N8721B
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
94 reports on file, 2005-05-18 – 2018-04-02.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,528 hrs · 28,231 cycles
LEFT CENTER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-21.
Part: POST — CRACKED (BS 409) · airframe 30,514 hrs · 28,216 cycles
INBD FLANGE OF VERTICAL POST AT LBL 27, BS 409+128 IS CRACKED AT BOTTOM EDGE NEAR RADIUS AND EXTENDING HALFWAY BETWEEN THE FIRST AND SECOND RIVET. REPAIRED IAW REO 601R-53-41-0056. MAJOR REPAIR.
Earlier reports · 2005–2017 · 92 reports
2017
Part: STOWAGE BOX — INOPERATIVE (CREW OXYGEN) · airframe 29,668 hrs · 27,296 cycles
OBSERVER`S OXYGEN MASK PRESS TO TEST AND RESET BUTTON, OXYGEN DOES NOT STOP AND SHUTOFF, CATS EYE STAYS TELLOW , OXYGEN KEEPS FLOWING. REPLACED THE OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15. OPS CHECKED GOOD. SERVICED THE CREW OXYGEN TO 1850 PSI IAW AMM 12-16-35.
Part: BALLAST — FAULTY (CABIN) · airframe 29,503 hrs · 27,120 cycles
BURNING SMELL AT THE BACK OF THE CABIN AT LAST ROW SEAT. FOUND POWER UNIT/DIMMER (BALLAST) BURNING REMOVED ANND REPLACED BALLAST IAW 33-21-10 OPS CHECK GOOD.
Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 29,496 hrs · 27,112 cycles
LAVATORY SMOKE DETECTOR FAILED TO TEST. R & R THE LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,473 hrs · 27,088 cycles
F/A FOUND FLASHLIGHT IN FWD CLOSET INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,467 hrs · 27,083 cycles
ON PRE-FLIGHT, F/A FOUND THE EMERGENCY FLASHLIGHT IN FWD BIN/CLOSET TO BE INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT, OPS CHECKED GOOD IAW 25-61-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,085 hrs · 26,673 cycles
DURING LC-1 CHECK, FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 10. REMOVED AND REPLACED CEILING EMERGENCY LIGHT ROW 10 BULB IAW AMM 33-51-16. OPS CHECKED GOOD.
Part: OXYGEN MASK — INOPERATIVE (FLIGHT DECK) · airframe 29,044 hrs · 26,628 cycles
FIRST OFFICER`S OXYGEN MASK HARNESS HAS A LEAK AND WILL NOT INFLATE. R & R THE OXYGEN MASK IAW AMM 35-11-12. OP CHECKED GOOD. OK FOR SERVICE.
Part: G SWITCH — INOPERATIVE (ELT) · airframe 28,847 hrs · 26,420 cycles
ELT FAILS OPS CHECK, THE G SWITCH FAILS TO OPERATE. REMOVED AND REPLACED ELT IAW AMM 25-62-01-400-801. ELT OPS CHECKED GOOD.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,835 hrs · 26,408 cycles
LEFT WING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-15. OPS CHECKED GOOD.
Part: OXYGEN MASK — LEAKING (FLIGHT DECK) · airframe 28,438 hrs · 25,990 cycles
OXGEN LEVEL LOW, 250 PSI. SUSPECT LEAK IN OBSERVER`S MASK. REMOVED AND REPLACED THE OXYGEN MASK IAW TASK 35-11-12-000-801.
Part: OXYGEN MASK — LEAKING (FLIGHT DECK) · airframe 28,427 hrs · 25,980 cycles
OBSERVERS OXYGEN MASK LEAKS. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12.
2016
Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 27,805 hrs · 25,360 cycles
CREW NOTED CAPTAIN`S OXYGEN MASK MICROPHONE INOPERATIVE. REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS / LEAK TEST GOOD. ACFT OK FOR SERVICE.
Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 27,554 hrs · 25,106 cycles
FIRST OFFICER OXYGEN MASK BROKEN THE TUBING HAS A LEAK. REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TEST GOOD. SERVICED CREW OXYGEN IAW AMM 12-16-35. VERIFIED FILL CAP AND SERVICE PANEL CLOSED.
