# N602CZ: 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: 18736P22896 - Type: Hybrid lift - Engine type: Electric - Certificate issued: June 12, 2026 - Expires: June 30, 2033 - Mode S code: A7CEF7 - 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=602CZ - Page: https://openairdocs.org/aircraft/N602CZ 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 N602CZ. ## FAA accident and incident reports None matched to N602CZ. ## 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 N602CZ not matched to an aircraft (117, newest 50) They name N602CZ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR C77A2019101100001](https://openairdocs.org/sdr/C77A2019101100001), Oct 8, 2019: SIGN. INOPERATIVE. R1 DOOR EMERGENCY LIGHT INOP - LOWER "EXIT" LIGHT. REPLACED R1 DOOR LIGHT ID SIGN PER AMM 33-50-17 OPS CHECK GOOD. - [SDR C77A2019010700001](https://openairdocs.org/sdr/C77A2019010700001), Jan 9, 2019: RIB. BROKEN. THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH PART II OF SB 170-57-0047, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION ON THE RT WING. THIS MODIFICATION CONSISTS - [SDR C77A2019010200003](https://openairdocs.org/sdr/C77A2019010200003), Jan 2, 2019: SEAT TRACK. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LT INBOARD SEAT TRACK P/N 170- - [SDR C77A2019010200002](https://openairdocs.org/sdr/C77A2019010200002), Jan 2, 2019: SEAT TRACK. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LT INBOARD SEAT TRACK P/N 170- - [SDR C77A2019010200001](https://openairdocs.org/sdr/C77A2019010200001), Jan 2, 2019: FLOORBEAM. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE UPPER FLANGE OF THE CENTER FUSELAGE II LT FLOORBEAM - [SDR C77A2020031800008](https://openairdocs.org/sdr/C77A2020031800008), Dec 20, 2018: BEAM. CORRODED. DURING BASIC CHECK IN BNA, INSPECTION DISCOVERED CORROSION IN TWO BOLT HOLES ON THE FORWARD PASSENGER DOOR LOWER BEAM, P/N 170-03719-005. (REF ETD2018-170-13519 - [SDR C77A2020031800022](https://openairdocs.org/sdr/C77A2020031800022), Dec 19, 2018: DOUBLER. CORRODED. MID BELLY PANEL 192CR DOUBLER CORRODED WORK ORDER 2450172623 - [SDR C77A2020031800013](https://openairdocs.org/sdr/C77A2020031800013), Dec 19, 2018: HEAT SHIELD. CRACKED. AIRCRAFT 602CZ WAS AOG IN SJC DUE TO THE DISCOVERY OF CRACKS ON THE LH ENGINE PYLON AFT FAIRING #5 HEAT SHIELD (REF ETD2018-170-093210A, FIGURES 1-3). COMPASS A - [SDR C77A2020031800016](https://openairdocs.org/sdr/C77A2020031800016), Dec 17, 2018: PANEL SUPPORT. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644- - [SDR C77A2020031800015](https://openairdocs.org/sdr/C77A2020031800015), Dec 17, 2018: SPLICE. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644- - [SDR C77A2020031800012](https://openairdocs.org/sdr/C77A2020031800012), Dec 17, 2018: FIREWALL. DAMAGED. DURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED FIRE LOOP CLAMP RIVET HOLES ELONGATED IN THE APU COMPARTMENT IN THE REAR FUSELAGE (REF ETD2018-170-133016, FIG - [SDR C77A2020031800021](https://openairdocs.org/sdr/C77A2020031800021), Dec 15, 2018: GUSSET. 