CESSNA 172Q CUTLASS Model Guide
CESSNA 172Q CUTLASS · Model Guide
Overview
The CESSNA 172Q CUTLASS is a 1983 model-year single-engine piston Cessna. Its Information Manual lists a carbureted 180 hp Lycoming O-360-A4N and a fixed-pitch propeller. The manual quotes 122 knots cruise at 75% power at 8500 ft. Total fuel is 54 gallons with standard tanks or 68 gallons with long range tanks.
- 180 hp Lycoming O-360-A4N, fixed-pitch prop: 122 kt cruise at 75% power at 8500 ft, 124 kt maximum at sea level.
- Max ramp weight 2558 lb, takeoff/landing 2550 lb. Useful load is 1072 lb (Cutlass) with a 120 lb baggage allowance.
- Standard tanks hold 54 gal (50 usable); long range tanks hold 68 gal (62 usable), for up to 775 nm of range.
- Registry-style data conflicts with the manual (engine, weights). Verify against the airplane's own POH.
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 ·
- 50 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 180
- Useful load (lb) ·
- 1,072
- Empty weight (lb) ·
- 1,486
- Fuel capacity (gal) ·
- 54
- Max ramp weight (lb) ·
- 2,558
- Baggage allowance (lb) ·
- 120
- Max takeoff weight (lb) ·
- 2,550
- Long range fuel capacity (gal) ·
- 68
Performance
- Max range (nm) ·
- 775
- Max speed (kt) ·
- 124
- Cruise speed (kt) ·
- 122
- Rate of climb (fpm) ·
- 680
- Service ceiling (ft) ·
- 17,000
- Landing ground roll (ft) ·
- 575
- Takeoff ground roll (ft) ·
- 960
- Takeoff distance over 50ft (ft) ·
- 1,690
V-speeds
- ROTATION_SPEED_KTS ·
- 55
- STALL_SPEED_CLEAN_KTS ·
- 53
- STALL_SPEED_LANDING_KTS ·
- 48
Weight & balance
- Useful load (lb) ·
- 1,072
- Empty weight (lb) ·
- 1,486
- Max ramp weight (lb) ·
- 2,558
- Baggage allowance (lb) ·
- 120
- Max takeoff weight (lb) ·
- 2,550
What engine does the CESSNA 172Q CUTLASS have?
The CESSNA 172Q CUTLASS Information Manual lists an Avco Lycoming O-360-A4N. It is a normally aspirated, carbureted, four-cylinder engine rated at 180 BHP at 2700 RPM, driving a fixed-pitch propeller.
How far can the CESSNA 172Q CUTLASS fly?
The CESSNA 172Q CUTLASS manual shows up to 775 nm at maximum range at 10,000 ft with 62 usable gallons. At 75% power it shows 475 nm with 50 gallons or 620 nm with 62 gallons.
What is the CESSNA 172Q CUTLASS useful load?
The manual lists 1072 lb for the Cutlass, with a standard empty weight of 1486 lb. Max ramp weight is 2558 lb and max takeoff/landing weight is 2550 lb. Baggage allowance is 120 lb.
What airworthiness item should I check on a CESSNA 172Q CUTLASS?
If the CESSNA 172Q CUTLASS engine was overhauled or had cylinders replaced, check AD 2009-26-12 on ECi Titan cylinder assemblies. No further action is needed if neither applies.
What is the CESSNA 172Q CUTLASS Model Guide?
The CESSNA 172Q CUTLASS Model Guide is a model guide for the CESSNA 172Q CUTLASS, dated 2026.
What year was the CESSNA 172Q CUTLASS Model Guide published?
The CESSNA 172Q CUTLASS Model Guide — the CESSNA 172Q CUTLASS 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 172Q CUTLASS.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
CESSNA 172Q CUTLASS for sale now
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In this document
Performance (manual figures)
Takeoff ground roll is 960 ft, or 1690 ft over a 50-ft obstacle. Landing ground roll is 575 ft, or 1335 ft over 50 ft. Climb at sea level is 680 fpm and service ceiling is 17000 ft. Stall is 53 knots flaps up and 48 knots flaps down. Figures assume standard atmosphere, level hard dry runway and no wind; individual airplanes vary.
Range and fuel
At 75% power with 50 usable gallons, the manual shows 475 nm in 4.0 hrs. With 62 usable gallons it shows 620 nm in 5.2 hrs. Maximum range at 10,000 ft is 600 nm (6.4 hrs) with 50 gallons and 775 nm (8.2 hrs) with 62 gallons. These figures include a 45 minute reserve. Confirm which tank option the airplane has.
What to check before buying
Ask whether the engine was overhauled or had cylinders replaced, since AD 2009-26-12 covers ECi Titan cylinders on the O-360. Check the engine mount vibration isolators; the vendor recommends replacing them at every overhaul. Oil capacity is 9 qts. Check magneto drop on the run-up: a max drop of 125 rpm and a difference between mags of 50 rpm.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- The 172Q Information Manual is for general purposes only and is not kept current. Operate from the airplane's official POH/AFM.
- AD 2009-26-12 applies to engines overhauled or with cylinders replaced. If it applies, confirm compliance records for the O-360-A4N.
- Weights and engine data vary between sources. Use the weight and balance data for the specific airplane, not generic listings.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
CESSNA 172Q CUTLASS Model Guide The CESSNA 172Q CUTLASS is a 1983 model-year single-engine piston Cessna. Its Information Manual lists a carbureted 180 hp Lycoming O-360-A4N and a fixed-pitch propeller. The manual quotes 122 knots cruise at 75% power at 8500 ft. Total fuel is 54 gallons with standard tanks or 68 gallons with long range tanks. • 180 hp Lycoming O-360-A4N, fixed-pitch prop: 122 kt cruise at 75% power at 8500 ft, 124 kt maximum at sea level. • Max ramp weight 2558 lb, takeoff/landing 2550 lb. Useful load is 1072 lb (Cutlass) with a 120 lb baggage allowance. • Standard tanks hold 54 gal (50 usable); long range tanks hold 68 gal (62 usable), for up to 775 nm of range. • Registry-style data conflicts with the manual (engine, weights). Verify against the airplane's own POH. Performance (manual figures) Takeoff ground roll is 960 ft, or 1690 ft over a 50-ft obstacle. Landing ground roll is 575 ft, or 1335 ft over 50 ft. Climb at sea level is 680 fpm and service ceiling is 17000 ft. Stall is 53 knots flaps up and 48 knots flaps down. Figures assume standard atmosphere, level hard dry runway and no wind; individual airplanes vary. Range and fuel At 75% power with 50 usable gallons, the manual shows 475 nm in 4.0 hrs. With 62 usable gallons it shows 620 nm in 5.2 hrs. Maximum range at 10,000 ft is 600 nm (6.4 hrs) with 50 gallons and 775 nm (8.2 hrs) with 62 gallons. These figures include a 45 minute reserve. Confirm which tank option the airplane has. What to check before buying Ask whether the engine was overhauled or had cylinders replaced, since AD 2009-26-12 covers ECi Titan cylinders on the O-360. Check the engine mount vibration isolators; the vendor recommends replacing them at every overhaul. Oil capacity is 9 qts. Check magneto drop on the run-up: a max drop of 125 rpm and a difference between mags of 50 rpm. Safety notes: • The 172Q Information Manual is for general purposes only and is not kept current. Operate from the airplane's official POH/AFM. • AD 2009-26-12 applies to engines overhauled or with cylinders replaced. If it applies, confirm compliance records for the O-360-A4N. • Weights and engine data vary between sources. Use the weight and balance data for the specific airplane, not generic listings.