Part: TERMINAL — DEFECTIVE (CABIN) · airframe 27,473 hrs · 25,021 cycles
EMERGENCY LIGHT OVERHEAD OUT. DEFERRED CABIN EMERGENCY LIGHT CEILING LIGHT IAW MEL 33-51-11. ENTERED IN MMO2, PLACARD INSTALLED AND MOC 4632 NOTIFIED. R & R TERMINAL LUG IAW ESPM 20-20-00. OPS CHECK GOOD IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED. THIS CLEARS DM 3236094-1 MMO2. UPDATED MOC 4632 NOTIFIED AND PLACARD REMOVED.
Part: CAM — DAMAGED (TE FLAP) · airframe 27,232 hrs · 24,764 cycles
RIGHT OTBD FLAP VANE MOUNTS 1, 2, 4, 6 & 7 ARE KNIFE EDGED. RT OTBD FLAP VANE BUTE DOOR MOUNTS 1, 2, 4 & 6 WERE FOUND TO BE ACCEPTABLE, AS IS BUTE DOOR CAM 7 FOUND TO BE OUT OF LIMITS IAW REO 601R-57-53-195. R & R BUTE DOOR CAM FITTING OTBD 7 IAW REO 601R-57-53-016.
Part: SKIN — DENTED (FUSELAGE) · airframe 27,232 hrs · 24,764 cycles
DENT IN FUSELAGE SKIN AT FS 682.0 BELOW STRINGER 23LT. PERFORMED CUT OUT TO REMOVE DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER IAW EA CRJ 253-04212.
Part: PANEL — CRACKED (VERTICAL STAB) · airframe 27,232 hrs · 24,764 cycles
LEFT PANEL 326AL IS BENT & CRACKED AT END, PANEL RACK. CUT OUT DAMAGE & FABRICATED FILLER & REPAIRED DOUBLER & INSTALLED IAW EA CRJ255-04224 & CRJ 200 51-42-06.
Part: PANEL — CRACKED (VERTICAL STAB) · airframe 27,232 hrs · 24,764 cycles
RIGHT PANEL 326 BR IS BENT & CRACKED AT END, PANEL RACK. DAMAGE WAS REMOVED, DOUBLER & FILLER WAS MANUFACTURED PARTS WERE TREATED & INSTALLED IAW REO 601R-55-32-233.
Part: VANE — CHAFED (TE FLAP) · airframe 27,232 hrs · 24,764 cycles
RIGHT OTBD FLAP VANE IS CHAFED INBD OF NR 7 MOUNT. REPLACED RT OTBD FLAP VANE LE IAW SRM 51-40-11 & 51-42-10.
Part: COVER PLATE — GOUGED (CARGO DOOR) · airframe 27,232 hrs · 24,764 cycles
AFT CARGO DOOR KICK PLATE COVER HINGE CRACKED & COVER PLATE GOUGED. REPLACED PLATE IAW SRM 51-42-02 PG 7 & 11.
Part: LANDING — CORRODED (FUSELAGE) · airframe 27,232 hrs · 24,764 cycles
FLOOR PANEL LANDING AT LBL 27 FROM FS 609 - 621 HAS CORROSION. REPAIRED IAW EA CRJ253-04223. INSTALLED REPAIR ON INBD & OTBD FLOOR PANEL LANDING IAW EA CRJ253-04223.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,232 hrs · 24,764 cycles
STATION 574 - 609, LBL 27 TRACK HAS CORROSION. R & R FLOORBEAM CAP 574FS-609FS IAW REO 601R-53-61-3778 & SRM 51-42-21.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,232 hrs · 24,764 cycles
STATION 589 - 621, RBL 27 TRACK HAS CORROSION. REPAIRED IAW EA CRJ253-04118. INSTALLED REPAIR ON INBD & OTBD LANDINGS AT RBL 27, STATION 609 - 621 IAW EA CRJ253-04118. REMOVED CORROSION FROM FS 589 - 609 & FOUND TO BE IN LIMITS WITH A MAX LOSS OF .004 IAW SRM 53-00-00.
Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,232 hrs · 24,764 cycles
PICCOLO TUBE SUPPORT BRACKET IS CRACKED ON OTBD UPPER EDGE AT RT WS 149.58. R & R PICCOLO TUBE SUPPORT BRACKET LT WING IAW SRM 51-42-10 & SRM 51-42-02. TORQUED BOLTS TO 35 IN POUNDS.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,232 hrs · 24,764 cycles
PASSENGER DOOR AFT DRAG ANGLE IS CRACKED, JUST FWD OF MOTOR PULLEY. R & R UNSERVICEABLE CRACKED DRAG ANGLE WITH A SERVICEABLE DRAG ANGLE IAW REO 601R-52-11-513.
Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 27,232 hrs · 24,764 cycles
RIGHT WING LE AT STATION 149, LE ATTACH BRACKET CRACKED ON LOWER END. REMOVED CRACKED UNSERVICEABLE RT LE ATTACH BRACKET & REPLACED IT WITH A NEW SERVICEABLE RT LE ATTACH BRACKET IAW SRM 51-41-02.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,763 hrs · 24,280 cycles
EMERGENCY LIGHTS FAIL TO EXTINGUISH WHEN SWITCH PLACED ARM. RESET CB 4-C-2, E-LIGHTS TESTED OK IAW AMM 33-51-00. OK FOR SERVICE.
2015
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 26,400 hrs · 23,922 cycles
CAPTAINS LIFE VEST HAS HOLE IN BAG. R & R CAPTAINS LIFE VEST IAW AMM 25-61-03.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 26,045 hrs · 23,544 cycles
CREW REPORTED FLIGHT DECK EMER LIGHT ON REAR OF MID CABIN LIGHT ASSEMBLY INOPERATIVE. REPLACED BULB IAW AMM 33-50-00. ALL CHECKED GOOD.
Part: LIFE VEST — TORN (CABNI) · airframe 26,027 hrs · 23,525 cycles
ONE INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-069A.
Part: CABLE — FRAYED (PAX DOOR) · airframe 25,526 hrs · 22,971 cycles
THE PAX DOOR ASSIST CABLES ARE FRAYED. REPLACED POWER ASSIST MOTOR & CABLE ASSEMBLY IAW MM 52-11-08-000 400-802. OPERATIONS CHECKED GOOD.
2014
Part: SPIGOT — OUT OF ADJUST (PAX DOOR) · airframe 25,005 hrs · 22,450 cycles
PAX DOOR WILL NOT OPEN. ADJUSTED FWD DOOR LATCH SPIGOT IAW 52-11-00. OPERATIONS CHECKED GOOD IAW N54245 FOR DETAILS.
Part: FITTING — CRACKED (FUSELAGE) · airframe 24,392 hrs · 21,825 cycles
TWO CRACKS IN CLIPS AT FS 484 INTERCOSTAL TO FLOOR BEAMS, 0.09" & 0.079". REPAIRED IAW REO 601R-53-41-059.
Part: FITTING — CRACKED (FUSELAGE) · airframe 24,392 hrs · 21,825 cycles
THE INBD & OTBD ATTACH CLIPS AT STRINGER 3L & FS 280 BULKHEAD ARE CRACKED, 0.5"EACH. REPAIRED IAW SRM 51-42-06 51-42-21.
Part: FRAME — CORRODED (BS 574) · corrosion level 2 · airframe 24,392 hrs · 21,825 cycles
CORROSION ON THE LOWER FRAME SECTOR AT BS 574 BETWEEN STRINGERS 26R & 26L. REPAIRED IAW EA CRJ253-02406.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,733 hrs · 11,406 cycles
FLOOR EMERGENCY LIGHT STRIP AT ROW 9, INOPERATIVE.
Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 22,994 hrs · 20,419 cycles
FLAPS FAILED MESSAGE OCCURRED DURING FLIGHT WITH THE FLAPS AT 30 DEGREES, AIRSPEED WAS 170KTS, APPROXIMATELY 30 MINUTES INTO THE FLIGHT WITH OAT AT 22 DEGREES C.
Part: FRAME — CHAFED (FUSELAGE) · airframe 22,746 hrs · 20,173 cycles
FRAME AT FS 718 BETWEEN S-16R AND S-17R CHAFED FROM BRAIDED HYD SYSTEM LINE. REPAIRED IAW EA CRJ253-01496 AND ASSOCIATED 8110-3.
Part: TRACK — DIRTY (CABIN DOOR) · airframe 22,651 hrs · 20,083 cycles
MAIN CABIN DOOR HARD TO UNLOCK FROM INSIDE, HAVE TO PULL EXTREMELY HARD ON THE HANDLE FOR IT TO OPEN. CLEANED & LUBED PASSENGER DOOR HANDLE STOW TRACK & BEARING IAW AMM 52-11-00.
