Atch_8a_and_b_-_Aircraft_Basic_and_Performance_Data_Sheets.pdf

SOLICITATION: HTC711-14-R-C002

CRAF Aircraft Basic Data Sheet 82, 20140301

C

NUMBER OVERWATER CAPABLE ENGINE TYPE NAVIGATION EQUIPMENT

AIRCRAFT CONFIGURATION

CRAF AIRCRAFT BASIC DATA SHEET

DATE (MM/DD/YY)

LIST EACH AIRCRAFT BY TAIL NUMBER ON

THE BACK SIDE OF THIS FORM

AIRCRAFT MODELCARRIER

SMALLER OF C5 AND C6

MAXIMUM TAKEOFF GROSS WEIGHT (LBS)

MAXIMUM ZERO FUEL WEIGHT (LBS)

C3 - C4

OPERATING EMPTY WEIGHT (LBS)

B2 - B4 - A11

B3 - B4

TARE WEIGHT PER CONTAINER (LBS)

NUMBER OF 463L PALLETS

INITIAL CRUISE ALTITUDE

UHF

HF

CRUISE SPEED

TYPE

VHF

WIDE-BODY AIRCRAFT LOWER LOBE

USEABLE FUEL CAPACITY (LBS)

NUMBER ON BOARD MAKE

COMMUNICATIONS EQUIPMENT

C2 - C4 - A11

AIRCRAFT CONFIGURATION

CARGO PASSENGER

NUMBER IN INVENTORY

MAXIMUM LANDING GROSS WEIGHT (LBS)

DESIGN AND OPERATIONAL DATA

A B

NUMBERS OF CONTAINERS / TYPES

SMALLER OF B5 AND B6

SEATS - COMPANY STANDARD (Enter total; Do not separate by class)

BELLY BULK AREA (CU FT)

DESTINATION LANDING FUEL (LBS)

NUMBER OF 463L PALLETS/PLACEMENT

(CENTERLINE/OFFSET/EITHER)

STRUCTURAL WEIGHT LIMIT (LBS) (Automatically calculated)

MAXIMUM LANDING PAYLOAD (LBS) (Automatically calculated)

WEIGHT LIMITED PAYLOAD (LBS) (Automatically calculated)

Attachment 8a 1 Mar 2014

DATE: 01/00/00

Mode S: Much of Eurocontrol (EC) airspace now requires at least Mode S-ELS. Additionally, for Mode S-EHS capable aircraft, as defined by EC specifications, EHS is also required. If your aircraft are non-Mode S-EHS capable, appropriate exemptions must be

Tail Number B-747 Nose Loader

RVSM RNP-5 RNP-10 8.33 MHz FM Immune Mode S

(ELS/EHS)

TCAS II (7.1)

Example: N123X X X X 6 Hrs X X EHS X

CRAF Aircraft Basic Data Sheet 82 (Reverse), 20140301

List tail numbers of type aircraft identified on the front which are committed to the CRAF program.

AIRSPACE OPERATIONS CAPABILITY

submitted with this form. For the long-range international section, Mode S-ELS or -EHS, as stated above, is required.

REMARKS:

Based on the guidance listed below, enter an "X" in the appropriate columns. In the RNP-10 column, instead of an "X", write in the number of hours the capability can be maintained without a ground station update. For the Mode S column, enter either "ELS" or "EHS".

B-747 Nose Loader: An aircraft with the ability to load cargo through the nose.

RVSM: Reduced Vertical Separation Minimums airspace RNP-5 (BRNAV): European Airspace requirement to be within 5 miles of course 95% of the time RNP-10: Pacific Airspace requirement to be within 10 miles of course 95% of the time

8.33 MHz: Equipped with 8.33 MHz radios required for operating in European airspace FM Immune: European requirement for navigation systems to be immune from FM interference

TCAS II (7.1): Traffic Alert and Collision Avoidance System (TCAS II), Version 7.1

Attachment 8a

(1) Maximum Zero Fuel Weight (MZFW): The range for this data point is automatically set to zero (0) nautical miles. The payload is automatically filled from Form 82 data and corresponds to the Weight Limited Payload calculated on line 7 of the Form 82, meaning that the aircraft is loaded with the maximum payload (structural or landing limited) and no fuel.

(2) MZFW & Maximum Take Off Weight (MTOW): This data point corresponds to the point where the aircraft is loaded with the maximum payload (structural or landing limited) and enough fuel to cause the aircraft to reach its MTOW. The payload data will be automatically filled, and the form will require entry of the appropriate range data. From this range data point forward, cargo will have to be displaced by fuel in order for the aircraft to fly further.

(3) MTOW and Maximum Fuel Capacity: This data point corresponds to the point where the aircraft is at its MTOW and has reached its maximum fuel capacity.

Payload weight has been reduced to allow for the increase in fuel weight. A good starting point for calculating the payload is MTOW minus OWE (Operating Weight- Empty) minus Useable Fuel Capacity. Both the appropriate range and payload data require entry.

