Atch_8a-c_-_Aircraft_81 _82 _83_Sheets.xlsx

XLSX spreadsheet 207 KB Posted Apr 25, 2016

Attached to: FY17 Charter Airlift Services in Support of the Civil Reserve Air Fleet (CRAF)
Solicitation number: HTC711-16-R-C001
Issued by: Department of Defense United States Transportation Command

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Atch 8a-c - Aircraft 81/82/83 Sheets

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File	Type	Posted
01_May_18_Final_FY18_Uniform_Rates_and_Rules.pdf	PDF	Apr 18, 2018
21_July_2017_Final_FY18_Uniform_Rates_and_Rules_for_International_Service.pdf	PDF	Jul 21, 2017
HTC711-16-R-C001-0006.pdf	PDF	Jun 22, 2017
Final_FY18_-_FY22_Ratemaking_Memorandum_of_Understanding.pdf	PDF	May 5, 2017
FY18_-_FY22_Final_MOU_Letter.pdf	PDF	May 5, 2017
25_April_Comments_-_Combined.pdf	PDF	May 5, 2017
FY18_Uniform_Rates_and_Rules.pdf	PDF	Apr 27, 2017
FY18_-_FY22_MOU_Carrier_Letter_V2.pdf	PDF	Apr 14, 2017
Proposed_FY18_-_FY22_MOU_for_CRAF_Ratemaking_for_International_Service_V2.docx	DOCX document	Apr 14, 2017
HTC711-16-R-C001-0005.pdf	PDF	Mar 31, 2017
FY18_-_FY22_MOU_Carrier_Comments.pdf	PDF	Dec 6, 2016
Comments_to_Proposed_FY18_-_FY22_MOU.pdf	PDF	Dec 6, 2016
FY18_-_FY22_MOU_Carrier_Letter.pdf	PDF	Oct 18, 2016
Proposed_FY18_-_FY22_MOU_for_CRAF_Ratemaking_for_International_Service.pdf	PDF	Oct 18, 2016
FY17_Amended_Uniform_Final_Rates_and_Rules_for_International_Service.pdf	PDF	Aug 30, 2016
HTC711-16-R-C001-0004.pdf	PDF	Aug 10, 2016
HTC711-16-R-C001-0003.pdf	PDF	Aug 1, 2016
FY17_Uniform_Final_Rates_and_Rules_for_International_Service.pdf	PDF	Jul 20, 2016
HTC711-16-R-C001-0002.pdf	PDF	Jul 8, 2016
HTC711-16-R-C001-0001.pdf	PDF	May 27, 2016
FY17-18_Q A_(26_May_16)_redacted_Spreadsheet.xls	XLS spreadsheet	May 26, 2016
FY17-18_Q A_(26_Apr_16)_Redacted_Spreadsheet.xls	XLS spreadsheet	Apr 26, 2016
1._HTC711-16-R-C001.pdf	PDF	Apr 26, 2016
FY17-18_Q A_(25_Apr_16)_Redacted_Spreadsheet.xls	XLS spreadsheet	Apr 25, 2016
Atch_2_-_DD_Form_254.pdf	PDF	Apr 25, 2016
Atch_3_-_iRAPT_and_Ferry_Declaration.pdf	PDF	Apr 25, 2016
Atch_13_-_Form_166A.pdf	PDF	Apr 25, 2016
Atch_12_-_Award_Fee_Plan.pdf	PDF	Apr 25, 2016
Atch_5a_-_WD_2009-0027_rev_10.pdf	PDF	Apr 25, 2016
1._FY17_CRAF_Solicitation.pdf	PDF	Apr 25, 2016
Atch_7_-_Indemnification_request.pdf	PDF	Apr 25, 2016
Atch_14_-_SB_Subcontract_Temp_.pdf	PDF	Apr 25, 2016
Atch_10_-_GFE.pdf	PDF	Apr 25, 2016
Atch_1_-_FY17_PWS.pdf	PDF	Apr 25, 2016
Atch_5_-_WD_1996-0460_rev_22.pdf	PDF	Apr 25, 2016
Atch_11_-_MOU_template_-_FY13_-_17.pdf	PDF	Apr 25, 2016
Atch_8_-_Instructions__Aircraft_Revalidation.pdf	PDF	Apr 25, 2016
Atch_4_-_Contracted_Ground_Ops.pdf	PDF	Apr 25, 2016
Atch_9_-_FPA.pdf	PDF	Apr 25, 2016
Atch_9a_-_Kerosene_Waiver.pdf	PDF	Apr 25, 2016
Atch_6_-_Statement_of_Intent-AMC_Form_207.pdf	PDF	Apr 25, 2016
22_April_2016_Proposed_FY17_Uniform_Rate_and_Rules_for_International_Service.pdf	PDF	Apr 22, 2016
FY17-18_Q A_(Redacted)_Spreadsheet.xls	XLS spreadsheet	Apr 5, 2016
Presolicitation_Slides_(FBO).pptx	PPTX presentation	Mar 2, 2016
J A_Signed_Redacted.pdf	PDF	Feb 25, 2016
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Atch_8a-c_-_Aircraft_81 _82 _83_Sheets.xlsx	XLSX spreadsheet	Feb 16, 2016
Atch_5_-_WD_1996-0460_Rv_21.pdf	PDF	Feb 16, 2016
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Revalidation

