Aircraft Specification Summary Convair CV580 SN: 372 Registration: ZK KFL

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1 Aircraft Specification Summary Convair CV580 SN: 372 Registration: ZK KFL Details as of: 26 January 2016

2 1. Aircraft Specifications AIRCRAFT SPECIFICATIONS Manufacturer: General Dynamics, Convair Division Type and Model: Allison Prop Jet Convair 580 Serial Number: 372 Date of first flight: Oct 1956 Current registration: ZK KFL Country of registration: New Zealand Current operator Air Freight NZ Ltd Current Owner Air Freight NZ Ltd Specification: FAA type certificate 6A6 and STC SA Aircraft Operating Limitations: AFM AIR Aircraft Certification CERTIFICATE OF AIRWORTHINESS Issuing Authority Civil Aviation Authority of New Zealand Initial date of Issue 23 April 1990 Last re issue date 23 April 1990 Expiry Date Non terminating CERTIFICATE OF REGISTRATION Issuing Authority Civil Aviation Authority of New Zealand Date of Issue 23 April 1990 Registered Owner/Operator Air Freight NZ Ltd NOISE CERTIFICATE Compliance FAA FAR 36 Appendix C (stage 3) Printed: Wednesday, 27 January 2016 Page 2 of 9

3 OPERATIONAL FEATURES Feature Comments RNP No ETOPS No 8.33 KHz channelling No GPS Single 3. Airframe Status Airframe Hours: 34,538.5 Landings: 28, Maintenance Program The aircraft is maintained in accordance with the Kelowna Flightcraft Convair CV 580 document P0094 Issue 9 (Number Check) program and current CAA NZ Rules. 3.2 Principal Operating Weights OPERATING WEIGHTS Maximum gross take off weight 58,156 lbs Maximum landing weight 53,000 lbs Basic empty weight 33,225 lbs Max Zero Fuel Weight 50,000 lbs Last reweigh 14 Oct Fuel System FUEL SYSTEM Number of tanks 2 Total fuel tank capacity 2058 US gallons Drip stick calibration US gallons Fuel instrumentation calibration Lbs Printed: Wednesday, 27 January 2016 Page 3 of 9

4 3.4 Overheat and Fire Warning System Engines Cargo compartment FIRE WARNING AND DETECTION Walter Kidde Smoke detectors only 4. Engine Status 4.1 Main Engines Engine LH RH Manufacturer: Allison Compressor Model: 501 D13 Serial number: Time since overhaul (hours): 3, ,296.0 Time remaining to level 1 inspection (hours): 1, ,704.0 Turbine Part number: Serial number: Time since overhaul (hours): 10, ,905.3 Time remaining to level 1 inspection (hours): 4, ,467.6 Time to level 2/next component inspection (hours): 5, ,794.7 Reduction Gearbox Part number: Serial number: Time since overhaul (hours): 1, ,784.7 Time remaining to level 1 inspection (hours): 3, ,849.8 Time remaining to level 2 inspection (hours): 8, ,215.3 Torquemeter Part number: Serial number: A5487 A2518 Time since overhaul (hours): ,744.8 Time remaining to level 1 inspection (hours): 4, ,411.9 Time remaining to level 2 inspection (hours): 9, Engine Efficiency % % Date: 20 Oct Oct 2015 Printed: Wednesday, 27 January 2016 Page 4 of 9

5 4.2 GPU GPU Manufacturer: Honeywell Part Number: GTC Serial number: P Propeller Status PROPELLER LH RH Manufacturer: Aeroproducts Part number: A6441FN 606 Serial number: HC104 HC258 Time since overhaul (hours/months): 131.2H/2.4M 1,296.0H/20.0M Life to mid term inspection (hours): 3, ,854.0 Life to overhaul (hours/months): 6,168.8H/52.6M 5,004.0H/35.0M Prop Regulator Part number: Serial Number: R 731 R349 Time since overhaul (hours): 2, ,296.0 Time to overhaul (hours): , Landing Gear LANDING GEAR NOSE LH RH Part number: Serial number: DH58 Cyl: 5511/Piston: CJ220 Life remaining (hours): 11, , , Printed: Wednesday, 27 January 2016 Page 5 of 9

6 7. Wheels and Brakes WHEELS #1 #2 #3 #4 Nose Part number: Serial number: Time since OH (h) 3, , , , , ,168.6 BRAKES #1 #2 #3 #4 Part number: Serial number: Time since last service 3, , , , Aircraft Cargo Interior The cargo compartment is a Class E compartment Printed: Wednesday, 27 January 2016 Page 6 of 9

