N708PS

Part: A/C PACK — ODOR (200) · airframe 40,137 hrs · 38,520 cycles

RT PACK OVERHEAT AND BLOWING SMOKE. REMOVED AND REPLACE ACM IAW CRJ 700 AMM 21-51-08-000/400-801-A01. PERFORMED OPS TEST ON RH AIR CONDITION SYSTEM IAW CRJ700 AMM 21-51-00-710-801-A01 OPS TEST GOOD. PERFORMED LEAK TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 700 AMM 21-51-00-790-801-A01 LEAK TEST GOOD WHITHIN PERMITTED LIMIT.NO FURTHER DEFECT NITED AT THIS TIME .A/C OK FOR SERVICE.

Part: PACKING — DAMAGED (NLG) · airframe 38,964 hrs · 37,479 cycles

DEPARTING OUT OF KBHM THE CREW RECEIVED A NOSE GEAR DISAGREE MSG. AFTER THE MSG THEY WERE OVER WEIGHT DID A LOW APPROACH WITH TOWER TO MAKE SURE GEAR WAS DOWN. IT WAS CONFIRMED BY THE TOWER THAT THE LANDING GEAR WAS DOWN AND THEY COULD LAND. AFTER LANDING SAFELY THE STEERING INOP MSG THAT WAS CLEARED THE NIGHT BEFORE CAME BACK, IT WAS CLEARED WITH MX CONTROL. THEY WOULD TAXI INTO THE GATE WITHOUT ANY ISSUES, EMERGENCY WAS DECLARED. / NOSE GEAR UPON INSPECTION HAS NO CHROME SHOWING. REMOVED AND REPLACED NLG SHOCK STRUT PACKINGS IAW CRJ 700 AMM 32-21-20-000/400-801-A01-PSA. PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION/ RETRACTION SYSTEM IAW CRJ700 AMM 32-30-00-710-801. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

STR 27 IS CORRODED BETWEEN FR AT FS 310.00 AND FR AT FS 319.70.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 37,290 hrs · 35,936 cycles

AFT CARGO DOOR SILL IS CORRODED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,290 hrs · 35,936 cycles

LT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK AFT OF THE REPAIR DOUBLER APPROXIMATELY 1" LONG.

Part: DOOR — CORRODED (MAIN PAX) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

PASSENGER DOOR REMOVED FOR NUMEROUS AREAS OF CORROSION ON THE INNER SKIN AND STRUCTURE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

STGR 26R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

FRAME AT FS 310.00 IS CORRODED BETWEEN STR 25 LT AND STR 25 RT, FWD SIDE OF FRAME.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

STR 20 RT IS CORRODED BETWEEN FR AT FS 295.00 TO FR AT FS 319.00, REPLACED STRINGER.

Part: SKIN — CANNING (RUDDER) · airframe 37,290 hrs · 35,936 cycles

RUDDER SKIN IS OIL CANNING ON LOWER RT CORNER AROUND CUTOUT.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

FRAME AT FS 319.70 IS CORRODED BETWEEN STR 26 LT AND STR 26 RT, FWD SIDE OF FRAME. REPLACED FRAME.

Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 37,290 hrs · 35,936 cycles

RT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK 1 1/2" LONG ON THE REPAIR DOUBLER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,290 hrs · 35,936 cycles

STR 21 RT HAS AREA OF CORROSION BETWEEN FR AT FS 364.00 AND FR AT FS 379.00.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

STGR 25R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,290 hrs · 35,936 cycles

CORROSION LOCATION IS STGR 21RT BEWTEEN FS 319.00 AND FS 349.00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,290 hrs · 35,936 cycles

FRAME AT FS 333.00 BETWEEN STRINGER 1RT AND STRINGER 2RT IS CRACKED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

LT INTERCOSTAL CORRODED, LOCATED BETWEEN FR AT FS 349.00 AND FR AT FS 364.00 AND BETWEEN STR 27 AND STR 26 LT, REPLACED INTERCOSTAL.