CRAF AIRCRAFT REVALIDATION SHEET DATE (MM/DD/YY)

CARRIER AIRCRAFT MODEL AIRCRAFT CONFIGURATION

NUMBER IN INVENTORY NUMBER OVERWATER CAPABLE ENGINE TYPE NAVIGATION EQUIPMENT

THIS SHEET IS ONLY USED TO REVALIDATE AIRCRAFT TAIL NUMBERS THAT WERE SUCESSFULLY SUBMITTED TO THE PREVIOUS SOLICITATION (NEW AIRCRAFT OF IDENTICAL PERFORMANCE CAPABILITY AND EQUIPAGE MAY ALSO BE LISTED)
	Tail Number		Tail Number		Tail Number		Tail Number
1		31		61		91
2		32		62		92
3		33		63		93
4		34		64		94
5		35		65		95
6		36		66		96
7		37		67		97
8		38		68		98
9		39		69		99
10		40		70		100
11		41		71		101
12		42		72		102
13		43		73		103
14		44		74		104
15		45		75		105
16		46		76		106
17		47		77		107
18		48		78		108
19		49		79		109
20		50		80		110
21		51		81		111
22		52		82		112
23		53		83		113
24		54		84		114
25		55		85		115
26		56		86		116
27		57		87		117
28		58		88		118
29		59		89		119
30		60		90		120
CRAF Aircraft Revalidation Data Sheet 81, 20150401

Solicitation: HTC711-16-R-C001

Attachment 8c 01 Apr 15

Basic, Front

CRAF AIRCRAFT BASIC DATA SHEET DATE (MM/DD/YY)

CARRIER	AIRCRAFT MODEL	AIRCRAFT CONFIGURATION		0.0
				LIST EACH AIRCRAFT BY TAIL NUMBER ON THE BACK SIDE OF THIS FORM
NUMBER IN INVENTORY	NUMBER OVERWATER CAPABLE		ENGINE TYPE		NAVIGATION EQUIPMENT

DESIGN AND OPERATIONAL DATA			AIRCRAFT CONFIGURATION
			CARGO	PASSENGER
		A	B	C
1	MAXIMUM TAKEOFF GROSS WEIGHT (LBS)
2	MAXIMUM LANDING GROSS WEIGHT (LBS)
3	MAXIMUM ZERO FUEL WEIGHT (LBS)
4	OPERATING EMPTY WEIGHT (LBS)
5	STRUCTURAL WEIGHT LIMIT (LBS) (Automatically calculated)		B3 - B4	C3 - C4
			0.0	0.0
6	MAXIMUM LANDING PAYLOAD (LBS) (Automatically calculated)		B2 - B4 - A11	C2 - C4 - A11
			0.0	0.0
7	WEIGHT LIMITED PAYLOAD (LBS) (Automatically calculated)		SMALLER OF B5 AND B6	SMALLER OF C5 AND C6
			0.0	0.0
8	NUMBER OF 463L PALLETS/PLACEMENT (CENTERLINE/OFFSET/EITHER)
9	SEATS - COMPANY STANDARD (Enter total; Do not separate by class)
10	BELLY BULK AREA (CU FT)
11	USEABLE FUEL CAPACITY (LBS)	DESTINATION LANDING FUEL (LBS)	CRUISE SPEED	INITIAL CRUISE ALTITUDE

