Good News for SWA Pilots!!!??? Breaking News?

[ultrarunner]

Does SWA FOM authorize landing on contaminated runways with a twc?

 

[LarryinTN]

[6522'-1000'=] 5522' contaminated runway

What is 6522-1000? The runway has a displaced threshold leaving only 5826' available for landing. Glide slope hits the runway with a little more than 4900' remaining.

 

[Dumbledore]

Yes, absolutely! Thrust reversers have negligible effect on a dry runway!

No! ABSOLUTELY untrue statement as an absolute. The effectiveness of reverse thrust is specific to the aircraft upon which the reversers are installed.

Reverse is all but irrelevant on a Falcon 50/900 - only one bucket. Reverse is frighteningly effective on a GII/III!

 

[Dumbledore]

A good way to think about it is: Part 121 tells you how much runway is required, and Part 25 tells you how much runway is actually used.

This is a really BAD way to think of it. Part 25 has ABSOLUTELY NOTHING to do with the daily operation of an aircraft of any kind.

Part 25 deals with certification of an aircraft that a manufacturer wants to sell to its customers. It is a list of things the manufacturer must do in constructing the plane, the performance goals that must be met by that plane once it enters flight testing, and the data that must be documented and made available to the pilots who will operate the plane once the aircraft is certified.

The only substantive connection between Part 121 and Part 25 is that Part 121 requires the use of Part 25 certified aircraft in order to obtain operations specifications and a certificate. The major reason? Part 25 guarantees that the plane will climb if the most critical powerplant suddenly becomes inoperative at or after V1.

 

[pilotpat]

While I certainly don't want to offend anyone, I keep reading and hearing that the landing was "smooth". I just landed my Falcon 20 in blowing snow during the same storm when it hit the northeast on Friday. AND on a runway that's 4840'. Understand, my airplane only weighed 26,000 #'s (I have no idea 737 data), but by landing "firm", I was able to deploy the TR's without any hesitation and barely touch the brakes (didn't want to crank them up on a contaminated rwy), leaving about 1000' remaining. I can tell you when I give the customer a smooth landing, the squat switch doesn't always engage immediately. I don't want to speculate on another pilot's technique, however I am saying what my experience has shown me. During the winter in the northeast, sometimes an ugly "carrier" landing is all I can give 'em if the runway precludes the much sought after grease.

 

[EagleRJ]

This is a really BAD way to think of it. Part 25 has ABSOLUTELY NOTHING to do with the daily operation of an aircraft of any kind.

I see. So what you're telling me is that I can land at Ref +30 using takeoff flaps, and use only reverse to save the brakes, and I'll use exactly the amount of runway it states in the performance charts?

Where do you think your takeoff and landing data comes from?

 

[Lampshade]

I had a source tell me that the reversers are included on the 737-700 landing data but not on the previous versions of the 737. Can anybody who flys the 737-700 nail that down. All I know is Airbus and they are not included in landing data.

 

[Oakum_Boy]

I had a source tell me that the reversers are included on the 737-700 landing data but not on the previous versions of the 737. Can anybody who flys the 737-700 nail that down. All I know is Airbus and they are not included in landing data.

Exactly which "landing data" are you talking about? Factored or actual?

 

[Oakum_Boy]

No! ABSOLUTELY untrue statement as an absolute. The effectiveness of reverse thrust is specific to the aircraft upon which the reversers are installed.

Reverse is all but irrelevant on a Falcon 50/900 - only one bucket. Reverse is frighteningly effective on a GII/III!

Not on a dry runway, I'm afraid. You're saying that two buckets are more effective than one? That isn't rocket science. My point is that on a dry runway, thrust reverse has relatively little importance when comared to a slippery runway. One bucket or four, it is all relative-

 

[Lampshade]

Exactly which "landing data" are you talking about? Factored or actual?

You crack me up. Why don't you answer both if you know? Or better yet just the important one.

