Beechcraft Baron 58 - Page 55

BEECHCRAFT Baron 58
Serial TH 773 and After
Section II
Limitations
On Left Sidewall (58 & 58A) (Serials TH-1027, TH-1062,
TH-1067, TH-1080 and after):
---- AIRSPEED LIMITATIONS ----
MAX. LOG GEAR EXTENDED (NORMAL)
----------152 KTs
MAX. FLAPS EXTENDED (15° DOWN)
--------152 KTs
MAX. flAPS EXTENDED (NORMAL)
---------122 KTs
MAX. DESIGN MANEUVER SPEED ---156 KTs
MIN.
CONTROL SPEED SINGLE ENGINE---81 KTs
NEVER EXCEED SPEED ----------223 KTs
MAX. STRUCTURAL CRUISE SPEED ---195 KTs
On Upper Left Hand Side Panel (58) (Serials TH-1027, TH-
1062,
TH-1067, TH-1080 and after):
--------OPERATION LIMITATIONS ,
THIS AIRPLANE MUST BE OPERA TED AS A NORMAL CATEGORY AIRPLANE IN
~ COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF ~
W PLACARDS. MARKINGS, AND MANUALS. MAXIMUM WEIGHT IS 5400 LBS. W
(PILOrS CHECK L1STI
II OCCUPIED SEATS MUST BE IN UPRIGHT POSITIONFOR TAKEOFF AND LANDING. II
L!=: NO ACROBATIC MANEUVERS INCLUDING SPINS APPROVED. d
On Upper Left Hand Side Panel (58A) (Serials TH-1027,
TH-1062, TH-1067, TH-1080 and after):
rr= OPERATION LIMITATIONS ,
THIS AIRPLANE MUST BE OPERA TED AS A NORMAL CATEGORY AIRPLANE IN
~ COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF ~
W PLACARDS, MARKINGS, AND MANUALS. MAXIMUM WEIGHT IS 4990 LBS. W
(PILOT'S CHECK LIST)
II OCCUPIED SEATS MUST BE IN UPRIGHT POSITIONFOR TAKEOFF AND LANDING. II
L!=: NO ACROBATIC MANEUVERS INCLUDING SPINS APPROVED. d
AugU8t, 1984
2-13