CORRODED. AFT CABIN RT OTBD GUSSET PLATE PN 170-60259-001 HAS CORROSION AT FRAME 90, RBL22, X= 24868, Y= 559. R & R RT OTBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 14966 - [SDR C77A20150505010](https://openairdocs.org/sdr/C77A20150505010), May 3, 2015: GUSSET. CORRODED. AFT CABIN LT OTBD GUSSET PLATE PN 170-60261-001 HAS CORROSION AT FRAME 90, LBL 21" X=24868, Y= -489. R & R LT OTBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 1496 - [SDR C77A20150505008](https://openairdocs.org/sdr/C77A20150505008), May 3, 2015: GUSSET. CORRODED. AFT CABIN LT INBD GUSSET PLATE PN 170-60257-001 HAS CORROSION AT FRAME 90, LBL 11", X= 24868, Y= -260. R & R LT INBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 14 - [SDR C77A20150505009](https://openairdocs.org/sdr/C77A20150505009), May 3, 2015: GUSSET. CORRODED. RIGHT INBD GUSSET PLATE HAS CORROSION AT FRAME 90, RBL 11. X= 24868, Y= 260. R & R RT INBD GUSSET IAW SRM 51-41-01 & 51-43-01. - [SDR C77A20150505007](https://openairdocs.org/sdr/C77A20150505007), May 3, 2015: PANEL. CORRODED. AFT CABIN LT SHEAR PANEL PN 170-65927-007 HAS CORROSION AT FRAME 87 BETWEEN LBL 12" - LBL 41" . X=23865.0, Y= -304.8- -1041.4. R & R LT SHEAR PANEL IAW SRM 51-4 - [SDR C77A20150505006](https://openairdocs.org/sdr/C77A20150505006), May 3, 2015: PANEL. CORRODED. AFT CABIN CTR SHEAR PANEL PN 170-65928-001 HAS CORROSION AT FRAME 87, BETWEEN LBL 10" - RBL 10", X=23865.0, Y= -222.3 - 222.3. R & R CTR SHEAR PANEL IAW SRM 51- - [SDR C77A20150505005](https://openairdocs.org/sdr/C77A20150505005), May 3, 2015: PANEL. CORRODED. AFT CABIN RT SHEAR PANEL PN 170-91919-001 HAS CORROSION BETWEEN FRAMES 87 - 88, RBL 12 TO 41, X= 23865.0 - 24048.0, Y= 304.8 - 1041.4. R & R RT SHEAR PANEL IAW - [SDR C77A20150505004](https://openairdocs.org/sdr/C77A20150505004), May 3, 2015: UPPER SHEET. CORRODED. AFT CABIN LT UPPER SHEET PN 170-86101-001 HAS CORROSION BETWEEN FRAMES 85 - 86, LBL 11". X= 23041 - 23453, Y= -260. R & R LT UPPER SHEET IAW SRM 51-41-01 & 51-4 All 91: https://openairdocs.org/aircraft/N605CZ/unmatched-reports.md ## 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.