Records Review
Records Review
RECORDS
RESEARCH
REPORT
TSF-001
DATE: August 14, 2006
AIRCRAFT MODEL: Hawker 800
RECORDS REGISTRATION NO.: N803CE
RESEARCH SERIAL NUMBER: 258271
TABLE OF CONTENTS
SECTION DESCRIPTION
TWO Inspections
SEVEN #1 Engine
EIGHT #2 Engine
NO. 1 ENGINE
NO. 2 ENGINE
APU Total Time: APUTT: 1692.5 CSN: 4215 APU Hour Meter: APUTT: 1692.5 C: 4215
Repairs:
• No Significant Repairs Noted.
3/26/1999 Concorde Batteries RG390E SA2984SO Yes -- -- ICA Dated 3-28-99 Yes -- -- Yes
Field Repair
FR-HK-00253 &
3/26/1999 Static Drain Repair -- -- -- -- -- -- Yes Yes
FAA Form 8110-3
Dated 3-19-99
FAA Form 8110-3
9/23/1996 Relocate Flitefone Antenna -- -- -- -- -- -- Yes Yes
Dated 9-23-96
Packer Installation On Inboard Side Of FAA Form 8110-3
11/16/1995 -- -- -- -- -- -- Yes Yes
RH Flap Shroud Panel Dated 11-16-95
FAA Form 8110-3
For Structural
11/6/1995 Solar APU T-62T-40C8D-1 Install SA4710SW Yes Rev C Dated 11-6-91 Yes -- -- Yes Yes
Drawing List
No. 258271-1
St. Louis Downtown Airport, 6400 Curtiss-Steinberg Drive, Cahokia, IL 62206
(s258271.MC-TSF-006.Form337-STC.doc) Certified Repair Station Number: RO3R822L 1 of 3
DATE: August 14, 2006
AIRCRAFT RECORDS MAKE: Hawker 800
RESEARCH REGISTRATION #: N803CE
SERIAL NUMBER: 258271
FAA FORM 337 / STC FMS DATA\
EFIS System On/Off Switch SA3539SW Yes FMS Dated 11-22-85 Yes -- --
FMS Rev A
Fairchild A100 CVR SA3644SW Yes Yes -- --
Dated 6-24-94
Dual Honeywell Primus II SRZ-850
Integrated Radio System With Optional FMS Rev A
SA3881SW Yes Yes -- --
Honeywell CD-850 Clearance Delivery Dated 12-28-94
Control FAA Form 8110-3
Radio Master Switch System SA4320SW Yes FMS Dated 8-25-87 Yes -- -- For Structural
Yes
Drawing List
Supplemental Taxi/Landing Lights SA5805SW Yes -- -- -- -- No. 258271-1
4370.8 ENG. HRS 4604.7 A/C HRS 6239.1 ENG. HRS as of 12-JUL-2006 6666
3492 ENC 5198 ENC as of 12-JUL-2006 5561
ENGINE NO. 2 SERIAL/PART: P-91659/3074600-1 MODEL: TFE731-5/-5AR/-5R MANUFACTURER: HONEYWELL
INSTALLED ON 18-AUG-2003 LAST ACTUALS PROJECTED
4171.9 ENG. HRS 4604.7 A/C HRS 6041.2 ENG. HRS as of 12-JUL-2006 6468
3323 ENC 5049 ENC as of 12-JUL-2006 5412
Each item on the Insufficient Information report has missing information needed to properly update
the items(s). Missing information will be one or more of the following:
*TSN and/or
*Date of Manufacture
*Date of Expiration
For each item (code number) in the left hand column, please supply the missing information
indicated by the question mark under the appropriate column heading, sign the authorization area
26-JUL-2006
1 Of 15
2 2
Insufficient Information Report
H R SB 34-3651 NAVIGATION - ELIMINATION OF POSSIBLE ERRONEOUS GLIDE SLOPE INDICATIONS ON THE RNZ-850 INTEGRATED NAV UNIT RECOMMENDED
SERVICE BULLETIN
DUE NEXT MOS 24 New Reqmt
DUE NEXT HRS/MSC 2400
REF: AFL
H R SB 24-3793 ELECTRICAL POWER - INSPECTION AND REPLACEMENT OF UAM100 LIMITERS SERVICE BULLETIN MANDATORY
DUE NEXT DAYS 30 New Reqmt
DUE NEXT HRS/MSC 25
REF: BULLETINS AFL
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
H - Task also due in hours due list
26-JUL-2006 COPYRIGHT 2002 CAMP SYSTEMS INT'L
4 Of 15
Aircraft Model - BAE.125-800 AIRFRAME Maintenance Due (CALENDAR)
Serial #: 258271 Reg. #: N803CE
SB TFE731-73-3152 NO. 2 ENGINE - CONTROLLING- REPLACE SPECIFIC IDENTIFIED FUEL CONTROL ASSEMBLIES HAVING A SUSPECT OVERSPEED RECOMMENDED
AND/OR MANUAL MODE SOLENOID VALVE INSTALLED SERVICE BULLETIN
DUE NEXT MOS 6 New Reqmt
HRS/MSC
REF: BULLETINS ENC
SB TFE731-73-3152 NO. 1 ENGINE - CONTROLLING- REPLACE SPECIFIC IDENTIFIED FUEL CONTROL ASSEMBLIES HAVING A SUSPECT OVERSPEED RECOMMENDED
AND/OR MANUAL MODE SOLENOID VALVE INSTALLED SERVICE BULLETIN
DUE NEXT MOS 6 New Reqmt
HRS/MSC
REF: BULLETINS ENC
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
AH - Task also due in APU hours due list
26-JUL-2006 COPYRIGHT 2002 CAMP SYSTEMS INT'L
5 Of 15
Aircraft Model - BAE.125-800 AIRFRAME Maintenance Due (CALENDAR)
Serial #: 258271 Reg. #: N803CE
+ 510003 DETAIL INSPECT FLIGHT COMPARTMENT SKIN AND WINDOW STRUCTURE ABOVE WINDSHIELDS F1
MOS 144 09-DEC-1994 09-DEC-2006 4.43
51.020 HRS/MSC 0
REF: AFMS STRUCT. INSP. AFL 0
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
+ 530003 DETAIL INSPECT WING TO FUSELAGE ATTACHMENT LINKS, BRACKETS AND BOLTS F1
MOS 144 09-DEC-1994 09-DEC-2006 4.43
53.160 HRS/MSC 0
REF: See Workcard AFL 0
262201 REPLACE FORWARD EXTINGUISHER FIRED FUSE (SERVICE LIFE) LIFE LIMIT F2
MOS 36 19-DEC-2003 19-DEC-2006 4.77
26.220 HRS/MSC
REF: AMM 26-20-41 AFL
262202 REPLACE AFT EXTINGUISHER FIRED FUSE (SERVICE LIFE) LIFE LIMIT F2
MOS 36 19-DEC-2003 19-DEC-2006 4.77
26.220 HRS/MSC
