N889EA

Part: HOSE — LEAKING (ZONE 700) · airframe 59,212 hrs · 71,921 cycles

#2 HYD ISO VLV ILLUMINATED. MANUAL GEAR EXTENSION PERFORMED

Part: NOT REPORTED — NOT REPORTED · corrosion level 3 · airframe 57,910 hrs · 71,506 cycles

FWD PAX DOOR THRESHOLD MEMBER CORRODED AROUND FLOOR BOARD FASTENERS.

Part: NOT REPORTED — NOT REPORTED · corrosion level 3 · airframe 57,910 hrs · 71,506 cycles

PAX DOOR CENTER FUSELAGE CHANNEL FOUND CORRODED BEYOND LIMITS.

Part: SEAT TRACK — CORRODED · airframe 57,910 hrs · 71,506 cycles

FORWARD R/H INBOARD SEAT RAIL HAS CORROSION BEYOND SERVICEABLE LIMIT.

Part: SEAT TRACK — CORRODED · airframe 57,910 hrs · 71,506 cycles

L/H AFT INBOARD SEAT RAIL CORROSION BEYOND SERVICEABLE LIMIT.

Part: SEAT TRACK — CORRODED · airframe 57,910 hrs · 71,506 cycles

R/H AFT SEAT RAIL CORROSION BEYOND SERVICEABLE LIMIT.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 55,546 hrs · 69,419 cycles

GEAR FAILED TO EXTEND. ALTERNATE GEAR EXTENSION USED.

Part: FIREWALL — CRACKED (NACELLE) · airframe 55,065 hrs · 68,971 cycles

DURING ENGINE REMOVAL, A CRACK WAS NOTICED ON FORWARD SIDE OF RIGHT FIREWALL.

Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 54,132 hrs · 68,038 cycles

DENT DAMAGE ON THE AIRSTAIR DOOR OUTER SKIN, LOCATED BETWEEN STA. X222.78 - X237.7 AND ABOVE DOOR STOP #4 OF THE AIRSTAIR DOOR ASSEMBLY P/N 85210003. ENSURE DENT IS WITHIN LIMITS OF RD, INSPECT FOR CRACK AND DISBOND INDICATIONS, AND REFINISH ANY BARE SURFACE WITH CORROSION INHIBITING COMPOUNDS. ALL WORK DONE IAW BOMBARDIER RD 8-52-1633 AND CORVUS ECO 008.52-18.10 DATED OCTOBER 30, 2018.

Part: SKIN — DENTED (BS 312-333) · airframe 54,132 hrs · 68,038 cycles

MULTIPLE DENT DAMAGE TO FUSELAGE SKIN PANELS BETWEEN STA. X312.35 - X333.3 AND STR. 3P - 2S. REMOVED DAMAGE AND ENSURE REMAINING DENT MEETS REQUIREMENT AS STATE IN RD, INSPECT FOR CRACK AND DISBOND INDICATIONS, FABRICATE AND INSTALL AN EXTERNAL REPAIR DOUBLER. RE-PROTECT REPAIR AREA WITH CORROSION INHIBITING COMPOUNDS IAW BOMBARDIER RD 8-53-15946 AND CORVUS ECO 008.53-18.52 DATED NOVEMBER 07, 2018.

Part: ATTACH FITTING — CHAFED (RUDDER) · airframe 54,132 hrs · 68,038 cycles

CHAFE DAMAGE ON THE FORE RUDDER YAW DAMPER ATTACHMENT FITTING. REPAIRED IAW RD 8-55-3254 AND ECO 008.55-18.06.

Part: DOOR FRAME — GOUGED (MLG DOOR) · airframe 54,132 hrs · 68,038 cycles

GOUGE DAMAGE TO MLG DOOR ACTUATOR ARM AND BORE HOLE REPAIRED IAW RD 8-32-4598 AND ECO 008.32.18.02.

