N8960A

Part: OXYGEN MASK — RUPTURED (COCKPIT) · airframe 25,258 hrs · 22,776 cycles

FO O2 MASK HARNESS RUPTURED DURING TESTING. REMOVED AND REPLACED FO'S OXYGEN MASK IAW AMM 35-11-12. OPS CHECK GOOD.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 24,533 hrs · 22,038 cycles

OBSERVER O2 MASK IS NOT TESTING CORRECTLY WHEN THE PRESS O2 TO TEST & RESET IS PUSHED. THE O2 DOES NOT STOP FLOWING IT NOT IN THE EMER SETTING. R & R OBSERVERS 02 MASK IAW AMM 35-11-12. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,958 hrs · 21,451 cycles

1ST OFFICER'S EMER FLASHLIGHT IS INOPERATIVE. R & R 1ST OFFICERS EMER FLASHLIGHT IAW AMM 25-61-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

AFT FUSELAGE BELOW FLOOR FRAME AT FS 605, BETWEEN STRINGERS 24LT & 24RT IS CORRODED. REMOVED CORROSION WITH A LOSS OF .008 WITH .042 REMAINING & IS OUT OF LIMITS IAW SRM 5300-00. REPAIRED FRAME IAW EA NR 253-03910.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,858 hrs · 21,351 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED & REINSTALLED NEW AFT DRAG ANGLE IAW REO 601R-52-11-082.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 23,858 hrs · 21,351 cycles

FLIGHT ATTENDANT OXYGEN MASKS FAILED TO DEPLOY DURING OPERATIONAL CHECK. R & R FLIGHT ATTENDANT OXYGEN MASK CATCH MECHANISM IAW AMM 35-21-05-020-803 STEP 3A. OPERATIONS CHECK OF FLIGHT ATTENDANT OXYGEN MASK GOOD IAW AMM 35-20-00-710-803. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

INTERCOSTAL SUPPORT CLIP CRACKED AT FS 621 BH, STRINGER 12L. REMOVED INTERCOSTAL SUPPORT CLIP AT FS 621, STRINGER 12L IAW SRM 51-42-06. REPLACED WITH NEW SUPPORT CLIP IAW SRM 51-42-06.

Part: GLOWSTRIP — DEBONDED (CABIN) · airframe 23,858 hrs · 21,351 cycles

ALL PHOTO LUMINESCENT EMER FLOOR LIGHTS STAINED & DISBONDED. R & R ALL PHOTO LUMINESCENT EMER FLOOR LIGHTS ON PANEL RACK.

Part: ANGLE — CRACKED (NR 1 COWLING) · airframe 23,858 hrs · 21,351 cycles

NUMBER 1 ENG INLET NOSE COWL, CRACKED SPRING ANGLE AT 6 O'CLOCK POSITION AFT OF PDU. R & R DAMAGED SPRING ANGLE ON NR 1 ENG INLET NOSE COWL AT 6 O'CLOCK POSITION IAW CMM 20-42-13.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

LEFT OBLIQUE ANGLE AT FS 621 BH STRINGER 13L CRACKED. R & R LT OBLIQUE ANGLE AT FS 621 BH. STRINGER 13L IAW SRM 51-42-21. "

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

INTERCOSTAL SUPPORT CLIP CRACKED AT FS 621 BH, STRINGER 13L. R & R CRACKED INTERCOSTAL SUPPORT CLIP WITH A SERVICEABLE INTERCOSTAL SUPPORT CLIP IAW SRM 51-42-21.

Part: BRACKET — CRACKED (RT WING) · airframe 23,858 hrs · 21,351 cycles

RIGHT WING REFUEL DEFUEL BRACKET IS CRACKED. REMOVED CRACK, FOUND IT TO BE WITHIN LIMITS IAW SRM 57-00-00.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,858 hrs · 21,351 cycles

PASSENGER DOOR INNER HANDLE CRACKED. R & R PAX DOOR INNER HANDLE IAW SRM 51-42-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

FLOORBEAM HAS CORROSION AT FASTENER HOLES STATION 574 - 621, LBL 27. R & R FLOORBEAM UPPER CAP FROM FS 574 - 621, LBL 27 IAW SRM 51-42-20 & REO 601R-53-61-3778.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

FLOOR STRUCTURE AT PAX DOOR OPENING, HAS CORROSION AT THE LOWER ANGLE, BETWEEN FS 310 & FS 349. R & R SILL PAX DOOR IAW SRM 51-42-21 & 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

RIGHT WINDSHIELD SIDE POST, LOWER AFT FITTING CRACKED. R & R RT WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

LEFT WINDSHIELD SIDE POST, LOWER AFT FITTING CRACKED. R & R LT WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.

