b737 high altitude-maneuvering
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B737 high altitude-maneuveringTRANSCRIPT
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737.1
High Altitude ManeuveringHigh Altitude Maneuvering
Catherine DavisFlight Operations Engineering
Boeing Commercial AirplanesMay 2004
Catherine DavisFlight Operations Engineering
Boeing Commercial AirplanesMay 2004
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737.2The Boeing Company
High Altitude ManeuversHigh Altitude Maneuvers
• Limits to Altitude Capability
• Maneuvering Issues – Impact of thrust limits on turn margins
• Recommendations/Considerations for Operation at High Altitude
• Limits to Altitude Capability
• Maneuvering Issues – Impact of thrust limits on turn margins
• Recommendations/Considerations for Operation at High Altitude
Discussion TopicsDiscussion Topics
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737.3The Boeing Company
Maximum AltitudeMaximum Altitude
Defined by Thrust / Drag relationship
• User-defined Residual Rate of Climb (RROC)
• Temperature-dependent!
Defined by Thrust / Drag relationship
• User-defined Residual Rate of Climb (RROC)
• Temperature-dependent!
Thrust-Limited Maximum Altitude
There are three things that can limit Altitude Capability:
Defined by Initial Buffet CL• User-defined maneuver margin
Buffet-Limited Maximum Altitude
Maximum Certified Altitude (Structural Limit)
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737.4The Boeing Company
Flight Management System (FMS)Control Display Unit (CDU)
Flight Management System (FMS)Control Display Unit (CDU)
Airline Policy Page 1/2
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737.5The Boeing Company
27000
29000
31000
33000
35000
37000
39000
30 40 50 60 70
Gross Weight (1000 kg)
Alti
tude
(ft)
737-400 Optimum and Maximum Altitude737-400 Optimum and Maximum AltitudeBuffet-limited Maximum
Altitude (1.3g)
Thrust-limitedMaximum
Altitude (100 fpm)
ISA + 20C
ISA + 15C
ISA + 10C
OptimumAltitude
140(1000 lb)
8070 10090 110
120 130 150
Max Cert Alt
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737.6The Boeing Company
31000
33000
35000
37000
39000
41000
43000
40 50 60 70 80
Gross Weight (1000 kg)
Alti
tude
(ft)
737-800 Optimum and Maximum Altitudes737-800 Optimum and Maximum Altitudes
Max Cert AltBuffet-limited
MaximumAltitude (1.3g)
Thrust-limitedMaximum
Altitude (100 fpm)
ISA + 20C
ISA + 15C
ISA + 10C
OptimumAltitude
160(1000 lb)
10090 120110 130
140 150 170
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737.7The Boeing Company
737-800W Optimum and Maximum Altitudes737-800W Optimum and Maximum Altitudes
31000
33000
35000
37000
39000
41000
43000
40 50 60 70 80
Gross Weight (1000 kg)
Alti
tude
(ft)
Buffet-limitedMaximum
Altitude(1.3g)
Thrust-limitedMaximum
Altitude(100 fpm)
ISA + 20C
ISA + 15C
ISA + 10C
OptimumAltitude
160(1000 lb)
10090 120110 130
140 150 170
Max Cert Alt
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737.8The Boeing Company
Primary Flight Display (PFD) Airspeed Indication
Primary Flight Display (PFD) Airspeed Indication
NOTE: The amber band does not give any
indication of thrust limits
The amber band:– displays the
maneuver speed– provides 1.3g/40
degrees of bank angle (default) margin to buffet
– constant regardless of ambient temperature
The amber band:– displays the
maneuver speed– provides 1.3g/40
degrees of bank angle (default) margin to buffet
– constant regardless of ambient temperature
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737.9The Boeing Company
850090009500
1000010500110001150012000125001300013500
0.6 0.65 0.7 0.75 0.8 0.85
Mach number
Dra
g (lb
)
737-800 Drag vs Mach number 737-800 Drag vs Mach number Gross Weight = 70000 kg = 154323 lbAltitude = 35000 ft
LRCDrag in level flight
Thrust Available
Drag in Level Flight
Margin to Thrust Limit in
Level Flight
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737.10The Boeing Company
850090009500
1000010500110001150012000125001300013500
0.6 0.65 0.7 0.75 0.8 0.85
