Total Airframe Time Since New : 13,920 Hours Total Airframe Cycles Since New : 16,098 Cycles
ENGINES
Type & Model : Pratt Whitney Canada PW121 Operator TBO : On Condition Left Right
Serial Number : PCE-120256 PCE-121019
Time Since New : 38,574 Hrs. 31,875 Hrs.
Cycles Since New : 48,318 34,895
Time Since Overhaul : NA NA
Cycles Since Overhaul : NA NA
Time Since HSI : 242 Hrs. 1,254 Hrs.
WEIGHT
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.
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
De Havilland DHC-8
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YEAR
1991
LOCATION
United States - MT, North America + Canada
S/N
265
REG
N637AR
TTAF
13,920 Hours
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