Part: STRAP — CORRODED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

FLOOR STRAP HAS CORROSION AT FS 559, BETWEEN RBL 27 & THE RT FLOOR SILL IN CABIN. REMOVED CORROSION WITH A LOSS OF .006 & WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-45. FABRICATED & INSTALLED NEW FLOOR STRAP IAW SRM 51-42-06.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 23,858 hrs · 21,351 cycles

DURING CORROSION REMOVAL A CRACK WAS NOTED WHILE PERFORMING NDT ON THE AFT CARGO LOWER DOOR SILL AT FS 589. REPAIRED CRACK ON AFT CARGO LOWER DOOR SILL AT FS .589 IAW EO 601R-53-61-433.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,780 hrs · 21,274 cycles

FLIGHT ATTENDANT FLASHLIGHT IS OUT OF CASE & DEAD. R & R FLIGHT ATTENDANTS FLASHLIGHT IAW AMM 25-61-04.

Part: LANDING GEAR — DEFECTIVE (NOSE) · airframe 23,776 hrs · 21,270 cycles

AFT TAKEOFF, WHEN LG CYCLED UP, WE RECEIVED NOSE DOOR OPEN, GEAR DISAGREE WARNING MSG. DASHED IN LT & RT GEAR & ON INDICATION IN CTR, ALSO RECEIVED STEERING INOPERATIVE. WOW INPUT & WOW INPUT FAILED CAUTION MSG. RAN QRH, WARNING MSG WENT AWAY, WOW INPUT REMAINED. RETURNED, NOT OVERNIGHT LANDING. DEFERRED ACFT LG IAW MEL 33-30-01. GEAR PINS INSTALLED. ALL PROCEDURES COMPLIED WITH. ENTERED INTO MM02, PLACARDED PER MEL. R & R NLG ASSEMBLY IAW JC 200-32-21-01, PN OFF & ON 16735-109, SN OFF 07MPT117, SN ON DCL1029/04. INSTALLED NEW RT RVDT PN 16735-109, SN 5138. RIGGED NOSE WHEEL STEERING. OPERATIONS CHECKED GOOD IAW MM 409 535975 & CONT CARDS FOR DETAILS. MM02 UPDATED & PLACARD REMOVED.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 23,773 hrs · 21,266 cycles

AFTER TAKEOFF, WHEN LG CYCLED UP, WE GOT NOSE DOOR OPEN, GEAR DISAGREE, STEERING INOPERATIVE, WOW INPUT & WOW INPUT FAIL. RAN QRH & GOT THE GEAR DOWN & LOCKED. WOW INPUT & WOW INPUT FAIL LIGHTS REMAINED ON. LANDED NORMALLY. IAW MOTR GROUP REPLACE NLG WOW NR 2 CENTERED HARNESS ASSEMBLY, NLG NR 2 WOW PROX SENSOR, NLG OLEO CENTERED & EXTENDED PROX SENSOR & OLEO CENTERED & EXTENDED BRACKET. COMPLETED NOSE STRUT SERVICE IAW AMM 12-12-32. TROUBLE SHOT NLG FIM 32-60-07. FOUND LOOSE BACK SHELL & TIGHTENED AS REQUIRED. COMPLETED GEAR SWINGS, NO FAULTS FOUND. SEE DISCREPANCY NR 1 & 2 ON LOG PAGE 3198928 FOR FURTHER ACTION. R & R NLG WOW 2 CENTERED HARNESS ASSEMBLY IAW AMM 32-61-25, NLG NR 2 WOW PROX SENSOR, NLG OLEO CENTERED & EXTENDED PROX SENSOR & OLEO CENTERED & EXTENDED BRACKET IAW AMM 32-61-05. OPERATIONS CHECKED GOOD.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 23,054 hrs · 20,530 cycles

CREW ESCAPE HATCH LEAKING. R & R CREW ESCAPE HATCH SEAL IAW AMM 55-22-07. OPERATIONS & LEAK CHECK GOOD, PN ON & OFF CC670-38022-1.

