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SAFE WINGS This issue… ICE CRYSTAL ICING 1971 WAR: A VOLUNTEER REMEMBERS * For Internal Circulation Only Flight Safety Magazine of Air India, Air India Express and Alliance Air Issue 39, AUGUST 2015

Mining Large Streams of User Data for Personalized - SIGKDD

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Page 1: Mining Large Streams of User Data for Personalized - SIGKDD

SAFE WINGS

This issue…

ICE CRYSTAL ICING

1971 WAR: A VOLUNTEER REMEMBERS

* For Internal Circulation Only

Flight Safety Magazine of Air India, Air India Express and Alliance Air Issue 39, AUGUST 2015

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

SAFE WINGS August Edition 39

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Intentionally left blank

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August Edition 39 SAFE WINGS

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

SAFE WINGS August Edition 39

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here are many articles on this subject in Aviation journals, however

none of them cover the events that have occurred in our airline on the

B737. High Altitude Ice Crystals have been recognised as a cause of

Engine damage and power loss that effects many different types of

airplanes. These events have occurred in conditions which pilots associate

with benign weather conditions with at most only light turbulence. The

conditions may sometimes even typically be classified as non-icing

conditions because super-cooled liquid water is not present at these

temperatures. Ice crystals normally do not adhere to cold surfaces because

the ice crystals bounce off. However the ice crystals can partially melt and

stick to relatively warm surfaces. Due to engine roll back and power loss

events, more recently on the B747-8 and 787, FAA has even issued an

Airworthiness directive (AD) 2013-24-01 on 27 Nov 2013. Boeing has also

issued a Technical Bulletin on the subject and also included procedures in

FCOM/QRH to be accomplished during suspected Ice crystal Icing. In the

B737 we have had a few suspected Ice crystal icing events which though

having some similarity to the events described by Boeing, haven't caused

engine damage or failure. The events on the 737 are described here. The

pilots reports were further authenticated by Flight Data Recording (DFDR)

data.

T

ICE CRYSTAL ICING

:- By Capt Vivek Kulkarni

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August Edition 39 SAFE WINGS

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

In all the events that occurred in the airline to the B737, the aircraft was

between latitudes 12 North to 17 North, between Flight levels 330 to 370

and TAT was between -10 to -17. There were no Cb clouds even well below

the aircraft but the aircraft may have flown through the anvil like cloud of a

dissipated Cb. The radar returns indicated intermittent light green and there

was light turbulence. In some cases engine anti-ice was switched on except

when SAT was below -40, the engine anti ice was off.

In all the events the following was noticed:

1) The TAT increased rapidly to 0 degrees over a period of about 10

seconds.

2) Speed steadily dropped by about 10 knots. In cases where the aircraft

was at Optimum or Above optimum, due to the smaller margin between

cruise speed/Mach and Max and Min speeds, this 10 knots decrease brought

the indicated speed close to lower amber speed band.

3) The Auto-throttle increased thrust in an attempt to return to selected

The image depicts a view of a CB cloud. The aircraft has avoided the Red and amber areas on weather

radar and is passing through the relatively “safe” anvil cloud. The Avil like cloud can contain High Ice

Water Content (HIWC).

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

SAFE WINGS August Edition 39

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speed/ Mach but in spite of the Auto-throttle increasing thrust to the limit

set in the FMC (ie Cruise or MCT), it was unable to regain speed. In one

case the airplane had to be descended to regain the selected speed.

4) The thrust limit N1 had reduced by about 4 percent.

5) There was no Surge/stall or any adverse effect noticed on the engine.

Though the Industry is still not very clear how Ice crystal ice causes

adverse effects on the aircraft, we suspect the following:

Whereas super-cooled water drops is present in Vertical development

clouds above freezing levels, very minute particles of Ice Crystals are

present in high altitude clouds. Sometimes as in an anvil like cirrus cloud

which is the remnant of a spent Cb, these minute ice crystals may be

present in large quantities.