WIDE-BODY AIRCRAFT LOWER LOBE
NUMBERS OF CONTAINERS / TYPES			/	/
TARE WEIGHT PER CONTAINER (LBS)
NUMBER OF 463L PALLETS
COMMUNICATIONS EQUIPMENT
TYPE	NUMBER ON BOARD	MAKE
UHF
VHF
HF
CRAF Aircraft Basic Data Sheet 82, 20150401

Basic, Back

AIRSPACE OPERATIONS CAPABILITY	DATE:	12/31/99
List tail numbers of type aircraft identified on the front which are committed to the CRAF program.
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
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
submitted with this form. For the long-range international section, Mode S-ELS or -EHS, as stated above, is required.
TCAS II (7.1): Traffic Alert and Collision Avoidance System (TCAS II), Version 7.1

			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
		1
		2
		3
		4
		5
		6
		7
		8
		9
		10
		11
		12
		13
		14
		15
		16
		17
		18
		19
		20
		21
		22
		23
		24
		25
		26
		27
		28
		29
		30
		REMARKS:

CRAF Aircraft Basic Data Sheet 82 (Reverse), 20150401

Basic, Back (31+)

AIRSPACE OPERATIONS CAPABILITY	DATE:	12/31/99
List tail numbers of type aircraft identified on the front which are committed to the CRAF program.		0.0
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
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
submitted with this form. For the long-range international section, Mode S-ELS or -EHS, as stated above, is required.
TCAS II (7.1): Traffic Alert and Collision Avoidance System (TCAS II), Version 7.1

			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
		31
		32
		33
		34
		35
		36
		37
		38
		39
		40
		41
		42
		43
		44
		45
		46
		47
		48
		49
		50
		51
		52
		53
		54
		55
		56
		57
		58
		59
		60
		REMARKS:

CRAF Aircraft Basic Data Sheet 82 (Reverse), 20150401

Basic, Back (60+)

AIRSPACE OPERATIONS CAPABILITY	DATE:	12/31/99
List tail numbers of type aircraft identified on the front which are committed to the CRAF program.		0.0
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
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
submitted with this form. For the long-range international section, Mode S-ELS or -EHS, as stated above, is required.
TCAS II (7.1): Traffic Alert and Collision Avoidance System (TCAS II), Version 7.1

			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
		61
		62
		63
		64
		65
		66
		67
		68
		69
		70
		71
		72
		73
		74
		75
		76
		77
		78
		79
		80
		81
		82
		83
		84
		85
		86
		87
		88
		89
		90
		REMARKS:

CRAF Aircraft Basic Data Sheet 82 (Reverse), 20150401

Basic, Back (90+)

AIRSPACE OPERATIONS CAPABILITY	DATE:	12/31/99
List tail numbers of type aircraft identified on the front which are committed to the CRAF program.		0.0
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
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
submitted with this form. For the long-range international section, Mode S-ELS or -EHS, as stated above, is required.
TCAS II (7.1): Traffic Alert and Collision Avoidance System (TCAS II), Version 7.1

			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
		91
		92
		93
		94
		95
		96
		97
		98
		99
		100
		101
		102
		103
		104
		105
		106
		107
		108
		109
		110
		111
		112
		113
		114
		115
		116
		117
		118
		119
		120
		REMARKS:

CRAF Aircraft Basic Data Sheet 82 (Reverse), 20150401

Performance Data Sheet Notes

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.)

(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)".
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.

Performance, B747 VZFW

	CRAF AIRCRAFT PERFORMANCE DATA SHEET								DATE PREPARED*		ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.
									12/31/99
	AIRCRAFT MODEL*					AIRCRAFT CONFIGURATION*		CARRIER*
	0.0					0.0		0.0
	TAKEOFF WEIGHT*		OPERATING WEIGHT*	ENTER AltZFW (LBs)			CRUISE SPEED*	ALTITUDE(S)*	DESTINATION LANDING FUEL*
	0		0				0.0	0.0	0
	* Data is auto-filled from associated HQ AMC Form 82									0.0
	RANGE/PAYLOAD DATA POINTS
	Limit Points		MZFW		MZFW & MTOW		AltZFW & MTOW	MTOW &
MAX FUEL CAP		MAX RANGE -

No Pyld

Range (NM)			0
Payload (lbs)			0	0						0
CFP	Time:	HR	75% of Alt MACL:	0	3500 NM Payload:		ERROR:#DIV/0!	ABS =		0	Kts
Data:		MIN	Payload at CFP Dist:	ERROR:#DIV/0!	Range at 75% ACL:		ERROR:#DIV/0!		ERROR:#DIV/0!		Pax
Distance (NM):			CFP Payload Variance =		ERROR:#DIV/0!	SEAT RESTRICTED AT			ERROR:#DIV/0!		Pax
Payload (lbs):			Approximate Base MV Points:			ERROR:#DIV/0!	w/ Range Bonus:			ERROR:#DIV/0!

