To examine the aircraft for structural damage after a flight where excessive
 load factors occurred. Such load factors can be caused by high turbulence,
 maneuvers not in the usual limits, or VMO/MMO values that are more than the
 specified limits.
 Refer to Para. 3. A. for the conditions in which an inspection is necessary.

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  warning notices
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-56-00-200-001 Inspection/Check of the Leveling and Measurement after Abnormal Operation of the Aircraft 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 27-14-00-710-001 Operational Test of the Aileron and Hydraulic
 Actuation 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-34-00-710-001 Operational Test of the Elevator and Hydraulic
 Actuation
 27-44-00-710-002  Operational Test of the Trimmable Horizontal Stabilizer Actuator with the Individual Hydraulic Systems
 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System
 1EFF : ALL 1 05-51-17Page 601 1 1 Aug 01/99R 1 1 1CES 1

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-64-00-710-001 27-80-00-866-004 27-80-00-866-005 27-84-00-710-001 28-10-00-910-002 28-25-00-650-001 29-00-00-864-001 31-37-00-200-001 32-00-00-481-001 32-12-00-010-001 32-12-00-410-001 71-13-00-010-040 78-31-00-710-040 78-36-00-010-040  Operational Test of the Spoiler Hydraulic ActuationExtending the Slats on the GroundRetracting the Slats on the GroundOperational Test of the Slat SystemAccess to the Fuel Tanks and the Work AreasPressure DefuelPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionCheck of the Load-Report Parameter after Hard/Overweight Landing or Excessive TurbulenceInstallation of the Safety Devices on the Landing GearsOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessOpening of the Fan Cowl DoorsOperational Test of the Thrust Reverser SystemOpening of the Thrust Reverser Doors
 3. Job Set-up__________
 **ON A/C 001-003, 051-054,
 Subtask 05-51-17-941-053
 A. Inspection Requirements
 (1) Do this inspection if the flight crew report and/or the data from the Digital Flight Recording System (DFDRS) and/or the data from the QAR (if installed) show: 
R R R R R  NOTE : Excessive turbulence is identified as turbulence that causes____ large, abrupt changes in altitude and/or attitude. It usually causes large variations in airspeed. Passengers and crew are moved violently against their seat belts and loose objects are moved around the aircraft.
 (a) Turbulence or maneuvers that caused a vertical load factor equal to or more than: - +2.5 g or -1 g (clean configuration) - +2 g or 0 g (flaps and/or slats extended), or
 (b) Speeds that were more than VMO + 20 Kts (CAS), or

 (c) Speeds that were more than MMO + 0.04 M, or

 (d) Speeds that were more than VMO or MMO and at which there was a vertical load factor equal to or more than +2 g or 0 g.
 **ON A/C ALL
 Post SB Post SB  31-1111 For A/C 001-003,31-1122 For A/C 051-054,
 Subtask 05-51-17-941-053-A
 A. Inspection Requirements
 (1) Do this inspection if the flight crew report and/or the data from the Digital Flight Recording System (DFDRS) and/or the data from the QAR (if installed) show: 
R R R R R  NOTE : Excessive turbulence is identified as turbulence that causes____ large, abrupt changes in altitude and/or attitude. It usually causes large variations in airspeed. Passengers and crew are moved violently against their seat belts and loose objects are moved around the aircraft.
 (a) Turbulence or maneuvers that caused a vertical load factor equal to or more than: - +2.5 g or -1 g (clean configuration) - +2 g or 0 g (flaps and/or slats extended), or
 (b) Speeds that were more than VMO + 20 Kts (CAS), or
 (c) Speeds that were more than MMO + 0.04 M, or
 (d) Speeds that were more than VMO or MMO and at which there was a vertical load factor equal to or more than +2 g or 0 g.
　
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