N8913A

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 26,284 hrs · 23,792 cycles

OBSERVER O2 MASK MIC INOP. DEFERRED OBSERVERS 02 SYSTEM IAW MEL 35-10-01. PLACARD INSTALLED. R&R OBSERVERS MASK IAW AMM 35-11-12. OPS CHECK GOOD. THIS CLEARS MEL 3319197-2. MM02 UPDATED PLACARD REMOVED MOC 96045 NOTIFIED.

Part: PBE — DAMAGED · airframe 25,592 hrs · 23,104 cycles

ALL THREE PBES PUNCTURED AND SOFT. REPLACED THE COCKPIT, WARDROBE AND AFT CABIN PBES IAW J/C EE-200

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,751 hrs · 22,242 cycles

LEFT FUSELAGE AFT EXTERNAL EMER LIGHT INOPERATIVE. DEFERRED LT FUSELAGE AFT EXTERNAL EMER LIGHT IAW MEL 33-51-22. PLACARD INSTALLED & MM02 UPDATED. REPLACED EMER BATTERY PACK CHARGER 4 IAW AMM 33-51-05. OPERATIONS CHECKED GOOD, PN BA5-0933-901. SN OFF C00494 SN ON C01693. THIS CLEARS CONTROL 3284252-1. REMOVED FROM MEL 33-51-22. VERIFIED PARTS EFFECTIVITY.

Part: WIRE — BROKEN (CABIN) · airframe 24,486 hrs · 21,992 cycles

CABIN EMER LIGHT AT FS 424.00, BROKEN WIRE RT OVERWING FLOOR LIGHT. REPAIRED BROKEN WIRE FOR CABIN EMER LIGHT AT FS 424.00 IAW ESPM 20-11-00.

Part: MOUNT BRACKET — CORRODED (CABIN) · airframe 24,486 hrs · 21,992 cycles

CABIN CEILING EMER LIGHT AT FS 409+96, WIRE TERMINAL, LUGS ATTACHING HARDWARE & MOUNTING BRACKET IS CORRODED. REMOVED & REINSTALLED THE EMER CEILING NR 2 FLOODLIGHT IAW AMM 33-51-16-000-400-801.

Part: WIRE — BROKEN (CABIN) · airframe 24,486 hrs · 21,992 cycles

FLOOR TRACK LIGHTING CONNECTOR AT LAVATORY DOOR HAS BROKEN WIRES. R & R FLOOR TRACK LIGHTING CONNECTOR P40LY & INSTALLED NEW SPLICES IAW EPSM 20-17-31 & WDM 33-51-00.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,486 hrs · 21,992 cycles

FORWARD FIRST 2 CONNECTORS ON LIGHT TRACK ARE BROKEN. R & R EMER FLOOR TRACK LIGHT CONNECTORS FOR FIRST 2 FWD LIGHTS IAW ESPM 20-16-00.

Part: POST — DAMAGED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

FS 409+128, RBL 18 INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX .250 INCHES LONG BY GREATER THEN 50% FSH. FAILED NDT INSPECTION. R & R FS 409+128, RBL 18 INBD VERTICAL POST. REF STEPS 1 - 4 FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

INDICATION NOTED AT LBL 27.50, 621 REAR PRESS BULKHEAD WL 130 AT CARGO DOOR TRACK, APPROX 1.00 INCH LONG, 100% FULL SCREEN HEIGHT, FAILED NDT. CONTINUATION JC 8791315 OP 70 - REPAIRED 621 BULKHEAD AT LBL 27.50, WL 130 IAW REO:601R-53-61-5613 REV DATED 12 22 15 & REO 601R-53-61-1541 REV E DATED 11 12 14. THIS IS A MAJOR REPAIR, SEE JC 8791315 OP 48 FOR STEPS 1 - 6.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

RIGHT FWD FUSELAGE ACFT POWER RECP STRUCTURE CRACKED. CONTINUATION CARD 8791311 OP 113. REPAIRED FWD FUSELAGE ACFT POWER RECP STRUCTURE. REF STEPS 1 - 5 FOR WORK PERFORMED JOB 8791311 OP 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

LEFT SEAT RAIL AT LBL 45, HAS PITTING & SURFACE CORROSION IN MULTIPLE LOCATIONS, BETWEEN FS 364 TO FS 559+80. R & R LT SIDE SEAT RAIL FROM FS 364 TO 559+80, REF STEPS 1 - 3 FOR WORK PERFORMED.