REF: AMM 26-20-41 AFL
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
C R SB 24-3793 ELECTRICAL POWER - INSPECTION AND REPLACEMENT OF UAM100 LIMITERS SERVICE BULLETIN MANDATORY
DUE NEXT DAYS 30 New Reqmt
DUE NEXT HRS/MSC 25
REF: BULLETINS AFL
C R SB 34-3651 NAVIGATION - ELIMINATION OF POSSIBLE ERRONEOUS GLIDE SLOPE INDICATIONS ON THE RNZ-850 INTEGRATED NAV UNIT RECOMMENDED
SERVICE BULLETIN
DUE NEXT MOS 24 New Reqmt
DUE NEXT HRS/MSC 2400
REF: AFL
R 32R123 INSPECT AND RESHIM MLG SISSOR LINKS ON ALL THREE GEAR
MOS
HRS/MSC 600 6169.80 M OVD
REF: AFL
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
C - Task also due in calendar due list
26-JUL-2006 COPYRIGHT 2002 CAMP SYSTEMS INT'L
8 Of 15
Aircraft Model - BAE.125-800 AIRFRAME Maintenance Due (HOURS)
Serial #: 258271 Reg. #: N803CE
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
+ 720002 INSPECT NO. 1 ENGINE AFT COWLING, INNER FAN DUCT AND EXHAUST DUCT PART OF MPI M1
MOS 18-AUG-2003
72.070 HRS/MSC 2100 4604.70 6704.70 231.70
REF: AFMS OUT OF PHASE INSP. AFL 3714
+ 720002 INSPECT NO. 2 ENGINE AFT COWLING, INNER FAN DUCT AND EXHAUST DUCT PART OF MPI M2
MOS 18-AUG-2003
72.070 HRS/MSC 2100 4604.70 6704.70 231.70
REF: AFMS OUT OF PHASE INSP. AFL 3714
+ 720003 INSPECT NO. 1 ENGINE EXHAUST NOZZLE/EXHAUST PIPE V CLAMP PART OF MPI M1
MOS 18-AUG-2003
72.080 HRS/MSC 2100 4604.70 6704.70 231.70
REF: AFMS OUT OF PHASE INSP. AFL 3714
+ 720003 INSPECT NO. 2 ENGINE EXHAUST NOZZLE/EXHAUST PIPE V CLAMP PART OF MPI M2
MOS 18-AUG-2003
72.080 HRS/MSC 2100 4604.70 6704.70 231.70
REF: AFMS OUT OF PHASE INSP. AFL 3714
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
+ 742120 NO. 1 ENGINE - REMOVE AND INSPECT 6 O'CLOCK IGNITER PLUG AND LEADS IN PLACE
MOS 23-MAR-2005
74.040 HRS/MSC 1200 5333.50 (6533.50) 294.40
REF: EMM 74-00-01 ENC 4398 6767.40
+ 742140 NO. 1 ENGINE - REMOVE AND INSPECT 7 O'CLOCK IGNITER PLUG AND LEADS IN PLACE
MOS 23-MAR-2005
74.060 HRS/MSC 1200 5333.50 (6533.50) 294.40
REF: EMM 74-00-01 ENC 4398 6767.40
+ 742120 NO. 2 ENGINE - REMOVE AND INSPECT 6 O'CLOCK IGNITER PLUG AND LEADS IN PLACE
MOS 23-MAR-2005
74.040 HRS/MSC 1200 5135.60 (6335.60) 294.40
REF: EMM 74-00-01 ENC 4222 6767.40
+ 742140 NO. 2 ENGINE - REMOVE AND INSPECT 7 O'CLOCK IGNITER PLUG AND LEADS IN PLACE
MOS 23-MAR-2005
74.060 HRS/MSC 1200 5135.60 (6335.60) 294.40
REF: EMM 74-00-01 ENC 4222 6767.40
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
C - Task also due in calendar due list
26-JUL-2006 COPYRIGHT 2002 CAMP SYSTEMS INT'L
14 Of 15
AIRFRAME Maintenance Due (APH)
( ) - Number of times task due in projected period + - FAA manual flag is set (xEXT) - Extension incorporated in the next due calculation (s) Suppressed Requirement
AIRFRAME LOGBOOK(S) 1
ENGINE LOGBOOK(S) 2
APU LOGBOOK(S) 1
FLIGHT MANUAL(S) 1
JEPPSEN MANUAL(S)
FLIGHT LOG(S)
REGISTRATION, AIRWORTHINESS,
RADIO LICENSE 1 each
MISCELLANEOUS BOOKS
TITLE QUANTITY MECHANIC
INCOMING DEPARTURE INCOMING DEPARTURE
Box 1
MM Addenda 1
Wiring Diagrams 4
Box 2
Hanging File Folders of Maintenance
Records 1-2002 – Present
Box 3
Pilot’s Checklist 1
Checklist 1
Crew Manual 2
Flight Manual 1
Pilots Guide 1
Box 4
COMMUNICATIONS 23
NOTE: Overhaul Periods For Communications Equipment Are Subject To Negotiations Between Individual Operators And Their Regulatory Authority, Unless Listed Below. For The Manufacturers
Recommended Overhaul Periods For Communication Equipment Refer To The Relevant CMM.
Bench
Underwater Locator Beacon
Not Applicable Check -- -- -- -- -- --
P/N: 266-E0305-00
2 Yrs
NOTE: Underwater Locator Beacons Can Be Installed On Cockpit Voice Recorders And Flight Data Recorders.
Underwater Locator Beacon -
Replace
Battery Not Applicable -- -- -- -- -- --
2 Years
P/N: ULB Part No. 15957
NOTE: For the ULB Part No. 266-E0305-00 the ULB has to be returned to the manufacturers for the battery to be replaced. For the earlier type ULB Part No. 15957 the replacement batteries can be
Obtained from the manufacturers.
(s258271.hs - 0800.cop.doc) Page 1 of 10
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 6400 Curtiss-Steinberg Drive, Cahokia, IL. 62206 Phone: 618-646-8000 CRS No. RO3R822L
HAWKER 800 OVERHAUL COMPONENT STATUS
AIRCRAFT MAINTENANCE SCHEDULE REVISION 10 JUNE 2006
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457
DESCRIPTION/PART NO. SERIAL #: REQUIREMENTS LAST COMPLIANCE NEXT DUE
HRS. LDGS. MON HRS. LDGS. DATE HRS. LDGS. DATE
ELECTRICAL POWER 24
EQUIPMENT/FURNISHINGS 25
NOTE: The overhaul period of 4 years is subject to a satisfactory examination of one pack after 2 years from 9 years onwards ALL packs must be overhauled every year.
