Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR T17A2020030521004Closeout Panel · crackedR/H UPPER INBOARD PYLON PANEL IS CRACKING AT REAR ATTACH POINTSDR T17A2020030521003Skin · crackedR/H UPPER TR DOOR SKIN CRACKEDSDR T17A2020030521002Skin · crackedL/H UPPER TR DOOR SKIN CRACKEDSDR T17A2020031821004Closeout Panel · crackedDURING SCHEDULED INSPECTION MX FOUND A CRACK ON THE RH INBOARD UPPER PYLON PANEL AT THE REAR ATTACH POINT. MX PERFORMED A REPAIR TO THE PANEL IAW BEECHJET 400XP SRM 51-10-00 AND 51-50-10SDR T17A2020031821003Thrust Reverser · crackedDURING SCHEDULED INSPECTION MX FOUND THE LH UPPER THRUST REVERSER DOOR SKIN CRACKED. MX REMOVED AND THEN INSTALLED A SERVICEABLE LH UPPER TR BUCKET.SDR T17A2020031821002Thrust Reverser · crackedDURING SCHEDULED INSPECTION MX FOUND THE RH UPPER THRUST REVERSER DOOR SKIN CRACKED. MX REMOVED THE RH UPPER THRUST REVERSER BUCKET AND REPLACED IT WITH A SERVICEABLE BUCKETSDR T17A2020031821007Beam · crackedDURING SCHEDULED INSPECTION MX FOUND A CRACK ON THE FWD BEAM THE RH MAIN LANDING GEAR DOOR. MX REMOVED AND REPLACED THE RIGHT INBOARD GEAR DOOR FORWARD BEAM WITH A NEW BEAM. INSTALLED NEW JO BOLTS, AND REINSTALLED IAW SRMSDR T17A2020031721006Bracket · cracked2 EA DOORLAND REINFORCMENT BRACKETS ON THE MAIN ENTRY DOOR FOUND CRACKED DURING VISUAL INSPECTION, MX REPLACED THE BRACKETS WITH NEWSDR T17A201710314027Skin · scratchedAREA ABOVE MAIN ENTRY DOOR STEP PADS HAS SEVERAL SCRATCHES. FUSELAGE SKIN BELOW MED, PERFORMED NDT, REPAIR, PAINT, AND SEALED IAW FIELD REPAIR DRAWING FR-RK-535-3409, REV 1, DATED 10-13-17.SDR T17A201710314026Rib · crackedCRACKS FOUND IN DOUBLERS IN HORIZONTAL STABILIZER REAR SPAR WHILE COMPLETING SB 55-4162. REPLACED RIBS ON H-STAB IAW AIR SERVICES DRAWING NR CAS-128-6200 REV B, STEPS 5-16 RECOMMENDED FOR APPROVAL ON FAA FORM 8110-3 DATED OCTOBER 12, 2017 & APPROVED BY AMOC LSDR T17A201311074003Landing Gear · malfunctionedDURING DESCENT AT FL330, UNCOMMANDED NOSE GEAR EXTENSION. AIRSPEED AT THE TIME OF EXTENSION WAS + 280 KTS AND TOTAL TIME ABOVE 200KTS APPROX 5-10 MINUTES. MAINTENANCE VISUALLY INSPECTED ALL NOSE GEAR COMPNENTS WITH NO DEFECTS NOTED. JACKED AIRPLANE AND PERFSDR E81RJT227916BTire · wrong part(E81R) DURING REPLACEMENT OF WORN NOSE WHEEL TIRE, NOTED PN OF INSTALLED NOSEWHEEL TIRE INCORRECT IAW THE ACFT MFG IPC (32-40-05-01). IAW MFG TIRE APPLICATION DATA, THE REMOVED PN TIRE WOULD BE INSTALLED ON ANOTHER ACFT. HAVE NOTED THIS INCORRECT TIRE PN INSTASDR E81RJT227916AWheel Half · corroded(E81R) DURING DISASSEMBLY OF NOSEWHEEL FOR TIRE REPLACEMENT NOTED CORROSION PITTING IN BOLT HOLES. PITTING WAS DEEPER THAN FIELD REPAIRABLE SERVICE LIMITS. THIS IS THE SECOND NOSEWHEEL ASSY FROM A RELATIVELY NEW ACFT REJECTED IN LAST 30 DAYS DUE TO EXCESSIV