Part: BRACKET — DAMAGED (NLG) · airframe 22,903 hrs · 20,357 cycles

GEAR DISAGREE AFTER ROTATION, NOSE GEAR WOULD NOT RETRACT FOR 20 SECONDS, SPEED APPROX 160 KTS. GEAR SELECTED DOWN, 3 GREEN LANDED WITHOUT INCIDENT. R & R CENTERING SWITCH BRACKET & WOW NR 2 CENTERING HARNESS IAW AMM 32-61-25. PERFORMED EXTENSION & RETRACTION CHECK IAW AMM 32-30-00. ALL CHECKED GOOD SEE NRCC N68317 & N70806 FOR WORK PERFORMED.

Part: WARNING SYSTEM — FALSE ACTIVATION (MLG) · airframe 22,553 hrs · 19,982 cycles

DURING DEPARTURE, AS GEAR WENT UP RECEIVED A TRIPLE CHIME GEAR DISAGREE NOSE WHEEL WARNINGS. PERFORMED QRH UPON SELECTING HYD 2B PUMP ON GEAR RETRACTED. CYCLED TWICE OK. LANDED WITHOUT PROBLEMS TROUBLESHOT IAW FIM 32-60-07, NLG HARNESS 31-61-25. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,451 hrs · 19,879 cycles

FIRST OFFICER`S EMER FLASHLIGHT INOPERATIVE. R & R THE FIRST OFFICER`S EMER FLASHLIGHT BATTERY IAW AMM 25-61-02. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,288 hrs · 19,711 cycles

DENT IN THE FUSELAGE SKIN AT FS 598 AT THE SKIN SPLICE AT STRINGER 20L. THE DENT MEASURES 1 INCH X 0.63 INCH X 0.017 INCHES DEEP. REPAIRED IAW EA CRJ253-02971.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 22,234 hrs · 19,654 cycles

DURING TAXI AFTER STARTING THE NR 1 ENG THE FIRST OFFICER NOTICED THAT THE APU TEMP SPIKED. TURNED THE APU BLEED OFF & ENG BLEEDS ON. ACFT FILLED WITH SMOKE AT THAT TIME PAX & CREW EVACUATED ACFT. PERFORMED OPERATIONAL CHECKS OF THE APU & LT & RT ENG BLEED AIR SYS. FOUND ENG BLEED SYS TO BE SATISFACTORY, FOUND APU TO BE INOPERATIVE. DEFERRED APU IAW MEL 49-10-11 IAW AUTHORIZATION 008599. PLACARD INSTALLED, SEE NON-ROUTINE CONTINUATION CARDS N60758, N61034 & N60933 FOR DETAILS. R & R APU IAW AMM 49-10-00 & CHECKLIST STEPS 22 - 28 NEED TO BE COMPLIED WITH FOR CLOSEOUT. SEE PAGE 3061796-1 FOR FURTHER DETAILS DM REMAINS OPEN.

Part: SPAR — OUT OF ALIGNMENT (WINGLET) · airframe 22,176 hrs · 19,591 cycles

FOUND 7 FASTENER HOLES COMMON TO THE WINGLET SPAR & SPAR FITTINGS DID NOT PROPERLY ALIGN. REPAIRED IAW EA CRJ257-02898.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,127 hrs · 19,543 cycles

AFT FACING EXIT SIGN & EXTERIOR EMER LIGHTS WHERE NOT WORKING. R & R NR 3 EMER BATTERY PACK IAW AMM 33-51-04. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,681 hrs · 19,097 cycles

THE FRONT CEILING EMER FLOODLIGHT TURNS ON & FADES TO BLACK AFTER 5 - 10 SECONDS WHEN THE EMERGENCY LIGHTS ARE TURNED ON. DEFERRED OVERHEAD EMER LIGHT IAW MEL 33-51-11. R & R EMER LIGHT BATTERY NR 1 IAW AMM 33-51-04.

