
Elite 5K
- Posts: 25409
- Joined: 05 May 2009, 21:31
- Location: ɐıןɐɹʇsn∀¯\_(ツ)_/¯
- Warnings: -2
The attached ZIPPED text only file has all the guff from AV-8B NATOPS, only the CL Conventional Landing has been entered here as an example.
AV-8B Harrier II Conventional Landing (CL). http://info.publicintelligence.net/AV-8B-000.pdf
A standard CL, figure 7-5, requires substantially greater distance to stop than a SL or RVL. Landing distance available is a critical consideration when performing a CL. The brakes are designed primarily for V/STOL and are marginal for a CL without PNB [Power Nozzle Braking]; therefore, No PNB CLs should be used only as an emergency procedure.
Refer to Performance Data, A1-AV8BB-NFM-400, for stopping distance with and without PNB.
Approaching 180 -
1. Nozzles - AFT
2. Flaps - Recheck in AUTO
3. AOA - 10-12°
Off the 180 -
4. Adjust flight path with stick
At 30-50 feet AGL -
5. Control AOA with throttle
6. Set Attitude - Witches Hat on to 2° above
the horizon
7. Control ROD with throttle
At touchdown -
8. Throttle - IDLE
9. Nosewheel Steering - ENGAGE WHEN
ROLLING STRAIGHT AND PEDALS ARE
NEUTRALIZED
10. Nozzles - AS REQUIRED (up to full braking
stop)
NOTE
Porpoising on touchdown will normally be damped out by selection of the braking stop. Do not use wheel brakes while conducting PNB.
11. Trim - MINIMUM 2° ND
12. Throttle - AS REQUIRED (for PNB a
maximum of 60% (406) to 70% (408))
At 60 kts -
13. Throttle - IDLE
14. Nozzles - HOVER STOP
15. Brakes - APPLY
16. Water - OFF
17. Nozzles - LESS THAN 60° WHEN
SLOW
7.7 POSTFLIGHT
7.7.1 After Landing
When clear of the active runway -
1. Trim - 4° ND
2. Flaps - CRUISE FOR TAXI
3. Water - OFF
_______________________________________
Rolling Vertical Takeoff (RVTO).
An RVTO may be performed in those instances when a VTO is desired but the takeoff surface is deemed unsuitable. The RVTO requires approximately 100 feet of ground roll and should be made as nearly into the wind as possible. RVTO can be performed up to hover weight...
Conventional Takeoff.
The CTO can be used when configuration or environmental conditions preclude use of any other takeoff type (i.e., crosswinds or asymmetric loadings). The CTO is restricted to gross weights that will not cause the wheel/tire limitation speed of 180 KGS to be exceeded on the takeoff roll.
AV-8B Harrier II Conventional Landing (CL). http://info.publicintelligence.net/AV-8B-000.pdf
A standard CL, figure 7-5, requires substantially greater distance to stop than a SL or RVL. Landing distance available is a critical consideration when performing a CL. The brakes are designed primarily for V/STOL and are marginal for a CL without PNB [Power Nozzle Braking]; therefore, No PNB CLs should be used only as an emergency procedure.
Refer to Performance Data, A1-AV8BB-NFM-400, for stopping distance with and without PNB.
Approaching 180 -
1. Nozzles - AFT
2. Flaps - Recheck in AUTO
3. AOA - 10-12°
Off the 180 -
4. Adjust flight path with stick
At 30-50 feet AGL -
5. Control AOA with throttle
6. Set Attitude - Witches Hat on to 2° above
the horizon
7. Control ROD with throttle
At touchdown -
8. Throttle - IDLE
9. Nosewheel Steering - ENGAGE WHEN
ROLLING STRAIGHT AND PEDALS ARE
NEUTRALIZED
10. Nozzles - AS REQUIRED (up to full braking
stop)
NOTE
Porpoising on touchdown will normally be damped out by selection of the braking stop. Do not use wheel brakes while conducting PNB.
11. Trim - MINIMUM 2° ND
12. Throttle - AS REQUIRED (for PNB a
maximum of 60% (406) to 70% (408))
At 60 kts -
13. Throttle - IDLE
14. Nozzles - HOVER STOP
15. Brakes - APPLY
16. Water - OFF
17. Nozzles - LESS THAN 60° WHEN
SLOW
7.7 POSTFLIGHT
7.7.1 After Landing
When clear of the active runway -
1. Trim - 4° ND
2. Flaps - CRUISE FOR TAXI
3. Water - OFF
_______________________________________
Rolling Vertical Takeoff (RVTO).
An RVTO may be performed in those instances when a VTO is desired but the takeoff surface is deemed unsuitable. The RVTO requires approximately 100 feet of ground roll and should be made as nearly into the wind as possible. RVTO can be performed up to hover weight...
Conventional Takeoff.
The CTO can be used when configuration or environmental conditions preclude use of any other takeoff type (i.e., crosswinds or asymmetric loadings). The CTO is restricted to gross weights that will not cause the wheel/tire limitation speed of 180 KGS to be exceeded on the takeoff roll.
- Attachments
-
AV-8B Harrier NATOPS T-O & Land.zip
- (7.34 KiB) Downloaded 376 times
Last edited by spazsinbad on 17 Jun 2011, 18:34, edited 3 times in total.
A4G Skyhawk: www.faaaa.asn.au/spazsinbad-a4g/ & www.youtube.com/channel/UCwqC_s6gcCVvG7NOge3qfAQ/videos?view_as=subscriber