N8907A

Part: PUMP — MALFUNCTIONED (ENGINE FUEL) · airframe 25,781 hrs · 22,844 cycles

LEFT ENGINE ROLLED BACK TO IDLE AT 1000 FT. N1 & ITT NORMAL FOR IDLE N2 70% ACCOMPLISHED QRH ENGINE SHUTDOWN. R & R THE ENGINE FUEL PUMP IAW AMM 73-11-01, R & R THE ENGINE MAIN FUEL CONTROLLER IAW AMM 73-21-01. OPS CHECKED GOOD IAW AMM 71-00-00

Part: CAP — BROKEN (CABIN) · airframe 25,389 hrs · 22,449 cycles

AT SEAT 12D CONNECTION FOR FLOOR TRACK EMERGENCY LIGHTING BROKEN. R & R THE EMERGENCY FLOOR LIGHT END CAP, P40LY, IAW AMM 33-51-01, OPS CHECK GOOD.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 25,344 hrs · 22,406 cycles

PLASTIC COVER OVER FLOOR EMERGENCY LIGHT NEAR 1CD, 2CD & 3CD ARE LOOSE & COMING UP. SECURED PLASTIC COVER AS REQUIRED.

Part: COVER — UNSECURE (CABIN) · airframe 25,320 hrs · 22,380 cycles

RIGHT REAR FLOOR COVERING FOR EMER LIGHTS CAME OFF. SECURED EMER LIGHT FLOOR COVER IAW AMM 33-51-01. OK FOR SERVICE.

Part: COVER — LOOSE (CABIN) · airframe 25,304 hrs · 22,363 cycles

FLOOR EMER LIGHT STRIP LOOSE. REINSTALLED PLASTIC COVER ON EMER FLOOR TRACK LIGHTING.

Part: COVER — LOOSE (CABIN) · airframe 25,282 hrs · 22,340 cycles

PLASTIC COVER OVER FLOOR EMER LIGHTING STRIP LOOSE NEXT TO FIRST TWO ROWS ON FIRST OFFICERS SIDE OF PLANE. SECURED EMER LIGHTING STRIP AS REQUIRED.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 25,232 hrs · 22,289 cycles

COCKPIT PBE BAG TORN. REPLACED COCKPIT PBE AS REQUIRED IAW AMM 35-30-00 & SUBTASK 35-30-00-941-007, PN ON & OFF MR-10047N.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,876 hrs · 21,944 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. OPENED DEFERRAL IAW MEL 25-61-04. ENTERED IN MM02 & PLACARD INSTALLED, OK FOR SERVICE. TEMP FLASHLIGHT PROVIDED IAW MEL & MOC 96211. REPLACED FLASHLIGHT ASSEMBLY WITH A SERVICEABLE FLASHLIGHT ASSEMBLY IAW CMM 26-60-02.

Part: COWLING — CHAFED · airframe 24,868 hrs · 21,936 cycles

OUTBOARD LE OF COWL 445AT, NEAR LATCH IS CHAFED. REPAIRED CHAFE IAW CMM 71-12-01 REPAIR SRS104.

Part: POST — CRACKED (COCKPIT) · airframe 24,868 hrs · 21,936 cycles

LEFT LOWER FITTING ON WINDSHIELD CENTER POST, AT FS 202.75 IS CRACKED. REMOVED LT LOWER FITTING & REPLACED WITH NEW FITTING IAW SRM 51-42-20.

Part: SUPPORT ANGLE — BROKEN (THRUST REVERSER) · airframe 24,868 hrs · 21,936 cycles

RIGHT UPPER THRUST REVERSER TRACK STAND FAIRING, SUPPORT Z ANGLE BROKEN. R & R SUPPORT Z ANGLE IAW MM 20-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 24,868 hrs · 21,936 cycles

IN RIGHT WW THE BRAKE PRESS TRANSDUCER BRACKET IS CRACKED. R & R BRAKE PRESS TRANSDUCER BRACKET IN RT MLG WW IAW SRM 51-42-22 & SRM 51-41-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 24,868 hrs · 21,936 cycles

LEFT WING INBD LE FUEL MANIFOLD, ATTACH ANGLE CRACKED AT OTBD LOWER RADIUS. REMOVED CRACK BY EDGE BLENDING IAW SRM 57-00-00.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 24,868 hrs · 21,936 cycles

RIGHT WING INBD FLAP VANE LE IS CHAFED IN 3 AREAS. REMOVED & INSTALLED 3 EA LE SKINS IAW SRM 51-42-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,868 hrs · 21,936 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED AREA, FABRICATED, LOCATED & INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV B. RESTORED TO ORIGINAL FINISH.