Part: SKIN PANEL — DENTED (CARGO DOOR) · airframe 54,132 hrs · 68,038 cycles

MULTIPLE DENT DAMAGE TO THE BAGGAGE DOOR OUTER SKIN BETWEEN STA X564.5 - X580.5 BELOW THE UPPER BEAM. REPAIRED IAW RD 8-52-1630 AND ECO 008-52-18-09.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 54,132 hrs · 68,038 cycles

MULTIPLE DENT DAMAGE TO THE LT FUSELAGE SKIN PANEL BETWEEN STA X270.5 - X291.4 AND STR 8P - 9P. REPAIRED IAW RD 8-53-15931 AND ECO 008.53-18.51.

Part: SMOKE DETECTOR — FALSE INDICATION (NOT REPORTED) · airframe 53,082 hrs · 66,976 cycles

SMOKE CAUTION LIGHT ILLUMINATED AFTER STARTUP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,535 hrs · 66,481 cycles

LOWER EMERGENCY LIGHT AT AIRSTAIR ENTRANCE IS NOT COMING ON WHEN EMERGENCY LIGHT SWITCH IS TURNED ON.

Part: DRAG STRUT — CHAFED (ZONE 700) · airframe 51,064 hrs · 64,365 cycles

CHAFE DAMAGE TO DRAG STRUT FROM FWD DOOR ATTACH HARDWARE. TWO LOCATIONS BEYOND LIMITS OF CMM 32-10-02. REPAIRED IAW ECO 008.32-17-01

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 49,206 hrs · 62,171 cycles

PERMANENT ALLOWANCE FOR BLENDS ON BOTTOM FUSELAGE SKIN PANEL, PN 85320106, BETWEEN FRAME STATION X240 - X253.4, STRINGER 30S & 32S. REPAIRED IAW RD8-53-14633 ISSUE 1.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 49,206 hrs · 62,171 cycles

LIGHTNING STRIKE DAMAGE TO LT WING STRESS PANEL 521AT, ONE COUNTERSINK NOT COVERED BY RD8-57-2674. REPAIRED IAW RD8-57-7379.

Part: FLAP TRACK — DAMAGED (TE FLAP) · airframe 49,206 hrs · 62,171 cycles

DAMAGE TO NR 4 FLAP TRACK INBD AFT FACE LOWER PORTION. BLENDED RD8-57-7380.

Part: COVER — BROKEN (CABIN) · airframe 45,258 hrs · 57,989 cycles

ROW 1 RT EMER EXIT LIGHT COVER BROKEN. R & R ROW 1 EMER EXIT LIGHT ASSEMBLY & OPS CHECKED GOOD. OK FOR SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,677 hrs · 57,273 cycles

RIGHT FUSELAGE AT STATION X 366, BTW STRINGER 30S - 31S, FRAME CORRODED. RT FUSELAGE AT STATION X 366 BTW STRINGER 30S - 31S FRAME REPAIRED IAW SRM 53-20-21.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 44,677 hrs · 57,273 cycles

BETWEEN STATION 547 & 599, CARGO THRESHOLD CORRODED. AT STATION 600 STIFFENER PN 85331150 CORRODED OUT OF LIMIT IAW SRM 53-00-16. STIFFENER PN 85331150 R & R WITH NEW PARTS. INSTALLED WITH SOLID RIVET IAW SRM 51-40-05.

Part: SKIN — DENTED (LT SPOILER) · airframe 44,677 hrs · 57,273 cycles

LEFT WING INBD GND SPOILER UPPER SURFACE DENTED. REPAIRED IAW RD8-57-6413.

Part: DOOR — DAMAGED (RT MLG) · airframe 44,677 hrs · 57,273 cycles

RIGHT MLG AFT OTBD DOOR COMPOSITE DAMAGED. REPAIRED IAW R8-54-3513.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,677 hrs · 57,273 cycles

BAGGAGE DOOR LOWER AFT CUT OUT INBD SKIN CORRODED BETWEEN FS X595.00 & 600.0. REPAIRED IAW RD8-53-13638.

