Hawker 400XP/Beechjet/Diamond

Beechjet/Hawker 400xp
Team Beechjet/400xp
April 26, 2016
AGENDA
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Introduction To Team Beechjet
Upcoming Events
Fleet Statistics
ADS-B
New Beechjet Team Group Email
TXTAVSupport.com
Service Directory App
Technical Information
Technical Panel Q & A
TEAM Beechjet/400xp
Jessica Busse
Manager
Office: 316.517.5458
JBusse@txtav.com
Bill Jarvela
Customer Service Engineer
Office: 316.517.4336
WJarvela@txtav.com
Jeff Bowen
Customer Service Engineer
Office: 316.517.4070
JBowen@txtav.com
Luke Liby
Customer Service Engineer
Office: 316.517.4989
LLiby@txtav.com
Jorge Valdes
Customer Service
Engineer
Office: 316.676.3602
JValdes@txtav.com
Premier Technical Support 1.800.429.5372 or 1.316.676.3140 or Beechjet400xp@txtav.com
UPCOMING EVENTS
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EBACE – GENEVA May 24-26
APAC Customer Conference – SINGAPORE June 13-14
Australia Customer Conference – BRISBANE June 16-17
LABACE – SAO PAULO August 23-25
NBAA – ORLANDO November 1-3
Beechjet/400xp Fleet Statistics
MU300 / 400 / 400A / 400T(T-1A) / 400T(TX)
Fleet Size: 949 Airplanes
Fleet Total Time: 6.2 Million Hours, 6.2 Million Cycles
Average Total Time: 6,568 Hours, 6,547 Cycles
ADSB SB 34-4154
• ADSB Optional SB 34-4154 for
RK-1 Thru RK-604
• Information Only Kits
• Aircraft With Single GPS
– 128-3419-1 Kit
– 128-3420-1 Kit
• Aircraft With Dual GPS
– 128-3419-3 Kit
– 128-3420-3 Kit
• Flight Manual Supplement
28-590001-0355 Is Required
and Ordered Separately
• Bulletin Only Available At
Textron Aviation Service
Centers
BEECHJET/400XP GROUP EMAIL
• New Group Email Address
– Beechjet400xp@txtav.com
– Replaces The Prior Email Of
Beechjet_400xp_Premier1_S
upport@txtav.com
– Prior Email Will Remain
Active
• New Address For The Premier
– Premier@txtav.com
TXTAVSUPPORT.COM
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TXTAVSUPPORT.COM
TXTAVSUPPORT.COM
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TXTAVSUPPORT.COM
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TXTAVSUPPORT.COM
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TXTAVSUPPORT.COM
SERVICE DIRECTORY APP
PRICE REVIEW FORM
• Avenue For Customers To
Request Price Review For Parts
– txtav.com
• Select Reason For The Request
– Price Higher Than Competition
– Price Much Higher Than Previous
Purchase
– Price Higher Than Related Part
– Other
• Provide As Much Additional
Information As Possible
SEALANT REMOVAL TOOLS
• Sealer Removal Tools
That Have Metallic
Sharp Edges/Points Can
Cause Damage To
Underlying Structure
 After Sealer Is
Removed Inspect
Underlying Structure
 If Damage Is Found,
Evaluate Damage Per
The SRM
 If Damage Falls
Outside The Scope Of
The SRM Contact
RDO
Suggested
Not
Recommended
FUEL QUANTITY INDICATION ISSUES
• LH/RH wing quantity
indication is
intermittent or
erratic.
• To help troubleshoot
the issue the 400A
fuel quantity test box
TE79-400A or the inshop made breakout
box (see AMM 2841-00-101) can be
used.
FUEL QUANTITY INDICATION ISSUES
• Mid Fuel Probe
Installed Upside
Down Relative to the
Rest Of The Probes.
• Probe Is Mounted
Just Outboard Of
The Collector
Chamber.
• Access Is through
the wing second
most inboard fuel
tank panel.
• Remove prove,
clean and air dry
probe and
connectors.
