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Archive / FAA Pilot’s Handbook of Aeronautical Knowledge / Pilot’s Handbook — Appendices

Appendices, Part 1

Appendices — Part 1

FAA-H-8083-25C (2023)

A-1

Short Field Takeoff Distance at 2,450 Pounds for a Cessna Model 172R

Performance Data for Cessna

Model 172R and Challenger 605

Appendix A

A-2

Time, Fuel, and Distance to Climb at 2,450 Pounds for a Cessna Model 172R

A-3

Cruise Performance for a Cessna Model 172R

A-4

Short Field Landing Distance at 2,450 Pounds for a Cessna Model 172R

A-5

0 500 1,000 1,500 2,000 2,500 3,000 3,500 4,000 4,500

4,219

3,600

5,840

4,940

3,465

3,401

SL

ISA

6,432

5,234

9,400

7,755

4,804

4,535

5,000 ft

ISA +20°C

40,000

35,000

50,000

46,000

30,000

2:00 4:00 6:00 8:00 9:50

Conditions: 26,985 lb BOW, M 0.74

cruise speed, ISA, zero wind, NBAA

IFR reserves (200 NM)

Note: Fuel burn figures provided on

top of graph are based on 1,000 lb

payload performance computations.

Range (NM)

Takeoff Field Length (feet) 3,190 6,570 10,230 14,200 18,105Fuel

Burn (lb)

Time (hour)

Gross

Takeoff

Weight (lb)

Max

Payload

3,000 lb

Payload

1,000 lb

Payload Zero Payload

Challenger 605 Range/Payload Profile

Original source PDFPublished from pages 1–5 of the recorded source chapter.
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