sexta-feira, 31 de janeiro de 2025

AMERICAN AIRLINES FLIGHT 5342 MID-AIR COLLISION MILITARY HELICOPTER - APPROACH RADAR SCREEN NOT SO PRECISE FOR TARGETS PRESENTATION

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Above image:
APPROVED FLIGHT PLAN



ATC: PAT25...PASS BEHIND...CRJ7"

PAT25 CVR: NOT RECORDED THE 'PASS BEHIND' PHRASE

Updated FEB 15, 2025 


NTSB Cleared up the ATC instruction to helicopter PA25



Ipsis Litteris

NTSB Feb. 14, 2025, NTSB Briefing Points on Mid-air Collision near DCA

Preliminary investigative information which is derived from a variety of electronic and other sources as of 1:00pm today.

• About 8:15 pm EST, the CRJ left 37,000 feet pressure altitude for an initial descent.

• About 8:30, the Blackhawk began travelling generally southbound after maneuvering near Laytonsville, Maryland. CVR audio from the Blackhawk indicated the instructor pilot was the pilot monitoring and transmitting on the radio and the pilot was the pilot flying. (ATC Radar & Blackhawk CVR)

• At 8:33:41, the Blackhawk crew requested Helicopter Route 1 to 4 to Davison Army Air Field, which the tower controller approved.

• 8:38:39, the Blackhawk reached the intersection of the DC Beltway and the Potomac River near Carderock, Maryland. After briefly turning westbound, the Blackhawk turned back to the east and began descending as it picked up helicopter route 1 over the Potomac River southeast toward downtown Washington, DC.

• At 8:39:10, Potomac Approach cleared the crew of the CRJ for the Mount Vernon Visual Runway 1 approach.

• At 8:40:46, the CRJ rolled out of a left turn established on the ILS Localizer for

Runway 1, at approximately 4,000 feet pressure altitude, 170 knots, with

landing gear up and flaps extended to 20 degrees.

• At 8:43:06, the CRJ crew made initial contact with DCA Tower. The tower

controller then asked if the crew could switch to runway 33. The CRJ crew

agreed to switch to runway 33.

• At 8:43:48, the Blackhawk was about 1.1 nautical miles (NM) west of the Key

Bridge. The pilot flying indicated they were at 300 feet. The instructor pilot

indicated they were at 400 feet. Neither pilot made a comment discussing an

altitude discrepancy. At this time, we do not know why there is a discrepancy

between the two; the investigative team is exploring this.

• At 8:44:27, as the Blackhawk approached the Key Bridge, the instructor pilot

indicated the Blackhawk was at 300 feet descending to 200 feet.

• Between 8:44:41 and 8:44:45 the CRJ crew selected 30 degrees of flaps and

then 45 degrees of flaps.

• At 8:44:49, the CRJ landing gear were down and locked. The aircraft was fully

configured for landing, approximately 6.2 NM south of the airport.

• At 8:45:27, the autopilot was disconnected and the CRJ began a shallow right

turn off of the Runway 1 localizer at a radio altitude of approximately 1,700 ft

and an airspeed of 134 kts. This occurred approximately 5.0 NM south of the

airport.

• At 8:45:30, the Blackhawk passed over the Memorial Bridge. The instructor

pilot told the pilot flying that they were at 300 feet and needed to descend.

The pilot flying said they would descend to 200 feet.

• At 8:45:58, the Blackhawk then crossed over the Washington Tidal Basin and

followed the Washington Channel consistent with Helicopter Route 1.

• It is now approximately two minutes before the collision.

• At 8:46:01, a radio transmission from the tower was audible on the CRJ CVR

informing the Blackhawk that traffic just south of the Wilson Bridge was a CRJ

at 1200 feet circling to runway 33.

3Feb. 14, 2025, NTSB Briefing Points on Mid-air Collision near DCA

• CVR data from the Blackhawk indicated that the portion of the transmission

stating the CRJ was “circling” may not have been received by the Blackhawk

crew. We hear the word “circling” in ATC communications, but we do not hear

the word “circling on the CVR of the Blackhawk. The Recorders Group is

evaluating this.

