A controllability check is conducted to determine the min safe _________ to maintain during approach and landing following inflight structural damage, fuel imbalance, or differential airspeed readings. Ordinarily, the check should be conducted in the landing configuration at approx. _______ft. altitude.
Answer: airspeed; 10,000ft
If the answers is incorrect or not given, you can answer the above question in the comment box. If the answers is incorrect or not given, you can answer the above question in the comment box.