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it.pilot737
14th Jan 2007, 11:38
Hello......
About the aerodorme reference reference code, the B737 is 4 C.... Is somebody knowing the minimum rwy with for 737? is it 45m?

FlightDetent
14th Jan 2007, 15:20
-400/500 had 30m I guess...

c100driver
14th Jan 2007, 23:56
Air NZ and QF use two airports with 30m x 1500m (Used to use one of 30 x 1300m on the B732) for sked services with the B733 here in the south pacific.

OverRun
15th Jan 2007, 00:08
For normal operations, the 737 runway width requirement is 45m, but yes, it does operate on 30m under certain restrictions. These vary between countries and airlines, but typically include:

Limitations:
- Minimum runway width 30m
- autoland is not allowed
- specific approval by Department of Aviation and Chief Pilot
- more restrictive cross wind limits, visibility requirements and crew qualifications

Dispatch from/to narrow runways is not allowed in case of:
- nose wheel steering inoperative
- one brake or more inoperative.
Furthermore some VMCG corrections have to be applied for takeoff performance calculations.

Spitoon
15th Jan 2007, 15:36
IIRC to be an ICAO runway code 4C it must be 45m wide.

OverRun
15th Jan 2007, 22:05
Yes, ICAO 4C is a minimum of 45m wide. The 737 ops into a narrower runway are done under concession.

Some background to runway width required, and some work done on this, is at http://www.pprune.org/forums/showthread.php?t=114235
Quoting JT from that thread who wrote about a rational handling assessment for aircraft intended to be operated from lesser width runways:
The concerns were purely operation .. regarding
(a) CL deviations during a failure for reject/continue cases
(b) worst case considerations for the wet runway case
(c) late final landing manoeuvring following a misaligned letdown and a side-step manoeuvre .. wonderful to watch from the ground ..
The main thing to come out of the work was that the lateral deviations can be a bit hairy depending on the proximity to Vmcg at Vef and, of course, depending on crosswind.

greek-freak
16th Jan 2007, 14:50
A lot of the smaller Greek island airports have 30m wide runways eg Karpathos, Skiathos, Zakinthos.
Apart 737s and A320s in summer there even seem to be operations with 757s and 767s in Zakinthos.

gonso
17th Jan 2007, 01:19
Greek-Freak, I must correct you on the Zakinthos width. It is 45m. :8

alexban
17th Jan 2007, 15:34
I did some search and I couldn't find any special restriction or requirement about 30 m width rwy,and 737 operation.
Could you give me some hint where to find an airport reference code,or requirements for the 737 on a 30m wide rwy?
I seem to remember reading about this in our OM,but I couldn't find it any more.Maybe it was removed due to the fact that we now often operate on some 30 m wide rwy's.:ugh:
So,where is it , in ICAO,Jarops 1 ...?

inducedrag
17th Jan 2007, 19:58
How about Airbus A320 and A310:ok:

FlightDetent
18th Jan 2007, 07:03
alex / id:
My memory may be fading, but the 737 (-500/400) I've flown had RWY width limitation of 30 meters and certainly were used that way, JAR OPS1 operator. Nowhere I had seen 45m number. The 320, on the other hand, has 45m NOMINAL width requirement, in FCOM 2 you'll find chapter operation on narrow runways and observing that (and certain paperwork) you can go to 30m as well.
link (http://www.mapy.cz/?mapType=ophoto&zoom=14&centerX=129637568&centerY=136421376&portWidth=938&portHeight=684&forceMapParams=1&query=Ol%C5%A1ov%C3%A1%20Vrata&page=1&searchPort=120181669_123783041_150918053_150357889)

I suppose the 45m 737 requirement was for the NG, that has noticeably larger wingspan, perhaps?