Part: SKIN — DAMAGED (FUELAGE) · airframe 37,290 hrs · 35,936 cycles

EXT FUSELAGE SKIN HAS AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AND STR 26 LT TO 26 RT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,290 hrs · 35,936 cycles

RT INTERCOSTAL CORRODED, LOCATED BETWEEN FR AT FS 349.00 AND FR AT FS 364.00 AND BETWEEN STR 27 AND STR 26 RT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,290 hrs · 35,936 cycles

FRAME AT FS 310.00 FROM STRINGER 25R TO PRODUCTION SPLICE AT 18R REQUIRES REMOVAL AND INSTALLATION TO FACILITATE OTHER MAINTENANCE, REPAIR OF STRINGERS 20R AND 21R.

Part: PIN — DISCONNECTED (EMERGENCY LIGHT) · airframe 37,187 hrs · 35,846 cycles

DURING OVERNIGHT MAINTENANCE IT WAS FOUND THE #2 EMERGENCY FLOODLIGHT WAS INOP. MAINTENANCE FOUND THE PINS AT THE LIGHT DISCONNECTED, RESEATED THE PINS AND THE LIGHT OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,071 hrs · 35,741 cycles

EMERGENCY LIGHT BATTERY IS DEAD. CHARGED EMERGENCY BATTERY WITH A/C POWER FOR 6HRS PER VCMM OPS CHECKS GOOD

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 36,478 hrs · 35,212 cycles

DURING REMOVAL OF PILOTS SIDE WINDOW FOUND A CRACK IN THE PRIMARY STRUCTURE OF THE FRAME BETWEEN THE SIDE WINDOW AND WINDSHELD. MX REMOVED AND REPLACED PILOTS SIDE WINDOW POST.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 35,853 hrs · 34,667 cycles

RH OVERWING EMERGENCY EXIT COVER PANEL WILL NOT STAY IN PLACE. STUCK HOOK AND LOOP BACK IN PLACE. PROBLEM DID NOT REOCCUR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,409 hrs · 34,281 cycles

EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED #1 AND #2 EMERGENCY POWER SUPPLY UNIT BATTERY P/N AD2013-1A S/N 136305, 79823 OPS CHECK GOOD AT THIS TIME

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,026 hrs · 33,940 cycles

FS 280.00 BULKHEAD LOWER WEBS ARE CORRODED AT LBL 12.0. REPLACED LT LOWER WEB IAW REO 670-53-11-594.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,026 hrs · 33,940 cycles

GUSSETS AT LBL 9.0 AND RBL 9.0 FS 278.00 ARE CORRODED BEYOND LIMITS. INSTALLED 2EACH GUSSETS AT LBL9 AND RBL9 FS278.00 PART #'S CC670-33467-1 AND CC670-33467-2 IAW SRM 51-42-06-001-001-A01.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,026 hrs · 33,940 cycles

WHILE REMOVING L/H INTERCOSTAL, FOUND STIFFNER WAS CRACKED AND NEEDS REPLACED. FS280 LBL 26.00. REMOVED AND REPLACED CRACKED STIFFNER WITH NEW STIFFNER P/N: CC670-34117-1 IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,026 hrs · 33,940 cycles

WHILE WORKING SERVICE BULLETIN FOUND 2EA ANGLES CRACKED AT FS260.00 - FS280.00 LBL9 AND RBL9. REMOVED AND REPLACED CRACKED ANGLES AT FS260-280 LBL9 AND RBL9 WITH NEW ANGLES PART #'S CC670-33199-35 AND CC370-33199-45 IAW SRM 51-40-11-001-001-A01, AND SRM 51-42-06-001-001-A01.