(4) Maximum Range with no Payload (Maximum Ferry Range): This data point corresponds to the maximum range the aircraft can fly carrying no payload. The payload data is set at zero (0) pounds, and the form will require entry of the appropriate range data.

(5) B-747 VZFW ONLY: Alternate Zero Fuel Weight (AltZFW) & MTOW: This data point will be positioned between points (2) and (3) above and will correspond to the point where the aircraft is at its MTOW and has reached the maximum payload permitted by its lower MZFW. This calculation requires entry of an additional field on the Performance Data Sheet entitled "Enter AltZFW (lbs)".

Range/Payload Data Points. The Range/Payload Graph is automatically plotted based on four specified data points (five for the B-747 VZFW), which are defined below.

When determining the range data points, you may use manufacturer’s data or an iterative flight planning process; however, the resulting graph will be validated through comparison with the payload on the associated 1500/3500 NM CFP (Ref Instructions, Para. 5.). We will accept a variance of less than 1.75% between the CFP payload and the plotted payload at the same range. (Note: on the CRAF Aircraft Performance Data Sheet, you will be able to fill only the tan shaded fields. All other fields are automatically filled from data pulled from the CRAF Aircraft Basic Data Sheet or computed on the Performance Data Sheet.)

CRAF Aircraft Performance Data Sheet Tab Selection. For aircraft types not listed, select the tab with payload and range ordinates that provide the best presentation of the aircraft's capabilities. If the performance capabilities of short-range aircraft do not fall within the ordinate parameters on the "S-R and Domestic" tab, an "S-R High Capacity" tab is provided.

0 0 0

CFP HR 0 0 Kts

Data: MIN #DIV/0! Pax

Pax

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

01/00/00

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

* Data is auto-filled from associated HQ AMC Form 82

TAKEOFF WEIGHT* OPERATING WEIGHT*

ENTER AltZFW

(LBs)

CRUISE SPEED* ALTITUDE(S)* DESTINATION LANDING FUEL*

0 0 0

Approximate Base MV Points: w/ Range Bonus: #DIV/0!

#DIV/0!

Limit Points MZFW MZFW & MTOW AltZFW & MTOW MTOW &

MAX FUEL CAP

MAX RANGE -

No Pyld

75% of Alt MACL:

Payload at CFP Dist:

Range (NM)

Payload (lbs)

3500 NM Payload: ABS =#DIV/0!

Range at 75% ACL:

Payload (lbs): #DIV/0!

#DIV/0!

Distance (NM): CFP Payload Variance =

#DIV/0!

#DIV/0!SEAT RESTRICTED AT

RANGE/PAYLOAD DATA POINTS

Time:

250,000

265,000

280,000

295,000

310,000

Range/Payload Graph (B-747 Variable ZFW)

CRAF Aircraft Performance Data Sheet 83, 20140301

55,000

70,000

85,000

100,000

115,000

130,000

145,000

160,000

175,000

190,000

205,000

220,000

235,000

0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

Attachment 8b

0 0 0

CFP HR 0 #DIV/0! ABS = 0 Kts

Data: MIN #DIV/0! #DIV/0! Pax

#DIV/0! #DIV/0! Pax

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

01/00/00

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

0 0 0

TAKEOFF WEIGHT* OPERATING WEIGHT* CRUISE SPEED* ALTITUDE(S)* DESTINATION LANDING FUEL*

* Data is auto-filled from associated HQ AMC Form 82

RANGE/PAYLOAD DATA POINTS

Limit Points MZFW MZFW & MTOW MTOW & MAX FUEL CAP MAX RANGE - No Pyld

#DIV/0!

Range (NM) Payload (lbs)

Time:

75% of Max ACL: 3500 NM Payload:

Payload at CFP Dist: Range at 75% ACL:

Payload (lbs): Approximate Base MV Points: #DIV/0! w/ Range Bonus:

#DIV/0!

Distance (NM): CFP Payload Variance = SEAT RESTRICTED AT

235,000

250,000

265,000

280,000

295,000

310,000

Range/Payload Graph (B-747, MD-11, and similar)

CRAF Aircraft Performance Data Sheet 83, 20140301

55,000

70,000

85,000

100,000

115,000

130,000

145,000

160,000

175,000

190,000

205,000

220,000

0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

1 Mar 2012

0 0 0

CFP HR 0 #DIV/0! ABS = 0 Kts

Data: MIN #DIV/0! #DIV/0! Pax

#DIV/0! #DIV/0! Pax #DIV/0!Payload (lbs):

3500 NM Payload:

Payload at CFP Dist: Range at 75% ACL:

75% of Max ACL:

Approximate Base MV Points: #DIV/0! w/ Range Bonus:

Distance (NM): CFP Payload Variance =

#DIV/0!

