Issued: 09-MAR-2010 | To: EASA | 04.L.2010.10.1 |
Conduct one-time non destructive inspections on Landing Gear Assemblies on all Boeing 737-300/400/500 series aircraft which have accumulated 15,000 Cycles Since Overhaul. Specifically, the inspections should be conducted on the outer surface of the axle root and the flange area (including brake attach flange, flange holes and adjacent axle surfaces). |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.1 |
Conduct one-time non destructive inspections on Landing Gear Assemblies on all Boeing 737-300/400/500 series aircraft which have accumulated 15,000 Cycles Since Overhaul. Specifically, the inspections should be conducted on the outer surface of the axle root and the flange area (including brake attach flange, flange holes and adjacent axle surfaces). |
Issued: 09-MAR-2010 | To: EASA | 04.L.2010.10.2 |
Conduct Eddy Current inspections of the brake attachment flange on inner cylinder and Ultrasonic inspections of the outer surface of axle root of Boeing 737-200/300/400/500 series aircraft at each C check inspection; |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.2 |
Conduct Eddy Current inspections of the brake attachment flange on inner cylinder and Ultrasonic inspections of the outer surface of axle root of Boeing 737-200/300/400/500 series aircraft at each C check inspection; |
Issued: 09-MAR-2010 | To: EASA | 04.L.2010.10.3 |
Replace Inner Cylinder/Sliding Member assemblies whenever a crack is
found in one or more brake mounting holes or any other part of the assembly. |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.3 |
Replace Inner Cylinder/Sliding Member assemblies whenever a crack is
found in one or more brake mounting holes or any other part of the assembly. |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.4 |
Conduct one time non destructive inspections on Landing Gear Assemblies on all Boeing 737-300/400/500 series aircraft which have accumulated 15,000 Cycles Since Overhaul. Specifically, the should be conducted on the outer surface of the axle root and the flange area (including brake attach flange, flange holes and adjacent axle surfaces). |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.5 |
Conduct Eddy Current inspections of the brake attachment flange on inner cylinder and Ultrasonic inspections of the outer surface of axle root of Boeing 737-200/300/400/500 series aircraft at each C check inspection; |
Issued: 09-MAR-2010 | To: National Transportation Safety Board (NTSB) | 04.L.2010.10.6 |
Replace Inner Cylinder/Sliding Member assemblies whenever a crack is
found in one or more brake mounting holes or any other part of the assembly. |
Issued: 09-MAR-2010 | To: Boeing Company | 04.M.2010.10.1 |
Conduct one-time non destructive inspections on Landing Gear Assemblies on all Boeing 737-300/400/500 series aircraft which have accumulated 15,000 Cycles Since Overhaul. Specifically, the inspections should be conducted on the outer surface of the axle root and the flange area (including brake attach flange, flange holes and adjacent axle surfaces). |
Issued: 09-MAR-2010 | To: Boeing Company | 04.M.2010.10.2 |
Conduct Eddy Current inspections of the brake attachment flange on inner cylinder and Ultrasonic inspections of the outer surface of axle root of Boeing 737-200/300/400/500 series aircraft at each C check inspection; |
Issued: 09-MAR-2010 | To: Boeing Company | 04.M.2010.10.3 |
Replace Inner Cylinder/Sliding Member assemblies whenever a crack is
found in one or more brake mounting holes or any other part of the assembly. |
Issued: 09-MAR-2010 | To: DGCA Indonesia | 04.R.2010.10.1 |
Conduct one-time non destructive inspections on Landing Gear Assemblies on all Boeing 737-300/400/500 series aircraft which have accumulated 15,000 Cycles Since Overhaul. Specifically, the inspections should be conducted on the outer surface of the axle root and the flange area (including brake attach flange, flange holes and adjacent axle surfaces). |
Issued: 09-MAR-2010 | To: DGCA Indonesia | 04.R.2010.10.2 |
Conduct Eddy Current inspections of the brake attachment flange on inner cylinder and Ultrasonic inspections of the outer surface of axle root of Boeing 737-200/300/400/500 series aircraft at each C check inspection; |
Issued: 09-MAR-2010 | To: DGCA Indonesia | 04.R.2010.10.3 |
Replace Inner Cylinder/Sliding Member assemblies whenever a crack is found in one or more brake mounting holes or any other part of the assembly. |