N892EA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AUX BATT HOT WARNING LIGHT CAME ON MOMENTARILY TWICE ON INITIAL CLIMB OUT. WE FOLLOWED FLIGHT OPS READ FILE NO. 2504. TURNED AUX BATT SWITCH OFF.
CAPTS FMS SCREEN WENT BLANK. UNRESPONSIVE TO ANY INPUT.
LOUD SQUEAL COMING FROM THE CARGO DOOR. VERIFIED BY F/A.
LEFT MAIN GEAR DOOR HANGING DOWN 1 INCH IN CRUISE FLIGHT. F/A SAID THE DOOR CAME COMPLETELY UP DURING DESCENT.
3RD SEGMENT INBOARD LEFT WING BOOT AND LEFT ENGINE INTAKE BOOTS NOT INFLATING. REPLACED L/H WING IB DEICE DISTRIBUTOR VALVE.
SMOKE DETECTOR DOES NOT TEST CORRECTLY
#1 IVSI INOP R&R VSI INDICATOR
AT 24,000 FT PRESSURIZATION PANEL INDICATED RANDOM VARIABLES ON DIFF, ALT, AND RATE. LEVEL AT 10000 RATE DIAL VIBRATING RAPIDLY REPLACED CABIN PRESSURE INDICATOR PANEL
CORROSION IN BORE OF LOWER TORQUE LINK BRAKE PIN LUG OF MLG STRUT PISTON.
STRINGER 30P CORRODED UNDER STANDOFF AT BS 312.
CORROSION DAMAGE TO LH TRACK #5
REPAIR FOR SCRATCH AND MULTIPLE DENT DAMAGE TO EMPENNAGE RH SIDE PANEL ASSEMBLY 85530007. REPAIRED IAW DEHAVILLAND RD8-55-3683 AND ECO 008.55-21.07.
REPAIR FOR SCRATCH AND MULTIPLE DENT DAMAGE TO EMPENNAGE RH SIDE PANEL ASSEMBLY 85530007. REPAIRED IAW DEHAVILLAND RD8-55-3683 AND ECO 008.55-21.07.
R ELEV HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT (SMELLED HOT ELECTRICAL SMELL IN FLIGHT DECK AND CABIN, STRONGEST IN WARDROBE, NO SMOKE)
DAMAGE LOWER COWL LHS EDGE MEMBER (P/N 87140380) BETWEEN XN 55.00 AND XN 60.00. PERMENANT REPAIR FOR DAMAGE LOWER COWL CONSISTS OF HAD DRESSING THE DAMAGED AREA BACK TO ORIGINAL CONTOUR, INSPECTING THE REWORK AREA FOR CRACK INDICATIONS(NONE PERMITTED), AND RE-PROTECTING THE REPAIRR AREA BY APPLYING CORROSION INHIBITING COMPOUNDS AS REQUIRED IAW DEHAVILLAND OF CANADA LIMITED RD 8-71-1356 ISSUE 1 DATED 25NOV 2019.
CHAFE DAMAGE TO BAGGAGE DOOR FWD AND AFT TRACKS. A PERMANENT REPAIR WILL BE ACCOMPLISHED FOR CHAFE DAMAGE TO BAGGAGE DOOR FWD AND AFT TRACKS IAW DEHAVILLAND AIRCAFT OF CANADA LIMITED RD 8-52-1688 ISSUE 1 DATED 08 NOVEMBER 2019.
GOUGE DAMAGE TOO FORE RUDDER, FRONT SPAR ON R/H SIDE AT RIB# 25. THE PERMANENT REPAIR FOR GOUGE DAMAGE TO FORE RUDDER, FRONT SPAR ON THE R/H SIDE AT RIB#25 WILL BE ACCOMPLISHED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-55-3406 ISSUE 1 DATED 08 NOVEMBER 2019.
MULTIPLE DENT DAMAGE TO TRAILING RUDDER, R/H SIDE LOWER SKIN BETWEEN RIBS #2 AND #3, BETWEEN THE FRONT AND REAR SPARS. PERMANENT REPAIR FOR THE MULTIPLE DENT DAMAGE TO TRAILING, ON ASSEMBLY P/N 85540002-001 AND R/H SIDE SKIN P/N 85545031-103, BETWEEN RIBS #2 AND #3 AND BETWEEEN THE FRONT AND REAR SPARS WILL BE ACCOMPLISHED IAW RD-55-3404 ISSUE 1 DATED 29 OCTOBER 2019.
CREASE AND MULTIPLE DENT DAMAGE TO PASSENGER DOOR OUTER SKIN ASSEMBLY BETWEEN X220.78 - X252.62 ABOVE STOP #3. THE PERMANENT REPAIR FOR CREASE AND MULITPLE DENT DAMAGE TO PASSENGER DOOR OUTER SKIN ASSEMBLY WILL BE ACCOMPLISHED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-52-1686 ISSUE 1 DATE 19 OCTOBER 2019.
THE REMOVAL OF AN EXISTING STC VHF ANTENNA INSTALLATION ON BOTTOM FUSELAGE SKIN PANEL ASSEMBLY, LOCATED BETWEEN X291.40 - X312.35 AND BETWEEN STRINGERS 30P - 31P. PERMANENT REPAIR FOR THE REMOVED STC VHF ANTENNA IS INSTALLING A EXTERNAL DOUBLER WHICH WILL BE ACCOMPLISHED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-53-16413 ISSUE 1 DATED 22 OCTOBER 2019.
