Sect L Atch 7 - IFARA Data Input Package 25 Sep 09.xlsx

XLSX spreadsheet 553 KB Posted

Attached to
KC-X Tanker Modernization Program Federal contract opportunity
Solicitation number
FA8625-10-R-6600-SpecialNotice
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base

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Section L Attachment 7 - IFARA Data Input Package

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Sect J Atch 24 - Definitions 25 Sept 09.pdf PDF
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Basic Data

Basic Data
The data provided in this workbook shall reflect the System and Product Specification configuration. The baseline configuration has all plumbing and structural modifications required for wing pods, but DOES NOT HAVE PODS INSTALLED FOR PERFORMANCE CALCULATIONS.Offeror's shall enter data for each item in this column
AIRCRAFT NAME:
CONFIGURATION (Cross referenced to other proposal data):
CMARPS File: Aircraft Characteristics Tab: Aircraft/Takeoff/Enroute/Landing...DescriptionUnits
Aircraft TypeEight character aircraft IDText
Takeoff: DistanceDistance traveled during the takeoff maneuver (takeoff roll through acceleration phase) to start climb pointNM
Takeoff: TimeTime duration for the takeoff maneuver throught start climbMIN
Takeoff: FuelFuel consumed during the takeoff maneuverLBS
Takeoff: AGL after takeoffAircraft altitude Above Ground Level (AGL) after takeoff and accelerationFT
Landing: Min. FuelMinimum fuel with which the aircraft must arrive over the landing base (See KC-X IFARA Analysis Plan for definition)100's LBS
Landing: Island Min. FuelMinimum fuel with which the aircraft must arrive over an island/remote base (See KC-X IFARA Analysis Plan for definition)100's LBS
Landing: MRB Min. FuelMinimum fuel an aircraft that missed an air refueling requires overhead the missed refueling base. (See KC-X IFARA Analysis Plan for definition)100's LBS
CMARPS File: Aircraft Characteristics Tab: Weights...
Min. EmptyAircraft minimum weight empty (operating weight). Weight of aircraft configured to fly an air refueling mission less the fuel weight. Includes aircrew weight.LBS
Misc. EquipmentWeight of additional equipment placed on the aircraftLBS
Total FuelTotal Capacity (JP8- 6.8 LBS/GALLON)LBS
Static GrossAircraft maximum static gross weightLBS
Start Engines and Taxi FuelFuel used during start engines, taxi, and auxiliary power unit operations (Assume 20 Minute Taxi Time)LBS
Max. Brake ReleaseMaximum weight at start of takeoff rollLBS
Max. Inflight GrossMaximum inflight gross weightLBS
CMARPS File: Aircraft Characteristics Tab: Aircraft Degrades...
Tanker A/R with BoomSpecific range degrade when a tanker is offloading fuel with the boom extendedPercent
Tanker A/R with DrogueSpecific range degrade when a tanker is offloading fuel with center line hosePercent
Tanker A/R with BoomDrag Index addition from clean aircraft when a tanker is offloading fuel with the boom extendedNone
Tanker A/R with DrogueDrag Index addition from clean aircraft when a tanker is offloading fuel with center line hoseNone
CMARPS File: Aircraft Characteristics Tab: Air Refueling...
Boom Transfer RateTanker offload fuel transfer rate when using a boomLBS / MIN
Drogue Transfer RateTanker offload fuel transfer rate when using a drogueLBS / MIN
Reserve Fuel Calculation Support Data
Min Fuel at LandingThe fuel required in tanks for normal ground taxi operations from touchdown to block-in. Taxi time will be 20 minutes from touchdown to block in and allow for normal engine shutdown.LBS
Approach and Landing FuelThe fuel required to fly from the final approach fix in the approach and landing configuration until clearing the runway.LBS
Tanker Ramp SpaceNote: These Dimensions will be used to calculate the number of tankers that can be based at each of the airfields
Vehicle WingspanWingspanFeet to nearest tenth
Vehicle LengthLengthFeet to nearest tenth
Reliability and Maintainability
Air Refueling Mission Capable Rate (ARMCR)Percentage of time that tanker is capable of performing its air refueling missions. Equal to the minimum of KC-X partial mission capable rates associated with boom and drogue aerial refueling missions (See System Requirements Document for KC-X). Maximum value used for IFARA will be 92%.Percent
Depot/Heavy MaintenanceFor each depot/heavy maintenance activity (operating command does not posess; See AFI 21-101, AIRCRAFT AND EQUIPMENT MAINTENANCE MANAGEMENT):
Depot/Heavy Maintenance Activity IdentificationName of Heavy Maintenance ActivityText
Depot/Heavy Maintenance Activity DescriptionBrief description of the nature of maintenance to be performedText
Depot/Heavy Maintenance Activity DurationEstimated time aircraft will be out of the operating command's posession for this maintenance activityDays
Depot/Heavy Maintenance Activity First EventTime before initial maintenance activity is dueDays
Depot/Heavy Maintenance Activity FrequencyPeriod (days until next activity is due) for heavy maintenance cycles after the initial cycleDays