Mach number
Dra
g (lb
)
737-800 Drag vs Mach number 737-800 Drag vs Mach number Gross Weight = 70000 kg = 154323 lbAltitude = 35000 ft
LRC
Thrust Available
Drag associated with a 15º turn
Drag in a 15º Turn
Drag in Level Flight
Margin to Thrust Limit with 15º turn
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737.11The Boeing Company
850090009500
1000010500110001150012000125001300013500
0.6 0.65 0.7 0.75 0.8 0.85
Mach number
Dra
g (lb
)
737-800 Drag vs Mach number 737-800 Drag vs Mach number Gross Weight = 70000 kg = 154323 lbAltitude = 35000 ft
LRC
Thrust Available
Drag associated with a 30º turn
Drag in a 30º Turn
Drag in a 15º Turn
Drag in Level Flight
Drag is higher than available thrust in
30º turn
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737.12The Boeing Company
850090009500
1000010500110001150012000125001300013500
0.6 0.65 0.7 0.75 0.8 0.85
Mach number
Dra
g (lb
)
737-800 Drag vs Mach number 737-800 Drag vs Mach number Gross Weight = 70000 kg = 154323 lbAltitude = 35000 ft
LRC
Thrust Available
Drag in a 30º Turn
Drag in a 15º Turn
Drag in Level Flight
Thrust Available in CNT Mode
More thrust is available in Max Continuous Thrust (MCT) mode
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737.13The Boeing Company
29000
31000
33000
35000
37000
39000
40 45 50 55 60 65 70 75 80Gross Weight (1000 kg)
Alti
tude
(ft)
737-400 Maneuver Capability at Maximum Altitude
Standard Day
140(1000 lb)
8070 10090 110 120 130 150
LRC, Optimum
1.3g Initial Buffet (40º Bank)
MCRT, 20º Bank
MCRT, 10º Bank
MCRT, 100 FPM
Max Cert Alt
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737.14The Boeing Company
737-800 Maneuver Capability at Maximum Altitude
737-800 Maneuver Capability at Maximum Altitude
31000
33000
35000
37000
39000
41000
43000
40 50 60 70 80Gross Weight (1000 kg)
Alti
tude
(ft)
Standard Day
LRC, Optimum
MCRT, 20º Bank
1.3g Initial Buffet (40º Bank)
MCRT, 100 FPMMCRT, 10º Bank
160(1000 lb)
10090 120110 130 140 150 170
Max Cert Alt
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737.15The Boeing Company
737-800 Maneuver Capability at Maximum Altitude
737-800 Maneuver Capability at Maximum Altitude
31000
33000
35000
37000
39000
41000
43000
40 50 60 70 80Gross Weight (1000 kg)
Alti
tude
(ft)
ISA + 20ºC Day
LRC, Optimum
1.3g Initial Buffet (40º Bank)
MCRT, 100 FPM
MCRT, 10º Bank
160(1000 lb)
10090 120110 130 140 150 170
Max Cert Alt
MCRT, 20º Bank
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737.16The Boeing Company
Recommendations/Considerationsfor Flight at High Altitudes
Recommendations/Considerationsfor Flight at High Altitudes
To get accurate altitude limits from the FMC:Enter an accurate aircraft weightEnter an accurate temperature deviation at the cruising altitude
To get accurate altitude limits from the FMC:Enter an accurate aircraft weightEnter an accurate temperature deviation at the cruising altitude
For LNAV operation:the FMC provides a real-time bank angle limiting function this function will protect the commanded bank angle from exceeding the current available thrust limit. this bank angle protection is not available when LNAV mode is deactivated.
For LNAV operation:the FMC provides a real-time bank angle limiting function this function will protect the commanded bank angle from exceeding the current available thrust limit. this bank angle protection is not available when LNAV mode is deactivated.
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737.17The Boeing Company
Recommendations/Considerationsfor Flight at High Altitudes (cont)
Recommendations/Considerationsfor Flight at High Altitudes (cont)
For LNAV deactivated:Fly at least 10 knots above the lower amber band
Limit bank angles to no more than 10º for manual steering in cruise (set MCP bank angle selector to 10º from TOC to TOD)
If speed drops below the lower amber band limit, immediately increase speed by doing one or more of the following:
1. Reduce bank angle (to 10 - 15º maximum)2. Increase thrust (up to maximum continuous thrust) as
required3. Descend