SMOKE DET LOOP LIGHT ON
CARGO DETECTION SUPPRESSION Panel TEST Switch.............PRESS FOR 3-5 SECONDS AND RELEASE
Normal test indications while switch is depressed:
.
Aural warning plus Master Caution & Warning lights are on.
.
Annunciator panel SMOKE DET LOOP & CARGO FIRE lights are on.
.
BTL 1 & BTL 2 DSCH lights are off.
.
All DET lights are on.
DET light on means that loop is operational.
DET light off means that loop is inoperative.
.
All other Cargo Detection Suppression Panel lights are on.
Caution: If both DET lights for a cargo bay do not illuminate during test, no cargo fire detection for that bay is available.
IF On Ground: Return to gate and contact maintenance.
* * * *
Inflight:
Caution: If the Cargo Fire Detection and Suppression System for a bay containing cargo malfunctions, consider landing at the nearest suitable airport.
IF Both Loops In A Cargo Bay Are Inoperative: Continue the flight at Captain’s discretion. IF Discharge of A Halon Bottle Into Compartment Is Desired:
OR ARM Switch ........ ROTATE TO AFFECTED CARGO BAY
BTL 1 PUSH TO DISCHARGE Switch ....................... PUSH
* * * *
IF At Least One Loop In Each Cargo Bay Is Operative:
CARGO DETECTION SUPPRESSION Panel ......... OBSERVE
IF A Loop FAIL Light Is On: The system has automatically switched to single loop mode. IF A Loop DET Light Is On: The system has malfunctioned. Continue flight and write up in logbook.
* * * *
Sec. 3 Page 40-B MD-80
Rev. 08/01/98 #27 Continental Flight Manual
INTENTIONALLY LEFT BLANK
MD-80 Flight Manual Continental Sec. 3 Page 41 Rev. 05/15/95 #23
FLIGHT CONTROLS
ABNORMAL FLAP LANDING
Note: Use this checklist for landing with flaps not in the normal landing range.
Note: If there is no hydraulic pressure available, refer to LANDING WITH NO HYDRAULIC PRESSURE, this section.
Note: Use longest available runway commensurate with conditions (wet or dry, crosswind, etc.)
Gross Weight............................REDUCE TO LOWEST PRACTICABLE
Approach Speeds......................DETERMINE FOR LANDING WEIGHT
Refer to V-SPEEDS FOR ABNORMAL LANDINGS in Section 5 for
the appropriate Vref speed. If landing with flaps up, do not make wind
corrections to the Vref speed.
Plan a wide pattern and longer than normal final approach for speed
stabilization. Maintain a descent gradient of not less than 2.5..
GND PROX WARN Switch.............................................................. OVRD
Landing Gear................................................................................EXTEND
Gear Lights .................................................................................. 3 GREEN
Anti-Skid............................................................................................. ARM
IAS...........................................................................................ESTABLISH
Fly maneuver speed until on final, then disconnect autothrottles and
slow to approach speed. Avoid excessive flare, make positive gear
touchdown to avoid float.
Note: Be aware of body angle. Tail will strike runway at approximately 11.5. (10.5. on heavy or hard landing).
On touchdown, take positive action to lower nose gear to runway and
apply brakes smoothly to full pedal.
Throttles.....................................................................REVERSE THRUST
Use normal reverse thrust procedures. Do not use asymmetric reverse
thrust to maintain directional control. Rudder control and differential
braking should be used as required for directional control.
* * * *
Sec. 3 Page 42 MD-80
Rev. 01/01/97 #25 Continental Flight Manual
ABNORMAL FLAP LANDING PROFILE
MD-80 Sec. 3 Page 42-A
Flight Manual Continental Rev. 08/01/98 #27
AIRCRAFT OSCILLATING OR DISPLACED IN YAW
DFGC 1-2 Switch ............................... SELECT OTHER POSITION
Airplane Flight Condition Is Normal:
Autopilot / Autothrottles .................................... AS REQUIRED
* * * *
Airplane Flight Condition Is Abnormal:
RUD HYD CONT Lever......................................................MAN
WARNING: Rudder will revert to manual. Minimum approach speed is 135 KIAS until landing is assured.
YAW DAMP Switch.............................................................. OFF
Note: The autopilot must be disengaged to deactivate the yaw damp system.
- - - - - AFTER CONDITION IS CORRECTED - - - - -
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