Beechcraft Skipper 77

This page's certificate is FAA TCDS A30CE, Revision 8 — confirmed against the FAA's own model list, which names exactly one model: "77." The page previously cited A24CE, which is the King Air 200/300/1900 series — a business turboprop sheet with no connection to this two-seat trainer. The correction holds up: A30CE's own text opens "Model 77, Skipper, 2 PCLM (Utility Category), Approved March 19, 1979," matches the engine (Lycoming O-235-L2C), weights (1,675 lb takeoff/landing, 1,680 lb ramp) and every airspeed limit this page stores. There is no serial split and no sibling variant on this certificate — every production Skipper (S/N WA-3 and on) is one configuration.

The Beechcraft Skipper Model 77 was Beechcraft's late-1970s attempt to enter the two-seat trainer market against the Cessna 152 and Piper Tomahawk. Early prototypes (1975-78) had a conventional tail with a stabilator and flaperons; production airplanes (1979-1981, the only ones ever certificated under A30CE) switched to the T-tail with a conventional elevator and separate flaps/ailerons this page describes. Only 312 Skippers were produced before production ended abruptly in 1981 when Beechcraft decided the low-margin trainer market wasn't worth pursuing.

The Skipper has a unique place in GA: it's a well-built Beechcraft that no one asked for. The T-tail design was fashionable in the late 1970s (Piper used it on the Tomahawk too) but added weight and complexity without clear benefit. The O-235 engine produces 115HP — adequate for a trainer but not exciting.

Today only about 118 Skippers remain active. Rarity makes parts sourcing challenging, and the small fleet means fewer mechanics have experience with the type. For a buyer specifically seeking a Beechcraft-quality trainer at budget prices, the Skipper delivers — but the parts availability concerns are real.

The Skipper is MOSAIC eligible (Vs1 54 KIAS per the POH's own airspeed-indicator placard, max gross 1,675 lbs), which may increase interest and values as the MOSAIC rule takes full effect.

No meaningful variants exist — all 312 Skippers are essentially identical.

The reference cruise is 105 KTAS at 6,500 ft, full throttle (2700 rpm), burning 7.4 GPH — one row of the POH's own Cruise Performance table. That table gives no percent-power column at all (a fixed-pitch, normally-aspirated engine's "full throttle" is not a constant percentage as altitude changes), so cruise_percent_bhp: 75 is recorded here only because AOPA's independent fact sheet states 75%-power burn as exactly 7.4 gph — the same number, at the same setting. No other row in the table has an independent %BHP statement, so no economy (~65%) row is stored on this page.

The full published cruise grid (all altitudes and RPM settings the POH tabulates) is saved as data/vault/performance/beechcraft-skipper-77.cruise.json.

Range at that same setting is approximately 340 nm, read off the POH's Range Profile chart (29 gal, standard day/ISA) at 6,500 ft on the 2700-rpm curve — already including start/taxi/takeoff/climb and Beechcraft's own 45-minute reserve at 2300 rpm. This replaces a prior 400 nm figure that traced to no located document.

Climb rate of 720 FPM is the POH's own book value (AOPA's review explicitly attributes it to "the book"), but AOPA's own flight-test prose is blunt about it in practice: "test flights show much less, especially on warm summer days; one pilot report said to expect 500 fpm on a 50°F day." The POH's climb chart is itself published at a representative 1,600 lb weight, not the 1,675 lb max gross, and at full throttle, 65 KIAS — so a loaded, warm-day Skipper should be planned well under the placard number.

Best rate of climb (Vy) is 68 KIAS and best angle (Vx) is 61 KIAS, both from the POH's own Section IV airspeed table — corrected from this page's prior 75/62, which appeared in no located document. Best glide is 63 KIAS, from the POH's Emergency Airspeeds table (corrected from a prior 72, also undocumented).

The T-tail means the horizontal stabilizer sits above the wing wake, which provides clean airflow in cruise but can create unexpected pitch behavior in slow flight. Stall characteristics are actually quite good — plenty of pre-stall buffet through the tail warns the pilot before the break. However, the elevator authority at very low speeds is reduced compared to conventional-tail designs.

The low wing provides better ground effect than high-wing trainers, which some students find makes landing easier. Others find the reduced visibility in turns a disadvantage during pattern work.

Takeoff and landing distance are not stored on this page. The POH publishes both only as four-panel correction nomographs (pressure altitude/OAT, then weight, then wind, then obstacle height) rather than a sea-level table, and reading exact figures off a hand-drawn 1979 chart risks the row/column misreading error this catalogue has been burned by before. The POH's own worked examples, given as plain text rather than requiring a chart trace, are real reference points even though they are not at sea level:

• Takeoff (5,650 ft pressure altitude, 15°C, 1,675 lb, 9.5 kt headwind): 1,060 ft ground roll, 1,750 ft total distance over a 50-ft obstacle. Rotate 56 KIAS, 60 KIAS at 50 ft.
• Landing (1,332 ft pressure altitude, 25°C, 9.5 kt headwind): 640 ft ground roll, 1,220 ft total distance over a 50-ft obstacle, at a 63-KIAS approach.

Sea-level, zero-wind figures would be somewhat shorter than both of these on both counts — the examples are several thousand feet of density altitude above sea level.

