N8390A

Part: LIFE VEST — TORN (COCKPIT) · airframe 28,554 hrs · 25,943 cycles

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

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 28,260 hrs · 25,655 cycles

ONE INFANT LIFE VEST HAD HOLE IN BAG. R & R INFANT LIFE VEST IAW PA 25-096A.

Part: CONTAINER — TORN (LIFE VEST) · airframe 28,121 hrs · 25,520 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,060 hrs · 25,460 cycles

EMERGENCY LIGHTS WON'T STAY ON. R & R BATTERY PACKS . OPS CHECKED GOOD IAW AMM 33-51-04.

Part: SEAL — TORN (RT OVERWING EXIT) · airframe 28,040 hrs · 25,440 cycles

RT OVERWING EMERGENCY EXIT DOOR PRESSURE SEAL TORN. REMOVED DAMAGED SEAL ON RT OVERWING EMERGENCY EXIT DOOR AND INSTALLED NEW PRESSURE SEAL IAW AMM 51-22-28 & 52-21-07. PERFORMED OPERATIONS TEST OF EMERGENCY EXIT SEAL IAW AMM 52-21-07. OPS TESTED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,040 hrs · 25,440 cycles

LEFT OTBD FLOORBEAM CAP RBL9 AT FS559+112 TO FS621, WL73.5 IS CORRODED BEYOND LIMITS. R & R IAW SRM 51-42-21 AND REO 601R-53-61-3780.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,040 hrs · 25,440 cycles

FLOOR SUPPORT FROM FS 559+105 TO 559+112, WL 73.5, LBL 27 CORRODED. SPLICED IAW SRM 53-00-43.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,040 hrs · 25,440 cycles

LEFT OTBD FLOORBEAM CAP LBL27 AT FS559+112 TO FS621, WL73.5 IS CORRODED BEYOND LIMITS. R & R IAW SRM 51-42-21 AND REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,040 hrs · 25,440 cycles

LEFT OTBD FLOORBEAM CAP LBL9 AT FS559+112 TO FS621, WL73.5 IS CORRODED BEYOND LIMITS. R & R IAW SRM 51-42-21 AND REO 601R-53-61-3778.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,040 hrs · 25,440 cycles

AFT PRESSURE BULKHEAD FORWARD FACE CRACKED AT LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,536 hrs · 24,964 cycles

MOST FORWARD OVERWING EMERGENCY LIGHT ON LEFT WING INOPERABLE. THE TWO REARWARD EMERGENCY LIGHTS WORK OK. REMOVED AND REPLACED FORWARD WING EMERGENCY LIGHT IAW AMM 33-51-21. OPERATIONS CHECK GOOD.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,208 hrs · 24,638 cycles

ENGINE BEAM DOUBLER CRACKED AT LBL 29.2. REPAIRED IAW BOMBARDIER REO 601R-53-61-4738.

Part: SKIN — DENTED (RT WING) · airframe 27,208 hrs · 24,638 cycles

RIGHT WING LOWER SKIN DENTED AT WS 29.42 MEASURING 2.3" X 2.6" X 0.038" DEEP AND 12.6" FROM THE LEADING EDGE OF THE SKIN. REPAIRED IAW BOMBARIDER REO 601R-57-21-1815.

Part: HINGE FITTING — GOUGED (LT HORIZ STAB) · airframe 27,194 hrs · 24,627 cycles

LEFT HORIZONTAL STABILIZER NR 2 HINGE FITTING GOUGED AT LBL 55.88. REPAIRED IAW BOMBARDIER REO 601R-55-11-442.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 27,176 hrs · 24,609 cycles

CREW REPORTS CENTER EMERGENCY EXIT SIGN MISSING BULB AND WHITE COVER. REMOVED AND REPLACED LAMP & LENS COVER FOR WHITE LIGHT ON CENTER EMERGENCY EXIT SIGN IAW AMM 33-51-14.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 27,159 hrs · 24,594 cycles

