Term
| Air Con, Normal Maximum Differential Pressure |
|
Definition
|
|
Term
| Air Con, Maximum Relief Valve Differential Pressure |
|
Definition
|
|
Term
| Cabin Pressure Rate Controller, Descent. |
|
Definition
|
|
Term
| Cabin Pressure Rate Controler, Climb |
|
Definition
| Min 100 FPM, Max 2000 FPM |
|
|
Term
| Annunciator light-CABIN ALT (RED) comes on |
|
Definition
|
|
Term
| Air Con. Supply Air Pressure Max. Regulating, engine supply. |
|
Definition
|
|
Term
| Air Con. Supply Air Pressure Max. Regulating. APU with engine in IDLE supply |
|
Definition
|
|
Term
| Air Con, HP Bleed Regulating |
|
Definition
|
|
Term
| Minimum Ice Protection Pressure |
|
Definition
|
|
Term
| Wing landing light motors should be allowed to cool after initial extension or retraction for |
|
Definition
|
|
Term
| Wing landing light motor should be allowed to cool after initial cycle each subsequent extension or retraction for |
|
Definition
|
|
Term
| Lamps should not be operated in still, ambient air for periods of over.....minutes |
|
Definition
|
|
Term
| To prevent overheating stairway actuators, allow minimum of ... minutes between each cycle |
|
Definition
| 3 minutes, and maximum of 6 cycles in any 18 minutes periods, allow 45 minutes between periods. |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| APU Maximum Rated continuous Load. EGT is |
|
Definition
|
|
Term
| APU Maximum Allowable transient Load. EGT is |
|
Definition
|
|
Term
| APU starter motor duty cycle |
|
Definition
One attempt followed by 5 min off (first)
One attempt followed by 5 min off (second)
One attempt followed by 60 min off (third)
|
|
|
Term
| APU operation is restricted to altitudes of ... feet (MSL) and below |
|
Definition
|
|
Term
| Maximum airspeed with an inoperative Mach trim compensator is |
|
Definition
|
|
Term
| The Honeywell Windshear Detection and Recovery Guidance System (WSS) is desensitized and alerts resulting from encountering windshear conditions will be delayed if the sustained banks grater than ... |
|
Definition
|
|
Term
| The maximum difference betweenthe two indications on DC Loadmeters (One DC Loadmeter has two arrow) should not exceed... |
|
Definition
|
|
Term
| Min and Max Allowable load on DC Loadmeters are |
|
Definition
|
|
Term
| Normal DC Bus voltage is ... |
|
Definition
|
|
Term
| Max Allowable DC Bus voltage is ... |
|
Definition
|
|
Term
| Normal AC Bus voltage is ... |
|
Definition
|
|
Term
| Max Allowable AC Bus voltage is ... |
|
Definition
|
|
Term
| Normal Engine AC Generator Friquency is ... |
|
Definition
|
|
Term
| Max Allowable Engine AC Generator Friquency is ... |
|
Definition
|
|
Term
| APU Generator Frequency is |
|
Definition
normal 400 -10+20
max 400±20 |
|
|
Term
| External Power is normal if the voltage is ... |
|
Definition
|
|
Term
| The External Power is normal if the friquency is ... |
|
Definition
|
|
Term
| The Max Allowable voltage for the External Power is ... |
|
Definition
|
|
Term
| The Max Allowable Frequency for the External Power is ... |
|
Definition
|
|
Term
| Generator overload ratings for short time operation are ... |
|
Definition
| 1.5 for 5 min, over 1.5 for 5 sec, and 2.0 for 5 sec |
|
|
Term
| Normal and max allowable APU Generator load below 25000 feet |
|
Definition
|
|
Term
| Normal and max allowable APU Generator load above 25000 feet |
|
Definition
|
|
Term
| Normal and max Allowable APU Generator load on the ground is ... |
|
Definition
|
|
Term
| CSD yellow radial on rise temp scale (...) indicates an operating point which, when exceeded may indicate a system malfunction and should be recorded in the flight log |
|
Definition
|
|
Term
| CSD Outlet Oil Temperature MAX Normal is ... |
|
Definition
|
|
Term
| CSD Outlet Oil Temperature Max Allowable is ... |
|
Definition
|
|
Term
| Battery Voltage should not be less than .... |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max Take off thrust time limit is 5 min, Max EGT is ... |
|
Definition
|
|
Term
| Max take off time limit is 2 min. Max EGT is ... |
|
Definition
|
|
Term
| Normal take off time limit is 5 min. Max EGT is ... |
|
Definition
|
|
Term
| Normal take off time limit is 2 min. Max EGT is ... |
|
Definition
|
|
Term
| With Max Continuous thrust, Max EGT is ... |
|
Definition
|
|
Term
| During an engine start on the ground the EGT momentary can be ... |
|
Definition
| 475°C, if exceeded, engine should be shut down and inspected |
|
|
Term
| During an engine start in flight the EGT momentary can be ... |
|
Definition
| 625°C, if exceeded, engine should be shut down and inspected |
|
|
Term
| The ground start EGT limit chevron corresponding to ... |
|
Definition
|
|
Term
| During an engine ground start The EGT digits will flash when EGT exceeds ... |
|
Definition
| 450°C or EGT rises rapidly. |
|
|
Term
|
