Beechcraft Bonanza 36 / A36 / G36 vs Cessna 210M/N Centurion II (1977-1984)

Head-to-head — specs, at a glance.

Seats
6 · 6
Engine
piston single · piston single
Gear
Retract · Retract
Beechcraft Bonanza 36 / A36 / G36Cessna 210M/N Centurion II (1977-1984)
Cruise speedKTAS
176
171
Stall speed (Vs0)lower is betterKIAS
58
57
Rangenm
920
855
Useful loadlbs
1,315
1,606
Full-fuel payloadlbs
835
1,072
Service ceilingft
18.5k
15.5k
Fuel burnlower is bettergph
15
15.8
Cruise MPGmpg
13.5
12.5
Typical pricelower is betterUSD
$280k
$160k

Beechcraft Bonanza 36 / A36 / G36

**This page's specifications describe one airplane: the 300 hp Continental IO-550-B A36**, serials **E-1946, E-2104 and E-2111 through E-3635** — 1,526 of 3,450 A36 serials, built from 1984 to 2005. It is the largest single block on the certificate, and the only one with both a freely available handbook and a manufacturer's specification sheet. The 285 hp IO-520 airplanes that came before it are in the variants table with their own figures, and everything on this page that differs between them says so.

  • +Six-seat capacity with double cargo doors — most versatile single-engine piston aircraft
  • +176 KTAS cruise speed with 920 nm range — genuine cross-country performance
  • +Excellent parts availability and mechanic familiarity — still in production as G36
  • !Spar carry-through cracks are the single most significant structural concern for A36 models
  • !Higher annual operating costs ($20k–$30k/year) and expensive overhauls limit affordability
  • !Aging fuel cell bladders and landing gear actuators on mid-to-high-time airframes require planned replacement
See the full Bonanza 36 profile →

Cessna 210M/N Centurion II (1977-1984)

> **The specifications on this page describe the Model 210N** (1979-1984), > which is 1,943 of the 3,325 serials in Sections XIV and XVI of FAA TCDS 3A21 — > 58%. That is a thin majority and it is said out loud: the 1977-1978 210M is a > Variants-table row with its own figures, and on one limit — maximum structural > cruising speed — the 210M is actually the **higher** of the two, so this page > is not quietly flattering the variant it describes.

  • +Electric gear system dramatically more reliable than pre-1977 engine-driven design (60-70% reduction in gear squawks)
  • +210N (1979+) deleted problematic gear doors, eliminating major failure points
  • +Mature, final-production normally aspirated Centurion with proven design
  • !1977-1978 models (210M) retain gear doors with chronic valve and actuator problems
  • !IO-520-L engine prone to cylinder cracking; borescope inspection essential
  • !Airframe age (40-49 years old); SID compliance a significant cost item
See the full 210N profile →

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