Part: FLAP — OBSTRUCTED (WING) · airframe 21,088 hrs · 18,520 cycles

FLAPS FAIL CAUTION MSG AT GATE. FLIGHT CONTROL SYNOPTIC PAGE SHOWS LT FLAP AT 0 DEGREES & RT FLAP AT 2 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. CLEANED ICE & SLUSH AWAY FROM FLAPS IAW FIM 27-50-00. OPERATIONS CHECKED FLAPS IAW AMM 27-54-00. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 21,046 hrs · 18,479 cycles

ONE INFANT LIFE VEST HAS TEAR IN BAG. R & R ONE INFANT LIFE VEST IAW PA 25-096A.

Part: SKIN — DAMAGED (BS 605-615) · airframe 20,960 hrs · 18,388 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN AT FS 605, 609, AND 615 JUST BELOW S24L TO HAVE LIGHTNING DAMAGE. REPAIRED IAW EA CRJ253-02226.

Part: SKIN — DAMAGED (BS 700) · airframe 20,960 hrs · 18,388 cycles

MAINTENANCE FOUND A LIGHTNING BURN TO THE LEFT FUSELAGE AT FS 700.00 AT S22L. REPAIRED IAW EA CRJ253-02224.

Part: SKIN — DAMAGED (BS 640) · airframe 20,960 hrs · 18,388 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN AT FS 640 AND S25L TO HAVE LIGHTNING DAMAGE. REPAIRED IAW EA CRJ253-02225.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 20,960 hrs · 18,388 cycles

FUSELAGE SKIN AT FS 580.00 BELOW STRINGER 24L HAS LIGHTNING DAMAGE. THE DAMAGE WAS REMOVED BY BLENDING RESULTING IN A BLEND OUT MEASURING 3 INCHES X 1.70 INCHES, ” X 0.017 INCHES DEEP. REPAIRED IAW EA CRJ253-02227.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,060 hrs · 16,517 cycles

FLIGHT ATTENDANT REPORTS EMERGENCY LIGHTS ACTIVATED AFTER LANDING. CANNOT TURN THEM OFF FROM THE FLIGHT DECK. REPLACED NR 1 EMERGENCY BATTERY AND EMERGENCY BATTERY CHARGER IAW CRJ200 AMM 33-51-00. OPS CHECKS GOOD. OK FOR SERVICE.

Part: SEAL — BROKEN (MEDICAL KIT) · airframe 18,570 hrs · 16,037 cycles

GREEN SEAL ON MEDICAL KIT IS BROKEN. REPLACED GREEN SEAL ON EMK AS REQUIRED. OK FOR SERVICE.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 18,394 hrs · 15,861 cycles

FLIGHT 4145, RECEIVED GEAR DISAGREE ON GEAR EXTENSION. QRH COMPLETED FOR GEAR UP DISAGREE AND HYD 3 LOW PRESSURE CAUTION GEAR EXTENDED AND LOCKED WITH MANUAL EXTENSION. HYD 3 SHOWED LESS THAT 5 PERCENT FLUID AND ZERO PRESSURE. EMERGENCY DECLARED AND COMPLETED NORMAL LANDING. REPLACED LEFT HYDRAULIC PUMP NR 3A IAW AMM 29-12-03. REPLACED RIGHT HYDRAULIC PUMP NR 3B IAW AMM 29-12-03. OPS AND LEAK CHECKED GOOD. BLEED HYDRAULIC SYSTEM NR 3 IAW AMM 29-10-00. COMPLETED INSPECTION OF HYDRAULIC SYSTEM NR 3 IAW AMM 05-51-34. COMPLIED WITH PA 05-018G. GEAR DISAGREE CAUSED BY HYDRAULIC SYSTEM NR 3 FLUID LOSS. ALL CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,313 hrs · 15,779 cycles

RIGHT NR 1 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: ANGLE — DAMAGED (BS 621) · airframe 18,275 hrs · 15,750 cycles

DURING THE ACCOMPLISHMENT OF GREO 601R-53-61-1230, IT WAS NOTED THAT THE LEFT LOWER CAP ANGLE AT APPROXIMATE BS 621, WL 106 HAS DRILL START DAMAGE. REPAIRED IAW REO 601R-53-61-4596.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,275 hrs · 15,750 cycles

FS 621 PRESSURE BULKHEAD CRACKED AT LEFT LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-5361-1230.

