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Limits Flashcards

(64 cards)

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1
Q

MINIMUM CREW

A

TWO PILOTS

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2
Q

BAGGAGE WEIGHT LIMITS

NOSE, AFT CABIN, TAIL CONE

A

NOSE: 350 LB
AFT CABIN: 600 LB
TAILCONE: 500

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3
Q

MAX TAXI AND RAMP WEIGHT

A

16,500 LB

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4
Q

MAX TAKEOFF WEIGHT

A

16,300 LB

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5
Q

MAX LANDING WEIGHT

A

15,200 LB

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6
Q

MAX ZERO FUEL WEIGHT

A

12,200 LB

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7
Q

MAX FLAPS EXTENDED (V fe)

A

7 or 15: 200 kias
35: 173 kias

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8
Q

MAX LANDING GEAR SPEED

A

Extending (V lo): 250 KIAS
Extended (V le): 292 KIAS
Retracting (V lo): 200 KIAS

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9
Q

MINIMUM CONTROL - AIR (Vmca)

A

95 KIAS

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10
Q

MINIMUM CONTROL - GROUND (Vmcg)

A

91 KIAS

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11
Q

MAXIMUM (Vmo) BELOW 8000’

A

262

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12
Q

MAXIMUM (Vmo) 8000’ - 28907’

A

292

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13
Q

MAXIMUM (Mmo) ABOVE 28907’

A

M .755 INDICATED

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14
Q

MAXIMUM SPEED BREAK EXTENSION (Vsb)

A

NO LIMIT

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15
Q

MAX AUTOPILOT OPERATION SPEED

A

292 KIAS OR .755M

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16
Q

ENGINE N2 GROUND IDLE LIMITS

A

NORM - 46%
HIGH - 52%

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17
Q

MAX PRESS ALT FOR T/O AND LANDING

A

14,000’ PRESSURE ALTITUDE

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18
Q

MAX TEMP T/O AND LANDING

A

ISA +39 c

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19
Q

MAX CROSSWIND DEMONSTRATED

A

20 KNOTS

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20
Q

MAX TAILWIND DEMONSTRATED

A

10 KNOTS

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21
Q

MAX TIRE GROUND SPEED

A

165 KNOTS

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22
Q

MAX WATER/SLUSH

A

0.5 INCH

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23
Q

VNAV OFF BELOW

A

500’ AGL

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24
Q

MINIMUM AIR TEMPERATURE FOR T/O LANDING

A

-54 C

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25
NOSE TIRE PRESSURE
120 +- 5 PSI
26
APPROX TURB PENETRATION SPEED
180
27
MIN A/S FOR SUSTAINED ICING
160
28
MAX CALIBRATED OP ALTITUDE
FL450
29
MAX LOAD FACTOR IN FLGHT FLAPS UP / 7-35
FLAPS UP: -1.52 TO +3.8 AT 16,300 LB FLAPS 7-35: -0.0 TO +2.0 AT 16,300 LB
30
MAX LOAD FACTOR LANDING / FLAPS 15 - 35
+3.5 G AT 15,200 LB
31
MINIMUM ALTITUDE FOR AUTOPILOT USE
ENROUTE: 1,000 AGL NON-PRECISION: 300 AGL CAT 1 ILS: 180 AGL
32
NOSE AVN FAN FAIL GROUND OPS LIMIT
30 MIN or until either PDF HOT ore MFD HOT illuminates, whichever happens first
33
AC POWER SOURCES
-TWO 375VA static inverter, each converting 28V DC into 26V AC and 115V AC at 400 HZ - TWO 26V AC BUSES - TWO 115V AC BUSES
34
DC POWER SOURCES
-TWO 28.5V DC 300A starter/gens -ONE 24V DC 40A/HR NICAD OR 44A/HR SLAB
35
APPROVED MAX GEN LOAD IN FLIGHT
300A
36
BATT LIMIT FOR START
3/HR
37
STARTER LIMITS FOR ENGINE STARTS: BATTERY: GPU:
BATTERY: 3 STARTS PER 30 MIN W/90s REST GPU: 2 STARTS PER 30 MIN W/90s REST
38
VOLTAGE CONSIDERATION WHEN USING GPU FOR ENGINE START
USE OF A GPUE WITH VOLTAGE IN EXCESS OF 28V OR CURRENT IN EXCESS OF 1000A MAY DAMAGE THE STARTER
39
MAX CONTINUOUS GEN LOAD DURING GROUND OPS: GROUND IDLE: FLIGHT IDLE:
GROUND IDLE: 125A FLIGHT IDLE: 225A
40
CAN YOU EXCEED MAX GEN AMPS IN EMERGENCY?
YES, 50% ABOVE THE ALLOWABLE ( UP TO 450 AMPS) FOR 5 MINUTES
41
MAX PRESS DIFF
8.9 +- 0.1 PSID
42
A/C COMPRESSOR LIMIT
OFF ABOVE 18,000'
43
MAX FUEL IMBALANCE
NORMAL: 200LB EMERGENCY: 600LB
44
MAX FUEL CAPACITY
5814 LB / 862 US GAL
45
SINGLE POINT PRESSURE RANGE
15 TO 60 PSI
46
APPROVED HYDRAULIC FLUIDS
SKYDROL HYJET
47
AT WHAT PSI DOES THE OPEN CENTER HYDRAULIC SYSTEM CONTINUOUSLY OPERATE
60 PSI
48
WHAT PSI IS REQUIRED TO ACTIVATE THE HYDRAULIC SYSTEM
1,350 - 1500 PSI
49
LIMIT GROUND OPS OF PITOT HEAT
2 MINUTES
50
DEFINITION OF ICING CONDITIONS
VISIBLE MOISTURE (VIS OF 1 MILE OR LESS) AND BELOW 10 C
51
AT WHAT TEMPS SHOULD THE W/S BLEED AIR BE SET TO HIGH
OAT < -18 C
52
MIN SPEED FOR FLIGHT IN ICING CONDITIONS
160
53
CONTINUOUS USE OF SUPPLEMENTAL OXYGEN IS PROHIBITED ABOVE: W/ PAX: CREW ONLY:
W/PAX: 25,000' CREW ONLY: 41,000' FOR EROS, OR LOWER DEPENDING ON MASK
54
AT WHAT ALTITUDE DOES OXYGEN BECOME AUTOMATICALLY AVAILABLE TO THE CREW AND PAX?
13,500' +- 600'
55
ENGINE NOMENCLATURE
PRATT AND WHITNEY JT15D-5D
56
REVERSE THRUST MUST BE REDUCED TO IDLE REVERSE BY WHICH SPEED
60KIAS
57
MAX ALLOWED MIXING OF OILS
NO MORE THAN 2 QUARTS EVERY 400 HOURS
58
THRUST REVERSER ARE PROHIBITED:
1. DURING TOUCH AND GO LANDINGS 2. FOR BACKING THE AIRPLANE 3. ON SOD OR GRAVEL RUNWAYS
59
MAX THRUST REVERSER DEPLOYMENT SPEED
115 KIAS
60
MAX DEPLOYMENT TIME
15 MIN IN ANY 1 HOUR
61
OPERATING LIMITES FOR T/O N1 N2 ITT
N1: 100% N2: 97% ITT: 720 C
62
MAX CONTINUOUS N1 N2 ITT
N1: 100% N2: 97% ITT: 720 C
63
START ABORT TEMP
550 C
64
STATIC THRUST PRODUCED BY JT15D-5D ISA at SL?
3,045 LB THRUST

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