Aerial Refueling Gross Weight Restrictions If applicable, Identify Air Refueling Gross Weight Restrictions by receiver type (For example, KC-135Rs will not begin air refueling with A-10s at gross weights over 250,000 lbs.) LBS

Basic Data FA-8625-10-R-6600 Section L, Attachment 7

&P

Takeoff Data

Takeoff Data
The offeror shall provide maximum takeoff gross weights for the parameters specified below based on Critical Field Length (CFL) criteria. The CFL is the total length of runway required to accelerate on all engines to critical engine failure speed, experience an engine failure, then continue to takeoff or stop. It is used during takeoff planning together with the climb out data to determine the maximum gross weight for a safe takeoff and climb out. In computing max takeoff gross weight, assume 0 grade, dry runway, no headwind/tail wind, and no obstacle. Maximum takeoff gross weights for specific airfields will be interpolated from the data in this table. Note that the table specifies "Runway Available" not "Runway Length." For IFARA, 300 feet for line up distance will be subtracted from the runway length to determine runway available. Offerors shall not change the format of the table below.
AIRCRAFT NAME:
CONFIGURATION (Cross referenced to other proposal data):
Runway Available (Ft)Pressure Altitude (Ft)Temp (Degrees F)Temp (Degrees C)Maximum Takeoff Gross Weight (Lbs)
6000020-6.7
60000404.4
600006015.6
600008026.7
6000010037.8
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6500020-6.7
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10500500020-6.7
105005000404.4
1050050006015.6
1050050008026.7
10500500010037.8
10500500012048.9
11000020-6.7
110000404.4
1100006015.6
1100008026.7
11000010037.8
11000012048.9
1100050020-6.7
11000500404.4
110005006015.6
110005008026.7
1100050010037.8
1100050012048.9
11000100020-6.7
110001000404.4
1100010006015.6
1100010008026.7
11000100010037.8
11000100012048.9
11000150020-6.7
110001500404.4
1100015006015.6
1100015008026.7
11000150010037.8
11000150012048.9
11000200020-6.7
110002000404.4
1100020006015.6
1100020008026.7
11000200010037.8
11000200012048.9
11000250020-6.7
110002500404.4
1100025006015.6
1100025008026.7
11000250010037.8
11000250012048.9
11000300020-6.7
110003000404.4
1100030006015.6
1100030008026.7
11000300010037.8
11000300012048.9
11000350020-6.7
110003500404.4
1100035006015.6
1100035008026.7
11000350010037.8
11000350012048.9
11000400020-6.7
110004000404.4
1100040006015.6
1100040008026.7
11000400010037.8
11000400012048.9
11000450020-6.7
110004500404.4
1100045006015.6
1100045008026.7
11000450010037.8
11000450012048.9
11000500020-6.7
110005000404.4
1100050006015.6
1100050008026.7
11000500010037.8
11000500012048.9
11500020-6.7
115000404.4
1150006015.6
1150008026.7
11500010037.8
11500012048.9
1150050020-6.7
11500500404.4
115005006015.6
115005008026.7
1150050010037.8
1150050012048.9
11500100020-6.7
115001000404.4
1150010006015.6
1150010008026.7
11500100010037.8
11500100012048.9
11500150020-6.7
115001500404.4
1150015006015.6
1150015008026.7
11500150010037.8
11500150012048.9
11500200020-6.7
115002000404.4
1150020006015.6
1150020008026.7
11500200010037.8
11500200012048.9
11500250020-6.7
115002500404.4
1150025006015.6
1150025008026.7
11500250010037.8
11500250012048.9
11500300020-6.7
115003000404.4
1150030006015.6
1150030008026.7
11500300010037.8
11500300012048.9
11500350020-6.7
115003500404.4
1150035006015.6
1150035008026.7
11500350010037.8
11500350012048.9
11500400020-6.7
115004000404.4
1150040006015.6
1150040008026.7
11500400010037.8
11500400012048.9
11500450020-6.7
115004500404.4
1150045006015.6
1150045008026.7
11500450010037.8
11500450012048.9
11500500020-6.7
115005000404.4