33816, 33832 5903.2 4944 9-7-05 -- -- 9-7-07
Lifejackets 33868, 33881 5903.2 4944 9-7-05 -- -- 9-7-07
(Manufactured After March 1980) Overhaul 5 Years
P/N: 102MK2BA, P0201-105, 33919, 33986 Overhaul 1 Years 5903.2 4944 9-7-05 -- -- 9-7-07
P0723E105P, P01074-101 34011, 271742 5903.2 4944 9-7-05 -- -- 9-7-07
707755, A37724 5903.2 4944 9-7-05 -- -- 9-7-07
NOTE: The Overhaul Period Of 5 Years Is Valid From The Date Of Manufacture Up To 20 Years Subject To A Satisfactory Examination Of One Pack Every 2 Years. After 20 Years The Overhaul
Period Changes To Every Year.
Install
Fire Extinguisher, Turbomach APU 1-15-04
34358B1 5 Years From Date Of Filling 4819.7 3915 -- -- 12-22-2008
P/N: 30402104 Hydro
12-22-03
Install
Cockpit 40617 6171 5188 3-8-06 -- -- 9-2011
Fire Extinguisher, Portable Hydro 9-05
(Mod. 259410A) 6 Yrs
P/N: 74-00, BA51015-3, PA-H3 Install
W479453
Cabin 6334 5335 5-31-06 -- -- 1-2011
No Tag
Hydro 1-05
NOTE: Mod. 259410A Is Applicable To Aircraft No’S 258067 And 258076 ONLY. Mod. 259410A Introduces A Special Interior Layout Finish.
NOTE: Fire Warning Switches Part No’S 17343-62-500 And 160275-1 And Generator Overheat Switch Part No. 67100-1-350 Are ONLY Applicable To Sundstrand / Turbomach APU Installations.
NOTE: Mod. 258894 Standardizes Graviner Fire Detection Switches At The APU For Aircraft Post Mod. 251605 (Garrett APU’s).
FLIGHT CONTROLS 27
HYDRAULIC POWER 29
Engine-Driven Pump
Not Applicable 2000
(Pre Mod. 252975A -- -- -- -- -- --
By Part Number Hours
P/N: 65WE-01030-*
NOTE: Mod. 252975A Introduces The ABEX Engine Driven Pump AP05V-086.
INSTRUMENTS 31
SAM/DHB/ 5000
LH Landings Or 5486.3 4543 1-27-05 -- 9593 1-27-2017
Side Stay Assembly 8SSP/024
12 Yrs
P/N: 25-8UM3/-*A
SAM/DHB/ Whichever
RH Occurs First 5486.3 4543 1-27-05 -- 9593 1-27-2017
8SSS/008
Note: If The Main Leg Assembly Is Older Than 10 Years Since New Or Last Overhaul, Overhaul Or Before 5000 Landings From New Or Last Overhaul, Or Before The End Of Dec. 2005 Whichever
Occurs First.
5000
Landings Or
Nose Leg Assembly
Not Applicable 12 Yrs -- -- -- -- -- --
P/N: 25-8UN1-*A
Whichever
Occurs First
Note: If The Main Leg Assembly Is Older Than 10 Years Since New Or Last Overhaul, Overhaul Or Before 5000 Landings From New Or Last Overhaul, Or Before The End Of Dec. 2005 Whichever
Occurs First.
5000
Nose Leg Assembly Landings Or
P/N: 25-9UN1-*A SAM/DHB/9N/049 12 Yrs 5486.3 4543 1-27-05 -- 9593 1-27-2017
(Post Mod. 253129A) Whichever
Occurs First
Note: If The Main Leg Assembly Is Older Than 10 Years Since New Or Last Overhaul, Overhaul Or Before 5000 Landings From New Or Last Overhaul, Or Before The End Of Dec. 2005 Whichever
Occurs First.
5000
Nose Landing Gear Drag Stay Landings Or
Assembly TA/DHB/059 12 Yrs 5486.3 4543 1-27-05 -- 9593 1-27-2017
P/N: 25-8UN3-*A Whichever
Occurs First
Note: If The Main Leg Assembly Is Older Than 10 Years Since New Or Last Overhaul, Overhaul Or Before 5000 Landings From New Or Last Overhaul, Or Before The End Of Dec. 2005 Whichever
Occurs First.
LH
Maxaret Unit 466 3828.3 3018 8-10-02 -- 6018 --
OUTBD 3000
P/N: AC65216
Landings
AC65218 RH INBD 364 3828.3 3018 8-10-02 -- 6018 --
LH
601 3828.3 3018 8-10-02 -- 6018 --
OUTBD
OXYGEN 35
Install 1-27-05
#1 007874 5486.3 4543 Hydro -- -- 12-2009
12-23-04
Oxygen Cylinder 5
Install 1-27-05
P/N: WKA37447 Years
#2 007868 5486.3 4543 Hydro -- -- 12-2009
7-4-05
#3 366325 In Work -- -- TBD
Passenger Masks
12 Masks Overhaul 6 Years 6185.6 5797 3-23-06 -- -- 3-23-2012
P/N: C351-200*
Passenger Masks
Not Applicable -- -- -- -- -- --
P/N#: 289-601* Overhaul 6 Years
Note: *Masks That Exceed The Overhaul Period Have 12 Months To Comply With The Vendors Recommendation.
Passenger Masks
Refer To The Vendor MM For The
As Applicable To The Installed Not Applicable -- -- -- -- -- --
Installed Unit
Unit.
Crew Masks
Refer To The Vendor MM For The
As Applicable To The Installed Not Applicable -- -- -- -- -- --
Installed Unit
Unit.
