N8458A

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 29,582 hrs · 26,812 cycles

EMERGENCY LIGHTING ON THE FLOOR ROWS 1 -5 INOPERATIVE. RESEATING FLOOR TRACK CONNECTOR OF EMER LIGHTS, ALL LIGHTS WORK. EMER LIGHTING SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-01. ACFT IS OK FOR SERVICE.

Part: CABLE — DEFECTIVE (CABIN) · airframe 29,554 hrs · 26,782 cycles

EMER FLOOR LIGHTING INOPERATIVE BETWEEN ROWS 2 & 6. R & R EMER FLOOR LIGHT CABLE FOR FWD SECTION IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,544 hrs · 26,773 cycles

CAPTAIN`S COCKPIT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT BATTERY FOR CAPTAIN`S SIDE. OPERATIONS CHECKED GOOD IAW AMM 25-61-02.

Part: STRUT — DEFECTIVE (NLG) · airframe 28,569 hrs · 25,829 cycles

GEAR DISAGREE ON DEPARTURE FROM ATL. AFTER THE LG WAS SELECTED IN THE UP THE FOLLOW MESSAGES APPEARED WITHIN 10 SECONDS, GEAR DISAGREE WARNING NLG DOOR OPEN WARNING NWS INOPERATIVE, CAUTION WOW, INPUT CAUTION WOW, OUTPUT STATUS. SERVICED NOSE GEAR IAW AMM 12-12-32. UPON JACK UP THE NOSE WE FOUND THE NOSE GEAR WOULD NOT CTR & RETAINING COLLAR LOOSE. WITH WEIGHT OFF WHEELS IF YOU TRY TO TURN THE NOSE WHEEL BY HAND RETAINING COLLAR WOULD TURN WITH IT. R & R PISTON & AXLE QUICK CHANGE KIT IAW AMM 32-21-30, LEAK & OPERATIONS CHECKED GOOD.

Part: MOTOR — INOPERATIVE (PAX DOOR) · airframe 28,505 hrs · 25,765 cycles

FORWARD PAX DOOR INOPERATIVE. R & R PAX DOOR ASSIST MOTOR IAW AMM 52-11-08, OPERATIONS CHECKED GOOD. THIS CLEARS DM 1870, PLACARD REMOVED & REMOVED FROM DMR.

Part: BATTERY — UNKNOWN (CABIN) · airframe 28,475 hrs · 25,732 cycles

EMERGENCY LIGHT BATTERY. R & R NR 4 EMERGENCY BATTERY IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 27,904 hrs · 25,170 cycles

REAR PRESSURE BULKHEAD HAS SCREW MARKS 0.003" -0.006" DEEP. REPAIRED IAW REO 601R-53-61-2155.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,904 hrs · 25,170 cycles

BS 621 BULKHEAD IS CRACKED AROUND THE LINTEL FITTING LT SIDE AT WL 107.17. REPAIRED IAW REO 601R-53-61-1230.

Part: FITTING — GOUGED (RT MLG) · airframe 27,904 hrs · 25,170 cycles

RT MLG SIDE BRACE FITTING IS GOUGED ON AFT FACE 2 INCHES OTBD OF AFT BUSHING. REPAIRED IAW REO 601R-57-21-2001.

Part: FITTING — GOUGED (RT MLG) · airframe 27,904 hrs · 25,170 cycles

RT MLG SIDE BRACE FITTING ANTI-ROTATION TANG IS GOUGED. REPAIRED IAW REO 601R-57-21-2001.

Part: TILLER — MALFUNCTIONED (NLG STEERING) · airframe 27,778 hrs · 25,048 cycles

NOSE WHEEL STEERING TILLER WILL NOT CENTER. R & R NOSE WHEEL STEERING TILLER IAW AMM 32-50-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,564 hrs · 24,829 cycles

MODERATELY STRONG BURNING RUBBER ODOR IN COCKPIT, 30 MINUTES AFTER BLOCK OUT. COFFEEMAKER TURNED OFF. ODOR RETURNED APPROX 15 MINUTES LATER. NO SMOKE. COMPLIED WITH INSPECTION OF COCKPIT, AFT EQUIPMENT BAY, & AVIONICS BAY. NO DEFECTS NOTED. COMPLIED WITH MINIMUM WORKSCOPE FOR SMOKE/FUMES IN CABIN/FLIGHT DECK. UNABLE TO DUPLICATE DISCREPANCY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,522 hrs · 24,780 cycles

EMERGENCY FLOOR PATH LIGHT THIRD FWD FROM THE AFT END INOPERATIVE.