Part: SUPPORT — BROKEN (LT COWLING) · airframe 24,486 hrs · 21,992 cycles

LEFT ENG NOSE COWL INLET, HAS A BROKEN SUPPORT ASSEMBLY THAT HOLDS THE BROWN WIRE ASSEMBLY. LOCATED AT THE 1 O'CLOCK POSITION. REPAIRED LT ENG NOSE COWL INLET SUPPORT BRACKET ASSEMBLY IAW REO 601R-71-613941 REV A DATED 04 27 10. "

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 24,486 hrs · 21,992 cycles

SERVICE DOOR STEP PLATE IS CORRODED. LOCATED & DRILLED NEW SERVICEABLE SERVICE DOOR STEP PLATE IAW SRM 51-40-11. INSTALLED 6 EACH NEW NUTPLATES ON STEP PLATE IAW SRM 51-42-06.

Part: POST — DAMAGED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

FS 409+128, LBL 18 OTBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250 INCHES LONG BY GREATER THAN 50% FSH. FAILED NDT INSPECTION. R & R FS 409+128, LBL 18, OTBD POST IAW SRM 51-42- 06 & REO 601R-53-41-889. "

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

FS 280, STRINGER 3L, FWD UPPER ATTACH ANGLE CRACKED, 3 INCHES LONG JUST AFT OF FS 280M BULKHEAD. REMOVED CRACKED ANGLE & INSTALLED NEW SERVICEABLE ANGLE AT STRINGER 3L, FS 280.00 IAW SRM 51-42-06 & 51-42-21.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

SEVEN EACH CARGO FLOOR RAIL SEGMENTS ARE CORRODED, 1 EA AT LBL 27, BETWEEN FS 559+80 TO FS 559+96, 3 EA AT LBL 9, BETWEEN FS 559+80 TO FS 621, 2 EA AT RBL 9 FOR FS 559+80 TO FS 570 & 1 EA AT RBL 27 FROM FS 559+80 TO FS 559+96. R & R 7 EA TRACK SEGMENTS IN THE CARGO FLOOR AREA IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: POST — DAMAGED (FUSELAGE) · airframe 24,486 hrs · 21,992 cycles

FS 409+128, BL0 INBD & OTBD SIDES, VERTICAL POST HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. BOTH APPROX .250 INCHES BY 50% FSH. BOTH FAILED NDT INSPECTION. R & R 409+128, BL0 INBD & OTBD POSTS IAW SRM 51-42-06 & REO 601R-5-41-889. "

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,486 hrs · 21,992 cycles

PASSENGER DOOR AFT DRAG ANGLE HAS VISUAL INDICATION OF CRACK NEAR ASSIST CABLE PULLEY BRACKET. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-51 REV B DATED 07 05 15. "

Part: COVER — TORN (LIFE VEST) · airframe 24,386 hrs · 21,894 cycles

FIRST OFFICERS LIFE VEST CONTAINER COVER IS TORN. R & R FIRST OFFICERS LIFE VEST CONTAINER COVER IAW CMM 25-14-10.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,271 hrs · 21,785 cycles

EMERGENCY LIGHTS COME ON FOR A FEW SECONDS, THEN GO OUT. FLIGHT ATTENDANT FOUND SWITCH ON HER PANEL LEFT ON. R & R BATTERY PACKS 1, 2, 3 &4 IAW AMM 33-51-04. OPERATIONS TESTED GOOD. REFERENCE LOG PAGE 3200871-2 FOR CORRECTIVE ACTION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,183 hrs · 21,697 cycles

AFT FLOOR EMER LIGHT STRIPS 9 - 12 INOPERATIVE. R & R NR 4 BATTERY CHARGER ASSEMBLY IAW AMM 33-51-05. OPERATIONS CHECKED GOOD.

Part: GASKET — WORN (ESCAPE HATCH) · airframe 24,131 hrs · 21,646 cycles

CREW ESCAPE HATCH LEAKING, LARGE PUDDLE OF WATER ON COCKPIT ENTRANCE FLOOR. FOUND GASKET FOR OUTER HANDLE ASSEMBLY WORN & LEAKING. REPLACED OUTER HANDLE ASSEMBLY WHICH INCLUDED NEW GASKET IAW CMM 52-22-03. OPERATIONAL TEST OF CREW ESCAPE HATCH LATCH ASSEMBLY GOOD. LEAK CHECKED GOOD AT THIS TIME.