Part: PLATE — CRACKED (TE FLAP) · airframe 24,868 hrs · 21,936 cycles

INBOARD FLAP LE PANEL 684JB, MOUNTING PLATE CRACKED. FABRICATED 2 EACH INBD FLAP LE PANEL 684JB MOUNTING PLATES IAW SRM 51-40-11.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 24,868 hrs · 21,936 cycles

RIGHT WW DRAG ANGLE ADJACENT TO BATT RIB CRACKED. REMOVED RT WW DRAG ANGLE & INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,868 hrs · 21,936 cycles

AFT ACCESSORY COMPARTMENT, AFT BULKHEAD, OTBD LBL 36, ANGLE IS CRACKED. R & R CRACKED ANGLE WITH A SERVICEABLE FABRICATED REPAIR ANGLE IAW SRM 51-42-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 24,868 hrs · 21,936 cycles

BATHTUB FITTING AT FS 461.0 & OTBD OF RBL 9 IS CRACKED. REMOVED FITTING, LOCATED & INSTALLED NEW FITTING IAW SRM 51-40-11, 51-42-06 & 53-41-43.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,868 hrs · 21,936 cycles

SEAT RAIL BEAM, LBL 27, OTBD FLANGE, FS 574.00 TO FS 608.00, IS CORRODED AT FASTENER HOLES. R & R SEAT RAIL BEAM WITH NEW BEAM IAW SRM REO 601R-53-61-3778.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,868 hrs · 21,936 cycles

CLIP UNDER CARGO DOOR SILL AT FS 589.00 IS CRACKED. REMOVED CLIP UNDER CARGO DOOR SILL & REPLACED WITH NEW CLIP IAW SRM 51-42-20.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 24,611 hrs · 21,679 cycles

THREE INFANT LIFE VESTS HAVE DAMAGED PACKAGES. R & R ALL THREE INFANT LIFE VEST IAW PA 25-096A.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,611 hrs · 21,679 cycles

FIRST OFFICERS EMER FLASHLIGHT DOES NOT SHOW A CHARGE. DEFERRED FLASHLIGHT IAW MEL 25-61-04, CAT C. UPDATED PLACARD INSTALLED. R & R FIRST OFFICERS FLASHLIGHT IAW AMM 25-61-04, CLEARED MM02, CLEARED DM 002511 & PLACARD REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,474 hrs · 21,543 cycles

GEAR DISAGREE AFTER ROTATION, WHEN GEAR LEVER WAS SELECTED TO UP, RETRACTION, WITHIN 6 SECONDS OF HANDLE MOVEMENT, MANUAL RELEASE WAS PULLED. ALSO STEERING INOPERATIVE CAUTION MSG CAME ON NUMEROUS TIMES DURING TAXI IN. PERFORMED GEAR SWINGS IAW AMM 32--30-00, NO DEFECTS NOTED. RESET MANUAL RELEASE IAW AMM 32-34-00. SEE LOG PAGE 3195579-2 FOR NLG STRUT SERVICE. SEE LOG PAGE 3195580-1 FOR STEERING.

Part: UNKNOWN — SMOKE (LT BRAKE) · airframe 24,249 hrs · 21,319 cycles

LEFT INNER BRAKE, TIRE WHEEL ASSEMBLY, SMOKE COMING FROM BRAKE AREA AFTER LANDING. BTMS WAS 7, 8, 3 & 3 IN GATE, AFTER 5 MINUTES AFTER LANDING. PERFORMED VISUAL INSPECTION OF LT INBD BRAKE ASSEMBLY IAW AMM 32-43-26. NO FAULTS FOUND.

