N8560F

Part: SMOKE GOGGLES — FAILED (COCKPIT) · airframe 26,122 hrs · 22,867 cycles

JUMP SEAT SMOKE GOGGLES ELASTIC BAND HAS NO ELASTIC LEFT AND IS FULLY STRETCHED. WON`T FIT EVEN IN TIGHTEST POSTION. REPLACED JUMP SEAT'S SMOKE GOGGLES IAW AMM 25-61-00.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 25,512 hrs · 22,271 cycles

FLIGHT ATTENDANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.

Part: CONNECTOR — LOOSE (NLG STEERING) · airframe 25,410 hrs · 22,167 cycles

ON FLIGHT 4043 (YYZ TO JFK) AFTER TAKEOFF "STEERING INOPERABLE" CAUTION MESSAGE FOLLOWED BY "WOW INPUT" CAUTION. NOSE WHEEL STEERING WOULD NOT RE-ENGAGE WITH QRH. MESSAGES PERSISTED EN ROUTE UNTIL GEAR WAS LOWERED ON APROACH INTO JFK. AFTER LANDING, NOSE WHEEL STEERING WAS ARMED SUCCESSFULLY AND A NORMAL TAXI TO GATE. FOUND LOOSE CONNECTIONS ALONG THE STEERING HARNESS ASSEMBLY (LT SIDE) & WOW NR 1 HARNESS ASSEMBLY. SECURED ALL CONNECTORS & SAFETY WIRED IAW AMM 32-61-25. OPERATIONAL TEST OF THE NOSEWHEEL STEERING SYSTEM & PROXIMITY SENSOR SYSTEM GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 25,373 hrs · 22,132 cycles

STRUCTURAL DAMAGE SUSTAINED DURING GEAR SWING AT RIGHT MAIN LANDING GEAR UPLOCK WITH DOOR UNATTACHED. REPAIRED IAW REO 601R-53-41-1669.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 25,313 hrs · 22,132 cycles

STRUCTURAL DAMAGE SUSTAINED DURING GEAR SWING AT LEFT MAIN LANDING GEAR UPLOCK WITH DOOR UNATTACHED. REPAIRED IAW REO 601R-53-41-1668.

Part: UNKNOWN — MALFUNCTIONED (CABNI PRESSURE) · airframe 25,010 hrs · 21,779 cycles

PERFORMED AN AIR RETURN TO JFK ON FLIGHT 4105 FOR CABIN ALTITUDE WARNING MESSAGE AFTER TAKEOFF DUE TO DEPRESSURIZATION AND MASKS DEPLOYING. REMOVED AND REPLACED THE 25 OXYGEN GENERATORS, OXYGEN MASK WERE STOWED, ALL CHECKS GOOD. COMPLIED WITH SERVICE CHECK ON AML 2372186 DATE 11/17/2012. COMPLETED TASK 35-23-13-03 DISCARD OXYGEN GENERATORS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,914 hrs · 21,688 cycles

CHECK FOUND EXIT EMERGENCY LIGHT DSLF INOPERABLE. REPLACED CHARGER ASSEMBLY PS2LF IAW CRJ-200 AMM 33-51-05. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,539 hrs · 21,306 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. OPEN

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 24,539 hrs · 21,306 cycles

ON FLIGHT 3952, THE CREW PERFORMED A RIGHT ENGINE SHUTDOWN DUE TO LOW ENGINE OIL PRESSURE (5PSI) AFTER TAKEOFF FROM FNT. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE IAW AMM 71-00-00 AND CHECKLIST PROVIDED. ALL REQUIRED ENGINE OP CHECKS AND LEAK CHECKS SATISFACTORY. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,539 hrs · 21,306 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,071 hrs · 20,839 cycles

FWD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 23,992 hrs · 20,762 cycles