EMERGENCY EXIT LIGHT OVER ROW 8 INOPERABLE ON ONE SIDE. REPAIRED CONNECTION AT BATTERY PACK NR 2 & OPS CHECK IAW AMM 33-51-04. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,012 hrs · 24,449 cycles

CENTER CABIN OVERHEAD CURVED EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY NR 2 IAW AMM 33-51-05. OPS CHECKS ARE GOOD. THIS CLEARS MEL 33-51-01 AUTH# 73720.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,988 hrs · 24,425 cycles

EXTERIOR EMERGENCY LIGHTS RIGHT AND LEFT SIDE 3 LIGHT BACK INOP, DEFERRED EXTERIOR EMERGENCY LIGHTS PER MEL 33-51-22. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY NR 3 IAW AMM 33-51-05. OPS CHECKS ARE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,847 hrs · 24,283 cycles

SECOND FROM THE BACK CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB IAW AMM 33-51-00. OK FOR SERVICE.

Part: DOOR — INOPERATIVE (NLG) · airframe 26,730 hrs · 24,167 cycles

NOSE GEAR DOOR WILL NOT OPEN. RESEATED LANDING GEAR EMERGENCY EXTENSION HANDLE IAW AMM 32-34-00. PERFORMED OPS CHECK OF EMERGENCY EXTENSION SYSTEM IAW AMM 32-34-00. OPS CHECKED GOOD, PERFORMED MLG SWING IAW AMM 32-30-00. OPS CHECKED GOOD, NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE, CLEAR DM 69984.

Part: CONTAINER — TORN (LIFE VEST) · airframe 26,701 hrs · 24,135 cycles

CAPTAIN'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.

Part: ENGINE — ODOR (RIGHT) · airframe 26,627 hrs · 24,056 cycles

DURING CLIMB-OUT, FLIGHT 4416, FLIGHT ATTENDANT NOTICED POSSIBLE SMOKE IN CABIN. SMOKE ODOR IN COCKPIT. NO FIRE INDICATIONS. AIR RETURNED TO DEPARTURE. FLIGHT ATTENDANT STATED THAT IS SEEMED TO COME FROM THE FLOOR VENTS. REMOVED AND REPLACED RIGHT ENGINE ASSY IAW AMM 71-00-00-04. OPS AND LEAK CHECKED GOOD.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 26,619 hrs · 24,047 cycles

FLT 4106, CREW REPORTED A SWEET SMOKE ODOR ON FINAL. NO VISIBLE SMOKE, EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY AT DESTINATION, IT IS NOTED THE RIGHT HAND ENGINE WAS CHANGED TWO DAYS PRIOR. REMOVED AND REPLACED RIGHT HAND AND LEFT COALESCER BAG IAW AMM 21-51-13.

Part: DRAIN — KINKED · airframe 26,619 hrs · 24,047 cycles

TOILET SMOKE CAUTION MESSAGE IN FLIGHT. PERFORMED QRH. SWEET ODOR ASSOCIATED WITH IT. DETECTOR WENT OFF. FLIGHT ATTENDANT REPORTED SMOKE, BUT IT DISSIPATED VERY QUICKLY. REPORTED NO PROBLEMS AND RESET SMOKE DETECTOR ALARM. SEVEN MINUTES LATER ALARM WENT OFF AGAIN WITH HAZY SMOKE. REPLACED BOTH COALESCER FILTERS IAW AMM 21-50-00. WATER FOUND IN RIGHT COALESCER. REPOSITIONED KINKED RIGHT WATER DRAIN HOSE. PERFORMED ENGINE RUNS WITH BOTH MOTORS AND APU. NO FAULTS NOTED. TESTED SMOKE DETECTOR IN LAVATORY TWICE, OPS CHECKED GOOD. COULD NOT DUPLICATE. SUSPECT SMOKE NOTED WAS CONDENSATION FROM AIRCRAFT. AIRCRAFT SYSTEM DUE TO HIGH HUMIDITY AND WET COALESCER FILTERS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 26,269 hrs · 23,709 cycles

RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-00. OPS CHECKED NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,158 hrs · 23,599 cycles

OVERHEAD EMERGENCY EXIT FLOODLIGHT AT SEAT 13B IS INOPERATIVE. REPLACED BULB AT EMERGENCY EXIT OVERHEAD ROW 13 P/N AML-1317. OPS CHECK GOOD IAW AMM 33-50.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,944 hrs · 23,395 cycles

FWD CEILING EMERGENCY LIGHT INOPERATIVE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 25,875 hrs · 23,329 cycles

AIR RETURN FOR STAB TRIM (AND MACH TRIM) CAUTION AFTER TAKEOFF. RAN QRH W/O RESOLUTION. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OP CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,330 hrs · 22,836 cycles

MASTER WARNING WING OVHT MESSAGE IN NORMAL. SELECTED STBY WITH NO FURTHER PROBLEMS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,253 hrs · 22,703 cycles

WING OVERHEAT ON CLIMBOUT RAN QRH MSG WENT OUT. PERFORMED OPS CHECK OF WING ANTI SYSTEM IAW AMM 30-12-00. OPS CHECK NORMAL. NO FAULTS FOUND. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 24,968 hrs · 22,429 cycles

IN CRUISE `MAN XFLOW` STATUS MSG CAME ON /SWITCH ON/ WITH SWITCH OUT THEN MSG WENT AWAY AND AUTO XFLOW INHIB STATUS MSG. CLEARED FAULT OUT OF FUEL COMPUTER AUTO XFLOW INHIB MESSAGE CLEARED IAW AMM 28-40-00, OK FOR SERVICE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,501 hrs · 21,985 cycles

FS 559.00 BULKHEAD FAILS NDT WITH AN INDICATION ON RIGHT WEB RBL 18 GREATER THAN 50 PERCENT FSH. REPAIRED FS 559.00 BY CUTTING OUT DAMAGE, FABRICATING PARTS, & INSTALL FABRCATED PARTS IAW BOMBARDIER REO 601R-53-41-260 REV E DATED 08/24/2010 AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION E.

Part: CONTROL CABLE — OBSTRUCTED (ELEVATOR) · airframe 24,355 hrs · 21,845 cycles

ELEVATOR WILL NOT PULL BACK. CLEANED DEBRIS FROM AROUND ELEVATOR CABLES. OPS CHECK GOOD IAW AMM 27-31-00.

Part: PROXIMITY SWITCH — INTERMITTENT (NLG) · airframe 24,350 hrs · 21,840 cycles

CREW DECLARED EMERGENCY & DIVERTED FROM BHM-DTW TO MEM FOR NOSE GEAR DISAGREE AFTER TAKEOFF. ADJUSTED NOSE CENERING PROX SENSOR, SERVICE NOSE STRUT, C/E PA, NO DEFECTS NOTED. OK FOR SERVICE.

Part: PROXIMITY SWITCH — INTERMITTENT (NLG) · airframe 24,350 hrs · 21,840 cycles

ORIGINAL AIRCRAFT 8390A DID AN AIR RETURN FOR NOSE GEAR UP DISAGREE ON TAKEOFF. PERFORMED TROUBLESHOOTING IAW PA05-018A AND AMM 32-61-05. FOUND PS3GA PROX SWITCH INTERMITTENT. REMOVED AND REPLACED PROX SWITCH PS3GA AND GEAR.

