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1.5.1 Pilot in command
Gender : Male
Date of birth : 25 November 1973
Nationality : Indonesia
Marital status : Married
Date of joining company : August 2003
License : ATPL 4567
3 Main landing gear wheels/tires are numbered from left outer number 1, to the right outer number 4.
6
Date of issue : 27 July 2007
Valid to : 30 September 2008
Type rating : Airbus A320F
Date of last medical : 21 April 2008
Last line check : 21 May 2008
Last proficiency check : 20 March 2008
FLIGHT TIME
Total time : 6,047 hours
This make & model : 22 hours
Last 90 days : 171 hours
Last 30 days : 79 hours
Last 24 Hours : 7 hours 20 minutes
1.5.2 Copilot
Gender : Male
Date of birth : 12 November 1985
Nationality : Indonesia
Marital status : Single
License : ATPL 5972
Valid to : 30 June 2008
Type rating : A320F
Instrument rating : 31 January 2009
Date of last medical : 27 December 2007
Last line check : 1 April 2008
Last proficiency check : 27 January 2008
FLIGHT TIME
Total time : 616 hours
This make & model : 446 hours
Last 90 days : 145 hours
Last 30 days : 66 hours
Last 24 Hours : 3 hours 15 minutes
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1.6 Aircraft Information
1.6.1 Aircraft Data
Registration Mark : PK-YVE
Manufacturer : Airbus
Country of Manufacturer : France
Type/ Model : A320 – 321
Serial Number : 441
Date of manufacture : April 1993
Certificate of Airworthiness
Issued : 18 March 2009
Validity : 6 July 2008
Certificate of Registration
Issued : 19 March 2008
Validity : 18 March 2009
Category : Transport
Crew (Cockpit/Cabin) : 2/5
Time Since New : 23,153 hours 33 minutes
Cycles Since New : 30,801
Last C-10 Check : 30 March 2007 (TSN=20,434:2 hrs)
Last D-01 Check : 18 April 2003 (TSN=3852:13 hrs)
Next C-11 Check : 26,434 hrs
Last Event 4 : 14 April 2008 (TSN=22,852 hrs)
Next Event 5 : 26 June 2008
1.6.2 Engine Data
Manufacturer : Rolls Royce
Type/Model : V 2500-A1
Serial Number-1 engine : V 0232
􀂃 Time Since New : 22,516 hrs.
􀂃 Cycles Since New : 29,327 cycles
Serial Number-2 engine : V0259
􀂃 Time Since New : 19,170 hrs
􀂃 Cycles Since New : 28,377 cycles
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1.6.3 Weight and Balance
Load and centre of gravity were within the allowable limits for the landing.
1.6.4 Maintenance
Maintenance had been carried out in accordance with the operators approved
maintenance schedule.
The left landing gear down-lock cable had been broken since the previous landing.
The cable was shorter that the original cable. The cable may have been shortened
during previous maintenance to change the proximity switch, effectively creating
tension on the cable during landing gear extension and retraction cycles.
Figure 5: Broken left landing gear down lock cable
1.7 Meteorological Information
02:00 UTC 02:30 UTC
Wind Calm Calm
Visibility 5,000 m 6,000 m
Weather Haze Haze
Cloud BKN 017 BKN 017
1.8 Aids to Navigation
Not relevant to this serious incident.
1.9 Communications
Not relevant to this serious incident
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1.10 Aerodrome Information
1.10.1 General
Airport Name : Polonia Airport
Airport Identification : WIMM / MES
Coordinate : 03 33 059 N 098 40 094 E
Elevation : 26.50 meters
Airport Operator : Angkasa Pura II
Class : Category 1
Runway Direction : 05 – 23
Runway Length : 2,900 meters
Runway Width : 45 meters
Surface : Asphalt concrete
Address : Polonia International Airport
Jl. Imam Bonjol
Medan, North Sumatera
1.11 Flight Recorders
The flight recorders were recovered from the aircraft on 2 June 2008 under the
supervision of NTSC investigators. The data download and analysis was
conducted by the Australian Transport Safety Bureau in Canberra, Australia.
1.11.1 Digital Flight Data Recorder (DFDR)
Manufacturer : L3 Communications
Type/Model : F–1000
Part Number : S800-3000-00
Serial Number : 000313063
1.11.2 Cockpit Voice Recorder (CVR)
Manufacturer : Fairchild
Type/Model : A100A
Part Number : 93-A100-83
Serial Number : 54416
1.11.3 Notable facts from the CVR
Power was left applied to the recorder after the aircraft came to a stop on the
runway, so much of the CVR data for the flight was over written. Eight minutes of
the flight was available, which covered the final approach and landing.
The cockpit voice recorder revealed that the pilots informed the approach
controller that they had an ‘abnormal condition; a problem with the left main
　
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