Part: LIFE VEST — WRONG PART (COCKPIT) · airframe 23,838 hrs · 21,347 cycles

CAPTAIN'S LIFE VEST WRONG TYPE, SHOULD BE ORANGE CURE VESTS PN P0723E105PWC. R & R CREW LIFE VEST IAW AMM 25-61-03.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 23,738 hrs · 21,234 cycles

FLAPS FAIL CAUTION MSGS CAME ON WHILE SELECTING FLAPS 0 TO 20 DEG AT EXTENSION 3000 FT MSL. OUTSIDE TEMP, TAT 07 DEG, CLEAR SKY. CURRENT SPEED AT SELECTION 185 KTS, TIME WAS APPROX 1 HR INTO FLIGHT, 6:52 LOCAL, FOLLOW QRH LANDING WEIGHT 43000. PERFORMED TROUBLESHOOTING IAW FIM REV 48 IAW AD-2009-06-12 PARAGRAPH H 6 I, AMOC LOG 14-15 DATED 12 30 2014 & TS 001100R1 FIM TECHNICAL SUPPLEMENT. R & R LT BPSU IAW AMM 27-51-10. ALL OPERATIONAL & FUNCTIONAL CHECKS, CHECKED GOOD. FAULT CODES FROM FECU, 5-1B, 5-2B, 12-1A & 12-2A.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 23,735 hrs · 21,228 cycles

FLAPS FAIL, FLAPS 0 LANDING, LIGHT CAME ON 195 KTS, 2500 FEET. FLAPS FAILED TRYING TO SET 20 DEG. REF FLAP FAIL EVENT ON AML 3222764. LT & RT FLAP BPSUS REQUIRED RIGGING IAW AMM 27-51-10. PERFORM OPERATIONAL TEST OF FLAPS IAW TASK 27-54-00-710-801. IAW FIM 27-50-00 CHECKED WIRING TO LT BPSCU & FECU, CHECKED GOOD. R & R FECU IAW AMM 27-51-05 IAW FIM 27-50-00 FIG 107 ITEM 3. ALL OPERATIONAL & FUNCTIONAL CHECKS CHECKED GOOD. SEE NON-ROUTINE WC N78188 FOR WORK DETAILS. ACFT CHECKED OK AT THIS TIME IAW TO AML 3222764 FOR STANDALONE SIGNOFF. PERFORMED TROUBLESHOOTING IAW FIM REV 48 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC LOG 14-105 DATED 12 30 2014 & TROUBLESHOOTING 001100R1 FIM TECHNICAL SUPPLEMENT. R & R FECU IAW FIM 27-50-00 IAW AMM 27-51-05, ALSO SHOT WIRES TO FECU & LT BPSU WIRES CHECKED GOOD. FECU CODES 5-1B, 5-2B, 12-1A, 12-2A, 25-BC & 33-BC. RIGGED LT & RT FLAP BPSUS IAW AMM 27-51-10-830-801. BOTH BPSUS READ 0.00 WITH FLAPS SET TO ZERO. ACCOMPLISHED OPERATIONAL TEST OF FLAP SYS IAW AMM 27-54-00. FLAPS OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 23,381 hrs · 20,862 cycles

FLIGHT ATTENDANT FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK IAW AMM 25-61-01. OPERATIONS CHECKED GOOD.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 23,206 hrs · 20,689 cycles

DENTS FOUND ON RT VERTICAL STABILIZER SKIN. FOUND TO BE WITHIN LIMITS IAW SRM 55-00-31. REPAIRED IAW EA 255-03171.

Part: WATER SEPARATOR — FAULTY (AC BAY) · airframe 22,820 hrs · 20,305 cycles

STRONG SMELL OF FUEL IN CABIN & COCKPIT. R & R WATER SEPARATOR IAW AMM 21-51-13. SMELL PURSUIT WITH APU BLEED ONLY NOT ON ENG BLEED. DEFERRED APU IAW MEL 45-10-11. PLACARD INSTALLED.

