Temps Froids Flashcards

(44 cards)

1
Q

RCC dans quel ordre sont ils donnés ?

A

RCC dans quel ordre sont ils donnés ?

Rcc: dans l’ordre par tiers de piste, du QFU le plus faible

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2
Q

Flex et contamination:

A

Flex et contamination:

FULL is mantdatory

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3
Q

more than (1/2in)13mm slush, water or wet snow. or more than 102mm dry snow

A
more than (1/2in)13mm slush, water or wet snow. or more than 102mm dry snow
T/O not recommanded
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4
Q

inflight: extended operations or holing in moderate to severe icing condition

A

inflight: extended operations or holing in moderate to severe icing condition
use WAI as anti-icer.

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5
Q

Engine Vibrations in Icing conditions

A

Engine Vibrations in Icing conditions
SP16 CW FAN ICE REMOVAL or (Better) Engine High Vibration NNC
SP16 IGN: FLT - AT off - 80% 1sec one by one - wait 15 sec.
VIB<4 -> repeat every 15 min or sooner
VIB>4 -> Engine Vibration Non Normal C/L

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6
Q

Sp16: comment la traiter

A
Sp16: comment la traiter
Relire en avance, et faire de tête,
trop longue pour de la do-list. de mémoire, sauf opérations de dégivrage et normalisation.
Apu bleed off et pack off, remettre les packs seulement après mise en route.
Structure à briefer:
Prône heat on
Calcul hot
Dégivrage en do-list
Flaps travel
Au point d’arrêt flaps X, fctl Check, before taxy C/l
Besoin de dégivrer a Orly
Demander au coordo.
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7
Q

Temp de protection dépassé et plus de conditions givrantes:

A

Temp de protection dépassé et plus de conditions givrantes:

Demander dégivrage.

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8
Q

WAI au T/O

A

WAI au T/O

prendre en compte ds OPT si besoin entre sol et 1500ft

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9
Q

Qui a la main sur le mélange du liquide de dégivrage

A

Qui a la main sur le mélange du liquide de dégivrage
CDB on demande ce qu’on veut
Icing conditions defintion:
(OAT or TAT<10°C) and Visible moisture or <1600m visi, or contaminant/water is present. (sp16)

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10
Q

CW Contamination admissible avion: frost on lower wing due

A

CW Contamination admissible avion: frost on lower wing due

< 3mm is allowable cold fuel

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11
Q

CW Contamination: controls or leading edge contaminated

A

CW Contamination: controls or leading edge contaminated

unnacceptatble (SP16)

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12
Q

Upper fuselage surface: Thin hoarfrost distinguishable markings: acceptability

A

Upper fuselage surface: Thin hoarfrost distinguishable markings: acceptability
Acceptable (SP16)

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13
Q

CW, Cavité des contrôle surfaces

A

CW, Cavité des contrôle surfaces

must be clear of ice/snow

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14
Q

Snow or ice on the fan ?

A

Snow or ice on the fan ?

snow or ice due ops in icing is allowed if the fan is free to rotate and ice shedding procedure is applied.

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15
Q

Que veut CSFF

A

Que veut CSFF

cold soaked fuel frost (SP3)

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16
Q

CSFF lower surface allowable if

A

CSFF lower surface allowable if
SP3 ALL LE, FCTL, tabs, winglets, balance paned cavities free from contaminants, then:
less than 3mm, or
T>+4, no visible moisture (1600m) & Fuel temps >-16

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17
Q

CSFF higher surface allowable if

A

CSFF higher surface allowable if
SP3 CSFF lines are present & nothing out of the lines.
ALL LE, FCTL, tabs, winglets, balance paned cavities free from contaminants, then:
less than 3mm, or
T>+4, no visible moisture (1600m) & Fuel temps >-16

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18
Q

Cold soaked fuel frost on upper wing of an aircraft with no lines:

A
Cold soaked fuel frost on upper wing of an aircraft with no lines:
not allowed (sp3)
19
Q

CW: Contamination: Eau gelée devant les ports statiques. acceptabilité:

A

CW: Contamination: Eau gelée devant les ports statiques. acceptabilité:
unacceptable (sp16)

20
Q

APU inlet / outflow valv contamination acceptabilité:

A

APU inlet / outflow valv contamination acceptabilité:

unacceptable (sp16)

21
Q

CW: engine/fan snow accumulation during extended shutdown acceptabilité:

A

CW: engine/fan snow accumulation during extended shutdown acceptabilité:
unacceptable (sp16)

22
Q

CW: Contamination: fuel vents acceptabilité:

A

CW: Contamination: fuel vents acceptabilité:

unacceptable (sp16)

23
Q

CW: Contamination: ldg doors acceptabilité:

A

CW: Contamination: ldg doors acceptabilité:

unacceptable (sp16)

24
Q

CW - what is modified in preflight beyond exterior inspection:

A

CW - what is modified in preflight beyond exterior inspection:
Probe heat - on (sp16)

