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LANDING WITH FAILED PRIMARY FLIGHT CONTROL (Continued)
• ELEVATOR
1. Elevator Trim. . . . . . . . . . . . . . . . . . . . . . . . . . . . USE MANUAL TRIM WHEEL in small
increments to control pitch attitude
NOTE
Use manual trim wheel for primary pitch control. Use of electric trim may result in
overcontrolling, especially at low speed.
2. Make small pitch and power changes and set up landing configuration early.
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VREF+10
4. Landing Distance / Weight:
5. After touch down and nose wheel on ground, apply wheel brakes as soon as possible.
CAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
• RUDDER
1. RUDDER TRIM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRIM for coordinated flight
2. If possible, choose a wide runway with the least possible crosswind.
3. Airspeed . . . . . . . . . . . . . . . . . VAPP MINIMUM until landing assured then slow to VREF
CAUTION
Use of differential braking may be required for directional control upon landing.
PROCEDURE COMPLETED
STALL
WARNING FLAPS *MULTIPLY LANDING
DISTANCE BY
*REDUCE MAX LANDING
WEIGHT BY
NORMAL LAND 1.28 50 lbs.
HIGH TO/APR 1.22 40 lbs.
* Basic landing distance and maximum landing weight values must be obtained
from the appropriate landing performance charts based on the STALL
WARNING and ANTI-ICE system settings.
510FM-07 AA 3-123
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
LANDING WITH ICE ON WING LEADING EDGE
This procedure should be used anytime there is an abnormal buildup of ice on the leading edge
of the wing. This may be caused by a failure of the de-ice boot system or an unusually heavy
accumulation of ice.
1. Landing Data . . . . . . . USE the following landing data (Landing Flaps limited to TO/APR):
a. Airspeed:
VREF (KIAS) - STALL WARNING HIGH
b. Landing Distance/Weight:
(1) MULTIPLY STALL WARNING-HIGH landing distance by 1.22.
(2) REDUCE maximum landing weight by 40 lbs.
CAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING
NOTE
Either a W/S A/I FAIL L or R failure will result in one anti-ice panel of each windshield
being inoperative. Visibility through the remaining panels is adequate for landing
using normal landing procedures. If both windshields are inoperative, adequate
visibility for a safe landing with an obscured windshield has been demonstrated using
the following procedure.
APPROACH
1. Select an airport with a straight-in ILS approach or a GPS/RNAV approach with vertical
guidance.
NOTE
ILS approach should be flown with AP coupled to 50 feet above minimums. After AP
disconnect, the pilot should slip as necessary to obtain and maintain runway visibility.
The pilot should consider landing on as wide of runway as possible and landing with a
favorable crosswind (right crosswind with left side pilot flying). If a straight-in approach
with vertical guidance is not available, choose a left circling approach (left pilot flying)
to improve visibility.
(Continued Next Page)
FLAPS
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
TO/APR 108 112 115 119 122 127
* Use in an emergency which requires landing at weights in excess of 8000 lbs.
3-124 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING
(Continued)
2. Landing Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
VREF (KIAS) - STALL WARNING NORMAL
VREF (KIAS) - STALL WARNING HIGH
CAUTION
Avoid landing with a tailwind.
3. Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST AND SECURE
NOTE
Pilot landing visibility may be improved by removing headsets, glasses, etc. If
possible and lowering the pilot’s seat to allow visibility out of the lower left windshield.
4. Avionics and Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. Minimums . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
6. Passenger Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FULL UPRIGHT
7. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
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Citation Mustang airplane flight manual 1(83)