• At 8:46:08, the Blackhawk crew responded they had the traffic in sight and

requested visual separation which was approved by DCA Tower.

• At 8:46:29, the CRJ crew received a 1000-foot automated callout.

• At 8:46:47, DCA tower cleared other jet traffic on Runway 1 for immediate

departure with no delay.

• At 8:47:27, or 32 seconds before impact, the Blackhawk passed the southern

tip of Hains Point.

• A second later, the CRJ began a left roll to turn to final on Runway 33. The CRJ

was at a radio altitude of 516 ft and 133 kts.

• At 8:47:29, the CRJ crew received a 500-foot automated callout.

• At 8:47:39, or 20 seconds before impact, a radio transmission from the tower

was audible on both CVRs asking the Blackhawk crew if the CRJ was in sight.

Audible in the ATC radio transmission was a Conflict Alert in the background.

• At 8:47:40, the CRJ crew received an automated traffic advisory from the TCAS

system stating “Traffic, Traffic.” TCAS is the Traffic Alert and Collision Avoidance

System on the CRJ.

• At 8:47:42, or 17 seconds before impact, a radio transmission from the tower

was audible on both CVRs directing the Blackhawk to pass behind the CRJ.

CVR data from the Blackhawk indicated that the portion of the transmission

that stated “pass behind the” may not have been received by the Blackhawk

crew. Transmission was stepped on by a 0.8 second mic key from the

Blackhawk. The Blackhawk was keying the mic to communicate with ATC.

• In response, at 8:47:44, the Blackhawk crew indicated that traffic was in sight

and requested visual separation which was approved by DCA Tower. The

instructor pilot then told the pilot flying they believed ATC was asking for the

helicopter to move left toward the east bank of the Potomac.

4Feb. 14, 2025, NTSB Briefing Points on Mid-air Collision near DCA

• At 8:47:52, or 7 seconds before impact, the CRJ rolled out on final for runway 33. The CRJ was at a radio altitude of 344 ft, 143 kts.

• At 8:47:58, or 1 second before impact, the CRJ began to increase its pitch, reaching about 9 degrees nose up at the time of collision. FDR data showed the CRJ elevators were deflected near their maximum nose up travel.

• The last radio altitude recorded for the CRJ was 313 ft and was recorded two seconds prior to the collision. The CRJ pitch at this time was, again, 9 degrees nose up, and roll was 11 degrees left wing down. The CRJ was descending at 448 feet per minute.

• The radio altitude of the Blackhawk at the time of the collision was 278 feet and had been steady for the previous 5 seconds. The Blackhawk pitch at the time of the collision was about a half degree nose up with a left roll of 1.6 degrees. Examination of wreckage will assist in determination of the exact angle of the collision.

• We are confident that the radio altitude of the Black Hawk at the time of the collision was 278 feet. I want to caution this does not mean this is what the Black Hawk crew was seeing on the barometric altimeters in the cockpit.

• We are seeing conflicting information in the data, which is why we aren’t releasing altitude for the Blackhawk’s route.


INSIDE ALL AIR TRAFFIC CONTROL TOWER THERE IS AT LEAST A RECORDER

  • The CRJ’s cockpit voice recorder has now been downloaded and read out. All times listed in Eastern Standard Time —
    • 20:45:27: CRJ Autopilot off
    • 20:46:01: ATC makes PAT25 aware of CRJ south of the Wilson Bridge
    • 20:46:29: 1000’ call out on CRJ
    • 20:47:29: 500’ call out on CRJ
    • 20:47:39: ATC asks if PAT25 has the CRJ in sight
    • 20:47:40: TRAFFIC TRAFFIC aural alert sounds
    • 20:47:42: DCA Tower directs PAT25 to pass behind the CRJ
    • 20:47:58: CRJ crew has verbal reaction and airplane begins to increase its pitch
    • 20:47:59: Sounds of impact
  • There were 5 air traffic controllers in the DCA tower at the time of the accident
    • 1 Local controller working fixed wing and helicopter traffic
    • 1 Ground controller
    • 1 local assistant controller
    • 1 Supervisor
    • 1 Supervisor in training

