N8710A

Part: PBE — UNSERVICEABLE (CABIN) · airframe 24,290 hrs · 21,736 cycles

GALLEY PBE HAS LOST ITS FIRMNESS. REPLACED GALLEY PBE AS REQUIRED.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 23,923 hrs · 21,363 cycles

FLAPS HALF SPEED MESSAGE AFTER SELECTING FLAPS 45. RESET FLAPS, OPS CHECKED GOOD IAW AMM 27-54-00. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,193 hrs · 20,656 cycles

L EMERGENCY DOOR MESSAGE IN FLIGHT. PRESSURE REMAINED NORMAL AND MESSAGE DISAPPEARED AFTER LANDING. MESSAGE OCCURRED ABOUT 10,000 FEET. PERFORMED FUNCTIONAL TEST OF EMERGENCY DOOR ON LEFT SIDE IAW AMM 52-21-00-720-001. NO DEFECTS NOTED. OK FOR SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 22,933 hrs · 20,404 cycles

CRACKED EMERGENCY FLOODLIGHT BY PASSENGER DOOR. REMOVED AND REPLACED EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPERATIONS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 22,714 hrs · 20,202 cycles

ON FLIGHT 3648 (CVG TO ORD) FLAPS FAIL ON APPROACH WHEN SELECTED TO 20. AIRCRAFT LANDED SAFELY AND PROCEEDED TO THE GATE. REMOVED AND REPLACED ALL FLAP ACTUATORS FOR THE INBD AND OTBD FLAPS, LEFT WING IAW CRJ AMM 27-53-01 REFER TO AML 2156655-1-2. INSPECTED CLEANED AND LUBED THE LEFT WING FLAP FLEX DRIVE SYSTEM IAW CRJ AMM 27-53-10 REFER TO AML 2156653-1. REMOVED AND REPLACED THE SKEW DETECTION UNIT IAW CRJ AMM 27-15 REFER TO 215 6656-1 TROUBLESHOOTING AND MAINT. PERFORMED PER MOTORGROUP DMI CLEARED AND PLACARD REMOVED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,412 hrs · 19,909 cycles

FIRST OFFICERS LIFE VEST BAG TORN. REMOVED AND REPLACED FIRST OFFICERS LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,368 hrs · 19,867 cycles

TWO INFANT LIFE VESTS HAVE HOLES IN BAGS. REMOVED AND REPLACED TWO INFANT LIFE VESTS IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,368 hrs · 19,867 cycles

FIRST OFFICER'S LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

LEFT AISLE NR 5 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: HINGE — WORN (PAX DOOR) · airframe 22,253 hrs · 19,754 cycles

PAX DOOR HINGE WORN. REMOVED AND REPLACED IAW SRM 53-21-23.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 22,253 hrs · 19,754 cycles

LEFT HORIZONTAL STABILIZER TIP NUT PLATE LANDING DAMAGED. REPAIRED IAW BOMBARDIER REO 601R-55-11-434.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 6 RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 3 LEFT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 2 RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 3 RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 7 LEFT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

RIGHT AISLE NR 4 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 22,253 hrs · 19,754 cycles

LEFT FS 559 OUTBOARD PANEL LANDING CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 6 LEFT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 7 RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 5 RIGHT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

LEFT AISLE NR 4 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

RIGHT FS 559 OUTBOARD PANEL LANDING CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,253 hrs · 19,754 cycles

NR 2 LEFT SIDE SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,253 hrs · 19,754 cycles

FUSELAGE IS DENTED AT RIGHT FS 703. REPAIRED IAW SRM 53-00-31.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,253 hrs · 19,754 cycles

REAR PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: CONTAINER — TORN (LIFE VEST) · airframe 21,673 hrs · 19,195 cycles

CAPTAIN LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN LIFE VEST IAM AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,655 hrs · 19,177 cycles

OVERHEAD EMERGENCY EXIT CEILING FLOODLIGHT INOPERATIVE. REPLACED OVERHEAD EMERGENCY FLOODLIGHT PER AMM 33-50-00.

Part: SHIELD — CRACKED (APU) · airframe 21,428 hrs · 18,955 cycles

APU EXHUAST DUCT SHIELD CRACKED. STOP DRILLED CRACK IAW REO 601R-49-81-007.

Part: SCHRADER VALVE — LEAKING (NLG) · airframe 21,359 hrs · 18,891 cycles

NOSE GEAR DISAGREE. PLACARD INSTALLED. DEFERRED GEAR EXT/ RETRACTION SYS, REPLACED SCHRADER VALVE ON NLG, FOUND TO BE LEAKING, PERFORMED GEAR SWINGS ALL CHECKS GOOD.

Part: LOUVER — LOOSE (RAM AIR DUCT) · airframe 21,326 hrs · 18,855 cycles

LT AND RT RAM AIR EXH DUCTS HAVE LOOSER LOUVERS. REPAIRED LT AND RT RAM AIR EXHUAST DUCTS LOUVERS IAW REO 601R-21-52-003.

Part: PBE — FAILED (CABIN) · airframe 20,621 hrs · 18,224 cycles

FORWARD CABIN PBE FAILS PRE-FLIGHT TEST. REPLACED PBE. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,062 hrs · 16,702 cycles

FS 559 SEMI-PRESSURE BULKHEAD FOUND CRACKED AT LBL 18 AND 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REOS 601R-53-41-260 REV "E", 601R-53-41-609 REV "B", AND BOMBARDIER SERVICE CORP EO 601R-53-20801.

Part: RECEPTACLE — CRACKED (EXTERNAL POWER) · airframe 18,018 hrs · 15,713 cycles

CRACK FOUND IN EXTERNAL POWER RECEPTACLE BASE 0.25 INCH LONG, UPPER FORWARD CORNER, AT FS 194.0, STR 18R-23R. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-165, DRILL STOP CRACK PER SRM 51-12-00, PARAGRAPH 11, REPEAT EDDY CURRENT INSPECTIONS EVERY A CHECK FLY ON TO NEXT C CHECK. PERMANENT REPAIR REMOVE AND REPLACE RECEPTACLE BASE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,247 hrs · 14,064 cycles

FWD PRESSURE BULKHEAD (FS 202.75) CRACKED AT PARKING BRAKE CUTOUT. REPAIRED PRESSURE BULKHEAD (FS 202.75) IAW GREO 601R-53-11-563.

Part: FLAP SYSTEM — UNKNOWN

FLAP FAIL AT ZERO DEGREES, SECOND OCCURRENCE WITHIN 72 HOURS.

Part: G SWITCH — FAILED (ELT)

ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.