Part: DOOR — ICED (CABIN) · airframe 22,425 hrs · 19,861 cycles
DOOR DIFFICULT TO OPEN DUE TO ICING. APPLIED HEAT TO PASSENGER DOOR. PERFORMED OPS CHECK OF DOOR IAW AMM 52-11-00. OPS CHECK GOOD. OK FOR SERVICE.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 22,353 hrs · 19,794 cycles
PASSENGER DOOR WILL NOT OPEN FROM INSIDE, AND IS DIFFICULT TO OPEN FROM OUTSIDE. FOUND DOOR REQUIRED LUBRICATION PER AMM 52-11-00. LUBRICATED REINSPECTED AND OPS CHECK PASSENGER DOOR IAW AMM 52-11-00. OPC GOOD COULD NOT DUPLICATE. AIRCRAFT OK FOR SERVICE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,347 hrs · 19,790 cycles
FLIGHT ATTENDANT FLASHLIGHT STILL NOT BLINKING LED LIGHT. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02. OK FOR SERVICE.
2012
Part: PANEL — CRACKED (RT NACELLE) · airframe 11,406 hrs · 24,770 cycles
RIGHT ENGINE LOWER FIREBOX PANEL P/N 601-37003-162 CRACKED ON BASE OF FORWARD SEPARATOR. REPAIRED IAW BOMBARDIER REO 601R-54-60-016.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 21,866 hrs · 19,328 cycles
ONE EA INFANT LIFE VEST POUCH HAS HOLE ON SIDE. REMOVED AND REPLACED INFANT LIFE VEST IAM AMM 25-61-03.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,722 hrs · 19,172 cycles
NR 1 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-04. OPS CHECKED GOOD.
Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 21,683 hrs · 19,134 cycles
EMERGENCY LIGHTS ROW 9 THRU 12 INOPERATIVE. TROUBLESHOOT PER WM 33-51-00. FOUND INVERTER INOPERATIVE. REMOVED AND REPLACED INVERTER IAW AMM 33-51-00. OPS CHECKED GOOD AT THIS TIME.
Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 21,139 hrs · 18,881 cycles
CAPTAINâS LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.
Part: ECU — MALFUNCTIONED (NLG STEERING) · airframe 21,644 hrs · 19,098 cycles
FLIGHT 4031, HAD A STEERING INOPERATIVE MESSAGE ON CLIMB-OUT. AIRCRAFT CONTINUED TO DESTINATION FOR AN EMERGENCY LANDING. REMOVED AND REPLACED RVDT IAW AMM 32-51-20. REMOVED AND REPLACED ECU IAW AMM 32-51-10. OPS CHECKED GOOD.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,597 hrs · 19,047 cycles
FLOOR EMERGENCY LIGHTS INOPERATIVE. RESET NR 4 INVERTER. REMOVED AND REPLACED EMERGENCY LIGHTS NR 6 AND NR 9 IAW 33-51-01. OPS CHECKED EMERGENCY LIGHTS NORMAL.
Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 21,252 hrs · 18,719 cycles
"NOSE DOOR OPEN" WARNING MESSAGE APPEARED AT 6000 FT ON CLIMB-OUT. THE MESSAGE WENT IN AND OUT SEVERAL TIMES.
Part: DOOR — OUT OF RIG (NLG LEFT) · airframe 21,252 hrs · 18,719 cycles
NOSE DOOR OPEN WARNINNG MESSAGE. FOUND LT NLG DOOR OUT OF RIG ADJUSTED NLG DOOR INTO RIG IAW CRJ 200 AMM 32-22-01. LT NLG DOOR PROX SENSOR MEASUREMENT IN LIMITS AT .047 INCH. OPS CHECXKS GOOD AT THIS TIME THIS ACTION CLEARS DM 65008. REMOVED FROM MMO2 PLACARD REMOVED.
Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 21,193 hrs · 18,663 cycles
NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGE ON GEAR RETRACTION. CYCLED GEAR DOWN, ALL APPEARED LOCKED AND GREEN. ALSO, HAD WOW INPUT CAUTION MESSAGE DURING ENTIRE EVENT. REMOVED AND REPLACED NLG ASSEMBLY IAW AMM 32-21-01.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,658 hrs · 18,849 cycles
NR 3 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04 OPS CHECKED GOOD.
