DC-9-83 / JT8D-219
Checklist / Weight Specification / Aircraft Performance
NORMAL PROCEDURES CHECKLIST:
BEFORE STARTING ENGINES
Logbook and SEL Checked
Wing clear ice/frost check Accomplished
Rudder pedals and seats adjusted and locked
Windows closed and locked
02 masks/regulators/interphone/
Goggles/02 pressure Set and checked
Emergency lights armed
Probe heat Capt
Windshield anti-ice On
Anti-Skid Off
Pressurization Auto(up) and set
Air Cond shutoff Auto
Flight Guidance panel Set and checked
Flt Instr/switches/bugs Set and crosschecked
Fuel panel/quantity and distribution Set/___ Lbs and checked
Gear handle and lights Down, 3 green
ONS Data inserted
Transponder Standby and set
Stabilizer trim Set
Spoiler lever Retract
Takeoff warning Checked
Throttles Closed
Fuel levers Off
Flaps/Slats Up/Ret
Aileron/Rudder trim Zero/Zero
Parking brake/pressure Parked/Normal
Shoulder Harnesses On
Flight forms Checked
No smoking signs On
5 minutes before pushback
Seat belt signs On
Log Book On board
PRIOR TO ENGINE START OR PUSH-BACK
Galley power Off
Engine ignition Continuous
Fuel pumps On
Aux hydraulic pump On
Anti-collision/exterior lights On/as required
Door annunciators Out
Air conditioning supplies Off
TAXI
(Before taxi or power back)
Galley power On
Engine Anti-ice As required
Hydraulic system Checked
(Taxi)
APU As required
Pneu x-feeds As required
Air conditioning supplies Auto
Anti-skid Arm
Right engine (for 1 engine taxi) Shut down
Flight controls checked
FGS T/O mode
Right engine (following 1 engine taxi) Start
Hydraulic pumps Checked and Hi/On
APU As required
Pnue x-feeds Closed
Transponder TA/RA
BEFORE TAKEOFF
Flt Instruments and bugs Set and crosschecked
Anti-Ice As required
Flaps and slats Set/verified
Stab Trim Set
APU/PNUE x-feeds As required
Anti-skid/ABS Armed
Spoiler lever Armed
T/O PA/Packs Completed/As required
Annun lights Checked
Nose lights On-BRT
AFTER TAKEOFF - CLIMB
Gear Up and no lights
Spoiler lever Disarmed
Auto Brake Off/Disarmed
Flaps and slats UP/RET and no lights
Flap T.O SEL wheel Stow
Pressurization and a/c checked
APU As required
(10,000' MSL)
Altimeters Reset and crosschecked
Engine ignition As required
Fuel system Checked
Hydraulic pumps Low/Off
Sterile cockpit Chime
(18,000' MSL)
Exterior lights As required
Altimeters Reset and crosschecked
CRUISE
TRI Cruise
Engine sync N1
Delay codes in ACARS As required
DESCENT
Landing data Prepared
Pressurization Set and checked
Engine sync Off
Engine ignition Continuous
Engine/Airfoil anti-ice As required
Windshield anti-fog As required
Shoulder harness On
(18,000' MSL)
Exterior lights If required
Altimeters Reset and crosschecked
Rad-nav/DFGC switches RAD/as required
Hydraulic panel HI/ON/Checked
(10,000' MSL)
Sterile cockpit Chime
BEFORE LANDING
Altimeters Reset and crosschecked
Flt Instr and bugs Set and crosschecked
Seat belt/No smoking sign ON
Gear Down, 3 green
Spoiler lever Armed
Auto brakes As required
Flaps/slats ___/___/Land position
Annun lights Checked
LANDING
Spoiler lever Check full aft
Reverse levers As required
AFTER LANDING - TAXI
Autopilot and autothrottle Off
Landing lights Ret
Spoiler lever Ret
Auto brake Off/Disarm
Flaps/slats UP/RET and no lights
Radar Off
Transponder Standby
Anti-skid Off
Brake pressure Monitor
APU As required
Pneu x-feeds As required
Right engine (for 1 engine taxi) Shut down
PARKING
Brakes Parked
Seat belt signs Off
Pnue x-feeds Open
APU or external power Established
Fuel lever Off
Anti-collision/exterior lights Off/As required
Engine ignition Off
Fuel Pumps Off
Probe Heat Off
Anti-ice Off
Air conditioning As required
Emergency lights Off
Oil/HYD/02 quantity Checked
Hydraulic pumps HI/Off
ONS Checked/As required
Arrival report As required
Logbook Completed
Voice recorder CB As required
Flight directors Off
02 regulator supply levers Off
Cockpit lights As required
Galley power Off
VOLT/AMP indicator selector As required
Air conditioning As required
APU As required
Battery switch As required
Ground service bus Powered
Post flight inspection As required
MD-83 Aircraft Performance/Weight Info
NOTE: ALL performance figures are for ISA conditions, unless
otherwise noted.
(ISA=INTERNATIONAL STANDARD ATMOSPHERE CONDITIONS)
29.92"
15C deg./59F deg.