Engine
Refer To Vendor Maintenance
T-62-40C8D1 SP-E945336 Reference Aircraft Technical Data
Manual For The Installed Unit
P/N: 165101
Fire Extinguisher
Extinguisher Bottle Gone Indication 1-15-04
Fwd 4819.7 3915 -- -- 1-15-2007
Fuse Cartridge, Engine DOM 9-03
3 Years From Installation Or
P/N: A1003
4 Years From Manufacture
Graviner Maintenance Leaflet -
ML 018 1-15-04
Aft 4819.7 3915 -- -- 1-15-2007
See Appendix DOM 9-03
Airbrake Jacks
P/N: AIR45398/7 or /8,
AIR46520/0, /1 25,000 -- -- -- -- 25,000 --
Body
P/N: AIR111462
Not
LH -- -- -- -- -- --
Side Stay Upper Arm Applicable
12,000
P/N: 25-8UM163-* Not
RH -- -- -- -- -- --
Applicable
Not
Side Stay Lower Arm LH -- -- -- -- -- --
Applicable
P/N: 25-8UM31-1A, -2A 27,000
Pre Mod. 253129A Not
RH -- -- -- -- -- --
Applicable
Side Stay Lower Arm LH TSN: 5486.3 CSN: 4543 1-27-05 -- 27,000 --
P/N: 25-8UM73-1A, -2A 27,000
Post Mod. 253129A RH TSN: 5486.3 CSN: 4543 1-27-05 -- 27,000 --
Not
LH -- -- -- -- -- --
Side Stay Lower Arm Applicable
27,000
P/n: 25-8UM165-1A, -2A Not
RH -- -- -- -- -- --
Applicable
Not
Jack Pivot LH -- -- -- -- -- --
Applicable
P/n: 25UM1229A 4,000
Post Mod 252267, See Appendix Not
RH -- -- -- -- -- --
Applicable
Not
Jack Pivot LH -- -- -- -- -- --
Applicable
P/N: 25-8UM87-1A 4,000
Post Mod 253129A, See Appendix Not
RH -- -- -- -- -- --
Applicable
Not
Upper Casing LH -- -- -- -- -- --
Applicable
P/N: 25-8UM169 24,000
Post Mod 253549A Not
RH -- -- -- -- -- --
Applicable
Not
LH -- -- -- -- -- --
Torque Link Applicable
20,000
P/N: 25-9UM9-1A, 25-9UM11-1A Not
RH -- -- -- -- -- --
Applicable
Not
Torque Link Pin LH -- -- -- -- -- --
Applicable
P/N: 25-8UM15* 20,000
Post Mod 253511A Not
RH -- -- -- -- -- --
Applicable
Pivot Pin
P/N: 25UN645A 16,000 TSN: 5486.3 CSN: 4543 1-27-05 -- 16,000 --
See Appendix
Plunger Tube
P/N: 25UN649 SAM0702 20,000 TSN: 5486.3 CSN: 4543 1-27-05 -- 20,000 --
Post Mod. 252094B
Axle Barrel
P/N: 25-8UN257 30,000 TSN: 5486.3 CSN: 4543 1-27-05 -- 30,000 --
Post Mod. 253129A
Axle Barrel
P/N: 25UN385A/* Not Applicable 30,000 -- -- -- -- -- --
Pre Mod. 253129A
Torque Links
P/N: 25-8UN267-23A
32,000 TSN: 5486.3 CSN: 4543 1-27-05 -- 32,000 --
25-8UN269-27A
Post Mod. 256168A/B
Torque Links
P/N: 25UN491A, 25UN489A Not Applicable 32,000 -- -- -- -- -- --
Pre Mod. 253129A
Connecting Rod
P/N: 25UN113A/B Not Applicable 20,000 -- -- -- -- -- --
Pre Mod. 253129A
Connecting Rod
P/N: 25-8UN433-1A 20,000 TSN: 0 CSN: 0 1-27-05 -- 24,543 --
Post Mod 253129A
Wheel Brake Control Valves LH TSN: 5486.3 CSN: 4543 1-27-05 -- 9043 --
P/N: AC61520, AC67352
AC67732, AC67740
Inner 4,500 TSN: 5486.3 CSN: 4543 1-27-05 -- 9043 --
Knife Edge
P/N: ACO34629, ACO34630,
ACO36133 RH TSN: 5486.3 CSN: 4543 1-27-05 -- 9043 --
Not
Emergency Brake Reducing Valves LH -- -- -- -- -- --
Applicable
P/N: AC61516,AC69006,AC69784,
AC67738,AC67742 Not
Inner 4,500 -- -- -- -- -- --
Knife Edge Applicable
P/N: ACO25103, ACO25104
Post Mod. 253522A Not
RH -- -- -- -- -- --
Applicable
Steering
Steering Pin
P/N: 25UN605 25,000 TSN: 0 CSN: 0 1-27-05 -- 29,543 --
Post Mod. 251909
Steering Sleeve
P/N: 25-8UN103-1A 20,000 TSN: 5486.3 CSN: 4543 1-27-05 -- 20,000 --
Pre Mod. 253129A
Steering Sleeve
P/N: 25-8UN439-1A Not Applicable 20,000 -- -- -- -- -- --
Post Mod. 253129A
Steering Sleeve
Not Applicable 20,000 -- -- -- -- -- --
P/N: 25UN395A/*
Steering Jack
P/N: AIR45396 14,400
-- -- -- -- 14,400 --
Jack Eye End Flights
P/N: AIR110646
Jack Pick-Up
P/N: 25-8UN263-1A 18,000 -- -- -- -- 18,000 --
Post Mod 253129A
Jack Pick-Up
P/N: 25UN7A/B Not Applicable 18,000 -- -- -- -- -- --
Pre – Mod 253129A
Engines #1 P91653
Reference
P/N: TFE731-5R See Engine Section Of Report
TFE731-72-3001
Allied Signal Service Bulletin - #2 P91659
Unreadable
86-14-08 To Prevent Loss Of Stall Warning
12-9-94 Complied With At Build One Raytheon
8-4-86 (S.B. 27-136, Revision 1)
DAI/2652/55
To Prevent Failure Of The Ventral Fuel Complied With At Build By Mod 3127 Recur Unreadable
87-12-10 Not
Tank Aft Support Fitting 12-9-94 90 Raytheon
7-30-87 Applicable
(S.B. 53-62, Revision 1) NOTE: Accomplishment of S.B. 53-63 (3127) Days DAI/2652/55
Revision 1, Terminates Recurring Action
John Pressnell
89-18-13 To Prevent A Fire In The Aft Equipment
8-3-95 Complied With One Raytheon
9-28-89 Compartment, Puncture of the Aft
CRS YK1R641K
Mike Preusch
90-08-07
To Prevent Loss Of Aileron Control 8-7-06 Not Applicable One Midcoast Aviation
5-29-90
CRS RO3R822L
Unreadable
91-10-10 To Prevent A Wheel Loosening From The
12-9-94 Complied With At Build One Raytheon
6-18-91 Axle And The Possible Loss Of A Wheel
DAI/2652/55
92-16-12 Unreadable
Revision 1 To Prevent Fire In The Tail Cone 12-9-94 Complied With At Build One Raytheon
9-28-92 (S.B. 53-74, Revision 1) DAI/2652/55
Unreadable
93-24-07 To Prevent Failure Of The Sealant Installed
12-9-94 Not Applicable One Raytheon
12-23-93 Around The Over-Temperature Sensor
DAI/2652/55
94-26-12
Superseded By 97-03-07 --- NOT APPLICABLE --- Recur
2-3-95
Mike Preusch
2005-16-02 To Prevent Smoke And Fumes In The 8-21-06 Previously Complied With
One Midcoast Aviation
9-6-05 Cockpit TT: 6185.6 On 12-8-00
CRS RO3R822L
Unreadable
21-3669 AIR CONDITIONING – Fan Venturi Motor
1-20-06 Complied With One
12-1-04 Replacement
A&P 199366917
24-264 Unreadable
DC Bus Tie System - Inspection For Correct
Revision 1 12-9-94 Complied With At Build One Raytheon
Operations
6-20-88 DAI/2652/55
Unreadable
24-3588 Electrical Power – Inspection / Repair Of Wire
1-15-04 Complied With Midcoast Aviation
9-1-03 Bundles Form Panel “JA”
CRS RO3R822L
EQUIPMENT/FURNISHINGS - Warming
Oven. To Introduce Warming Oven
25-54 255D-LH-28/115, 255D-RH281115, And 255- Unreadable
Revision 1 362A With Overheat Protection. 12-9-94 Not Applicable One Raytheon
8-14-89 Mod. 259758A DAI/2652/55
Mod. 259758B
(A.D. 91-03-18)
EQUIPMENT/FURNISHINGS - Warming
Unreadable
25-64 Oven. To Introduce Oven 206D-LH-28/115
12-9-94 Not Applicable One Raytheon
8-10-92 With Overheat Protection.
