LANDING
LANDING
TABLE OF CONTENTS
TABLE OF CONTENTS
SUBJECT PAGE SUBJECT PAGE MINIMUMMINIMUM LANDING LANDING RUNWAY RUNWAY LENGTH LENGTH (737-600)...(737-600)...2...2 MINIMUM
MINIMUM LANDING LANDING RUNWAY RUNWAY LENGTH LENGTH (737-600)...(737-600)...3...3 MINIMUM
MINIMUM LANDING LANDING RUNWAY RUNWAY LENGTH LENGTH (737-700)...(737-700)...4...4 MINIMUM
MINIMUM LANDING LANDING RUNWAY RUNWAY LENGTH LENGTH (737-800)...(737-800)...5...5 MINIMUM
MINIMUM LANDING LANDING RUNWAY RUNWAY LENGTH LENGTH (737-900)...(737-900)...6...6 RUNWAY
RUNWAY WEIGHT WEIGHT LIMIT LIMIT OVERVIEW (737-ALL)OVERVIEW (737-ALL) ...7...7 AUTOBRAKE
AUTOBRAKE SYSTEM SYSTEM ISSUES ISSUES (B737-AL(B737-ALL)L)... 77 LANDING
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Minimum Landing Runway Length (737-600)
Minimum Landing Runway Length (737-600)
FLAPS 40 - Landing Runway LimitFLAPS 40 - Landing Runway Limit Weight TableWeight Table
Required Required Field Field L Leennggtth h fftt DDRRYY WWEETT DDRRYY WEWETT DDRRYY WWEETT DDRRYY WWEETT 3 3330000 8811..11 4 4000000 110044..77 8866..22 110011..66 8833..66 9988..33 8800..99 9955..55 4 4550000 112266..55 101066..77 112233..77 110033..66 112200..88 110000..33 111177..55 9977..44 5 5000000 114455..77 112255..99 114422..00 112233..00 113388..22 111199..99 113344..99 111166..66 6 6000000 116633..88 114422..00 116600..11 113388..77 115566..11 113355..11 115522..33 113322..11 6 6550000 151588..55 115544..88 115511..00 114466..88 AIRPORT PRESSUR
AIRPORT PRESSURE ALTITUDE (E ALTITUDE ( FT)FT) 0
0 11000000 22000000 33000000
To use this table:
To use this table: Enter from the top of the table by selecting the pressure altitEnter from the top of the table by selecting the pressure altitude that mostude that most closely matches the landi
closely matches the landing airport. ng airport. (For airports higher than 3000f(For airports higher than 3000ft use the 3000ft columns.)t use the 3000ft columns.) Select the DRY or WET runway column to suit circumstances, then find the weight that most Select the DRY or WET runway column to suit circumstances, then find the weight that most closely matches the planned landing weight for your destination.
closely matches the planned landing weight for your destination. Find the minimum requiredFind the minimum required runway length by moving left to the first column.
runway length by moving left to the first column. Example:
Example: 0ft. MSL airport wit0ft. MSL airport with a dry runway and landing weight of 126,000lbs will result in ah a dry runway and landing weight of 126,000lbs will result in a minimum runway requirement of 4,500ft.
minimum runway requirement of 4,500ft.
Required Runway Length Wind Correction Table Required Runway Length Wind Correction Table (Headwinds are negative numbers /
(Headwinds are negative numbers / Tailwinds positive)Tailwinds positive) Runway Runway L Leennggtthhfftt.. --1155 --1100 --55 00 1100 2200 3300 4400 3 3330000 22665577 22995533 33330000 33447788 33770077 33993377 44116677 4 4000000 22992200 33224488 33660099 44000000 44116677 44339966 44665599 44992211 4 4550000 33551100 33887711 44223322 44550000 44882233 55111188 55338811 55664433 5 5000000 44110011 44446622 44885566 55000000 55551122 55880077 66007700 66339988 6 6000000 44669922 55008855 55447799 66000000 66220011 66449966 66779911 77111199 6 6550000 55228822 55667766 66110022 66550000 66889900 77118855 77551133 77887744 7 7330000 55887733 66229999 66772266 77330000 77557799 8 8000000 66446633 66992233 77338822 88000000 8 8550000 77005544 77551133 9 9220000 77664444 WIND COMPONENT (KTS) WIND COMPONENT (KTS) To use thi
To use this table: s table: Enter table Enter table at left edge at left edge using runway length. using runway length. Adjust required Adjust required landing lengthlanding length based on winds reported at surf
based on winds reported at surface. ace. Headwinds will shorten requirHeadwinds will shorten required landing runway distanceed landing runway distance while tail winds will increase landing runway
Minimum Landing Runway Length (737-700)
Minimum Landing Runway Length (737-700)
FLAPS 40 - Landing Runway LimitFLAPS 40 - Landing Runway Limit Weight TableWeight Table