Part: HOSE — LEAKING (COCKPIT) · airframe 24,164 hrs · 21,229 cycles

OXYGEN HOSE FOUND LEAKING DURING INSTALLATION & LEAK CHECKS OF CREW OXYGEN STOWAGE BOX. R & R OXYGEN HOSE IAW AMM 35-11-15. OPERATIONS & LEAK CHECKED GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,833 hrs · 20,870 cycles

FLAP FAIL MASTER CAUTION MSG AFTER LANDING, ON TAXI IN ON GND WHILE RETRACTING, FAILED AT 27' TEMP OAT 1C. REFER TO AML PAGE 3177544 DISC 1, FLAP FAIL MSG AFTER LANDING ON GND DURING FLAP RETRACTION, TROUBLE SHOT FLAP FAIL EVENT IAW FIM CHAPTER 27-50-00 REV 48 & AD 2009-06-12 PARAGRAPH H 6 I AMOC LOG 14-105 DATED 12/30/2014 IAW TC 001100R1 TEC. RESET FLAP FAIL CAUTION IAW FIM RESET PROCEDURES, MSG EXTINGUISHED CYCLED FLAPS 5 CONSECUTIVE TIMES PROBLEM DID NOT REOCCUR. DEFERRED IAW MEL 27-50-00 CAT A UNDER DIRECTION OF MOC. ENTERED ITEM IN MM 2 PLACARD INSTALLED. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC LOG 14-105 DATED 12/30/2014 & TC 001100R1 FIM TECHNICAL SUPPLEMENT. LEG11812 CODE 5-2B, 19-C1, 19-C2 LEG 11812 5-2B, 19-C!, 19-C & 33-BC. TROUBLE SHOT IAW FIM 27-50-00 FIGURE 109. PERFORMED FLAP LEVER, CHECKED GOOD. OPERATED FLAPS 5 CYCLES CHECKED GOOD. SYS NORMAL, OK FOR SERVICE. THIS CLEARS DM000997. REMOVED FROM MM02 PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,430 hrs · 20,445 cycles

EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT SEAT 1C. REPAIRED EMER FLOOR TRACK LIGHTING IAW MM CH 33-51-01. SEE NON-ROUTINE N61000 FOR WORK COMPLETED.

Part: CAGE — DAMAGED (SMOKE DETECTOR) · airframe 23,006 hrs · 20,012 cycles

CARGO COMPARTMENT FWD SMOKE DETECTOR CAGE IS DAMAGED. R & R CARGO SMOKE DETECTOR NR 1 CAGE ASSEMBLY IAW AMM 26-15-01. OPERATIONS CHECKED OK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,341 hrs · 19,354 cycles

FS 280 BULKHEAD WEB OTBD OF RBL 9 & LBL 9 IS CRACKED. REPAIRED IAW REO 601R-53-11-171 & 601R-53-11-136.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 22,341 hrs · 19,354 cycles

STIFFENER ON AFT SIDE OF FS 621 BULKHEAD AT BL 0 BEHIND ISOLATION VLV IS CHAFED. REPAIRED IAW REO 601R-53-61-1523.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,341 hrs · 19,354 cycles

FOUND CORROSION TO THE FRAME AT FS 605. CORROSION WAS BLENDED FROM THE VERTICAL WEB RESULTING 3” X 2” X 0.007” DEEP MATERIAL REMOVAL. CORROSION WAS ALSO NOTED BETWEEN THE SKIN & LOWER FLANGE. REPAIRED IAW EA 253-02457.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,341 hrs · 19,354 cycles

THE DAMAGE CONSISTS OF A DENT TO THE FUSELAGE SKIN MEASURING 3.9” X 3.2” X 0.085” DEEP AFT OF THE PRODUCTION SKIN SPLICE AT FS 333 & BETWEEN STRINGER 20R & STRINGER 21R. REPAIRED IAW EA 253-02443A.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,004 hrs · 19,021 cycles

FLIGHT ATTENDANT`S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 21,233 hrs · 18,262 cycles

AT FL 290, AUTOPILOT HAD AN UNCOMMANNDED PITCH UP THAT CAUSED THE ACFT TO CLIMB APPROX 200 FT.

