1605NM between the 2 airports - that's over the top end for an RJ85
What do you mean by top end?
1605NM between the 2 airports - that's over the top end for an RJ85
What do you mean by top end?
From some of the articles it sounds like the airport he was supposed to refuel at was closed, so he had to choose to divert to get fuel or carry on as he had enough to make it. Sadly his decision didn't factor in an emergency at the destination airport putting him into a holding pattern.
I don't mean to sound like a jerk I just can't think of another way to phrase this.standard range for an RJ85 is 1570nm
The scary thing is I know a lot of pilots would have made the same decision with airlines breathing down their necksI honestly do not understand why they didn't go to bogota - it was behind them by 150miles , and they have flown near on route!
What do you mean by top end?
I don't understand why, even if it could make it by a small margin, why that risk would be taken when there was an option to avoid the risk altogether.
According to the NTSB investigations performed into air accidents, over 88 percent of all chartered plane crashes are attributed, at least in part, to pilot error. In private or general aviation, loss of aircraft control by the pilot is the number one cause of plane and helicopter crashes.
Unfortunately, many airlines place pressures on their pilots and crew that increase the likelihood of human error. Airline corporate negligence often leads to improperly trained or fatigued pilots flying planes, thus putting passengers' lives at risk.
I don't mean to sound like a jerk I just can't think of another way to phrase this.
Are you sure about that because the fact they made it to the airport and completed several circuits of the holding pattern kinda implies it was within range.
The scary thing is I know a lot of pilots would have made the same decision with airlines breathing down their necks![]()
They made it to the airport with enough left for several orbits of the holding pattern. So the pilot was obviously correct in assessing he had enough fuel to make it but not correct in making the correct decision.They didn't make it...?
There's more to it that just that, flying with the wind reduces the amount of fuel needed to get to the destination, as does flying underweight, etc.A factory fresh RJ85 may well have a range of 1600nm without extended tanks
Is it normal that between 2:42 and 2:45 tracking is lost? or could that give validity to there being electrical problems?
No fuel dumping provisions in the 146/RJ
- Fuel Qty indication is availible with only battery power. Infact, there's a momentary Fuel Qty pushbutton above the Engine Insturments that lets you check qty with battery off. It's a digital display on the bottom of the EIS.
- Pannier tanks can be installed and removed regardless if aircraft was delivered from factory with/without them. I suspect this one did not have any installed though, as it's a relatively big job and usually the entire (relatively small) operator community will get wind of someone looking for pannier tanks parts.
- Pannier(or auxillary) tanks are considered part of the wing tanks and thier qty indication is combined with wing tanks if installed. Also an annunciation if they are not empty on the overhead panel. Pannier tanks will feed into thier respective wing tanks.
- I highly doubt any of the belly aux tanks were installed in this aircraft. They are very rare and the only outfit that I know that uses them consistenly nowadays is the FAAM aircraft. Home
- Redundancy is king on this aircraft (it is British...). As detailed above a bit, electrical power is primarily derived from two 115/200 VAC generators on engines 1 and 4. The APU also drives an identical generator without the CSD. Each single AC generator is capable of completely powering the aircraft. In the Avro RJ, bus switching in the event of a generator failure is automatic (provided panel is configured correctly). There is no paralled AC buses in this aircraft. DC power is provided through two (optional third) Transformer Rectifier Units. 26VAC power through transformers for some avionics.
- Essential and Emergency (different buses on this aircraft) AC & DC power can be provided from: Battery (in conjunction with static inverter), and/or a hydraulically powered standby generator (Powered off green system - requires #3 engine-driven-hydraulic pump functioning. Isolates Green system)
- With emergency DC (battery) and AC (static inverter) only:
- Standby Horizon
- #1 VOR/ILS
- #1 COM
- #1 XPNDR
- Standby ASI and Altimeter (straight old pitot/static insturments - no DC draw)
- *I think* L/H landing light
- Pilot's Windshield wiper
- Yellow system DC pump (used to help extend yellow emergency extension jack on main gear, and pump up brake accumulator)
- Anti-skid (Anti-Skid sys. switch has to be placed in BATT position)
- EIS N2 indication
- EIS EGT indication
- FADEC continues to function (if engines are) through PMA's on the FADEC/HMU units on engines.
With Essential AC & DC (from Green system hydraulic stand-by generator)
- couple more engine indications
- More avionics
- normal cockpit lighting
- Battery is isolated w/ standby generator operating.
- Fuel system is a mix of complexity and simplicity.
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Anhedral wings will make fuel in the wing tanks go outboard through mavity. mavity & jet transfer pumps flow fuel from wing tanks to Inboard and Outboard feed tanks in each wing. Inboard for #2/3 engine - Outboard for #1/4. AC pumps in each feed tank provide jet-transfer pump pressure and pressure fuel to engines. Engines will suction-feed fine from feed-tanks though as well.
Center-tank fuel will flow into wing tanks. Floats in each feed tank will annuciate a low fuel condition if any tank is less than full (~600 lbs each).
- In the event of an AC electrical failure, standby hydraulically driven fuel pumps can provide fuel pressure.
- Primary flight controls with exception of rudder are completely manual with flying/servo tabs.
- Loss of yellow hydraulics means no roll spoilers, and some ground spoilers
- Loss of green means no speed-brake, other ground spoilers, and primary gear extension.
- Flaps can run half-speed off a single (yellow or green) hydraulic system.
- Alternate gear extention is mavity, with an emergency-yellow assister-jack for the main gear that may be powered from Yellow DC pump.
It is typical operator method to have APU running below 10,000 ft, providing bleed air for AC packs and pressurization. Frees up bleed air from the anemic engines (LF507). The APU Gen switch will usually be left on, although it will not be on either bus. In event of Gen failure with APU Gen on, APU gen will power the failed bus. APU running does jump into your fuel usage a bit though too...
Having said all this.....this redundancy is very suspect when you have no fuel....
APU never ran - it needs fuel!