 

  • The CRJ’s cockpit voice recorder has now been downloaded and read out. All times listed in Eastern Standard Time —
    • 20:45:27: CRJ Autopilot off [Piloto Automático do avião foi desligado]
    • 20:46:01: ATC makes PAT25 aware of CRJ south of the Wilson Bridge [Controlador de Tráfego Aéreo alerta o piloto do helicóptero acerca do avião ao sul da ponte Wilson]
    • 20:46:29: 1000’ call out on CRJ [o Sistema de automático de alerta de altitude do avião anuncia que a aeronave está 1000 pés acima da superfície da água]
    • 20:47:29: 500’ call out on CRJ [o EGPWS alerta que o avião está 500 pés acima da superfície da água]
    • 20:47:39: ATC asks if PAT25 has the CRJ in sight [o Controlador de Tráfego Aéreo pergunta ao piloto do helicóptero se ele tem na visão dele o avião]
    • 20:47:40: TRAFFIC TRAFFIC aural alert sounds [o Sistema de Alerta de Colisão entre Aeronaves dispara o anúncio TRÁFEGO, TRÁFEGO]
    • 20:47:42: DCA Tower directs PAT25 to pass behind the CRJ [o Controlador de Tráfego Aéreo instrui o helicóptero para passar por trás do avião]
    • 20:47:58: CRJ crew has verbal reaction and airplane begins to increase its pitch [o piloto do avião reage verbalmente e inicia o aumento de inclinação do nariz do avião para cima]
    • 20:47:59: Sounds of impact [ouve-se o ruido da colisão das duas aeronaves]
    •  
  • There were 5 air traffic controllers in the DCA tower at the time of the accident
  • Havia 5 Controladores de Tráfego Aéreo na hora do acidente:

 

    • 1 Local controller working fixed wing and helicopter traffic

[Um Controlador local trabalhando no tráfego de aeronave com asa fixa(avião) e helicóptero].

    • 1 Ground controller

[Um Controlador de tráfego no solo]

    • 1 local assistant controller

[Um Assistente de Controlador]

    • 1 Supervisor

[Um Supervisor]

    • 1 Supervisor in training

[Um Supervisor em treinamento]

According to an Army report, the service began issuing night-vision devices to its aviators in 1985 and has continually acquired goggles that allow pilots and aircrew to see more clearly and with better depth perception at night ever since.

Pete Hegseth, secretary of defense, said the Army crew members involved in Wednesday’s crash were performing a required annual night training and that they “did have night-vision goggles.”

Recent Army-wide standardization inspections and accident investigations have revealed deficiencies in maintenance and use of night vision goggles (NVGs) and the Aviator’s Night Vision Imaging System (ANVIS). The purpose of this article is to clarify requirements for modification, inspection, and use of AN/PVS-5 series NVGs and the ANVIS-6.

 

AN/PVS-5 series NVGs Modification.  Only two modifications are authorized for ANI PVS-5 series NVGs used in aviation operations. One is the modified faceplate

(MFP) described in the U.S. Army Aviation Center booklet: AN/PVS-5, 5A Night Vision Goggle Aviator Modifications, dated 10 Jun 83.

The other modification authorized for AN/PVS-5 NVGs in aviation use is the GX-5 flip-up described in an April 1987 booklet published by the Aviation Life Support Equipment Project Manager’s Office, Aviation Systems Command (AVSCOM).




Runway 33 and Runway 04 CLOSED







Above image: OFFICIAL HELICOPTER CORRIDORS in hard blue; APPROVED Flight Plan in magenta; MAXIMUM ALTITUDE in red circle.


 







The Air Traffic Controller's radar screen demonstrates that there is NO PRECISION for each aircraft geographical position in the target presentation on the radar screen. The targets are shown as if the helicopter had already passed behind the CRJ7 plane. In conclusion, the ATC see the target in FALSE position. There is an ERROR between the target shown on radar screen and the real aircraft position.