OverRun
20th Jan 2007, 00:18
ICAO use a code system, known as the Aerodrome Reference Code, to specify the standards for individual aerodrome facilities which are suitable for use by aeroplanes within a range of performances and sizes. The Code is composed of two elements: element 1 is a number related to the aeroplane reference field length; and element 2 is a letter related to the aeroplane wingspan and outer main gear wheel span. Thus 4C is an aeroplane reference field length greater than 1800m (4) and wingspan 24m to less than 36m/outer main gear span of 6m to less than 9m (C). This detail (and all the limits) is found in the ICAO aerodromes manual, and the UK CAP 168 at section 2.2, and in similar publications from other countries. The linkage between aerodrome reference code and minimum runway width is found in the same publications, such as section 3.2 of the CAP 168 http://www.caa.co.uk/docs/33/CAP168.PDF

Note that the aeroplane reference field length is solely for the selection of a Code number and should not be confused with operational runway length requirements, which are influenced by other factors. [I like to think of it as TORR for accountants <grin>]

This ICAO Aerodrome Reference Code is not the same as the JAR-OPS aeroplane category which is related to indicated airspeed at threshold (such as JAR-OPS 1 Subpart E, Appendix 2 to JAR-OPS 1.430c). Confusingly, the codes look similar. There was a Tech Log post a couple of years ago where the circling minima (which were in terms of aeroplane category) were linked to the runway strip width (in terms of aerodrome reference code) and it had me confused for quite a while until I turned up a simplistic rule of thumb that the bit where the aircraft is on the ground is dominated by the ICAO Aerodrome Reference Code, and the bit when it is in the air it is dominated by the JAR-OPS aeroplane category. The link between operations, JAR-OPS, and the aerodrome reference code is found cryptically in JAR-OPS 1.220 where An operator shall only authorise use of aerodromes that are adequate for the type(s) of aeroplanes and operation(s) concerned
All model B737s are code 4C aircraft, from the -200 throught to the -900. The A320 is a code 4C aircraft. The A310 is a code 4D aircraft (like all widebodies and the longer narrowbodies including the B757-200).
There are lists published of aircraft with their ICAO aerodrome reference codes to save having to work it out each time. The Australian list is in Chapter 2.1.6 of their MOS139. The Transport Canada have another list. The Oz one is here: http://www.casa.gov.au/rules/1998casr/139/139m02.pdf
It is interesting to see the interpretation of this requirement in action. If the aerodrome is not adequate for the type of aeroplane/operation under JAR-OPS 1.220 (and I think that failure to meet ICAO runway width might be such a case), then the operator/authority must do something to make it adequate. This is done here by adjusting the operation to make the aerodrome suitable. Putting operational limitations in place to cope with the effect of reduced width is a way of doing this (such as those limits discussed in earlier posts), and clearly is a common enough action.
I am familiar with B737 ops on 30m wide runways - both the -400 and the -800 series. They are normal at several Australian aerodromes, such as Ayres Rock and the busy Gold Coast/Coolangatta; even though the bulk of Australian 737 operations are on 45m wide runways. I have seen the written dispensation by CASA to the operator for at least one of these 30m runway operations, and it was an open-ended dispensation [that is, it was without time limit although I think there were some operational restrictions]. I reckon there must be some such dispensation in place covering operations at other 30m wide runways elsewhere in the world, because this ICAO runway width requirement is a very long standing one and not easy to ignore.

737incognito
1st Apr 2007, 10:57
Does anybody has an extract from OM or similar publication specifying under which conditions rwy width can be reduced to 30m foe B737?

john_tullamarine
1st Apr 2007, 12:54
Does anybody has an extract from OM or similar publication specifying under which conditions rwy width can be reduced to 30m foe B737?

Be a tad careful. Normally, most States will adopt the ICAO practices. If not the usual variation can be published. Generally, an individual State will determine under what conditions concessions may be granted .. and such conditions may vary from State to State .. ie, if you get access to OM data from operator A .. it may not have much relevance to your operation around the other side of the globe.

mutt
1st Apr 2007, 16:23
Boeing has a special takeoff analysis program for operating the B737 from narrow runways, although, under the FAA system they do not have any limitation on the runway width.