1150050006015.6
1150050008026.7
11500500010037.8
11500500012048.9
12000020-6.7
120000404.4
1200006015.6
1200008026.7
12000010037.8
12000012048.9
1200050020-6.7
12000500404.4
120005006015.6
120005008026.7
1200050010037.8
1200050012048.9
12000100020-6.7
120001000404.4
1200010006015.6
1200010008026.7
12000100010037.8
12000100012048.9
12000150020-6.7
120001500404.4
1200015006015.6
1200015008026.7
12000150010037.8
12000150012048.9
12000200020-6.7
120002000404.4
1200020006015.6
1200020008026.7
12000200010037.8
12000200012048.9
12000250020-6.7
120002500404.4
1200025006015.6
1200025008026.7
12000250010037.8
12000250012048.9
12000300020-6.7
120003000404.4
1200030006015.6
1200030008026.7
12000300010037.8
12000300012048.9
12000350020-6.7
120003500404.4
1200035006015.6
1200035008026.7
12000350010037.8
12000350012048.9
12000400020-6.7
120004000404.4
1200040006015.6
1200040008026.7
12000400010037.8
12000400012048.9
12000450020-6.7
120004500404.4
1200045006015.6
1200045008026.7
12000450010037.8
12000450012048.9
12000500020-6.7
120005000404.4
1200050006015.6
1200050008026.7
12000500010037.8
12000500012048.9
12500020-6.7
125000404.4
1250006015.6
1250008026.7
12500010037.8
12500012048.9
1250050020-6.7
12500500404.4
125005006015.6
125005008026.7
1250050010037.8
1250050012048.9
12500100020-6.7
125001000404.4
1250010006015.6
1250010008026.7
12500100010037.8
12500100012048.9
12500150020-6.7
125001500404.4
1250015006015.6
1250015008026.7
12500150010037.8
12500150012048.9
12500200020-6.7
125002000404.4
1250020006015.6
1250020008026.7
12500200010037.8
12500200012048.9
12500250020-6.7
125002500404.4
1250025006015.6
1250025008026.7
12500250010037.8
12500250012048.9
12500300020-6.7
125003000404.4
1250030006015.6
1250030008026.7
12500300010037.8
12500300012048.9
12500350020-6.7
125003500404.4
1250035006015.6
1250035008026.7
12500350010037.8
12500350012048.9
12500400020-6.7
125004000404.4
1250040006015.6
1250040008026.7
12500400010037.8
12500400012048.9
12500450020-6.7
125004500404.4
1250045006015.6
1250045008026.7
12500450010037.8
12500450012048.9
12500500020-6.7
125005000404.4
1250050006015.6
1250050008026.7
12500500010037.8
12500500012048.9
13000020-6.7
130000404.4
1300006015.6
1300008026.7
13000010037.8
13000012048.9
1300050020-6.7
13000500404.4
130005006015.6
130005008026.7
1300050010037.8
1300050012048.9
13000100020-6.7
130001000404.4
1300010006015.6
1300010008026.7
13000100010037.8
13000100012048.9
13000150020-6.7
130001500404.4
1300015006015.6
1300015008026.7
13000150010037.8
13000150012048.9
13000200020-6.7
130002000404.4
1300020006015.6
1300020008026.7
13000200010037.8
13000200012048.9
13000250020-6.7
130002500404.4
1300025006015.6
1300025008026.7
13000250010037.8
13000250012048.9
13000300020-6.7
130003000404.4
1300030006015.6
1300030008026.7
13000300010037.8
13000300012048.9
13000350020-6.7
130003500404.4
1300035006015.6
1300035008026.7
13000350010037.8
13000350012048.9
13000400020-6.7
130004000404.4
1300040006015.6
1300040008026.7
13000400010037.8
13000400012048.9
13000450020-6.7
130004500404.4
1300045006015.6
1300045008026.7
13000450010037.8
13000450012048.9
13000500020-6.7
130005000404.4
1300050006015.6
1300050008026.7
13000500010037.8
13000500012048.9
13500020-6.7
135000404.4
1350006015.6
1350008026.7
13500010037.8
13500012048.9
1350050020-6.7
13500500404.4
135005006015.6
135005008026.7
1350050010037.8
1350050012048.9
13500100020-6.7
135001000404.4
1350010006015.6
1350010008026.7
13500100010037.8
13500100012048.9
13500150020-6.7
135001500404.4
1350015006015.6
1350015008026.7
13500150010037.8
13500150012048.9
13500200020-6.7
135002000404.4
1350020006015.6
1350020008026.7
13500200010037.8
13500200012048.9
13500250020-6.7
135002500404.4