Part: SKIN — DENTED (BS 625-640) · airframe 21,048 hrs · 18,091 cycles

THE FUSELAGE SKIN DENTED MEASURING 2.710" X 1.5" X .0655" DEEP WITH MATERIAL LOSS FROM BLENDING MEASURING .007" MAXIMUM DEPTH OVER AND SURROUNDING THE DAMAGED AREA. REPAIRED IAW EA CRJ253-01771 AND ASSOCIATED 8110-3.

Part: CONTAINER — TORN (LIFE VEST) · airframe 20,822 hrs · 17,865 cycles

CAPTAIN'S LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.

Part: SIGN — LOOSE (CABIN) · airframe 20,010 hrs · 17,058 cycles

EXIT SIGN OVER GALLEY SERVICE DOOR LOOSE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-13. OPS CHECKS GOOD. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,435 hrs · 19,986 cycles

FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLIGHT ATTENDANT'S FLASHLIGHT BATTERY IAW 25-60-00. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 19,905 hrs · 16,952 cycles

GALLEY EMERGENCY EXIT SIGN BROKEN. RE-ATTACHED EMERGENCY LIGHT IAW AMM 33-51-09.

Part: SWITCH — INOPERATIVE (MACH TRIM) · airframe 19,132 hrs · 16,182 cycles

MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED MACH TRIM ENGAGE SWITCH AND OPS CHECKS GOOD IAW AMM 22-21-00.

Part: SWITCH — DIRTY (AILERON TRIM) · airframe 20,514 hrs · 17,970 cycles

AILERON TRIM IS DIFFICULT TO MOVE TO THE LEFT. REMOVED DEBRIS FROM AILERON TRIM SWITCH, CHECKS NORMAL IAW AMM 27-11-00. OK FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 18,660 hrs · 15,728 cycles

NLG GEAR DISAGREE. PROBLEM OCCURRED ON TAKEOFF NOSE GEAR WOULD NOT RETRACT. NOSE GEAR NEVER MOVED FROM THE DOWN AND LOCKED POSITION AS VERIFIED BY CODES. S35 SHOWED DOWN AND NEAR AND S21 SHOWED DOWN AND NEAR. CODE 23 SHOWED DOWN AND FAR WHICH IS FOR THE OLEO EXTENSION. BRACKET APPEARS TO BE IN GOOD CONDITION. COMPLIED WITH PA, 05-018F DUE TO GEAR DISAGREE MESSAGE MAINT & INSPECTION COMPLIED WITH IAW AMM 32-61-05. NO DEFECTS NOTED. OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 18,502 hrs · 15,584 cycles

GEAR DISAGREE ON LANDING (GEAR EXTENSION). FOUND NOSE GEAR UPLOCK PIN STICKING AND FOUND SEVERAL PROX SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCHES, LUBED ROLLER, AND OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,330 hrs · 15,404 cycles

ON APPROACH AT 7000 FT, FLIGHT ATTENDANT INDICATED A STRONG GASOLINE ODOR IN REAR OF AIRCRAFT AROUND LAVATORY. RAN PACKS WITH ENGINES, AND APU IAW AMM'S 72-20-00 & 49-10-00, COULD NOT FIND LEAK OR FIND ANY EVIDENCE OF FUEL ODOR. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,147 hrs · 15,238 cycles

EMERGENCY LIGHT FLOOR STRIP AT SEAT 6CD IS INOP. REMOVED AND REPLACED THE 6CD POSITION EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-51-01. OPS CHECKS GOOD. THIS CLEARS DM 57676. A/C READY FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,998 hrs · 15,099 cycles

FS 280 AFT SIDE, JUST OUTBOARD OF LBL 9 "J" ANGLE IS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,998 hrs · 15,099 cycles

DENT AND GOUGE DAMAGE ON FUSLAGE SKIN B/W FS 589 - FS 605 & STR 24R - STR 26R. REPAIRED IAW BOMBARDIER REO 601R-53-61-4329 REV B.

Part: FITTING — CHAFED (LT WING) · airframe 17,998 hrs · 15,099 cycles

LEFT WING AFT SPAR FLAP ROLLER GUIDE FITTING CHAFED APPROX .025 DEEP AND WING PLANK LOWER SKIN CHAFED APPROX .010 DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-51-143 AND SRM 51-12-00.