Part: SKIN — GOUGED (RT WING) · airframe 24,346 hrs · 21,836 cycles

RIGHT WING LOWER PLANK ACCESS HOLE NR 9 AT WS 163.00 HAS GOUGE IN THE CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

DURING REPLACEMENT OF RIGHT AFT NOSE LANDING GEAR DOOR FITTING FOUND S-26R TO HAVE APPROXIMATELY 0.450" DIAMETER CHAFE WITH PITTING APPROXIMATELY 0.065" DEEP. REPAIRED IAW REO 601R-53-11-2131.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FRAME FLANGE AT FS 682 (FWD SIDE) IS DEFORMED AND CRACKED 1.00" WIDE X 0.35" LONG AT S-26R AND THE AFT REINFORCING ANGLE IS DAMAGED 1.00" WIDE AT S-26L. REPAIRED IAW BOMBARDIER SERVICE CORP EO 601R-53-21487C AND ASSOCIATED 8110-3.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FS 621 BULKHEAD FWD SIDE HAS SCREW MARKS FROM ACCESS PANEL HARDWARE AT LBL 18, LBL 27, RBL 18, RBL 27, AND RBL 36, WITH NONE DEEPER THAN 0.002". REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — GOUGED (LT WING) · airframe 24,346 hrs · 21,836 cycles

THE LEFT WING PLANK AROUND FUEL ACCESS PANEL 650DB GOUGED IN CRITICAL AREA, HOLE NR 12 AT WS 230.415. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: RIB — CRACKED (RT WING) · airframe 24,346 hrs · 21,836 cycles

RIGHT WING BATT RIB CRACKED AT RWS 53.6. REPAIRED IAW BOMBARDIER REO 601R-57-51-046 REV B.

Part: RIB — CRACKED (LT WING) · airframe 24,346 hrs · 21,836 cycles

LT BATTERY RIB CRACKED AT WS 53.60. REPAIRED IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 2.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

DOUBLER AT FS 589-613 S-19L-22L TEMP REPAIRED IAW BSC EO 601R-53-15724 AND BOMBARDIER REO 601R-53-61-3361. PERMANENTLY REPAIRED IAW BOMBARDIER REO 601R-53-61-4071.

Part: SKIN — DAMAGED (BS 409) · airframe 24,346 hrs · 21,836 cycles

SECOND FASTENER BELOW STRINGER 13R AT FS 409+16 HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK MEASURING 0.500"L X 0.400"W X 0.003" DEEP. REPAIRED IAW REO 601R-53-00-419, REPAIR 13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,346 hrs · 21,836 cycles

SERVICE DOOR THRESHOLD VERTICAL FLOOR SUPPORT FROM FS 319.00 TO FS 349 IS CORRODED. REPAIRED IAW SRM 51-42-21, 51-42-06, 51-42-13.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

ONE FASTENER LOCATED AT FS 439 BETWEEN S-5L AND S-6L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK 0.050" DIAMETER X 0.013" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 5.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

THE THIRD FASTENER FWD OF FS 364.00 AT S-8L HAS LIGHTNING STRIKE DAMAGE AND AREA HAS BEEN PREVIOUSLY BLENDED 0.400" DIAMETER 0.005" DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 16.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

ONE FASTENER LOCATED AT FS 409+32 BETWEEN S-7L AND S-8L HAS LIGHTNING STRIKE DAMAGE ON OUTER PERIMETER OF COUNTERSINK 0.075"L X 0.050"W X 0.007" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 19.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FASTENER AFT OF FS 424 AT S-10R HAS LIGHTNING STRIKE DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 7.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FASTENER AFT OF FS 513 BETWEEN S-10R AND S-11R HAS LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 6.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

THE SECOND FASTENER AFT OF FS 409+80 IN S-6L HAS LIGHTNING STRIKE DAMAGE ON COUNTERSINK 0.180"L X 0.070"W X 0.021" DEEP. REPAIRED IAW BOMBARDIER REO REO 601R-53-00-419 REPAIR 18.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FASTENER AFT OF FS 409+81 BETWEEN S-26L AND S-27 HAS LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 1.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