Required Required Field Field L Leennggtth h fftt DDRRYY WWEETT DDRRYY WEWETT DDRRYY WWEETT DDRRYY WWEETT 3 3880000 9922..66 8899..88 8877..00 4 4220000 110066..22 8877..66 110033..00 8855..00 9999..99 9966..99 4 4660000 112200..00 9999..44 111166..55 9966..44 111122..99 9933..44 110099..55 9900..66 5 5000000 113344..00 111111..33 113300..11 110088..00 112266..22 110044..77 112222..44 110011..55 5 5440000 114477..44 112233..44 114433..33 111199..77 113399..22 111166..11 113355..11 111122..66 5 5880000 115588..99 113355..55 115544..88 113311..66 115500..88 112277..66 114466..99 112233..88 6 6220000 117700..44 114477..11 116655..99 114433..00 116611..44 113388..99 115577..33 113344..88 6 6660000 118800 115577..11 117766..44 115533..22 117722..11 114499..22 116677..66 114455..11 7 7000000 161677..11 116622..88 118800 115588..44 117777..44 115544..44 7 7440000 171766..55 117722..11 116677..88 116633..44 AIRPORT PRESSUR
AIRPORT PRESSURE ALTITUDE (E ALTITUDE ( FT)FT) 0
0 11000000 22000000 33000000
To use this table:
To use this table: Enter from the top of the table by selecting the pressure altitEnter from the top of the table by selecting the pressure altitude that mostude that most closely matches the landi
closely matches the landing airport. ng airport. (For airports higher than 3000f(For airports higher than 3000ft use the 3000ft columns.)t use the 3000ft columns.) Select the DRY or WET runway column to suit circumstances, then find the weight that most Select the DRY or WET runway column to suit circumstances, then find the weight that most closely matches the planned landing weight for your destination.
closely matches the planned landing weight for your destination. Find the minimum requiredFind the minimum required runway length by moving left to the first column.
runway length by moving left to the first column. Example:
Example: 0ft. MSL airport wit0ft. MSL airport with a dry runway and landing weight of 134,000lbs will result in ah a dry runway and landing weight of 134,000lbs will result in a minimum runway requirement of 5000ft.
minimum runway requirement of 5000ft.
Required Runway Length Wind Correction Table Required Runway Length Wind Correction Table (Headwinds are negative numbers /
(Headwinds are negative numbers / Tailwinds positive)Tailwinds positive) Runway Runway L Leennggtthhfftt.. --1155 --1100 --55 00 1100 2200 3300 4400 3 3000000 22667700 33000000 33222200 33444400 33668800 33991100 3 3440000 22772200 33006600 33440000 33663300 33887700 44111100 44336600 3 3880000 22775500 33009900 33444400 33880000 44004400 44229900 44554400 44880000 4 4220000 33111100 33447700 33883300 44220000 44445500 44771100 44997700 55224400 4 4660000 33448800 33884400 44221100 44660000 44886600 55113300 55441100 55669900 5 5000000 33884400 44221100 44660000 55000000 55227700 55555500 55884400 66113300 5 5440000 44220000 44559900 44999900 55440000 55668800 55997700 66227700 66557700 5 5880000 44556600 44996600 55337700 55880000 66009900 66339900 66770000 77002200 6 6220000 44992200 55333300 55776600 66220000 66550000 66881100 77113300 77446600 6 6660000 55228800 55771100 66114400 66660000 66991100 77223300 77556600 77990000 7 7000000 55664400 66008800 66553300 77000000 77332200 77665500 77999900 88335500 7 7440000 66000000 66445500 66991100 77440000 77773300 88007700 88442200 7 7880000 66336600 66883300 77330000 77880000 88114400 88449900 8 8220000 66772200 77220000 77669900 88220000 88555500 WIND COMPONENT (KTS) WIND COMPONENT (KTS) To use thi
Minimum Landing Runway Length (737-800)
Minimum Landing Runway Length (737-800)
FLAPS 40 - Landing Runway LimitFLAPS 40 - Landing Runway Limit Weight TableWeight Table
Required Required Field Field L Leennggtth h fftt DDRRYY WEWETT DDRRYY WWEETT DRDRYY WWEETT DDRRYY WWEETT DDRRYY WWEETT 3 3330000 7799..44 4 4000000 110011..44 8844..22 9955..77 7799..44 9900..22 8844..88 7799..88 4 4660000 112222..88 110033..44 111166..66 9977..55 111100..00 9911..99 110033..88 8686..44 9977..77 8866..44 5 5000000 114400..44 112222..11 113344..00 111155..77 112288..00 110099..11 112222..11 110033..00 111155..55 110033..00 5 5440000 115599..44 113377..33 115511..55 113311..22 114433..77 112255..22 113377..11 111199..33 113300..77 111199..33 5 5880000 117799..22 115533..44 117700..00 114455..77 116611..44 113388..99 115533..00 113322..77 114455..11 113322..77 6 6220000 119955..22 117700..66 118888..00 116611..88 117799..00 115533..77 116699..88 114455..77 116600..77 114455..77 6 6660000 118877..44 117788..11 119933..66 116699..11 118866..33 116600..33 117766..66 116600..33 7 7000000 119999..33 119922 118844..55 119988 117744..88 181888..77 117744..88 7 7440000 119955..88 118888..55 119944..99 118888..55 8000 8000 AIRPORT PRESSUR
