Skip to main content

Cessna 177RG Cardinal Model Guide

Cessna 177RG Cardinal · Model Guide

Free account — keep the POHs & checklists you reference in one place.

Overview

The Cessna 177RG Cardinal is a four-seat, single-engine piston airplane with retractable landing gear, built from 1971 to 1978. It has a 200 hp Lycoming IO-360 engine. The 1976 handbook lists 156 knots top speed at sea level, 148 knots cruise at 75% power at 7000 ft, and a 2800 lb maximum weight.

  • Four seats, 200 hp, retractable gear. 1976 handbook: 148 knots cruise at 75% power at 7000 ft.
  • Fuel capacity changed: 1971-72 airplanes carry 50 gal usable, 1973 and later carry 60 gal usable.
  • Landing gear condition is the key inspection item: a UK accident report found fatigue failure of a main gear downlock pivot pin.
  • Check for the Hartzell propeller or turbonormalizer modifications, since each comes with its own placards and paperwork.

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.

Report a problem or request removal

Document details

Type
·
Model Guide
Year
·
2026
File size
·
50 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Engine power (hp)
·
200
Max baggage (lb)
·
120
Usable fuel (gal)
·
60
Max takeoff weight (lb)
·
2,800
Fuel capacity total (gal)
·
61
Propeller diameter (in)
·
78

Performance

Max range (nm)
·
895
Range 75pct (nm)
·
715
Rate of climb (fpm)
·
925
Service ceiling (ft)
·
17,100
Cruise speed 75pct (kt)
·
148
Landing ground roll (ft)
·
730
Max speed sea level (kt)
·
156
Takeoff ground roll (ft)
·
890

V-speeds

VA_KT
·
113
VFE_KT
·
95
VLE_KT
·
125
VLO_KT
·
125
VNE_KT
·
174
VNO_KT
·
142
STALL_FLAPS_UP_KT
·
57
STALL_FLAPS_DOWN_KT
·
50

Weight & balance

Max weight (lb)
·
2,800
Max baggage (lb)
·
120
Useful load (lb)
·
1,120
Empty weight (lb)
·
1,680
Cg aft limit (in)
·
114.7
Cg forward limit light (in)
·
101
Cg forward limit at max weight (in)
·
105.8
About this document
How many people does the Cessna 177RG Cardinal carry?

The Cessna 177RG Cardinal has four seats: two front and two rear. Maximum weight is 2800 lbs, and the baggage limit is 120 lbs.

How fast and how far does the Cessna 177RG Cardinal fly?

The 1976 handbook lists 156 knots maximum at sea level and 148 knots cruise at 75% power at 7000 ft. Range is 715 NM at 75% power and 895 NM at 10,000 ft, both with 60 gal usable fuel.

Which fuel does the Cessna 177RG Cardinal need?

Serials 177RG0001 through 177RG1051 need 100/130 minimum grade avgas. Serial 177RG1052 and up use 100LL/100. Alcohol-based fuels are prohibited.

What is the main pre-buy concern on a Cessna 177RG Cardinal?

The landing gear. A UK accident report on a Cessna F177RG Cardinal found fatigued main gear downlock pivot pins and a misadjusted nose gear downlock. Have the whole gear system inspected and review the gear maintenance history.

What is the Cessna 177RG Cardinal Model Guide?

The Cessna 177RG Cardinal Model Guide is a model guide for the Cessna 177RG Cardinal, dated 2026.

What year was the Cessna 177RG Cardinal Model Guide published?

The Cessna 177RG Cardinal Model Guide — the Cessna 177RG Cardinal model guide on file — is dated 2026.

How rare is it?
2,626Cessna 177RG Cardinal registered worldwide · 2,618 active

Common. More common than 99% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Cessna 177RG Cardinal.

More Cessna 177RG Cardinalmanuals & documents

See all 18 →

In this document

Performance and loading

The 1976 handbook lists a 925 fpm sea-level climb rate and a 17,100 ft service ceiling. Takeoff ground roll is 890 ft (1585 ft over a 50 ft obstacle). Landing roll is 730 ft (1350 ft over 50 ft). Maximum weight is 2800 lbs with up to 120 lbs of baggage. Range at 75% power is 715 NM with 60 gal usable.

What to inspect

Check the landing gear first. A UK Cessna F177RG accident report found out-of-adjustment nose gear downlock and fatigued main gear downlock pivot pins, after earlier signs of incomplete gear retraction. Also review the log for the service manual temporary revisions, which add component time limits and a fuel quantity indicating system test.

Fuel, engine and modifications

Serials through 177RG1051 need 100/130 minimum grade avgas. Serial 177RG1052 and up use 100LL/100. Alcohol-based fuels are prohibited. A mandatory bulletin covers turbonormalized airplanes (fuel servo reflow, new flight manual supplement) for better hot-weather cooling. A Hartzell 78-inch propeller STC is also available.

Safety notes

  • Do not fly with the gear pump circuit breaker pulled or with unresolved gear retraction faults; the UK accident airplane did so and its nose gear collapsed on landing.
  • Hartzell propeller STC placard: continuous operation is prohibited between 2000 and 2300 RPM with less than 10 inches manifold pressure.
  • Alcohol-based fuels can cause serious performance degradation and fuel system damage, and are prohibited.

Full document text

Cessna 177RG Cardinal Model Guide The Cessna 177RG Cardinal is a four-seat, single-engine piston airplane with retractable landing gear, built from 1971 to 1978. It has a 200 hp Lycoming IO-360 engine. The 1976 handbook lists 156 knots top speed at sea level, 148 knots cruise at 75% power at 7000 ft, and a 2800 lb maximum weight. • Four seats, 200 hp, retractable gear. 1976 handbook: 148 knots cruise at 75% power at 7000 ft. • Fuel capacity changed: 1971-72 airplanes carry 50 gal usable, 1973 and later carry 60 gal usable. • Landing gear condition is the key inspection item: a UK accident report found fatigue failure of a main gear downlock pivot pin. • Check for the Hartzell propeller or turbonormalizer modifications, since each comes with its own placards and paperwork. Performance and loading The 1976 handbook lists a 925 fpm sea-level climb rate and a 17,100 ft service ceiling. Takeoff ground roll is 890 ft (1585 ft over a 50 ft obstacle). Landing roll is 730 ft (1350 ft over 50 ft). Maximum weight is 2800 lbs with up to 120 lbs of baggage. Range at 75% power is 715 NM with 60 gal usable. What to inspect Check the landing gear first. A UK Cessna F177RG accident report found out-of-adjustment nose gear downlock and fatigued main gear downlock pivot pins, after earlier signs of incomplete gear retraction. Also review the log for the service manual temporary revisions, which add component time limits and a fuel quantity indicating system test. Fuel, engine and modifications Serials through 177RG1051 need 100/130 minimum grade avgas. Serial 177RG1052 and up use 100LL/100. Alcohol-based fuels are prohibited. A mandatory bulletin covers turbonormalized airplanes (fuel servo reflow, new flight manual supplement) for better hot-weather cooling. A Hartzell 78-inch propeller STC is also available. Safety notes: • Do not fly with the gear pump circuit breaker pulled or with unresolved gear retraction faults; the UK accident airplane did so and its nose gear collapsed on landing. • Hartzell propeller STC placard: continuous operation is prohibited between 2000 and 2300 RPM with less than 10 inches manifold pressure. • Alcohol-based fuels can cause serious performance degradation and fuel system damage, and are prohibited.