Part: SMOKE GOGGLES — UNSERVICEABLE (COCKPIT) · airframe 22,676 hrs · 20,156 cycles

FIRST OFFICERS SMOKE GOGGLES TRIM NOT SEALED TO PLASTIC. R & R SMOKE GOGGLES AS REQUIRED.

Part: PIN — DIRTY (PAX DOOR) · airframe 22,378 hrs · 19,844 cycles

BOARDING DOOR HANDLE DIFFICULT TO OPEN & CLOSE. CLEANED & LUBED LATCH PINS & CAM ROLLERS IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,363 hrs · 19,831 cycles

CAPTAIN`S EMER FLASHLIGHT NO BLINKING RED LIGHT. R & R CAPTAIN'S FLASHLIGHT BATTERY IAW AMM 25-61-00, OK FOR SERVICE.

Part: PIN — DIRTY (EMERGENCY EXIT) · airframe 22,345 hrs · 19,810 cycles

LEFT & RIGHT OVERWING EMER EXIT FAILED FUNCTIONAL TEST. CLEANED LATCH PINS & RECEPTACLES IAW AMM 51-26-00-110-801. LUBRICATED LATCH PINS IAW TASK CARD 000-12-800-881. ADJUSTED AFT LATCH PIN IAW CMM 52-21-02. PERFORMED OPERATIONS CHECK IAW AMM 52-21-00-710-801, NO DEFECTS NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,323 hrs · 19,790 cycles

MAINTENANCE FOUND MULTIPLE NICKS, GOUGES & DENTS BETWEEN FS 584 - 600 & STRINGER 21R - 26R. REPAIRED IAW EA CRJ253-02569.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 22,323 hrs · 19,790 cycles

FS 280 WEB CRACKED OTBD RBL 9 & LBL 9 & AFT UPPER ANGLE CRACKED OTBD OF RBL 9. FWD ANGLE FOUND CORRODED. REPAIRED IAW REOS 601R-53-11-171, 601R-53-11-136 & 601R-53-21-2537.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,185 hrs · 19,656 cycles

CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW AMM 245-61-03.

Part: CABLE — BROKEN (CABIN DOOR) · airframe 21,846 hrs · 19,310 cycles

WHILE CLOSING THE MAIN CABIN DOOR ONE OF THE CABLES BROKE WHEN THE DOOR WAS ABOUT 3 FEET OFF THE FOUND. THE DOOR THEN DROPPED BACK TO GND. APPARENTLY A WAND FROM ONE OF THE RAMP AGENTS WAS LT ON THE STAIRS & JAMMED THE DOOR AS IT WAS BEING RAISED. INSPECTED DOOR FOR DAMAGE, NO DAMAGE FOUND. DEFERRED PAX DOOR ASSIST SYS IAW MEL 52-11-01.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 21,829 hrs · 19,297 cycles

MAIN CABIN DOOR IS HARD TO OPEN & CLOSE INSIDE HANDLE TAKES EXTRA EFFORT TO MOVE. LUBRICATED PAX DOOR, CHECKED GOOD IAW AMM 52-11-00, OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,852 hrs · 17,371 cycles

MID OVERWING EMERGENCY LIGHT ON LT & RT SIDE INOPERATIVE, DEFERRED. R & R NR 3 EMERGENCY BATTERY CHARGER IAW AMM 33-51-05. ALSO, R & R NR 3 EMERGENCY BATTERY IAW AMM 33-51-04-04. OPERATIONS CHECKED GOOD. THIS CLEARS DM-000092 PLACARD REMOVED.

Part: LIGHT — BROKEN (CABIN) · airframe 20,387 hrs · 17,885 cycles

EMERGENCY FLOOR LIGHT ON AFT SIDE OF WARDROBE IS BROKEN. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPERATIONS CHECK GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,297 hrs · 17,793 cycles

PILOT & FIRST OFFICER'S LIFE VEST BAGS TORN. REMOVED AND REPLACED PILOT AND FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: FLAP — DENTED (LT WING) · airframe 19,756 hrs · 17,277 cycles

LEFT INBOARD FLAP (P/N 601R14002-1, S/N SB/RJ/948) FOUND DENTED AT WS 60. REPAIRED IAW SRM 57-52-00 REPAIR 3.