In the next second, the plane descends 300 feet and collides with the helicopter.



sábado, 18 de janeiro de 2025

JEJU AIR 7C2216 CVR and FDR LAST 4 MINUTES RECORDINGS OUT - POSSIBLE EVENT - CROSS BUS TIE RELAY NOT OPENED

 


On the very moment the GLIDE SLOPE is intercepted the CROSS BUS TIE RELAY automatically opens.


 The CROSS BUS TIE RELAY opens to isolate the navigation receivers and Flight Control Computers. The RELAY opening prevents all approach phase data be removed from FDR because of only one electrical failure.



The CROSS BUS TIE RELAY also opens when the BUS TRANSFER switch is moved to OFF.

 If NORMAL power sources to DC BUS fail, the emergency source of DC power is the batteries.

 If both generators come disconnected from the BUS TRANSFER BUS, the AUTOPILOT disengages and it can't be ENGAGED up to the generators are available. The plane must be piloted MANUALLY. It will be hard work.

With no electrical source available, the batteries can supply electrical power up to minimum of 60 minutes.

UPDATED UPON PRELIMINARY REPORT Jan 27, 2025


Cockpit Voice Recorder

The cockpit voice recorder uses four independent channels to record flight deck audio for 30 minutes or 120 minutes. Recordings older than 30 or 120 minutes are automatically erased. One channel records flight deck area conversation using the area microphone. The other channels record individual ACP output (headset) audio and transmissions for the pilots and observer. (Aircraft fit dependent) The RIPS (Recorder Independent Power Supply) provides power to the cockpit voice recorder for 10 minutes after aircraft power is interrupted either by normal shutdown or by any other loss of power. Normal power supply 115V TRANSFER BUS 2 and 28 V from DC BUS 2.

VOICE RECORDER Switch (when fitted):

AUTO - powers the cockpit voice recorder from first engine start until 5 minutes after last engine shutdown

ON - powers the cockpit voice recorder until the first engine start, then trips the switch to AUTO. On aircraft with no switch the voice recorder is active anytime 115V AC is applied to airplane.

As soon as the aircraft has intercepted the LOCALIZER course, following that the pilot attention will be on GLIDE SLOPE interception.

BATTERY POWER

Emergency source for:

- Static Inverter/AC Standby Bus

- DC Standby Bus

- Battery Bus

- Hot Battery Bus

- Switched Hot Battery Bus

The Static Inverter changes 24 DC power to 115 AC power for the AC STANDBY BUS.

The HOT BATTERY BUS is always connected to the battery, and all its components operate as long as the battery voltage is above a minimum value.

The pilot must move the BUS TRANSFER switch to OFF position and turn off the HIDRAULICS ELECTRIC PUMPS.

After trying to restore the generators, if both GEN OFF BUS (L & R) lights stay ON, the pilot must land the plane ASAP.










The CVR is a customer option, popular choices are the L-3 FA2100 and Honeywell 980-6020/980-6022. Both manufacturers offer these with a crash survivable memory unit (CSMU) for protection of the solid state voice recording memory. The capacity of the CSMU is a customer option, legally the state of registration may only need 30 minutes. The CSMU retains the most recent 30 or 120 minutes of audio, digital, and timing information. Unless you know the part number of the CVR installed, you will not know if it is a 30 minute or 120 minutes capacity, they look identical.

Another customer option is the overhead "Voice Recorder" switch, with ON and AUTO positions. If it has that switch it should shut down 5 minutes after the engines are shut down (based upon oil pressure), if it does not have that optional auto switch it can record whenever 115V is supplied.


sexta-feira, 10 de janeiro de 2025

WET RUNWAY LANDING DISTANCE CORRECTION - TRANSDUCER IN MAIN WHEELS - NO REVERSERS - HIGH SPEED

 







UBATUBA (SDUB) SP, BRAZIL 23° 26' 29" S, 045° 04' 34" W




RWY 09 FST 380M CLSD for LDG


TRANSDUCER SIGNALS WHEEL LOWER RPM COMPARED TO THE OTHER WHEEL

14 CFR 135.385(b), and says (in part):

no person operating a turbine engine powered large transport category airplane may take off that airplane unless its weight on arrival ... would allow a full stop landing at the intended destination airport within 60 percent of the effective length of each runway

So to follow the regulation by the letter, you need to take 60% of the runway length and compare it to your actual landing distance.

