Sect L Atch 7 - IFARA Data Input Package 24 Feb 10.xlsx

XLSX spreadsheet 555 KB Posted

Attached to
KC-X Tanker Modernization Program Federal contract opportunity
Solicitation number
FA8625-10-R-6600
Issued by
Department of the Air Force Materiel Command

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Sect L Atch 7 - IFARA Data Input Package 24 Feb 10.xlsx

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KC-X RFP Questions and Answers 25 Jun 10.pdf PDF
Sect J Atch 3 - Production SOO 18 Jun 2010.pdf PDF
Sect L Instruction to Offerors 24 Jun 2010.pdf PDF
Sect L Atch 1 - Correlation Matrix 18 Jun 2010.pdf PDF
Sect J Atch 7 - VIQ Matrix 18 Jun 2010.pdf PDF
Sect J Atch 9 - Option Matrix 18 Jun 2010.pdf PDF
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Sect L - Instructions to Offerors 4 May 10.pdf PDF
FA8625-10-R-6600 Amend 0003.pdf PDF
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Sect J Exhibit A - A086 22 Apr 10.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. In the table below, if there is a value outside the aircraft's operating envelope, enter a value of "0" (zero). 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
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10500400012048.9
10500450020-6.7
105004500404.4
1050045006015.6
1050045008026.7
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10500450012048.9
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11000020-6.7
110000404.4
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11500300010037.8
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12000020-6.7
120000404.4
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12000100020-6.7
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12000300020-6.7
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1200030006015.6
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12000300010037.8
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12000350020-6.7
120003500404.4
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1200035008026.7
12000350010037.8
12000350012048.9
12000400020-6.7
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12000400010037.8
12000400012048.9
12000450020-6.7
120004500404.4
1200045006015.6
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12000450010037.8
12000450012048.9
12000500020-6.7
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1200050006015.6
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12000500010037.8
12000500012048.9
12500020-6.7
125000404.4
1250006015.6
1250008026.7
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1250050020-6.7
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125005006015.6
125005008026.7
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12500100020-6.7
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1250010006015.6
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12500150020-6.7
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1250015006015.6
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12500200020-6.7
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12500250020-6.7
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12500250010037.8
12500250012048.9
12500300020-6.7
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1250030006015.6
1250030008026.7
12500300010037.8
12500300012048.9
12500350020-6.7
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12500350010037.8
12500350012048.9
12500400020-6.7
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12500400010037.8
12500400012048.9
12500450020-6.7
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12500450010037.8
12500450012048.9
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13000020-6.7
130000404.4
1300006015.6
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1300050020-6.7
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13000100020-6.7
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1300010006015.6
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13000100010037.8
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13000150020-6.7
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1300015006015.6
1300015008026.7
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13500020-6.7
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13500100020-6.7
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13500200020-6.7
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13500300020-6.7
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13500300010037.8
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13500350020-6.7
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13500400020-6.7
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13500450020-6.7
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14000020-6.7
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14500020-6.7
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15000020-6.7
150000404.4
1500006015.6
1500008026.7
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1500050020-6.7
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15000100010037.8
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1500015008026.7
15000150010037.8
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15000200020-6.7
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15000200010037.8
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15000250020-6.7
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1500025006015.6
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15000300020-6.7
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1500030006015.6
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15000300010037.8
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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. For any of the tables below, if there is a value outside the aircraft's operating envelope, enter a value of "0" (zero). 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)
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

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