N892EA

Part: DE-ICE VALVE — INOPERATIVE (LT WING) · airframe 35,051 hrs · 40,136 cycles

3RD SEGMENT INBOARD LEFT WING BOOT AND LEFT ENGINE INTAKE BOOTS NOT INFLATING. REPLACED L/H WING IB DEICE DISTRIBUTOR VALVE.

Part: SMOKE DETECTOR — FAILED · airframe 49,096 hrs · 54,568 cycles

SMOKE DETECTOR DOES NOT TEST CORRECTLY

Part: VSI — FAILED (NR 1) · airframe 48,764 hrs · 54,268 cycles

#1 IVSI INOP R&R VSI INDICATOR

Part: INDICATOR — FAILED (CABIN PRESSURE) · airframe 48,754 hrs · 54,259 cycles

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

Part: STRINGER — CORRODED (BS 312 S30L) · corrosion level 2 · airframe 48,670 hrs · 54,202 cycles

STRINGER 30P CORRODED UNDER STANDOFF AT BS 312.

Part: PISTON — CORRODED (MLG STRUT) · corrosion level 2 · airframe 48,670 hrs · 54,202 cycles

CORROSION IN BORE OF LOWER TORQUE LINK BRAKE PIN LUG OF MLG STRUT PISTON.

Part: FLAP TRACK — CORRODED (LT WING NR 5)

CORROSION DAMAGE TO LH TRACK #5

Part: NONE — NONE · airframe 47,374 hrs · 52,821 cycles

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.

Part: NONE — NONE · airframe 47,374 hrs · 52,821 cycles

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.

Part: RELAY — FAILED (COCKPIT) · airframe 46,537 hrs · 52,234 cycles

R ELEV HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT (SMELLED HOT ELECTRICAL SMELL IN FLIGHT DECK AND CABIN, STRONGEST IN WARDROBE, NO SMOKE)

Part: COWL DOOR — DAMAGED (LT NACELLE) · airframe 45,578 hrs · 51,453 cycles

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.

Part: TRACK — CHAFED (CARGO DOOR) · airframe 45,578 hrs · 51,453 cycles

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.

Part: SPAR — GOUGED (RUDDER) · airframe 45,578 hrs · 51,453 cycles

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.

Part: SKIN — DENTED (RUDDER TE) · airframe 45,578 hrs · 51,453 cycles

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.

Part: SKIN — NONE (ZONE 100) · airframe 45,578 hrs · 51,453 cycles

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.

Part: SKIN — DENTED (PAX DOOR) · airframe 45,578 hrs · 51,453 cycles

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.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 45,578 hrs · 51,453 cycles

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.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 42,119 hrs · 47,517 cycles

DAMAGE TO LEFT WING SPOILER. FIFTEEN DENTS. REPAIRED IAW RD 8-57-6929, ISSUE 2.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 42,119 hrs · 47,517 cycles

CORROSION ON AFT CARGO DOOR LOWER MAIN SILL, UNDER THE BRACKETS. REMOVED DAMAGE, WITHIN LIMITS SRM 53-00-16. WC 53-280

Part: SEAT TRACK — CORRODED (BS 182-202) · corrosion level 2 · airframe 42,119 hrs · 47,517 cycles

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.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 42,119 hrs · 47,517 cycles

DAMAGE TO THE RT WING OUTBOARD SPOILER. SEVEN DENTS. REPAIRED IAW RD 8-57-8058 WC 57-387.

