The 1982 revision incorporated lessons from a runway excursion in South America caused by improper rudder use in crosswind landing. The manual expanded its crosswind technique section: “In strong crosswind, use wing-down method. Do not use rudder alone. Crab until flare, then kick straight with aileron into wind. The F27’s high wing makes it susceptible to crosswind gusts during decrab. Be aggressive but precise.”
In 2020, the Dutch Aviation Museum digitized the complete 1982 edition of the F27 Flight Control Manual. It remains one of the most downloaded technical documents in the museum’s collection – not only by pilots but by aerospace engineers studying human-centered design. The Flight Control Manual Fokker F27 is more than a set of procedures. It is a moral document. It teaches that flight control is not about domination but about partnership – between human muscle and aerodynamic force, between written word and muscle memory, between Fokker’s engineers and the unknown pilot flying a thirty-year-old Friendship into a gravel strip at dusk. Every page whispers the same warning: the aircraft will forgive much, but not ignorance. And every page offers the same promise: if you study, practice, and respect the controls, the F27 will be your most loyal friend in the sky. Flight Control Manual Fokker F27
In the end, the manual’s most important lesson appears not in the emergency section but in the preface, in plain block letters: “THIS AIRCRAFT HAS NO FLY-BY-WIRE. YOU ARE THE WIRE. FLY ACCORDINGLY.” End of essay The 1982 revision incorporated lessons from a runway
The flight control manual opens with a bold warning: “The F27 is a manual control aircraft. At high speeds, forces rise rapidly. At low speeds, harmony changes. Do not confuse absence of power with absence of authority.” This preamble sets the tone. Unlike a Boeing or Douglas jet of the same era, the Friendship demands physical engagement. The manual immediately categorizes three flight regimes: low speed (flaps extended, approach), cruise (clean configuration), and high speed (VMO/MMO limits). Each regime imposes distinct control feel. The original Fokker F27 Flight Control Manual (document number F27-AC-001, revised 1962, 1972, 1982) is divided into six major sections, a layout that has influenced many subsequent turboprop manuals. Section 1: General Description A system schematic shows cable runs from cockpit to tail, pulley diameters, turnbuckle inspection points, and breakout forces. Notably, the manual includes a foldout color plate of the “Control Circuit Diagram” – a masterpiece of technical illustration. For each control surface, the manual lists maximum deflection, cable tension ranges (summer/winter), and rigging tolerances. Maintenance personnel and pilots are expected to understand both. Section 2: Normal Procedures This section reads like a choreography. For preflight: “Check aileron and elevator freedom. With gust locks removed, move each control slowly to full stop. Return to neutral. Listen for cable slap – none permitted.” The engine start sequence includes a “controls free and correct” callout. After takeoff, the manual prescribes a reduction in control sensitivity as speed builds: “At 140 KIAS, aileron deflection beyond 1/3 travel is rarely required. Use trim, not arm strength.” Section 3: Abnormal and Emergency Procedures Here the manual reveals its wisdom. For a jammed elevator: “Use power and trim. Pitch with throttles. Descend with flaps.” For a rudder hardover (rare, but possible due to cable jamming): “Bank into the yaw. Do not fight directly. Coordinate aileron and asymmetric power.” These are not generic airline platitudes; they are F27-specific recipes born from incident analysis. Section 4: Performance and Flight Characteristics A dense chapter of charts: stick force per G, turn coordination, adverse yaw in go-around, and the famous “Fokker Shuffle” – a slight nose-up pitch when flaps extend to 15°. The manual explains: “Flap extension changes downwash at the tail. Anticipate 2–3° nose-up. Do not trim immediately. Wait 3 seconds.” Such detailed phenomenological guidance is rare in modern fly-by-wire manuals but essential for the F27. Section 5: Weight and Balance Implications Control effectiveness degrades with aft CG. The manual dedicates ten pages to loading scenarios: “With CG aft of 32% MAC, elevator becomes light. At 34% MAC, neutral stability is approached. At 36% MAC – not permitted. Do not fly.” This section connects load planning directly to handling. Section 6: Training and Checkride Standards The final section reads like a syllabus. It outlines maneuvers: steep turns (45° bank, 170 KIAS), stalls (clean and with flaps, power off and on), engine-out control, and the “single-engine go-around” – the F27’s most demanding maneuver. A table lists allowable altitude loss during a stall recovery: “Maximum 150 ft. If more, repeat training.” Part III: The Manual’s Handling Philosophy – “Friendship, Not Autopilot” The F27 has no yaw damper. Dutch roll is damped naturally by the vertical stabilizer’s large area, but in turbulence, the pilot must actively coordinate turns. The manual states: “Step on the ball. If the ball is left, left rudder. Do not fixate. Feel the seat.” This is anachronistic advice in an era of glass cockpits, but for the F27, it is gospel. Crab until flare, then kick straight with aileron into wind