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Date: | Monday 14 February 2011 |
Time: | 21:20 LT |
Type: | Boeing 737-9GPER (WL) |
Owner/operator: | Lion Air |
Registration: | PK-LFI |
MSN: | 35711/2320 |
Fatalities: | Fatalities: 0 / Occupants: 219 |
Other fatalities: | 0 |
Aircraft damage: | Minor |
Category: | Serious incident |
Location: | Pekanbaru-Sultan Syarif Kasim II Airport (PKU/WIBB) -
Indonesia
|
Phase: | Landing |
Nature: | Passenger - Scheduled |
Departure airport: | Jakarta-Soekarno-Hatta International Airport (CGK/WIII) |
Destination airport: | Pekanbaru-Sultan Syarif Kasim II Airport (PKU/WIBB) |
Investigating agency: | NTSC |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The Boeing 737-900, registration PK-LFI operated by Lion Air as flight number LNI 392 departed from Soekarno-Hatta Airport, Jakarta to Sultan Syarif Kasim II Airport, Pekanbaru (PKU/WIBB).
The pilot made holding and waited for weather improvement and decided to continue approach after the weather improved to above the minima for landing.
At 14.20 UTC (21.20 LT) the aircraft landed at Sultan Syarif Kasim II Airport, Pekanbaru. The weather condition was rain and the runway was wet. Prior to landing, the Tower controller gave clearance to land and informed that the wind was calm, while the pilot saw the wind condition on the Flight Management Computer (FMC) was tail wind up to 11 knots. The aircraft overran and stopped at the stop way with the right main wheels at the corner of the stop way.
The passengers evacuated normally via passenger stair and no one injured.
The examination on the runway found rubber deposit and several spots of standing water up to 3 cm depth.
The FDR data revealed that the aircraft reached the target of deceleration until the thrust reversers stowed at 1000 feet remaining runway length available when the aircraft speed approximately 70 knots.
The investigation concluded that the aircraft was decelerated according to the preselected value until the thrust reversers stowed which was known at the last 1000 feet of the runway available and the aircraft speed approximately 70 knots. According performance calculation the aircraft should be able to stop on the remaining runway available. The failure of the aircraft to stop most likely due to the significant deterioration of both the runway friction and brake effectiveness as result of the existing of the combination of the rubber deposit and water spots.
Accident investigation:
|
| |
Investigating agency: | NTSC |
Report number: | |
Status: | Investigation completed |
Duration: | 2 years and 4 months |
Download report: | Final report |
|
Sources:
Revision history:
Date/time | Contributor | Updates |
15-Feb-2011 04:13 |
harro |
Added |
15-Feb-2011 04:15 |
harro |
Updated [Aircraft type, Cn, Total occupants, Location, Destination airport] |
15-Feb-2011 04:28 |
harro |
Updated [Departure airport] |
15-Feb-2011 08:49 |
Anon. |
Updated [Damage] |
19-Feb-2011 15:44 |
harro |
Updated [Total occupants, Source, Narrative] |
11-Sep-2017 19:52 |
harro |
Updated [Time, Total occupants, Source, Narrative] |
11-Sep-2017 19:54 |
harro |
Updated [Source, Narrative] |
26-May-2022 06:54 |
harro |
Updated [Source] |
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