“planes is in Grenoble France it'us registered N118HC all the phase has been done (1,2,3,4) signed.
Item specifics
| Used |
| “planes is in Grenoble France... it'us registered N118HC all the phase has been done (1,2,3,4) signed by the french shop on february 2016, but not by the faa inspector due to his defect.airworthy, but need to finish the paperwork..paint is ok, interior usable but tired, new carpet.there is a condition notice on the airplane.” |
| Make: | beechcraft | Model Year: | 1974 |
new power section on one engine, garmin 430 avionic, ifr equipment.
all the notification below has been done in a french shop, with french agreement, but rudy bichelmeyer, the faa inspector, didn"t sign all the work he has asked himself... wich is really unfair... so the plane is still grounded.
Rudolf Bichelmeir FAA A & P I.A. Kreuthstr. 4 86609 Donauwörth Germany Mobile: 0049 (177-586-1290) E-mail: bichelmeir @ hotmail.com # Aircraft Specification & Work Sheet:
Manufacturer: Hawker Beechcraft Corp.
AFTT: (iaw FlightLog) 14453.03 Hours Aircraft Model: C90 Hobbsmeter: N/A Hours
Aircraft Serial #:
LJ-648 TT Landings: TT Cycles: TIS/Ldgs/Cyl s Last Insp.: 12948 Ldgs 12948 Cycles 86.0 Hrs & 75 Cycles Aircraft Tail #: N118HC Last Periodic Insp. Phase 1 & 2 @ 14453.03 Hrs
TCDS: 3A20 Rev. 75 March-26-2014
Location of last Insp.: Blue Aero Grenoble, France Built & Certified: Reg Owner: Reg Expiration: 1974 Grimaud Inc. June-30-2017
Final Date:
Feb-05-2015 # Remarks: Aircraft needs to by rechecked / inspected for Conformity or an Special Flight Permit must be issued to relocate the Airplane where the Discrepensis can be completed. # STC´s installed: #STC ST02621NY Kanad 406AF-ELT per Form 337, dated Dec-6-2008. # Installations per Form 337: Garmin GTX 330 Txp, Txp & GPS Antennas, dated: Dec-6-2008. Garmin GMA 340P, Garmin GNS 430W and WAAS Antennas, GAD 42 Interface Unit, dated: Feb-23-2010. # Open Items found on Inspection: #(3) Seat Belts are not correct (Aluminium Lock) #RH Stall Strip is missing. #Registration Marks not in size iaw FAR 45. #Dataplate has been made of Stainless Steel (Serial# and Model). #Oxygen Cylinder (DOT 3HT 1850) Hydrostatic Test Overdue (Chapter 4 Item) #Cabin Fire Extinguisher Hydrostatic Test overdue (Chapter 4 Item), #LDG Actuator OH Overdue (Chapter 5 Item). #Prop Governor Woodward OH Overdue (Chapter 5 Item). #FAR 91.411 & 413 Overdue. #Crack on RH Main Wheel Assy (see NDT Test Report for Details. #RH Aileron Upper Inboard Attach Bracket corroded & cracked. #See Detailed Listing on Page 2 Manufacturer: Pratt & Whitney Manufacturer: Pratt & Whitney Model: PT6A-20A Model: PT6A-20A Serial #: PC-E 21850 Serial #: PC-E 22282 ETT: 15754.85 Hours ETT: 23232.93 Hours ET s New or OH : 714.03 Hours ET s New or OH: 1473.03 Hours Total Cycles: Cycles s last OH : Last OH :
TBO iaw P& W: 20535 Cycles 464 Cycles by 13739.00 Hrs AFTT with 0.00 Hrs ETsOH & 20071 TT Cycles 3600 Hours Total Cycles: Cycles s last OH: Last OH:
TBO iaw P&W 28481 Cycles 975 Cycles by 12980.00 Hrs AFTT with 0.00 Hrs ETsOH & 27506 TT Cycles 3600 Hours #LH Engine was installed after OH with 0.0 Hrs ETsOH @ 13739.00 Hrs AFTT @ Dec-2007. #RH Engine was installed after OH with 0.0 Hrs ETsOH @ 12980.00 Hrs AFTT @ April-2004. Manufacturer: Hartzell Manufacturer: Hartzell Prop Model: HC-B3TN-3B Prop Model: HC-B3TN-3M Blade Model: T10173NB-8 Blade Model: T10173NB-8 Hub Serial #: BUA22615 Hub Serial #: BUA21203 PTT: 4562.65 Hours PTT: 1319.62 Hours PTsOH: 265.05 Hours PTsOH: 265.05 Hours Last OH:
by 14187.98 Hrs AFTT with 0.00 Hrs PTsOH @ March-2011
Last OH:
by 14187.98 Hrs AFTT with 0.00 Hrs PTsOH @ March-2011 #LH & RH Propeller was installed after OH with 0.0 Hrs PTsOH @ 14187.98 Hrs AFTT @ March-2011.