Part: WINDSHIELD — CRACKED (RIGHT) · airframe 33,586 hrs · 32,622 cycles

WHILE BEING VECTORED TO FINAL THE FIRST OFFICER NOTICED A HAIRLINE CRACK ON HIS WINDSHIELD AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENT. THE AIRCRAFT FERRIED TO A MAINTENANCE BASE AND THE FIRST OFFICER WINDSHIELD AND WINDOW HEAT CONTROLLER WAS REPLACED.

Part: A/C PACK — FAILED (AC BAY) · airframe 33,228 hrs · 32,267 cycles

AIRCRAFT WAS AN ORIGINATOR AND WHILE IT WAS ON THE GATE THE RT PACK FAILED AND THE CABIN FILLED WITH SMOKE. NO PASSENGERS WERE ONBOARD. MAINTENANCE VISUALLY INSPECTED A/C NO EVIDENCE OF FIRE. DEFERRED CABIN TEMP CONTROL SYSTEM AND RT AIRCONDITIONING PACK MX REMOVED AND REPLACED RH ACM. OPS CHECKS GOOD.

Part: LIGHT — DETACHED (CABIN) · airframe 31,334 hrs · 30,600 cycles

THE EMERGENCY LIGHT ON THE RIGHT HAND FORWARD BULKHEAD IN FRONT OF THE FIRST CLASS SEATS IS DETACHED FROM THE WALL. FERRIED THE AIRCRAFT TO A MAINTENANCE BASE AND REPLACED THE LIGHT ASSEMBLY.

Part: HANDLE — BROKEN (SERVICE DOOR) · airframe 30,064 hrs · 29,477 cycles

THE SERVICE DOOR HANDLE WAS BROKEN OFF. REMOVED AND REPLACED GALLEY SERVICE DOOR ASSIST HANDLE.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 29,327 hrs · 28,770 cycles

LEFT BS 280 LOWER BULKHEAD WEB CORRODED. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW AMM.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 29,327 hrs · 28,770 cycles

LEFT BS 280 FLOORBEAM CORRODED. MAINTENANCE PERMORMED A MAJOR REPAIR TO THE FLOORBEAM IAW AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,327 hrs · 28,770 cycles

RIGHT BS 280 FLOORBEAM CRACKED. MAINTENANCE PERMORMED A MAJOR REPAIR AND PERFORMED CHECKS IAW THE AMM.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 29,327 hrs · 28,770 cycles

RIGHT BS 280 LOWER BULKHEAD WEB CORRODED. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW AMM.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · corrosion level 2 · airframe 29,327 hrs · 28,770 cycles

FOWARD J ANGLE AT F.S. 280 CORRODED BETWEEN LBL 9 AND RBL 9. MAINTENANCE INSTALLED FORWARD THE ANGLE AND PERFORMED CHECKS IAW THE AMM.

Part: CONTROL SYSTEM — STIFF (AILERON)

AILERONS ARE HARD TO MOVE, FEEL INDENTS. MECHANICS TROUBLESHOT LEFT AND RIGHT HAND FORWARD FUEL QUADRANTS, NO DEFECTS NOTED. INSPECTED RIGHT HAND REAR FUEL QUADREANT AND FOUND BUSHING OUT OF ROUND AT APPROX 45 DEGREES FULL RIGHT AILERON MOVEMENT. TECHNICIANS CORRECTED THE BUSHING AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: YAW DAMPER — FAULTY (RUDDER) · airframe 29,159 hrs · 28,619 cycles

RUDDER KICKING TO LT ON TAKEOFF. REMOVED AND REPLACED YAW DAMPER NR 1 IAW AMM, ALL SYSTEMS OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 28,623 hrs · 28,111 cycles

INBD SPOILERONS AND INBD FLIGHT SPOILERS FAULT. THE CREW DECLARED AN EMERGENCY, CONTINUED APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, PERFORMED SYSTEM RESET AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,241 hrs · 27,759 cycles

