You can't get more unequivocal than this
From the POH
2.8.4.4 CK FLAPS Caution Display. The CK FLAPS DDI caution is displayed at takeoff when the
FLAP switch is in AUTO.
2.10.1.3 Weight-On-Wheels (WOW) System. Numerous aircraft systems function differently
depending upon whether the aircraft is on the ground or is airborne. The most important of these
functions include: various flight control laws, landing gear operation, master arm and stores jettison,
fuel dump operation, AOA HUD indexers and approach lights, Automatic Throttle Control (ATC) and
autopilot operation, pitot static, AOA and total temperature probe heating, fuel tank pressurization,
and the inflight IDLE and afterburner lockout throttle stops. To determine when the aircraft is on the
ground, a proximity switch on each gear indicates when there is weight on each of the wheels. There
are a variety of failure conditions which may result in false indications of WOW or weight off wheels.
These include: a misrigged landing gear WOW proximity switch, a WOW proximity switch failure, an
improperly serviced landing gear strut, a landing gear control unit failure, or a problem with the
aircraft wiring.
An uncommanded pitch up after takeoff may occur if a WOW system
failure results in the aircraft sensing weight on wheels while inflight.
The first indication of the aircraft sensing WOW while inflight is the inability to raise the landing
gear handle. Other possible indications include the CHECK TRIM caution, NWS on the HUD, and the
CK FLAPS caution if the FLAP switch is moved to AUTO. The aircraft may then quickly undergo an uncommanded pitch up which is caused by the large stabilator deflection present at takeoff. Normally,the stabilator deflection would be trimmed out automatically by the flight control system. As airspeedincreases, the uncommanded pitch up rate increases. Maintaining airspeed as slow as practical helpscontrol nose pitch up and assists in lowering the aircraft’s nose. Above 180 knots, full forward stickalone does not stop aircraft nose up rotation, so nose down trim is required to regain control of theaircraft. The FLAP switch should also remain in HALF since the pitch up rate increases if the FLAPswitch is moved to AUTO.