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Gulfstream 100 > Limitations > Flashcards

Limitations Flashcards

1
Q

BAGGAGE COMPARTMENT CAPACITY:
Maximum w/o fuel extension tanks -
With fuel extension tanks -
Floor Loading -

A
  • 1100 lbs
  • 370 lbs
  • 105 lbs / sf
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2
Q 
MAXIMUM CERTIFICATED WEIGHTS:
ZFW -
Landing - 
Takeoff - 
Ramp -
A
  • 17,000 lbs
  • 20,700 lbs
  • 24,650 lbs
  • 24,800 lbs
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3
Q

FUEL TANK CAPACITY:
W/O extension tanks -
With extension tanks -
Maximum lateral fuel unbalance -

A
  • 1,297 gallons (8,692 lbs)
  • 1397 gallons (9,365 lbs)
  • 800 lbs
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4
Q

MAXIMUM N1 and N2:
Transient -
Overspeed -
Prior to Shutdown -

A
  • N1 - 100 to 100.5% for 10 sec, N2 101 to 102.5% for 10 sec
  • N1 - 100.5%, N2 102.5% (log overspeed duration in logbook)
  • Operate 2 minutes at 38% or below before shutdown (including taxi time)
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5
Q 
MAXIMUM ITT:
Starting -
Takeoff -
Takeoff with APR activated -
Continuous -
Climb (recommended)
Cruise (recommended)
A
  • 991 C
  • 991
  • 1013 for 5 minutes maximum
  • 974
  • 949
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6
Q 
OIL PRESSURE (AT NORMAL OPERATING TEMP):
Start -
Idle -
Takeoff, Climb, Cruise -
Transient -
A
  • Indication within 10 sec after light off
  • 50 psi minimum
  • 65-80 psi
  • 100 psi max for 3 min
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7
Q

OIL TEMPERATURE:
Up to 30,000 ft -
Above 30,000 ft -
Transient -

A
  • 30 to 127 C
  • 30 to 140 C
  • 149 C for 2 min at any altitude
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8
Q 
START TIMES:
Light-off (from initial fuel flow) -
From light-off to idle -
Starter-assist air starts (from initial FF to 60% N2 -
Windmilling air start -
A
  • 10 sec max
  • 60 sec max
  • 45 sec max
  • No time limit
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9
Q 
APU LIMITS:
Maximum altitude for operation -
Maximum altitude for start -
Not approved for \_\_\_\_\_\_\_ operations 
How much time must be allowed between shut-down and the next start -
Do not operated APU if -
A
  • 30,000’
  • 20,000’
  • Unattended
  • 5 min
  • the right FUEL PRESS light is ON
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10
Q

MAXIMUM NORMAL OPERATION SPEEDS (VMO/MMO):
Autopilot Engaged or Mach Trim operative -
Autopilot Disengaged and Mach Trim inoperative -

A
  • Below 27,600 - 353 KIAS, Above .875 M

- Below 23,900 - 353 KIAS, Above .816 M

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11
Q 
MANEUVERING SPEEDS (Va)
24,650 -
22,000 -
20,000 -
18,000 -
16,000 -
14,000 -
A
  • 236 KIAS
  • 228
  • 218
  • 207
  • 195
  • 183
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12
Q 
MAXIMUM SPEEDS
Slats -
Flaps 12 -
Flaps 20 -
Flaps 40 -
Landing Gear -
ALTN Extension -
Tire Speed - 
Vmca /Vmcg -
A
  • 250 KIAS
  • 250
  • 225
  • 180
  • 180 Vlo ext, ret and Vle
  • 160 or less
  • 182
  • 100
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13
Q

PROHIBITED MANEUVERS AND OPERATIONS
Prohibited Maneuvers -
Do not takeoff -
Do not extend SLATS, FLAPS or LANDING GEAR -

A
  • No aerobatic maneuvers and spins
  • With any stabilizer trim inoperative
  • Above 20,000 feet
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14
Q 
MAXIMUM APPROVED OPERATING ALTITUDES:
Enroute -
Autopilot and Y/D inoperative -
Cabin Door light or defect -
Takeoff and Landing -
A
  • FL450
  • FL310
  • FL410
  • minus 2,000 to 14,000
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15
Q 
OPERATING PERFORMANCE LIMITATIONS (Takeoff and Landing):
Ambient Temperature (On Ground) -
Runway Slope -
Tailwind Component -
Demonstrated Crosswind Component -
A
  • minus 54 to ISA+35 degrees C
  • +/- 2%
  • 10 Knots
  • 22 Knots
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16
Q 
THRUST REVERSER LIMITS:
Maximum N1 for Reverse Thrust  -
Do not exceed Idle Deploy position -
Do not Deploy T/R for more than -
Thrust Reverser ARM switch must be OFF -
A
  • 70% N1 (DEEC normally controls)
  • Below 70 KIAS or with a T/R UNSAFE light illuminated
  • 1 min in a 15 min period
  • Prior to 180 KIAS
17
Q

HYDRAULIC SYSTEM LIMITATIONS:

Preferred Fluid -

A
  • SKYDROL LD 4
18
Q

ENVIRONMENTAL CONTROL SYSTEM LIMITATIONS:

Max Cabin Differential Pressure -

A
  • 9.0 psid
19
Q

ANTI-ICE SYSTEM LIMITATIONS:
Ground -
InFlight (Engine Anti-Ice) -
InFlight (De-Ice Systems) -

A
  • Engine Anti-Ice systems must be ON when icing conditions exist. OAT is 10 degrees C or less and Visible Moisture in any form is present
  • Initiate Continuous IGNITION prior to turning ON NAC Anti-Ice
  • Engine Anti-Ice must be ON when icing conditions are imminent. TAT below 10 degrees C (or SAT below 5 degrees C if TAT is inoperative) and visible moisture in any form is present
  • Activate Windshield HEAT only after recognition of ice
  • Do not operate BOOTS below minus 40 degrees C
20
Q 
ELECTRICAL SYSTEM LIMITATIONS:
Engine Generator Load -
Clearing Engine -
Minimum Battery Voltage -
Aircraft with NO APU -
DO NOT Takeoff if -
A
  • 300 amps Ground or Flight
  • Starter: 15 sec ON / 2 min OFF, 15 sec ON / 2min OFF, 15 sec ON / 20 min OFF
  • With STBY FUEL PUMPS ON and DEEC’s in AUTO:
    Above 0 degrees C - 24 V / Equal to or below 0 degrees C - 23 V
  • Have a 36 amp/hr battery and the minimum voltage must be accomplished with the TAXI lights ON also
  • Battery Temperature exceeds 140 degrees F
21
Q

LONGITUDINAL TRIM SYSTEM LIMITS:

Takeoff is PROHIBITED -

A

With either NORMAL, OVRRD or EMER trim systems inoperative

22
Q

AUTOPILOT ENGAGEMENT OPERATIONS:
On Takeoff -
On Landing -
During Flight -

A
  • Do not engage below 500 feet AGL
  • Should be disengaged by 80 feet AGL
  • One pilot must be seated at the controls with his/her seatbelt fastened

Gulfstream 100 (19 decks)

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