One such event described here is a firsthand account and the sequence of

events are as follows: The aircraft was at the optimum altitude ie FL 360

halfway between Mangalore and Dubai. It was night time and the weather

radar was painting intermittent green and it was obvious that the aircraft

was in cloud due to reflection from the strobe lights. There were no red or

amber returns in the vicinity even with the weather radar tilted at -3

degrees. Engine limit thrust had earlier been manually changed from

“Cruise” to” Continuous”. Due to an earlier experience the engine

parameters were noted and the Max Continuous limit displayed on the FMC

was noted as 100.5. The TAT at FL 360 was – 16 degrees and after about 5

mins in the cloud as described above, the TAT over a period of about 15

secs increased to 0 and then hovered at 0 to -1. The aircraft speed started

dropping steadily and it was noticed that the Auto throttle had increased

thrust to the N1 limit. However the N1 limit was now indicating 97.0

percent N1. Inspite of the Auto throttle maintaining 97.0 N1, the speed

continued to drop. When Auto throttle was disengaged and thrust increased

to the thrust limit noted earlier, ie 100.5, the speed decay was arrested, A

short while later the TAT started dropping and returned to its earlier value

of -16 and now the aircraft speed started increasing and thrust had to be

reduced accordingly. Auto throttle was reengaged and thereafter operations

were normal.

From the above we deduced the following. The tiny ice crystals may have

attached to the TAT probe which is heated. On contact with the heated

surface, they may have melted, which caused the TAT probes to sense a

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August Edition 39 SAFE WINGS

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

(false) higher TAT. The TAT is also transmitted to the engine EEC. Normally

at higher temperature, due to the reduced density, the mass flow of air into

the engine is lower and hence the fuel fed into the engine needs to be lower

to maintain the air/fuel ratio. The thrust will naturally decrease. In this

case, the Auto throttle sensing the speed reducing, increases the thrust to

the N1 limit to maintain speed. However, the EEC fed with a (false) higher

temperature, reduces the N1 limit too, because it assumes that higher TAT

at the same speed means that OAT has increased.

To understand the phenomenon better, we can compare this to using

Assumed Tempe / Flex Temperature .We know that we “cheat” the EEC by

feeding it a false OAT ( Assumed temperature/Flex Temperature ).This

causes the EEC to set a lower N1 based on the “assumed” outside air

temperature. In other words we are “cheating” the engine to believe that

the temperature outside is high and it has to regulate the fuel flow

accordingly. The net effect is that less thrust is produced so that we can

achieve a Reduced take off thrust .In such cases regulations permit you to

increase thrust to maximum in an emergency such as wind-shear because

the actual OAT is much lower than what has been fed into the FMC.

A similar phenomenon probably occurs when Ice

crystals melt on the TAT probe and transmit a

“false” TAT. In suspected Ice Crystal icing if this

occurs, the thrust could be increased to the correct

MCT to prevent an unsafe condition (incursion into

the lower amber band or worse stick-shaker). You

have to anticipate though that when the TAT

indication returns to normal, the increased thrust

will increase the aircraft speed and thrust will need

to be regulated to prevent an over-speed event.

Summary

Different aircraft types have had varying events

due to Ice crystal icing. Pilots are advised to read

articles on the subject with particular attention to

events that have occured on their aircraft type,

Since the Industry is still analysing suspected Ice

Crystal Icing events, any events that may in your

opinion relate to the subject should be promptly

reported to the Flight safety department.

:

Capt V. Kulkarni is

an ex-Naval pilot. He

joined Air India in

1987 and has flown

the A310, B747

Classic, B747-400,

B777 and is presently

flying the B738 and is

also the Chief of Flight

Safety, Air India

Express.

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

SAFE WINGS August Edition 39

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y experience of the 1971 war began a few days before the outbreak

of hostilities. I was at that time doing ground duty tenure at CAC

Allahabad. The buzz in the offices and corridors of our building was

palpable. There was an air of detached sense of expectancy.

