System, Description and limitation differences 系统、描述和限制差异
**** Hidden Message ***** B737 -800/AICLlFOB-791iI1~ .""""'''''111
~Xp~SS
AIR-INDIA CHARTERS LIMITED
OPERATIONS DEPARTMENT
FLIGHT OPS BULLETIN
To: ALL FLIGHT CREW
Ogth February, 2007
Sub: 8737-800 aircrafts System Differences
Enclosed herewith is the list of differences of 8737-800 aircrafts in our fleet.
It is, therefore, advised to keep the differences in mind and the procedures thereof
while undertaking the flights.
The above is for your information and guidance.
(Capt. Rajeev Bajpai)
Chief of Operations
cc: Chief of Flight Safety
cc: Chief of Engineering
cc: All Ground Instructors
cc: All Technical Officers (HQ)
cc: Documentation Section, OAP! NIPTC
System, Description and limitation differences between Air India Express owned and dry leased Airplanes
Note: The remarks coloum consist of respective page numbers where the topics are present. Page no. are displayed as per following pattern: Dry
leased / Expressed Owned
Sr.
Systems Description,
No.
Equipment and
leased AirplanReemAaXrAk,sB,/ECRx,Dperf,eeEsr,eFsn,Gcoewned AXH,I,J,M,N,P
1
Tailwind component L.10.1/L.1 01.10 kts15 kts
Max. crosswind during tio
AXA-AXC -- 36 kts, AXD-AXG -. 33kts
L.10.21 L.10.1 (Check 33kts
Annexure 1)
3
landing weather minima
HW - 25 kts, CW - 20 kts, TW - 10 kts
L.H1W0.3-/2L5.1kt0s.,3CW - 25 kts, TW - 15 kts
pilot landing
4
Autoland capability with
ntooinbfe1orLum.s1ea0dt.io3onnly with flaps 30
Emergency lighting and
NO SMOKING Sign- AXA - has three position. AXB
passenger signsAoXnG -- NO smoking sw1i.t3c0h.7is/1c.o3n0s.7tantly illuPmlaicnaartdeedd. - CHIME ONLY,
So the switch is inoperative (Placarded - INOP)
annunciator . AXD & AXE - Annunciator light above EQUIP is lights on forward There is no Annunciator above EQUIP 1.30.13/1.30.12
placarded INOP
Oxygen mask panel
Location of tesUReset switch is to the left side of
Locat1io.3n0.o1f6Te11s.U30R.e15set switch is on top right side of Red clip
Oxygen Mask donning
Refer page 1.40.11of FCOM volume II
Refer Page 1.40.10 FCOMValli I
PB/GKlDiff
9
Location of Emergency
Refer page 1.40.20 & 1.40.21 of FCOM valli
Refer Page 1.40.20 of FCOM Valli
10
Number and lacatation of
AXD & AXE - three life rafts
1.40.20, 1.4021 11.40.20 Four life rafts Window no. 3 is electrically heated to prevent
Flight Deck Window heat
Window no. 3 isn't electrically heated since it consist
RfoegfgeirngdiaTghraemrmaal t spwagitcehes located on window no. 3
helps to m3.a2in0t.a3in correct temperature of window
Speed control Panel on
AXB - AXG doesn't have speed intervention switch.
4.10.2 f 4.10.1 Has speed intervention switch.
AXB - AXG doesn't have altitude intervention
Has altitude intervention switch.
4.10.5/4.10.4
AXB - AXG -VNAV mode will not engage if the
airplane altitude is in between FMC altitude in RTE
In4c.1a0s.e6/4o.f10co.4nflict the airplane levels and VNA V altitude is maintained
airplane levels and VNAV altitude is maintained.
on glareshield
VNleAvVel SofPf,DautotoAthLroTtAtleCOwildl AutarXirnBgget-dAutoXriGnlAgSw,ihnetirenrremsPpidieteccthteivemode is changed from
--
4.10.71
VIS, the airspeed wreinsduoltwinoopveenrsspwe"itehd IAS which may
During VNAV path Descent when pushed,
switch
No altitude intervention switch
automatic trans4it.io1n0.1t1o/4a.1V0.N9AV speed is made if all
deleted.