THE FIRST FASTENER FWD OF FS 409+48 IN S-27 HAS LIGHTNING STRIKE DAMAGE AROUND ENTIRE PERIMETER OF COUNTERSINK AND DAMAGE TO FASTENER HOLE MAX DEPTH 0.009". REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 2.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

CABIN WINDOW FRAME SCREW COUNTERSINK JUST AFT OF FS 409+48 LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 11.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FASTENER HOLE AT FS 409+32 IN S-13R LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 12.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FIRST FASTENER AFT OF FS 235 ON S-16R HAS LIGHTNING STRIKE DAMAGE ON FASTENER HEAD. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 14.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FOURTH FASTENER FWD OF FS 409+112 AT S-11R HAS LIGHTNING STRIKE DAMAGE TO COUNERSINK 0.125"L X 0.050"W X 0.013" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 8.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

THE FIRST BELOW S-13R AT FS394 HAS LIGHTNING STRIKE DAMAGE AROUND THE OUTSIDE PERIMETER OF COUNTERSINK 0.325"L X 0.525"W X 0.004" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 OP91.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FOURTH FASTENER AFT OF FS 473 IN S-5L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK .1"L X 0.05" X 0.010" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 4.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

THIRD FASTENER FWD OF FS 379 AT S-8L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 15.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FASTENER BETWEEN FS 409+64 AND 409+80 IN S-12R HAS LIGHTNING STRIKE DAMAGE IN COUNTERSINK 0.400"L X 0.0450"W X 0.005" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 10.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

PRESSURE BULKHEAD AT FS 202.75 LBL 23.75 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-563 REV A TYPE 1 AND BSC SR 601R-53-0101A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,346 hrs · 21,836 cycles

FS 280 BULKHEAD AFT FLOOR SUPPORT ANGLE CRACKED ON AFT SIDE UPPER RADIUS IN TWO PLACES (RBL 9 AND LBL 9). REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.

Part: BULKHEAD — CORRODED (BS 280) · corrosion level 2 · airframe 24,346 hrs · 21,836 cycles

FS 280 BULKHEAD LOWER WEB IS CORRODED FROM LBL 9 TO RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.

Part: BRACKET — OUT OF ADJUST (LANDING GEAR) · airframe 23,423 hrs · 21,027 cycles

GEAR DISAGREE. DEFERRED GEAR IAW MEL. FOUND PROXIMITY TARGET MOUNTING BRACKET OUT OF ADJUSTMENT, REPOSITIONED, OPS CHECK GOOD IAW AMM 32-61-05-400-804. THIS CLEARS DM 34876.

Part: SEAL — MISSING (WINDSHIELD) · airframe 23,244 hrs · 20,830 cycles

DURING ARRIVAL IN MILWAUKEE, WI (MKE), THE FLIGHT CREW REPORTED AN AIR NOISE IN THE FLIGHT DECK AREA. A CABIN PRESSURE FLUCUATION WAS ALSO REPORTED BUT NOT ABLE TO BE QUANTIFIED. UPON FURTHER INSPECTION, A 1.5 INCH PORTION OF THE SEAL BETWEEN THE MAIN WINDSHIELDS AT THE UPPER END OF THE CENTER POST WAS FOUND MISSING. ALSO, AT THE LOWER AFT CORNER OF THE FIRST OFFICER MAIN WINDSHIELD AT THE I-STRAP THE SEALANT HAS FLOWED AND WAS NOT CURED PRIOR TO FLIGHT AFTER THE I-STRAP WAS INSTALLED. NO OTHER DISCREPANCIES WERE NOTED DURING THE POST FLIGHT INSPECTION. ONE TIME FERRY FLIGHT FROM MKE TO TYS IAW STS ENGINEERING EA 5-2010-265 AND PA 56-010 WHERE THE WINDSHIELD SEALANT WAS PROPERLY INSTALLED IAW CRJ 200 AMM 56-11-01.

