Model Years: 1973–1976 | Engine: Lycoming O-320-E2D | Horsepower: 150 HP
Important Disclaimer
The data below is provided for educational reference only. Always use the POH for your specific aircraft N-number and serial number for actual flight planning. Performance varies by individual aircraft condition, equipment, and environmental factors.
What the Cessna 172M POH Covers
The FAA-approved Pilot Operating Handbook for the Cessna 172M is organized into nine sections. Every section is testable on your Private Pilot checkride oral — the DPE expects you to find information quickly, not just recite numbers from memory.
- Section 1 — General: Aircraft description, three-view drawings, engine and propeller specs, and basic dimensions
- Section 2 — Limitations: Airspeed limits, engine limits, weight limits, maneuver limits, fuel and oil specs, placards
- Section 3 — Emergency Procedures: Engine failure in flight, engine fire, electrical fire, forced landing, emergency descent
- Section 4 — Normal Procedures: Preflight, engine start, runup, takeoff, climb, cruise, descent, landing, shutdown checklists
- Section 5 — Performance: Takeoff distance, climb rate, cruise performance, range, landing distance charts
- Section 6 — Weight and Balance: Loading graph, moment envelopes, sample calculations, equipment list
- Section 7 — Systems Description: Fuel, electrical, pitot-static, vacuum, flight controls, landing gear, avionics
- Section 8 — Handling and Servicing: Fueling, oil, tire pressure, towing, cleaning, storage
- Section 9 — Supplements: Approved optional equipment — COM radios, transponder, autopilot, nav systems
Limitations: What the DPE Will Test
Section 2 is the most heavily tested section on a Private Pilot checkride oral. The Designated Pilot Examiner (DPE) expects you to locate and recite limitations without hesitation. Key limitations in the 172M POH:
- Vne (163 KIAS): Never exceed — structural limit. Red line on the airspeed indicator.
- Va (97 KIAS at max gross weight): Maneuvering speed. Do not apply full or abrupt control inputs above Va. Va decreases as aircraft weight decreases — this trips up many checkride candidates.
- Vfe (100 KIAS for 10° flaps, 85 KIAS for full flaps): Max flap extension speeds. Exceeding these can cause structural damage to the flap mechanism.
- Max gross weight (2,300 lbs): Do not depart above this weight under any circumstances.
- Baggage compartment (120 lbs): Structural limit regardless of whether the CG is within limits.
- Approved fuel: 100LL (blue) or 100 octane (green). The 172M is NOT approved for automotive gasoline (mogas) without a specific STC for the individual aircraft.
- Oil: 6 quarts maximum, 4 quarts minimum for flight. SAE 30 or 40 depending on temperature.
- Approved maneuvers: The 172M is approved for normal category only — max load factor +3.8g / -1.52g. No aerobatics.
Emergency Procedures: What to Know From Memory
The FAA expects Private Pilot applicants to know emergency procedures well enough to execute them without checklist reference during an actual emergency. The POH's emergency procedures section gives you the memory items and amplified procedures. Key emergencies in the 172M:
- Engine failure during flight: Best glide speed 65 KIAS. Mixture — rich, fuel selector — both, ignition — both, throttle — full forward (if restart fails), primer — in and locked. Select emergency landing field, declare emergency if able. Fuel shutoff valve off, mixture idle cut-off, ignition off, master off, flaps as required, unlatch door before touchdown.
- Engine failure after takeoff: Pitch for best glide (65 KIAS), land straight ahead. Never attempt to return to the runway below 1,000 ft AGL.
- Engine fire during start: Crank engine to pull flames back into engine. If fire continues: mixture idle cut-off, fuel shutoff valve off, throttle full open, master switch off, evacuate.
- Electrical fire in flight: Master switch off, all avionics off, fire extinguisher if smoke persists, land as soon as possible.
- Spin recovery (PARE): Power off, Ailerons neutral, Rudder full opposite the spin, Elevator forward to break stall, recover from dive.
