Aviation Services Airworthiness Directive Compliance Record N800TS SIN BB-1032 Compliments of Air Care Maintenance Department Repair Station No. ACOR030C
Content Revision: 3/2/2015 Beech Aircraft Corp. 75-14-03 7/3/1985 83-07-14 4/18/1983 84-24-01 1/1/1984 85-22-05 11/12/1985 86-20-03 10/15/1986 87-04-24 4/14/1987 Airframe FAA Airworthiness Directive Com liance Record File ID: N800TS TO PREVENT THE AIRCRAFT FROM EXCEEDING 60 DEGREES BANK ANGLE AS A RESULT OF AN AUTOPILOT HARD OVER TO PREVENT DECOMPRESSION AND POSSIBLE INJURY CAUSED BY FAILURE OF A ONE-PLY WINDOW THAT MAY HAVE BEEN, CONTD. by 87-17-05 TO ASSURE STRUCTURAL INTEGRITY OF ATTACHMENTS OF OUTER WING PANELS TO THE WING CENTER SECTION by 87-04-24 TO PRECLUDE MALFUNCTION 5/18/2003 OF THE ELEVATOR TRIM CABLE SYSTEM 4/6/2006 TT:8655.5 NA by acft s/n NA by acft s/n Atnendnient Number od of~ompljap~~/applica bility CW by replacing wing bolts and nuts.ring inspection NA PCW as SB 2028R3 Aircraft Registration: Next Due Facility. or Date Cert. Typ:e. Time BB-1032 Printed 3/4/2015 4:41 :09PM Pa e 1 of 10
FAA Airworthiness Directive ComQliance Record Content Revision: 3/2/2015 File ID: NSOOTS Aircraft Registration: F~ A~ ~umber. Am~lidmeht Number.cnc:... uvt: Date I. of: Compliance/Applicability ::. ~ ~ '-'-..'... _:_...'.:.. Beech Aircraft Corp. Airframe 8200 87-17-05 R1 2/17/1988 87-22-01 R1 9/30/1989 89-19-04 R1 7/9/1990 89-22-14 11/17/1989 90-08-17 5/7/1990 91-12-10 7/15/1991 by 89-19-04 by 2004-23-02 TO ASSURE THE CONTINUED STRUCTURAL INTEGRITY OF THE WING FUEL BAY UPPER SKIN PANELS TO PREVENT POSSIBLE AILERON FLUTTER 3/5/2015 TT: 10116 Para (a)(3) PCW. ring due only on RH panel NA by acft s/n TO PREVENT WATER 2/4/2008 ACCUMULATION IN THE AFT TT:9047 CW by inspection FUSELAGE WHICH CAN FREEZE AND RESTRICT CONTROL MOVEMENT TO PREVENT IN-SERVICE FATIGUE FAILURES & TO ALLOW CONTINUED OPERATION OF THE NA by acft s/n INTERIM SAFE LIFE LIMIT, CONTD. 0tice ~ue Facility ~ 3~ Cert Nurri. or. Date Cert. t ype 4; A.uthor'. By ~ BB-1032 9-2016/TT:10 AirCarelnc 716 CRS ACOR030C Air Care Inc CRS ACOR030C Printed 3/4/2015 4:41 :09PM Pag_e 2of10
Content Revision: 3/2/2015 Beech Aircraft Corp. 91-12-11 7/15/1991 91-18-11 9/3/1991 92-06-11 3/30/1992 92-10-12 6/12/1992 92-15-01 8/21/1992 92-27-10 2/5/1993 Airframe FAA Airworthiness Directive Com liance Record File ID: N800TS TO PREVENT CRACKING & 7/19/1992 POSSIBLE BLOWOUT OF CAST ACRYLIC COCKPIT "D" SIDE WINDOWS THAT COULD RESULT, CONTD. by 92-10-12 PCW as SB 2208R1 TO PREVENT INCORRECT PILOT DECISIONS BASED ON ' NA by acft sin UNDETECTED ERRONEOUS ATTITUDE INFORMATION DISPLAYED BY, CONTD. TO PREVENT SEPARATION OF 12/3/1991 THE AFT COWLING DOORS, PCW as SB 2416R1 WHICH COULD RESULT IN OCCUPANT INJURY IF DECOMPRESSION OR, CONTD. TO PREVENT UNDETECTED 9/14/1992 FAILURE OF ENGINE PCW as SB 2432 TRUSS-TO-FIREWALL BOLTS, WHICH COULD EVENTUALLY LEAD TO SEPARATION, CONTD. by 97-06-06 Amendment Number f Compliance/Applicability Aircraft Registration: Next Du.e fc(lcility or Date C:ert Type Au. Time BB-1032 Printed 3/4/2015 4 :41 :09PM Pa e3of10
FAA Airworthiness Directive Com_p_liance Record Content Revision: 3/2/2015 File ID: N800TS Aircraft Registration: ~~~v~u~~=t... ~~.. ~ --. Complied - Amendment Number Orice e 1-:-t,-=o:-u-e~-:'1~...::.::. i_ : -'- Beech Aircraft Corp. 93-25-07 2/15/1994 95-13-03 7/28/1995 96-03-13 4/1/1996 96-09-13 c 6/11/1996 97-06-06 c 5/9/1997 97-23-17 12/29/1997 Airframe by 2005-01-18 - -' -L"''-' - Date Time B200 TO PREVENT EXCESSIVE 10/19/2006 CURRENT FLOW THROUGH THE TT:8857 PCW as SB 2035R3 ELECTRICAL LANDING GEAR MOTOR, WHICH COULD RESULT IN AN,CONTD. TO PREVENT MAIN LANDING 9/1/1996 GEAR COLLAPSE CAUSED BY ' PCW as SB 2607R1 DRAG LEG LOCK LINK FAILURE, WHICH COULD RESULT IN LOSS OF. CONTD. TO MINIMIZE THE POTENTIAL HAZARDS ASSOCIATED WITH OPERATING THE AIRPLANE IN PCW SEVERE ICING CONDITIONS, CONTD. TO PREVENT INADVERTENT 4/30/1995 MOVEMENT OF THE PILOT OR PCW as SB 2444R2 COPILOT CHAIR, WHICH COULD RESULT IN LOSS OF,CONTD.. F=a-c~il:":":ity-.