MLG SIDE STRUT LEVER
• Lever Compresses
the MLG Down-Lock
Switch
• Corrosion and Lack
of Lubrication
Causes Lever Pin to
Bind
• A binding lever
mechanism may not
properly compress
the related down lock
switch which will
cause L/G
extend/indication
problems
MLG SIDE STRUT LEVER
• Pin Has Forward and
Aft Lube Point.
• Insure Lube Flows Out
From Side Strut
Bushings.
RUDDER BOOST
• Rudder Boost Fail Light Illuminates
• Rudder Boost Fail Light Illuminates with Yaw Damp Disengagement at the
same time
 “FCS Diagnostic” fault code
retrieval must be
done prior to turning off the
Radio Master switches.
Codes are stored in
Volatile Memory.
 Look for any non-zero
REPAIR, YD DIS, YD ENG
and BOOST codes.
Record all six digits
or take picture of screen
and call Tech Support
for Decode.
RUDDER BOOST
• Rudder Boost Fail Light Illuminates
 AMM section 27-21-00-201. Rudder Boost System Test – Engine Ground
Operating Procedure
 Monitor the Bleed Air Transducer voltages in the “Input Mode” of FCC
Diagnostics on the Pilot’s MFD
 Look for the BLEEDL and BLEEDR transducer voltages to be within .04 volts
 If any of these voltages do not match the others, swap pressure transducers
to eliminate wiring to the FCC’s and determine if pressure transducer is at fault
 If these voltages are approximately equal, the problem is most likely not the
transducers and could be related to an erroneous DAU output or annunciator
problem
RUDDER BOOST
• Rudder Boost Fail Light Illuminates with Yaw Damp Disengagement
at the same time
 Faulty engine bleed air transducer is less likely and points towards a
Rudder Servo or FCC
 Servo and FCC Test Procedures are located in the Maintenance section
of the Collins Avionics System Manual p/n 523-0775807
LORD MOUNTS
• For overhaul/exchange questions on your LM-420-SA42 or other LORD
mounts, please contact Repairstation@LORD.com – they can provide pricing
and estimated turnaround time.
• Here is their website for reference: http://www.lord.com/industries/aerospaceand-defense/owners-operators-and-mro
• LORD Corporation
• http://www.lord.com
LH/RH BUS TIE ¾ AMP C/B POPS INTERMITTENTLY
• During ground or flight
operations the LH or
RH Bus Tie ¾ amp c/b
pops.
• After resetting c/b it
may stay set for a
while or pop soon
after.
• The ¾ c/b can be
checked by pulling it
and setting it to see if it
feels defective.
• Confirm there are no
shorts from the Bus
Tie RCCB to the
Feeder RCCB’s.
LH/RH BUS TIE ¾ AMP C/B POPS INTERMITTENTLY
RCCB p/n 45AS88810-3
• Majority of time the
fault is in the LH/RH
Bus Tie Remote
Control C/B (RCCB).
• The RCCB is located
in the aft power
distribution panel.
• The RCCB current
sense internal logic
circuits go bad and
provides a signal to ¾
amp c/b to pop as if
there was an
overcurrent condition.
ENGINE WILL NOT ROTATE ON START
• The LH/RH engine start
switch is pressed and the
engine will not rotate. A ‘clunk’
or ‘shuttering’ may be noted
instead.
• One of two components are
the usual cause of this. One is
the Gen Field RCCB and the
other is the nacelle mounted
Generator Current
Transformer (CT).
ENGINE WILL NOT ROTATE ON START
• If the start switch button does not
stay lit after pushing it the fault
may be the field RCCB.
• The LH/RH RCCB is located in the
aft power distribution box.
• The RCCB internal switch contacts
for the aux start relay develop high
resistance which makes the engine
try to start using the generator
contactor instead of the start
contactor.
• The RCCB switch contact can be
troubleshot using the GCU
connector contact ‘Z’. Normal
resistance through contact is aprox
290-300 ohms.
RCCB P/N SM600BA10A1
ENGINE WILL NOT ROTATE ON START
• If the start switch button
stays lit then the fault may
be the engine mounted CT.
• The CT is part of the
ground fault protection
circuit for the generator
power output cable.
