The file's text, extracted by GovTribe without its formatting.
Attachment 10 – Aircraft Performance Data Chart Attachment 10 has three components:
1. Performance Data Chart, Excel File. This file has multiple tabs that correspond to each Mission and allows multiple aircraft to be entered on each chart. The Excel file is available as an attachment to the RFP on SAM.GOV or from the CO. Offerors shall complete Attachment 10 in the excel version from SAM.GOV for proposals. See Section E.1 for specifications for Attachment 10 proposal requirements.
2. Flight Profile Diagrams
3. Instructions for completing Performance Data Chart.
Remainder of Page Intentionally Left Blank
Flight Profile Diagrams for Exhibit 10
Instructions for completing Performance Data Chart – Attachment 10 Missions 1, 2a & b, 3a & b, 4a, b, & c
| Column |
| Description or Instruction |
| All Columns |
| Weights shall be in Pounds (Lbs.) |
Time shall be in Hours, Tenths and Hundredths (0.00) Flight Distances shall be in Nautical Miles (NM) Takeoff Distance shall be in Feet (ft.)
| F |
| If no MZFW limitation is published enter NA |
| K |
| Enter Vyse Airspeed. If it is Not Applicable to the aircraft use a Mission Category where the cell is identified with (If Applicable to Aircraft) and enter NA. |
| L |
| Single Engine Service Ceiling Definition: Altitude when a multiengine airplane can no longer maintain a 50-FPM rate of climb with one engine inoperative. If it is Not Applicable to the aircraft use a Mission Category where the cell is identified with (If Applicable to Aircraft) and enter NA |
| P |
| Enter the actual takeoff weight (N + Fuel Weight) of the aircraft to perform the mission as identified in Q - AP Reference B-1 (a thru i) typical mission profile |
| U-W |
| From Top of climb 1 to start of Descent 1 |
| AA-AE |
| From bottom of Descent 1 through loiter phase (Reference B-1(a thru i) until start of Climb 2. |
| AF-AH |
| Climb 2 - From Loiter back to cruise altitude |
| AI-AK |
| Cruise 2 - From the top of the climb 2 to the start of the Descent 2 |
| AL-AN |
| Descent from cruise 2, approach, and landing at departure airport elevation and ISA temperature |
| AO, AP |
| Fuel remaining at the completion of the flight described P through AN. Must meet minimum fuel requirements identified in the contract. |
Remainder of Page Blank
Missions 5a & b, 6a & b, 7a & b
| Column |
| Description or Instruction |
| All Columns |
| Weights shall be in Pounds (Lbs.) |
Time shall be in Hours, Tenths and Hundredths (0.00) Flight Distances shall be in Nautical Miles (NM) Takeoff/Landing Distance shall be in Feet (ft.)
| F |
| Identify configuration of aircraft offered. If multiple configurations offered complete additional lines for each configuration |
| G |
| Identify if Gravel, Grass, Unimproved airstrip capable and configured. Identify which type of runway surface. If all enter ALL |
| L |
| If there is an identified airframe limitation enter here. If none exists enter NA |
| P |
| If single engine enter NA |
| Q |
| Single Engine Service Ceiling Definition: Altitude when a multiengine airplane can no longer maintain a 50-FPM rate of climb with one engine inoperative. Enter NA for single engine aircraft. |
| V |
| Enter the actual takeoff weight (T + Fuel Weight) of the aircraft to perform the mission as identified in W-AV Reference B-1 (a thru i) typical mission profile |
| AA-AC |
| From Top of climb 1 to start of Descent 1 |
| AG-AK |
| From bottom of Descent 1 through loiter phase until start of Climb 2. |
| AL - AN |
| Climb 2 - From Loiter back to cruise altitude |
| AO-AQ |
| Cruise 2 - From the top of the climb 2 to the start of the Descent 2 |
| AR-AT |
| Descent from cruise 2, approach, and landing at departure airport elevation and ISA temperature |
| AU, AV |
| Fuel remaining at the completion of the flight described P through AN. Must meet minimum fuel requirements identified in the contract. |
Remainder of Page Blank image1.emf
Department of Agriculture Forest Service