Part: SHUTOFF VALVE — FAILED (APU BLEED) · airframe 27,457 hrs · 24,717 cycles

"CABIN ALT MESSAGE "LEFT 10TH SOV ARMED BUT NEVER OPENED, LT PACK NEVER CAME ON, DUE TO RT PACK DEFER, ACFT NEVER PRESSURIZED TRIED MULTIPLE RECYCLES, LT 10TH SOV REMAINED ARMED. RAN QRH LT 10TH REMAIN ARMED. TOOKOFF WITH APU ON BLEEDS ON APU. PROBLEM OCCURRED WHEN THE BLEED TRANSFER FROM APU ENGINE. CABIN ALT NEVER GOT ABOVE 9500. OVERWEIGHT LANDING DUE TO UNPRESSURIZED ACFT AIR RETURN. WEIGHT 48050 RATE OF DECENT, 300FPM REPLACEMED LT 10TH STAGE SOV.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,351 hrs · 24,605 cycles

EMERGENCY LIGHT FLOOR TRACK LIGHTING TORN UP FROM ROW 11&12. REINSTALLED FLOOR TRACK LIGHTING. OPS CHECK GOOD. REFERANCE AMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 27,266 hrs · 24,509 cycles

EMERGENCY LIGHT STRIP MISSING AT SEATS 12 C/D. REPLACED MISSING EMERGENCY LIGHT STRIP AT SEAT 12 C/D IAW AMM 33-50-01. OPERATIONS CHECK GOOD.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 27,135 hrs · 24,380 cycles

AC GROUND AIR SERVICE BACKING PLATE CHAFED AND GOUGED. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,135 hrs · 24,380 cycles

FUSELAGE SKIN AT FS 509+8 BETWEEN S-14L AND S-15L DENTED. REPAIRED IAW SRM 53-00-31 FIGURE 204 REPAIR 1.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 27,106 hrs · 24,352 cycles

NOSEWHEEL STEERING PULLS HEAVILY TO THE RIGHT. NOSE WHEEL INOPERABLE CAUTION CAME ON AS WE SELECTED GEAR UP. RAN QRH NO FURTHER PROBLEMS. TAXIED AIRCRAFT NO DISCREPANCIES NOTED AT THIS TIME. OK FOR SERVICE IAW AMM 32-51-00.

Part: TIRE — WORN (NLG) · airframe 27,100 hrs · 24,346 cycles

NOSE WHEEL STEERING LOOSE / VAGUE WANDERS DURING TAXI & TAKEOFF ROLL. INSPECTED NOSE LANDING GEAR AND TIRES, FOUND TIRE PRESSURE UNEVEN AND BOTH TIRES CLOSE TO WEAR LIMITS. REMOVED AND REPAIRED LEFT & RIGHT NOSE TIRES IAW AMM 32-41-01. (TIRE PRESSURE AT 175 PSI)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,923 hrs · 24,167 cycles

FLIGHT ATTENDANT FLASHLIGHT OUT OF SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IN WARDROBE PER AMM 25-60-00. BATTERY EXPIRATION DATE 5/24/2016.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,685 hrs · 23,933 cycles

ORANGE SECTION OF IN-FLOOR EN ROUTE LIGHTING ABEAM THE EXIT ROW IS INOPERABLE. REMOVED AND REPLACED ORANGE SECTION OF EMERGENCY FLOOR STRIP LIGHT AT EXIT ROW. OPS CHECKS GOOD IAW CRJ AMM 33-51-01.

Part: COVER — MISSING (CABIN) · airframe 26,310 hrs · 23,551 cycles

EXIT COVER AT THE TOP OF MAIN CABIN DOOR MISSING. REMOVED AND REPLACED EMERGENCY EXIT FLOOR FLOOD LIGHT ASSEMBLY IAW AMM 33-51-19. OPS CHECK GOOD, OK FOR SERVICE.

Part: YOKE — UNKNOWN (CONTROL COLUMN) · airframe 25,815 hrs · 23,065 cycles

CAPTAIN'S SIDE YOKE FEELS LIKE CONTROL CABLE SLIPPING WHEN BANKING LEFT AND RIGHT. COMPLIED WITH PA 27-066D.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 25,609 hrs · 22,866 cycles

CAPTAIN'S LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED CAPTIAN`S LIFE VEST IAW AMM 25-61-03.