CRACK DAMAGE OF L/H NACELLE ACCESS PANEL LANDING STRIP, P/N 85410182, AT XN 64.0 AND YN 8.48. THE PERMANENT REPAIR FOR CRACK DAMAGE TO L/H NACELLE ACCESS PANEL LANDING STRIP WILL ACCOMPLISHGED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-54-4224 ISSUE 1 DATED 18 OCTOBER 2019.
CORROSION ON AFT CARGO DOOR LOWER MAIN SILL, UNDER THE BRACKETS. REMOVED DAMAGE, WITHIN LIMITS SRM 53-00-16. WC 53-280
DAMAGE TO LEFT WING SPOILER. FIFTEEN DENTS. REPAIRED IAW RD 8-57-6929, ISSUE 2.
CORROSION DAMAGE FOUND OUT OF LIMITS ON THE LT FWD INBD SEAT TRACK. REPLACED THE SEAT TRACK SECTION IAW RD 8-53--1102 AND ECO 008.51-17.01.
CORROSION FOUND ON THE RT SEAT TRACK. REPLACED THE SEAT TRACK IAW RD 8-53-1102 AND ECO 008.51-17.01.
DAMAGE TO THE RT WING OUTBOARD SPOILER. SEVEN DENTS. REPAIRED IAW RD 8-57-8058 WC 57-387.
NICK DAMAGE TO THE RT TRAILING FLAP OUTBOARD SKIN. REPAIRED IAW ECO 008.57-17.05 WC 57-262
AFT CARGO SKIN STIFFENER CORRODED. REPLACED WITH NEW PART IAW SRM WC 53-277.
MULTIPLE DENTS ON UPPER FUSELAGE AND FRONT PRESSURE BULKHEAD. REPAIRED IAW ECO 008.53-13.31.
CENTER FUSELAGE SKIN DENTS AT X424 AND X434 REPAIRED WITH RIVET PLUG AND RD8-53-7310.
RT CABIN WINDOW FRAME CORRODED ON MATING SURFACE AT FRAME. REPLACED FRAME IAW BOMBARDIER RD 8-53-6323.
FORWARD & MIDDLE OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY IN POWER SUPPLY 3351-PS2 & OPS CHECKED GOOD IAW MM 33-52-00. OK FOR SERVICE.
FWD LEFT OUTSIDE EGRESS AND LEFT LOWER EXIT EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED THE BATTERY PACK . OPS CHECKED NORMAL IAW MM 33-51-00.
CRACK ON THE LT NACELLE HORSECOLLAR 85410146. CUT OUT DAMAGED SECTION. NDT CHECK OK ON REMAINING ANGLE. APPLIED PACKER AND PATCH IAW RD 8-54-1736 AND ECO 008.54-16.06.
CRACK DAMAGE TO LT NACELLE LANDING STRAP. REPAIRED IAW RD8-54-3821
PASSENGER DOOR LIGHT WARNING CAME ON DURING DESCENT. CHECKED CLEARANCE GAPS AND FREEDOM OF SWITCH OPS ALL WITHIN SPECS, FUNCTION CHECKS OK.
NORMAL NR 2 ENG START, EXTERNAL POWER, BATTERY OBSERVED WITH INCREASING TEMP & NR 2 GCU OFFLINE. ENG SHUTDOWN DUE TO HOT BATTERY. SPARKS OBSERVED OUT OF NR 2 COWLING, ACFT EVACUATED. R & R NR 2 STARTER GENERATOR. OPERATIONS CHECKED GOOD.
GEAR FAILED TO EXTEND NORMALLY. ACCOMPLISHED BY, NR 2 HYD ISO VLV, CAUTION LIGHT & ROLL SPLR OTBD HYD, ILLUMINATED ONCE ON GND. SPOILER LIGHT, GND, WAS ALSO ILLUMINATED IN FLIGHT & ON GND.
CHAFE DAMAGE TO FIREWALL PLATE BEYOND SRM LIMITS.
VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF RT INBD AFT SEAT TRACK.
VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF RT OTBD SEAT TRACK.
VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG OF RT OTBD SEAT TRACK.
THREE DENTS IN FUSELAGE BELLY BEYOND SRM LIMITS.
0.25 INCH DIAMETER CHAFE DAMAGE TO RT MLG GEAR YOKE.
VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF LT INBD SEAT TRACK.
DAMAGE BEYOND SRM LIMITS TO THE O RING GROOVE FOR THE LT LADDER PLATE ASSEMBLY.
ELONGATED ACTUATOR MOUNTING HOLE IN OTBD LUG OF THE RT INBD GND SPOILER INBD HINGE.
GAP OF LT MLG AFT DOORS TO NACELLE & EACH OTHER EXCEEDS AMM LIMITS.
DENT DAMAGE BEYOND SRM & GENERIC REPAIR DWG LIMITS OF LT OTBD GND SPOILER.
DENT DAMAGE BEYOND LIMITS OF SRM & GENERIC REPAIR DWGS LT INBD GND SPOILER.