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CESSNA 182Q SKYLANE Model Guide

CESSNA 182Q SKYLANE · Model Guide

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Overview

The CESSNA 182Q SKYLANE is a single-engine piston Cessna with a 230 hp Teledyne Continental O-470-U and a McCauley constant-speed propeller. The handbook lists 144 kt cruise, 880 NM range, 2,950 lb max takeoff weight and 1,260 lb useful load.

  • Handbook figures: 148 kt max speed, 144 kt cruise at 75% power at 8,000 ft, 1,010 fpm climb, 16,500 ft service ceiling.
  • Useful load is 1,260 lb on 1,700 lb empty weight, with 200 lb of baggage allowed. Max takeoff weight is 2,950 lb.
  • Takeoff over a 50 ft obstacle needs 1,350 ft, and landing over 50 ft also needs 1,350 ft.
  • Confirm fuel capacity and any engine or propeller conversion before you buy. Handbooks and listings differ.

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.

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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)
·
230
Height (ft)
·
9.25
Length (ft)
·
28
Wingspan (ft)
·
36
Empty weight (lb)
·
1,700
Fuel capacity (gal)
·
92
Max takeoff weight (lb)
·
2,950

Performance

Range (nm)
·
880
Fuel burn (gph)
·
12
Max speed (kt)
·
148
Cruise speed (kt)
·
144
Rate of climb (fpm)
·
1,010
Service ceiling (ft)
·
16,500
Landing distance (ft)
·
590
Takeoff distance (ft)
·
705

V-speeds

VA_KTS
·
111
VX_KTS
·
65
VY_KTS
·
70
VFE_KTS
·
140
VNE_KTS
·
179
VNO_KTS
·
143
STALL_SPEED_CLEAN_KTS
·
56
STALL_SPEED_LANDING_KTS
·
50

Weight & balance

Cg range (in)
·
33.0 to 48.5
Useful load (lb)
·
1,260
Empty weight (lb)
·
1,700
Max ramp weight (lb)
·
2,960
Baggage allowance (lb)
·
200
Max landing weight (lb)
·
2,950
Max takeoff weight (lb)
·
2,950
About this document
How fast and how far does the CESSNA 182Q SKYLANE go?

The CESSNA 182Q SKYLANE is listed at 148 kt maximum at sea level and 144 kt cruise at 75% power at 8,000 ft. The 1979 handbook gives 880 NM range with 88 gal usable fuel.

What can the CESSNA 182Q SKYLANE carry?

The CESSNA 182Q SKYLANE has a 1,260 lb useful load, a 2,950 lb max takeoff weight and a 200 lb baggage allowance. Fuel is 92 gal total, so check the weight and balance with full fuel and passengers.

How much runway does the CESSNA 182Q SKYLANE need?

The CESSNA 182Q SKYLANE needs 705 ft of ground roll and 1,350 ft to clear a 50 ft obstacle on takeoff. Landing needs 590 ft of ground roll and 1,350 ft over a 50 ft obstacle.

What is the CESSNA 182Q SKYLANE Model Guide?

The CESSNA 182Q SKYLANE Model Guide is a model guide for the CESSNA 182Q SKYLANE, dated 2026.

What year was the CESSNA 182Q SKYLANE Model Guide published?

The CESSNA 182Q SKYLANE Model Guide — the CESSNA 182Q SKYLANE model guide on file — is dated 2026.

How rare is it?
17,685CESSNA 182Q SKYLANE registered worldwide · 17,645 active

Common. One of the most common aircraft types we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the CESSNA 182Q SKYLANE.

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In this document

Check which fuel setup the airplane has

The 1979 handbook lists 92 gal total fuel and 88 gal usable, with 880 NM range at 75% power at 8,000 ft. The 1977 handbook lists 56 and 75 gal usable options, with 520 NM and 735 NM at 75% power. Confirm which tanks the airplane has.

Modifications and STCs

Some 182Qs are converted. One 1979 listing has a 300 hp Continental IO-550, 3,100 lb gross weight and 1,198.8 lb useful load. An EASA STC covers an MT-Propeller on IO-550-D 182Qs, and a Robertson STOL supplement exists under STC SA1382WE. Verify the paperwork and weight and balance.

Maintenance records to review

The 1977-1986 service manual carries a temporary revision on inspecting cracks at the trailing edge of corrugated-skin control surfaces (Service Bulletin SEB99-18). It also adds a fuel quantity indicating system test. Ask for logbook proof. Oil capacity is 12 qts, and the preflight checklist reads 9-12 qts.

Safety notes

  • An accident report on a 182Q (G-PLEE) describes engine power loss on final near 0°C with visible moisture. The pilot suspected carburetor icing, and no mechanical cause was found.
  • The handbook lists max ramp weight as 2,960 lb and max takeoff and landing weight as 2,950 lb. Stay within these limits unless an approved STC raises them.
  • The checklist lists best glide at 70 kts. Practise the engine-failure procedure, including carburetor heat and fuel selector checks.

Full document text

CESSNA 182Q SKYLANE Model Guide The CESSNA 182Q SKYLANE is a single-engine piston Cessna with a 230 hp Teledyne Continental O-470-U and a McCauley constant-speed propeller. The handbook lists 144 kt cruise, 880 NM range, 2,950 lb max takeoff weight and 1,260 lb useful load. • Handbook figures: 148 kt max speed, 144 kt cruise at 75% power at 8,000 ft, 1,010 fpm climb, 16,500 ft service ceiling. • Useful load is 1,260 lb on 1,700 lb empty weight, with 200 lb of baggage allowed. Max takeoff weight is 2,950 lb. • Takeoff over a 50 ft obstacle needs 1,350 ft, and landing over 50 ft also needs 1,350 ft. • Confirm fuel capacity and any engine or propeller conversion before you buy. Handbooks and listings differ. Check which fuel setup the airplane has The 1979 handbook lists 92 gal total fuel and 88 gal usable, with 880 NM range at 75% power at 8,000 ft. The 1977 handbook lists 56 and 75 gal usable options, with 520 NM and 735 NM at 75% power. Confirm which tanks the airplane has. Modifications and STCs Some 182Qs are converted. One 1979 listing has a 300 hp Continental IO-550, 3,100 lb gross weight and 1,198.8 lb useful load. An EASA STC covers an MT-Propeller on IO-550-D 182Qs, and a Robertson STOL supplement exists under STC SA1382WE. Verify the paperwork and weight and balance. Maintenance records to review The 1977-1986 service manual carries a temporary revision on inspecting cracks at the trailing edge of corrugated-skin control surfaces (Service Bulletin SEB99-18). It also adds a fuel quantity indicating system test. Ask for logbook proof. Oil capacity is 12 qts, and the preflight checklist reads 9-12 qts. Safety notes: • An accident report on a 182Q (G-PLEE) describes engine power loss on final near 0°C with visible moisture. The pilot suspected carburetor icing, and no mechanical cause was found. • The handbook lists max ramp weight as 2,960 lb and max takeoff and landing weight as 2,950 lb. Stay within these limits unless an approved STC raises them. • The checklist lists best glide at 70 kts. Practise the engine-failure procedure, including carburetor heat and fuel selector checks.