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	3500
0	0	500000	3500
0	7000

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

Range/Payload Graph (B-747 Variable ZFW)

Plot Line	0	0	0	0	75% of Max ACL
0	7000	0	0	3,500 NM Marker	3500	3500	0	500000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

PAYLOAD (lbs)

Performance, B747, MD11, etc.

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.

12/31/99

AIRCRAFT MODEL*

AIRCRAFT CONFIGURATION*

CARRIER*

0.0

TAKEOFF WEIGHT*

OPERATING WEIGHT*

CRUISE SPEED*

ALTITUDE(S)*

DESTINATION LANDING FUEL*

0.0

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

0.0

RANGE/PAYLOAD DATA POINTS

Limit Points

MZFW

MZFW & MTOW

MTOW & MAX FUEL CAP

MAX RANGE - No Pyld

Range (NM)

Payload (lbs)

CFP

Time:

75% of Max ACL:

3500 NM Payload:

ERROR:#DIV/0!

ABS =

Kts

Data:

MIN

Payload at CFP Dist:

ERROR:#DIV/0!

Range at 75% ACL:

ERROR:#DIV/0!

Pax

Distance (NM):

CFP Payload Variance =

ERROR:#DIV/0!

SEAT RESTRICTED AT

ERROR:#DIV/0!

Pax

Payload (lbs):

Approximate Base MV Points:

ERROR:#DIV/0!

w/ Range Bonus:

ERROR:#DIV/0!

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	3500
0	0	500000	3500
0	7000

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

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

Plot Line	0	0	0	0	75% of Max ACL
0	7000	0	0	3,500 NM Marker	3500	3500	0	500000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

Performance, B777, etc.

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.

12/31/99

AIRCRAFT MODEL*

AIRCRAFT CONFIGURATION*

CARRIER*

0.0

TAKEOFF WEIGHT*

OPERATING WEIGHT*

CRUISE SPEED*

ALTITUDE(S)*

DESTINATION LANDING FUEL*

0.0

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

0.0

RANGE/PAYLOAD DATA POINTS

Limit Points

MZFW

MZFW & MTOW

MTOW & MAX FUEL CAP

MAX RANGE - No Pyld

Range (NM)

Payload (lbs)

CFP

Time:

75% of Max ACL:

3500 NM Payload:

ERROR:#DIV/0!

ABS =

Kts

Data:

MIN

Payload at CFP Dist:

ERROR:#DIV/0!

Range at 75% ACL:

ERROR:#DIV/0!

Pax

Distance (NM):

CFP Payload Variance =

ERROR:#DIV/0!

SEAT RESTRICTED AT

ERROR:#DIV/0!

Pax

Payload (lbs):

Approximate Base MV Points:

ERROR:#DIV/0!

w/ Range Bonus:

ERROR:#DIV/0!

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	3500
0	0	500000	3500
0	7000

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

Range/Payload Graph (B-777 and similar)

Plot Line	0	0	0	0	75% of Max ACL
0	7000	0	0	3,500 NM Marker	3500	3500	0	500000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

Performance, B767, etc.

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.

12/31/99

AIRCRAFT MODEL*

AIRCRAFT CONFIGURATION*

CARRIER*

0.0

TAKEOFF WEIGHT*

OPERATING WEIGHT*

CRUISE SPEED*

ALTITUDE(S)*

DESTINATION LANDING FUEL*

0.0

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

0.0

RANGE/PAYLOAD DATA POINTS

Limit Points

MZFW

MZFW & MTOW

MTOW & MAX FUEL CAP

MAX RANGE - No Pyld

Range (NM)

Payload (lbs)

CFP

Time:

75% of Max ACL:

3500 NM Payload:

ERROR:#DIV/0!

