
Cessna (Textron Aviation)
182 Skylane
Single-engine piston · Trainer and personal aircraft · Pre-1980 classic
Photo: Adrian Pingstone (Arpingstone) via Wikimedia Commons · Public domain
- Power
- 230 hp
- Cruise
- 145 kt
- MTOW
- 3,100 lb
- Range
- 915 nm
- Fuel
- 100LL avgas
🇺🇸Specs shown in Imperial.
Performance
- Cruise speed (Vc)145 kt
- Never-exceed speed (Vne)175 kt
- Stall (landing config) (Vs0)49 kt
- Climb rate924 fpm
- Service ceiling18,100 ft
- Range915 nm
- Endurance6 h
- Takeoff roll1,515 ft
- Landing roll1,350 ft
Weights
- MTOW3,100 lb
- Empty weight1,990 lb
- Useful load1,110 lb
- Baggage capacity200 lb
Dimensions
- Wingspan36 ft
- Length29 ft
- Height9.4 ft
- Cabin width42 in
Powerplant
- EngineLycoming IO-540-AB1A5 — 230 hp · 100LL · 13 gph
- Total horsepower230 hp
- Primary fuel100LL avgas
- Unleaded pathG100UL eligible (STC available)
Cockpit & avionics
- Cockpit typeglass
- Autopilot commonly availableYes
- Typical packages
- Garmin G1000 NXi— modern (current new-build)
- Garmin G1000 (original)— 2005–2017 new-build
- Six-pack analog— pre-2005 airframes
Certification
- RegulatoryFAR Part 23 · EASA CS-23
- Certified rolesNormal category · Utility category
- IFRYes
- Spin approvedNo
- Aerobatic-categoryNo
- TailwheelNo
- Complex (FAR 61.31)No
- High-performance (FAR 61.31)Yes
Why is the 182 Skylane popular?
Structured popularity-driver evidence. Each axis below carries one factual statement; we don't grade, the facts speak.
Production volume
Approximately 23,000 Cessna 182 Skylanes have been built since 1956 — the third-most-produced civil aircraft after the 172 and 150 / 152.
Pedagogy and handling
230 hp Lycoming IO-540-AB1A5 places the 182 above the FAR 61.31 high-performance threshold, making it the canonical airframe for the high-performance endorsement at schools that operate the type.
Operating economics
1,130 lb useful load and a four-seat cabin make the 182 the typical airframe at schools that need both training utility and personal cross-country use; 18,100 ft service ceiling and 924 fpm sea-level climb open the type to high-density-altitude operations.
Parts and MRO ecosystem
Textron Aviation continues factory production and rebuild support; Cessna Owner Organization and Cessna Pilots Association provide independent type-club coverage.
Fuel future-proofing
Lycoming IO-540 series is on Lycoming's list of engines compatible with G100UL once supply is regional, giving the 182 fleet a path off 100LL without engine swap.
Before you buy more aircraft
The next airframe is rarely the highest-leverage move.
Flight school revenue is a function of three things — utilization, dispatch reliability, and student progression — that multiply rather than add. Most schools running below 850 hours per aircraft per year have hidden capacity worth more than the next purchase, already paid for and sitting on the ramp.
Read: Why buying more aircraft probably won't grow your schoolHow flight schools track this aircraft in Aviatize
Schools typically configure 182s as the high-performance / mountain / cross-country airframe paired with a 172 ab-initio fleet. Engine reserves track against the IO-540-AB1A5 2,000-hour TBO. The high-performance endorsement requirement is commonly modelled as a per-pilot validation that gates booking creation if the endorsement is missing.
Weighing up the numbers? Model the operating economics of a 182 Skylane fleet with our free profitability calculator — no signup required.
Editorial confidence
3 primary sources cited (POH / TCDS / type-club). Spec data and regulatory positioning are well-attributed; narrative synthesis is editorial.
Sources
Primary sources are POH / TCDS / manufacturer pages; derived sources record where Aviatize editorial synthesis is layered on top.
- Primary sourcePOH·Retrieved 2026-05-26
Textron Aviation (Cessna)
https://cessna.txtav.com/en/piston/cessna-skylaneCessna Skylane product page. Facts verified on this page on 2026-05-26: Lycoming IO-540-AB1A5, 230 hp; McCauley 3-blade constant-speed propeller; Max Range 915 nm; Max Cruise Speed 145 ktas; Useful Load 1,110 lb (entry updated from 1,130 to match factory page); MTOW 3,100 lb; Max Landing Weight 2,950 lb; Empty Weight ~1,990 lb (updated from 1,970); usable fuel 87 gal / 522 lb; Garmin G1000 NXi avionics with GI 275 electronic standby.
- Primary sourceFAA TCDS·Retrieved 2026-05-26
Federal Aviation Administration (FAA)
https://drs.faa.gov/browse/TCDSFAA TCDS 3A13.
- Primary sourceEASA TCDS·Retrieved 2026-05-26
European Union Aviation Safety Agency (EASA)
https://www.easa.europa.eu/en/document-library/type-certificatesEASA TCDS A.066.
- Editorial synthesisAviatize-internal·Retrieved 2026-05-05
Aviatize editorial
Entry authored by Aviatize from accumulated industry knowledge cross-referenced against the primary sources cited above. Specific fleet figures, fleet wins, and recent production status changes are research-backlog candidates and should be verified against primary sources before flipping verified: true.
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Photos & credits: each thumbnail opens that aircraft’s page, where the photographer and licence are credited under the hero image.