RuBi Aviation Aviation Maintenance & Consulting Germany
Phase Inspection performed and Signd in the Logbook
Phases performed Dated Performed @ AFTT: Hrs flown between Insp.
3 & 4 & Annual
Dec-6-2008
13895.70 Hrs
156.58 Hrs
1 & 2 & Annual
Jan-18-2010
14000.00 Hrs
104.30 Hrs
3 & 4
Mar-14-2011
14187.59 Hrs
187.59 Hrs
1 & 2
Mar-24-2012
14323.02 Hrs
135.43 Hrs
3 & 4 & Annual
Mar-12-2013
14367.02 Hrs
44.00 Hrs
1 & 2 & Annual
April-25-2014
14453.03 Hrs
86.00 Hrs
Note: using Chapter 5-00-00 & 5-21-00 Inspection Programs for Explanation: Hawker Beechcraft Corp. requires that no Airplane exceed 12 months without completing at least one Phase Inspection.
BIENNIAL INSPECTION PROGRAM For users flying less than 200 hours in 24 months, perform the Biennial Inspection Program in Chapter 5-22-00 or 5-26-00.
Biennial Inspection: the Inspection Program is for users flying less than 200 hours in 24 months and it is made up of an INTERIM INSPECTION and a COMPLETE INSPECTION.
▪ Perform an INTERIM INSPECTION at 12 months and every 24 month thereafter. ▪ Perform a COMPLETE INSPECTION at 24 months and every 24 months thereafter.
Note: Hawker Beechcraft Corp. requires that no airplane exceed 12 months without completing at least one Phase Inspection or Interim as appropriate to the Program used.
200 HOURS PHASE INSPECTION PROGRAM All four Phase Inspections must be completed each 24 Calendar Months. Hawker Beechcraft Corp. requires that no Airplane exceed 12 Months without of least one Phase Inspection.
Although the times of the Inspections may be altered, each Item should be accomplished as stated in the Inspection Program. A detailed Preamble to this Subchapter is included and should be read and understood before beginning the Inspection Program.
ALTERNATE PHASE INSPECTION PROGRAM For Users flying less than 400 Hours but more than 200 Hours in 24 Months, perform the Alternate Phase Inspection in Chapter 5-21-00 or 5-25-00.
Alternate Phase Inspection: if an Airplane is not flown at least 400 Hours in 24 Months, the Owner/Operator has the Option of inspecting the airplane as follows:
▪ Perform scheduled Phase Inspections 1 & 2 together within 12 Months after the last Inspection, then perform scheduled Phase Inspections 3 & 4 together within 12 Months after completing the Phase 1 & 2 Inspections.
RuBi Aviation Aviation Maintenance & consulting Germany
# Open Items & Discrepancis found on Inspection:
#Passenger Seat Belts (3) are not correct (Aluminium Lock). Not iaw FAR 23.785 (b) Corrective Action: Replace Passenger Seat Belt with new or servicible Items
#RH Stall Strip is missing. Corrective Action: install new missing Stall Strip iaw M.M. Chapter 30-10-00
#Size of Registration Mark not iaw FAR 45.29 Corrective Action: reinstall Reg Marks iaw FAR 45.29 (b) (1) in the correct Size.