Part: ACM — SMOKE (RIGHT) · airframe 21,180 hrs · 18,649 cycles
DURING BOARDING, CABIN FILLED WITH SMOKE. SUSPECT RIGHT PACK. REMOVED AND REPLACED RT ACM IAW AMM 21-51-10. OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,159 hrs · 18,627 cycles
RIGHT EXTERIOR EMERGENCY LIGHTS INOP (2). REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT BULBS POSITION RIGHT NR 2 AND NR 3 IAW AMM 33-50-01.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,129 hrs · 18,602 cycles
AFT CABIN EMERGENCY STRIP LIGHTS ON FLOOR INOP. REMOVED AND REPLACED FURTHEST AFT FLOOR LIGHT STRIP IAW AMM 33-51-01, OPC GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,050 hrs · 18,533 cycles
LEFT NR 1 EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT NR 1 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.
Part: CONNECTOR — BROKEN (CABIN) · airframe 20,968 hrs · 18,453 cycles
LAST 4 EMERGENCY LIGHT FLOOR STRIPS INOP. REPLACED BROKEN CONNECTOR ON EMERGENCY LIGHT FLOOR STRIP IAW CRJ 200 AMM 20-16-00. PERFORMED OPS CHECKS IAW CRJ 200 AMM 33-51-00-710-801. NO DEFECTS NOTED AT THIS TIME.
Part: FLOOR SUPPORT — CORRODED (BS 574-610) · corrosion level 2 · airframe 20,960 hrs · 18,451 cycles
LBL 27 FLOOR SUPPORT CORRODED AROUND NUT PLATES FROM FS 574-FS 610. REPAIRED IAW REO 601R-53-61-3778.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,927 hrs · 18,415 cycles
MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERTIVE. REMOVED AND REPLACED BAD LIGHT BULB IN EXTERIOR LIGHT ASSY FWD OF PAX DOOR AND OPS CHECKED GOOD PER AMM 33-40-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,639 hrs · 18,119 cycles
FWD EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT STRIP IAW AMM 33-51-01.
2011
Part: FLAP — FAILED (WING) · airframe 23,405 hrs · 20,282 cycles
FLAPS FAIL 8 DEGREES ON CLIMBOUT.
Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 20,421 hrs · 17,911 cycles
SMOKED FILLED COCKPIT AND CABIN ON TAKEOFF AFTER 80 KNOTS. ABORTED TAKEOFF. COMPLIED WITH MINIMUM WORK SCOPE, NO DEFECTS NOTED. REMOVED AND REPLACED COALESCER BAGS, RAN PACKS NO SMOKE NOTED, SYSTEM OPS CHECK GOOD IAW AMM 21-51-13.
Part: ENGINE — MAKING METAL (LEFT) · airframe 20,187 hrs · 17,748 cycles
LEFT OIL MASTER WARNING MESSAGE. EMERGENCY DECLARED. FOUND METAL CONTAMINATION ON LT ENGINE CHIP DETECTOR AND ON LUBE AND SCAVENGE PUMP FILTER. R&R LT ENG IAW AMM 71-00-00 AND CHECKLIST PROVIDED. PART EFFECTIVITY VERIFIED. PERFORMED ALL REQUIRED BREAK-IN RUNS IAW AMM 71-00-00 AND PPGRM 71-00-00. ALL OPS FC LKC GOOD.
Part: BRAKE ASSY — SMOKE (MLG) · airframe 19,116 hrs · 16,677 cycles
CREW REPORTED SMOKE FROM LT MAIN GEAR AFTER LANDING. PERFORMED VISUAL INSP OF LT INBD OTBD BRAKE UNITS IAW AMM 32-43-26 & DEFERRED BTMS IAW MEL 32-46-01, DM-43681.
Part: BRAKE — SMOKE (MLG) · airframe 19,116 hrs · 16,677 cycles
CREW REPORTED SMOKE FROM LT MAIN GEAR AFTER LANDING, PERFORMED VISUAL INSP OF LEFT I/B O/B BRAKE UNITS IAW AMM 2-43-26 & DEFERRED BTMS IAW MEL 32-46-01 DM-43681.