FLIGHT ATTENDANT REPORTED CABIN HOT AND THEN SMOKE ODOR, CREW HAD NO WARNINGS, ECS PAGE SHOWED RIGHT PACK DUCT TEMP REACHED 59 DEG C, TURN OFF. SWAPPED COMPRESSOR INLET DUCT FROM LEFT SIDE PER MOD IAW AMM 21-51-10. OPS CHECK LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,927 hrs · 20,702 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED FORWARD OVERHEAD EMERGENCY LIGHT IAW AMM 33-50-00.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 23,892 hrs · 20,667 cycles

SPLIT FLAP CONDITION. SELECTED FLAPS 8: LT FLAP DEPLOYED TO 8 DEG, RT FLAP DEPLOYED TO 2 DEG. RT FLAP POSITION SENSOR RIG CHECKS GOOD. BEGINNING OF THE NIGHT THE RT FLAP WAS 6 DEGREES HIGHER ON EACH FLAP DETENT. BEFORE DEFERRING FLAP POSITION SENSOR IT WAS ABOUT 15 DEGREES OFF AND FLAPS WEREN’T SKEWED OR TWISTED, JUST AN INDICATION PROBLEM. NEEDS NEW SENSOR PN: 601R93030-3. REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER IAW AMM 27-55-01 OPC GOOD PLACARD REMOVED. THIS CLEARS DMX62469. OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,033 hrs · 19,847 cycles

ONE EMERGENCY FLOOR LIGHT STRIP INOP AT 8CD. REMOVED AND REPLACED 1 EMERGENCY FLOOR LIGHT STRIP AT 8CD IAW AMM 33-51-01. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,033 hrs · 19,847 cycles

ONE EMERGENCY FLOOR LIGHT STRIP INOP AT 6CD. REMOVED AND REPLACED 1 EMERGENCY FLOOR LIGHT STRIP AT 6CD IAW AMM 33-51-01. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,886 hrs · 18,817 cycles

FS 559 BULKHEAD HAS CRACK INDICATION AT LBL 18. REPAIRED IAW BOMBARDIER REO REO 601R-53-41-260 REV E.

Part: ISIS UNIT — CONTAMINATED (COCKPIT) · airframe 21,875 hrs · 18,742 cycles

DIS-328597-2011 ISIS INDICATED 0 KNOTS DURING T/O AT 80 KNOTS T/O ABORTED PERGED STBY ISIS SYSTEM WITH NITROGEN TO REMOVE WATER. PERFORMED OPS CHECK OF ISIS IAW AMM 34-14-01. OPS CHECK GOOD. NO OTHER DEFECTS FOUND.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,433 hrs · 18,403 cycles

PASSENGER DOOR SILL PLATE ANGLE INCURRED LEVEL 2 CORROSION FROM FS 319 TO FS 333. REMOVED AND REPLACED PASSENGER DOOR SILL PLATE ANGLE.

Part: FLOORBEAM — CORRODED (FS 280) · airframe 21,494 hrs · 18,401 cycles

FS 280, FWD FLOOR SUPPORT FOUND CORRODED.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 21,494 hrs · 18,401 cycles

FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IS CORRODED. REPAIRED IAW SRM 51-42-06, 51-42-11, 51-42-21, 51-42-22, AND REO 601R-53-61-3778.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,494 hrs · 18,401 cycles

CARGOTRACK AT FS 621 LBL 9 CORRODED. CARGO TRACK REPAIRED IAW SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,494 hrs · 18,401 cycles

FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IS CORRODED. REPAIRED FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IAW CRJ 200 SRM 51-42-06, 51-42-11, 51-42-21, 51-42-22, AND BOMBARDIER REO 601R-53-61-3778.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,494 hrs · 18,401 cycles

CARGO SEAT TRACKS AT FS 621 LBL NINE, FS 559+112 RBL AND LBL NINE, FS 559+96 RBL AND TWENTY-SEVEN ARE CORRODED. CARGO TIE DOWN TRACKS REPAIRED AT LBL 9, FS 621, RBL + LBL 559+112, RBL + LBL 27, FS 559+96 IAW CRJ 200 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,494 hrs · 18,401 cycles

FS 280 FWD FLOOR SUPPORT IS CORRODED. REPAIRED FS 280 FWD FLOOR SUPPORT ANGLE P/N 600-34017-351S IAW CRJ 200 SRM 51-42-06, 51-40-11, 51-21-11, 51-23-00, AND 51-42-21.