Mutt

I Just Drive
1st Apr 2007, 19:37
Buzz and Ryanair used to operate into La Rochelle which I think only used to be 30M. The only restriction in place was a xwc limit higher than normal.

737incognito
4th Apr 2007, 06:12
What exactly is the definition of "Aeroplane reference field length".

Sleeve Wing
4th Apr 2007, 09:42
Some years ago but remember having to take off from a snowy DUB in a -400, just after they'd reopened for an Air Ambulance flight.
The CLEARED WIDTH was 30m. The airfield was to be closed again indefinitely for snow clearance afterwards.
Only other OM restrictions were a snow banks limit of, IIRC, 50cms., no crosswind and usually braking/reverser restrictions.

(Strange thing was that ATC would not allow a Fungus 73' to depart, saying conditions were outside his limits ???) :hmm:

quickturnaround
4th Apr 2007, 10:16
The 737 classic and ng even lands well on a 28m wide strip as was the case on Mayote.
Off-course with the nessessary V1 and weight/thrust calculations involved. Piece of cake.... The acft doesn't know the width of the runway involved....
Fly safe QTA

Wycombe
4th Apr 2007, 10:25
Southampton (SOU) Rwy 20/02 is I think 37m wide and sees regular-ish 737 Ops (eg, European/Titan when flying for Flybe). Has seen the odd 757/320 aswell, esp in Summer.

OverRun
8th Apr 2007, 07:37
Was at last able to haul out the paperwork and find, from the Australian AIP ENR 60_1, the definition sought by 737incognito, which is:

An aeroplane's reference field length is:
(1) in the case of an aeroplane to which section 20.7.1B of the Civil Aviation Orders applies (see below but basically civil turbines & jets) – the balanced field length; or
(2) in the case of any other aeroplane – the take-off distance; that the aeroplane requires for take-off in accordance with subpara b. below:
b. For the purposes of sub-para a. (1) and (2) above, the balanced field length or take-off distance that an aeroplane requires for take-off is the balanced field length or take-off distance that, according to its flight manual, the aeroplane requires:
(i) on a level runway,
(ii) at maximum take-off weight,
(iii) in still air,
(iv)at sea level, and
(v) in standard atmospheric conditions.


Section 20.7.1B of the Civil Aviation Orders says:
Subject to paragraph 2.2, this section applies to:
(a) all turbine powered aeroplanes having a maximum take-off weight in
excess of 5 700 kg; and
(b) all new types of piston engine aeroplanes having a maximum take-off
weight in excess of 5 700 kg placed on the Register after 1 June 1963.
2.2 For paragraph 2.1:
(a) a certificate of airworthiness for the aircraft must be in force; and
(b) the certificate must include a statement to the effect that the certificate is issued in the transport, commuter or normal category.

Aeroengineer1
11th Apr 2007, 20:07
According to ICAO Doc 9157 Aerodrome Design Manual, Part-1, Runways (2nd ed):

The aeroplane reference field length is defined as the minimum field length required for take-off at maximum certificated take-off mass, sea level, standard atmospheric conditions, still air and zero runway slope, as shown in the appropriate aeroplane flight manual prescribed by the certificating authority or equivalent data from the aeroplane manufacturer.

Similar definition exists in ICAO Annex 14, Chapter I - General:


Aeroplane reference field length.
The minimum field length required for take-off at maximum certificated take-off mass, sea level, standard atmospheric conditions, still air and zero runway slope, as shown in the appropriate aeroplane flight manual prescribed by the certificating authority or equivalent data from the aeroplane manufacturer. Field length means balanced field length for aeroplanes, if applicable, or take-off distance in other cases.

Regarding Boeing 737 narrow runway operations some descriptive information can be found in Boeing presentation entitled "Guidelines for Narrow Runway Operations" by Rob Root, Flight Operations Engineer, Flight Technical Services, Boeing Commercial Airplanes. I guess you can all find the document elsewhere on the net.