--=3;-::c=-e-rt-:-.-:-N:-u-m--t. -= Me~~~~ Compli.:_nce/Applica~I~ _ R:~ur. ~~: Cert. t ype A~hor ~By TO PREVENT A LOSS OF 1/1/1997 VACUUM TO DEPRESSURIZE PCW as SB 2676 THE AIRPLANE CABIN, WHICH COULD RESULT IN PERSONAL INJURY TO THE.CONTD. BB-1032 Printed 3/4/2015 4:41 :09PM Pa_g_e 4 of 10
FAAA" 1rwo rth" 1ness o 1rec f 1ve c r om~1ance R ecor d Content Revision: 3/2/2015 File ID: N800TS Aircraft Registration: FAA AO. N.Omber I 0T Complied AmendmentNl!lllber Next Due Facility Cert.NUl'll. Effective Date Description Date Method of Cornpliance/Applicabilify or Date Cert. Type Al!thor. E!Y '-'...2 Time '-'.. Time Beech Aircraft Corp. Airframe B200 BB-1032 97-25-01 TO PREVENT OUTFLOW/SAFETY 1/11/1998 VALVE CRACKING AND NA by valve sin CONSEQUENT FAILURE, WHICH COULD RESULT IN RAPID DECOMPRESSION OF.CONTD. 97-25-03 TO PREVENT NOSE DOWN 2/1/1998 1/21/1998 PITCH AND A DESCENT RATE PCW LEADING TO AIRCRAFT DAMAGE AND INJURY TO PERSONNEL CAUSED BY.CONTD. 98-10-05 TO PREVENT FAILURE OF THE ' 6/27/1998 ENGINE FIRE DETECTOR NA by acft s/n SYSTEM IF HIGH HEAT AND/OR FIRE STOPPED AN ELECTRICAL SIGNAL, CONTD. 98-15-13 by 2005-01-04 8/28/1998 98-21-35 TO PREVENT FAILURE OF THE 11/23/1998 ACTUATOR CLEVIS ASSEMBLY NA by acft s/n IN THE MAIN LANDING GEAR CAUSED BY FATIGUE CRACKING OF.CONTD. 99-09-10 To prevent the inability to extend 6/7/1999 the landing gear with the hand NA by acft s/n pump caused by debris entering the landing, contd. Printed 3/4/2015 4:41 :09PM PC!9_e 5 of 10
FAAA" 1rwo rth" 1ness o 1rec f 1ve c r om~1ance R ecor d Content Revision: 3/2/2015 File ID: N800TS Aircraft Registration: FAA AD Number Complied Amendment Number \ once Next.Due Facility Cert. Num. Effective Date Descripti911 Date Method.. of Compliance/Applicability or Date <;ert. Type 4; A!Jthor. By Ti.me Time.. Beech Aircraft Corp. Airframe 8200 BB-1032 99-09-15 To prevent any components or 5/18/1999 wiring from interfering with the flight NA by acft s/n control mechanism caused by inadequate, contd. 99-18-15 To detect any improperly machined 9/27/1999 landing gear emergency hand NA by acft sin pumps, which, if not removed from, contd. 2001-11-03 To protect the blower motor circuit 7/20/2001 and reduce the possibility of the. NA by acft s/n emission of smoke or a burning odor.contd. 2002-23-11 To prevent the balance weight 4/6/2006 1/10/2003 attachment screws from becoming TT:8655.5 PCW loose 2003-02-03 To assure that clear and complete 9/18/2003 3/7/2003 operating instructions are visible for PCW opening the airstair,contd. 2003-13-16 To detect and correct damage to 4/6/2006 8/25/2003 the aft pressure bulkhead of the PCW fuselage Printed 3/4/2015 4:41 :09PM Pa_g_e 6 of 1 O
FAA Airworthiness Directive Com liance Record Content Revision: 3/2/2015 File ID: N800TS Aircraft Registration: Beech Aircraft Corp. Airframe 8200 BB-1032 2004-17-02 To detect and correct loose bolts 11/3/2003 10/4/2004 not securing the pedestal cross PCW as SB 73-362ring NA shaft, which could result in limited, contd. 2004-23-02 c To detect and correct cracks in the 3/5/2015 TI:10316 Air Care Inc 12/23/2004 Nose Landing Gear (NLG) fork, TI:10116 CW by visual and FPI inspection CRS which could result in reduced structural, contd. ACOR030C 2005-01-04 C2 To prevent fuel flow interruption, 2/4/2008 Air Care Inc 2/22/2005 which could lead to uncommanded TI:9047 PCW as AD 98-15-13 and no suspect hose CRS loss of engine power & loss of installed up to effective date of AD ACOR030C control, contd. 