• There are two CT’s per
generator system, but the
one at the engine is the
one that fails due to its
harsh environment.
• To confirm if the fault is in
the CT both CT’s on the
problem side are bypassed.
CT P/N 45AS88801-21
AIRCRAFT WASHING
• Dos
– Check EPA and Airport
Regulations
– Regularly Clean Your Aircraft
– Cover Exposed Openings:
Pitot Static Ports Etc.
– Use Mild Detergent and Water
– Rinse Thoroughly
– Hand Wash Gear
– Clean Windows With Approved
Cleaner
• Don’ts
– Wash Away Lubrication
– Use Rubbing Compounds Or
Abrasive Cleaners
– Pressure Wash
– Wear Jewelry
ELEVATOR HEATER HORNS
Application Procedure Chapter 30
Polyurethane Erosion Resistant
Coating 81C24-VC
VIBRATION SIGNAL CONDITIONING UNIT
• Meggitt MRO is offering repair and evaluation on the Vibration Signal
Conditioning Unit p/n 45AS86803-11.
• Contact:
Johnna Garcia
949 276-0458
johnna.garcia@meggitt.com
• Address:
Meggitt OC
14600 My Fort Rd.
Irvine Ca. 92606
Attn: MRO
ULB 90 DAY BATTERY REQUIREMENT
• On Dec 1, 2015 the FAA’s TSO-C121b requires all newly manufactured
Underwater Locator Beacons (ULB) to comply with a 90 Day minimum
duration.
• There is currently no requirement to retrofit a 30 day ULB to a 90 day ULB.
The FAA hopes to move the 30 day ULB to the 90 day ULB through attrition.
The 30 day ULB’s can be used as long as they are serviceable.
• EASA Notice of Proposed Amendment (NPA) indicates that European aircraft
will however be mandated to carry only the 90 day ULB.
• 30 day ULB’s are no longer available for sale with a valid TSO certification
and can only be maintained. Batteries for these units will continue to be
produced.
• 90 day ULB replacement on recorder
device will not change CVR or FDR
part number. Will be a MOD Plate strike.
PART NUMBER VARIANCE
• If Part Number Called
Out In IPC Does Not
Show Up On Parts
Website
– Search For First Few
Characters Of The
Number
– As You Build Up
Characters In Your
Search Remove
Hyphens And Spaces
• Verify Part
Description Matches
IPC
1st Search
2nd Search
34
PILOT SERVICES GROUP
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Supports All Citations, 208’s,
King Air & Hawker Products
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Pilot Oriented Technical Support
 CESNAV, CPCalc, CLCalc,
EOM
 Electronic Flight Documents
 AFM and OM content
 Performance, W&B
 Certification Issues
•
Note: For subscription related issues,
please contact Technical Manual
Distribution Center
Rob Below
Pilot Services
cesnav@txtav.com
RVSM MANUAL SERVICE
•
New and Pre-Owned Textron
Aviation Products
•
Manuals come with:
 RVSM, RNP-10, RNP-4, NATHLA Operations Procedures
 RVSM Maintenance Program
 Applicable Hawker, Beech,
Cessna Tech Pubs
 For Citation Part 91 operators:
Request to Use MMEL as an
MEL (along with supporting MMEL and
Operations and Maintenance Procedures)
•
GMU Service Available
 GPS Height Monitoring Flight

We Can Come To Your Location
Matt Thompson
RVSM Manuals
rvsm@txtav.com
INSPECTION AUTHORIZATION CARD
Technical Presentation Worth IA Credit
EVENING EVENT
Everyone Is Invited To Attend This Evenings
Social Gathering From 6:00 to 8:30
At:
Charles Koch Arena
1845 Fairmount St.
Wichita, Kansas 67260
Note: You Must Have Your Conference Badge To Attend
TECHNICAL PANEL
• Beechjet Model Team Panel
– Jorge Valdes, Bill Jarvela, Jeff Bowen and Luke Liby Tech
Support
– Gary Long Engineering
– Chris Harrold Flight Test
– Tim Kucharo RDO
– Chris Kidd Parts
– Randy Znamenak Aftermarket Sales
QUESTIONS
Questions