#Aircraft Identificationplate in Aluminium Type. Corrective Action: install new fabricated Identificationplate iaw FAR 45.11 (Stainless Steel ) with Model and Serial#
#Oxygen Cylinder (DOT 3HT1850) Hydrostatic Test Overdue by Time (Feb-2010) (Chapter 4 Item). Corrective Action: send O2 Cylinder and Regulator to approved facility to perform HydroStatic Test.
#Cabin & Cockpit Fire Extinguisher Hydrostatic Test overdue by Time (Nov-2013 & July-2014) (Chapter 4 Item), Corrective Action: install new Cabin Fire Extinguisher or perform Test
#LDG Actuators OH Overdue by Time (Sept-2014) (Chapter 5 Item). Corrective Action: send Actuator for Overhaul or replace with servicible Actuators
#Prop Governor Woodward OH Overdue by Time (LH Nov-2012, RH April-2009) (Chapter 5 Item). Corrective Action: send GOVs for Overhaul to approved Facility
#FAR 91.411 & FAR 91.413 Overdue by Time (March-2012) (Chapter 5 Item) Corrective Action: perform Test by FAA approved CRS
#Crack on RH Main Wheel Assy (see NDT Test Report for Details.) Corrective Action: replace with new (Note: new Wheel and Brake Assy iaw Cleveland STC is on Order and on the Way)
#RH Aileron Upper Inboard Attach Bracket cracked and Corrosion noted. Corrective Action: replace or repair cracked and Corroded Areas
#Floor Carpets are not iaw FAR 23.853(3) (ii) Corrective Action: replace Floor Carpets with approved Item iaw FAR 23.853, Note: Seats, Refurbishment , Sidewalls, Headliners are Original Beechcraft Items. # FAA Aircraft Condition Notice, dated June-22-2014 at Grenoble, France (see FAA Form 8620-1)
#Provide proof of Completion and Current Status of Inspection Program. Performed Action : inspected Aircraft File and reorganized Documents ,using Hawker Beechcraft Corp. M.M. Schedule Inspection Programs ,Chapter 5-21-00, dated: Dec-01-2007 and found that this Aircraft is in Schedule Phase Inspection Program. (14CFR FAR 91.409(f) (3) (Note : See Phases performed on attached Sheet). Aircraft is on KARDEX System and Life Limited Components tracked iaw FAR 43 by Blue Aero, Grenoble FR.
#Provide approval Documentation to substantiate the currently installed Avionics and ELT. Performed Action: found by the Document Research that the Installation of Avionic and ELT an FAA Form 337 was issued and the ICA are in the permanent Aircraft File (Note: Form 337s dated: Dec-6-2008 and Feb-23-2010), an updated Equipment Listing (dated: July-12-2014) and Weight & Balance Report (dated.March-15-2011) was found is inside the Flight Manual
#Visible Corrosion Problems on Aircraft. Performed Action : inspected the Aircraft Interior and Exterior iaw M.M. and found on RH Aileron inboard upper Attach Bracket, Corrosion and cracked Surface Skin.
#Show Aircraft Airworthiness Directive Compliance. Performed Action: found in the Aircraft File/Documents an AD Listing (Airframe, Engines, Propellers, Appliances) with recurrent Status Items, issued at the last Phase Inspection (Note: dated: April-2014, signed by Jean Claude Itofo, A&P# 2478983)
#Provide Proof of NDT Inspection Compliance. Performed Action: found in the Aircraft File/Documents the Testing Report (Work Order#: 1420244PT-1) of Marlier SA, approved as NDT Company FR 145-438 per ASNT-TC-1A. (Inspection was performed by Patrick Fabre, performing Date: April-24 to 25 2014) Inspection was perfomed iaw SIRM Chapter 57-13-01, Part#: 98-39006, dated: Dec-1-1982 & Part#: 98-39006C10, dated: Nov-2013.
Rudolf Bichelmeir A&P 2421308 I.A. Location: Grenoble France Date: Feb-5-2015
Current date: 2016-08-30