Part: SKIN — DENTED (FUSELAGE) · airframe 18,508 hrs · 16,141 cycles
AIRCRAFT EXPERIENCED A BIRD STRIKE EVENT TO THE FORWARD FUSELAGE AREA BELOW THE FORWARD FLIGHT DECK WINDOWS. UPON INSPECTION, NUMEROUS AREAS OF DAMAGE WERE FOUND SPECIFICALLY 8 DENTS TO THE FUSELAGE SKIN, 2 BUCKLED FRAMES/STIFFENERS, 2 AREAS CRACKED, A BROKEN RIVET, AND THE LT FORWARD-EQUIPMENT COMPARTMENT (TRU) DOOR WILL NOT OPEN. FERRY FLIGHT AIRCRAFT FROM MEM TO CKB IAW STS ENGINEERING EA 09-2011-026, WHERE A PERMANENT REPAIR WILL BE ACCOMPLISHED IAW EA 01-2011-019 AND EA 253-00001A.
2010
Part: HINGE FITTING — CHAFED (AILERON) · airframe 18,311 hrs · 15,943 cycles
CHAFED RT AILERON HINGE FITTING NR 1, WS 295.4, TWO PLACES .160" X .090" X 0.010" DEEP AND .250" X .090 X .003 DEEP. PERMANET REPAIR IAW REO 601R-57-51-489.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,169 hrs · 15,809 cycles
GROUND POWER UNIT (GPU) ACCESS DOOR LANDING WAS FOUND DEFORMED AND DAMAGED IN THE UPPER FORWARD CORNER. DAMAGE TO THE POWER PLUG RECEPTACLE IS LIMITED TO THE PLASTIC HOUSING WITH NO REPORTED IMPACT TO THE SYSTEM FUNCTION. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-273. REPEAT INSPECTIONS DAILY, FLY ON FOR 10 DAYS WITHIN WHICH TIME PERMANENT REPAIR IAW REO 601R-53-11-569.
Part: RETAINER — CORRODED (E&E BAY DOOR) · airframe 17,644 hrs · 15,406 cycles
FOUND LEVEL 2 CORROSION ON AVIONICS DOOR, SEAL RETAINERS. REMOVED AND REPLACED AVIONICS DOOR SEAL RETAINERS IAW CRJ-200 SRM 51-42-06. PART NUMBERS REPLACED: CC670-38675-3, CC670-38662-5, CC670-38663-5, CC67038674-3.
Part: ENGINE — FAILED (LEFT) · airframe 17,674 hrs · 15,331 cycles
DURING CLIMBOUT FROM KIND, AT 4000 FEET, THE AIRCRAFT EXPERIENCED A LEFT ENGINE FAILURE. ALL INDICATIONS WERE NORMAL UNTIL THE FAILURE. THE FLIGHT CREW COMPLETED THE QRH AND NOTIFIED ATC. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS VECTORED BACK TO KIND. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WERE MADE. CFR WAS WAITING FOR THE AIRCRAFT AT LANDING. THERE WAS NO FIRE. MAINTENANCE DETERMINED THE LEFT ENGINE TO HAVE METAL PARTICLES IN THE TAILPIPE INDICATIVE OF AN INTERNAL FAILURE. THE AIRCRAFT WAS MOVED OFF THE GATE TO A HANGAR WHERE THE LEFT ENGINE WAS REPLACED. FOLLOW UP GROUND RUNS WERE SUCCESSFUL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE REMOVED ENGINE IS EN ROUTE TO THE COMPANY MAINTENANCE BASE AT KTYS AND WILL BE INSPECTED FOR THE CAUSE OF THE FAILURE, EITHER AT THE COMPANY SHOP OR AT STANDARD AERO.
2009
Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 15,573 hrs · 13,369 cycles
JAN/MEM ON APPROACH INTO MEM RECEIVED CARGO BOTTLE LOW CAUTION MESSAGE, QRH FOLLOWED DECLARED EMERGENCY, LANDED WITHOUT INCIDENT CFR, INSPECTED AIRCRAFT NO FIRE OR SMOKE FOUND. TAXIED TO GATE. MAINTENANCE REMOVED AND REPLACED CARGO STANDBY BOTTLE IAW AMM.
Part: TORQUE LINK — DISENGAGED (NLG) · airframe 15,578 hrs · 13,375 cycles
AFTER TAKEOFF RECEIVED A NOSE GEAR DOOR OPEN WARNING, GEAR DISAGREE WARNING, WOW OUTPUT CAUTION AND NW STEERING INOP CAUTION. THE NOSE WHEEL WAS INDICATING TO BE DOWN AND LOCKED AND THE MAIN GEAR WAS INDICATING UP AS SELECTED. QRH PROCEDURES FOLLOWED FOR EACH MSG. LANDED SAFELY IN BTR. THE TORQUE LINKS WERE FOUND NOT ENGAGED. MTX REMOVED AND REPLACED TQ LINK TEE HANDLE.
