scramjet
10th Mar 2003, 08:34
Take Off Distance Req'd?
Before the CASA flight manuals were thrown away and we were required to use the original manufacturers handbook, we were required to use charts that were factored by the appropriate amount. Now that we are using the manufacturers hand books again we have to do the factoring ourselves. The trouble is from the following CAO excerpts it would appear as though there is a reduced requirement for RPT ops in the same aircraft then there is for Charter? This to my way of thinking fly's in the face of the idea that RPT has more stringent requirements than Charter.
For example If I am fly to a particular desitination in my Piper Navajo on a RPT flight then I only have to use the manufacturers figures. But If I finish the RPT and then get a charter to the same destination then I have to Factor the "P" Charts and possibly require a reduced take off weight then I had only a few hours before. Am I missing something here? Surely there has got to be some other legislation hiding somewhere that explains this situation?
AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS –
AEROPLANES NOT ABOVE 5700 KG — PRIVATE, AERIAL WORK
(EXCLUDING AGRICULTURAL) AND CHARTER OPERATIONS
CAO 20.7.4
6 TAKE-OFF DISTANCE REQUIRED
6.1 Subject to paragraph 6.3, the take-off distance required is the distance to
accelerate from a standing start with all engines operating and to achieve takeoff
safety speed at a height of 50 feet above the take-off surface, multiplied by
the following factors:
(a) 1.15 for aeroplanes with maximum take-off weights of 2000 kg or less;
(b) 1.25 for aeroplanes with maximum take-off weights of 3500 kg or greater;
or
(c) for aeroplanes with maximum take-off weights between 2000 kg and 3500
kg, a factor derived by linear interpolation between 1.15 and 1.25
according to the maximum take-off weight of the aeroplane.
AEROPLANE WEIGHT AND PERFORMANCE
LIMITATIONS — MULTI-ENGINE
AEROPLANES NOT ABOVE 5700KG –
REGULAR PUBLIC TRANSPORT OPERATIONS
CAO 20.7.2
3 TAKE-OFF PERFORMANCE LIMITATIONS
3.1 No aeroplane shall take off at a weight in excess of the take-off weight
specified in the aeroplane flight manual for the take-off distance available.
In determining this weight, account shall be taken of the aerodrome pressure
altitude, ambient temperature, runway surface and slope, and the wind
velocity at the time of take-off.
Before the CASA flight manuals were thrown away and we were required to use the original manufacturers handbook, we were required to use charts that were factored by the appropriate amount. Now that we are using the manufacturers hand books again we have to do the factoring ourselves. The trouble is from the following CAO excerpts it would appear as though there is a reduced requirement for RPT ops in the same aircraft then there is for Charter? This to my way of thinking fly's in the face of the idea that RPT has more stringent requirements than Charter.
For example If I am fly to a particular desitination in my Piper Navajo on a RPT flight then I only have to use the manufacturers figures. But If I finish the RPT and then get a charter to the same destination then I have to Factor the "P" Charts and possibly require a reduced take off weight then I had only a few hours before. Am I missing something here? Surely there has got to be some other legislation hiding somewhere that explains this situation?
AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS –
AEROPLANES NOT ABOVE 5700 KG — PRIVATE, AERIAL WORK
(EXCLUDING AGRICULTURAL) AND CHARTER OPERATIONS
CAO 20.7.4
6 TAKE-OFF DISTANCE REQUIRED
6.1 Subject to paragraph 6.3, the take-off distance required is the distance to
accelerate from a standing start with all engines operating and to achieve takeoff
safety speed at a height of 50 feet above the take-off surface, multiplied by
the following factors:
(a) 1.15 for aeroplanes with maximum take-off weights of 2000 kg or less;
(b) 1.25 for aeroplanes with maximum take-off weights of 3500 kg or greater;
or
(c) for aeroplanes with maximum take-off weights between 2000 kg and 3500
kg, a factor derived by linear interpolation between 1.15 and 1.25
according to the maximum take-off weight of the aeroplane.
AEROPLANE WEIGHT AND PERFORMANCE
LIMITATIONS — MULTI-ENGINE
AEROPLANES NOT ABOVE 5700KG –
REGULAR PUBLIC TRANSPORT OPERATIONS
CAO 20.7.2
3 TAKE-OFF PERFORMANCE LIMITATIONS
3.1 No aeroplane shall take off at a weight in excess of the take-off weight
specified in the aeroplane flight manual for the take-off distance available.
In determining this weight, account shall be taken of the aerodrome pressure
altitude, ambient temperature, runway surface and slope, and the wind
velocity at the time of take-off.