Part: SKIN — DENTED (FLAP VANE) · airframe 23,092 hrs · 20,679 cycles

LEFT OUTBOARD FLAP VANE HAD A DENT IN THE VANE LEADING EDGE SKIN APPROXIMATELY 9 INCHES FROM THE INBOARD EDGE AT WS 181.5. THE DAMAGE MEASURES 1.6 INCHES LONG BY 0.9 INCH WIDE WITH A MAXIMUM DEPTH OF 0.095 INCH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-219. REPEAT INSPECTIONS EVERY 250 FH. AT NEXT C-CHECK, NOT TO EXCEED 2500FH, PERMANENT REPAIR IAW CRJ-200 SRM 57-53-00, FIGURE 202, REPAIR NR 1, REPAIR TO FLAP VANE SKIN OR REPLACE THE DAMAGED SECTION WITH A NEW, SERVICEABLE P/N 601R14571-7 LEADING EDGE SKIN.

Part: ECU — FAILED (TE FLAP) · airframe 22,859 hrs · 20,456 cycles

FLAPS FAIL CAUTION AT FL210 FLAPS AT 0 DEGREES, LANDING WITH 0 DEGREE FLAPS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I), AMOC DATED MARCH 27, 2009, TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REMOVED AND REPLACED FECU IAW AMM 27-51-01. FECU CODES 12 1A, 12 2A. OPC GOOD. PROBABLE CAUSE LT BPSU, FECU, WIRING LT BPSU.

Part: SENSING ELEMENT — MALFUNCTIONED (MLG) · airframe 22,282 hrs · 19,892 cycles

MLG OVERHEAT FAIL FOLLOWED BY MLG OVERHEAT WARNING. T/S WIRING PER FIM 26-10-00. REMOVED AND REPLACED RT WHEEL BIN HEAT SENSING ELEMENT IAW AMM 26-14-04. OPS CHECK GOOD. OK FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 17,344 hrs · 15,558 cycles

CREW REPORTED A LAV SMOKE WARNING WHICH WAS CONFIRMED BY FLIGHT ATTENDANT. ENGINE WAS SHUT DOWN AT THE GATE AND MAINTENANCE WAS CALLED. MAINTENANCE TROUBLESHOT LAV SMOKE DETECTOR AND FOUND NO DISCREPANCIES. FURTHER INVESTIGATION LED TO A BOROSCOPE OF THE LT ENGINE WHICH REVEALED A LEAKING NUMBER THREE BEARING CARBON SEAL. AIRCRAFT WAS FERRIED TO A MAINTENANCE BASE FOR CARBON SEAL REPLACEMENT.

Part: APU — LEAKING (APU BAY) · airframe 15,091 hrs · 13,655 cycles

THE AIRCRAFT WAS BOARDING PASSENGERS AT KXNA WHEN THE CABIN BEGAN TO FILL WITH OIL SMOKE. BOARDING WAS SUSPENDED AND ALL PASSENGERS WERE REMOVED FROM THE AIRCRAFT. CFR RESPONDED AS A PRECAUTION. NO EVIDENCE OF FIRE WAS NOTED, BUT THERE WAS A PUDDLE OF OIL UNDER THE TAIL OF THE AIRCRAFT. MAINTENANCE DETERMINED THAT THE SOURCE OF THE OIL WAS THE APU. WITH THE APU DEFERRED, THE AIRCRAFT WAS LOADED AND DEPARTED KXNA. DURING CLIMB-OUT, A "SMOKE, TOILET" WARNING ILLUMINATED AND THE FLIGHT ATTENDANT ADVISED OF SMOKE IN CABIN. AN EMERGENCY WAS DECLARED AND AN OTHERWISE UNEVENTFUL LANDING WAS MADE AT KXNA. THE AIRCRAFT WAS STOPPED ON THE RUNWAY AND THE PASSENGERS DEPLANED THROUGH THE MAIN CABIN DOOR. MAINTENANCE