AIRPORT PRESSURE ALTITUDE (E ALTITUDE ( FT)FT) 0
0 22000000 44000000 66000000
To use this table:
To use this table: Enter from the top of the table by selecting the pressure altitEnter from the top of the table by selecting the pressure altitude that mostude that most closely matches the landi
closely matches the landing airport. ng airport. (For airports higher than 8000f(For airports higher than 8000ft use the 8000ft columns.)t use the 8000ft columns.) Select the DRY or WET runway column to suit circumstances, then find the weight that most Select the DRY or WET runway column to suit circumstances, then find the weight that most closely matches the planned landing weight for your destination.
closely matches the planned landing weight for your destination. Find the minimum requiredFind the minimum required runway length by moving left to the first column.
runway length by moving left to the first column. Example:
Example: 0ft. MSL airport wit0ft. MSL airport with a dry runway and landing weight of 134,000lbs will result in ah a dry runway and landing weight of 134,000lbs will result in a minimum runway requirement of 5000ft.
minimum runway requirement of 5000ft.
Required Runway Length Wind Correction Table Required Runway Length Wind Correction Table (Headwinds are negative numbers /
(Headwinds are negative numbers / Tailwinds positive)Tailwinds positive) Runway Runway L Leennggtthhfftt.. --1155 --1100 --55 00 1100 2200 3300 4400 3 3228800 22665577 22995522 33228800 33770066 33993366 44116666 44116666 3 3993366 33228800 33660088 33993366 44339955 44665588 44992200 44992200 4 4559922 33554422 33887700 44223311 44559922 55111177 55337799 55664422 55664422 5 5224488 44110000 44446611 44885544 55224488 55880066 66006688 66336633 66339966 5 5990044 44669900 55008844 55447788 55990044 66449944 66779900 77111188 77111188 6 6556600 55228811 55667744 66110011 66556600 77118833 77551111 77883399 77887722 7 7221166 55887711 66229988 66772244 77221166 77887722 88223333 88559944 7 7887722 66446622 66888888 77338800 77887722 88556611 88992222 8 8552288 77001199 77551111 88000033 88552288 9 9118844 77661100 88110022 88662266 99118844 9 9884400 88220000 88669922 1 100449966 88779900 WIND COMPONENT (KTS) WIND COMPONENT (KTS) To use thi
To use this table: s table: Enter table Enter table at left edge at left edge using runway length. using runway length. Adjust required Adjust required landing lengthlanding length based on winds reported at surf
based on winds reported at surface. ace. Headwinds will shorten requirHeadwinds will shorten required landing runway distanceed landing runway distance while tail winds will increase landing runway
Minimum Landing Runway Length (737-900)
Minimum Landing Runway Length (737-900)
FLAPS 40 - Landing Runway LimitFLAPS 40 - Landing Runway Limit Weight TableWeight Table
Required Required Field Field L Leennggtth h fftt DDRRYY WEWETT DDRRYY WWEETT DRDRYY WWEETT DDRRYY WWEETT DDRRYY WWEETT 3 3880000 9933..33 8877..88 4 4220000 110077..11 8888..33 110000..88 9944..77 8888..99 4 4660000 112211..00 110000..22 111144..00 9494..33 110077..11 8888..66 110000..66 9944..33 5 5000000 113322..22 111122..33 112255..99 110055..66 111199..88 9999..33 111122..55 9933..22 110055..55 8844..44 5 5440000 114433..55 112233..77 113366..55 111177..22 113300..00 111100..11 112233..77 101033..55 111166..88 9977..00 5 5880000 115599..66 113333..44 115511..99 112277..11 114400..00 112200..99 113333..22 111133..88 112266..66 110066..77 6 6220000 117711..11 114433..22 116622..99 113366..33 115544..99 112299..77 114422..77 112233..55 113355..66 111166..66 6 6660000 118822..77 115577..88 117733..88 114488..55 116655..22 113388..55 115577..11 113311..77 114466..77 112255..22 7 7000000 119911..99 116677..99 118844..88 115599..88 117755..66 115511..88 116666..99 114400 115588..55 113333 7 7440000 117777..99 119933 116699..33 118866 116611 117766..77 115533 116677..88 114400..99 7 7880000 118877..55 171788..88 119933..33 117700 118866..55 116611..66 117777..11 115533..55 8 8220000 119944..66 118877..88 117799 191933..33 117700..11 118866..33 116611..55 8 8660000 119944..55 118877..55 117788..66 119900..77 116699..66 9 9000000 119933..88 118866..99 119944..33 117777..77 9 9440000 119922..99 118855..77 9 9880000 118899..99 1 100220000 119933..11 10600 10600 8000 8000 AIRPORT PRESSUR