Aeroengineer1
11th Apr 2007, 20:18
I am familiar with B737 ops on 30m wide runways - both the -400 and the -800 series. They are normal at several Australian aerodromes, such as Ayres Rock and the busy Gold Coast/Coolangatta;


I just wonder whether these 30m runways have 7.5 meters wide paved shoulders on both sides?

Aeroengineer1
11th Apr 2007, 20:28
Boeing has a special takeoff analysis program for operating the B737 from narrow runways, although, under the FAA system they do not have any limitation on the runway width.


Anyone who has this program of Boeing?

OverRun
12th Apr 2007, 02:46
Ayres Rock is 30m wide without 7.5m sealed shoulders. I just talked to them now to confirm.
Gold Coast/Coolangatta is now 45m wide, 7.5m sealed shoulders (been that way for quite a while) and has just been lengthened to 2492m. But up the road from them is the new Hervey Bay airport – 30m runway width with ops by Virgin Blue 737-700s and -800s, and also without 7,5m sealed shoulders.
The issue of the 7.5m sealed shoulders, and their protection against FOD has been on my plate at a few airports lately. ICAO require the shoulders to have bearing strength plus measures to avoid ingestion of loose stones. This can only be reliably provided for jet aircraft by using bitumen or concrete surfaced shoulders at most airports. Some airports, with good strong soil + moderate rainfall + few jet operations to erode the soil + good maintenance, can use grass/soil shoulders, but this is the exception rather than the rule. Some national authorities make it simple, and state that bitumen/surfaced shoulders SHALL be provided where 7.5m shoulders are required.
For the airport assessing risk, well if an aircraft goes off the side of the runway and there is a problem or it ingests stone/damages an engine, one of the first things to be looked at will be the shoulders and if the airport's position will be difficult if they are not surfaced.
The Boeing presentation is great - pulls together all the factors - thanks be to 'wing files'
Boeing narrow runways (http://www.wingfiles.com/files/performance/narrowrwys.pdf)

737incognito
12th Apr 2007, 05:05
Thanks everybody, especially Aeroengineer1.
I've found Boeing presentation on http://www.wingfiles.com/ (http://www.wingfiles.com/) and it was great help.

Aeroengineer1
12th Apr 2007, 18:25
Your welcome 737Incognito.

Now, I have a question after reading Boeing's narrow runway document.

Does Boeing provide supplement pages to AFM regarding narrow runway operations?

And, I assume that the operator should add some procedures pages in the OM. Am I right?

If I were the civil aviation authority, I would ask the operator to fulfill these. What is your opinion, people?

Aeroengineer1
12th Apr 2007, 18:52
From OverRun's comments in another thread:


This started me thinking about the original question by Prof2MDA on runway width. Taking the design? normal? engine failure case on takeoff where Vef is just above true Vmcg. The aircraft will probably have wandered slightly off centreline during takeoff anyway; I don't have the relevant research to hand, but from memory a normal aircraft wander could be up to say 5m off centreline. Then given a wheeltrack (distance between the outer tyres of the outer main gears of approximately 12.6m for a 747-400, this places the outer tyres at (12.6/2 + 5=) 11.3m off centreline. Then have an engine failure just above Vmcg and experience a parallel path departure of 9m allowed in the regs, and the outer wheels are now (11.3 + 9 =) 20.3m off centreline. If the minimum clearance between the outer tyre and the edge of the runway was set to be 1.5m (my estimate to allow for load spreading in the lower pavement), then that is equivalent to a minimum runway width of (20.3+1.5)*2 = 43.6m. Hmm - doesn’t leave much fat in a 45m wide runway.


I did some work regarding 737-300 and 800 for 2m initial offset from centreline. Regulations allow 9.14 m deviation after engine failure above Vmcg. In case of 737-300, after an engine failure, the distance between outer edges of outer tyres and runway edge becomes 0.655 m, and engine CL goes 0.966 m out of runway. These figures become 0.36 m and 0.966 m respectively for 737-800 case. I am now confused about 737 operations on narrow runways and especially on such runways without paved shoulders. What if initial offset is 3 m? Note: I am not a pilot... Any pilot opinion?