Sea Level
POWER PLANT:(2) JT8D-219 TURBOFANS (21,700LB ST)
TAKE-OFF LENGHT(FAR)
8,370 FT/ISA, Sea Level
10,059FT/35deg C, Sea Level
6,837 FT/ISA, 5000FT MSL
9,800 FT/35deg C, 5000FT MSL
LANDING LENGHT(FAR)
5,200 FT/ISA Sea Level
5,849 FT/ISA 5,000FT
SERVICE CEILING 37,000 FT
MAX RANGE 2,369 NM
WEIGHTS:
OPERATING WEIGHT EMPTY = 83,800 LBS
MAX PAYLOAD = 41,272 LBS
MAX RAMP WEIGHT 161,000 LBS
MAX TAKE-OFF WEIGHT 160,000 LBS
MAX LANDING WEIGHT 139,500 LBS/130,000 LBS (optional)
MAX ZERO FUEL WEIGHT 122,000 LBS
MAX FUEL (6.7 lbs./gallon) 46,772 LBS
-------------------------------------------------------------------TAKEOFF (T/O)
T/O weight (lbs.)/V1/VR/V2/Flaps Setting
160,000/150/|152/|162/11
150,000/143/148/156/11
140,000/137/142/150/11
130,000/130/137/145/11
120,000/123/131/139/11
--------------------------------------------------------------------
CLIMB (CLB)
CLIMB 250 KTS / 290 KTS / M.72 PERFORMANCE SCHEDULE:
MAX. CLIMB THRUST
1 PACK PER ENGINE
ANTI-ICING OFF
ISA
160,000 lbs.
FL370 N/A
FL350 N/A
FL330 N/A
FL310 N/A
FL290 16.5MIN/100NM/3797LBS
150,000 lbs.
FL370 N/A
FL350 N/A
FL330 N/A
FL310 16.5MIN/101NM/3674LBS
FL290 14.6MIN/88NM/3384LBS
140,000 lbs.
FL370 N/A
FL350 N/A
FL330 16.5MIN/103NM/3547LBS
FL310 14.5MIN/89NM/3262LBS
FL290 13MIN/78NM/3025LBS
130,000 lbs.
FL370 N/A
FL350 16.6MIN/104NM/3407LBS
FL330 14.5MIN/90NM/3130LBS
FL310 12.9MIN/78NM/2903LBS
FL290 11.6MIN/70NM/2704LBS
-------------------------------------------------------------------CRUISE (CRZ)
Mach 0.760 / LONG RANGE CRUISE OPTIMUM ALTITUDE
160,000 LBS /FL310
150,000 LBS /FL330
140,000 LBS /FL330
130,000 LBS /FL350
M.76 CRUISE PERFORMANCE:
FL NAM Per 1000 Pounds/TAS
Fuel Burn (1000 pounds/hr) = TAS/NAM Per 1000 Pounds
158, 000 LBS
FL NAM
TAS
FL330
N/A
N/A
FL310
60.1
446 TAS
FL290
59.1
450 TAS
158,000LBS 150,000LBS
FL330 N/A FL330 63.1/442TAS
FL310 60.1/446TAS FL310 62.8/446TAS
FL290 59.1/450TAS FL290 61.1/450TAS
142,000LBS 130,000LBS
FL350 N/A FL350 72.9/438TAS
FL330 66.8/442TAS FL330 71.5/442TAS
FL310 65.4/446TAS FL310 68.8/446TAS
FL290 62.9/450TAS FL290 65.7/450TAS
LONG RANGE CRUISE PERFORMANCE:
Gross Weight
FL/MACH/NAM Per 1000 Pounds/TAS
Fuel Burnout (1000 pounds/hr) = TAS/NAM Per 1000 Pounds
160,000LBS 150,000LBS
FL330 N/A FL330 .764/62.7/444TAS
FL310 .764/59.0/448TAS FL310 .762/62.5/447TAS
FL290 .761/58.4/451TAS FL290 .759/61.1/449TAS
140,000LBS 130,000LBS
FL350 .762/66.9/439TAS FL350 .764/72.5/440TAS
FL330 .762/67.4/443TAS FL330 .761/71.4/443TAS
FL310 .760/66.0/446TAS FL310 .754/69.2/442TAS
FL290 .750/63.9/444TAS FL290 .736/67.1/435TAS
DESCENT (DSC)
DESCENT M.76 / 290 KT/ 250 KT PERFORMANCE SCHEDULE:
IDLE THRUST
ZERO WIND
ISA
115,000LBS
FL370 24.4MIN/1093LB/154 NM
FL350 21.9MIN/928LB/136 NM
FL330 19.4MIN/752LB/117 NM
FL310 16.9MIN/564LB/99 NM
FL290 14.4MIN/366LB/80 NM
-------------------------------------------------------------------LANDING (LDG)
VREF Approach Bug speeds
Flaps 28/EXT deg
LNDG weight VREF Flaps
130,000LBS 136 28
140,000LBS 141 "
150,000LBS 146 "
160,000LBS 151 "
VREF Approach Bug speeds
Flaps 40/EXT deg
LNDG weight VREF Flaps
130,000LBS 132 40
140,000LBS 137 "
150,000LBS 141 "
160,000LBS 146 "
********************************************************************
AIRPORT OPERATIONS:
Takeoff Runway Slope (mean) +1.7%/-2.0%
Landing Runway Slope (mean) +1.7%/-2.0%
Runway Pressure Altitude: 8500 ft / -1000 ft
Runway Temp: -65F / +122F
Wind:
- TO and LDG
X wind: max demonstrated for takeoff 30 Kt
X wind: max demonstrated for landing 30 Kt
Max tail wind component 10 Kt
SPEED LIMITATIONS:
MMO FL390-250 0.84M
VMO FL250-0' 340 Kts
MAX FLAPS, SLATS speeds:
MFE M.57
0-13 deg. 280kias
14-20 deg. 240kias
21-25 deg. 220kias
26-30 deg. 205kias
31-40 deg. 200kias
Slats
Mid EXT 280kias/M.57
Full EXT 240kias/M.57
GEAR DOWN SPEEDS:
-Max speed with landing gear extended (VLE/MLE) 300kias /M.70
-Max speed landing gear operating(VLO/MLO extension) 300kias /M.70
-retracted (VLO retraction) 250kias/M.70
OTHER DATA: (MISC)
Turbulent Air Penetration:
275-285kias/M.75-M.79
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