Serious incident Boeing 777-F D-ALFG,
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ASN Wikibase Occurrence # 246156
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Date:Saturday 10 October 2020
Type:Silhouette image of generic B77L model; specific model in this crash may look slightly different    
Boeing 777-F
Owner/operator:Lufthansa Cargo
Registration: D-ALFG
MSN: 66090/1596
Year of manufacture:2019
Fatalities:Fatalities: 0 / Occupants: 4
Aircraft damage: None
Category:Serious incident
Location:near Frankfurt International Airport (FRA) -   Germany
Phase: Initial climb
Departure airport:Frankfurt International Airport (FRA/EDDF)
Destination airport:Shanghai-Pudong International Airport (PVG/ZSPD)
Investigating agency: BFU
Confidence Rating: Information verified through data from accident investigation authorities
Lufthansa Cargo flight LH8402, a Boeing 777-F, returned to land at Frankfurt International Airport (FRA), Germany after the cockpit crew noticed unreliable airspeed indicator readings.
Prior to the departure on October 10, 2020, various scheduled maintenance tasks had been performed on the aircraft. One work package included the flushing of the connection lines of the static system
For the flight from Frankfurt to Shanghai, China, there were 4 pilots on board. The co-pilot was Pilot Flying, while the commander assumed the role of Pilot Monitoring. The airplane took off from runway 25C at 09:21 local time with an indicated speed of 204 kt and a ground speed of 191 kt.
Approximately 15 seconds later, a windshear warning was recorded on the FDR and CVR. The indicated speed at this time was 176 kt and the ground speed was 199 kt. The copilot then requested, "Max Thrust." This was acknowledged by the commander. He reported the windshear warning to ATC and added: "[...] we now have five-zero knots tailwind [...]". The bank slowly reduced from 11° to 7°. After another 10 seconds or so, the commander asked the copilot to increase the bank angle.
The copilot replied that she did not want to go below the indicated speed. The indicated speed at this time was 178 kt. The commander noted that the tailwind had increased to 80 kt.
Both expressed surprise that it was not possible to reach the required speed at full thrust, even though the longitudinal inclination was already unusually low. After the indicated tailwind had increased to 100 kt, the commander concluded, "[...] well, that seems very strange to me, I would say that it's unreliable airspeed."
As a result, the commander and the copilot agreed to switch their roles as pilot monitoring and pilot flying, and the commander took over the controls.
Shortly thereafter, the copilot noted that the Integrated Standby Flight Display indicated a speed of 300 kt. A ground speed of 300 kt was also recorded on the FDR at this time.
After the crew unanimously concluded that the airspeeds shown on the two primary flight displays must be unreliable values, the commander decided to declare an emergency at 09:23 and to stabilize the aircraft's attitude by making longitudinal pitch angle changes.
At this time, the aircraft was approximately 8 NM southwest of the airport at an altitude of approximately 6,000 ft.
There was coordination between the crew and controllers as the flight progressed. The course took the aircraft back to Frankfurt Airport and from there in a northeasterly direction over the VOR Metro for about 50 NM. At 09:40, in consultation with ATC, the crew began dumping fuel to reduce the mass of the aircraft to the maximum allowable landing mass. Approximately 5 minutes later, the aircraft turned to a heading of approximately 250° and maintained this heading for 55 NM. At 10:02, the aircraft turned to approximately 210°. Fuel dumping was completed at 10:11. The aircraft was then guided by ATC to the ILS approach to runway 07C at Frankfurt Airport. It touched down on the runway at 10:23 and then taxied to a parking position accompanied by the airport fire department.

After landing, it was found that the sensors of the left and right static systems were not connected.
During maintenance before the incident flight the pneumatic lines of the static system were disconnected and flushed with dry air. The lines were then supposed to be reconnected to the system.
To ensure proper functioning of the pitot-static system, a leak test and a system test were then scheduled. This work was signed off the corresponding work cards as having been carried out without any problems.

The investigation is ongoing.


Preliminary report (in German):


FDR parameters (BFU)

Revision history:

23-Dec-2020 16:17 ASN Update Bot Added
23-Dec-2020 18:04 harro Updated [Aircraft type, Total occupants, Location, Nature, Source, Narrative]
23-Dec-2020 19:55 harro Updated [Source, Narrative]
23-Dec-2020 20:14 harro Updated [Photo]

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