适航手册 AIRWORTHINESS MANUAL(141)

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1.13.3.2  Operators should produce procedures for the use of the CDL, such as: 
a)  The pilot in command should be notified and aware of each missing part(s) before the flight. These missing part(s) should be listed in the aircraft logbook in an appropriate notation
b)  If an additional part is lost in flight, the aircraft may not depart the airport at which it landed following this event, until it again complies with the limitations of the CDL. 
1.14  Recommendations following assessment
Following the satisfactory completion of the inspections described in this Chapter and the required correction of any deficiencies by the applicant, AID inspectors should submit to the inspector-in-charge their recommendations as to the applicant’s ability, in respect of maintenance, to carry out safely the proposed operation. These recommendations should of course be accompanied by inspection reports and other documentation to substantiate the recommendation.
1.15 Surveillance

This aspect is addressed in Chapter 8 of the Manual of Procedures for Operations Inspection, Certification and Continued Surveillance (Doc 8335). The areas to be covered are essentially the same as those assessed for the issuance of the AOC.
— — — — — — — — APPENDIX A.—  SAMPLE MASS AND BALANCE REPORT
MASS CONTROL CERTIFICATE
Date issued . . . . . . . . . . . . . . . . . . . . . . . . . *Date/time of first flight . . . . . . . . . . . . . . . . . . . . . UTC
* Note: This date/time must be later than the date of issue
Aircraft mass and centre of
 gravity determination
No. Date Aircraft registration Aircraft type Aircraft serial number Name of operator Place of determination of mass Reason for determination of mass 
Performed by
Checked by

Empty mass 
Empty CG from datum line 
Index 

Approved by:
 (Authorized personnel)

Empty mass lever arms  MASS CONTROL CALCULATION 
Aircraft type Registration 
Reaction (wheel, jack, point, etc.)  Average scale reading (kg)  ARM (cm)  Moment (cm-kg) 
Left main gear Right main gear Sub-total Nose/tail gear Total (as measured) 

Items included in empty mass:
1.

2.

3.

4.

5.

Remarks:
MASS CONTROL CALCULATION
Aircraft mass and centre of gravity determination

COLUMN I 
Items included but not part of empty mass  Mass (kg)  AR M (cm)  Momen t (cm-kg) 

 

TOTAL 

COLUMN II 
Basic items not included when determining mass  Mass (kg)  AR M (cm)  Momen t (cm-kg) 

 

TOTAL 

Aircraft mass record
Description  Net mass (kg)  ARM (cm)  Moment (cm-kg) 
Total (as measured) 
Less total mass from Column I 
Plus total mass from Column II 
Net empty mass 

CG 
limitation: 
forward  . . . . . . . . . . . . cm 
aft  . . . . . . . . . . . . cm  }  from reference line 

Index formula:
INDEX:

APPENDIX B.—  OPERATIONS SPECIFICATIONS, PART D — MAINTENANCE
Government of _________________________ Page 1 of ______
OPERATIONS SPECIFICATIONS PART D
 XYZ AIRLINES
 AUTHORIZATION PAGE
General
Irrespective of the type of operation to be conducted by (name of operator), the continuing airworthiness and inspection programme limitations which are described and specified in these operations specifications shall be applicable to all (name of operator) aircraft listed and authorized for use under CAA Regulations.
The operator shall provide a comprehensive maintenance programme necessary to fulfil his responsibility to maintain the aircraft in an airworthy condition in accordance with applicable CAA Regulations and standards prescribed and approved by the Director.
　
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