THE CREW REPORTED THE CABIN EMERGENCY LIGHT FLOOR LEVEL EXIT SIGN WAS INOPERABLE, THE LT EMERGENCY EXIT DOOR, EXIT SIGN, HAD 1 OF 5 LIGHTS INOPERABLE. MAINTENANCE TROUBLESHOT AND DEFERRED THE LT AFT FLOOR LEVEL LIGHTED EXIT SIGN IAW MEL 33-51-01-2E, CAT C. MAINTENANCE PERFORMED CHECKS IAW THE AMM, AND RELEASED THE ACFT FOR SEVICE. MAINTENANCE RELAMPED THE LT EMERGENCY EXIT LOWER LIGHT, WHICH CLEARED THE MEL, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 27,406 hrs · 27,005 cycles

CREW REPORTED SIGN UNDER F/A FORWARD FLASHLIGHT MISSING. MAINTENANCE INSPECTED, R & R MAIN CABIN ENTRANCE FLOOR LEVEL EMERGENCY FLOODLIGHT ASSY DUE TO MISSING COVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRINGER SPLICE — CORRODED (FS 333 - 349) · airframe 25,770 hrs · 25,457 cycles

CORROSION ON STRINGER 25R BETWEEN FS 333 AND FS 349. REMOVED CORRODED STRINGER SPLICE AND INSTALLED SERVICABLE STRINGER SPLICE IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,770 hrs · 25,457 cycles

LATCH PIN INTERCOSTAL AT STR 27L IS CORRODED, FILIFORM, ON INBD SIDE BETWEEN FS349 AND FS364 OUT OF LIMITS, PN SH670-32075-3. R & R INTERCOSTAL, PN SH670-32075-3 BETWEEN FS349 AND FS364.

Part: ANGLE — CORRODED (BS 280) · corrosion level 2 · airframe 25,770 hrs · 25,457 cycles

FS280 FWD FLOOR SUPPORT J-ANGLE CORRODED, FILIFORM, BEYOND SRM LIMITS. R & R J-ANGLE ON FWD SIDE OF FS280 CROSSBEAM, PN CC670-33292-13S.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,770 hrs · 25,457 cycles

LEFT FWD VERT STAB DRAG ANGLE IS CRACKED APPROXIMATELY .25 ON AFT END. PERFORMED A MAJOR REPAIR TO THE LT VERTICAL STABILIZER FUSELAGE ATTACHMENT DRAG ANGLE AT 67.5 PERCENT REAR SPAR DATUM IAW REO 670-55-31-018, REV-DATED 16-APR-07.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 25,080 hrs · 24,810 cycles

CREW REPORTED GEAR DISAGREE MESSAGE AND THAT NOSE GEAR FAILED TO COME UP AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND CHECKED RIG OF NLG LOCK POSITION PROXIMITY SENSORS. RIG CHECKED GOOD. MAINTENANCE FOUND NLG UP POSITION PROXIMITY SENSOR WITHIN LIMITS, BUT AT HIGH END OF ADJUSTMENT. SENSOR WAS RESET. OPS CHECKS AND GEAR SWINGS WERE GOOD. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 24,834 hrs · 24,571 cycles

CREW REPORTED LIGHTS OUT FOR EMERGENCY EXIT SIGN OVER SEAT 4D. MAINTENANCE INSPECTED, SECURED LOOSE WIRE ON RT EMERGENCY EXIT SIGN ON CLASS DIVIDER AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (RT INBD SLAT) · airframe 23,636 hrs · 23,341 cycles

CREW REPORTED A BIRD STRIKE ON RT WING. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION IAW AMM, FOUND RT INBD SLAT SKIN PANEL DENTED AND DETERMINED DAMAGE TO BE WITHIN LIMITS IAW SRM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — MISSING (GALLEY) · airframe 23,132 hrs · 22,853 cycles

CREW REPORTED ACFT MISSING EMERGENCY LIGHT IN GALLEY. MAINTENANCE INSPECTED, INSTALLED LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 23,132 hrs · 22,853 cycles

