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PSP 604-15 SINGLE ENGINE DATA
HIGH SPEED DRIFTDOWN – MACH 0.72/300 KIAS
44,000 LB & 46,000 LB INITIAL WEIGHT
(Maximum Continuous Thrust / One Pack on High / Anti−Ice Off / 30 C.G.)
QR1_DXSE_018
PERF-08-18
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15 SINGLE ENGINE DATA
HIGH SPEED DRIFTDOWN – MACH 0.72/300 KIAS
48,000 LB & 50,000 LB INITIAL WEIGHT
(Maximum Continuous Thrust / One Pack on High / Anti−Ice Off / 30 C.G.)
QR1_DXSE_019
PERF-08-19
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15 SINGLE ENGINE DATA
PERF-08-20
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15 SINGLE ENGINE DATA
THIS PAGE INTENTIONALLY LEFT BLANK
CONTENTS PAGE
Cold Wx Ops
Preparation for Deicing/Anti-Icing ....................................SUPP−01−1
Deicing/Anti-Icing .............................................................SUPP−01−2
Deicing Fluid Holdover Time ............................................SUPP−01−4
Steep Approach
Steep Approach (5.5°) Landing Speeds
and Distances ..................................................................SUPP−02−1
Altitude − Sea Level .........................................................SUPP−02−1
Altitude − 500 Feet ...........................................................SUPP−02−2
Altitude − 1,000 Feet ........................................................SUPP−02−3
Altitude − 2,000 Feet ........................................................SUPP−02−4
Altitude − 4,000 Feet ........................................................SUPP−02−5
Altitude − 5,000 Feet ........................................................SUPP−02−6
Contaminated Runway
Contaminated Runway Corrections .................................SUPP−03−1
Take-Off Corrections − Wet Runway ...............................SUPP−03−1
Take-Off Corrections − 0.125 In. Water or
Equivalent ........................................................................SUPP−03−1
Take-Off Corrections − 0.25 In. Water or
Equivalent ........................................................................SUPP−03−1
Take-Off Corrections − Runway Covered
with Ice .............................................................................SUPP−03−1
Take-Off Corrections − Runway Covered
by Compacted Snow ........................................................SUPP−03−2
Landing Corrections .........................................................SUPP−03−2
SUPP-00-1
REV 70, Jun 08/07
QUICK REFERENCE HANDBOOK
PSP 604-15 SUPPLEMENTS CONTENTS
SUPP-00-2
REV 69, Jun 04/07
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PSP 604-15 SUPPLEMENTS CONTENTS
THIS PAGE INTENTIONALLY LEFT BLANK
PREPARATION FOR DEICING/ANTI-ICING
Before fluid is applied:
If engines/APU are off:
(1) Proceed to step (7).
If engines/APU are operating:
(2) Thrust levers.........................................................................IDLE
(3) PACKs.................................................................................. OFF
(4) 10TH STAGE bleeds.....................................................CLOSED
(5) WING and COWL ANTI-ICE ................................................ OFF
(6) 14TH STAGE bleeds.....................................................CLOSED
(7) Stabilizer trim.......................................................AS REQUIRED
(8) Flaps....................................................................AS REQUIRED
(9) Airplane ......................................................... HEAD INTO WIND
if possible.
(10) Deicing operator ............................................................. ADVISE
to avoid direct spraying on:
• Windshields, side windows and cabin windows;
• Pitot/static and TAT probes;
• AOA vanes;
• Static pressure ports;
• Engine air intake and exhaust;
• APU inlet and exhaust;
• Antennas;
• Vents and drains;
• Winglets;
• Wheels and brakes.
CAUTION
Application of deicing/anti-icing fluid on
wheel brake assemblies will seriously
degrade braking performance.
SUPP-01-1
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15 COLD WX OPS
DEICING/ANTI-ICING
CAUTION
1. Under no circumstances can an airplane that has
been anti-iced receive another coat of Type II or
　
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