OverRun
13th Apr 2007, 01:40
The required minimum runway width obviously varies depending on how close to the centreline the aircraft is when the engine fails. Assuming that aircraft wander patterns are normally distributed, based on field measurements (Brown, D.N. and Thompson, O.O. (1973). "Lateral Distribution of Aircraft Traffic,"Miscellaneous Paper S-73-56, U.S. Army Corps of Engineers, Waterways Experiment Station, Vicksburg, MS.), the distribution of aircraft on runways is assumed to have a standard deviation of 1.55 m. So at the 95% confidence level, this is mean + 2 s.d = 3.1m. Aeroengineer1 had used 2m (which is the 80% confidence level - also a reasonable assumption). Either 2 or 3m could be used, and I now think that the 5m value used in my earlier post was too conservative.

Aeroengineer1 calculated the Boeing 737-800 outer wheels to be 0.36m inside the runway for the 30m wide runway and a 9m lateral deviation. That is at the 80% confidence level. At the 95% confidence level, the outer tyre would be 0.74 m outside the runway (and onto the runway shoulder).

The Boeing way of handling this seems to be to reduce the takeoff thrust, and load to more forward CG to improve directional control. This would reduce the lateral deviation to less than 9m, and so even at the 95% confidence level, should keep the aircraft on the 30m wide runway, albeit very close to the edge.

When the wheel is on the runway edge, the load and load spreading will be taken partly by the runway and partly by the material/subgrade in the shoulders. Since the number of aircraft ever doing this is hopefully very few, we need only design for a few passes. It should be OK, provided the shoulder pavement material is kept dry. From the highway concepts of edge wetting and shoulders, we know that a sealed shoulder of 1,5m protects the edge of the carriageway from the edge wetting effects of rainfall. So to be sure about 737 operations on a 30m wide runway, we might look at something like a 1.5m sealed shoulder with a bearing strength suited to a couple of passes of the aircraft.

The engine is hanging out a bit further than the wheels, and is well out over the shoulder. But then it is probably the engine that failed, causing the yaw in the first place. So there may not be too much risk of FOD.

This accords with slide 18 of Root's Boeing presentation:
No regulatory link between VMCG definition and actual runway width, so the maximum 30ft deviation could result in reduced (or nonexistent) clearance between outboard main landing gear tire[s] and runway edge…
and his slide 30:
Increased risk of Foreign Object Damage (FOD) to wing-mounted engines

The real trick now is get the 747 onto the 30m runway - here's how it is done (http://www.geocities.com/profemery/united.jpg)

Aeroengineer1
15th Apr 2007, 22:22
Thank you OverRun.

After all of this discussion, I think we can conclude that min runway width for 737 can be 30 meters only with some limitations. If we do not want any limitations then min runway width for 737 becomes 45 meters.

However, I still could not get any response regarding AFM and OM supplements for "narrow runway" operations. I wonder if there are any pilots in this community, who have seen such supplemental pages in AFM and OM about "narrow runway" operations of 737.

john_tullamarine
16th Apr 2007, 09:49
.. when narrow runway ops acquired an airworthiness interest in Australia, along with some test requirements, the normal deal involved a suitable FMS.

mutt
16th Apr 2007, 15:36
the normal deal involved a suitable FMS.Interesting, but why?

Aeroengineer1,
Boeing considers narrow runway data as an AFM appendix, it therefore costs money. If you are a Boeing operator you can ask your tech rep for a non-operational version of the STAS program for test purposes.

AFAIK, the Australian CAA are the only ones who require performance data to be based on the runway width.

Mutt

john_tullamarine
17th Apr 2007, 00:05
Mutt,

To specify narrow runway restrictions etc ... (got to stick the words somewhere ..) ... main restriction will generally be a crosswind limitation (or an artificial increase in minV1 to get away from the Vmcg problem area) .. which relates to the best we found on the day(s) in question.