Atch 8a-c - Aircraft 81 82 83 Sheets.xlsx
XLSX spreadsheet 236 KB Posted
- Solicitation number
- HTC711-24-R-CC01
About this file
This document is a collection of CRAF (Civil Reserve Air Fleet) aircraft revalidation sheets and aircraft performance data sheets. The CRAF Aircraft Revalidation Sheet is used to revalidate aircraft tail numbers that were successfully submitted to a previous solicitation, or to list new aircraft of identical performance capability and equipment. The CRAF Aircraft Basic Data Sheet captures information on the aircraft's design, operational, and airspace operations capabilities.
The CRAF Aircraft Performance Data Sheet provides details on the aircraft's range and payload capabilities, including four or five data points corresponding to the aircraft's maximum zero fuel weight (MZFW), MZFW and maximum takeoff weight (MTOW), MTOW and maximum fuel capacity, and maximum range with no payload. The performance data is automatically calculated based on the information provided in the Basic Data Sheet. This information supports the related federal contract opportunity, Solicitation Number HTC711-24-R-CC01, which is seeking international long-range and short-range passenger and/or cargo airlift services in support of the CRAF program.
View the file
Other files
Show 40 more
50 files listed here. See the rest on GovTribe.
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
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: HTC711-15-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 | 0.0 | 0.0 | |||||||||||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | 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 | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | |||||||||||
| Range (NM) | 0 | ||||||||||||||
| Payload (lbs) | 0 | 0 | 0 | ||||||||||||
| CFP | Time: | HR | 75% of Max ACL: | 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, 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 | 0.0 | 0.0 | |||||||||||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | 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 | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | |||||||||||
| Range (NM) | 0 | ||||||||||||||
| Payload (lbs) | 0 | 0 | 0 | ||||||||||||
| CFP | Time: | HR | 75% of Max ACL: | 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-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 | 0.0 | 0.0 | |||||||||||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | 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 | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | |||||||||||
| Range (NM) | 0 | ||||||||||||||
| Payload (lbs) | 0 | 0 | 0 | ||||||||||||
| CFP | Time: | HR | 75% of Max ACL: | 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 (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 | 0.0 | 0.0 | |||||||||||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | 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 | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | |||||||||||
| Range (NM) | 0 | ||||||||||||||
| Payload (lbs) | 0 | 0 | 0 | ||||||||||||
| CFP | Time: | HR | 75% of Max ACL: | 0 | 1500 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: | 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 | 0.0 | 0.0 | |||||||||||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | 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 | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | |||||||||||
| Range (NM) | 0 | ||||||||||||||
| Payload (lbs) | 0 | 0 | 0 | ||||||||||||
| CFP | Time: | HR | 75% of Max ACL: | 0 | 1500 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: | 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 .