Appendix 5.
AIRWORTHINESS REVIEW REPORT
NOTE:
A COPY OF THIS REPORT TO BE RETAINED IN THE AIRCRAFT RECORDS.
ORGANISATION NAME
APPROVAL REFERENCE NUMBER
ACCURATE COMMODEAL PRIVATE LIMITED
DAW/Q3-ACPL Valid up to 31-07-2015
1. AIRCRAFT DETAILS
Registration
VT- RPG
Type,
Designation and
Series
BEECHJET
Serial No.
RK 190
Current
Flight
Hours/Cycles
Hours/Cycles at
31 December
2723:41 Hrs.
2648:43 Hrs /
400A
RK 190
2105 Landings
2046 Landings
As on 10th October 2014.
As on 31 st December 2013.
Engine Type
(1) P & W JT15D-5 (LH)
(2) P & W JT15D-5 (RH)
Serial No
(1) PCE-JA-0148 (LH)
(2) PCE-JA-0147(RH)
Hours/Cycles
(1) 2723:41 Hrs / 2132 Cycle (LH) (2) 2723:41 Hrs / 2132 Cycle (RH)
Propeller
Serial No
Hours/Cycles
Hub Pt/No
N/A
N/A
N/A
N/A
Blade Pt/No
N/A
AIRWORTHINESS REVIEW PERIOD
From
(Last
Review) Date,
98:51 Hrs / 79 Landings(Last ARC Dated 29th November 2013)
Aircraft
Hours/Cycles
To Date, Aircraft
2723:41 Hrs. / 2105 Landings As on 10th October 2014.
Hours/Cycles
01
2. PART M.A.710 AIRWORTHINESS REVIEW DETAILS
2.1. Flight Manual/Pilots Handbook Issue Flight Manual P/N 128-590001-167B Revision No 23 Dated
and Revision:
June 2011.
Is this the correct document for the current
YES
NO
aircraft configuration
1.1. The Mass and Balance Statement is correct for
the current aircraft configuration
YES
NO
2.2. Maintenance Program Approval
DAW/Q3-ACPL/3227 Dated 13/06//2014
DAW/A7/RPG/1304, DATED 10.04.2014
Provide
reference/issue/revision/date
of
Reference
statement
All scheduled maintenance required by the YES
NO
referenced Program has been carried out
Date aircraft was last weighed
14-08-2012 NO
2.3. All known defects have beenDate:
YES
corrected or deferred in accordance
1.2. The
its
current
with anaircraft,
approved in
procedure:
NO
configuration, complies with the type YES
design
approved
by
DGCA
2.4. All applicable airworthiness directives YES
NO
have been incorporated
Provide
reference/issue/revision/date
Quote documents
assessed after 1st of
the
latest
regulatory
of state of
Extension of ARC authority
:design
approved or accepted Type
Certificate Data Sheet
DGCA MAN MOD Issue No /
Amendment No. Issued
1.3.
Aircraft
Documentation
reviewed:
DGCA/NEW-MISC/150 R1 N/A to VT-RPG, BEECHJET 400A
A16SW / Rev. 28 / 12-04-2013 N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/152 R5
DGCA/NEW-MISC/153 R4 N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/159 R1 N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/160 R2 N/A to VT-RPG, BEECHJET 400A
N/A to VT-RPG,
400A
All DGCA/NEW-MISC/161
documents reviewed are available,
current BEECHJET
and complete
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/162
N/A to VT-RPG, BEECHJET 400A
YES
NO
Registration
DGCA/NEW-MISC/163
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/164
YES
NO
Certificate of Airworthiness
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/165
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/166
YES
NO
Radio License
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/167
N/A to VT-RPG, BEECHJET 400A
DGCA/NEW-MISC/168
Technical/Journey Log
(as
YES
NO
applicable)
Aircraft State of Design Airworthiness FAA AD NO. 2014-15-15 DATED 14-07-2014
APPLICABLE TO VT-RPG (S/N.RK-190) BY SERIAL NO.
Directives
YES
NO
Airframe
Logbook
UPDATED
IN MONITORING DUE AT 7,400 AFH
Bi-weekly/AD No./Issue no./Date
No ADissued on PWC JT15D-5
NO
Engine
EngineLogbook(s)
State of Design AirworthinessYES
Directives
Propeller Logbook(s)
N/A
Bi-weekly/AD No./Issue no./Date
Propeller Logbook
State
of
DesignYES
NO
Modification
Airworthiness Directives
Bi-weekly/AD No./Issue no./Date
Note:
Equipment
State
of
Design
An unsatisfactory answer to any of the questions 2.1 to 2.10 will mean a recommendation may not be made.
Airworthiness
Directives
Details
of any NO answers
should be listed in Section 4 with details of the corrective actions taken.
Bi-weekly/AD No./Issue no./Date
Published
EASA
Airworthiness EASA AD NO. US 2014-15-15 DATED 14-07-2014
Directives
APPLICABLE TO VT-RPG (S/N.RK-190) BY SERIAL NO.
UPDATED IN MONITORING DUE AT 7,400 AFH
Bi-weekly/AD No./Issue no./Date
2.5. Confirm all modifications and repairs
NO
have been approved in accordance YES
with Part 21
2.6. All installed life limited components
NO
have been recorded and have not YES
exceeded their approved service life
2.7. All maintenance accomplished within
this airworthiness review period has
YES
NO
been released to service iaw M.A.801
-----N/A-----
-----N/A-----
3. PHYSICAL SURVEY OF AIRCRAFT
3.1. Survey Report Reference No
(Copy of survey report to be
attached to this airworthiness
RPG 01 / 12 2014
review report)
3.2. Date and location where survey
undertaken
29-10-2013 and KOLKATA
3.3. All known defects and problems
found during the survey have been
appropriately addressed
YES
NO
Note:
Answering NO will mean a recommendation may not be made until the identified problems and defects have
been appropriately addressed.
