N637AR - 1991 DEHAVILLAND DHC 8 103

1991

DEHAVILLAND

DHC-8-103

265

Used

N637AR

30 Passenger Seat Cabin Configuration Last Painted February 2016 (Touch-Ups) Eligible for Upgrade to 106 Series Optional STC for Air Operable Baggage Door Unpaved Runway Protection (SB-8-53-41) Part 135 STC for 21 or 30 Seat Combi Config Forward Lav and Galley

Total Airframe Time Since New : 13,920 Hours Total Airframe Cycles Since New : 16,098 Cycles

Type & Model :Pratt Whitney Canada PW121 Operator TBO : On Condition Serial Number : PCE-120256 / PCE-121019 Time Since New : 38,574 / 31,875 Hrs. Cycles Since New : 48,318 / 34,895 Time Since HSI : 242 / 1,254 Hrs.

Type & Model : Hamilton Sundstrand 782701-5 Propeller TBO : 10,500 Hrs / 84 Months Prop 1 Serial Number : 2011041274 Prop 1 TSO : Blade 1 3,410 Hrs. Blade 2 9,802 Hrs. Blade 3 3,426 Hrs. Blade 4 3,057 Hrs. Prop 2 Serial Number :2092 Prop 2 TSO : Blade 1 3,044 Hrs. Blade 2 3,779 Hrs. Blade 3 3,329 Hrs. Blade 4 4,592 Hrs.

VHF Comm Rockwell Collins CTL-22C VHF Nav Rockwell Collins VIR-32 Audio Control/PA/PX AVTECH ADF Rockwell Collins CTL-62 DME Rockwell Collins DME-42 Transponder Rockwell Collins TDR-94D Radio Altimeter Sperry RT-300 Horizontal Situation Indicator Sperry RD-550 Vertical Situation Indicator Rockwell Collins TVI-920D EGPWS/TAWS Honeywell MKVIII FMS with Data Loader Universal Avionics UNS-1Lw TCAS/TCAD Rockwell Collins TTR-921 CVR L3/Fairchild A100A FDR Sunstrand Data UFDR ELT Artex C-406N EFIS NA NA GPS Universal Avionics Satellite Tracking System Blue Sky Network ACH1000 Multi-Function Display Honeywell ID-802 Air Data Computer Sperry AZ-810

Installed NVIS Compatible Supplemental Lighting System 16-May-16 Installation of Provisions for Aircraft Survivability Equipment (ASE) including structural & electrical provisions for AN/AAR-47 Missile Warning System & AN/ALE-47 Countermeasures Dispenser System 25-Jan-16 Removed Auxiliary Power Unit (APU), GTCP36-150W, Engine SN P-102 & associated components 7-Jan-16 Installation of Rosen Visor Kit 18-Apr-14 Installed supplemental oxygen bottles in passenger cabin, Revised aircraft weight and balance, Incorporated airplane Flight Manual Supplement into AFM 14-Feb-14 Upgrade of UNS FMS 1M to UNS FMS 1LW 9-Feb-13 Installed cockpit windshield drain system 4-Feb-13 EGPWS configuration data update 2-Feb-13 Installed High Flotation Tires on Nose Landing Gear, MLG High Flotation Tires PCW 14-Feb-11 Installed Wulfsberg Flexcomm II C-5000 Multi-Band Communications System 26-May-10 Installed Second UNS-1M Navigation Management System and GPS Receiver 28-Apr-10 Reconfiguration of 30 Passenger Seat Arrangement 24-Mar-10 Removed B&D Cabin Inflight Information System 23-Mar-10 Installed Honeywell Mark VIII EGPWS (TAWS A) System 23-Mar-10 Conversion from DHC-8 Model 102 Aircraft to Model 103 Aircraft 18-Mar-10 Removed Rockwell Collins AN/ARC-182 Multi-Band Transceiver & Control Unit 15-Jan-10 Installed Allied Signal KHF-950 HF System 8-Dec-09 SB8-53-41 Fuselage Unpaved Runway Protection 4-Nov-09 Removed SafTGlo Floor Path Emergency Lighting System 24-Mar-09 Installed Dual Hawker Lead Acid Batteries 30-Oct-08 Installed Bluesky Satcom System 30-Oct-08 Installed Collins TCAS II System/Mode-S Transponder 30-Oct-08 Installed Artex C-406N MHZ ELT 30-Oct-08 Installed KGP860 and MD-41-Ref STCSA00886WI-D 18-Aug-04 Installed Beta Lockout 1-Apr-02 MODSUMS (AMOC for AD 2000-02-13) 29-Mar-02 Installed Universal Navigation System 12-Feb-98 Installed Overboard Drain Heat System Wiring 23-Aug-91 Installed Global/Wulfsberg Flight Fone VI Radio Telephone System and Cabin Display 15-Aug-91

Maximum Takeoff Weight (lbs) 34,500 Maximum Landing Weight (lbs) 33,900 Maximum Zero Fuel Weight (lbs) 31,300 Operating Empty Weight (lbs) 22,882 Maximum Payload (lbs) 8,400 Fuel Capacity (US gallons) 848 Maximum Cargo Volume (cubic feet) 300 * Source: FleetAnalyzer (as of June 2013), actual may vary.