CREW REPORTED RT OVERWING EXIT LOWER EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE TROUBLESHOT, R & R EMERGENCY LIGHTS BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 23,088 hrs · 22,808 cycles

DURING SCHEDULED MAINTENANCE, RT VERTICAL STAB DRAG ANGLE CRACKED. REPAIRED IAW AMM. AIRCRAFT WAS RELEASED FOR SERVICE

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 23,088 hrs · 22,808 cycles

DURING SCHEDULED MAINTENANCE OF THE BS 280 FLOORBEAM CORRODED. REPAIRED IAW AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,088 hrs · 22,808 cycles

DURING SCHEDULED MAINTENANCE, FS 202.75 PRESSURE BULKHEAD FOUND INDICATION OF CRACKED. THE AREA WAS INSPECTED AND REPAIRED IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: DISPLAY — OVERHEATED (COCKPIT) · airframe 21,991 hrs · 21,693 cycles

CREW REPORTED DISPLAY UNIT ED1 FAILED ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND PULLED TO A TAXI WAY. CREW CALLED MX AND EICAS DISPLAY UNIT ED1 WAS DEFERRED IAW MEL. FLIGHT CONTINUED WITH NO FURTHER INCIDENT. MX INSPECTED AND FOUND DISPLAY COOLING FAN IN STANDBY POSITION AND OVERHEATED ED1. MX R & R ED1, TURNED DISPLAY COOLING FAN TO NORMAL POSITION, PERFORMED CHECKS AND CLEARED DEFERRAL USING ACFT MM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 21,541 hrs · 21,215 cycles

CREW REPORTED EMERGENCY EXIT SIGN LOCATED BY MAIN CABIN DOOR HAD ONE LIGHT OF FIVE (5) INOPERATIVE. MAINTENANCE INSPECTED, RELAMPED EMERGENCY EXIT SIGN AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: AOA — DAMAGED (STALL WARNING) · airframe 21,096 hrs · 20,782 cycles

CREW REPORTED APPARENT LIGHTNING STRIKE TO NOSE OF AIRCRAFT DURING CLIMBOUT. CREW LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE FOLLOWING: RIGHT AOA VANE, NUMBER TWO (2) VHF ANTENNA, LEFT HORIZONTAL STAB TIP FAIRING GRANGER MOD AND SEVERAL STATIC WICKS. MAINTENANCE REPAIRED VARIOUS BURN SPOTS ON RIGHT SIDE OF FUSELAGE AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 20,283 hrs · 19,995 cycles

CREW REPORTED GEAR DISAGREE WARNING MESSAGE AFTER RETRACTION WITH TWO (2) MAIN WHITE AND RED NOSE. CREW FOLLOWED QRH, SELECTED GEAR DOWN, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, ADJUSTED GAP ON PROXIMITY SENSORS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,894 hrs · 19,615 cycles

CREW REPORTED SLAT FAIL MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RESET BREAKERS TO SLAT / FLAP SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. PROBLEM DID NOT REOCCUR. AIRCRAFT RELEASED FOR SERVICE.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 19,258 hrs · 18,989 cycles

CREW REPORTED RED NOSE DOOR OPEN MESSAGE AND PROXIMITY SYSTEM FAULT 1 WHITE STATUS MESSAGE IN FLIGHT. CREW FOLLOWED QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RE-ADJUSTED NOSE LANDING GEAR DOOR SENSOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (COCKPIT) · airframe 19,093 hrs · 18,819 cycles

CREW REPORTED F/O SIDE MAP LIGHT FAILED. SPARKS WERE SEEN, AS WELL AS ODOR THAT DISAPPEARED QUICKLY. CIRCUIT BREAKER ALSO POPPED. MAINTENANCE INSPECTED, FOUND F/O MAP LIGHT WIRES DAMAGED IN LIGHT ASSEMBLY, REMOVED AND REPLACED F/O MAP LIGHT ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: PANEL — ODOR (FUEL SYSTEM) · airframe 16,871 hrs · 16,545 cycles