Weight and Balance: A Required Checkride Calculation
Every FAA checkride requires a weight and balance calculation for the planned flight. The 172M POH loading graph in Section 6 requires you to calculate the moment for each item (pilot, passengers, fuel, baggage) and plot the result on the CG envelope. Key items for the 172M:
- CG range forward limit varies with weight — consult the moment envelope, not just the forward/aft numbers
- Full fuel (38 usable gallons × 6 lbs/gal = 228 lbs) shifts CG depending on loading
- Heavy baggage with light passengers can push the CG aft of limits — check this scenario on every preflight
- The standard empty weight listed in the POH is nominal — your aircraft's actual empty weight is on the Weight and Balance data sheet in Section 6 or the aircraft records
Using POH Performance Charts
Section 5 performance charts are used for cross-country planning and are tested on the Instrument Rating and Commercial Pilot checkrides as well. Key planning concepts:
- Density altitude matters: Performance figures in the POH are for standard atmosphere (59°F / 29.92 inHg at sea level). Dallas summer temperatures routinely push density altitude 2,000–3,500 ft above field elevation — expect longer takeoff rolls and reduced climb rates.
- Pressure altitude vs. field elevation: Use pressure altitude (altimeter set to 29.92) for all chart entries, not field elevation.
- Interpolation: POH charts rarely match your exact conditions — you must interpolate between table values. DPEs watch for this on orals.
- Conservative planning: Add a 10–15% safety margin to POH performance data for actual planning — the charts assume a new aircraft, experienced pilot, and optimal technique.
Why Student Pilots Train in Glass Cockpit Aircraft Today
The Cessna 172M was the standard training aircraft at most flight schools from the 1970s through the early 2000s. Today, most professional flight training programs — including Parrish Aviation's Career Pilot Program — have transitioned to modern aircraft with Garmin G3X glass cockpits and fuel-injected engines. The underlying aerodynamics and POH literacy skills, however, remain identical. Airlines and DPEs alike expect pilots to demonstrate the ability to extract, interpret, and apply performance data from any aircraft's handbook — the skill built on the 172M transfers directly to every aircraft you will ever fly.
If you're currently working through your PPL ground school and need to drill airspeeds, limitations, or systems knowledge, call Parrish Aviation at (469) 886-8089 or book a Discovery Flight to see how structured, Part 141 ground training prepares students for checkrides.
Weights
2,300 lbs
Max Gross Weight
~1,393 lbs
Standard Empty Weight
~907 lbs
Useful Load (approx.)
Fuel
- Total capacity: 43 gallons (standard tanks)
- Usable fuel: 38 gallons (standard tanks)
- Approved fuel grades: 100LL (blue), 100 (green) — check TCDS and POH for specific aircraft
Cruise Performance (75% Power, 8,000 ft)
122 KTAS
True Airspeed
~8.5 GPH
Fuel Burn
~635 nm
Range (45 min reserve)
Takeoff Performance (Sea Level, Standard Day, Max Gross Weight)
865 ft
Ground Roll
1,525 ft
Over 50-ft Obstacle
Landing Performance (Sea Level, Standard Day)
520 ft
Ground Roll
1,250 ft
Over 50-ft Obstacle
Ceiling
14,200 ft
Service Ceiling
Key Airspeeds (172M)
| Speed | Definition | Value |
|---|---|---|
| Vne | Never Exceed | 163 KIAS |
| Vno | Max Structural Cruising | 122 KIAS |
| Va | Maneuvering (max gross) | 97 KIAS |
| Vfe | Max Flap Extension (10°) | 100 KIAS |
| Vx | Best Angle of Climb | 59 KIAS |
| Vy | Best Rate of Climb | 73 KIAS |
| Vso | Stall, Landing Config | 40 KIAS |
| Vs | Stall, Clean | 44 KIAS |
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Parrish Aviation — FAA Part 141 Flight School at Dallas Executive Airport (KRBD)