Part: SKIN — DENTED (RT SPOILER) · airframe 44,677 hrs · 57,273 cycles

RIGHT WING OTBD GND SPOILER UPPER SURFACE DENTED. REPAIRED IAW RD8-57-6439.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,677 hrs · 57,273 cycles

MULTIPLE DENTS ON LT FUSELAGE SKIN AROUND ICE SHIELD BETWEEN STATION X270 - X315, STRINGER 3P - 8P. REPAIRED IAW RD8-53-13635.

Part: SKIN — CRACKED (RT NACELLE) · airframe 44,677 hrs · 57,273 cycles

CRACK ON RT NACELLE OTBD SKIN AT TOP CORNER OF COWLING PANEL 426AR CUT OUT. REPAIRED IAW RD8-54-3511.

Part: SKIN — DENTED (BS 331) · airframe 44,677 hrs · 57,273 cycles

TWO DENTS ON LT FUSELAGE SKIN AT BS 331, BETWEEN STRINGER 14P-16P. REPAIRED IAW RD8-53-13623.

Part: RIVET — LOOSE (RT MLG DOOR) · airframe 44,677 hrs · 57,273 cycles

DURING C CHECK FOUND RT MLG DOOR FWD HINGE ATTACHMENT BRACKET RIVETS LOOSE REQUIRING REPAIR IAW DWG.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 44,677 hrs · 57,273 cycles

DURING C CHECK FOUND LT WING FUEL PANEL 524AT, TWO HOLES CORRODED, REPAIRED IAW DWG.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 44,677 hrs · 57,273 cycles

DURING C CHECK FOUND RT WING FUEL PANEL 624CT, TWO HOLES CORRODED REPAIRED IAW DWG.

Part: CONTROL BOX — DEFECTIVE (EMERGENCY LIGHTS) · airframe 44,503 hrs · 57,104 cycles

EMERGENCY LIGHTS FLICKERING INTERMITTENTLY. REPLACED EMERGENCY LIGHT CONTROL BOX & GND TEST GOOD IAW -8 MM 33-51-02.

Part: CONTROL BOX — DEFECTIVE (CABIN) · airframe 44,498 hrs · 57,100 cycles

EMERGENCY LIGHTS FLICKER INTERMITTENTLY. R & R FLIGHT ATTENDANT CONTROL BOX, TESTS GOOD IAW -8 MM 22-10-00.

Part: FUEL LINE — LOOSE (NR 2 ENGINE) · airframe 42,020 hrs · 54,525 cycles

FUEL LEAK OBSERVED ON NR 2 FORWARD NACELLE. SECURED LINE AT FUEL FLOW TRANSMITTER IAW AMM 73-32-00 AND 20-06-18 LOW POWER AND HIGH POWER LEAK CHECK GOOD. OK FOR SERVICE.

Part: TUBE — LEAKING (HYDRAULIC SYS) · airframe 41,976 hrs · 54,482 cycles

NR 2 HYDRAULIC FLUID 1.5 QUARTS. REPLACED TUBE ASSY P/N 82950010-219 WITH NEW IAW Q100 MM 20-06-03, BLED LINE, OPS CHECKED NORMAL, OK FOR SERVICE, SERVICED NR 2 HYDRAULIC FLUID.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,748 hrs · 53,271 cycles

CRACK AND DELAMINATION ON CAPTAINS WINDSCREEN. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW DASH 8 MM 56-10-11.

Part: SWITCH — INTERMITTENT (CABIN) · airframe 40,071 hrs · 52,433 cycles

EMERGENCY LIGHTS FLASHING ON AND OFF IN THE CABIN. REMOVED AND REPLACED THE EMERGENCY LIGHTS GALLEY SWITCH AND OPS CHECKED GOOD.