FUELER REPORTED BURNING SMELL FROM FUSELAGE REFUEL / DEFUEL PANEL PER CREW AT CLT. MAINTENANCE INSPECTED, REMOVED AND REPLACED FUSELAGE REFUEL / DEFUEL PANEL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,583 hrs · 16,267 cycles

DURING SCHEDULED MAINTENANCE, REPAIRS WERE MADE TO THE FUSELAGE SKIN FROM FS 1015 TO 1047 BETWEEN STRINGERS 17L - 21L. AIRCRAFT WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,583 hrs · 16,267 cycles

DURING SCHEDULED MAINTENANCE, REPAIRS WERE MADE TO THE FUSELAGE SKIN FROM FS 967 TO 977 BETWEEN STRINGERS 25L - 26L. AIRCRAFT WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,655 hrs · 15,403 cycles

CREW REPORTED A CRACKED COCKPIT RIGHT WINDOW. FLIGHT DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS REMOVED AND REPLACED THE RIGHT COCKPIT WINDOW. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 15,440 hrs · 15,189 cycles

AT TYS, CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RADOME ASSEMBLY, REPAIRED DAMAGE TO THE UPPER LEFT HAND SIDE OF THE FUSELAGE AND PERFORMED CHECKS. AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS AND REPAIR ENGINEERING ORDER (REO).

Part: BALLAST — FAULTY (LAVATORY) · airframe 14,708 hrs · 14,408 cycles

CREW REPORTED THE AFT LAV HAS ELECTRIC SMELL FROM MIRROR LIGHT. MAINTENANCE TROUBLESHOT USING AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE REMOVED AND REPLACED THE AFT LAV LIGHT BALLAST. OPERATIONAL CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT RETURNED TO SERVICE.

Part: DETECTOR — DAMAGED (ICE PROTECTION) · airframe 14,189 hrs · 13,868 cycles

CREW REPORTED A LIGHTNING STRIKE ON THE RIGHT FRONT OF THE AIRCRAFT IN FLIGHT EN ROUTE TO CLE. AIRCRAFT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT ICE DETECTOR, STATIC DISCHARGERS AND BONDING WIRES. MAINTENANCE REPAIRED BURN MARKS ON RIVETS AND FASTENERS ON THE RIGHT SIDE OF THE FUSELAGE. CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS AND REO.

Part: RADOME — CRACKED (FUSELAGE) · airframe 14,091 hrs · 13,771 cycles

CREW REPORTED A BIRD STRIKE ON THE RADOME ON DESCENT INTO MDT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RADOME AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 12,217 hrs · 11,892 cycles

CREW REPORTED A LEFT ENGINE OIL PRESSURE MESSAGE ON TAKEOFF ROLL FROM CLT. THE TAKEOFF ROLL WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE AT CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DETERMINED THE PROBLEM TO BE INDICATION ONLY. MAINTENANCE DEFERRED THE LT ENGINE LOW OIL PRESSURE SWITCH PER MEL 79-30-01 CATEGORY A. THE MEL WAS CLEARED BY CLEANING WIRE CONNECTIONS PER THE AIRCRAFT MAINTENANCE MANUAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,199 hrs · 10,843 cycles

CREW REPORTED RT WINDSHIELD SHATTERED WHILE AT CRUISE. CREW DECENDED TO 10,000 FEET AND THEN LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE WINDSHIELD IAW THE ACFT MM. ACFT WAS RETURNED TO SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 10,884 hrs · 10,534 cycles