Part: HINGE FITTING — GOUGED (TE FLAP) · airframe 20,880 hrs · 17,881 cycles

DAMAGE WAS FOUND ON THE LEFT WING OUTBOARD FLAP HINGE ARM ASSEMBLY ON THE P/N 601R14611-41 FITTING AT WS-264. DAMAGE TO THE HINGE ARM FITTING CONSISTS OF GOUGING THAT MEASURES 0.75 INCH LONG BY FULL WIDTH OF FITTING WIDE WITH A MAXIMUM DEPTH OF 0.030 INCH. REPAIRED IAW STS ENGINEERING EA 5-2010-250.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 20,307 hrs · 17,623 cycles

ACESS BUS CAUTION MESSAGE. AIRCRAFT STILL IN WORK.

Part: ENGINE — LEAKING (LEFT) · airframe 19,780 hrs · 16,847 cycles

AT THE 80 KNOT CALL OUT, ON TAKEOFF ROLL FROM KMEM THE F/O ALERTED THE CAPTAIN TO THE LT ENGINE ITT INDICATION BEING APPROXIMATELY 900 DEGREES AND IN THE RED. THE CAPTAIN ABORTED THE TAKEOFF AND CLEARED THE RUNWAY. THE QRH WAS COMPLETED AND THE CAPTAIN ELECTED TO SHUT DOWN THE LT ENGINE. MAINTENANCE DETERMINED THAT THE ENGINE HAD AN INTERNAL OIL LEAK. THE ENGINE IS BEING REPLACED TODAY.

Part: COALESCER BAG — CONTAMINATED (CABIN AIR)

AFTER ENGINE START USING GROUND AIR START CABIN BEGIN TO FILL WITH SMOKE. ENGINE SHUTDOWN AND PLANE DEPLANED. MX INSPECTED ACFT, FOUND BOTH LT AND RT ACM (AIR CYCLE MACHINE) WATER SEPARATOR COALESCER BAGS CONTAMINATED WITH OIL, COALESCER BAGS REPLACED, GROUND RUNS PERFORMED WITH NO DEFECTS NOTED. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 10,372 hrs · 8,945 cycles

ON APPROACH RECEIVED FLAPS FAIL MESSAGE WHEN SELECTING FLAPS EIGHT DEGREES. QRH PERFORMED, DECLARED EMERGENCY, PERFORMED FLAPS ZERO UNEVETFUL LANDING. MAINT RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: ENGINE — DAMAGED (RIGHT) · airframe 9,738 hrs · 8,440 cycles

WHEN LEVEL AT FL300 THE RT ENGINE SHUTDOWN. FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND SEVER DAMAGE TO THE ENGINE'S FAN SECTION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. DAMAGED ENGINE WILL BE INSPECTED FOR CAUSE DURING THE REPAIR PROCESS.

Part: SENSOR — FAILED (TE FLAPS)

(REF NR 05-090) FLAPS FAIL AT 4 DEGREES ON FINAL. PERFORMED RIGGING OF LT AND RT BRAKE POSITION SENSING UNIT ( BPSL) IAW AMM. (K)

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG CENTERING)

(SWITCH) -ON DEPARTURE AFTER GEAR SELECTED UP, CREW RECEIVED A (NOSE DOOR OPEN) MESSAGE AND A GEAR DISAGREE WARNING. CHECKLIST WAS FOLLOWED AND A UNEVENTFUL LANDING WAS MADE. FOUND NOSE LANDING GEAR STRUT CENTERING PROXIMITY SWITCH OUT OF ADJUSTMENT.