Part: STRUCTURE — CHAFED (CENTER WING) · airframe 17,998 hrs · 15,099 cycles

RIGHT OF CENTER WING LOWER PLANK JUST I/B OF RBL 45.0 AFT EDGE IS CHAFED .5 WIDE X .5 WIDE APPROX .025 DEEP. DAMAGE WAS IN ONE AS DEFINED IN REO 601R-57-21-880. REPAIRED IAW BOMBARDIER REO 601R-57-21-880.

Part: STRUCTURE — CHAFED (CENTER WING) · airframe 17,998 hrs · 15,099 cycles

LEFT OF CENTER WING LOWER PLANK JUST I/B OF LBL 45.0 AFT EDGE IS CHAFED. 1" LONG X .5" WIDE X APPROX .025" DEEP. DAMAGE WAS IN ONE AS DEFINED IN REO 601R-57-21-880. REPAIRED IAW BOMBARDIER REO 601R-57-21-880.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,992 hrs · 15,093 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621 AT LT LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: UNKNOWN — STIFF (ELEVATOR) · airframe 17,779 hrs · 14,876 cycles

ELEVATOR FELT STIFF DURING THE FINAL APPROACH WHILE HAND FLYING. THE STIFFNESS WAS FELT ABOUT THREE INCHES OFF CENTER BOTH FORWARDS AND BACKWARDS. PERFORMED VISUAL INSP OF ELEVATOR AND OPS TEST OF ELEVATOR CONTROL SYSTEM IAW AMM 27-31-00. COULD NOT DUPLICATE. OPS GOOD. NO DEFECTS NOTED. A/C REQUIRES FCF DUE TO REPORT OF EXISTENT ELEVATOR RESISTANCE. REF AML PAGE 865257 ITEM 1. FCF FOUND SATISFACTORY.

Part: CONTROL QUADRANT — DEFECTIVE (THROTTLE) · airframe 17,739 hrs · 14,836 cycles

RT FUEL SHUTOFF LEVER ON RIGHT THURST LEVER LOOSE. RT THURST LEVER ADVANCES WITHOUT MOVING FUEL LEVER FROM SHUTOFF TO IDLE. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 72-11-01 OPC GOOD. OK FOR SERVICE, VERIFIED PART EFFECTIVITY.

Part: SKIN — DENTED (HORIZ STAB) · airframe 16,243 hrs · 13,472 cycles

ONE DENT 0.010" DEEP X 0.25" DIA ON H-STAB LEFT LEADING EDGE SKIN AND SURFACE SCRATCHES WITH NO DEPTH REPORTED LOCATED 13.00" FROM BL6.00 AND 4.50" FROM BOTTOM SKIN EDGE. INSPECT AND REPAIR IAW BOMBARDIER REO 601R-55-12-496.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 14,681 hrs · 12,007 cycles

AS THE THRUST LEVERS WERE ADVANCED FOR TAKEOFF, THE L REV UNLOCK CAUTION MESSAGE ILLUMINATED. THE FLIGHT CREW ELECTED TO ABORT THE TAKEOFF AND PULL OFF THE RUNWAY. THIS ACFT HAD A PREVIOUSLY DEFERRED LT THRUST REVERSER. DUE TO THE MEL REQUIREMENT TO REMOVE AND STOW THE CONNECTORS FROM THE POWER DRIVE UNIT, THE ILLUMINATION OF THE REV UNLOCK MESSAGE IS A COMMON OCCURRENCE. MX VERIFIED THAT THE THRUST REVERSER WAS PROPERLY DEFERRED INCLUDING THE INSTALLATION OF LOCKING PINS, AND THE ACFT WAS RELEASED FOR SERVICE.