1350025006015.6
1350025008026.7
13500250010037.8
13500250012048.9
13500300020-6.7
135003000404.4
1350030006015.6
1350030008026.7
13500300010037.8
13500300012048.9
13500350020-6.7
135003500404.4
1350035006015.6
1350035008026.7
13500350010037.8
13500350012048.9
13500400020-6.7
135004000404.4
1350040006015.6
1350040008026.7
13500400010037.8
13500400012048.9
13500450020-6.7
135004500404.4
1350045006015.6
1350045008026.7
13500450010037.8
13500450012048.9
13500500020-6.7
135005000404.4
1350050006015.6
1350050008026.7
13500500010037.8
13500500012048.9
14000020-6.7
140000404.4
1400006015.6
1400008026.7
14000010037.8
14000012048.9
1400050020-6.7
14000500404.4
140005006015.6
140005008026.7
1400050010037.8
1400050012048.9
14000100020-6.7
140001000404.4
1400010006015.6
1400010008026.7
14000100010037.8
14000100012048.9
14000150020-6.7
140001500404.4
1400015006015.6
1400015008026.7
14000150010037.8
14000150012048.9
14000200020-6.7
140002000404.4
1400020006015.6
1400020008026.7
14000200010037.8
14000200012048.9
14000250020-6.7
140002500404.4
1400025006015.6
1400025008026.7
14000250010037.8
14000250012048.9
14000300020-6.7
140003000404.4
1400030006015.6
1400030008026.7
14000300010037.8
14000300012048.9
14000350020-6.7
140003500404.4
1400035006015.6
1400035008026.7
14000350010037.8
14000350012048.9
14000400020-6.7
140004000404.4
1400040006015.6
1400040008026.7
14000400010037.8
14000400012048.9
14000450020-6.7
140004500404.4
1400045006015.6
1400045008026.7
14000450010037.8
14000450012048.9
14000500020-6.7
140005000404.4
1400050006015.6
1400050008026.7
14000500010037.8
14000500012048.9
14500020-6.7
145000404.4
1450006015.6
1450008026.7
14500010037.8
14500012048.9
1450050020-6.7
14500500404.4
145005006015.6
145005008026.7
1450050010037.8
1450050012048.9
14500100020-6.7
145001000404.4
1450010006015.6
1450010008026.7
14500100010037.8
14500100012048.9
14500150020-6.7
145001500404.4
1450015006015.6
1450015008026.7
14500150010037.8
14500150012048.9
14500200020-6.7
145002000404.4
1450020006015.6
1450020008026.7
14500200010037.8
14500200012048.9
14500250020-6.7
145002500404.4
1450025006015.6
1450025008026.7
14500250010037.8
14500250012048.9
14500300020-6.7
145003000404.4
1450030006015.6
1450030008026.7
14500300010037.8
14500300012048.9
14500350020-6.7
145003500404.4
1450035006015.6
1450035008026.7
14500350010037.8
14500350012048.9
14500400020-6.7
145004000404.4
1450040006015.6
1450040008026.7
14500400010037.8
14500400012048.9
14500450020-6.7
145004500404.4
1450045006015.6
1450045008026.7
14500450010037.8
14500450012048.9
14500500020-6.7
145005000404.4
1450050006015.6
1450050008026.7
14500500010037.8
14500500012048.9
15000020-6.7
150000404.4
1500006015.6
1500008026.7
15000010037.8
15000012048.9
1500050020-6.7
15000500404.4
150005006015.6
150005008026.7
1500050010037.8
1500050012048.9
15000100020-6.7
150001000404.4
1500010006015.6
1500010008026.7
15000100010037.8
15000100012048.9
15000150020-6.7
150001500404.4
1500015006015.6
1500015008026.7
15000150010037.8
15000150012048.9
15000200020-6.7
150002000404.4
1500020006015.6
1500020008026.7
15000200010037.8
15000200012048.9
15000250020-6.7
150002500404.4
1500025006015.6
1500025008026.7
15000250010037.8
15000250012048.9
15000300020-6.7
150003000404.4
1500030006015.6
1500030008026.7
15000300010037.8
15000300012048.9
15000350020-6.7
150003500404.4
1500035006015.6
1500035008026.7
15000350010037.8
15000350012048.9
15000400020-6.7
150004000404.4
1500040006015.6
1500040008026.7
15000400010037.8
15000400012048.9
15000450020-6.7
150004500404.4
1500045006015.6
1500045008026.7
15000450010037.8
15000450012048.9
15000500020-6.7
150005000404.4
1500050006015.6
1500050008026.7
15000500010037.8
15000500012048.9

