Cessna 177 Cardinal

The Cessna 177 Cardinal is a four-seat, single-engine high-wing aircraft produced from 1968 to 1978. The fixed-gear line (177/177A/177B) totals approximately 2,752 airframes; a further 1,543 retractable-gear 177RGs were built between 1971 and 1978 on a separate certificate and are covered on their own page. It was designed as a modern replacement for the Cessna 172, featuring a cantilever wing (no struts), an all-flying stabilator instead of a conventional elevator/stabilizer, wide cabin doors, and a more contemporary appearance.

The Cardinal's story is one of Cessna's great what-ifs. Intended to retire the 172, it was torpedoed by early handling problems (pilot-induced oscillation from the stabilator), Cessna's own Marketing Division fighting to keep the best-selling 172 in production, and a cantilever wing that cost significantly more to manufacture. The 172 never retired, and the Cardinal — after significant improvements that resolved its early problems — ended up competing against the very airplane it was supposed to replace. The Cardinal lost.

Today the fixed-gear 177B is a rewarding cross-country touring airplane with a wider cabin, better visibility, and more modern feel than a 172, often available at similar or lower prices. See the 177RG page for the 200 HP retractable, a materially different airplane on a different certificate.

The Cardinal Flyers Online (cardinalflyers.com) community is one of the strongest type clubs in general aviation, providing excellent technical support, parts sourcing, and collective knowledge for both fixed-gear and RG models.

Figures are FAA TCDS A13CE Rev. 32's own per-section numbers (see data/vault/raw/tcds/cert-cessna177fixed-a13ce-rev32-2026-09-08.md). The 177RG (200 HP retractable, TCDS A20CE, 1,543 built) is covered on its own page, Cessna 177RG Cardinal RG.

Critical note on the original 1968 177: The first-year Cardinal with its 150 HP O-320 engine was genuinely underpowered and suffered from stabilator-induced porpoising during landing flare. Cessna's response, Operation "Cardinal Rule," involved 23 inspection and modification instructions including slotted stabilator leading edges and full counterbalance weights. All post-1968 Cardinals should have these modifications incorporated. Any 1968 model that has not been modified should be avoided.

Sourced from the 1975 Owner's Manual, cross-checked against the type certificate on maximum weight (2,500 lb) before transcribing anything.

Cruise: 123 KTAS at exactly 75% power, 2,500 ft (Figure 6-4, 2300 RPM, 24 in.Hg) — a clean match to the house 75% reference setting. Burn at this setting is 10.0 GPH and range is 600 NM on the standard 49-gal-usable tanks — this is the chart's own NO-RESERVE figure, so plan a real reserve on top of it. No economy row is stored: the neighbouring rows could not be read with confidence at the available scan resolution.

Climb: 840 FPM at sea level, 2,500 lb (Figure 6-3) — unchanged from the prior pass, now sourced. Vy 80 KIAS at sea level. Vx is not published as a distinct figure in the sections read this pass.

Runway: 750 ft ground roll / 1,400 ft over a 50-ft obstacle for takeoff (sea level, standard day, gross weight, flaps 15). This is a real correction from the prior page's unsourced 890/1,585 ft. Landing distance was not found this pass — no landing chart was read in the time available, and the page's 640/1,350 ft figures are carried over unsourced rather than dropped.

Stall speeds: Vs1 (flaps up) 55 KIAS, Vs0 (flaps 30 deg) 46 KIAS, gross weight, power off, aft CG (Figure 6-2), labelled "MPH CAS" on the chart and converted by exact arithmetic.

The stabilator provides noticeably crisper pitch response than the 172's conventional elevator, particularly in the landing flare. This is an advantage for experienced pilots but contributed to the porpoising problems that plagued early Cardinals in the hands of transitioning 172 pilots. Post-modification, the stabilator is well-harmonized and a genuine pleasure to fly.

The Cardinal's wide cabin and large doors make loading significantly easier than a 172. The fixed-gear 177B has payload-range characteristics broadly similar to a 172 with the same engine, which is expected. Where the Cardinal gains is in cabin comfort during long flights — the wider cabin and better door access make the same payload feel less cramped. See the 177RG page for the retractable's materially different payload-range profile (60 gal standard, 2,800 lb gross).