No ROLL OUT indications
4.10.2R2O/4L.L10.O20UT indication (green)
(FMAs) -- Roll Engaged
mode No LNAV, LNAV ROLL OUT indications
LNAV ROLL OUT (white) and LNAV (white)
4.10.22/4.10.20
PB/GKlDiff 2
Flight mode annunciatons
16
(FMAs) -- Pitch mode VNA V AL4T.1i0n.d2i2cat1io4n.s10o.2n1lyVNinAVAXAAL T indications
17
Flight mode annunciatons
No >LAND 2< and NO AUTO LAND indications
>LAND 2< (green) and NO AUTOLAND (amber)
4.10.23/4.10.21
indications
18
(FMAs) -- Pitch armed No 4V.N1A0.V23Vi/n4Nd.iA1cVa0t.i2o(1nwshite) indications
When TO/GA is pressed after touchdown with both
When TO/GA is pressed after touchdown with both
Autopilot disengagement
AlPs engaged in CMD
AlPs engaged in4.C2M0.D2/4(e.2xc0e.2pt when LAND 3 or
--.---"" Fail operational Autoland
No annunciation
Features LAND 3. LAND 2 AND NO AUTOLAND
14.20.4
annunciation
VNAV (armed) is displayed if armed prior to TIO,
ft RA. 4.20.4 14.20.6
Pitch mode
annunciation. After LaC and GIS capture, in addition of second
4.2A0lP.12e/n4g.a2g0m.1e4nt, autopilot rudder servo test is
annunciated
At 500 ft RA , check for LAND 3 or LAND 2 so as to
4.20.12/4.20.14
Alignment mode is enabled. But there is no
4.20.15
No RROOLLLLOOUUTTinadrimcastiownhsen LAND 3 or LAND 2
and landing 4.20.15
annunciates.
Prior to LAND 3, LAND 2, annunciation, Alp
present
disconne4c.2ts0.1i6f LaC or GIS beam anamoly is
Single4.2e0n.g1i6ne autolanding annunciations are provided along with automatic rudder compensation
.
PB/GKlDiff 3
If engaged AlP controls assymetric thrust control
G/A by AlP
and g4e.t2s0.d1is8engaged only if new pitch mode is
Go Around
No Go around Roll mode annunciation and
Go aroun4d.20R.2o1ll mode annunciations along with command engagment of certain AFD features
If speed limit to particular mode is exceeded, the
If speed limit to particular mode is exceeded, the
4.20.22/4.20.24 AfT will revert speed back slightly less than the
AfT will revert speed back to placarded limit speed.
placarded limit speed.
Radio tuning Panel fail
AAA - has feature to display Radio FAIL mode
5N.o10.R3adio FAIL mode display is present
26
Audio Control Panel
AXB -AXC have a mask -boom switch
5.10.4 NO mask boom switch
27
SELCAL PaAnXeSl , AXC have separate SELCAL panel along with
NO separate SELCAL panel is provided
5.10.10
ACARS printer notParveasielanbt le5o.1n0.a6ft electronic panel
Communication contois Doesn't lolocckksontotoIN5ITN.1pT0o.s1pi2otio/s5int.i1o0nu.9ntil selected OFF or MIC
appliedAr5et.o1a0A.m1ir6pic/lar5on.1pe0h.o1n1e activate anytime 115V AC is
Cockpit voice Recorder
cockpit voice recorder swich is availble at Forward
No switch is available
5.10.17
PS/GKlDiff 4
31 Call system
AXB,AXC have flight deck call light which
Indication comes on integrated audio control panel.
