Robin DR400/140B - Load Planning Guidance; Engine Operating Limits

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Issue 3 – July 2014 Page 2 - 3
LOAD PLANNING
(Refer also to weight and balance chart, section 6)
The weight of the engine oil, as well as the unusable fuel must be
included in the empty weight of the aircraft.
Weight
kg (lb)
Arm
m (in)
Front Seats
2 x 77
(2 x 170)
0.36 - 0.46
(14 - 18)
Rear Seats (*)
2 x 77
(2 x 170)
1.19
(47)
Fuel, main fuselage tank
88
(194)
1.12
(44)
Baggage (**)
40
(88)
1.9
(75)
Table 2-4 Load Planning
* The carriage on the rear seats of more than two passengers (whose
total weight remain below or equal to the maximum indicated) is
authorized, provided that passenger seat belts are installed for each
passenger and that weight and balance are kept within the authorized
limits.
** Within the authorized weight and balance limits.
ENGINE OPERATING LIMITS
Engine manufacturer ........................................... Technify Motors GmbH
Engine model .......................................... TAE 125-01 or TAE 125-02-99
Takeoff and max. continuous power .............................. 99 kw (135 HP)
Takeoff and max. continuous RPM ................................................. 2300
 Note: In the absence of any other explicit
statements, all of the information on RPM in this
supplement to the Pilot´s Operating Handbook are
propeller RPM.