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 C77A2020031800020](https://openairdocs.org/sdr/C77A2020031800020), Dec 15, 2018: SPLICE. 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 C77A2020031800019](https://openairdocs.org/sdr/C77A2020031800019), Dec 15, 2018: DOOR SILL. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-0566 - [SDR C77A2020031800018](https://openairdocs.org/sdr/C77A2020031800018), Dec 15, 2018: DOUBLER. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-0566 - [SDR C77A2020031800017](https://openairdocs.org/sdr/C77A2020031800017), Dec 15, 2018: DOOR SILL. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-0566 - [SDR C77A2020031800014](https://openairdocs.org/sdr/C77A2020031800014), Dec 15, 2018: GUSSET. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644- - [SDR C77A2020031800011](https://openairdocs.org/sdr/C77A2020031800011), Dec 15, 2018: SHEAR TIE. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON TWO SHEAR CLIPS IN THE AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO - [SDR C77A2020031800010](https://openairdocs.org/sdr/C77A2020031800010), Dec 15, 2018: SHEAR TIE. CORRODED. DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON TWO SHEAR CLIPS IN THE AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO - [SDR C77A2020031700007](https://openairdocs.org/sdr/C77A2020031700007), Dec 15, 2018: TUBE. CHAFED. DURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED CHAFE DAMAGE ON THE MOVABLE SHAFT TUBE, P/N 170-83123-001, WHICH IS PART OF THE FORWARD PASSENGER DOOR FORWARD - [SDR C77A2020031800023](https://openairdocs.org/sdr/C77A2020031800023), Dec 14, 2018: SEAL REST. CORRODED. FORWARD CARGO CUTOUT, AFT SEAL REST REST HAS CORROSION AS MARKED.WORK ORDER 2450172273 - [SDR C77A2020031800009](https://openairdocs.org/sdr/C77A2020031800009), Dec 12, 2018: BEAM. CORRODED. DURING BASIC CHECK IN BNA, INSPECTION DISCOVERED CORROSION IN A FASTENER HOLE LOCATED IN THE FORWARD SERVICE DOOR LOWER BEAM (REF ETD2018-170-132950, FIGURE 1). - [SDR C77A2018072400002](https://openairdocs.org/sdr/C77A2018072400002), Jul 23, 2018: WARNING SYSTEM. FALSE ACTIVATION. SOC RECEIVED ACARS MESSAGE STATING "CABIN HIGH ALT. DECLARED EMERGENCY." CREW ALSO STATED IN ACARS THEY WOULD BE RETURNING TO SEA. SEA OPS NOTIFIED. AC HAS LAND - [SDR C77A20171124002](https://openairdocs.org/sdr/C77A20171124002), Nov 18, 2017: WIRE HARNESS. CHAFED. CREW REPORTED A LOSS OF IDG 1 AFTER TAKE-OFF. FLIGHT RETURNED TO DEPARTURE, EMERGENCY DECLARED. IDG 2 OIL CAUTION MESSAGE IN FLIGHT. QRH 5.15 COMPLIED WITH. DIS - [SDR C77A20170216002](https://openairdocs.org/sdr/C77A20170216002), Feb 16, 2017: RIB. CRACKED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CRACK DAMAGE TO THE UPPER AND LOWER FLANGES OF RT RIB 11A P/N 170-62783-0 - [SDR C77A20170216001](https://openairdocs.org/sdr/C77A20170216001), Feb 16, 2017: RIB. CRACKED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CRACK DAMAGE TO THE UPPER AND LOWER FLANGES OF RT RIB 11A P/N 170-62783-0 - [SDR C77A20170211002](https://openairdocs.org/sdr/C77A20170211002), Feb 