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KNKT
Penerbangan Final Report Serious Incident

Boeing 737-400 PK-MDO — Sultan Hasanuddin International Airport, Makassar

Nomor investigasi
KNKT.09.01.01.04
Waktu kejadian
Lokasi
Sultan Hasanuddin International Airport, Makassar
Wilayah administratif
MAROS, SULAWESI SELATAN

Kronologi & deskripsi kejadian

During take-off roll and aircraft speed 125 Knot, the PIC feel the aircraft was vibrate. The PIC aborted take-off, the aircraft stopped on taxiway A and end of runway.

Data teknis

Data teknis kejadian Boeing 737-400 PK-MDO — Sultan Hasanuddin International Airport, Makassar
Operator / maskapai Merpati Nusantara Airlines
Registrasi PK-MDO
Tipe pesawat Boeing 737-400
MTOW above 5,700 kg
Tahun pembuatan 1988
Tipe operasi AOC 121
Fase penerbangan Takeoff (TOF)
Jenis kejadian System/Component Failure or Malfunction (Non-Powerplant)
Jenis kejadian II tire & bolt failure

Faktor penyebab & kontributor

Faktor I
Technical; Technical

Sarana & operator terkait

Daftar sarana dan operator yang terlibat
Operator Flight Number Registrasi Tipe Pesawat Mtow Tahun Pembuatan Tipe Operasi
Merpati Nusantara Airlines PK-MDO Boeing 737-400 above 5,700 kg 1988 AOC 121

Rekomendasi keselamatan yang diterbitkan

Penerima: Directorate General of Civil Aviation

  • OPEN 0 tanggapan

    The National Transportation Safety Committee recommends that the Directorate General Civil Aviation to oversight the operators in the mentioned issues.

    Lihat butir & lini masa tanggapan

Penerima: Merpati Nusantara Airlines

  • TDTL 0 tanggapan

    The National Transportation Safety Committee recommends that the PT Merpati Nusantara Airline should perform cadmium re-plating to the tie bolts after ten times wheel hub assembling as stated in the CMM.

    Lihat butir & lini masa tanggapan
  • TDTL 0 tanggapan

    The National Transportation Safety Committee recommends, Refer to Honeywell Aircraft Landing System (ALS) CMM chapter 32-40-09, the PT Merpati Nusantara Airline should: • For single bolt failures, each tie bolt adjacent to the broken bolt should be removed and scrapped. • For multiple bolt failures, all tie bolts in the wheel should be scrapped

    Lihat butir & lini masa tanggapan
  • TDTL 0 tanggapan

    The National Transportation Safety Committee recommends, Refer to Honeywell Aircraft Landing System (ALS) CMM page 518, Attachment Hardware Inspection, the PT Merpati Nusantara Airline should: • Operator should adopt a life-limit replacement plan for the wheel hub machine bolts to the life limit at 8,000 landings. • Cadmium plating should be restored on the machine bolt after 10 nut instal...

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