CREW REPORTED THE AIRCRAFT EXPERIENCED STATIC DISCHARGE FROM THE FRONT RIGHT, WHICH WAS VISIBLE AND AUDIBLE FROM THE COCKPIT WHILE FLYING THROUGH A RAIN SHOWER. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT WINGLET, THE RIGHT SIDE OF THE FUSELAGE AND THE RADOME. THE LEFT AND RIGHT WIPER ARMS WERE FOUND TO BE MAGNETIZED. REPAIRS WERE MADE TO THE WINGLET AND FUSELAGE. THE RADOME WAS REMOVED AND REPLACED. THE WIPER ARMS WERE DEMAGNETIZED. NO FURTHER DEFECTS WERE NOTED. CHECKS WERE PERFORMED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (GROUND POWER) · airframe 9,749 hrs · 9,383 cycles

CREW REPORTED AN EXTERNAL GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DAMAGE OR DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. ACFT WAS RELEASED FOR SERVICE. (S)

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 8,527 hrs · 8,208 cycles

CREW REPORTED A STEERING INOP AMBER MESSAGE DURING LANDING. AIRCRAFT WAS TOWED TO THE GATE UPON REQUEST FROM THE CREW. MAINTENANCE INTERROGATED THE MDC AND PERFORMED AN OPS TEST OF THE NOSE WHEEL STEERING IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FUEL CAP — MISSING (FUEL SYSTEM) · airframe 7,744 hrs · 7,421 cycles

CREW REPORTED THE FUEL CAP MISSING ON CLIMBOUT. CREW ELECTED TO RETURN TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE FUEL CAP. MAINTENANCE IN CLT REPLACED THE MISSING FUEL CAP, MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NONE)

CLT - FLT 2292 - CREW REPORTED ON TAKEOFF SEVERAL BIRDS STRUCK THE AIRCRAFT ON THE RIGHT WING, THE NOSE WHEEL ASSEMBLY AND ALSO THE RIGHT ENGINE. CREW CONTINUED ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT WING FOR DAMAGE AND FOUND NO DAMAGE.

Part: ACTUATOR — LEAKING (VG) · airframe 6,669 hrs · 6,310 cycles

CREW REPORTED FUEL RUNNING OUT OF RIGHT ENGINE NACELLE. MAINTENANCE INSPECTED AND FOUND THE LEAK OCCURING AT THE VG ACTUATOR WITH THE FUEL PUMP ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 VG MASTER ACTUATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ELEMENT — FAILED (RT DUCT) · airframe 5,588 hrs · 5,285 cycles

CREW REPORTED AN ANTI ICE DUCT RED WARNING MESSAGE. MAINTENANCE INSPECTED AND FOUND A RIGHT HAND BLEED AIR LEAK. MAINTENANCE REMOVED AND REPLACED THE BLEED AIR SENSING ELEMENT. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE DUCT) · airframe 5,566 hrs · 5,265 cycles

CREW REPORTED AN ANTI ICE DUCT WARNING MESSAGE. MAINTENANCE INSPECTED AND PERFORMED A LEAK TEST. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ACTIVATED (TE FLAPS) · airframe 5,151 hrs · 4,840 cycles

THE CREW REPORTED A FLAPS HALF SPEED MESSAGE ON CLIMBOUT. MAINTENANCE DEFERRED PER MEL 2751-02-1 CODE C. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (NLG STEERING) · airframe 5,116 hrs · 4,803 cycles

THE CREW REPORTED THE NOSE WHEEL STEERING FAILED ON LANDING AND WOULD NOT RESET WITH THE NOSE WHEEL STEERING SWITCH. MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECKS. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ALTIMETER — UNKNOWN (COCKPIT) · airframe 5,037 hrs · 4,719 cycles

THE CREW REPORTED THE CAPTAIN AND F/O'S ALTIMETER DIFFER BY 50 FEET AND THE CAPTAIN AND STANDBY ALTIMETERS DIFFER BY 100 FEET, BOTH AT CRUISE. MAINTENANCE PERFORMED A PITOT STATIC AND OPERATION CHECK OF THE ALTIMETER SYSTEM. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — LEAKING (FUEL SYSTEM) · airframe 4,884 hrs · 4,565 cycles