11, 2017: FLOORBEAM. CORRODED. AFT CABIN FLOOR, RT FLOORBEAM P/N 170-65669-004 HAS CORROSION IN SEVERAL AREAS FROM FRAME 86 - 89. X=23403 -24408, Y= 273. REMOVED AND REPLACED AFT CABIN RT FLO - [SDR C77A20170211001](https://openairdocs.org/sdr/C77A20170211001), Feb 11, 2017: FLOORBEAM. CORRODED. AFT CABIN FLOOR, LT FLOORBEAM P/N 170-65669-003, HAS CORROSION IN SEVERAL AREAS FROM FRAME 86 - 89 X=23403 - 24408. Y= -273. REMOVED AND REPLACED AFT CABIN LT F - [SDR C77A20170210002](https://openairdocs.org/sdr/C77A20170210002), Feb 10, 2017: FLOORBEAM. CORRODED. CORROSION DAMAGE TO THE UPPER FLANGE OF THE FRAME 14 FLOORBEAM. REPAIRED IAW ETD2015-170-016971A. - [SDR C77A20170209002](https://openairdocs.org/sdr/C77A20170209002), Feb 9, 2017: GUSSET. GOUGED. EO E175-52MR-003 WAS ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE R1 DOOR INTERNAL GUSSET PLATE, WHICH WAS DISCOVERE - [SDR C77A20170209001](https://openairdocs.org/sdr/C77A20170209001), Feb 9, 2017: CROSSBEAM. CORRODED. EO E175-53MR-159 WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR17 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015 - [SDR C77A20170207001](https://openairdocs.org/sdr/C77A20170207001), Feb 7, 2017: SEAT TRACK. CORRODED. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE FWD CABIN FLOOR STRUCTURE RT SEAT TRACK P/N 170-0326 - [SDR C77A20161219003](https://openairdocs.org/sdr/C77A20161219003), Dec 18, 2016: WARNING LIGHT. ILLUMINATED. IN FLIGHT THE CREW RECEIVED A CARGO FWD FIRE SYSTEM FAIL EICAS MESSAGE. AN EMERGENCY WAS DECLARED AND THE FLIGHT PERFORMED AN AIR RETURN TO DEPARTURE. - [SDR C77A20161031003](https://openairdocs.org/sdr/C77A20161031003), Oct 27, 2016: WIRE HARNESS. FAULTED. DURING DESCENT, THE CREW RECEIVED A FLAP/SLAT FAIL MESSAGE AT 4000 FT. DECLARED AN EMERGENCY AND MANAGED TO GET A NO SLAT/FLAP FAIL MESSAGE PRIOR TO LANDING. TH - [SDR C77A20160816002](https://openairdocs.org/sdr/C77A20160816002), Aug 14, 2016: UPLOCK. FAILED. NLG UNCOMMANDED DOWN WITH NO ABNORMAL EICAS INDICATION. R & R NOSE LANDING GEAR UPLOCK IAW AMM 32-32-03. OPS TEST OF LANDING GEAR EXTENSION & RETRACTION SYSTEM - [SDR C77A20160718002](https://openairdocs.org/sdr/C77A20160718002), Jul 14, 2016: LANDING GEAR. MALFUNCTIONED. AFTER GEAR RETRACTION, NOSE GEAR MADE CONTINUOUS BANGING NOISE WITH LANDING GEAR INDICATION TURNING AMBER AT SAME TIME. RETURNED HANDLE TO GEAR DOWN POSITION. T - [SDR C77A20160713002](https://openairdocs.org/sdr/C77A20160713002), Jul 12, 2016: COMPRESSOR. ODOR. DURING FLIGHT, THERE WAS AN ODOR OF BURNING PLASTIC. THE AIRCRAFT DIVERTED AND AN EMERGENCY WAS DECLARED. FOUND PROBLEM TO BE CAUSED BY POTABLE WATER SYSTEM AIR - [SDR C77A20151026003](https://openairdocs.org/sdr/C77A20151026003), Oct 24, 2015: ACTUATOR. INOPERATIVE. ON DECENT NOTICED NO PITCH TRIM INDICATION, DISCOUNTED AP, UPON DISCONNECTION OF AP, RECEIVED AP FAIL & PITCH TRIM FAIL EICAS MSG. PERFORMED QRH CH S 3.3 & 7.16 - [SDR C77A20150521001](https://openairdocs.org/sdr/C77A20150521001), May 20, 2015: BATTERY. DISCHARGED. L1 FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD. - [SDR C77A201503050021](https://openairdocs.org/sdr/C77A201503050021), Mar 2, 2015: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN INNER SURFACE AT AFT CARGO COMPARTMENT BETWEEN FRAME 80 & 81, STATION 21446 & OTBD SIDE OF STRINGER 28R. BLENDED CORRODED AREA IAW SR - [SDR C77A201503050019](https://openairdocs.org/sdr/C77A201503050019), Mar 2, 2015: RETAINER. CORRODED. CORROSION ON WATER SERVICE ACCESS PAN FWD RETAINER, PN 170-86656-001 & AFT RETAINER, PN 170-86657-001, BETWEEN STATION 21263 & 21675, STRINGER 27L - 29L. PERMAN - [SDR C77A201503050020](https://openairdocs.org/sdr/C77A201503050020), Mar 2, 2015: RETAINER. CORRODED. CORROSION ON WASTE SERVICE ACCESS PAN FWD RETAINER, PN 170-86654-003, AFT RETAINER, PN 170-86655-003, BETWEEN STATION 22270 & 22680, STRINGER 24R - 26R. PERMANE - [SDR C77A20150305019](https://openairdocs.org/sdr/C77A20150305019), Mar 2, 2015: RETAINER. CORRODED. CORROSION ON WATER SERVICE ACCESS PAN FWD RETAINER, PN 170-86656-001, AFT RETAINER, PN 170-86657-001, BETWEEN STATION 21263 & 21675, STRINGER 27L - 29L. PERMANE - [SDR C77A20150305018](https://openairdocs.org/sdr/C77A20150305018), Mar 2, 2015: SKIN. CORRODED. AFT CARGO COMPARTMENT BILGE SKIN HAS CORROSION AROUND RIVETS BETWEEN FRAME 77 - 78 & BETWEEN STRINGER 29L - 29R, X=20007 - 20387. REMOVED CORROSION BY BLENDING - [SDR C77A20150305017](https://openairdocs.org/sdr/C77A20150305017), Mar 2, 2015: SEAL DEPRESSOR. CORRODED. AFT CARGO DOOR LOWER CTR SEAL DEPRESSOR, PN 170-85251-401, HAS CORROSION X=20242.0 - 20950.7, STRINGER 27R. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01. M - [SDR C77A20150305016](https://openairdocs.org/sdr/C77A20150305016), Mar 2, 2015: UPPER SHEET. CORRODED. AFT CABIN RT UPPER SHEET, PN 170-86101-001 HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y=260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON - [SDR C77A20150305015](https://openairdocs.org/sdr/C77A20150305015), Mar 2, 2015: UPPER SHEET. CORRODED. AFT CABIN LT UPPER SHEET, PN 170-86101-001, HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y= -260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 - [SDR C77A20150305014](https://openairdocs.org/sdr/C77A20150305014), Mar 2, 2015: PANEL. CORRODED. AFT CABIN RT SHEAR PANEL, PN 170-91919-001, HAS CORROSION BETWEEN FRAME 87 & 88, X= 23865, FROM Y= 304.8 - Y= 1041.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 5 - [SDR C77A20150305013](https://openairdocs.org/sdr/C77A20150305013), Mar 2, 2015: PANEL. CORRODED. AFT CABIN FLOOR CTR SHEAR PANEL, PN 170-65928-001, HAS CORROSION BETWEEN FRAME 87 & 88, X= 23865, FROM Y= -222.3 - Y= 222.3. BLENDED CORRODED AREA IAW SRM 51-10 - [SDR C77A20150305012](https://openairdocs.org/sdr/C77A20150305012), Mar 2, 2015: PANEL SUPPORT. CORRODED. AFT CABIN CROSS FRAME 87, RT OTBD FLOOR PANEL SUPPORT, PN 170-66797-001, HAS CORROSION AT FRAME 87, X= 23865, Y=711.2. BLENDED CORRODED AREA IAW SRM 51-10-03 & All 117: https://openairdocs.org/aircraft/N602CZ/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.