Meanwhile in the squadrons the imminent certainty of war meant that all

preparations were well and truly in place in a measured way. Unlike the

pre-1965 war scenario induction of pilots on ground duties to bolster the

pilot strength in Squadrons was not a critical need. To me however the

comfort zone of a desk job away from the reality of action was

disconcerting. Call it payback time or an expression of confidence in oneself

built on the back of my 1965 operational experience I volunteered for action

and was quickly assigned to No.35 Sqn. then based in Poona.

Poona was the launch pad for targets in southern Pakistan. The limited

range and reach of Canberra aircraft at low level meant a refuelling halt at

Jamnagar on our way out to targets. It proved to be a welcome break for us

to meet with Gp.Capt.Pete Wilson Vr.C. Stn.Cdr. Jamnagar, a veteran of

Canberra operations and my mentor in more ways than one.

Of the 6 night missions that I undertook from Poona, 2 are worth

mentioning here; one for a lucky escape and the other for a side show

narrative to the leaping flames of Karachi on a night raid.

M

1971 War: A Volunteer Remembers

By :- Capt K.S.Chandrasekar

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

And so it was on 8th Dec.1971. after a reassuring tarmac chat with Groupie

Wilson over hot tea on a cold and wintery night on our way to Drigh Rd., a

satellite PAF base close to Karachi. No worries and mission successful, I was

down to deck level over the dark waters of the Arabian Sea heading south

away from the prowling eyes of Pak radar , eased my body, silently ebbing

away the adrenaline. Close to Jamnagar I had just initiated my climb to

Poona when the silence was broken with the calm voice of Groupie Wilson

asking me to get down fast. No questions asked, I realised I was not the

only one in the night sky at that point. Instinctively I went into a spiral dive,

throttles back, speed brakes out to hit the deck back to the safety of the

black and glistening surface of the waters whizzing past below. After what

seemed an eternity at low level and reassured with an all clear from

Groupie Wilson, I made my way up again back to Poona with near dry

tanks. Back again on 9th. Dec., another mission and another tarmac chat

with Groupie brought home the reality of the previous night's close call. The

Pak chase plane ( had to be a F-102 for it to gain on me so rapidly ) was

picked up by our radar in time to wake me to action. The rest is safe inside

me since then. Lucky are the ones that live to tell a tale another day.

The side show of the night on 15th. Dec. 1971 (the last day of the war).

This was a night raid on the Karachi harbour installations. As leader of a 6

aircraft raid, planning and briefing carried out, we were off in a stream from

Jamnagar on a circuitous route via Bhuj, approaching the target from the

north. Even far out at low level it became clear that navigation that night

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SAFE WINGS August Edition 39

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was going to be easy. We had a homing beacon in the form of a gigantic

inferno lighting up the night sky from miles away. Our Hunters and Naval

boats beat us to the job earlier and made our job easy by lighting up the

target. Closing in, the leaping flames were riveting and yet distracting. As

we made the final bombing run, the effect of our bombs hitting the target

reignited another burst of shooting flames sky high. A spectacle to carry

away with you forever as I sped away with blinking eyes and a nodding

head in disbelief at the sights of the night.

Capt Chandrasekar joined

Air India in 1976. Prior to

Air India he served in the

Indian Air Force and retired

as a Wg.Cdr. He was

awarded a Vayu Sena Medal

(Gallantry). During his

career in Air India he has

flown B707, A300 and B747

and has been a Training

Captian throughout. He is

currently a Simulator

Instructor with Air India

Express on B737.

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F l i g h t S a f e t y M a g a z i n e o f A i r I n d i a , A i r I n d i a E x p r e s s a n d A l l i a n c e A i r

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PROMISING A SAFER SKY, AIR INDIA, AIR INDIA EXPRESS & ALLIANCE AIR

We give utmost importance to your valuable comments and feedback. Please do mail us at

[email protected] or

[email protected]

Editorial: -Capt. V. Kulkarni, Bhavish B S, Designed by Bhavish BS