Part: SEAT TRACK — CORRODED (BS 182-264) · corrosion level 2 · airframe 42,119 hrs · 47,517 cycles

CORROSION FOUND ON THE RT SEAT TRACK. REPLACED THE SEAT TRACK IAW RD 8-53-1102 AND ECO 008.51-17.01.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 42,119 hrs · 47,517 cycles

NICK DAMAGE TO THE RT TRAILING FLAP OUTBOARD SKIN. REPAIRED IAW ECO 008.57-17.05 WC 57-262

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 42,119 hrs · 47,517 cycles

RT CABIN WINDOW FRAME CORRODED ON MATING SURFACE AT FRAME. REPLACED FRAME IAW BOMBARDIER RD 8-53-6323.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 42,119 hrs · 47,517 cycles

CENTER FUSELAGE SKIN DENTS AT X424 AND X434 REPAIRED WITH RIVET PLUG AND RD8-53-7310.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,119 hrs · 47,517 cycles

AFT CARGO SKIN STIFFENER CORRODED. REPLACED WITH NEW PART IAW SRM WC 53-277.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 42,119 hrs · 47,517 cycles

MULTIPLE DENTS ON UPPER FUSELAGE AND FRONT PRESSURE BULKHEAD. REPAIRED IAW ECO 008.53-13.31.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 41,181 hrs · 46,278 cycles

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.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,888 hrs · 45,870 cycles

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.

Part: COLLAR — CRACKED (LT NACELLE) · airframe 40,000 hrs · 44,702 cycles

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.

Part: STRAP — CRACKED (LT NACELLE) · airframe 39,345 hrs · 43,816 cycles

CRACK DAMAGE TO LT NACELLE LANDING STRAP. REPAIRED IAW RD8-54-3821

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,270 hrs · 43,738 cycles

PASSENGER DOOR LIGHT WARNING CAME ON DURING DESCENT. CHECKED CLEARANCE GAPS AND FREEDOM OF SWITCH OPS ALL WITHIN SPECS, FUNCTION CHECKS OK.

Part: STARTER GEN — MALFUNCTIONED (NR 2 ENGINE) · airframe 38,386 hrs · 42,610 cycles

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.

Part: UNKNOWN — BROKEN (HYDRAULIC SYS) · airframe 38,050 hrs · 42,168 cycles

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.

Part: SPOILER — DENTED (LT WING) · airframe 37,468 hrs · 41,430 cycles

DENT DAMAGE BEYOND SRM & GENERIC REPAIR DWG LIMITS OF LT OTBD GND SPOILER.

Part: FIREWALL — CHAFED (ZONE 400) · airframe 37,468 hrs · 41,430 cycles

CHAFE DAMAGE TO FIREWALL PLATE BEYOND SRM LIMITS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,468 hrs · 41,430 cycles

VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF LT INBD SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,468 hrs · 41,430 cycles

VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF RT OTBD SEAT TRACK.

Part: PLATE — DAMAGED (WING) · airframe 37,468 hrs · 41,430 cycles

DAMAGE BEYOND SRM LIMITS TO THE O RING GROOVE FOR THE LT LADDER PLATE ASSEMBLY.

Part: SPOILER — DENTED (LT WING) · airframe 37,468 hrs · 41,430 cycles

DENT DAMAGE BEYOND LIMITS OF SRM & GENERIC REPAIR DWGS LT INBD GND SPOILER.

Part: HINGE FITTING — DAMAGED (RT SPOILER) · airframe 37,468 hrs · 41,430 cycles

ELONGATED ACTUATOR MOUNTING HOLE IN OTBD LUG OF THE RT INBD GND SPOILER INBD HINGE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,468 hrs · 41,430 cycles

VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG OF RT OTBD SEAT TRACK.

Part: DOOR — OUT OF ADJUST (LT MLG) · airframe 37,468 hrs · 41,430 cycles

GAP OF LT MLG AFT DOORS TO NACELLE & EACH OTHER EXCEEDS AMM LIMITS.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,468 hrs · 41,430 cycles

THREE DENTS IN FUSELAGE BELLY BEYOND SRM LIMITS.

Part: YOKE — CHAFED (RT MLG) · airframe 37,468 hrs · 41,430 cycles

0.25 INCH DIAMETER CHAFE DAMAGE TO RT MLG GEAR YOKE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,468 hrs · 41,430 cycles

VARIOUS SPOTS OF CORROSION BEYOND SRM & GENERIC REPAIR DWG LIMITS OF RT INBD AFT SEAT TRACK.