BE-77 (O-235-L2C, 115HP, 29 gal usable fuel):

The Skipper's 575 lbs useful load (per TCDS max gross weight 1,675 lb minus the POH's 1,100 lb standard empty weight) is adequate for two average-weight adults with full fuel. Two larger adults (200+ lbs each) will be right at gross weight with full fuel and essentially no baggage. This is typical for the two-seat trainer category. Range figures are the POH's own Range Profile chart value at 6,500 ft/75% power (~340 nm), scaled proportionally for the reduced-fuel row — an approximation, since the reserve is a fixed quantity rather than a proportional one.

• Flight Training (6): Designed as a trainer and adequate for the role. Good stall characteristics with advance warning through tail buffet. However, the T-tail pitch behavior in slow flight is unusual, parts availability is a real concern for fleet operators, and the tiny fleet means limited training ecosystem. The Cessna 152 and Piper Warrior are superior training platforms simply due to parts and maintenance support.
• Backcountry (1): Low-wing, low-performance, not suitable.
• Business Travel (1): Two seats, 105 KTAS, no IFR capability. Not applicable.
• Aerobatics (1): Not aerobatic certified. Normal category only.
• Cross-Country (2): Too slow and only two seats for practical cross-country. Range of roughly 340 nm at cruise power is adequate but you'll be outpaced by almost everything.
• Cargo Hauling (1): Two seats, minimal baggage area. Not applicable.
• Local Fun Flying (5): Pleasant low-wing handling, good visibility, cheap to operate. A decent weekend recreational airplane for a pilot who wants something unique and affordable.
• Surveying (2): Too small and low-powered for practical survey work.

Most Skippers fly with basic VFR panels:

• Typical: Dual VOR, basic com radio, standard six-pack. Many are still equipped with original 1979-1981 avionics.
• Upgraded ($5K-$15K): Garmin GPS (aera or GTN 650Xi), ADS-B transponder. Limited panel space constrains options.
• IFR upgrade: Generally not worth the investment on a $38,000 aircraft, though technically possible.

The Skipper has an extremely limited STC ecosystem — one of the smallest of any certified aircraft:

• Engine upgrades: Virtually none available. The O-235 is the only approved powerplant.
• Propeller options: Limited to the original Sensenich 72CKS12-0-52 fixed-pitch propeller (per TCDS A30CE and the POH's Descriptive Data section — corrected here from a prior "McCauley," which is not the certificated propeller).
• Speed mods: Minimal aftermarket support due to tiny fleet.
• The bottom line: What you see is what you get. The Skipper is essentially unmodifiable.

• Annual inspection: $1,200-$2,500 base. Simple airframe but Skipper-specific items may require longer sourcing times.
• Parts availability: Poor. This is the critical concern. Beechcraft-specific parts for the Skipper are increasingly scarce. Generic Lycoming O-235 parts are readily available, but airframe-specific components (T-tail hardware, cowling pieces, unique fairings) may require fabrication or searching for donor aircraft.
• Mechanic familiarity: Specialist — few A&Ps have Skipper experience. The Beech Aero Club (BAC) is the best resource for connecting with knowledgeable mechanics and sourcing parts.
• Annual operating cost: $5,000-$9,000 all-in — one of the cheapest certified aircraft to operate.

Pricing was NOT independently re-verified in this research pass. A live Trade-A-Plane search returned HTTP 202 with zero bytes of content (the same bot-protection behavior noted on other pages in this catalogue), and Controller.com's keyword search does not filter results down to the Skipper specifically. The figures below are carried forward from the prior data pass unchanged, per this pass's instruction to leave existing values alone rather than replace them with an unsourced guess; they are not listed in this page's sourced: block.

• Typical range: $25,000-$50,000. Skippers are among the cheapest certified aircraft available — consistent with AOPA's own framing of the type as inexpensive to buy and to insure.
• Factors: Engine time is the primary driver. A freshly overhauled O-235 can be worth more than half the airframe value.
• MOSAIC impact: MOSAIC eligibility may increase values as sport pilot demand grows. Monitor this trend.

Key value adjusters per Aircraft Valuation Methodology:

• Engine time: Fresh overhaul adds $10,000-$15,000 vs mid-time
• Corrosion: Any significant corrosion dramatically reduces value given parts sourcing concerns
• Complete logbooks: Critical for a rare type — incomplete records are a deal-breaker

Key ADs:

• T-tail stabilizer attachment: Inspection of horizontal stabilizer mounting hardware.
• Standard Lycoming O-235 ADs: Same engine ADs as Cessna 152 and Tomahawk.
• Fuel system: Fuel line and selector valve inspections.

Common Problems:

• T-tail fatigue: The T-tail configuration puts stress on the vertical stabilizer that carries the horizontal tail. Inspection of this junction is important.
• Parts availability: With only 312 built and ~118 active, Skipper-specific parts are increasingly difficult to source. This is THE primary ownership concern.
• Nose gear shimmy: Common complaint on low-time-between-maintenance examples.
• Corrosion: Like all 1970s-80s aircraft, coastal examples need careful corrosion inspection.

Per GA Insurance Underwriting:

• Hull insurance: $400-$700/year for $25,000-$50,000 hull value. Among the cheapest GA aircraft to insure.
• Liability: Minimal premiums — $200-$400/year for standard coverage.
• Pilot minimums: Very low — student pilot certificate for dual, private pilot for solo.
• The Skipper is one of the cheapest aircraft to insure in all of GA.