2005-01-04 2005-01-18 C2 To detect and correct any cracked 3/5/2015 TC:9496 Air Care Inc 3/1/2005 fuselage stringers in the rear TC:8996 CW by inspection CRS pressure bulkhead area, which could, contd. ACOR030C 2006-12-25 To prevent failure of the actuator 3/7/2014 7/28/2006 nut assembly for the right MLG TI:8857 CW by inspection actuator, which could result in failure, contd. 2006-23-02 c by 2007-12-06 12/13/2006 Printed 3/4/2015 4:41 :09PM Pa e 7of10
Content Revision: 3/2/2015 I FAAAD Number 1 ~fffctiv~ p~te _:j Beech Aircraft Corp. 2007-12-06 7/16/2007 2008-07-10 4/10/2008 2010-26-03 12/20/2010 Hartzell Propeller 96-15-04 7/29/1996 Airframe To detect and correct improperly assembled or damaged flight controls, which could result in an, contd. FAA Airworthiness Directive ComQliance Record File ID: N800TS Complied Date. time B200 2/4/2008 TT:904 7 To.prevent collapsed pneumatic 2/6/2009 supply tubes, which could result in TT:9181 failure of the tail deice boots to operate AinendinentNuinber Method of Compliance/Applicability --'- ~ NA by acft sin NA by acft s/n To prevent collapsed pneumatic 2/3/2011 supply tubes, which could result in TT:9570 NA by acft s/n failure of the tail deice boots to operate Propeller TO PREVENT PROPELLER BLADE SEPARATION CAUSED BY PROPELLER BLADE SHANK CRACKS EMANATING FROM FORGING FLAWS.CONTD. HC-D4N-3A 2005-14-11 To prevent blade failure that could 2/4/2008 8/17/2005 result in separation of a propeller TT:9047 blade and loss of control of the airplane NA by p/n NA, no work performed by suspect company Aircraft Registration: or... Next Due.Date Time Facility Cert. Num. Cert. Type Author. By BB-1032 Air Care Inc CRS ACOR030C Air Care Inc CRS ACOR030C Air Care Inc CRS ACOR030C FY-372A Air Care Inc CRS ACOR030C. :_: - Printed 3/4/2015 4:41 :09PM Pa_g_e 8 of 10
- FAA Airworthiness Directive Com liance Record Content Revision: 3/2/2015 File ID: NSOOTS Aircraft Registration: Hartzell Propeller 96-15-04 7/29/1996 2005-14-11 8/17/2005 Pratt & Whitney Canada 97-04-12 3/14/1997 2002-23-13 12/31/2002 Propeller TO PREVENT PROPELLER BLADE SEPARATION CAUSED BY PROPELLER BLADE SHANK CRACKS EMANATING FROM FORGING FLAWS.CONTD. HC-D4N-3A NA by p/n mendment.number pliahce/applic~bility Next Due Facility or Date Cert. Type Au Time FY-261A To prevent blade failure that could 2/4/2008 Air Care Inc result in separation of a propeller TT:9047 NA.no work performed by suspect company CRS blade and loss of control of the ACOR030C airplane Engine TO PREVENT ENGINE POWER REDUCTION DUE TO MALFUNCTION OF THE COMPRESSOR BOV, WHICH COULD RESULT IN A FORCED, CON~TP To prevent failure of the turbine exhaust duct due to cracking that could result in possible separation of.contd. PT6A-52 12/11/2009 CW at build NA by engine min PCE - RX0283 Printed 3/4/201 5 4:41 :09PM Pa e 9of10
Content Revision: 3/2/2015 FAA AD Number Effective bate Pratt & Whitney Canada 97-04-12 3/14/1997 2002-23-13 12/31/2002 Engine Description TO PREVENT ENGINE POWER REDUCTION DUE TO MALFUNCTION OF THE COMPRESSOR BOV, WH ICH COULD RESULT IN A FORCED,CON~TP FAA Airworthiness Directive Com_Q_liance Record File ID: N800TS To prevent failure of the turbine exhaust duct due to cracking that could result in possible separation of.contd. Corri plied. Date Time PT6A-52 12/13/2009 Amendment Numb~r Method of!compliance/applicability CW at build NA by engine min Aircraft Registration: or Next Due Date Time Facility Cert. Nl.Jm., Cert. Type Author. By PCE - RX0284 Printed 3/4/201 5 4:41 :09PM P'!.9_e 10 of 10