Part: SIGNAL COND UNIT — DEFECTIVE (NR 2 ENGINE) · airframe 40,066 hrs · 52,429 cycles

DURING TAKEOFF AT 0739 TORQUE GAUGE INACCURATE. REMOVED AND REPLACED NR 2 ENGINE TSCU PW121 MM CHAPTER 72 OPS CHECKED GOOD AT ENGINE RUN IAW PSM 8-2-ER MIN CHECKOUT TABLE. OK FOR SERVICE.

Part: SWITCH — DIRTY (CONTROL PANEL) · airframe 39,984 hrs · 52,343 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE AT FLIGHT ATTENDANTS CONTROL PANEL UNLESS EMERGENCY LIGHTS ARE ARMED IN COCKPIT. CLEANED CONTACTS OF EMERGENCY LIGHTS CONTROL SWITCH S2 AT F/A PANEL, OPS CHECKED GOOD.

Part: CONTROL BOX — FAILED (CABIN) · airframe 39,874 hrs · 52,233 cycles

CABIN EMERGENCY LIGHTS FLASHING INTERMITTENTLY

Part: SKIN — CANNING (FUSELAGE) · airframe 39,846 hrs · 52,197 cycles

APPLIED PERMANENT REPAIR FOR OIL CANNING DAMAGE ON LT FUSELAGE SKIN PANEL 85310045 BETWEEN FRAME STATIONS X=97 TO FUSELAGE PRODUCTION BREAK (X=110) AND BETWEEN STIFFENERS 12P TO 15P IAW BOMBARDIER REPAIR DRAWING 8-53-12210.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,846 hrs · 52,197 cycles

RT SEAT TRACK CORRODED OUT OF LIMITS AT FS 215. SPLICED IN NEW SECTION OF SEAT TRACK FROM X=182 TO X=264 AT Y=9RT AS REQUIRED IAW BOMBARDIER REPAIR DRAWING 8-53-3074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,846 hrs · 52,197 cycles

OUTBOARD SIDE OF SEAT RAIL AT Y=9LH IS CORRODED FROM X=201 TO 222. SPLICED IN NEW SECTION OF SEAT RAIL FROM X=182 TO X=231 AT Y=9LT AS REQUIRED IAW BOMBARDIER REPAIR DRAWING 8-53-3074. W/O 50307, W/C 1118.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,846 hrs · 52,197 cycles

PASSENGER DOOR THRESHOLD CORRODED OUT OF LIMITS. REPLACED THRESHOLD MEMBER IAW DASH 8 SRM 51-40-07, 51-40-11, 51-42-05, AND DHC DRAWING 85320686. W/O 50307, W/C 2308

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,846 hrs · 52,197 cycles

CORROSION ON ANGLE AT X=600 AND Y=9L. MATCH DRILLED STIFFENER TO AIRCRAFT AND INSTALLED IAW DHC-8 100 SRM 51-40-07, 51-30-26, 51-40-10 AND 51-40-11. W/O 50307, W/C 1132.

Part: LEVER — CRACKED (LT SPOILER) · airframe 39,846 hrs · 52,197 cycles

LT OUTBOARD GROUND SPOILER LEVER ASSEMBLY CRACKED AT ACTUATOR LINK BEARING. REMOVED AND REPLACED LT OUTBOARD GROUND SPOILER LEVER ASSEMBLY IAW DHC-8 100 AMM 27-60-00. W/O 50307, W/C 5100.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 39,846 hrs · 52,197 cycles

CORROSION ON PASSENGER DOOR THRESHOLD TOP AND BOTTOM SIDE. REMOVED LIGHT CORROSION FROM BOTTOM SIDE OF PASSENGER DOOR THRESHOLD AT NUT PLATE LOCATIONS, IS WITHIN ALLOWABLE LIMITS, ALODINED AND PRIMED AREAS. TOP THRESHOLD MEMBER IS CORRODED OUT OF LIMITS, SEE WORK CARD 2308 FOR WORK ACCOMPLISHED. W/O 50307, W/C 2301.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 39,846 hrs · 52,197 cycles