Time:

SEAT RESTRICTED AT

Range (NM)

Payload (lbs)

0 0

RANGE/PAYLOAD DATA POINTS

Limit Points MZFW MZFW & MTOW MTOW & MAX FUEL CAP MAX RANGE - No Pyld

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

01/00/00

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

* Data is auto-filled from associated HQ AMC Form 82

TAKEOFF WEIGHT* OPERATING WEIGHT* CRUISE SPEED* ALTITUDE(S)* DESTINATION LANDING FUEL*

180,000

190,000

200,000

210,000

220,000

230,000

240,000

Range/Payload Graph (B-777 and similar)

CRAF Aircraft Performance Data Sheet 83, 20140301

30,000

40,000

50,000

60,000

70,000

80,000

90,000

100,000

110,000

120,000

130,000

140,000

150,000

160,000

170,000

180,000

0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

0 0 0

CFP HR 0 #DIV/0! ABS = 0 Kts

Data: MIN #DIV/0! #DIV/0! Pax

#DIV/0! #DIV/0! Pax

Range (NM)

Time:

75% of Max ACL:

RANGE/PAYLOAD DATA POINTS

Limit Points MZFW MTOW & MAX FUEL CAP

Distance (NM):

Payload (lbs)

MZFW & MTOW

3500 NM Payload:

Range at 75% ACL:

TAKEOFF WEIGHT* OPERATING WEIGHT*

0 0

01/00/00

CRUISE SPEED*

CRAF AIRCRAFT PERFORMANCE DATA SHEET

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

* Data is auto-filled from associated HQ AMC Form 82

CFP Payload Variance =

Payload (lbs):

ALTITUDE(S)* DESTINATION LANDING FUEL*

Approximate Base MV Points: #DIV/0! w/ Range Bonus: #DIV/0!

Payload at CFP Dist:

MAX RANGE - No Pyld

SEAT RESTRICTED AT

#DIV/0!

DATE PREPARED*

120,000

130,000

140,000

150,000

160,000

Range/Payload Graph (A-330, B-767, and similar)

CRAF Aircraft Performance Data Sheet 83, 20140301

75% of Max ACL

10,000

20,000

30,000

40,000

50,000

60,000

70,000

80,000

90,000

100,000

110,000

0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

0 0 0

CFP HR 0 #DIV/0! ABS = 0 Kts

Data: MIN #DIV/0! #DIV/0! Pax

#DIV/0! #DIV/0! Pax

Range (NM)

Payload (lbs)

75% of Max ACL:

Time:

1500 NM Payload:

Payload at CFP Dist: Range at 75% ACL:

#DIV/0!

Limit Points MZFW MZFW & MTOW MTOW & MAX FUEL CAP MAX RANGE - No Pyld

N/A

TAKEOFF WEIGHT* OPERATING WEIGHT* CRUISE SPEED* ALTITUDE(S)* DESTINATION LANDING FUEL*

0 0 0

* Data is auto-filled from associated HQ AMC Form 82

RANGE/PAYLOAD DATA POINTS

#DIV/0!

Distance (NM): CFP Payload Variance = SEAT RESTRICTED AT

Payload (lbs): Approximate Base MV Points: w/ Range Bonus:

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

01/00/00

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

40,000

42,500

45,000

47,500

50,000

52,500

55,000

Range/Payload Graph (Short-Range and Domestic)

CRAF Aircraft Performance Data Sheet 83, 20140301

75% of Max ACL

2,500

5,000

7,500

10,000

12,500

15,000

17,500

20,000

22,500

25,000

27,500

30,000

32,500

35,000

37,500

0 250 500 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 3250 3500

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

0 0 0

CFP HR 0 #DIV/0! ABS = 0 Kts

Data: MIN #DIV/0! #DIV/0! Pax

#DIV/0! #DIV/0! Pax

Range (NM)

Payload (lbs)

75% of Max ACL:

Time:

1500 NM Payload:

Payload at CFP Dist: Range at 75% ACL:

#DIV/0!

Limit Points MZFW MZFW & MTOW MTOW & MAX FUEL CAP MAX RANGE - No Pyld

N/A

TAKEOFF WEIGHT* OPERATING WEIGHT* CRUISE SPEED* ALTITUDE(S)* DESTINATION LANDING FUEL*

0 0 0

* Data is auto-filled from associated HQ AMC Form 82

RANGE/PAYLOAD DATA POINTS

#DIV/0!

Distance (NM): CFP Payload Variance = SEAT RESTRICTED AT

Payload (lbs): Approximate Base MV Points: w/ Range Bonus:

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

01/00/00

AIRCRAFT MODEL* AIRCRAFT CONFIGURATION* CARRIER*

90,000

97,500

105,000

112,500

120,000

Range/Payload Graph (Short-Range High Capacity)

CRAF Aircraft Performance Data Sheet 83, 20140301

75% of Max ACL

7,500

15,000

22,500

30,000

37,500

45,000

52,500

60,000

67,500

75,000

82,500

0 250 500 750 1000 1250 1500 1750 2000 2250 2500 2750 3000 3250 3500

P A

Y L

O A

D lb s)

STILL AIR RANGE (Stage Length)--Nautical Miles (NM)