7 9. Principal Radio and Avionics Equipment ATA Chapter 22 Auto Flight Equipment Quantity Manufacturer Model/Part number Flight Director 2 Collins FD 108 Autopilot 1 Collins AP 103 ATA Chapter 23 Communications Cockpit Voice Recorder 1 Honeywell VHF Transceivers 2 Collins 618M Intercom 2 NAT AA 80 ATA Chapter 25 Equipment Furnishings ELT 1 Artex/Cobham C406 1 ATA Chapter 31 Indicating and Recording Digital Flight Data Recorder 1 Honeywell GQUS ATA Chapter 34 Navigation Compass 2 Sperry C14A ADF 1 Collins 51Z 4 VHF Navigation 2 Collins 51RV1 Marker Beacon 1 Collins 51Y 4 Transponder (Mode S) 1 Garmin GTX 328 Transponder 1 Collins 621A 3 DME 1 Collins 860E 2 Radar Altimeter 1 Collins or Bendix 860F 1 or Radar 1 Bendix King RDS81 EGPWS 1 Honeywell MK VI GPS 1 Bendix King KLN94 Printed: Wednesday, 27 January 2016 Page 7 of 9

8 10. Supplemental Type Certificates/modifications STC/Modification AF0003 AF0010 ARL776 ARL842/FM1092 ARL934 Av Radio ARL Mod 937 FM1124 MB MF MF ntech Mod Bulletin ntech Mod Bulletin ntech Mod Bulletin ntech Mod Bulletin ntech Mod Bulletin , 27 and 28 ntech Mod Bulletin P505 P LSA P LSA P LSA SA1146WE SA1174WE SA3294WE SA3574WE SA SA780WE SA874WE SA88 37 SA909WE Description RDS81 radar installation Starter switch replacement NAT AA 80 installation Cabin depressurisation warning Bendix KLN 94 GPS installation KLN94 GPS installation Blind encoder installation Honeywell MK VI EGPWS installation Garmin GTX 328 transponder installation Installation of C 14A compass system Tail support installation 406 ELT installation Standby AH installation Main cargo door interlock Repairs to LH and RH wing skins and spar EGPWS installation 9G cargo net installation Cargo handling system installation Cargo interior installation Collins AP103/FD108 AFCS Fuel jettison system Increased max zero fuel weight Increased 56,156 lb max take off weight Allison 501 D13 installation Yoke assembly modification Shoulder harness modification Main cargo door installation Collins AP103/FD108 AFCS Printed: Wednesday, 27 January 2016 Page 8 of 9

9 11. Servicing History Check Done at Remaining Check 1 34, (hrs) Check 2 34, Check 3 34, Check 4 34, Check 5 33, Check 6 33, Certificate of Maintenance Review 14 Aug (mth) PHASE 1 Aileron O/H. (LH) 26, ,086.8 (hrs) PHASE 1 Aileron O/H. (RH) 26, ,086.8 PHASE 2 Rudder Mid Term. 33, ,210.9 PHASE 3 Elevator Mid Term. (LH) 33, ,210.9 PHASE 3 Elevator Mid Term. (RH) 33, ,210.9 PHASE 4 Aileron Mid Term. (LH) 33, ,210.9 PHASE 4 Aileron Mid Term. (RH) 33, ,210.9 PHASE 5 Wing Flap O/H. (LH) 27, ,173.2 PHASE 6 Wing Flap O/H. (RH) 27, ,173.2 PHASE 7 Rudder Pedals O/H. 27, ,285.3 PHASE 8 Undercarriage O/H. (LH) 27, ,285.3 PHASE 8 Undercarriage O/H. (RH) 27, ,285.3 PHASE 9 Undercarriage O/H. (Nose) 32, ,544.0 PHASE 10 Entrance Door 32, ,544.0 PHASE 11 Nacelle Landing Gear Doors. 26, ,086.8 PHASE 12 Rudder & Vertical Stabilizer. 27, ,285.3 PHASE 13 Horizontal Stabilizer & Elevators. 26, ,086.8 PHASE 14 Wing. (RH) 26, ,086.8 PHASE 15 Wing. (LH) 26, ,086.8 PHASE 16 Fuselage. 27, ,173.2 PHASE 17 Fuselage Stringers (Upper) 27, ,173.2 PHASE 17 Fuselage Stringers (Lower) 27, ,285.3 CD14000 Cargo Door O/H. 33, ,314.6 Printed: Wednesday, 27 January 2016 Page 9 of 9

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