Take Off Data FA-8625-10-R-6600

&P

ACN

ACN
The offeror shall provide the Aircraft Classification Number (ACN) for Max Ramp Weight (Static Gross from Basic Data Tab) and operating weight (Min. Empty from Basic Data Tab) for the two pavement types and four pavement subgrade codes.
AIRCRAFT NAME:
CONFIGURATION (Cross referenced to other proposal data):
ACN
Flexible PavementRigid Pavement
Weight (lbs)High
(A)Medium
(B)Low
(C)Ultra Low
(D)High
(A)Medium
(B)Low
(C)Ultra Low

(D)

Operating Weight:
Maximum Ramp Weight:
Tire Pressure (pounds per square inch)
Center of Gravity (percent)

Aircraft Classification Number FA-8625-10-R-6600

&P

Climb and Cruise

Cruise and Climb (No Pods Installed)
The offeror shall provide the specific range during the cruise segment (NAM per 1000 pounds of fuel) for the aircraft cruise configuration (boom/drogue stowed) at the listed mach numbers, flight levels and gross weights. Offerors shall enter 20 gross weights from operating weight (Min. Empty from Basic Data Tab) to maximum takeoff weight (Max. Brake Release from Basic Data Tab), spaced at equal intervals. Offerors shall also provide the cruise fuel flows (pounds per hour) for the aircraft cruise configuration (boom/drogue stowed) for the conditions of gross weight, true airspeeds, and altitudes listed in the Cruise Fuel Flow Table below. Offerors shall provide the fuel used, distance, and time for the aircraft to climb to the specified flight level from sea level for the 20 gross weights in the Climb Table. Also provide best holding speeds at the requested flight levels for the 20 gross weights in the Holding Table. In the Max Range Cruise (MRC) table, enter the MRC airspeed (KTAS) and initial gross weight (Lbs) for the listed Flight Levels. Offerors shall not change the format of the tables below.
CONTRACTOR PROPRIETARY DATA
AIRCRAFT NAME:
CONFIGURATION (Cross referenced to other proposal data):
SPECIFIC RANGE TABLE (NAUTICAL AIR MILES PER 1000 POUNDS OF FUEL)
ACFT SR 00 15 12 20
# Machs
0.30.350.40.45
# Flt Lvls
SL80100150180200210230250270300350400SL80100150180200210230250270300350400SL80100150180200210230250270300350400SL80100150180200210230250270
# Aircraft Weight (Lbs)Specific Range (NAM/1000 Lbs Fuel)
Operating Weight00.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 200.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 300.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 400.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 500.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 600.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 700.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 800.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 900.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1100.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1200.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1300.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1400.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1500.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1600.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1700.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1800.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Wt 1900.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
Maximum Takeoff Weight00.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.0000.00
# CLIMB TABLE
ACFT CL 00 15 12 20
#Flight LevelFlight LevelFlight Level
SL80100150180200210230250270300350400SL80100150180200210230250270300350400SL80100150180200210230250270300350400
# Aircraft Weight (Lbs)Fuel Burn (Lbs)Distance (NM)Time (Minutes)
Operating Weight00000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 200000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 300000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 400000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 500000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 600000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 700000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 800000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 900000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1000000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1100000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1200000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1300000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1400000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1500000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1600000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1700000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1800000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Wt 1900000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
Maximum Takeoff Weight00000000000000.00.00.00.00.00.00.00.00.00.00.00.00.00.000.000.000.000.000.000.000.000.000.000.000.000.00
# HOLDING TABLE
# Best Holding Speed (KCAS)80100150200250300
Operating Weight000000
Wt 2000000
Wt 3000000
Wt 4000000
Wt 5000000
Wt 6000000
Wt 7000000
Wt 8000000
Wt 9000000
Wt 10000000
Wt 11000000
Wt 12000000
Wt 13000000
Wt 14000000
Wt 15000000
Wt 16000000
Wt 17000000
Wt 18000000
Wt 19000000
Maximum Takeoff Weight000000
# MAX RANGE CRUISE (MRC)

Author: This information goes into the CMARPS Aircraft Characteristics File, "Aircraft HEM/MRC" Table to enable MRC for experimental aircraft. If an experimental aircraft can climb to multiple altitudes at the same gross weight only enter a gross weight for the highest Flight Level.

