CESSNA 172E SKYHAWK Model Guide
CESSNA 172E SKYHAWK · Model Guide
Overview
The CESSNA 172E SKYHAWK is a single-engine piston Cessna with a 150 hp Lycoming O-320 and a McCauley 1A170/DM propeller. Listed figures are 110 kt cruise, 600 nm range, 40 gal of fuel, 2400 lb max takeoff weight and 850 lb useful load. The wider 172 family is listed with up to 4 passengers.
- Listed cruise is 110 kt at about 10 gph, with a 600 nm range on 40 gal of fuel.
- Empty weight is 1550 lb and useful load is 850 lb, with up to 120 lb in the baggage area. Max takeoff weight is 2400 lb.
- Older 172 handbooks in the file show 2300 lb gross weight and Continental power. Check the weights and engine of the airplane you inspect.
- Listed climb is 730 fpm and service ceiling is 14000 ft. Max demonstrated crosswind is 15 kt.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 48 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm) ·
- 600
- Engine (hp) ·
- 150
- Height (ft) ·
- 8
- Length (ft) ·
- 27
- Wingspan (ft) ·
- 36
- Empty weight (lb) ·
- 1,550
- Fuel capacity (gal) ·
- 40
- Max takeoff weight (lb) ·
- 2,400
Performance
- Fuel burn (gph) ·
- 10
- Max speed (kt) ·
- 124
- Cruise speed (kt) ·
- 110
- Max crosswind (kt) ·
- 15
- Rate of climb (fpm) ·
- 730
- Service ceiling (ft) ·
- 14,000
- Landing distance (ft) ·
- 1,200
- Takeoff distance (ft) ·
- 1,500
V-speeds
- VA_KTS ·
- 105
- VX_KTS ·
- 62
- VY_KTS ·
- 74
- VFE_KTS ·
- 85
- VNE_KTS ·
- 163
- VNO_KTS ·
- 125
- VS1_KTS ·
- 48
- VSO_KTS ·
- 40
Weight & balance
- Useful load (lb) ·
- 850
- Cg aft limit (in) ·
- 40
- Max ramp weight (lb) ·
- 2,400
- Baggage allowance (lb) ·
- 120
- Basic empty weight (lb) ·
- 1,550
- Max landing weight (lb) ·
- 2,400
- Max takeoff weight (lb) ·
- 2,400
- Cg forward limit (in) ·
- 34
How far and how fast does the CESSNA 172E SKYHAWK fly?
The CESSNA 172E SKYHAWK is listed at 110 kt cruise and 124 kt max speed. Range is 600 nm on 40 gal at about 10 gph. The 172 family is listed up to 140 kt and 700 nm, which is family-level context only.
How much can the CESSNA 172E SKYHAWK carry?
The CESSNA 172E SKYHAWK has a 2400 lb max takeoff weight, 1550 lb empty weight and 850 lb useful load. The baggage allowance is 120 lb. Weigh the actual airplane, because installed equipment changes empty weight.
Why do the older handbooks show different numbers for the CESSNA 172E SKYHAWK?
The 1965 to 1972 handbooks in the file cover other 172 models. They show 2300 lb gross weight and 36 to 42 gal of fuel, with Continental O-300 or Lycoming O-320 engines. Check the 172E's own paperwork and weight and balance.
What is the CESSNA 172E SKYHAWK Model Guide?
The CESSNA 172E SKYHAWK Model Guide is a model guide for the CESSNA 172E SKYHAWK, dated 2026.
What year was the CESSNA 172E SKYHAWK Model Guide published?
The CESSNA 172E SKYHAWK Model Guide — the CESSNA 172E SKYHAWK model guide on file — is dated 2026.
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172E SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
CESSNA 172E SKYHAWK for sale now
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More CESSNA 172E SKYHAWKmanuals & documents
- Aircraft Checklist USAF T-41C (Cessna 172E)Checklist
- table of contentsTraining Manual
- 1967 Cessna 172H Owner's Manual - AeroElectricWeight & Balance
- Cessna. - Seaplane ScenicsPerformance Data
- N2134Y Operating HandbookPilot's Operating Handbook
- Weight & Balance for CESSNA 172E SKYHAWKWeight & Balance
- Supplemental Type Certificate for CESSNA 172E SKYHAWKSupplemental Type Certificate
- C172F POH.pdf - Monticello Flying ClubWeight & Balance
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In this document
Performance and runway needs
Listed takeoff distance is 1500 ft, or 2000 ft to clear a 50 ft obstacle. Landing distance is 1200 ft, or 1500 ft over 50 ft. Climb is 730 fpm. Stall is 50 kt clean and 45 kt in landing configuration. Best glide is 65 kt.
What to check on a pre-buy
The USAF T-41C (172E) checklist gives these checks. Oil: 6 quarts minimum, 8 maximum. Brake pads: 3/32 inch minimum. Magnetos at run-up: 150 RPM maximum drop and 50 RPM maximum difference. Drain the fuel strainer for 4 seconds. Also confirm that the engine and propeller match the listed Lycoming O-320 and McCauley 1A170/DM. A Cleveland wheel and brake conversion kit is listed for 172/Skyhawk models, so check which brakes are fitted.
Safety notes
- Do not operate with less than 6 quarts of oil (T-41C 172E checklist).
- Drain the fuel strainer for 4 seconds and check the sample before flight.
- At run-up, a magneto drop over 150 RPM or a difference over 50 RPM between magnetos is outside the checklist limits.
Full document text
CESSNA 172E SKYHAWK Model Guide The CESSNA 172E SKYHAWK is a single-engine piston Cessna with a 150 hp Lycoming O-320 and a McCauley 1A170/DM propeller. Listed figures are 110 kt cruise, 600 nm range, 40 gal of fuel, 2400 lb max takeoff weight and 850 lb useful load. The wider 172 family is listed with up to 4 passengers. • Listed cruise is 110 kt at about 10 gph, with a 600 nm range on 40 gal of fuel. • Empty weight is 1550 lb and useful load is 850 lb, with up to 120 lb in the baggage area. Max takeoff weight is 2400 lb. • Older 172 handbooks in the file show 2300 lb gross weight and Continental power. Check the weights and engine of the airplane you inspect. • Listed climb is 730 fpm and service ceiling is 14000 ft. Max demonstrated crosswind is 15 kt. Performance and runway needs Listed takeoff distance is 1500 ft, or 2000 ft to clear a 50 ft obstacle. Landing distance is 1200 ft, or 1500 ft over 50 ft. Climb is 730 fpm. Stall is 50 kt clean and 45 kt in landing configuration. Best glide is 65 kt. What to check on a pre-buy The USAF T-41C (172E) checklist gives these checks. Oil: 6 quarts minimum, 8 maximum. Brake pads: 3/32 inch minimum. Magnetos at run-up: 150 RPM maximum drop and 50 RPM maximum difference. Drain the fuel strainer for 4 seconds. Also confirm that the engine and propeller match the listed Lycoming O-320 and McCauley 1A170/DM. A Cleveland wheel and brake conversion kit is listed for 172/Skyhawk models, so check which brakes are fitted. Safety notes: • Do not operate with less than 6 quarts of oil (T-41C 172E checklist). • Drain the fuel strainer for 4 seconds and check the sample before flight. • At run-up, a magneto drop over 150 RPM or a difference over 50 RPM between magnetos is outside the checklist limits.