Part: STRUT — LACK OF LUBE (NLG) · airframe 25,312 hrs · 22,570 cycles

UPON GEAR RETRACTION GEAR DISAGREE WARNING MSG NOSE GEAR INDICATION DOWN NOSE DR WARNING ALSO QRH COMPLETE GEAR DN AND LOCKED. SVC NLG STRUT FLUID AND N2 IAW AMM 12-12-32 REF AML PAGE 2155457. COMPLIED WITH OPS CHECK IAW AMM 32-30-00. OPS CHECKS GOOD REF AML 2155458.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 25,310 hrs · 22,567 cycles

RIGHT SEAT TRACK AT FS 559+16 GOUGED. REPAIRED IAW SRM 53-21-49.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,225 hrs · 22,482 cycles

BOTH FORWARD FUSELAGE EMER LIGHTS INOP. CLEANED LAMP SOCKETS IAW CRJ 200 AMM 51-0-00 AND RELAMPED IAW AMM 33-51-21, OP CHECKS GOOD, OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,006 hrs · 22,272 cycles

ABORTED TAKEOFF FOR ELT MSG ON. OPC ELT IAW AMM 25-62-00. OPC GOOD, A/C OK FOR SVC.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 24,699 hrs · 22,038 cycles

HYD 3 LO PRESS CAUTION MSG IN FLIGHT; 0 PERCENT HYDRAULIC FLUID INDICATION. EMERGENCY DECLARED. FOUND LOOSE LINE ON 3B HYD PUMP. TIGHTENED LINE & OP/C CHECKS NORMAL & LEAKS CHECKS GOOD. FOUND HYD LEAKING WHICH WAS CAUSED BY A DAMAGED O-RING. REMOVED AND REPLACED O-RING. SERVICED HYD SYSTEM NR 3A IAW AMM 12-12-29. PERFORMED OPS CHECK. NO LEAK FOUND. A/C OK FOR RETURN TO SVC.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,696 hrs · 22,035 cycles

F/A FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY, OPC GOOD IAW CRJ AMM 25-61-00. VERIFIED PART EFFECTIVITY.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,620 hrs · 21,966 cycles

LT OBLIQUE ANGLE AT FS 526 IS CRACKED. REPAIRED IAW SRM 51-24-21, 51-40-11, 51-42-06.

Part: SKIN — CHAFED (TE FLAP) · airframe 24,620 hrs · 21,966 cycles

FLAP S/N SB/RJ/478. THE INBD AND OTBD FLAP VANE CARRIAGES BONDING JUMPER HAVE CHAFED THE INNER FLAP SKIN. REPAIRED IAW BOMBARDIER REO 601R-57-52-1805.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 24,620 hrs · 21,966 cycles

CHAFING DAMAGE ON VERTICAL STIFFENER ON AFT SIDE OF FS 621 BL 0 FROM CONTACT WITH 10TH STAGE ISO VALVE. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,462 hrs · 21,752 cycles

CAPT'S EMERGENCY FLASHLIGHT FAILS RED LED TEST. REMOVED AND REPLACED CAPTAIN'S EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD IAW AMM 25-61-00. VERIFIED PARTS EFFECTIVITY.

Part: YAW DAMPER — FAULTY (RUDDER) · airframe 24,451 hrs · 21,742 cycles

YAW DAMPNER MOVES RUDDER IN FLIGHT. REMOVED AND REPLACED NR 1 YD ACTUATOR IAW CRJ AMM 22-22-01, OP CHECK GOOD OK FOR SERVICE. REPEAT FROM 9/19/11.

Part: YAW DAMPER — FAULTY (RUDDER) · airframe 24,446 hrs · 21,737 cycles

CREW REPORTED YAW DAMPER WAS KICKING THE RUDDER THE ENTIRE FLIGHT. CREW DID NOT DECLARE EMERGENCY.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI ICE SYS) · airframe 23,915 hrs · 21,236 cycles

A/I DUCT WARNING ABORTED TAKEOFF. REMOVED AND REPLACED ANTI ICE TEMP CONTROL UNIT IN REF AMM 30-12-19. PART VERIFIED EFFECTIVELY.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 23,305 hrs · 20,664 cycles

ON TAKEOFF ROLL FROM KMCI THE FLIGHT CREW HEARD A LOUD NOISE FROM THE RIGHT ENGINE FOLLOWED BY HIGH ITT INDICATION AND ENGINE SHUTDOWN. THE FLIGHT CREW ABORTED THE TAKEOFF. AFTER INSPECTION OF THE AIRCRAFT BY CFR THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED THE ENGINE AND FOUND METAL PARTICLES IN THE TAIL PIPE. THE CAUSE OF THE FAILURE IS STILL UNDER INVESTIGATION. THE AIRCRAFT WAS GROUNDED AND THE ENGINE WILL BE CHANGED TONIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,169 hrs · 20,537 cycles

FS 559.00 BULKHEAD WEB FOUND CRACKED AND REQUIRES REPAIR.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,169 hrs · 20,537 cycles

FS 559.00 BULKHEAD WEB FOUND CRACKED AND REQUIRES REPAIR.

Part: FLAP — FAILED (WING) · airframe 20,117 hrs · 17,654 cycles

FLAPS FAILED AT ZERO IN CRUISE. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH H6I PER AMOC DATED MARCH 27 AND PA AD27-052C. REMOVED AND REPLACED FLAP PDU PER AMM 27-50-00.

