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Chapter 6<br />
Cost<br />
Costs are estimated using statistical models based on historical aircraft price and maintenance cost<br />
data, with appropriate factors to account for technology impact and inflation. The aircraft flyaway<br />
cost (CAC, in $) consists of airframe, mission equipment package (MEP), and flight-control-electronics<br />
(FCE) costs. The direct operating cost plus interest (DOC+I, in cents per available seat mile (ASM))<br />
is the sum of maintenance cost (Cmaint, in $ per flight hour), flight crew salary and expenses, fuel and<br />
oil cost, depreciation, insurance cost, and finance cost. Inflation factors can be input, or internal factors<br />
used. Table 6-1 gives the internal inflation factors for DoD (ref. 1) and consumer price index (CPI,<br />
ref. 2). For years beyond the data in the table, optionally the inflation factor is extrapolated based on the<br />
last yearly increase.<br />
6–1 CTM Rotorcraft Cost Model<br />
The CTM rotorcraft cost model (refs. 3–5) gives an estimate of aircraft flyaway cost and direct<br />
operating cost plus interest. The basic statistical relations for airframe purchase price and maintenance<br />
cost per hour are:<br />
cAF = 739.66 KETKENKLGKR W 1.0619<br />
AF (P/WAF ) 0.5887 N 0.1465<br />
blade + ccomp<br />
cmaint =0.49885 W 0.3746<br />
E P 0.4635<br />
with WAF = WE −WMEP−WFCE. The term ccomp = LWcomp accounts for additional costs for composite<br />
construction; Wcomp is the composite structure weight, obtained as an input fraction of the component<br />
weight, with separate fractions for body, tail, pylon, and wing weight. The configuration factors are:<br />
KET = 1.0 for turbine aircraft 0.557 for piston aircraft<br />
KEN = 1.0 for multi-engine aircraft 0.736 for single-engine aircraft<br />
KLG = 1.0 for retractable landing gear 0.884 for fixed landing gear<br />
KR = 1.0 for single main rotor 1.057 for twin main rotors, 1.117 for four main rotors<br />
The MEP and FCE costs are obtained from input cost-per-weight factors: CMEP = rMEPWMEP and<br />
CFCE = rFCEWFCE. These cost equations are based on 1994 dollars and current technology levels.<br />
Including an inflation factor Fi and technology factors χ gives the unit flyaway cost CAC and maintenance<br />
cost per flight hour Cmaint:<br />
CAC = Fi (χAF cAF + CMEP + CFCE)<br />
Cmaint = Fi χmaintcmaint<br />
The statistical equation for cAF predicts the price of 123 out of 128 rotorcraft within 20% (figs. 6-1 and 6-<br />
2). These equations also serve to estimate turboprop airliner flyaway costs by setting Nrotor = Nblade =1