5.10.18/5.10.12
Inoperative
Flight instuments available on AXB,AXC are
and battery power is
standby instruments, while on AXA, AXD-AXG -
Integrat6e.d20.s1t5andby flight instrument display and
Integrated standby flight instrument display along
standby instruments
Fuel Quantity display Dia! form on Upper display unit, in kilograms
Numeric display in kg * 1000 , along with total fuel
7.11.1
LE FLAP TRANSIT LIGHT illuminates until LE
/9.10.12
devices is fully extended and TE reaches flals 25
Lever stop feature is available which prevents
SPEED
SPEE/9D.20B.1R4AKE lever to move beyond FLIGHT DETENT, in flight and flaps up. The feature is
removed when electrical power is lost.
When 9F.2L0A.P18/l9e.v2e0r.1i7s moved to 1,2,5,10,15,25 the TE flaps extends to commanded position of the lever.
Flight controls
If FLAP lever is moved beyond 5, TE flaps extend to
If FLAP lever is moved beyond 25, TE flaps extend
with
to com9m.2a0n.1d8 p/o9s.2it0io.1n7 and LE flaps extend along with
full extension of slats.
Fl9a.p2s0/.s1l9a/t9s.20e.1le8ctronics units provide flap relief operation for flaps 10,15,25,30 & 40.
9.2A0u.1to9s/9la.t2s0.1fu8nction is available at flap position
1,2,5,10,15 and 25
PB/GKlDiff 5
No Vref speed annunciation on PFD airspeed
Vref speed annunciation are present on Airspeed
indications, indicates selected landing flaps position
/10.11.8
and Vref
disagree alsert message comes if the
difference of 1/010d.e1g1r.2e6e or more is continuous for
Vertical situation display shows vertical profile of
/10.11.32, 10.11.36,
airplane and its1e0n.1v1ir.o3n7ment along with current
Flight Instruments
No track failure flag
Track failure flag1, 0s.1h1o.w42s/1t0ra.1c1k.4d8isplay has failed"
AXB, AXC -NO ADF 2 switch selection on EFIS
Has A10D.F16.21 selection switch along with VOR 2 selection on EFIS panel
AXA, AXC-AXG - has integrated standby flight
10.16.12/10H.a1s6.1in1tegrated standby flight display.
doesn't have ADF 2 selection on standby
Has ADF 2 selection on standby RMI
10.16.20/10.16.16
PDFDoesn't show numerical landing FlapNref on PFD
Shows/1n0u.3m1e.1rical landing FlapNref on PFD once FlapNrefis set in MCDU aproach Vref.
elevation
Has Terrain obstacle and Terrain elevation features
10.41.13/10.41.15
NO TCAS also gives absolute altit1u0d.e41a.D1d5ov/ei1ss0on.r4'yt1.h1a8ve absolute altitude advisory
/10.65.1 Has Electronic flight bag
EeFleBctrical motor pumps, Power is removed from the
In13c.a2s0e.3o/1f0o.2v0e.r2heat in the electrical motor pumps then only OVERHEAT light illuminates
Hydraulic System
AXA - AXC - Nose wheel steering wheel is on
Nose w1h4e.1e0l .7steIe1ri4n.g10.w7heel is on Captain's and FIO side panel
PB/GKfDiff 6
Has Autoland Advisory messages whenever system
Landing Gear No Autoland Advisory messages
faults affect autoland status.Advisory messages can
MFD /15.10.3/15.20.7
panelwhich displays one messages at a time.
peak below
Terra/i1n5.1p0e.a1k0 below 2000 ft of airplane altitude is displayed.
In addition to TERRAIN annunciation it also gives
15.10.9/15.10.10
Warning messages
Doesn't display Terrain Elevation
Displays highe/1s5t .1a0n.d11lowest elevation of terrain.
displayed /a1n5d.20a.l1e2rt/i1n5g.2p0r.1o3vides caution and warning
15R.2a0d.1io4 ailt1itu5d.2e0.1c6ailouts start from 2500 ft.
PB/GKIDiff 7 谢谢，下载了看看先 很好的资料，谢谢分享
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