Part: FLAP — FAILED (WING) · airframe 20,106 hrs · 17,642 cycles

FLAP FAIL AT ZERO IN CRUISE. RESET AND DEFERRED PER MEL 27-50-00.

Part: ECU — FAILED (TE FLAP) · airframe 20,085 hrs · 17,614 cycles

FLAPS FAIL IN FLIGHT FLAPS AT ZERO. TROUBLESHOOTING PER BOMB FIM REV 39 IAW AD 2009-06-12 PARA H6I PER AMOC DATED 3-27-09. REMOVED AND REPLACED FECU IAW AMM 27-51-05, OPS CHECK GOOD. THIS CLEARS DM 4953, PLACARD REMOVED.

Part: ECU — FAILED (TE FLAP) · airframe 19,968 hrs · 17,511 cycles

ON CLIMBOUT RECEIVED "FLAP FAILURE" MESSAGE, QRH FOLLOWED, RETURNED TO MEMPHIS. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE FLAP ELECTRONIC CONTROL UNIT (FECU) FAILED. FECU REPLACED PER BOMBARDIER AMM, OPERATIONAL CHECK PERFORMED, NO DEFECTS NOTED.

Part: FCU — MALFUNCTIONED (TE FLAPS)

RECEIVED FLAPS DEGRADED MSG AT FL 26000 AT 310 KNOTS, FLAPS MOVED UNCOMMANDED TO 8 DEGREES SEVERAL TIMES. QRH FOLLOWED WITH AN UNEVENTFUL ZERO FLAPS LANDING. SYSTEM INTERROGATED PER FIM FECU CODES PULLED. FECU SHOWED INTERNAL FAILURE. FECU R&R PER BOMBARDIER AMM. OPS CHECKS PERFORMED.

Part: IDG — MALFUNCTIONED (NR 2)

ON CLIMBOUT OF KDSM, IDG2 CAUTION MESSAGE ILLUMINATED, FOLLOWED ONE MINUTE LATER BY THE GEN 2 CAUTION MESSAGE. THE FLIGHT CREW PERFORMED THE QRH AND REQUESTED TO LAND AT MSP. PERMISSION WAS GRANTED TO DIVERT TO KMSP. EN ROUTE TO KMSP THE APU OIL TEMP CAUTION ILLUMINATED. DUE TO THE FACT THE AIRCRAFT WAS DOWN TO TWO GENERATORS AND HAD AN APU OIL TEMP CAUTION, THE FLIGHT CREW DECLARED AN EMERGENCY AND REQUESTED CFR ASSISTANCE. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMSP. THE F/O SECURED THE APU ON LANDING ROLL OUT. MAINTENANCE REPLACED IDG 2 AND FOUND THE APU OIL LEVEL LOW. THE APU OIL WAS SERVICED AND THE ACFT WAS GROUND RUN AND RELEASED FOR SERVICE. (S)

Part: COUPLING — LEAKING (BLEED VALVE) · airframe 17,397 hrs · 15,257 cycles

ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AURAL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT WAS RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AND THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRAFT.

Part: COUPLING — LEAKING (BLEED VALVE) · airframe 17,397 hrs · 15,257 cycles

ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AURAL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT WAS RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AND THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRAFT.

Part: COUPLING — LEAKING (BLEED AIR) · airframe 17,397 hrs · 15,257 cycles

ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AURAL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT WAS RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AND THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRAFT.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS)

FLAPS FAIL MESSAGE ON TAXI OUT. COMPLIED WITH AD2006-12-21, NO DISCREPANCIES NOTED. MONITORING FLAPS FOR 72 HOURS.

Part: FLAP SYSTEM — FAILED · airframe 13,175 hrs · 11,711 cycles

FLAPS FAIL AT 20 DEGREES ON TAXI. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,340 hrs · 10,977 cycles

ON APPROACH INTO DTW, FLAP FAILED AT 20. COMPLETED QRH PROCEDURES AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE COMPLIED WITH AD98-20-01 AND RELEASED AIRCRAFT.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,754 hrs · 10,483 cycles

FLAP FAIL MESSAGE DURING DEICING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

(REF NR: 05-088) NOSE GEAR WAS NOT DOWN AND LOCKED WITH THE LANDING GEAR SELECTOR IN THE DOWN POSITION, ON APPROACH. THE CREW RECYCLED THE GEAR UP AND DOWN. LANDING GEAR CAME DOWN NORMALLY ON SECOND ATTEMPT. QRH FOLLOWED, LANDING UNEVENTFUL. PERFORMED GEAR SWING IAW AMM. OPS CHECK GOOD. (K)

Part: FLAP — MALFUNCTIONED (WING)

FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0 FLAP LANDING WAS PERFORMED. SYSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD. (M)