Beechcraft Bonanza 35 Series, D-1 to D-10119 OEM Shop Manual (P/N 35-590096B19)
471 Pages • 20.78 MB • Instant, Printable PDF
Beechcraft Models Covered & Key Technical Specifications
Models: Bonanza 35 Series (Serials D-1 through D-10119, except D-10097)
Sub-models / Variants: 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, V35TC
Model Years: 1947–1996 (1947, 1948, 1949, 1950, 1951, 1952, 1953, 1954, 1955, 1956, 1957, 1958, 1959, 1960, 1961, 1962, 1963, 1964, 1965, 1965, 1967, 1968, 1969, 1970, 1971, 1972, 1973, 1974, 1975, 1976, 1977, 1978, 1979, 1980, 1981, 1982, 1983, 1984, 1985, 1986, 1987, 1988, 1989, 1990, 1991, 1992, 1993, 1994, 1995, 1996)
Serial Numbers: D-1 through D-10119 (excluding D-10097)
Technical Data:
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Engine Displacement: 185 to 520 cu in
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Manifold Pressure: 32.5 inches Hg maximum
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Landing Gear Retraction Speed: 80 to 90 mph
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Oil System Capacity: 2.5 gallons (early models), 9 to 12 quarts (D-4866 and after)
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Flap Travel: 20 to 35 degrees
Beechcraft Manual Features & Content Preview
- Covers the Beechcraft Bonanza 35 Series from 1947–1996, including all variants from serial D-1 through D-10119 (excluding D-10097).
- Official Beechcraft publication P/N 35-590096B19, revised through March 1996.
- Features 8 comprehensive sections, including electrical wiring diagrams, periodic inspection schedules, and component replacement charts.
- Represents the final factory update for the 35 Series, incorporating vital engine overhaul schedules for Teledyne Continental Motors variants.
- Explores complex systems including turbochargers, evaporative air conditioning, shimmy dampeners, Goodyear brakes, and electric propeller deicers.
- Details New-Matic autopilot tuning, bladder fuel cell replacement, and Grimes strobe light troubleshooting.
Documented Maintenance Scope
This comprehensive 471-page PDF resource provides the exact factory specifications required for routine servicing, repair work, and major overhauls. Utilizing this data directly on a shop tablet allows mechanics to cross-reference dimensions and tolerances right at the airframe, significantly streamlining daily workflow on the hangar floor. It details airframe systems, fuel cell configurations, flight controls, and landing gear mechanisms for models ranging from the original 35 through the V35B. Mechanics can quickly reference precise control surface rigging parameters for ailerons, elevators, and the rudder, ensuring accurate alignments. By supplying step-by-step diagnostic procedures for tasks that typically require a specialized aviation facility—such as rebuilding master cylinders, overhauling shimmy dampeners, timing magnetos, and bleeding the dual brake system—the manual allows you to safely fix complex issues.
Technical Data Preview
The documentation breaks down crucial daily operational requirements. You will find complete lubrication charts, targeted tire inflation pressures, and landing gear strut requirements tailored to various series configurations. To further assist with system analysis, the text provides specialized visual aids such as Fuselage and Empennage Skin Plating diagrams, Cable Temperature-Tension graphs, the Electrical Utilization Load Chart, the Nipple Clamp Torque Chart, and the Turbocharger System Schematic. Fuel cell capacities (20 to 40 gallons) and usable fuel ratings are clearly mapped by specific serial ranges.
When tackling a complex repair, knowing the model-specific pitfalls is essential. For instance, when servicing the V-tail assembly, mechanics must be aware of the strict ruddervator balancing tolerances; failing to maintain the static moment within the precise limits after painting can induce severe airframe vibration. Furthermore, accidentally operating the landing gear electrically while the emergency handcrank is still engaged will cause catastrophic damage to the worm shaft engagement slot.
The included technical data covers critical tolerances, such as intake valve clearances (0.11–0.20 mm), coolant system capacities (2.73 liters), and magneto pick-up coil resistance (450–650 ohms). Because aviation maintenance demands absolute precision, the included specifications serve as the definitive baseline for safe flight operations. All hands-on work and adjustments must be performed by qualified personnel directly referencing this original OEM data. Learn more about the technical structure of the airframe, engine, and electrical systems.
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