CREW REPORTED NR 2 ENGINE DRAIN MAST LEAKING FUEL. MAINTENANCE REQUESTED THE CREW TO START THE ENGINE. F/F AND ITT WERE MONITORED. NO ABNORMALITIES NOTED. ENGINE START GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE · airframe 4,344 hrs · 4,021 cycles

THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DURING CRUISE. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE LT HORIZONTAL STAB TIP AND SEVERAL SPOTS ON THE RT FUSELAGE. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (LAVATORY SMOKE) · airframe 3,842 hrs · 3,504 cycles

DURING CLIMBOUT THE CREW REPORTED A -SMOKE AFT LAV- WARNING MESSAGE THAT DISAPPEARED AFTER 30 SECONDS. THE FLIGHT RETURNED TO SRQ AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFT LAVATORY AND FOUND NO EVIDENCE OF SMOKE, OVERHEAT, OR FIRE. THE GALLEY HEAT CIRCUIT BREAKER WAS FOUND POPPED. THE CIRCUIT BREAKER WAS RESET AND THE GALLEY HEAT SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUCTURE — GROUND DAMAGE (RT WING) · airframe 3,690 hrs · 3,349 cycles

WHILE PARKED AT THE GATE THE RIGHT WING TIP LEADING EDGE TRANSITION FAIRING AND OUTBOARD SLAT WERE HIT BY A VEHICLE. THE FAIRING WAS DENTED AND THE SLAT WAS DENTED & CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING TRANSITION FAIRING AND OUTBOARD SLAT WITH SERVICEABLE UNITS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DENTED (ANTI ICE SYS) · airframe 3,457 hrs · 3,121 cycles

DURING CLIMB THE LT AND RT WING ANTI-ICE SYSTEMS CYCLED ON AND OFF. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE NR 2 - NR 3 SLAT TRACK CONNECTOR FLEX TUBE DENTED CAUSING REDUCED BLEED AIR FLOW TO THE LT OUTBOARD SLAT. THE CONNECTOR WAS REPAIRED IAW BOMBARDIER REO 670-30-11-06. BOTH WING ANTI-ICE SYSTEMS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (RT PITCH FEEL) · airframe 3,438 hrs · 3,102 cycles

DURING CLIMB THE PITCH FEEL CAUTION LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE RT PITCH FEEL LINEAR ACTUATOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERONS) · airframe 2,697 hrs · 2,411 cycles

ON FINAL APPROACH, APPLICATION OF THE FLIGHT SPOILER LEVER RESULTED IN I/B SPOILERONS & I/B FLT SPLRS CAUTION MESSAGES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE SSCU IAW CRJ700 SL-27-028. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 2,359 hrs · 2,076 cycles

DURING CRUISE THE CREW REPORTED TOTAL LOSS OF THE NR 1 HYDRAULIC SYSTEM PRESSURE AND FLUID QUANTITY. MAINTENANCE FOUND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE LEFT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29-11-01-400-801-A01. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: PUMP — FAILED (NR 1 HYD SYSTEM) · airframe 344 hrs · 320 cycles

DURING CRUISE THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM HIGH TEMP CAUTION MESSAGE. TWO SECONDS LATER O/B SPLRON, O/B FLT SPLRS, O/B GND SPLRS, & HYD 1 LOW PRESS CAUTION MESSAGES WERE RECEIVED. THE CREW ELECTED TO DIVERT FLIGHT 2219 TO DAY WHERE MAINTENANCE WAS AVAILABLE. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ200 AMM 29-11-01. FUNCTIONAL & LEAK TEST WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (FIRE WARNING) · airframe 75 hrs · 70 cycles

THE CREW REPORTED RECEIVING A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE CONTROL HAD THE CREW RESET THE CIRCUIT BREAKERS CBP-1, N1, AND N2, IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-10-00 AND THE MESSAGE CLEARED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.