User manual

Part B Section 1.2
Stichting Catalina PH-PBY Rev No: 01
25 May, 2005 Page: 1
1.2 FLYING LIMITATIONS
01 GENERAL
The aircraft is designed for duty as a general reconnaissance flying boat. Intentional
spinning and aerobatics are prohibited. All flying must be In accordance with STICAT rules
and procedures.
02 ENGINE LIMITATIONS
Refer to engine operational charts In Section 5.1
03 WAVE HEIGHT LIMITATION
Two feet maximum
04 WEIGHT LIMITS
Take-off
Landing
11999 kg (26458 lbs)
11999 kg (26458 lbs)
05 C OF G LIMITATIONS 11999 KG (26458 IBS) AUW
Forward CG.limit
Aft C.G.limit
Datum
22.9% MAC (242.2.ins)
28.5% MAC (251.5 ins)
3 inches aft of the bow nose
06 LOAD FACTOR LIMITATIONS
26458 lbs AUW
26458 lbs
26000lbs
2.9+ve accel, 1.5-ve accel, at 106 kts 175 kts
max speed
3.0+ve accel, 1.5-ve accel, at 106 kts 182 kts
max speed
3.2+ve accel, 1.6-ve accel, at 106 kts 190 kts
max speed
07 MAXIMUM PASENGERS
Cabin arrangements Allows for 8 seats in Forward and 8 seats in Aft Compartment. One
seat is dedicated cabin crew seat. Maximum passengers allowed 15.
08 MAXIMUM PASSENGERS IN BLISTER
During Take-Off and Landing the maximum number of persons in the blister area is one.
(1). This person. Is to be a crewmember strapped securely into the side (Inboard) facing
seat.
At other times during normal flight the number of persons in the blister area is to be limited
to four (4).