AIRPORT PRESSURE ALTITUDE (E ALTITUDE ( FT)FT) 0
0 22000000 44000000 66000000
Required Runway Length Wind Correction Table Required Runway Length Wind Correction Table (Headwinds are negative numbers /
(Headwinds are negative numbers / Tailwinds positive)Tailwinds positive) Runway Runway L Leennggtthhfftt.. --1155 --1100 --55 00 1100 2200 3300 4400 3 3000000 22664400 33000000 33220000 33442200 33663300 33886600 3 3440000 22665500 33002200 33440000 33662200 33884400 44007700 44331100 3 3880000 22666600 33002200 33440000 33880000 44003300 44226600 44550000 44775500 4 4220000 33001100 33338800 33777700 44220000 44444400 44668800 44994400 55220000 4 4660000 33337700 33774400 44115500 44660000 44885500 55111100 55338800 55665500 5 5000000 33773300 44110000 44553300 55000000 55226600 55553300 55881100 66110000 4 4550000 44009900 44447700 44991100 55440000 55667700 55995500 66225500 66555500 5 5880000 44444400 44883300 55228800 55880000 66008800 66338800 66668800 77000000 6 6220000 44880000 55119900 55666600 66220000 66550000 66880000 77112200 77444400 6 6660000 55116600 55556600 66004400 66660000 66991100 77222200 77555500 77889900 7 7000000 55551100 55992200 66441100 77000000 77332200 77665500 77999900 88334400 7 7440000 55887700 66228800 66779900 77440000 7777333300 88007700 88442200 88779900 7 7880000 66223300 66664400 77007700 77880000 88114400 88449900 88886600 99224400 8 8220000 66559900 77001100 77555500 88220000 88555500 88992200 99330000 99669900 8 8660000 66994400 77337700 77992200 88660000 88996600 99334400 99773300 1100114400 9 9000000 77330000 77773300 88330000 99000000 99337700 99776600 1010117700 1100558800 9 9440000 77666600 88110000 88668800 99440000 99779900 1100119900 1100660000 1111003300 WIND COMPONENT (KTS) WIND COMPONENT (KTS)
RUNWAY WEIGHT LIMIT OVERVIEW (737-ALL)
RUNWAY WEIGHT LIMIT OVERVIEW (737-ALL)
TheThe Landing Runway Limit TablesLanding Runway Limit Tables provided here are calculated based on a normal approach,provided here are calculated based on a normal approach, flown at FLAPS40 at the target approach RE
flown at FLAPS40 at the target approach REF speed as specified by the FMC. F speed as specified by the FMC. The runway limitThe runway limit predictions are based upon a
predictions are based upon a threshold crossing of 50ft followed by normal touchdown usingthreshold crossing of 50ft followed by normal touchdown using spoilers, minimal braking with no reverse
spoilers, minimal braking with no reverse thrust.thrust. Crews should keep in mind that these
Crews should keep in mind that these figures were acquired using a new aircraft with new figures were acquired using a new aircraft with new brakesbrakes and tires, so actual performance of an in-service aircraft may vary sl
and tires, so actual performance of an in-service aircraft may vary slightly. ightly. Runway Limit WeightsRunway Limit Weights in excess of the known structural weight limit are included for
in excess of the known structural weight limit are included for emergency use should a forcedemergency use should a forced landing in excess of the
landing in excess of the Structural Limit WeightStructural Limit Weight be required. be required. Inclusion of these Inclusion of these figures does notfigures does not imply permission to land the aircraft above the Structural Limit Weight, and crews are
imply permission to land the aircraft above the Structural Limit Weight, and crews are encouraged to land the aircraft in such
encouraged to land the aircraft in such a condition only as a a condition only as a matter of last recourse.matter of last recourse. If required to land the aircraft while still
If required to land the aircraft while still above the Structural Limit Weight,above the Structural Limit Weight, crews shouldcrews should anticipate a hot-brake condition, and ensure that adequate
anticipate a hot-brake condition, and ensure that adequate ground safety precautions are takenground safety precautions are taken prior to arrival.
prior to arrival.