Part: ACM — SEIZED (LEFT) · airframe 13,436 hrs · 10,834 cycles

FLIGHT 3785 PWM/MSP AT THE GATE CREW RECEIVED LT ACM (AIR CYCLE MACHINE) OVERTEMP CAUTION AND SMOKE INTO COCKPIT. LT ACM DEFERRED PER MEL 21-51-11. AIRCRAFT INSPECTED IN MSP AND FOUND THE LT ACM SEIZED. ACM REMOVED AND REPLACED PER BOMBARDIER AMM WITH OPERATIONAL CHECK PERFORMED WITH NO DEFECTS.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 12,498 hrs · 9,975 cycles

FLIGHT 2994 - AFTER TRANSFERRING BLEEDS TO THE APU DURING BOARDING PROCESS FO NOTICED SMOKE IN COCKPIT AND CABIN. AIRCRAFT DEPLANED AND SHUTDOWN, NO FIRE OR SMOKE FOUND BY FIRE PERSONNEL. NO DEFECTS FOUND BY CONTRACT MAINTENANCE, AIRCRAFT FERRIED TO DTW. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED OPERATIONAL CHECKS OF APU AND BLEED SYSTEM WITH NO DEFECTS FOUND.

Part: FLAP SYSTEM — OUT OF RIG

FLAPS FAILED ON APPROACH WHEN SELECTED TO 30 DEGREES. VREF ADJUSTED AND APPROACH CONTINUED WITH UNEVENTFUL LANDING. RESET FLAPS AND PERFORMED RIG CHECK PER BOMBARDIER AMM. OPS CHECKED GOOD.

Part: FLAP SYSTEM — OUT OF RIG

FLAPS FAILED ON APPROACH WHEN SELECTED TO 30 DEGREES. VREF ADJUSTED AND APPROACH CONTINUED WITH UNEVENTFUL LANDING. RESET FLAPS AND PERFORMED RIG CHECK PER BOMBARDIER AMM. OPS CHECKED GOOD.

Part: ECU — FAILED (TE FLAP)

FLAPS FAILED AT ZERO WHEN SELECTED TO 8 DEGREES. QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY AN UNEVENTFUL LANDING. FLAP SYSTEM TROUBLESHOOTING PERFORMED PER BOMBARDIER FIM AND AMM PULLED CODES FROM FLAP ELECTRON CONTROL UNIT FECU. PER FIM CODES SHOWED FAILED FECU. FECU REPLACED PER BOMBARDIER AMM SYSTEM. OPS TESTED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG)

GEAR DISAGREE MESSAGE (NOSE NOT DOWN AND LOCKED) ON APPROACH, QRH FOLLOWED GEAR LOCKED DOWN. EMERGENCY DECLARED WITH UNEVENTFUL LANDING. TROUBLESHOT SYSTEM IAW MM, GEAR SWINGS PERFORMED WITH NO DEFECTS FOUND. (S)

Part: IDG — FAILED (NR 2)

ON CLIMBOUT RECEIVED NR 2 IDG FAILED, APU FAILED TO START QRH FOLLOWED DECLARED EMERGENCY RETURNED TO FIELD WITH UNEVENTFUL LANDING. OUTSTATION MAINTENANCE PERFORMED OPERATIONAL CHECKS FOR BOTH THE NR 2 IDG AND THE APU PER BOMBARDIER MAINTENANCE MANUAL AND RETURNED ACFT TO SERVICE. APU PART NUMBER 3800488-3 TSN 6881 CSN 13944 TSI 2047 CSI 3897. (S)

Part: A/C PACK — CONTAMINATED · airframe 7,659 hrs · 6,093 cycles

AFTER TAKEOFF GOT SMOKE IN CABIN. FOLLOWED QRH AND RETURNED TO AIRPORT. SYSTEM TESTED AND FOUND TO RESIDUAL DE-ICE FLUID IN ECS PACKS. HIGH POWER ENGINE RUNS OPERATIONAL CHECK GOOD.

Part: SCAVENGE PUMP — FAILED (RT ENGINE) · airframe 4,076 hrs · 3,219 cycles

EN ROUTE TO DTW FROM GSP THE RT ENGINE MASTER WARNING ILLUMINATED FOLLOWED BY THE FLUCTUATION OF THE OIL PRESSURE GAUGE. THE FLIGHT CREW EXECUTED THE QRH AND SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY. ATC CLEARED THEM DIRECT TO AVL WHERE AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WERE MADE. MAINTENANCE FOUND THAT THE ENGINE LUBE AND SCAVENGE PUMP WAS DEFECTIVE. THE PUMP WAS REPLACED AND GROUND RUNS SUCCESSFULLY COMPLETED. THE AIRCRAFT WAS RELEASED FOR FLIGHT.