DAI/2652/55
Mod. 259758C
Unreadable
26-3496 FIRE PROTECTION – Introduction of
1-15-04 Complied With Midcoast Aviation
11-1-03 Electrical Wire Protection Kit
CRS RO3R822L
Unreadable
27-155 FLIGHT CONTROLS - Inspection Of Rudder
12-9-94 Not Applicable By Serial Number One Raytheon
8-16-91 Pedal Torque Tubes For Cracking
DAI/2652/55
Unreadable
27-3589 FLIGHT CONTROLS - Removal Of Corrosion
1-15-04 Not Applicable Midcoast Aviation
3-3-04 From Airbrake Jack Valve Body
CRS RO3R822L
32-184 Unreadable
LANDING GEAR - Nose Leg Drag Stay
Revision 5 1-27-05 Not Applicable One Midcoast Aviation
Assembly. Cracking Of Bridge Casting.
2-18-92 CRS RO3R822L
32-A203 Unreadable
LANDING GEAR - Nose Gear Door Quick
Revision 1 12-9-94 Complied With At Build One Raytheon
Release Strut, Incorrect Closure.
9-6-85 DAI/2652/55
Unreadable
32-217 LANDING GEAR - Nose Gear Pivot Pin.
1-15-04 Complied With One Midcoast Aviation
2-29-88 Crack Test.
CRS RO3R822L
Unreadable
32-3499 LANDING GEAR - Inspection And Removal
8-9-02 Not Applicable One AVMats
10-1-01 Of Suspect Maxarets (Anti-Skid Device)
Unknown
Unreadable
32-3522 LANDING GEAR - Dunlop Wheel Tie-Bolt
12-14-02 Complied With One
9-1-02 Nuts Inspection / Replacement
A&P 199366917
32-3746 Unreadable
Landing Gear – Main Landing Gear (MLG)
Revision 1 6-13-06 Complied With
Wheel Tie Bolt And Nut Retirement Life.
10-05 A&P 199366917
33-3586 Open
LIGHTS – Pulselite System Bus Wiring
Revision 1 One
Modification
11-1-04 Not Applicable
Open
33-3682 LIGHTS – Reactivation Of Precise Flight
3-14-05 Pulelite System
Not Applicable By Serial Number
Unreadable
35-3014 OXYGEN - Inspection Of Passenger Oxygen
12-12-97 Complied With One
9-1-97 Face Mask For Possible Tears In Face Cushion
A&P 170406748
35-3495 Unreadable
OXYGEN - Introduction Of Scott Protective
Revision 1 8-10-02 Complied With One Av Mats
Breathing Equipment (PBE)
12-1-02 CRS UVVR932L
53-95 Unreadable
FUSELAGE - Inspection / Introduction Of
Revision 1 6-25-99 Complied With One Garrett Aviation
Rivets At Frame 19
4-1-99 CRS U02R221L
Unreadable
53-3118 FUSELAGE - Inspection For Out-Of-Position
2-23-99 Complied With One
12-1-98 Bolts
A&P 170406748
74-08-09 Unreadable
Transport Category Aircraft 9-7-05 RECUR
Revision 2 Complied With 1000 HR
TT: 6903.2 Midcoast Aviation
Lavatory Receptacles TT: 5903.2
7-29-96 CRS RO3R822L
Unreadable
94-01-04 Honeywell, Inc.
11-6-95 Not Applicable Raytheon
2-4-94 TCAS II Computer Units
CRS YK1R641K
Mike Preusch
94-01-05 Alliedsignal Aerospace 3-21-06
Not Applicable Midcoast Aviation
2-4-94 TCAS II Processor TT: 6185.6
CRS RO3R822L
Mike Preusch
94-01-06 Rockwell Collins, Inc. 3-21-06
Not Applicable Midcoast Aviation
2-4-94 TCAS II Processors TT: 6185.6
CRS RO3R822L
Mike Preusch
94-02-02 Rockwell Collins, Inc. 3-21-06
Not Applicable Midcoast Aviation
2-21-94 DME 700 TT: 6185.6
CRS RO3R822L
Mike Preusch
94-06-04 Eros 3-21-06
Not Applicable Midcoast Aviation
5-23-94 Full Face Mask Regulators TT: 6185.6
CRS RO3R822L
Mike Preusch
94-14-03 Nordskog Industries 3-21-06
Not Applicable Midcoast Aviation
8-1-94 Water Heaters And Coffee Makers TT: 6185.6
CRS RO3R822L
Mike Preusch
95-01-01 Terra Corporation 3-21-06
Not Applicable Midcoast Aviation
2-6-95 Transponders TT: 6185.6
CRS RO3R822L
Unreadable
95-22-01 Aerospace Lighting Corporation Not
11-15-95 Not Applicable RECUR Raytheon
12-4-95 Cabin Fluorescent Lighting System Applicable
CRS YK1R641K
Mike Preusch
95-25-08 Royal Invention Company 3-21-06
Not Applicable Midcoast Aviation
5-20-96 Water Heaters TT: 6185.6
CRS RO3R822L
Mike Preusch
96-21-13 LITEF Gmbh 3-21-06 Not
Not Applicable RECUR Midcoast Aviation
11-12-95 ARHS Unit TT: 6185.6 Applicable
CRS RO3R822L
Mike Preusch
97-04-15 Pacific Scientific 3-21-06
Not Applicable Midcoast Aviation
3-7-97 Fire Extinguisher Bottle Cartridges TT: 6185.6
CRS RO3R822L
97-05-03
Alliedsignal Avionics, Inc. Unreadable
Revision 1 4-1-99 Not Applicable
Global Positioning Systems A&P 170406748
4-20-99
Mike Preusch
99-01-14 Honeywell, Inc. 3-21-06
Not Applicable Midcoast Aviation
2-12-99 IC-600 Integrated Avionics Computers TT: 6185.6
CRS RO3R822L
99-23-22
Transport Category Aircraft
Revision 2 RESCINDED
Mode “C” Transponder
4-20-00
Britax Sell
2001-10-13
Water Boilers, Coffee Makers And SUPERSEDED BY 2002-21-01
6-15-01
Beverage Makers
Mike Preusch
2001-15-17 Rockwell Collins, Inc. 3-21-06
Not Applicable Midcoast Aviation
8-20-01 CTL-92 Transponder Control Panels TT: 6185.6
CRS RO3R822L
Mike Preusch
2002-13-07 Honeywell, Inc. 3-21-06
Not Applicable Midcoast Aviation
8-09-02 Inertial Reference Unit (IRU) TT: 6185.6
CRS RO3R822L
Mike Preusch
2002-14-19 Rockwell Collins, Inc. 3-21-06
Not Applicable Midcoast Aviation
8-23-02 Air Data Computers (ADC) TT: 6185.6
CRS RO3R822L
Mike Preusch
2002-20-09 Rockwell Collins 3-21-06