Definition
|
|
Term
| Normal oil pressure is ... |
|
Definition
|
|
Term
| Oil pressure between ... and ... psi are undesirable and should be tolerated only for completion of the flight, preferably at redused power setting. |
|
Definition
|
|
Term
| Engine operation should be avoided with oil pressure below ... |
|
Definition
|
|
Term
| Max continuous oil temperature is ... |
|
Definition
|
|
Term
| An oil temperature of 165°C is allowed for a max period of ... |
|
Definition
|
|
Term
| The ... pound max take off thrust at sea level is flat rated to 28.9°C ambient temperature |
|
Definition
|
|
Term
| The ... pound normal take off thrust at sea level is flat rated to 28.9°C ambient temperature. |
|
Definition
|
|
Term
| Max rotor speed N1 on Max Take off thrust is ... |
|
Definition
|
|
Term
| Max rotor speed N2 on Max take off thrust is ... |
|
Definition
|
|
Term
| Max rotor speed N1 on Normal take off thrust is ... |
|
Definition
|
|
Term
| Max rotor speed N2 on Normal take off thrust is ... |
|
Definition
|
|
Term
| Max rotor speed N1 on Max continuous thrust is ... |
|
Definition
|
|
Term
| Max rotor speed N2 on Max continuous thrust is ... |
|
Definition
|
|
Term
| ENG SYNC selector must be in OFF any time below ... |
|
Definition
|
|
Term
| Engine ignition duty cycle |
|
Definition
|
|
Term
| Engine starter duty STANDARD cycle |
|
Definition
90 sec on
5 min off
30 sec on
5min off
30 sec on |
|
|
Term
| Engine starter ALTERNATE duty cycle |
|
Definition
90 sec on
10 min off
60 sec on
10 min off
60 sec on |
|
|
Term
| MAX AIRSPEED sea level to 27300 feet is ... |
|
Definition
|
|
Term
| Max AIRSPEED above 27300 feet is ... |
|
Definition
|
|
Term
| Flap limit speed 0 to 13 degrees is ... |
|
Definition
|
|
Term
| Flap limit speed 15 to 20 degrees is |
|
Definition
|
|
Term
| Flap limit speed 21 to 25 degrees is ... |
|
Definition
|
|
Term
| Flap limit speed 26 to 30 degrees is ... |
|
Definition
|
|
Term
| Flap limit speed 31 to 40 degrees is ... |
|
Definition
|
|
Term
| Do not use flap settings between |
|
Definition
|
|
Term
| Slat limit speed mid position is ... |
|
Definition
|
|
Term
| Slat limit speed full extend is ... |
|
Definition
|
|
Term
| Speedbrakes may be used only in the ... flap configuration. |
|
Definition
|
|
Term
|
Definition
MD-83: 122000
MD-87: 112000 |
|
|
Term
| Engine stabilized idle indication: |
|
Definition
N2 50 to 61%
FUEL FLOW 600 to 1100 lb/hr
EGT 300° to 480°C
OIL PRESS 40 to 55 psi |
|
|
Term
| Turbulence penetration speed above 10000 feet |
|
Definition
285 knots .79 mach
275 knots .75 mach |
|
|
Term
| when will fuel level low light comes on? |
|
Definition
| Less than 2500 pounds in respective tank |
|
|
Term
|
Definition
|
|
Term
| Manual reversion rudder movement restriction |
|
Definition
|
|
Term
| Speed limit with mach trim compensator is inop |
|
Definition
|
|
Term
| Max brake temp on take off |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| No airfoil anti-ice above this temp |
|
Definition
|
|
Term
|
Definition
+6°C with visible moisture less than 3°C dewpoint spread
May be turned off at -15°C |
|
|
Term
| Landing gear max extend/extended speed |
|
Definition
|
|
Term
| Max landing gear retracting speed |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max crosswind rudder restricted |
|
Definition
|
|
Term
| Max crosswind manual rudder |
|
Definition
|
|
Term
| Max crosswind poor braking |
|
Definition
|
|
Term
| Max main fuel tanks imbalance |
|
Definition
|
|
Term
| Max take off and landing altitude |
|
Definition
| 8500 pressure altitude ±1000 |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max pneumatic pressure for cross bleed start |
|
Definition
|
|
Term
| Min pneumatic pressure for start |
|
Definition
| 36 psi ±6 psi subtract 1 psi per 1000 feet |
|
|
Term
|
Definition
|
|
Term
|
Definition
1 attempt by 5 min off (first)
1 attempt by 5 min off (second)
1 attempt by 60 min off (third) |
|
|
Term
| Max EGT before engine fuel lever on to start engine |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max discharge with emergency power on |
|
Definition
|
|
Term
|
Definition
82° with tiller
17° with rudder |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
main left/right-9100/9100 pound
center-20600 pound
auxilary f/a-3800/3800 pound |
|
|
Term
| No more than .... pound of center fuel may be used prior to transferring all auxiliary fuel to the center tank |
|
Definition
|
|
Term
| Rudder travel unrestricted light comes on |
|
Definition
|
|
Term
| Rudder travel unrestricted light comes off |
|
Definition
|
|
Term
| Engine Hydraulic pressure pumps switched to high mode |
|
Definition
|
|
Term
| Engine hydraulic pressure pumps switched to low mode |
|
Definition
|
|
Term
Trans hydraulic pump for functional check 3000 psi input from right system.