Part: BEARING — WORN (LT ELEVATOR) · airframe 18,257 hrs · 15,750 cycles

LEFT ELEVATOR INBOARD HINGE BEARING WORN. REPAIRED IAW SRM 51-42-21/51-42-06.

Part: ANGLE — CRACKED (BS 559) · airframe 18,275 hrs · 15,750 cycles

CRACK IN FS 559 CAP ANGLES RBL 9, RBL18, AND LBL18. REPAIRED IAW REO 601R-53-41-206 AND REO 601R-53-41-609.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 17,900 hrs · 15,379 cycles

EMERGENCY EXIT LIGHT IN ROW 1 A+B CAME OFF THE BULKHEAD. LIGHT STILL WORKS. REMOVED AND REPLACED EMERGENCY LT IAW CRJ200 AMM 33-51-13 VERIFIED PARTS EFFECTIVITY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,875 hrs · 15,353 cycles

F/A FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-00. CHECKS GOOD. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,760 hrs · 15,234 cycles

NR 4 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04 OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED · airframe 17,594 hrs · 15,068 cycles

SMOKE TOILET CAUTION MSG AFTER TAKEOFF AIR RETURNED, NO SMOKE IN CABIN OR LAV ALL INDICATIONS NORMAL. CHANGED THE ENGINE.

Part: A/C PACK — INOPERATIVE (AC BAY) · airframe 17,516 hrs · 14,996 cycles

SMOKE TOILET CAUTION ON CLIMB, BURNT RAG SMELL IN COCKPIT, NEGATIVE DE ICE PRIOR TO T/O, TOILET ALARM GOING OFF AS WELL, PAX REPORTED BURNT CHEMICAL SMELL. C/W SMOKE/FUMES IN CABIN WORKSCOPE. FOUND RT PACK INOP AND DEFERRED. DEFERRED IAW MEL 21-51-01.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 17,520 hrs · 15,001 cycles

DENT REPORTED BETWEEN FS 682 AND FS 700 AND S-21L AND S-22L MEASURING 4.625 X 2.125 X 0.105 DEEP. REPAIRED IAW EA CRJ253-00390A AND CORRESPONDING 8110-3.

Part: CONNECTOR — DAMAGED (RT IDG) · airframe 17,449 hrs · 14,936 cycles

UNSCHEDULED LANDING FOR IDG NR 2 CAUTION IN-FLIGHT. REPINNED RT IDG OIL TEMP BULB CONNECTOR AND RECONNECTED IDG. OPS CHECKED IAW AMM 24-13-05. NO DEFECTS NOTED. REPINNED TEMP BULB CONNECTOR IAW ESPM 20. READY FOR SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 17,356 hrs · 14,843 cycles

AIR RETURN FOR SMOKE IN TOILET. REPLACED COALESCER BAGS IAW TCM 21-310-003 AND PERFORMED ENGINE RUNS IAW AMM 71-00-00. OP/C CHECK GOOD. NO SMOKE OR SMELL NOTED.

Part: CABLE — DEFECTIVE (PAX DOOR) · airframe 17,226 hrs · 14,761 cycles

MAIN CABIN DOOR VERY DIFFICULT TO CLOSE. REMOVED AND REPLACED PAX DOOR ICE BREAKER CABLE IAW AMM 52-11-15. PAX DOOR OPS CHECKS NORMAL.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 17,235 hrs · 14,718 cycles

AIR RETURN. EMERGENCY DECLARED. ON DEPARTURE EN COUNTERED STRONG SMELL LIKE SMOKE, SHORTLY THEREAFTER THE SMOKE TOTLET MASTER CAUTION APPEARED. THE MESSAGE DISSAPPEARED ON FINAL WHEN THE THRUST WAS BROUGHT BELOW APPROXIMATELY 60%. COMPLIED WITH MINIMUM WORK-SCOPE FOR SMOKE & FUMES. FOUND COALESCER SOCKS DIRTY, PERFORMED GROUND RUNS NO DEFECT'S NOTED IAW 71-00-00.