Flight LevelAirspeed (KTAS)MRC Wt (Lbs)
18000
19000
20000
21000
22000
23000
24000
25000
26000
27000
28000
29000
31000
33000
35000
37000
39000
41000
43000
45000
CRUISE FUEL FLOW TABLE
Altitude (feet above mean sea level)Airspeed (knots true airspeed)Weight (pounds)Burn (Fuel Flow, pounds per hour)
0150Operating Weight
0150Wt 2
0150Wt 3
0150Wt 4
0150Wt 5
0150Wt 6
0150Wt 7
0150Wt 8
0150Wt 9
0150Wt 10
0150Wt 11
0150Wt 12
0150Wt 13
0150Wt 14
0150Wt 15
0150Wt 16
0150Wt 17
0150Wt 18
0150Wt 19
0150Maximum Takeoff Weight
0175Operating Weight
0175Wt 2
0175Wt 3
0175Wt 4
0175Wt 5
0175Wt 6
0175Wt 7
0175Wt 8
0175Wt 9
0175Wt 10
0175Wt 11
0175Wt 12
0175Wt 13
0175Wt 14
0175Wt 15
0175Wt 16
0175Wt 17
0175Wt 18
0175Wt 19
0175Maximum Takeoff Weight
0200Operating Weight
0200Wt 2
0200Wt 3
0200Wt 4
0200Wt 5
0200Wt 6
0200Wt 7
0200Wt 8
0200Wt 9
0200Wt 10
0200Wt 11
0200Wt 12
0200Wt 13
0200Wt 14
0200Wt 15
0200Wt 16
0200Wt 17
0200Wt 18
0200Wt 19
0200Maximum Takeoff Weight
0225Operating Weight
0225Wt 2
0225Wt 3
0225Wt 4
0225Wt 5
0225Wt 6
0225Wt 7
0225Wt 8
0225Wt 9
0225Wt 10
0225Wt 11
0225Wt 12
0225Wt 13
0225Wt 14
0225Wt 15
0225Wt 16
0225Wt 17
0225Wt 18
0225Wt 19
0225Maximum Takeoff Weight
0250Operating Weight
0250Wt 2
0250Wt 3
0250Wt 4
0250Wt 5
0250Wt 6
0250Wt 7
0250Wt 8
0250Wt 9
0250Wt 10
0250Wt 11
0250Wt 12
0250Wt 13
0250Wt 14
0250Wt 15
0250Wt 16
0250Wt 17
0250Wt 18
0250Wt 19
0250Maximum Takeoff Weight
0275Operating Weight
0275Wt 2
0275Wt 3
0275Wt 4
0275Wt 5
0275Wt 6
0275Wt 7
0275Wt 8
0275Wt 9
0275Wt 10
0275Wt 11
0275Wt 12
0275Wt 13
0275Wt 14
0275Wt 15
0275Wt 16
0275Wt 17
0275Wt 18
0275Wt 19
0275Maximum Takeoff Weight
0300Operating Weight
0300Wt 2
0300Wt 3
0300Wt 4
0300Wt 5
0300Wt 6
0300Wt 7
0300Wt 8
0300Wt 9
0300Wt 10
0300Wt 11
0300Wt 12
0300Wt 13
0300Wt 14
0300Wt 15
0300Wt 16
0300Wt 17
0300Wt 18
0300Wt 19
0300Maximum Takeoff Weight
0325Operating Weight
0325Wt 2
0325Wt 3
0325Wt 4
0325Wt 5
0325Wt 6
0325Wt 7
0325Wt 8
0325Wt 9
0325Wt 10