ABS =

Kts

Data:

MIN

Payload at CFP Dist:

ERROR:#DIV/0!

Range at 75% ACL:

ERROR:#DIV/0!

Pax

Distance (NM):

CFP Payload Variance =

ERROR:#DIV/0!

SEAT RESTRICTED AT

ERROR:#DIV/0!

Pax

Payload (lbs):

Approximate Base MV Points:

ERROR:#DIV/0!

w/ Range Bonus:

ERROR:#DIV/0!

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	3500
0	0	500000	3500
0	7000

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

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

Plot Line	0	0	0	0	75% of Max ACL
0	7000	0	0	3,500 NM Marker	3500	3500	0	500000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

Performance, S-R and Domestic

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.

12/31/99

AIRCRAFT MODEL*

AIRCRAFT CONFIGURATION*

CARRIER*

0.0

TAKEOFF WEIGHT*

OPERATING WEIGHT*

CRUISE SPEED*

ALTITUDE(S)*

DESTINATION LANDING FUEL*

0.0

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

0.0

RANGE/PAYLOAD DATA POINTS

Limit Points

MZFW

MZFW & MTOW

MTOW & MAX FUEL CAP

MAX RANGE - No Pyld

Range (NM)

Payload (lbs)

CFP

Time:

75% of Max ACL:

1500 NM Payload:

ERROR:#DIV/0!

ABS =

Kts

Data:

MIN

Payload at CFP Dist:

ERROR:#DIV/0!

Range at 75% ACL:

ERROR:#DIV/0!

Pax

Distance (NM):

CFP Payload Variance =

ERROR:#DIV/0!

SEAT RESTRICTED AT

ERROR:#DIV/0!

Pax

Payload (lbs):

Approximate Base MV Points:

ERROR:#DIV/0!

w/ Range Bonus:

N/A

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	1500
0	0	55000	1500
0	3500

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

Range/Payload Graph (Short-Range and Domestic)

Plot Line	0	0	0	0	75% of Max ACL
0	3500	0	0	1,500 NM Marker	1500	1500	0	55000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

Performance, S-R High Capacity

CRAF AIRCRAFT PERFORMANCE DATA SHEET

DATE PREPARED*

ALL BLOCKS HIGHLIGHTED IN THIS COLOR REQUIRE DATA ENTRY.

12/31/99

AIRCRAFT MODEL*

AIRCRAFT CONFIGURATION*

CARRIER*

0.0

TAKEOFF WEIGHT*

OPERATING WEIGHT*

CRUISE SPEED*

ALTITUDE(S)*

DESTINATION LANDING FUEL*

0.0

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

0.0

RANGE/PAYLOAD DATA POINTS

Limit Points

MZFW

MZFW & MTOW

MTOW & MAX FUEL CAP

MAX RANGE - No Pyld

Range (NM)

Payload (lbs)

CFP

Time:

75% of Max ACL:

1500 NM Payload:

ERROR:#DIV/0!

ABS =

Kts

Data:

MIN

Payload at CFP Dist:

ERROR:#DIV/0!

Range at 75% ACL:

ERROR:#DIV/0!

Pax

Distance (NM):

CFP Payload Variance =

ERROR:#DIV/0!

SEAT RESTRICTED AT

ERROR:#DIV/0!

Pax

Payload (lbs):

Approximate Base MV Points:

ERROR:#DIV/0!

w/ Range Bonus:

N/A

CRAF Aircraft Performance Data Sheet 83, 20150401

75% of Max ACL	range	0	1500
0	0	120000	1500
0	7000

AIRCRAFT MODEL			0
AIRCRAFT CONFIGURATION			0
CARRIER			0
TAKEOFF WEIGHT			0			0
OPERATING WEIGHT			0			0
CRUISE SPEED			0
INITIAL ALTITUDE			0
RESERVE FUEL			0
		Useable Fuel Capacity			0
		Weight Limited Payload			0		0
MTOW & Max Fuel Cap Payload			0			0
	Seats - Company Standard			0

01 Apr 15

Range/Payload Graph (Short-Range High Capacity)

Plot Line	0	0	0	0	75% of Max ACL
0	7000	0	0	1,500 NM Marker	1500	1500	0	120000	STILL AIR RANGE (Stage Length)--Nautical Miles (NM)

File details come from the government source that posted it. Updated Nov 14, 2017.