Part: BPSU — FAILED (TE FLAP) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND RT BPSU FAILED.
Part: ACTUATOR — FAILED (TE FLAPS) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER FIM IAW AD 2009-06-12 FOUND NR 7 FLAP ACTUATOR FAILED.
Part: ECU — FAILED (TE FLAP) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND FECU FAILED.
Part: FLEX DRIVE — BROKEN (TE FLAP) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND NR 3 FLEX SHAFT FAILED / BROKEN.
Part: ACTUATOR — FAILED (TE FLAP) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND NR 8 FLAP ACTUATOR FAILED.
Part: BPSU — FAILED (TE FLAP) · airframe 15,402 hrs · 13,206 cycles
JUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND LT BPSU FAILED.
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 15,143 hrs · 12,978 cycles
CRACKS IN FWD PRESSURE BULKHEAD AROUND PARK BRAKE CABLE CUT-OUT. REPAIRED CRACKS IAW REO 601R-53-11-563.
2008
Part: FLAP — MALFUNCTIONED (WING)
ON APPROACH WHILE SELECTING FLAPS 30 RECEIVED FLAP FAIL MSG. QRH COMPLETED, EMERGENCY DECLARED WITH UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH AD 2006-12-21.
Part: COALESCER BAG — ODOR (AIR CON SYS) · airframe 12,842 hrs · 11,042 cycles
DURING TAXI, HAD SMOKE IN THE COCKPIT, RETURNED TO BLOCKS. COALESCER BAG FOUND CONTAMINATED LT AIR CYCLE MACHINE DEFERRED UNTIL REPLACEMENT PART AVAILABLE
2005
Part: FLAP — MALFUNCTIONED (T/E FLAP) · airframe 7,196 hrs · 6,293 cycles
FLAPS FAIL AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01
Part: PDU — INOPERATIVE (TE FLAPS) · airframe 7,187 hrs · 6,287 cycles
FLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED POWER DRIVE UNIT IAW AMM SYSTEM OPERATIONALLY CHECKED GOOD.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,162 hrs · 6,266 cycles
FLAPS FAIL AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01
Part: SMOKE — DETECTED (COCKPIT) · airframe 6,746 hrs · 5,943 cycles
ABORTED TAKEOFF FOR COCKPIT SMOKE. NO WARNING INDICATIONS, SMOKE VISIBLE. FOLLOWED QRH AND CHECKLIST, NOTIFIED DISPATCH AND MAINTENANCE CONTROL ALONG WITH LOCAL OPERATIONS, RETURN TO GATE. AIRCRAFT SWAP. GVI OF LEFT ENGINE COMPLETED AND HIGH POWER RUNS PERFORMED WITH NO DEFECTS NOTED.
Part: FCU — INOPERATIVE (TE FLAPS) · airframe 6,742 hrs · 5,939 cycles
FLAPS FAILED ON APPROACH AT 0 WHEN SELECTED TO 20.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)
FLAPS FAIL MESSAGE AND FLAPS FAILED AT 0 DEGREES. PERFORMED QUICK REFERENCE HANDBOOK. LANDING UNEVENTFUL.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,635 hrs · 5,854 cycles
EMERGENCY LANDING FOR FLAPS FAIL AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 98-20-01. RESET PER FAULT ISOLATION MANUAL, OPERATIONALLY CHECKS GOOD.
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 6,575 hrs · 5,802 cycles
FLAP FAILURE AT 0 WHEN SELECTED DOWN ON APPROACH.
Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS)
(REF NR 05-077) FLAPS FAIL ON APPROACH AT 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)
Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY)
(REF NR: 05-067) RECEIVED (CARGO SMOKE) WARNING IN FLIGHT. EMERGENCY DECLARED, QRH FOLLOWED EXTINGUISHING SYSTEM ACTIVATED WITH UNEVENTFUL LANDING AND PASSENGER EVACUATION ON TAXI WAY. INVESTIGATED, FOUND TO BE FALSE WARNING. SYSTEM DEFERED IAW MEL. (K)