Not Applicable Midcoast Aviation
11-12-02 Adaptive Flight Display Units TT: 6185.6
CRS RO3R822L
Mike Preusch
2002-22-13 Rockwell Collins, Inc. 3-21-06
Not Applicable Midcoast Aviation
12-20-02 Flight Management Computers (FMC) TT: 6185.6
CRS RO3R822L
Mike Preusch
2004-08-16 NARCO Avionics Inc. 3-21-06
Not Applicable Midcoast Aviation
6-1-04 AT150 Transponders TT: 6185.6
CRS RO3R822L
Mike Preusch
2005-07-27 Aviointeriors S.P.A. 3-21-06 Not
Not Applicable RECUR Midcoast Aviation
5-16-05 Model 312 Seats TT: 6185.6 Applicable
CRS RO3R822L
Mike Preusch
2005-20-26 Aviointeriors S.P.A. 3-21-06
Not Applicable Midcoast Aviation
11-16-05 Model 312 Seats TT: 6185.6
CRS RO3R822L
(s258271.eng1.TFE-731-5R-1H.adc.doc) Page 1 of 1
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 6400 Curtiss-Steinberg Drive, Cahokia, IL. 62206 Phone: 618-646-8000 CRS No. RO3R822L
Unreadable
A72-3296
Replacement Of #1 Bearing 5-31-94 Complied With At Production Allied Signal
11-1-84
Unreadable
A72-3624
One Time Oil And Filter Resample 3-25-99 Not Applicable Garrett Aviation
1-21-98
CRS U02R221L
Recur –
A72-3641 Prevent Failure Of HPC Impeller Initial @ CZI John Gilmore
CZI Or
Revision 5 Effectivity: 7-24-03 Complied With Repeat @ Premier Turbines
Next CZI /
Access
6-2-04 P/N: 3074600-1/-2/-3/-4/-5 CRS NZUR892L
Next Access
Engine – Temperature – Remove
Unreadable
A77-3020 And Replace Specific Serial
7-21-97 Not Applicable Garrett Aviation
4-27-90 Numbered Thermocouple Lead
CRS U02R221L
Assemblies
(s258271.eng1.TFE-731-5R-1H.msb.doc) Page 1 of 1
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457
ENGINE SERIAL NO.: P91653 (#1) ENGINE TOTAL TIME: 6250.1 ENGINE CYCLES: 5208
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
(FAN) FAN ROTOR
Fan Disc
90PX152 10,000 0 0 5-31-94 -- 10,000 --
3074621
Fan Spinner
4-13262-136 See Note 1 of SB 0 0 5-31-94 -- -- --
3074623
s258271.eng1.TFE-731-5R-1H.llc.doc Page 1 of 3
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457
ENGINE SERIAL NO.: P91653 (#1) ENGINE TOTAL TIME: 6250.1 ENGINE CYCLES: 5208
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
Disc
Not Applicable 6,000 -- -- -- -- -- --
3074935
(HPT) HP TURBINE
HPT Rotor Seal Plate
0-03160-1163 30,000 0 0 5-31-94 -- 30,000 --
3075205
HPT Disc
3-12172-1282 10,000 0 0 5-31-94 -- 10,000 --
3075227
HPT Disc
Not Applicable 10,000 -- -- -- -- -- --
3075772
(LPT) LP TURBINE
LPT 1st Stage Disc
Not Applicable 10,000 -- -- -- -- -- --
3074747
s258271.eng1.TFE-731-5R-1H.llc.doc Page 2 of 3
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457
ENGINE SERIAL NO.: P91653 (#1) ENGINE TOTAL TIME: 6250.1 ENGINE CYCLES: 5208
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
Note 1: These Component Parts Have Not Had Cyclic Life Limits Assigned, But May Be Subject To Failure As A Result Of Undetected Abuse And Unpredictable
Contingencies. Therefore, To Provide A Record Of Service Experience And Cycles (Partial Cycle Counting Does Not Apply), A Life Limited Part Log Card
Must Be Maintained. If The Part Is Removed, The Life Limit Part Log Card Must Be Updated And Stay With That Part .
Note 2: When The Cycle Life Limit Is Reached On Impeller, P/N: 3070274, It Is Re-workable To P/N: 3073393 Per SB TFE731-72-3239 RWK. After Impeller Is
Reworked To P/N: 3073393, Cycle Count Returns To Zero, With A Service Life Limit Of 10,000 Cycles. Return Impeller With Life Limit Part Log Card To
Honeywell, Phoenix, AZ For Rework.
Note 3: When The Cycle Life Limit Is Reached Impeller, P/N: 3072639, It Is Re-workable To P/N: 3073394 Per SB TFE731-72-3239RWK. After Impeller Is
Reworked To P/N: 3073394, Cycle Count Returns To Zero, With A Service Life Limit Of 10,000 Cycles. Return Impeller With Life Limit Part Log Card To
Honeywell, Phoenix AZ For Rework.
Note 4: Dimensionally Inspect Dis For Growth At Each Major Periodic Inspection At Intervals Defined By The Applicable Inspection Interval Service Bulletin, But
Not To Exceed 1,700 Hours.
Note 5: Refer To Service Bulletin TFE731-A72-3519. Replacement Of The Disc Is Required When The Disc Has Accumulated 1,5000 Engine Operating Hours. If
The Disc Accumulates 1,500 Engine Operating Hours Prior To Reaching Its Cycle Life Of 3,000 Cycles, It Must Be Retired From Service.
Note 6: Refer To Service Bulletin TFE731-A72-3519. Replacement Of This Disc Is Required When The Disc Has Accumulated 750 Engine Operating Hours. If The
Disc Accumulates 750 Engine Operating Hours Prior To Reaching Its Cycle Life 3,000cycles, It Must Be Retired From Service.
Note 7: Refer To Service Bulletin TFE731-A72-3519. Inspection Of The Disc Is Required At Intervals Not To Exceed 1,500 Engine Operating Hours. If The Disc
Accumulates 4,500 Engine Operating Hours Prior To Reaching Its Cycle Life Of 3,000 Cycles, It Must Be Retired From Service.
