AM.II.J.S13

From the FAA library

• Aircraft Weight and Balance Handbookp. 1-3
  Chapter 1: Weight and Balance Control › Weight Changes

  with tandem seating normally have a limitation requiring solo flight to be made from the front seat in some airplanes or the rear seat in others. Some of the smaller helicopters also require solo flight be made from a specific ... noted by a placard, usually on the instrument panel, and they should be strictly followed. As an aircraft ages, its weight usually increases due to debris and dirt collecting in hard-to-reach locations and moisture absorbed in the cabin…

• Aviation Maintenance Technician Handbook - Generalp. 6-11
  Chapter 6: Aircraft Weight & Balance › Weight and Balance Equipment › Scales

  certificated empty weight and corresponding center of gravity locations must include undrainable system oil (not included in oil capacity) and unusable fuel as noted below: NOTE 2 All placards required in the approved Airplane Flight Manual or Pilot's Operating…

• Aviation Maintenance Technician Handbook - Airframep. 14-16
  Chapter 14: Aircraft Fuel Systems › Aircraft Fuel Systems › Helicopter Fuel Systems

  fuel pressure warning lights are also common on jet transport aircraft. The sensors for these are located in the boost pump outlet line. They give an indication of possible boost pump failure. Fuel quantity gauges are important features ... aircraft. Indications exist for all tanks on a transport category aircraft. Often, these use a capacitance type fuel quantity indication system and a fuel totalizer as is discussed later in this chapter. The location of fuel instrumentation varies depending…