Atch8a.xls
XLS spreadsheet 405 KB Posted
- Attached to
- Award Notice Federal contract opportunity
- Solicitation number
- HTC71111RC002
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Attachment 8A
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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, 20110524 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 5&RAttachment 8a 24 May 2011
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): (Data Collection Only) Future Eurocontrol-required system. Expected mandatory for Int'l Long-Range section by 2014. | ||||||||
| Tail Number | B-747 | |||||||
| Nose Loader | RVSM | RNP-5 | RNP-10 | 8.33 MHz | FM Immune | Mode S | ||
| (ELS/EHS) | TCAS II (7.1) |
Data Collection Only
| Example: N123X | X | X | X | 6 Hrs | X | X | ELS | X | |
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| REMARKS: | |||||||||
| CRAF Aircraft Basic Data Sheet (Reverse), 20110524 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 2 of 5&RAttachment 8a 24 May 2011
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 | |||||||
| 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): (Data Collection Only) Future Eurocontrol-required system. Expected mandatory for Int'l Long-Range section by 2014. | ||||||||
| Tail Number | B-747 | |||||||
| Nose Loader | RVSM | RNP-5 | RNP-10 | 8.33 MHz | FM Immune | Mode S | ||
| (ELS/EHS) | TCAS II (7.1) |
Data Collection Only
| Example: N123X | X | X | X | 6 Hrs | X | X | ELS | X | |
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| REMARKS: | |||||||||
| CRAF Aircraft Basic Data Sheet (Reverse), 20110524 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 3 of 5&RAttachment 8a 24 May 2011
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 | |||||||
| 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): (Data Collection Only) Future Eurocontrol-required system. Expected mandatory for Int'l Long-Range section by 2014. | ||||||||
| Tail Number | B-747 | |||||||
| Nose Loader | RVSM | RNP-5 | RNP-10 | 8.33 MHz | FM Immune | Mode S | ||
| (ELS/EHS) | TCAS II (7.1) |
Data Collection Only
| Example: N123X | X | X | X | 6 Hrs | X | X | ELS | X | |
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| REMARKS: | |||||||||
| CRAF Aircraft Basic Data Sheet (Reverse), 20110524 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 4 of 5&RAttachment 8a 24 May 2011
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 | |||||||
| 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): (Data Collection Only) Future Eurocontrol-required system. Expected mandatory for Int'l Long-Range section by 2014. | ||||||||
| Tail Number | B-747 | |||||||
| Nose Loader | RVSM | RNP-5 | RNP-10 | 8.33 MHz | FM Immune | Mode S | ||
| (ELS/EHS) | TCAS II (7.1) |
Data Collection Only
| Example: N123X | X | X | X | 6 Hrs | X | X | ELS | X | |
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| REMARKS: | |||||||||
| CRAF Aircraft Basic Data Sheet (Reverse), 20110524 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 5 of 5&RAttachment 8a 24 May 2011
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 Para. 4e.). 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 unshaded fields. Shaded fields are automatically filled from data computed on the CRAF Aircraft Basic 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. A dedicated tab is provided for aircraft to be assigned to the Aeromedical Evacuation segment. |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 2 of 2&RAttachment 8b 24 May 2011
Performance, B747 VZFW
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | |||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | |||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | |||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | ENTER AltZFW (LBs) | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | 0.000 | w/Range Bonus | ||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | |||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | ||||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | AltZFW & MTOW | MTOW & | ||
| MAX FUEL CAP | MAX RANGE - |
No Pyld
| Range (NM) | 0 | |||||||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||||||
| 75% of Alt MACL = | 0 | 3500 NM Payload = | 0 | 0 | Pax | Range at 75% ACL = | 0 | Enter data in this section | ||||||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||||||
| CFP Distance (NM) | ||||||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||||||
| Graph Payload | 0 | |||||||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b 24 May 2011
Performance, B747 VZFW
STILL AIR RANGE (Stage Length)--Nautical Miles (NM) PAYLOAD (lbs) Range/Payload Graph (B747 Variable ZFW)
Performance, B747, etc.
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | 0.000 | w/Range Bonus | ||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 3500 NM Payload = | 0 | 0 | Pax | Range at 75% ACL = | 0 | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| 0 | ||||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Performance, B747, etc.
Range/Payload Graph (B747, MD-11, and similar)
Performance, DC-10, etc.
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | 0.000 | w/Range Bonus | ||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 3500 NM Payload = | 0 | 0 | Pax | Range at 75% ACL = | 0 | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Performance, DC-10, etc.
Range/Payload Graph (DC-10, L1011, and similar)
Performance, B767, DC-8, etc.
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | 0.000 | w/Range Bonus | ||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 3500 NM Payload = | 0 | 0 | Pax | Range at 75% ACL = | 0 | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Performance, B767, DC-8, etc.
Range/Payload Graph (B767, DC-8, and similar)
Performance, B767 Aeromed
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | 0.000 | w/Range Bonus | ||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 3500 NM Payload = | 0 | 0 | Pax | Range at 75% ACL = | 0 | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Performance, B767 Aeromed
Range/Payload Graph (B767 Aeromedical Certified Only)
Performance, S-R High Capacity
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | ||||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 1500 NM Payload = | 0 | 0 | Pax | ER Bonus = | N/A | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Performance, S-R High Capacity
Range/Payload Graph (Short-Range High Capacity)
Performance, S-R and Domestic
CRAF AIRCRAFT PERFORMANCE DATA SHEET DATE PREPARED* Approximate Base MV Points
| 12/31/99 | ||||||||
| AIRCRAFT MODEL* | AIRCRAFT CONFIGURATION* | CARRIER* | ||||||
| 0.0 | 0.0 | 0.0 | 0.000 | Points | ||||
| TAKEOFF WEIGHT* | OPERATING WEIGHT* | CRUISE SPEED* | ALTITUDE(S)* | DESTINATION LANDING FUEL* | ||||
| 0.0 | 0.0 | 0.0 | 0.0 | 0.0 | ||||
| * Data is auto-filled from associated HQ AMC Form 82 | 0.0 | |||||||
| RANGE/PAYLOAD DATA POINTS | CFP Variance Check |
and Average Block Speed Calculation
| Limit Points | MZFW | MZFW & MTOW | MTOW & MAX FUEL CAP | MAX RANGE - No Pyld | ||||||||||||
| Range (NM) | 0 | |||||||||||||||
| Payload (lbs) | 0.0 | 0.0 | 0 | |||||||||||||
| 75% of Max ACL = | 0 | 1500 NM Payload = | 0 | 0 | Pax | ER Bonus = | N/A | Enter data in this section | ||||||||
| CFP Payload Variance = | 0.00% | SEAT RESTRICTED AT | 0 | Pax | ABS = | 0 | Kts | CFP Time | HR | MIN | ||||||
| CFP Distance (NM) | ||||||||||||||||
| CFP Payload (lbs) | ||||||||||||||||
| Graph Payload | 0 | |||||||||||||||
| Percent Variance | 0.00% | |||||||||||||||
| Average Block Speed (ABS) | 0 | |||||||||||||||
| CRAF Aircraft Performance Data Sheet, 20110524 | ||||||||||||||||
| 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 |
&RSOLICITATION NO: HTC711-11-R-C002
&CPage 1 of 2&RAttachment 8b
Range/Payload Graph (Short-Range and Domestic)
File details come from the government source that posted it. Updated .