1. Confirmer l’item, la catégorie et le nombre requis dans le MEL officiel (lien PDF).
2. Appliquer les procédures (O) et/ou (M) du MEL avant dispatch — texte officiel ci-dessous.
3. Placard (texte MEL) :
Apply sticker adjacent to affected display(s) and, if applicable, placard Captain's forward instrument
panel: CAT II OPS PROHIBITED.
4. Journey log / other instructions (texte MEL) :
Print the following information in the journey log sheet.
(#1) (#2) (BOTH) RADAR ALTIMETER SYSTEM(S) or INDICATIONS INOP - VERIFY CAT II STATUS
5. Respecter toutes les restrictions du MEL — ne pas en inventer.
(O) OPERATIONS PROCEDURES — texte MEL :
34-20-01-03 One Radio Altimeter Receiver/Transmitter Inop:
NOTE 1: CAT II operations prohibited.
NOTE 2: For airplanes with -1, -2, or -3 SMYD, an invalid signal from radio altimeter number 1 will
result in failure of both stick shakers to self test.
1. Ensure that weather minimums or operating procedures are not dependent upon its use.
2. With a radio altimeter inoperative, do not use the associated autopilot, associated flight director,
or autothrottle for approach and landing.
NOTE: The FCC engages LNAV when the radio altimeters indicate that airplane is 50ft above
ground level (AGL). Dispatching with an inoperative radio altimeter system may
generate an erroneous radio height indication of 50 ft AGL and may cause the LNAV
FMA to flash when armed on ground.
3. For airplanes with FCC Operational Program Software (OPS) 2212-HNP-03B-05 or later installed,
if the remaining radio altimeter fails:
NOTE: Rockwell Collins FCC Operational Program Software (OPS) part numbers are
considered to be equivalent to Honeywell FCC OPS part number 2212-HNP-03B-05 and
later.
a) AFDS (both sides) will limit the bank angle to a maximum of 8 degrees in all roll modes.
b) Use of the Autopilot/Flight Director System (AFDS) is at the discretion of the flight crew.
AFDS may not:
1. Command sufficient bank angle to execute proper departure and/or approach
maneuvers.
4. Make enroute course changes within airspace limitations.
5. For airplanes without FCC Operational Program Software (OPS) 2212-HNP-03B-05 or later
installed, dispatch with an inoperative radio altimeter:
NOTE: Rockwell Collins FCC Operational Program Software (OPS) part numbers are
considered to be equivalent to Honeywell FCC OPS part number 2212-HNP-03B-05 and
later.
a) Results in the same side Autopilot/Flight Director System (AFDS) limiting the bank angle to 8
degrees in LNAV mode.
b) The opposite side AFDS (operative radio altimeter) is not affected.
c) Failure of the remaining radio altimeter can result in:
2. AFDS (both sides) limiting the bank angle to a maximum of 8 degrees (all roll modes)
when flaps are extended, 8 degrees in LNAV with flaps retracted.
3. Use of the Autopilot/Flight Director System (AFDS) is at the discretion of the flight
crew. AFDS may not:
i) Command sufficient bank angle to execute proper departure
and/or approach maneuvers.
ii) Make enroute course changes within airspace limitations.
34-20-02B Indications - Associated Receiver/Transmitter Verified To Operate Normally:
NOTE: CAT II operations prohibited.
Ensure that weather minimums or operating procedures are not dependent upon its use.
(M) MAINTENANCE PROCEDURES — texte MEL (maintenance ; l’équipage vérifie que c’est fait) :
34-20-01-03 One Radio Altimeter Receiver/Transmitter Inop:
Do these steps (AMM 34-00-00/901):
1. Open and collar associated P6-1/P18-1 panel Radio Altimeter circuit breaker to deactivate the
inoperative radio altimeter.
NOTE: With one radio altimeter deactivated, the SPEED BRAKE DO NOT ARM light will
illuminate on the ground when speed brake handle is moved from the DOWN detent.
2. For airplanes without FCC Operational Program Software (OPS) 2212-HNP-03B-05 or later
installed, re-initialize the Flight Control Computer (FCC) associated with the inoperative radio
altimeter by momentarily opening and then closing the applicable P6-2/P18-1 panel FCC circuit
breaker.
NOTE: Rockwell Collins FCC Operational Program Software (OPS) part numbers are
considered to be equivalent to Honeywell FCC OPS part number 2212-HNP-03B-05 and
later.
3. For airplanes with PSEU part number 285A1600-5 or earlier, refer to MEL Item 32-17. An invalid
radio altimeter signal will generate a dispatchable PSEU fault.
(M#) MAINTENANCE PROCEDURES — personnel maintenance obligatoire — texte MEL :
34-20-02B Indications:
To verify that the associated receiver/transmitter is operating normally, refer to the Airplane
Maintenance Manual for troubleshooting and system test procedures (AMM 34-33-00).