Bank Angle Awareness | SKYbrary Aviation Safety (2024)

Description

Loss of Controlaccidents and incidents can happen as a result of a particular form of flight crew ’loss ofsituational awareness’, namely a temporary loss of awareness of the aircraft bank angle.

There are three typical ways in which an unusual roll attitude can develop with delayed flight crew awareness:

  • When an aircraft is being flown manually and being controlled solely by external visual reference in conditions of poor flight visibility and/or visual discrimination, sometimes at night.
  • When a flight crew temporarily cease flight instrument scan to undertake other duties in the false belief that theAPis engaged and that their aircraft will therefore follow the flight trajectory defined byFMS/FDinputs.
  • When a singleADI or AHmalfunctions.

In all cases, loss of awareness is possible because there is an absence of tactile sensory feedback. Any sensations that might be readily detected and identified are often masked by a simultaneous lowering of the aircraft nose - resulting in altitude loss or a reduced rate of climb.

However, in all cases, loss of bank angle awareness should be confined to just one pilot and the consequence of this should be promptly observed by themonitoring pilot (PNF)and corrected by Pilot Flying (PF). Nevertheless, reports of accidents and serious incidents, in which a loss of control occurs, show that even with three crew members on the flight deck, this scenario can still occur.

Examples of documented occurrences of this sort, where recovery is successful, are relatively scarce. However, two current trends are providing increasing evidence that there are many more incidents than are documented. These are a gradually increasing habit of self reporting flight crew errors under'just culture'regimes and the increasing prevalence of routineFlight Data Monitoring (FDM)programmes.

The ideal source of data is a combination of comprehensive flight crew reports/interviews and the flight data record to go with it. Relevant parameters which should be monitored for the particular risk being considered here are bank angle, rate of roll, flight control inputs, and angle of attack. The altitude of occurrence is also of interest in relation to the recovery opportunity. If, for whatever reason, flight crew initial reports are not received promptly, then it becomes even more important that the capture and identification of the incident flight data is both reliable and prompt. Flight crew recollections of all the circ*mstances are less easily recalled as time passes.

In terms of accident prevention, knowledge of a potential risk scenario provides the reason to re-visit crew procedures and training. Unfortunately, whilst all Operators can act on evidence from others (“learning from other peoples mistakes”), it is likely that data on this type of incident found as a result of FDM analysis will not be sufficiently serious to qualify as a ‘Serious Incident' under the ICAO definition, and will not be widely or openly shared.

Finally, there is one partial technical safety net which has become quite widespread. This is the simple device of a voice call-out to alert pilots to abnormal bank angle. This comes as an option with various forms ofTAWSas an inclusion inGPWSMode 6. As a result of TAWS becoming ICAO-mandated equipment, most multi crew aircraft operated have the ‘enhanced Mode 6’ option of ‘Bank Angle Alert’. If linked with other GPWS Modes this may come with the usual cut off above 2500 feet agl (and below 30 feet agl). The Alert call is activated at a bank angle which increases with height in this range - at 10 degrees bank angle at 30 feet agl increasing linearly with increasing height to trigger at 40 degrees at 150 feet and then remaining at 40 degrees at greater heights. There is also a version of TAWS equipment available which provides bank angle alerting at heights above 2500 ft agl without limit and aircraft fitted with this have an important additional protection for the cruise where many documented losses of control en route have begun.

Accidents and Incidents

The following events involved lack of awareness of aircraft bank angle:

  • B737, Adam Air, HF LOC, Sulawesi Indonesia, 2007- gives an account of the loss of an Adam Air Boeing 737-400 after both pilots became distracted from awareness of the AP status (not engaged) during the cruise whilst the bank angle gradually reached an extreme from which they could not effect a recovery.
  • B767, LOC, New York USA, 2000- which gives an account of the transient loss of control of a Delta Airlines Boeing 767-300 during a night initial climb being made solely by visual reference without timely intervention by either of the other two pilots on the flight deck during which bank angle reached nearly 66 degrees.
  • B747, vicinity Stansted UK, 1999- which gives an account of how control of a Boeing 747-200 Freighter was lost when the pilot followed the erroneous indications of a single ADI without effective intervention from either of the other two crew members.

Related Articles

  • Inadvertent VFR Flight Into IMC
  • Aerodynamic Stall Awareness and Avoidance
  • Pilot Handling Skills
  • Flight Instrument Presentation of Aircraft Attitude

Further Reading

  • ICAO Amendment No.3 to PANS-TRG (Doc 9868) - Chapter 7, Upset Prevention and Recovery Training, April 2014.
  • FAA AC 120-111 Upset Prevention and Recovery Training, January 2017.
  • Aircraft Loss-of-Control Accident Analysis, C. Belcastro and J. Foster, NASA, 2010.
Bank Angle Awareness | SKYbrary Aviation Safety (2024)

FAQs

What is the maximum safe bank angle? ›

An airplane banking must also have a coefficient of lift to keep the airplane in flight, overcoming the g-force. As an example, any airplane in a 60-degree bank will be at two times its weight or 2g's. That g-force is too great to over achieve at approximately a 75-degree bank which is the maximum bank angle achieved.