Note 8: Refer To Service Bulleting TFE 731-A72-3668 And Airworthiness Directive (AD) 2001-23-09 For Fan Disc Replacement Schedule.
Note 9: Refer To Service Bulletin TFE731-72-3705 And Airworthiness Directive (AD) 2005-05-15 For Disc Replacement Schedule.
Note 10: Applicable To All Dash Numbers.
s258271.eng1.TFE-731-5R-1H.llc.doc Page 3 of 3
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 6400 Curtis-Steinberg Drive Cahokia, IL. 62206 Phone: 618-646-8000 CRS No. RO3R822L
AIRWORTHINESS DIRECTIVE COMPLIANCE RECORD
THROUGH BI-WEEKLY 2006-16
Manufacturer Model Registration No.: N803CE
Honeywell, Inc. TFE731-5R-1H Engine Serial Number: P-91659 (#2) Serial No.: 258271
1. Authorized by
AD Number Complied One Next Due
1. Subject 1. Status 2. Facility
Ctry - AD# 1. Date or 1. Date
2. Comments 2. Method of Compliance/Applicability 3. Certificate Type
Revision - Paragraph 2. Time Recur 2. Time
4. Certificate Number
To Prevent An Uncommanded
Unreadable
89-22-16 L Engine Acceleration or Deceleration. 7-21-97
Not Applicable By Serial Number One Garrett Aviation
11-16-89 S.B. 76-3049 TT: 1131.6
CRS U02R221L
Effectivity: All
To Prevent Over temperature and
Unreadable
90-24-06 Damage of Turbine Components 7-21-97
Not Applicable By Serial Number One Garrett Aviation
11-13-90 S.B. A77-3020 TT: 1131.6
CRS U02R221L
Effectivity: All
To Prevent Multiple In-flight Engine
Unreadable
92-02-18 Failures 7-21-97
Not Applicable One Garrett Aviation
2-10-93 S.B. 72-3470 TT: 1131.6
CRS U02R221L
Effectivity: All
Recur
To Prevent Failure of the HPC Every CZI Or
John B. Gilmore
2000-15-09 Impeller Due to Fatigue Cracking 7-25-03 CZI or Access To
Complied With Premier Turbines
10-10-00 S.B. A72-3641 TT: 4171.9 Access HPC
CRS NZUR892L
Effectivity: All to HPC Impeller
Impeller
(s258271.eng2.TFE-731-5R-1H.adc.doc) Page 1 of 1
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 6400 Curtiss-Steinberg Drive, Cahokia, IL. 62206 Phone: 618-646-8000 CRS No. RO3R822L
Unreadable
A72-3296
Replacement Of #1 Bearing 5-13-02 Not Applicable Garrett Aviation
11-1-84
CRS U02R221L
John Gilmore
A72-3624
One Time Oil And Filter Resample 7-25-03 Complied With Premier Turbines
1-21-98
CRS NZUR892L
Recur –
A72-3641 Prevent Failure Of HPC Impeller Initial @ CZI John Gilmore
CZI Or
Revision 5 Effectivity: 7-25-03 Complied With Repeat @ Premier Turbines
Next CZI /
Access
6-2-04 P/N: 3074600-1/-2/-3/-4/-5 CRS NZUR892L
Next Access
Engine – Temperature – Remove
Unreadable
A77-3020 And Replace Specific Serial
7-21-97 Not Applicable Garrett Aviation
4-27-90 Numbered Thermocouple Lead
CRS U02R221L
Assemblies
(s258271.eng2.TFE-731-5R-1H.msb.doc) Page 1 of 1
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457.0
ENGINE SERIAL NO.: P91659 (#2) ENGINE TOTAL TIME: 6052.2 ENGINE CYCLES: 5059
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
(FAN) FAN ROTOR
Fan Disc
3-12172-728 10,000 0 0 7-31-94 -- 10,000 --
3074621
Fan Spinner
4-13262-264 See Note 1 of SB 0 0 7-31-94 -- -- --
3074623
s258271.eng2.TFE-731-5R-1H.llc.doc Page 1 of 3
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457.0
ENGINE SERIAL NO.: P91659 (#2) ENGINE TOTAL TIME: 6052.2 ENGINE CYCLES: 5059
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
Disc
Not Applicable 6,000 -- -- -- -- -- --
3074935
(HPT) HP TURBINE
HPT Rotor Seal Plate
0-03160-1183 30,000 0 0 7-31-94 -- 30,000 --
3075205
HPT Disc
3-12172-1292 10,000 0 0 7-31-94 -- 10,000 --
3075227
HPT Disc
Not Applicable 10,000 -- -- -- -- -- --
3075772
(LPT) LP TURBINE
LPT 1st Stage Disc
Not Applicable 10,000 -- -- -- -- -- --
3074747
s258271.eng2.TFE-731-5R-1H.llc.doc Page 2 of 3
Report Produced By: Midcoast Aviation, Inc. Address: St. Louis Downtown Airport, 14 Archview Dr., Cahokia, IL. 62206 Phone: 618-337-2100 CRS NO. RO3R822L
LIFE LIMITED COMPONENTS
TFE 731-5R-1H
REFERENCE SERVICE BULLETIN TFE731-72-3001, REVISION 51 DATED: 3-2-06
REGISTRATION NO.: N803CE SERIAL NO.: 258271 TOTAL TIME: 6484.0 LANDINGS: 5457.0
ENGINE SERIAL NO.: P91659 (#2) ENGINE TOTAL TIME: 6052.2 ENGINE CYCLES: 5059
DESCRIPTION / PART NO. SERIAL NO. REQUIREMENT LAST COMPLIANCE NEXT DUE
SERVICE LIFE CYCLES HRS. CYCLES DATE HRS. CYCLE DATE
Note 1: These Component Parts Have Not Had Cyclic Life Limits Assigned, But May Be Subject To Failure As A Result Of Undetected Abuse And Unpredictable
Contingencies. Therefore, To Provide A Record Of Service Experience And Cycles (Partial Cycle Counting Does Not Apply), A Life Limited Part Log Card
Must Be Maintained. If The Part Is Removed, The Life Limit Part Log Card Must Be Updated And Stay With That Part .
Note 2: When The Cycle Life Limit Is Reached On Impeller, P/N: 3070274, It Is Re-workable To P/N: 3073393 Per SB TFE731-72-3239 RWK. After Impeller Is
Reworked To P/N: 3073393, Cycle Count Returns To Zero, With A Service Life Limit Of 10,000 Cycles. Return Impeller With Life Limit Part Log Card To
Honeywell, Phoenix, AZ For Rework.