Part: SKIN — CHAFED (RT WING) · airframe 17,181 hrs · 14,718 cycles

RIGHT WING LOWER PLANK FUEL ACCESS DOOR CUTOUT CHAFED AT WS 294.5 - WS 314.5. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 17,181 hrs · 14,718 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 56.30, WS 104.099, AND WS 139.924. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.

Part: SKIN — CHAFED (RT WING) · corrosion level 2 · airframe 17,181 hrs · 14,718 cycles

RIGHT WING LOWER PLANK FUEL TANK ACCESS PANEL DOOR CUTOUT CHAFED AT WS 294.5 TO WS 314.5. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CHAFED (RT WING) · airframe 17,181 hrs · 14,718 cycles

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT CHAFED AT WS 47.61 - WS 66.2. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 17,181 hrs · 14,718 cycles

RIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 60.005, WS 98.509, AND WS 137.012. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 17,181 hrs · 14,718 cycles

RIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 60.005, 98.509, 137.012. REPAIRED IAW REO 601R-57-52-004.

Part: WIRE — SHORTED (BLEED AIR SYS) · airframe 16,968 hrs · 14,460 cycles

ANTI ICE DUCT WARNING IN FLIGHT LEFT WING CAME ON WITH NO WING ICE ON. T/S SYSTEM FOUND WIRE STUD AT 1GSWK SHORTED. REPAIRED WIRE, SYSTEM OPC GOOD IAW CRJ 200 AMM 36-21-00.

Part: FUEL CONTROL — MISRIGGED (LT ENGINE) · airframe 16,839 hrs · 14,339 cycles

LT ENG SHUT DOWN / FLAME OUT ONCE THE TRUST REVERSER WAS STOWED AFTER LANDING. CREW DID NOT DELCARE AN EMERGENCY. RIGGED LT MFC IAW CRJ AMM 73-21-01, PERFORMED ENGINE POWER RUNS OF LT ENG AT RUN PAD IAW AMM 71-00-00. OP CHECK NORMAL. OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,770 hrs · 14,267 cycles

AIRCRAFT DIVERTED INTO TYS FOR APU OIL TEMP CAUTION AIRCRAFT DIVERTED INTO TYS AND MAINT IS IN THE PROCESS OF T/SHOOTING TO REPAIR AS REQUIRED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,550 hrs · 13,132 cycles

GEAR DISAGREE DURING EXTENSION WHILE INBOUND TO JFK. FLIGHT LANDED WITHOUT INCIDENT.

Part: SAFETY SWITCH — OUT OF RIG (NLG) · airframe 15,418 hrs · 13,013 cycles

AIR RETURN FOR NOSE GEAR DISAGREE ON A/C 8960 SWAPPED INTO 8797 SWUNG NOSE GEAR AND WERE ABLE TO DUPLICATE DISCREPANCY. WHILE JACKED, CHECKED THE RIG ON THE NR 1 NLG WOW SWITCH AND FOUND IT TO BE .094 INCH. PROPER RIG IS .045 - .055 INCH. SYSTEM OP'S CHECKED GOOD IAW AMM 32-61-05.

Part: LANDING GEAR — MALFUNCTIONED (RT MLG) · airframe 13,380 hrs · 11,061 cycles

ON TAKEOFF FROM 36L FROM MEM THE RIGHT MAIN GEAR WOULD NOT RETRACT CAUSING A GEAR DISAGREE WARNING MESSAGE. THE QRH WAS COMPLETED AND ATTEMPTED TO CONTACT DISPATCH ON 131.22, WITH NO SUCCESS. THE ACRS WAS DEFERRED. AFTER SEVERAL ATTEMPTS CONTACTED OPERATIONS AND ASKED THEM TO RELAY THE MESSAGE TO DISPATCH, RETURNED TO MEM AND LANDED OVERWEIGHT.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 5,625 hrs · 4,405 cycles

RECEIVED A FALSE LAVATORY SMOKE WARNING AFTER TAKEOFF. REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR IAW BOMBARDIER AMM.

Part: FLAP — MALFUNCTIONED (WING) · airframe 2,315 hrs · 1,807 cycles

FLAPS FAILED AT 20 ON TAXI OUT, QRH FOLLOWED RETURN TO BLOCKS. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.