• Flight Training (5): The Cardinal's stabilator and wider cabin are fine for training, but it is not a standard training platform. Flight schools chose the 172 because it is cheaper to operate and has more forgiving handling. Not a bad trainer, just not the optimal one.
• Backcountry (3): Fixed gear and high wing are appropriate, but the Cardinal was designed as a touring airplane, not a utility aircraft. No meaningful STOL capability. Ground clearance is adequate.
• Business Travel (5): Moderate speed for business use.
• Aerobatics (1): Not certified for aerobatic flight.
• Cross-Country (7): This is the Cardinal's core mission. The wide, comfortable cabin, stable IFR platform characteristics, and good range make it an excellent cross-country touring airplane.
• Cargo Hauling (4): Useful load is adequate at roughly 1,005 lbs. The wide doors are a genuine advantage for loading awkward items — they open fully to expose the entire cabin width, unlike the 172's narrower door.
• Local Fun (7): The Cardinal is a genuinely enjoyable airplane to fly. The cantilever wing looks clean and modern, the stabilator is responsive, and the wide cabin with its panoramic windows makes every flight feel special.
• Surveying (6): High wing with no struts obstructing downward visibility. The cantilever wing is a significant advantage for aerial observation compared to a strut-braced 172.

The Cardinal's panel is wider than a 172's and accommodates modern avionics installations easily.

• Budget ($50K-$70K): Steam gauges, basic IFR with older GPS (GNS 430 non-WAAS or KLN-94). Functional but dated.
• Mid-range ($70K-$110K): Garmin GNS 430W or GTN 650, KAP 140 or S-TEC autopilot, ADS-B. Solid IFR platform.
• Premium ($110K-$150K): G500 TXi or Aspen PFD, GTN 750, GFC 500 autopilot, full glass. These aircraft command strong premiums.

See Avionics Pricing Reference for current equipment and installation costs.

The Cardinal's cantilever wing limits the STOL modifications available compared to strut-braced Cessnas — there is no wing strut to mount STOL fences on, for example. Speed modifications are the most popular upgrades.

• Parts availability: Good. The Cardinal shares many components with the broader Cessna single-engine line. Cardinal-specific parts (stabilator components, cantilever wing fittings, wide door hinges) are available through normal channels and the Cardinal Flyers Online parts network.
• Mechanic familiarity: Common. Most Cessna-experienced A&Ps can work on Cardinals, though the stabilator system benefits from type-specific knowledge.
• Annual inspection cost: $2,000-$3,500. The stabilator inspection adds time compared to a standard 172 annual.
• Engine overhaul: National specialty-shop pricing for the O-360 family is $45,000 (see reference/engine-overhaul-pricing.md); a local shop reusing serviceable cylinders runs 30-50% under.
• Expensive maintenance items: Fuel bladder replacement ($3,000-$5,000 per side), stabilator rebalancing after paint ($1,500-$2,500), nose gear shimmy dampener overhaul ($800-$1,500).

Cardinal Flyers Online (cardinalflyers.com) is an essential resource for Cardinal owners. See Maintenance Ecosystem for general context.

The fixed-gear Cardinal has historically traded at a discount to comparable 172s, despite being arguably a better airplane. This discount stems from the Cardinal's early reputation for handling problems (long since resolved), lower production numbers (smaller parts and knowledge base), and the 172's overwhelming brand dominance.

These bands are unsourced generated figures, not a Vref/Bluebook pull. A dedicated pricing pass (runbook rule 27) was not performed this session. Cardinal Flyers Online membership and complete logbooks command premiums due to the confidence they provide in maintenance quality.

Stabilator AD History

The stabilator is the Cardinal's most important AD topic. The original 1968 design was prone to pilot-induced oscillation during landing flare, prompting Cessna's Operation "Cardinal Rule" — a comprehensive modification program including slotted stabilator leading edges, full counterbalance weights, and trim tab modifications. These modifications were mandated by AD and are incorporated in all post-1968 production. Any 177 or 177A without documented completion of the Cardinal Rule modifications is a red flag.

Additional ADs and Common Problems

• AD 77-13-22: Stabilator trim tab bolt inspection and replacement. Recurring inspection for bolt security.
• AD 84-10-01: Fuel system vent line inspection. Applies broadly to Cessna singles.
• Stabilator balance: The stabilator must be precisely balanced. Any paint, filler, or modification that alters the balance can cause flutter. Repainting the stabilator requires rebalancing — this is a non-negotiable safety item.
• Nose gear shimmy: A common nuisance. The nose gear shimmy dampener requires periodic service.
• Fuel bladder leaks: The rubber fuel bladders in the wet wing can develop leaks with age. Bladder replacement is a $3,000-$5,000 job per side.

Pre-Buy Priorities

1. Stabilator: Verify all Cardinal Rule modifications are documented and incorporated. Check balance, hinge bearings, and trim tab security.
2. Wing spar carry-through: Standard Cessna single spar inspection for corrosion.
3. Nose gear shimmy dampener condition and truss for fatigue cracks.
4. Fuel bladder condition (age, evidence of seepage).

Standard fixed-gear insurance category. Premiums are comparable to a Cessna 172 — expect $1,200-$1,800 annually for a private pilot with 200+ hours. The stabilator and cantilever wing do not trigger any special underwriting concerns for post-1968 models. See GA Insurance Underwriting for category details.