How do you calculate bank angle in aviation? ›

To calculate the approximate bank angle required for a standard rate turn, divide the True Airspeed (TAS) by 10 and add 7. For example, an aircraft flying at 120 knots TAS will require a bank angle of 19 degrees for a standard rate turn: 120 TAS / 10 = 12. 12 + 7 = 19 degrees.

What are the limitations on the bank angle? ›

The bank angle should be limited to to avoid having a wing tip or engine pod hit the runway. In the ILS, similar situations are encountered, for instance, when an aircraft is to land on a nonstationary runway as on an aircraft carrier.

What is the maximum bank angle for traffic pattern? ›

Limit your bank angles to 30 degrees or so.

What is the normal law for bank angle protection? ›

Bank Angle Protection limits the maximum bank angle of the aircraft. Within the normal flight envelope, if the sidestick is released when bank angle is above 33°, the bank angle is automatically reduced to 33°. With full sidestick deflection, the maximum acheiveable bank angle is 67°.

What is the calculation for bank angle? ›

The bank angle required to conduct a turn at a specific rate is directly proportional to True Airspeed (TAS). The approximate bank angle required to accomplish a coordinated rate one turn (3°/second) can be calculated by dividing the TAS (in knots) by 10 and then adding 7.

What is the standard bank angle for aircraft? ›

For aircraft holding purposes, the International Civil Aviation Organization (ICAO) mandates that all turns should be made, "at a bank angle of 25° or at a rate of 3° per second, whichever requires the lesser bank." By the above formula, a rate-one turn at a TAS greater than 180 knots would require a bank angle of more ...

What happens to an aircraft when the bank angle is increased? ›

If the angle of bank is permitted to increase, insufficient vertical component of lift will be produced, and the aeroplane will descend. The natural tendency is to attempt to pitch the nose up by increasing backpressure.

What is bank angle warning in aircraft? ›

This is the simple device of a voice call-out to alert pilots to abnormal bank angle. This comes as an option with various forms of TAWS as an inclusion in GPWS Mode 6. As a result of TAWS becoming ICAO-mandated equipment, most multi crew aircraft operated have the 'enhanced Mode 6' option of 'Bank Angle Alert'.

What is the bank angle limit on a 737? ›

On the 737 you have a bank angle selector that allows up to 30° of bank, however depending on AFDS mode it can command a bank up to 30° regardless of the selector position. GPWS provides warning callouts, at 32 to 33° a soft "Bank Angle" warning, from 45° on a hard "Bank Angle" warning.

Does bank angle affect pivotal altitude? ›

The pivotal altitude is the altitude at which, for a given groundspeed, the projection of the visual reference line to the pylon appears to pivot. The pivotal altitude does not vary with the angle of bank unless the bank is steep enough to affect the groundspeed.

What is the bank angle limit on the 787? ›

LNAV can command 30 degrees of bank on most or all Boeing models. I'm not as familiar with the 747, but the Autopilot in LNAV will command 30 on the 767, 777, and 787. HDG SEL is limited to 25 degrees on all Boeing models except the 787 and 777-9, in which it will also command up to 30 degrees at lower airspeeds.

When flying at 100 knots what bank angle is required to secure a standard rate turn? ›

In other words, divide true airspeed by 10 and add half again that amount. For example, at 100 knots, that's 10 plus five, or 15 degrees of bank. At 120 knots, the same arithmetic suggests 18 degrees of bank, just shy of the 20-degree bank indicator on a typical AI.

What is the bank angle in ICAO? ›

Max bank angle 25°. Flight guidance should remain in LNAV mode while on an RF leg when a procedure is abandoned or a go-around is initiated.

What is the steepest bank angle allowed during ground reference maneuvers? ›

Before performing any maneuver, the pilot should complete the required checklist items, make any radio announcements (such as on a practice area frequency), and safety clearing turns. As a general note, a ground reference maneuver should not exceed a bank angle of 45° or an airspeed greater than the maneuvering speed.

What is the maximum bank angle for a 747? ›

The 747 has bank angle warnings (visual when >30º, audible when >35º), but there's nothing physically stopping the pilot from doing so. That said, a 747 could do a barrel roll if the pilot knew what he was doing. Tex Johnson did just that once in a 707.

What is the maximum bank angle of a 747? ›

Flying at Mach 0.85 in 30.000 ft will produce an equivalent airspeed of 306 kt in normal atmospheric conditions. The precise value varies with the actual flight speed, and the maximum safe bank angle is in the region of 60° to 70°.

What is the maximum bank angle on a 737? ›

On the 737 you have a bank angle selector that allows up to 30° of bank, however depending on AFDS mode it can command a bank up to 30° regardless of the selector position. GPWS provides warning callouts, at 32 to 33° a soft "Bank Angle" warning, from 45° on a hard "Bank Angle" warning.

Can a plane bank 90 degrees? ›

Also some powerful aircraft with a high side area. This of course normally requires a high side slip angle, effectively a high alpha. The thrust vector component is important, and large rudder deflections also. Flying at a bank angle of 90° is possible, but it requires a great deal of training.

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