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Search: Posts Made By: pichu17
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27th Jan 2010, 11:50
Replies: 2,906
Views: 1,450,462
Posted By pichu17

single channel retard?

If my memory not fail the autothrottle flare retard mode is only a double channel ILS app.This plane was in single channel (B)
2nd Jun 2009, 12:49
Replies: 947
Views: 1,115,463
Posted By pichu17

DCate

The problem is the size off antena . In c band must be bigest and there are space limitation in the aircraft nose
Forum: Tech Log
24th May 2009, 16:15
Replies: 6
Views: 4,606
Posted By pichu17

AFB balatón

Is an automatic system ( sb 28-58 or production) to alter the baseline fuel schedule . When both center tank boost pumps are in AUTO position ,float sws cycle the center tanks pumps on and off to...
Forum: Tech Log
24th Mar 2009, 22:30
Replies: 2
Views: 1,185
Posted By pichu17

FMS

The CMA-900,FMS has GPS ,DME-DME, VOR-DME. GPS is the highest priority.The FMS continuosly x check the GPS position against the nex best sensor (DME-DME) to ensure that the position is within the...
8th Mar 2009, 14:55
Replies: 2,906
Views: 1,450,462
Posted By pichu17

RAlt.

Strange airplane: Dont have radio altímeter comparator light. Neither a Test sw
8th Mar 2009, 14:30
Replies: 2,906
Views: 1,450,462
Posted By pichu17

Alfa floor

This funtion in ILS aproach only flashing the Ambar ASA A/T light when detected the A/T can´t maintain the MCP speed and slow to 1.3 vs
In V/S mode the AP/FD change to LCHG pitch mode
6th Mar 2009, 11:08
Replies: 2,906
Views: 1,450,462
Posted By pichu17

ASA light

These conditions cause the A/T warning light to flash AMBER:

_ Airspeed is 10 knots more than target speed and not decreasing.

_ Airspeed is 5 knots lees than target speed and not increasing....
11th Jan 2009, 10:55
Replies: 581
Views: 183,554
Posted By pichu17

Rudder

Rudder hardover evidence is the pedal displacement and hardness .Nothing about this is declared for pilots.
From Boeing about RPR: Valves like this have proven to be reliable in-service....
9th Jan 2009, 21:16
Replies: 581
Views: 183,554
Posted By pichu17

steering

The pedal nose wheel steering became inop when nose gear shock strut is extended until 2.5 inches from the top. An defective state off the shock strut , ( low oil ,bubles ) and a rear CG may relif...
22nd Nov 2008, 12:33
Replies: 3
Views: 4,934
Posted By pichu17

Thankyou gas path

Thankyou gas path
22nd Nov 2008, 11:49
Replies: 3
Views: 4,934
Posted By pichu17

part power

In CFM56-3 the test No .6 is MEC trim check,part power trim.What is part power?
6th Sep 2008, 21:52
Replies: 2,686
Views: 1,140,684
Posted By pichu17

forget All DC9 and md80 series are similar in...

forget
All DC9 and md80 series are similar in this item.
29th Aug 2008, 16:00
Replies: 2,686
Views: 1,140,684
Posted By pichu17

The same relay, the R2-5 ,is responsable for...

The same relay, the R2-5 ,is responsable for both,the rat probe heating and the TO configuration warning. If only this relay is faulty the rest ground sensing system remains ok .Remember the plane...
29th Aug 2008, 12:23
Replies: 2,686
Views: 1,140,684
Posted By pichu17

wow

Wow is in the main landing gear.Ground sensing in in nose gear.The take off configuration warning depend on the ground sensing.This is a group off 15 relays energized when the nose gear is barely...
25th Aug 2008, 12:59
Replies: 2,686
Views: 1,140,684
Posted By pichu17

Especulation.

1) Part of the ground sensing ,change to flight condition.( A circuit breaker open or some wrong in relays or circuit)

2) Pilots, during first takeoff intention, notes the RAT increase and...
24th Aug 2008, 21:18
Replies: 2,686
Views: 1,140,684
Posted By pichu17

Rat probe heater fail.

Mi quest is how the pilot detected this fail. No light,no ammeter current because this heater dont have power in ground.
Secont: the mecanic disconect the heater: HOW? .If pull the respectic CB let...
23rd Aug 2008, 22:02
Replies: 2,686
Views: 1,140,684
Posted By pichu17

Rat,art,atr

In the MD,the RAT probe send temp data into Air Data Computers.These, in digital format feed both digital flight guidance computers.The DFGC compute the EPR for each flight phase and pilot seleccion...
Showing results 1 to 17 of 17


 
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