4. DEFECTS AS REPORTED IN SECTION 2
All defects must be rectified before a recommendation can be made.
REF
FRB
page
no.441
dated
17/12/12
FRB
page
no.493
dated
03/03/13
FRB
page
no.505
dated
24/03/13
FRB
page
no.542
dated
DEFECT
Shimmy ON Taxing
RECTIFICATION/ACTIONS
Found hydraulic leak from shimmy damper.
Replaced with overhauled unit of same part no.
Refuelling cap CB pops out during
landing
In trouble shooting found VCM motor not
working . Replaced with new motor of same part
no.
LH engine start switch shucked during
engine start up
LH engine start switch replaced with new switch
of same part no.
On landing after selecting TR, found RH
TR deploy light flickering
On inspection , found RH TR actuator leaking
replaced with overhauled actuator .Operational
check done found satisfactory
01/06/13
Defect
resistor
book
dated
04/08/13
FRB
page
no.576
dated
01/10/13
5.
During functional test of brake system ,
found gage of emergency brake system
plumbing in yellow range
Beacon light not working
Troubleshooting done on emergency brakes
system and found emergency brake control
valve defective, replaced valve with repaired
modified brake valve. functional test done found
satisfactory
On Troubleshooting found beacon light
assembly not working replaced complete
assembly with new unit of same part no..
operational check found satisfactory
RECOMMENDATION FOR THE ISSUE OF AN AIRWORTHINESS REVIEW CERTIFICATE
5.1.
This is to certify that all of the above records have been reviewed for the period 30-10-2013 to
10-10-2014 and the aircraft VT-RPG was found to be fully in compliance with all of the applicable
requirements of CAR M. On this basis it is recommended that an Airworthiness Review Certificate be
issued in accordance with M.A.901.
Note:
If the result of the full airworthiness review is unsatisfactory or inconclusive then this form, along with
all necessary supporting data should be sent to the DGCA in order to satisfy the requirements of
M.A.710(h)
Signed
Authorisation No
Refer DAW/Q3-ACPL/1296 and Form 4 approval of post holder Continuing
Airworthiness Manager.
Company Approval
No
DAW/Q3-ACPL/3750 Dated 14-07-2014
Date
10-10-2014
Copy of this report shall be provided to the aircraft owner and a copy to be retained in the aircraft
records.
AIRWORTHINESS REVIEW
PHYSICAL SURVEY REPORT
Survey Report Number
RPG 01 / 12 2013
Aircraft Registration
Date of Survey
VT - RPG
Place of Survey
N.S.C.B.I. Airport Kolkata.
Areas of the Aircraft that were surveyed and resultant findings
Finding/Defect
Area
Rectification/Action
Refer to Physical
survey report.
DETAILS OF PHYSICAL SURVEY
All required markings and placards are installed
Aircraft complies with its approved Flight Manual
Aircraft Configuration complies with the approved documents.
(Including radio/navigation equipment capable of transmission)
No evident defects currently exist on the aircraft and not addressed in
accordance with M.A.403
No inconsistencies exist between the aircraft and the aircraft records as per
the review details
Airworthiness
Name
Review
Staff
DGCA Licence Number/Auth
Number
Sanjib Dey
Refer DAW/Q3-STSL and Form 4 approval of post holder
Continuing Airworthiness Manager.
Signature
If required: Licensed Engineer who assisted with the survey
Name
Shivraj Kumar Singh
DGCA Licence Number/Auth
Number
AME Lic. No. 6379
Signature
Copy of Survey Report is to be attached to the recommendation made to the DGCA
PHYSICAL SURVEY REPORT RPG 01
SL.N
O
1
2
3
4
5
6
7
8
PHYSICAL SURVEY OF AIRCRAFT
Description
Check for damages, dents/ any extensive, patch, repairs in the
airframe/engine and quality of repair.
Check tyres, brakes, landing gears.
Check engine inlet, fan blades, outlets, open the cowling and
check for oil leaks.
Check fuel tanks for any leakage.
Check the condition of flaps/aileron/stabilizer for any dent delamination etc.
Check the condition of pilot /AOA probes and cleanliness of
static ports.
Check the condition of static dischargers/wicks.
Check the condition of Radom.
A.M.E
A.R.S
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
Check evidence of over rotation.
Check any evidence of toilet fluid leakage.
Check for any hydraulic leakage.
Check any evidence of pneumatic leaks from doors, window etc.
Check for any missing rivets, fasteners, peeling of paint.
Check for any evidence of corrosion, hydraulic fluid leak in
wheel well area.
Check cleanliness of wheel well area.
Check the cleanliness of aircraft.
Painting of registration marking and aircraft weight outside of
the aircraft
Installation of Owner Name Plate.
Operations of various systems such as flaps, under-carriage,
ailerons, rudder etc.
Operation of external lights such as Navigation, Anti-collision
,Landing/Taxing, Strobe light etc.
Check condition of Baggage doors.
Check condition of Baggage compartment floor.
Condition of Radio/ Navigation Antennas.
Inspect for normal operating pressure of portable Fire
Extinguisher in cockpit and Passenger compartment.
Inspect for operation and free play of control column.
Inspect safety belts & operation (rewind) of safety belts inertial
reels of Pilot and co-pilot. Seats.
Visually inspect for proper operation and condition of entrance
door and door step.
Carry out engine ground run and Check for proper start, idle
power setting , takeoff power
During engine run Check all the engine instruments for proper
operation.
Placard: Replace/ Repairs necessary.
Date:
Signature :
Place: Kolkata
A.M.E NO.:
Auth NO :
