36421b6802f26c5f9b3b57ee27f1fce8afb597b655638c5fb4061c2627fae245 Section "Flight Planning Sheet" item count differs between passes (123 vs 120); verify nothing was dropped. Section "General Specifications" item count differs between passes (35 vs 42); verify nothing was dropped.

1. WEIGHT SYMBOL | DESCRIPTION | VALUE [lbs] MTOW maximum takeoff 2550 (normal); 2130 (utility) MLW maximum landing 2550 (normal); 2130 (utility) Mbc maximum baggage compartment 200 (normal); 0 (utility) Wb (unusable fuel + fluids) basic empty 1604 MUW (MTOW - Ws) maximum useful 946 (normal); 526 (utility) utility = no rear passengers; no (baggage + cargo) useful load normal = usable fuel + front passengers + rear passengers + (baggage + cargo) useful load utility = usable fuel + front passengers 2. SPEED SYMBOL | DESCRIPTION | SPEED VALUES [kias] Va maneuvering 113 (2550 GW); 89 (1634 GW) Vfe max flap extended 102 Vne never exceed 154 Vno structural cruising (> in smooth air) 125 Vs stalling speed fig. 5-3 Vso Vs/Vs in landing config. n/a Vx best angle of climb 64 Vy best rate of climb 76 Vapp (full flaps) final approach speed 66 Vcrosswind max crosswind 17 Green arc operational range 55-125 White arc flaps range 49-102 3. CENTER OF GRAVITY datum @ WLE + 78.4" NORMAL 2550 lbs 88.6" aft / 82" aft NORMAL < 2050 lbs 93" aft / 93" aft UTILITY 2130 lbs 82" aft / 83" aft UTILITY < 2050 lbs 93" aft / 93" aft 4. FUEL CONDITION | VALUE [US gal] max 50 unusable 2 usable 48

STEP | VALUES 0. LOAD CONFIGURATION 1. CONFIG-O-MATIC ITEM | WEIGHT [lbs] standard empty — operational equipment — basic empty — pilot — passenger 1 (co-pilot) — passenger 2 (rear) — passenger 3 (rear) — baggage + cargo — MAXIMUM USABLE FUEL — MAXIMUM GROSS — DRY — 2. CLIMB a. Climb Performance STATE | ITEM | VALUE INPUT OAT [°C] — Hp [ft] — OUTPUT V/S [ft/min] — b. Climb time, distance, fuel STATE | ITEM | VALUE INPUT OAT [°C] departure — Hp [ft] departure — OAT [°C] cruise — Hp [ft] cruise — OUTPUT CORRECTIONS climb time departure [min] — climb distance departure [mi] — climb fuel departure [gal] — climb time cruise [min] — climb distance cruise [mi] — climb fuel cruise [gal] — OUTPUT climb time [min] 0 climb distance [mi] 0 climb fuel [gal] 0 3. DESCENT STATE | ITEM | VALUE INPUT OAT [°C] arrival — Hp [ft] arrival — OAT [°C] cruise 0 Hp [ft] cruise 0 OUTPUT CORRECTIONS descent time arrival [min] — descent distance arrival [mi] — descent fuel arrival [gal] — descent time cruise [min] — descent distance cruise [mi] — descent fuel cruise [gal] — OUTPUT descent time [min] 0 descent distance [mi] 0 descent fuel [gal] 0 4. CRUISE a. Distance [mi] TRIP DISTANCE [mi] | CLIMB DISTANCE [mi] | DESCENT DISTANCE [mi] | CRUISE DISTANCE [mi] TRIP DISTANCE [mi] 0 CLIMB DISTANCE [mi] 0 DESCENT DISTANCE [mi] 0 CRUISE DISTANCE [mi] 0 b. TAS [kts] STATE | ITEM | VALUE | CRUISE TYPE [P/E] INPUT OAT [°C] cruise 0 Hp [ft] cruise 0 Cruise Power [65 %, 70 %, 75 %] — OUTPUT TAS [kts] — c. Time [hr] CRUISE DISTANCE [mi] | TAS [kts] | TAS [mi/hr] | CRUISE TIME [hr] CRUISE DISTANCE [mi] 0 TAS [kts] 0 TAS [mi/hr] 0 CRUISE TIME [hr] 7 d. Fuel [gal] CRUISE POWER [%] | CRUISE TYPE [P/E] | FUEL FLOW [gph] | CRUISE FUEL [gal] CRUISE POWER [%] 0 CRUISE TYPE [P/E] 0 FUEL FLOW [gph] — CRUISE FUEL [gal] 7 e. Mixture range [nm] CRUISE OAT [°C] | CRUISE Hp [ft] | CRUISE POWER [%] | CRUISE P/E RANGE [nm] CRUISE OAT [°C] 0 CRUISE Hp [ft] 0 CRUISE POWER [%] 0 CRUISE P/E RANGE [nm] — 5. TOTAL FLIGHT TIME TOTAL FLIGHT TIME [hr] 7 6. TOTAL FLIGHT FUEL TOTAL FLIGHT FUEL [gal] 7 7. FLIGHT SIM FUEL CAPACITY [lbs] | LEFT WING FUEL [lbs] | RIGHT WING FUEL [lbs] CAPACITY [lbs] 288 LEFT WING FUEL [lbs] 7 RIGHT WING FUEL [lbs] 7 8. LOADING CONSTRAINTS ITEM | WEIGHT [lbs] | ARM AFT DATUM [in] | MOMENT [lb*in] basic empty 0 / 87.6 / — pilot + passenger 1 (front) 0 / 80.5 / — passenger 2 + passenger 3 (rear) 0 / 118.1 / — baggage + cargo 0 / 142.8 / — total flight fuel 7 / 95 / — ACTUAL GROSS 7 / — / 0 a. Weight constraint The actual gross weight must be < 2550 lbs (normal) and < 2130 lbs (utility). a. CG constraint CG POSITION THEO. [in] — CG POSITION GRAPH [in] 7 The CG position must adhere to the value range from the "General Specifications" data sheet with operational maxima and minima shown on the graph. 9. TAKEOFF STATE | ITEM | VALUE INPUT OAT [°C] departure 0 Hp [ft] departure 0 Headwind (H) / Tailwind (T) [kts] — Actual Gross Weight [lbs] 7 Flaps 0/25 [°] — Performance (P) / Ground Roll (G) — OUTPUT minimum takeoff distance [ft] — 10. LANDING STATE | ITEM | VALUE INPUT OAT [°C] arrival 0 Hp [ft] arrival 0 Headwind (H) / Tailwind (T) [kts] — Landing Gross Weight [lbs] 7 Performance (P) / Ground Roll (G) — OUTPUT minimum landing distance [ft] — 11. EXTRA

All information in this worbook was based on the Piper Archer II manuals by Dreamfleet. All information contained herein is only to be used for flight simulation entertainment purposes and NOT real world flying! The coding and layout of the document was made by me, Peter. I am in no way responsible for the manner in which you use this document and am not responsible for any damages it may incurr with your software or hardware. You are free to modify certain things (but wouldn't recomment it due to the programming and cell detail) but cannot distribute this document for financial gain. If you choose to upload the document with your modifications to a flight simulator enthusiasts website, I require credit for my work cause this took some time. Enjoy! Peter VERSION : 1.0 37377