This document provides performance specifications for two aircraft variants: EP (shorter range) and LR (longer range). Key specifications listed include maximum takeoff, landing, and zero fuel weights, fuel capacity per tank, oxygen system pressures, and engine temperature limits. The LR variant can carry more fuel and payload over greater distances than the EP variant.

1. 145 - EP
Max. Ramp 46,495 lbs.
Max. Takeoff 46,275 lbs.
Max. Landing 41,226 lbs.
Max. Zero Fuel 38,250 lbs.
Max. Fuel per tank 4,600 lbs.
Unusable per tank 48 lbs.
Loss of Pump +266 lbs.
Pressure Refuel – 7.9 gal.
ITT - Start 8000C
ITT - Continuous 8680C
ITT - Takeoff (5 min.) 9210C
Rated Thrust ISA+15 7,426 lbs.
2 Crew O2 1,100 psi.
3 Crew O2 1,500 psi.
Portable O2 1,200 psi.
Pilot / ACM 190 Flight Kit 20
Flight Att. (-.3) 170 Overnight 30
EP
145 - LR
Max. Ramp 48,722 lbs.
Max. Takeoff 48,501 lbs.
Max. Landing 42,549 lbs.
Max. Zero Fuel 39,462 lbs.
Max. Fuel per tank 5,717 lbs.
Unusable per tank 39 lbs.
Loss of Pump + 365 lbs.
Pressure Refuel – 13.2 gal.
ITT - Start 8000C
ITT - Continuous 9010C
ITT - T/O 1 (5 min.) 9480C
ITT - ALT T/O 1 9170C
Rated Thrust ISA+30 7,426 lbs.
Aft. Baggage 2,646 lbs.
2,000 lbs. Fuel Bags 1,764 lbs.
2,000 lbs. Fuel Elec/Aft 1 Person
Wardrobe Closet 154 lbs.
LR