 Nenhuma pessoa operando um avião de grande categoria de transporte movido a motor com turbina pode decolar esse avião, a menos que seu peso na chegada ... permitiria um pouso completo no aeroporto de destino pretendido dentro de 60% do comprimento efetivo de cada pista.

Portanto, para seguir o regulamento juridicamente, você precisa pegar 60% do comprimento da pista e compará-lo com a distância real de pouso.

 14 CFR 135.385(d) says:

(d) Unless, based on a showing of actual operating landing techniques on wet runways, a shorter landing distance (but never less than that required by paragraph (b) of this section) has been approved for a specific type and model airplane and included in the Airplane Flight Manual, no person may take off a turbojet airplane when the appropriate weather reports or forecasts, or any combination of them, indicate that the runways at the destination airport may be wet or slippery at the estimated time of arrival unless the effective runway length at the destination airport is at least 115 percent of the runway length required under paragraph (b) of this section.

 (d) A menos que, com base na demonstração de técnicas reais de pouso operacional em pistas molhadas, uma distância de pouso mais curta (mas nunca inferior à exigida pelo parágrafo (b) desta seção) tenha sido aprovada para um tipo e modelo de avião específico e incluída no Manual de Voo do Avião, nenhuma pessoa pode decolar um avião turbojato quando os boletins meteorológicos ou previsões meteorológicas apropriados,  ou qualquer combinação deles, indicam que as pistas do aeroporto de destino podem estar molhadas ou escorregadias no horário estimado de chegada, a menos que o comprimento efetivo da pista no aeroporto de destino seja de pelo menos 115 por cento do comprimento da pista exigido no parágrafo (b) desta seção.

So basically, you use the information from your AFM for wet runway landing distance, or if it isn't provided (since it isn't required), you do the same calculation that you did before but include an additional 15%.

Então, basicamente, você usa as informações do seu AFM para a distância de pouso na pista molhada ou, se não for fornecida (já que não é necessária), você faz o mesmo cálculo que fez antes, mas inclui um adicional de 15%.

Cada vez que um pneu principal passa em uma poça de água, a RPM (Rotação Por Minuto) desta roda diminui muito em relação à outra roda no outro lado que não está passando em poça de água (RPM maior).

A roda que passa na poça de água, contém um dispositivo chamado TRANSDUCER, o qual compara as RPM das duas rodas e libera a rotação da roda mais LENTA. Neste instante esta roda mais lenta não aceita FREIO, pois está precisando girar mais rápido para acompanhar a rotação da roda do outro lado (mais rápida), em sendo assim, o avião não consegue diminuir significativamente a velocidade. Diminui, mas não o suficiente para parar.

Each time a main tire passes through a puddle of water, the RPM (Rotation Per Minute) of this wheel decreases greatly relative to the other wheel on the other side that is not passing through a puddle of water (higher RPM).

The wheel that passes through the puddle of water contains a device called TRANSDUCER, which compares the RPM of the two wheels and releases the slower wheel rotation. At this moment, this slower wheel does not accept BRAKES, because it needs to rotate faster to keep up with the rotation of the wheel on the other side (faster), so the plane cannot significantly slow down. It decreases, but not enough to stop.




quarta-feira, 8 de janeiro de 2025

JEJU AIR 2216 CRASH - LOCALIZER ANTENNAS INTALATION - CONCRETE STRUCTURE BERM NOT RECOMMENDED INSIDE RESA AREA

 


제주항공 사고기 블랙박스 2종, 사고 4분 전부터 기록 멈춰


Jeju Air Accident Plane 2 Types of Black Boxes, Recording Stopped 4 Minutes Before Accident