AUTOBRAKE SYSTEM ISSUES (B737-ALL)
AUTOBRAKE SYSTEM ISSUES (B737-ALL)
Unlike a simple anti-skid system, the autobrake system used aboardUnlike a simple anti-skid system, the autobrake system used aboard the Next Generation 737the Next Generation 737 aircraft is designed to modulate brake pressure to
aircraft is designed to modulate brake pressure to all four main gear brake systems in order all four main gear brake systems in order toto provide the aircraft with a specific rat
provide the aircraft with a specific rate of deceleration. e of deceleration. This rate of deceleration will be proviThis rate of deceleration will be providedded and maintained regardless of t
and maintained regardless of the use of spoilers or reverse the use of spoilers or reverse thrust. hrust. The rate of deceleratiThe rate of deceleration ison is provided according to the settings below:
provided according to the settings below: Setting
Setting 1: 1: 4ft 4ft [1.2 [1.2 M]/Second/SM]/Second/Second econd Setting Setting 4: 4: 7.5ft 7.5ft [2.3 [2.3 M]/Second/SM]/Second/Secondecond Setting
Setting 2: 2: 5ft 5ft [1.5 [1.5 M]/Second/SecoM]/Second/Second nd MAX MAX AUTO: AUTO: 11ft 11ft [3.4 [3.4 M]/Second/SecoM]/Second/Secondnd Setting
Setting 3: 3: 6ft 6ft [1.8 [1.8 M]/Second/SecoM]/Second/Secondnd
When used, spoilers and reverse thrust will reduce
When used, spoilers and reverse thrust will reduce the total energy that would otherwise bethe total energy that would otherwise be absorbed by the brake systems.
absorbed by the brake systems. By reducing the amount of By reducing the amount of energy absorbed into the brakeenergy absorbed into the brake pads, spoilers and reverse thrust reduce the
pads, spoilers and reverse thrust reduce the overall wear of the brake systems and overall wear of the brake systems and aircraft tires.aircraft tires. As such, crews are encouraged to
As such, crews are encouraged to use reverse thrust commensurate with safety and control of use reverse thrust commensurate with safety and control of the aircraft on all landings.
the aircraft on all landings.
LANDING SPEED TERMINOLOGY
LANDING SPEED TERMINOLOGY
__REF__REF: The calculated reference speed for a specific flap configuration. : The calculated reference speed for a specific flap configuration. (e.g. 30REF for a flaps(e.g. 30REF for a flaps 30 approach.)
30 approach.) This speed is used to calculate the actual target speeds at which the aircraft willThis speed is used to calculate the actual target speeds at which the aircraft will be flown.
be flown. 40REF, 30REF, 25R40REF, 30REF, 25REF speeds etc can be found using the APPROACH page of theEF speeds etc can be found using the APPROACH page of the FMC.
FMC.
Target Speed:
Target Speed: The speed at which the apprThe speed at which the approach should be flown. oach should be flown. Target speed should equalTarget speed should equal 25REF+5 or 30REF+5 knots.
25REF+5 or 30REF+5 knots. To this figure, add “1/2 steady wind plus the full gust factor (up to aTo this figure, add “1/2 steady wind plus the full gust factor (up to a maximum of 20 knots.)
maximum of 20 knots.) Threshold Speed:
Threshold Speed: Speed crossing the threshold. Speed crossing the threshold. Equal to 25REF or Equal to 25REF or 30REF plus the f30REF plus the full gustull gust factor, up to a maximum of 20kts.
Autoland Target Speeds:
Autoland Target Speeds: The speed at which the Autoland/Autothrottle approach is flown.The speed at which the Autoland/Autothrottle approach is flown. Equal to 25REF+5 or 30REF + 5 knots, regardless of wind conditi
Equal to 25REF+5 or 30REF + 5 knots, regardless of wind conditions. ons. The Autothrottle correctsThe Autothrottle corrects for normal wind gust conditions through the airspeed an