 

[Oakum_Boy]

You crack me up. Why don't you answer both if you know? Or better yet just the important one.

It makes a big difference, that's why. The SWA pilots were (I'd bet my life on it) using actual landing distance numbers. Those "actual" distance numbers
are published in the AFM for contaminated runways. They take into account reverse.

Factored landing distance is calculated using no reverse on a dry runway. The FAA says you must [be able to] land within 60% of the available pavement at your destination. Plus 15% on a runway 15% longer if the runway is wet. The wet factored data includes reverse. These are planning numbers only used for dispatch.

 

[Lampshade]

It makes a big difference, that's why. The SWA pilots were (I'd bet my life on it) using actual landing distance numbers. Those actual distance numbers are published in the AFM for contaminated runways. They take into account reverse. Factored landing distance is calculated using no reverse on a dry runway. The FAA says you must [be able to] land within 60% of the available pavement at your destination. Plus 15% on a runway 15% longer if the runway is wet. The wet factored data includes reverse. These are planning numbers only used for dispatch.

I don't know why you're betting your life on them using ALD? Do you really think that they are going to call dispatch up on every landing looking for FLD? lol It's been dispatched there, the consideration has been done. ALD is the important one once airborne. If TR are taken into account what is the adjustment if they don't work? i.e. spoilers fault x1.3, anti skid x1.5, auto brakes x1.2 If you don't fly the 737-700 don't reply. thank you

 

[Oakum_Boy]

I don't know why you're betting your life on them using ALD? Do you really think that they are going to call dispatch up on every landing looking for FLD? lol It's been dispatched there, the consideration has been done. ALD is the important one once airborne. If TR are taken into account what is the adjustment if they don't work? i.e. spoilers fault x1.3, anti skid x1.5, auto brakes x1.2 If you don't fly the 737-700 don't reply. thank you

They were using ALD that considered T/R, that will come out in the findings. My point was, that the only numbers that don't consider reverse, would be the dry FLD. Those, obviously, are not of use when airborne. I would be curious to see Airbus numbers for a contaminated runway. They must be rather restrictive if not considering reverse, no?

 

[Lampshade]

They were using ALD that considered T/R, that will come out in the findings. My point was, that the only numbers that don't consider reverse, would be the dry FLD. Those, obviously, are not of use when airborne. I would be curious to see Airbus numbers for a contaminated runway. They must be rather restrictive if not considering reverse, no?

Care to comment on this: The -700 OPC landing module computes a deceleration rate as a combination of reversers and brakes. (-300/-500) The OPC computes landing performance based on ‘brakes only’ deceleration. Actual braking performance using brakes and thrust reversers will decrease computed landing distance. As far as the Airbus numbers they are not unusually different from any other plane that I have flown.

 

[GVFlyer]

Part 25 is not of consequence only to test pilots during certification.

If you look in the limitations section of a transport category aircraft's AOH, I suspect you will see Part 25 mentioned as a basis for the data. Part 25 regulations are used along with Part 121 regulations in governing the daily operation of an airliner.

A good way to think about it is: Part 121 tells you how much runway is required, and Part 25 tells you how much runway is actually used.

You are correct in assuming that you should go to the Aircraft Flight Manual for take-off and landing data. That information is required to be certificated data, however, the methodology we use to provide that data is inappropriate for your use. For instance all landing data derived for GV certification was accomplished with 95% worn brakes at weights up to 91,000 lbs. V1 data was determined by actually canning engines at V1 at MGTOW. Mmo at M 0.885 was derived by accelerating the aircraft until we encountered a rudder control reversal at M 0.955.

Cruise manual data, by the way, is not certificated data and is required only to be indicative of a test article in the certification program.

Even as a manufacturer, when assisting a major customer in developing Terrain Critical High Altitude Special Procedures, we were required to use FAR Part 121.189 and Far Part 135.379 as we were developing operational standards, not seeking aircraft certification.

GV