Part: A/C PACK — MALFUNCTIONED · airframe 19,321 hrs · 16,833 cycles

PACKS FOG UP IN CABIN AND FLIGHT DECK WHEN TEMP SET TO COOLER TEMPS. TROUBLESHOOT PER AMM 21-51-13. OPS CHECKED GOOD.

Part: CAM — OBSTRUCTED (PAX DOOR) · airframe 19,153 hrs · 16,666 cycles

MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE, VERY DIFFICULT TO DO EITHER. REMOVED DEBRIS FROM LOCKING CAMS (BOTH SIDES UPPER). DOOR OPERATION IS NORMAL WITH NO DEFECTS IAW 52-10-00.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 19,098 hrs · 16,613 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE. APPROX ROW 2 THRU ROW 5. SECURED FLOOR TRACK LIGHTING CONNECTOR AT SEAT 5C IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BONDING JUMPER — BROKEN (PAX DOOR) · airframe 19,098 hrs · 16,613 cycles

CREW REPORTS THAT THE MAIN PASSENGER DOOR IS DIFFICULT TO OPEN AND CLOSE. NOTED BONDING JUMPER BROKEN AND PINCHING IN PASSENGER DOOR HINGE AREA. REMOVED AND REPLACED BONDING JUMPER IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,641 hrs · 16,171 cycles

F/O LIFE VEST BAG TORN. REMOVED AND REPLACED F/O VEST IAW AMM 25-61-03.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,487 hrs · 16,035 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT FORWARD EXTERIOR EMERGENCY LIGHT .OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LATCH — MISSING (ESCAPE ROPE) · airframe 18,480 hrs · 16,030 cycles

EMERGENCY ESCAPE ROPE LATCH IS MISSING ON RT EMERGENCY EXIT. INSTALLED LATCH IN REF WITH AMM 25-63-04. A/C OK FOR SVC.

Part: TERMINAL — SHORTED · airframe 17,946 hrs · 15,666 cycles

ANTI-ICE DUCT MESSAGE ON CLIMBOUT. REPOSITIONED TERMINAL LUG ON TB28WK CLEAR OF STRUCTURE IAW ESPM 20-20-00. OPS TEST OF BLEED AIR LEAK DETECTION SYSTEM AND WARNING SYSTEM WAS GOOD AT THIS TIME IAW AMM 36-21-00-710-801.

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 17,870 hrs · 15,484 cycles

"WING OVERHEAT " WARNING MSG ON CLIMBOUT WITH WING ANTI-ICE ON. MSG WENT AWAY AFTER 5 SECONDS AFTER TURNING OFF ANTI-ICE. PERFORMED OPERATIONAL TEST OF WING ANTI-ICE SYSTEM IAW AMM 30-11-00. OPS CHECKS GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (FUEL FLOW) · airframe 17,578 hrs · 15,140 cycles

RIGHT ENGINE FUEL FLOW RAPID FLUCUATION ON TAKEOFF BETWEEN 2500 PPH-2000 PPH FLUCTUATION STABALIZED AFTER 4 MIN INDICATION NORMAL THERE AFTER. PERFORMED OPS CHECK OF FUEL DISTRIBUTION IAW AMM 73-10-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,586 hrs · 13,270 cycles

RIGHT T/R UNLOCK MSG AFTER TAKEOFF. DEFERRED PER MEL 78-30-01.

Part: MODULE — FAULTY (NLG STEERING) · airframe 14,587 hrs · 12,279 cycles

NOSE WHEEL STEERING INOP MSG IN FLT. QRH COMPLIED WITH MSG RETURNED. REMOVED AND REPLACED STEERING MODULE IAW AMM 32-51-01, OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 13,098 hrs · 10,854 cycles

CRACK FOUND AT FS 202.75 WL 69.684. REPAIRED IAW REO 601R-53-11-563 AND EO 601R-53-17350.

Part: ACTUATOR — OUT OF RIG (NLG)

UPON GEAR RETRACTION A LOUD "KNOCKING" NOISE WAS HEARD, NO CAUTION OR WARNING MESSAGES RECEIVED BUT NOISE CONTINUED. FOLLOWED QRH AND DECIDED TO RETURN TO DTW, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NOSE GEAR DOOR ACTUATOR RE-RIGGED AND OPERATIONAL CHECK PERFORMED IAW BOMBARDIER AMM. (S)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 5,458 hrs · 4,353 cycles

FLAP FAIL ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.