0325Wt 11
0325Wt 12
0325Wt 13
0325Wt 14
0325Wt 15
0325Wt 16
0325Wt 17
0325Wt 18
0325Wt 19
0325Maximum Takeoff Weight
0350Operating Weight
0350Wt 2
0350Wt 3
0350Wt 4
0350Wt 5
0350Wt 6
0350Wt 7
0350Wt 8
0350Wt 9
0350Wt 10
0350Wt 11
0350Wt 12
0350Wt 13
0350Wt 14
0350Wt 15
0350Wt 16
0350Wt 17
0350Wt 18
0350Wt 19
0350Maximum Takeoff Weight
0375Operating Weight
0375Wt 2
0375Wt 3
0375Wt 4
0375Wt 5
0375Wt 6
0375Wt 7
0375Wt 8
0375Wt 9
0375Wt 10
0375Wt 11
0375Wt 12
0375Wt 13
0375Wt 14
0375Wt 15
0375Wt 16
0375Wt 17
0375Wt 18
0375Wt 19
0375Maximum Takeoff Weight
0400Operating Weight
0400Wt 2
0400Wt 3
0400Wt 4
0400Wt 5
0400Wt 6
0400Wt 7
0400Wt 8
0400Wt 9
0400Wt 10
0400Wt 11
0400Wt 12
0400Wt 13
0400Wt 14
0400Wt 15
0400Wt 16
0400Wt 17
0400Wt 18
0400Wt 19
0400Maximum Takeoff Weight
0425Operating Weight
0425Wt 2
0425Wt 3
0425Wt 4
0425Wt 5
0425Wt 6
0425Wt 7
0425Wt 8
0425Wt 9
0425Wt 10
0425Wt 11
0425Wt 12
0425Wt 13
0425Wt 14
0425Wt 15
0425Wt 16
0425Wt 17
0425Wt 18
0425Wt 19
0425Maximum Takeoff Weight
0450Operating Weight
0450Wt 2
0450Wt 3
0450Wt 4
0450Wt 5
0450Wt 6
0450Wt 7
0450Wt 8
0450Wt 9
0450Wt 10
0450Wt 11
0450Wt 12
0450Wt 13
0450Wt 14
0450Wt 15
0450Wt 16
0450Wt 17
0450Wt 18
0450Wt 19
0450Maximum Takeoff Weight
0475Operating Weight
0475Wt 2
0475Wt 3
0475Wt 4
0475Wt 5
0475Wt 6
0475Wt 7
0475Wt 8
0475Wt 9
0475Wt 10
0475Wt 11
0475Wt 12
0475Wt 13
0475Wt 14
0475Wt 15
0475Wt 16
0475Wt 17
0475Wt 18
0475Wt 19
0475Maximum Takeoff Weight
0500Operating Weight
0500Wt 2
0500Wt 3
0500Wt 4
0500Wt 5
0500Wt 6
0500Wt 7
0500Wt 8
0500Wt 9
0500Wt 10
0500Wt 11
0500Wt 12
0500Wt 13
0500Wt 14
0500Wt 15
0500Wt 16
0500Wt 17
0500Wt 18
0500Wt 19
0500Maximum Takeoff Weight
0525Operating Weight
0525Wt 2
0525Wt 3
0525Wt 4
0525Wt 5
0525Wt 6
0525Wt 7
0525Wt 8
0525Wt 9
0525Wt 10
0525Wt 11
0525Wt 12
0525Wt 13
0525Wt 14
0525Wt 15
0525Wt 16
0525Wt 17
0525Wt 18
0525Wt 19
0525Maximum Takeoff Weight
0550Operating Weight
0550Wt 2
0550Wt 3
0550Wt 4
0550Wt 5
0550Wt 6