25
CW température below which things start to be complex:
CW température below which things start to be complex: | -35°C
26
CW Engine start
CW Engine start adverse weather heating of HMU by maintenance adverse weather starter servicing by maintenance Oil pressure > normal, and oil filterbypass msg, ok for several minutes, Idle until normal. if oil press > normal after engine oil stabilised: shut down engine. display units may be brighter than normal…warm- up.
27
(OAT or TAT<10°C) and Visible moisture or <1600m visi, or contaminant/water is present.
(OAT or TAT<10°C) and Visible moisture or <1600m visi, or contaminant/water is present. Engine AI on the GROUND IGN:CONT - AI - AIoff -IGN:OFF (sauf au sol, si on les enlève, laisser IGN-cont) off when SATprog2
28
! After setting Engine AI on, if cowl A/A stays bright with engine Idle
``` ! After setting Engine AI on, if cowl A/A stays bright with engine Idle SP16 Check APU BLEED IS OFF check ISOL VALVE IS AUTO check acft clear and increase N1-> 30% ```
29
Icing conditions on the ground
Icing conditions on the ground use WAI between start and T/O unless protected by Fluid Type II or IV WAI-on (may cycle on-off due loic) WAI automatic off when T/O thrust is set. preliminary use is de-ice
30
CW: after start, the flaps stop to a different position than flaps lever
CW: after start, the flaps stop to a different position than flaps lever immediately set the set the flap lever in the same position.
31
CW Before Taxi
CW Before Taxi GEN switches on: wait until stabilized (up to 5 minutes needed) Flight control check after de-icing. Flaps Test: check full down and back before setting T/O Flaps SHOULD THE FLAP STOP: position the flap lever immediately in the same position
32
CW TAXI
CW TAXI minimum thrust above standing deicing fluid Ice Shedding: T<3°, Check area behind the airplane 70% N1 for 30 sec Every 30 min, (including taxi in) heavy conditions: 70% for 1 sec every 10 minutes. after taxi in contamination: do not retract flaps more than to 15°
33
Ice Shedding, résumé des procédures
Ice Shedding, résumé des procédures le fan peut être normalement givré lors de la PPV, si on ice-shed au sol T<3°, check behind airplane, 70%N1/30sec, 30min. T<3°, heavy cond: check behind airplane, 70%N1/1sec, 10min. inflight: Fan Ice Removal SP16IGN: FLT - AT off - 80% 1sec one by one - wait 15 sec. (VIB<4 -> repeat every 15 min or sooner) (VIB>4 -> Engine Vibration Non Normal C/L) High Engine Vibration NNC
34
Engine run up, CW: recommendations ?
Engine run up, CW: recommendations ? éviter les 70% de N1 1 sec toutes les 10 minutes. difficile sur TW Enchaîner runup et T/O
35
CW DE-ICING
CW DE-ICING APU (shut down unless necessary due fumes) Flaps up Idle - Trim set - Eng Bleed off - APU bleed off Holdover time: beginning of anti-icing proc
36
CW AFTER DE-ICING
``` CW AFTER DE-ICING APU as necessary (éviter si possible) 1 minute wait -> eng bleed ON Flaps - T/O Flight control Check ```
37
! Wing has been de-iced, do we use WAI for Take off ?
! Wing has been de-iced, do we use WAI for Take off ? | not if Type II or IV has been applied and is protecting the acft
38
! T/O, icing conditions, T<3°C
! T/O, icing conditions, T<3°C | 30 sec 70% N1
39
If flight in moderate to sever icing condition cannot be avoided, do:
If flight in moderate to sever icing condition cannot be avoided, do: SP16: CW FAN ICE REMOVAL IGN: FLT - AT off - 80% 1sec one by one - wait 15 sec. VIB<4 -> repeat every 15 min or sooner VIB>4 -> Engine Vibration Non Normal C/L Use WAI Use of WAI above FL350 may lead to bleed trip off and loss of cabin pressure
40
CW Altitude temp corrections
CW Altitude temp corrections Correct all minimum altitude inc FAF, app, AD, G/A except, between (FAF and MDA) for minimas VNAV (mais respecter tempé mini) radar vectors or ATC level T>0
41
CW Shutdown procedure after Lansing in icibg condition:
CW Shutdown procedure after Lansing in icibg condition: | stabiliser trim 5 units (avoid water freezing and locking controls)
42
After landing, if contamination or slush, flaps.
After landing, if contamination or slush, flaps. | retract flaps to 15 (sp16)
43
CW Secure procedure:
CW Secure procedure: if warm air circulation in the E/E compartiment is required: APU start - gen on - packs auto - isol valve open -press man - outflow open.
44
Moderate to heavy Rain, Hail or SLeet (neige fondue)
Moderate to heavy Rain, Hail or SLeet (neige fondue) Ref SP16 IGN CONT A/T OFF , adjust thrust manually, slower than AT, do not change direction until stabilisation. maintain minimum thrust setting Reduce speed consider Start APU (why ?)