CARGO DOOR AFT FRAME, COUNTERBALANCE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED CARGO DOOR AFT FRAME COUNTERBALANCE SUPPORT BRACKET IAW BOMBARDIER PPS 2.20. W/O 50307, W/C 8085

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 39,846 hrs · 52,197 cycles

CRACK EMANATING FROM RIVET HOLE ON BOTTOM SKIN OF LT ELEVATOR ON RIB 13 AT XH 10.5 FWD OF 0XH CENTER LINE. REMOVED CRACK AND REPAIRED BOTTOM SKIN OF LT ELEVATOR ON RIB 13 (YH = 139.5) AT XH 10.5 FWD OF 0XH CENTER LINE IAW DHC-8 100 SRM 51-10-21 AND BOMBARDIER RD 8-55-2406, W/O 50307, W/C 3067.

Part: TRU — INTERMITTENT (NR 2) · airframe 39,666 hrs · 51,996 cycles

EMERGENCY LIGHTS FLICKERING ON AND OFF DURING FLIGHT, OVERHEAD LIGHTS AT ROW 8&9 RIGHT SIDE ALSO FLICKERING. REMOVED AND REPLACED NR 2 TRU IAW DASH 8 MM 24-31-00 AND OPS CHECKS OK.

Part: TRANSPONDER — MALFUNCTIONED (COCKPIT) · airframe 39,293 hrs · 51,554 cycles

ACRID SMELL IN COCKPIT. REMOVED AND REPLACED NR 2 TRANSPONDER CONTROL AND OP CHECKS GOOD. FOUND DISPLAY INOP AND SMELLS BURNT.

Part: SEAT BACK — LOOSE (CABIN) · airframe 37,543 hrs · 49,474 cycles

DURING TRAINING, FLIGHT ATTENDANT FOUND THAT EMERGENCY EXIT DOOR WAS BLOCKED BY TOP OF ROW 3 SEAT. MAINTENANCE INSPECTED AND FOUND SEAT PITCH CORRECT AND THAT TIGHTENING OF SEAT FRAME AND SEAT BACK HARDWARE GAVE CORRECT CLEARANCE FOR EXIT OPENING. OPERATIONAL CHECK OF CENTER CABIN EMERGENCY EXITS SATISFACTORY.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 35,058 hrs · 46,559 cycles

(V0XR) PASSENGER DOOR SILL THRESHOLD IS CORRODED BEYOND LIMITS. R & R THRESHOLD. W/C 8031

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 35,058 hrs · 46,559 cycles

(V0XR) LT FLOOR TRACK AT STA 589.5. CORRODED BEYOND LIMITS. R & R FLOOR TRACK. W/C 1086

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 35,058 hrs · 46,559 cycles

(V0XR) LT FLOOR TRACK AT STA 589.5. IS CORRODED BEYOND LIMITS. R & R FLOOR TRACK. W/C 1086

Part: SHEAR WEB — CORRODED (CARGO BAY) · airframe 35,056 hrs · 46,559 cycles

FLOOR UNDER PANEL 144AZ BAGGAGE COMPARTMENT HAS CORROSION. INSTALLED REPAIR DOUBLERS IAW BOMBARDIER RD8-53-11254.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 35,056 hrs · 46,559 cycles

UPPER FRAME OF BAGGAGE DOOR HAS TWO GOUGES, EVALUATED DAMAGE TO BE WITHIN LIMITS IAW BOMBARDIER RD8-53-11257, W/C 2260, W/O 50150.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 35,010 hrs · 46,502 cycles

HYD FAILURE DURING TAKEOFF. FLUID LEAKING ON NR 2 SIDE FAILURE IN NR 1 SYSTEM. REMOVED RIGHT I/B SPOILER ACTUATOR THAT IS LEAKING.