0550Wt 7
0550Wt 8
0550Wt 9
0550Wt 10
0550Wt 11
0550Wt 12
0550Wt 13
0550Wt 14
0550Wt 15
0550Wt 16
0550Wt 17
0550Wt 18
0550Wt 19
0550Maximum Takeoff Weight
0575Operating Weight
0575Wt 2
0575Wt 3
0575Wt 4
0575Wt 5
0575Wt 6
0575Wt 7
0575Wt 8
0575Wt 9
0575Wt 10
0575Wt 11
0575Wt 12
0575Wt 13
0575Wt 14
0575Wt 15
0575Wt 16
0575Wt 17
0575Wt 18
0575Wt 19
0575Maximum Takeoff Weight
8000150Operating Weight
8000150Wt 2
8000150Wt 3
8000150Wt 4
8000150Wt 5
8000150Wt 6
8000150Wt 7
8000150Wt 8
8000150Wt 9
8000150Wt 10
8000150Wt 11
8000150Wt 12
8000150Wt 13
8000150Wt 14
8000150Wt 15
8000150Wt 16
8000150Wt 17
8000150Wt 18
8000150Wt 19
8000150Maximum Takeoff Weight
8000175Operating Weight
8000175Wt 2
8000175Wt 3
8000175Wt 4
8000175Wt 5
8000175Wt 6
8000175Wt 7
8000175Wt 8
8000175Wt 9
8000175Wt 10
8000175Wt 11
8000175Wt 12
8000175Wt 13
8000175Wt 14
8000175Wt 15
8000175Wt 16
8000175Wt 17
8000175Wt 18
8000175Wt 19
8000175Maximum Takeoff Weight
8000200Operating Weight
8000200Wt 2
8000200Wt 3
8000200Wt 4
8000200Wt 5
8000200Wt 6
8000200Wt 7
8000200Wt 8
8000200Wt 9
8000200Wt 10
8000200Wt 11
8000200Wt 12
8000200Wt 13
8000200Wt 14
8000200Wt 15
8000200Wt 16
8000200Wt 17
8000200Wt 18
8000200Wt 19
8000200Maximum Takeoff Weight
8000225Operating Weight
8000225Wt 2
8000225Wt 3
8000225Wt 4
8000225Wt 5
8000225Wt 6
8000225Wt 7
8000225Wt 8
8000225Wt 9
8000225Wt 10
8000225Wt 11
8000225Wt 12
8000225Wt 13
8000225Wt 14
8000225Wt 15
8000225Wt 16
8000225Wt 17
8000225Wt 18
8000225Wt 19
8000225Maximum Takeoff Weight
8000250Operating Weight
8000250Wt 2
8000250Wt 3
8000250Wt 4
8000250Wt 5
8000250Wt 6
8000250Wt 7
8000250Wt 8
8000250Wt 9
8000250Wt 10
8000250Wt 11
8000250Wt 12
8000250Wt 13
8000250Wt 14
8000250Wt 15
8000250Wt 16
8000250Wt 17
8000250Wt 18
8000250Wt 19
8000250Maximum Takeoff Weight
8000275Operating Weight
8000275Wt 2
8000275Wt 3
8000275Wt 4
8000275Wt 5
8000275Wt 6
8000275Wt 7
8000275Wt 8
8000275Wt 9

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