Note 3: When The Cycle Life Limit Is Reached Impeller, P/N: 3072639, It Is Re-workable To P/N: 3073394 Per SB TFE731-72-3239RWK. After Impeller Is
Reworked To P/N: 3073394, Cycle Count Returns To Zero, With A Service Life Limit Of 10,000 Cycles. Return Impeller With Life Limit Part Log Card To
Honeywell, Phoenix AZ For Rework.
Note 4: Dimensionally Inspect Dis For Growth At Each Major Periodic Inspection At Intervals Defined By The Applicable Inspection Interval Service Bulletin, But
Not To Exceed 1,700 Hours.
Note 5: Refer To Service Bulletin TFE731-A72-3519. Replacement Of The Disc Is Required When The Disc Has Accumulated 1,5000 Engine Operating Hours. If
The Disc Accumulates 1,500 Engine Operating Hours Prior To Reaching Its Cycle Life Of 3,000 Cycles, It Must Be Retired From Service.
Note 6: Refer To Service Bulletin TFE731-A72-3519. Replacement Of This Disc Is Required When The Disc Has Accumulated 750 Engine Operating Hours. If The
Disc Accumulates 750 Engine Operating Hours Prior To Reaching Its Cycle Life 3,000cycles, It Must Be Retired From Service.
Note 7: Refer To Service Bulletin TFE731-A72-3519. Inspection Of The Disc Is Required At Intervals Not To Exceed 1,500 Engine Operating Hours. If The Disc
Accumulates 4,500 Engine Operating Hours Prior To Reaching Its Cycle Life Of 3,000 Cycles, It Must Be Retired From Service.
Note 8: Refer To Service Bulleting TFE 731-A72-3668 And Airworthiness Directive (AD) 2001-23-09 For Fan Disc Replacement Schedule.
Note 9: Refer To Service Bulletin TFE731-72-3705 And Airworthiness Directive (AD) 2005-05-15 For Disc Replacement Schedule.
Note 10: Applicable To All Dash Numbers.
s258271.eng2.TFE-731-5R-1H.llc.doc Page 3 of 3
DATE: August 14, 2006
MODEL: Hawker 800
REGISTRATION NUMBER: N803CE
SERIAL NUMBER: 258271
RECORDS RESEARCH FINDINGS
Section One
101. Fire Blocking Log Entry Date 11-6-95 Reference FAR 25.853(b) – Should Reference FAR 25.853(c)
o FAR Changed From FAR 25.853(b) To FAR 25.853(c) In 3-95
o Fire Blocking Report References FAR 25-853(c)
102. FAA Form 337 Dated 11-6-95
o STC Coversheet SA8588SW For Honeywell TCAS Not Located
o STC Coversheet ST09119SC For Dual Honeywell FMZ-2000 Flight Management System Not Located
Section Two
201. No Discrepancies Noted.
Section Three
301. No Maintenance Release Tag Located For Cabin Portable Fire Extinguisher SN W479453 Installed on 5-31-06
302. LP Warning Emergency Brake Pressure Switch SN 908 Installed On 3-12-02, FAA Form 8130-3 Indicates Unit As Repaired.
Unable To Determine TSO Or Next Due.
Section Four (The following airworthiness directives were not signed off in aircraft records as being complied with, not complied with, or not applicable.)
401. All Open Airframe AD’s Are Complied With As Part Of Inspection Or Signed Off As Not Applicable Thru FAA Bi-weekly
2006-16.
Section Five (The following airworthiness directives were not signed off in aircraft records as being complied with, not complied with, or not applicable.)
501. All Open Appliance AD’s Are Complied With As Part Of Inspection Or Signed Off As Not Applicable Thru FAA Bi-weekly
2006-16.
Section Six (The following service bulletins were not signed off in aircraft records as being complied with, not complied with, or not applicable.)
601. Mandatory Service Bulletin 21-3377 Revision 1 Dated 7-1-00 Not Signed Off (Not Applicable)
602. Mandatory Service Bulletin 21-3414 Revision 1 Dated 7-1-00 Not Signed Off (Not Applicable)
603. Mandatory Service Bulletin 24-319 Dated 2-15-95 Not Signed Off (Not Applicable By Serial Number)
604. Mandatory Service Bulletin 31-3055 Revision 1 Dated 2-1-99 Not Signed Off (Not Applicable)
605. Mandatory Service Bulletin 32-166 Dated 1-27-76 Not Signed Off (Not Applicable)
606. Mandatory Service Bulletin 32-167 Dated 1-27-76 Not Signed Off (Not Applicable)
607. Mandatory Service Bulletin 32-3386 Dated 6-1-00 Not Signed Off (Not Applicable By Serial Number)
608. Mandatory Service Bulletin 32-3696 Dated 7-1-05 Not Signed Off (Due By 1-27-2017)
609. Mandatory Service Bulletin 33-3586 Revision 1 Dated 11-1-04 Not Signed Off (Not Applicable)
610. Mandatory Service Bulletin 33-3682 Dated 3-14-05 Not Signed Off (Not Applicable By Serial Number)
611. Mandatory Service Bulletin 34-137 Dated 11-28-79 Not Signed Off (Not Applicable)
612. Mandatory Service Bulletin 35-A25 Dated 10-13-77 Not Signed Off (Not Applicable)
613. Mandatory Service Bulletin 35-3171 Dated 9-1-98 Not Signed Off (Not Applicable)
614. Mandatory Service Bulletin 53-85 Revision 1 Dated 5-23-95 Not Signed Off (Not Applicable By Serial Number)
Section Seven (The following service bulletins were not signed off in aircraft records as being complied with, not complied with, or not applicable.)
701. No Discrepancies Noted.
Section Eight
801. No Discrepancies Noted.
St. Louis Downtown Airport, #6400 Curtiss Steinberg Drive, Cahokia, IL 62206
Certified Repair Station Number: RO3R822L
(s258271.Tech Survey Findings.doc) Page 1 of 1
DATE: August 14, 2006
MODEL: Hawker 800
REGISTRATION NUMBER: N803CE
SERIAL NUMBER: 258271
135 FINDINGS
In Addition To Records Research Findings, The Below Listed Items Would Need To Be Addressed In Order To
Operate This Aircraft In Accordance With FAR 135.
Not Included In This List Are Items That Would Need To Be Completed Or Obtained By The Potential Operator.
These Are Items Such As But Not Limited To;
a. An Approved MEL
b. Pertinent Aeronautical Charts
c. IFR Operational Charts
d. Polices And Procedures Manual
e. Approved Aircraft Inspection Program (AAIP)
FINDINGS
1. Last Actual Weighing Dated 10-16-95 (36 Month Interval)
2. First Aid Kit Expired (In Work)
3. Numerous Interior Placards Worn, Unreadable Or Missing
St. Louis Downtown Airport, 6400 Curtiss Steinberg Drive, Cahokia, IL 62206
Certified Repair Station Number: RO3R822L
(s258271.Tech 135 Findings.doc) Page 1 of 1