(Left engine Pump off) In left system should be |
|
Definition
|
|
Term
|
Definition
| remains below 900±100 psi for 3 sec |
|
|
Term
|
Definition
| when pressure increases above 1200 psi |
|
|
Term
| PIC/CENTR/FO Windshield Anti-ice inoperative Limits below 10000 feet |
|
Definition
|
|
Term
| PIC/CENTR/FO OUTER GLASS Craced Windshield Operating Limits below 10000 feet |
|
Definition
|
|
Term
| Airspeed limits on PIC/CENTR/FO windshield above 10000 feet |
|
Definition
| There are no airspeed limits. |
|
|
Term
| PIC/CENTR/FO INNER GLASS Cracked windshield operation limits below 10000 feet |
|
Definition
|
|
Term
| Airspeed limits on the clearview or eyebrow windshield |
|
Definition
| There are no airspeed limits. |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Horizontal stabilizer span |
|
Definition
|
|
Term
| The span between the nouse weels and the main weels. |
|
Definition
|
|
Term
Aircraft hight (include the fin)
|
|
Definition
|
|
Term
If the airplane is not in flight within ... seconds after throttles are advanced for
takeoff, the cabin depressurizes |
|
Definition
|
|
Term
| Ruder travel restricted and speed above 300Kts. The maximum available rudder movement is |
|
Definition
|
|
Term
| The maximum available rudder movement if unrestricted is |
|
Definition
|
|
Term
| If N2 tachometer is inoperative, move FUEL control lever to ON at |
|
Definition
|
|
Term
| If N2 tachometer is inoperative, release START switch at |
|
Definition
|
|
Term
| If only one hydraulic system is operaiting, the steering is restricted |
|
Definition
| 55° in the direction of the operation system and 82° in the direction of inoperative system |
|
|
Term
| Single engine operation. The initial take off pitch target is |
|
Definition
|
|
Term
| Do not fly less than ... glide path in NO FLAP/ NO SLAT APPROACH |
|
Definition
|
|
Term
AIR FOIL switch and the crossfeed valves which provide a
continuous cycle of ... minutes of wing anti-icing and ... minutes of horizontal
stabilizer de-icing. |
|
Definition
|
|
Term
Any part of the AIR FOIL automatic cycle can be overriden by means
of a manual override TAIL button which, when pushed, provides for ...
minutes of horizontal stabilizer de-icing after which a new wing/tail cycle starts.
|
|
Definition
|
|
Term
Placing the AIR FOIL anti-ice switch in OFF position with the pneumatic
crossfeed valve(s) open, causes the horizontal stabilizer de-icing cycle to be
activated for ... |
|
Definition
|
|
Term
Do not operate APU with center boost pumps on and
main boost pumps off if center tank quantity is low than
|
|
Definition
|
|
Term
Except in an emergency, do not shut down
APU by moving APU FIRE CONT switch to OFF &
AGENT ARM, BATT switch to OFF, or pulling APU
CONTROL circuit breaker, without first allowing...
|
|
Definition
| a 60-second cool-down with bleed air off. |
|
|
Term
|
Definition
|
|
Term
| When an EMERGENCY DESCENT do not exceed pitch or bank |
|
Definition
|
|
Term
fully extended slat
limit speed |
|
Definition
|
|
Term
BRAKE OVHT light illuminates when any one brake
temperature exceeds...and extinguishes when
brakes cool to ...
|
|
Definition
|
|
Term
RED LIGHT ILLUMINATED WITH
LANDING GEAR HANDLE UP
Max Airspeed is |
|
Definition
|
|
Term
| One engine out take off, the initial pitch target is |
|
Definition
|
|
