N827AY

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 17,705 hrs · 15,008 cycles

CAPTAIN & FIRST OFFICER'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN & FIRST OFFICER'S LIFE VESTS IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VEST) · airframe 17,197 hrs · 14,483 cycles

ONE INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED ONE INFANT LIFE VEST IAW PA 25-096A.

Part: CONTROL QUADRANT — DEFECTIVE (THROTTLE) · airframe 16,013 hrs · 13,354 cycles

ON LANDING ALL SPLR'S DEPLOYED AS NORMAL, HOWEVER ONE FULL TR THEY SPLR'S ALL RETRACTED AND THE DEPLOYED AGAIN ONCE THE TR WENT TO IDLE. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-00 OPS CHECKS GOOD. AND FUNCTIONAL CHECK OF SPOILER GROUND LIFT DUMP FUNCTION GOOD IAW AMM 27-61-00.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,417 hrs · 11,831 cycles

INTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.75 ON RBL 27, SKIN IS CHAFED APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 14,417 hrs · 11,831 cycles

INTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 94.5 ON LBL 9 HAS BROKEN ISOLATOR NUT PLATE. REPAIRED IAW SRM 51-42-06.

Part: SKIN — DENTED (FUSELAGE) · airframe 14,417 hrs · 11,831 cycles

TWO DENTS WERE FOUND PROTRUDING FROM THE FUSELAGE SKIN FWD OF ESC BAY DOOR AT FS 672 BETWEEN STRINGERS 26L AND 27. REPAIR DENTS IAW SRM 53-00-31 FIG 103 ALLOWABLE DAMAGE AND SRM 51-12-00 PAGE 21 REPAIR OF SMALL HOLES PAGE 22 FIG 7.

Part: RIVET — DAMAGED (FUSELAGE)

INTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN RBL 18 AND RBL 36 HAS TWO DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 14,417 hrs · 11,831 cycles

INTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN LBL 9 AND LBL 36 HAS FOUR DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,417 hrs · 11,831 cycles

INTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 103.5 BETWEEN LBL 27 AND RBL 36, SKIN IS CHAFED AT NINE LOCATIONS APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 12,483 hrs · 10,075 cycles

AT CRUISE ALTITUDE, ENROUTE, THE R REV UNLOCK MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND DETERMINED THAT THE THRUST REVERSER WAS NOT ACTUALLY DEPLOYED. FLIGHT CREW ELECTED TO PERFORM AN AIR RETURN. AN OTHERWISE NORMAL APPROACH AND LANDING WERE MADE. MX INSPECTED THE ACFT, DEFERRED THE RT THRUST REVERSER AND RELEASED THE ACFT FOR SERVICE.

Part: SWITCH — INOPERATIVE (STAB TRIM)

STAB TRIM RUN AWAY. CAPTAIN`S SWITCH NOT FUNCTIONING. MAINTENANCE FOUND NO STAB TRIM RUN AWAY. THE CAPTAIN`S SWITCH WAS NOT CONTROLLING THE TRIM. SWITCH WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (K)

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 4,249 hrs · 3,243 cycles

RECEIVED FLAPS FAIL MESSAGE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,231 hrs · 3,228 cycles

RECEIVED FLAPS FAIL MESSAGE DECLARED EMERGENCY QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,196 hrs · 3,200 cycles

RECEIVED "FLAPS FAIL" MESSAGE ON DESCENT DIVERTED TO COS FOR FLAPS AND BAD WEATHER IN DEN. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21

Part: BPSU — FAILED (TE FLAPS) · airframe 1,097 hrs · 803 cycles

FLAPS FAIL AT ZERO ON CLIMBOUT.

Part: FLAP SYSTEM — FAILED (TE FLAPS)

EMERGENCY DELCARED WHEN FLAPS FAILED AT 20 DEGREES ON APPROACH. LANDING UNEVENTFUL.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 1,009 hrs · 738 cycles

FLAPS FAILED AT 20 DEGEES ON APPROACH. COMPLIED WITH AD98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 1,009 hrs · 738 cycles

FLAPS FAILED AT 20 DEGREES ON APPROACH. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

( REF NR: 05-102) FLAP FAILURE ENROUTE, AT 0. QRH FOLLOWED UNEVENTFUL LANING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

(REF NR: 05-082) FLAP FAIL CAUTION MESSAGE. QRH FOLLOWED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: FCU — FAILED (TE FLAPS)

(REF NR: 05-081) FLAPS FAIL ON CLIMB-OUT. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU). (K)