Part: ENGINE — FAILED (NR 2)

(REF NR: 05-064) ON CLIMB OUT, AT ABOUT FL303, THERE WAS A LOUD BANG AND THE NR 2 ENGINE ITT SPIKED. THIS WAS FOLLOWED BY A LOSS OF N1 AND OIL PRESSURE. FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND DECLARED AN EMERGENCY. THE PIC REQUESTED AND RECEIVED PERMISSION TO DIVERT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MAINTENANCE DETERMINED PROBLEM TO BE 2 BROKEN INLET GUIDE VANE ACTUATOR ARMS. THIS ENGINE WAS REMOVED AND WILL BE SENT FOR REPAIR. (K)

Part: ACM — MALFUNCTIONED (RIGHT)

LAVATORY EICAS SMOKE INDICATION IN FLIGHT. TROUBLESHOT PROBLEM TO THE RT AIR CYCLE MACHINE. DEFERRED RIGHT ACM IAW MEL.

Part: ODOR — DETECTED (LAVATORY)

CREW RECEIVED EICAS TOILET SMOKE INDICATION, THERE WAS A SLIGHT SMOKY HAZE IN THE VICINITY OF THE LAVATORY AS WELL AS A STRONG SMELL OF BURNED PLASTIC. QRH FOLLOWED UNEVENTFUL UNSCHEDULED RETURN TO AIRPORT. RAN CABIN PACK, INSPECTED AND OPERATIONALLY CHECKED LAV SMOKE DETECTOR. OPS CHECK GOOD IAW MM. NO EVIDENCE OF SMOKE. PERFORMED TEST FLIGHT, ALSO NO EVIDENCE OF SMOKE. AIRCRAFT OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY)

CREW RECEIVED EICAS TOILET SMOKE INDICATION ALONG WITH VISIBLE SMOKE IN AFT CABIN AND LAVATORY QRH FOLLOWED UNEVENTFUL UNSCHEDULED RETURN TO AIRPORT. PERFORMED ENGINE RUNS AND OPERATIONAL CHECKS OF BLEED AIR SYSTEM WITH NO DEFECTS NOTED.

Part: PIN — OUT OF POSITION (COWLING)

EN ROUTE TO MONTEREY, MEXICO THE FLIGHT CREW DISCOVERED THAT THE THRUST LEVER OF THE LEFT ENGIEN COULD NOT BE REDUCED BELOW 97 PERCENT N1. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL FOR POSSIBLE RESOLUTION. AFTER CONFERRING WITH MAINTENANCE ENGINEERING, IT WAS DECIDED TO HAVE THE AIRCRAFT RETURN TO MEMPHIS, USING THE APPROPRIATE CHECKLISTS AND AN OTHERWISE NORMAL LANDING WAS MADE. MAINTENANCE FOUND THAT THE PIN LOCKING THE COWLING STAY ROD IN THE STOWED POSITION HAD BACKED OUT ALLOWING THE STAY ROD TO FALL DOWN AND JAM THE ENGINE CONTROL LINKAGE. FURTHER INSPECTION OF THE PIP TYPE PIN FOUND TAHT ONE OF THE LOCKING BALLS WAS MISSING. (M)

Part: HANDLE — DEFECTIVE (MLG)

UPON TAKEOFF OUT OF MEMPHIS, GEAR WAS SELECTED UP AND THE GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO MEMPHIS WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL HANDLE THAT WAS INSTALLED ON 8/11/2000 WAS DEFECTIVE. REPLACED LANDING GEAR CONTROL HANEL PERFORMED GEAR SWINGS AND OPERATIONAL TEST FLIGHT, NO FURTHER DEFECTS NOTED. (M)

Part: HANDLE — BROKEN (COCKPIT)

AFTER TAKEOFF UPON A GEAR RETRACTION, THE LANDING GEAR HANDLE SHAFT BROKE. AIRCRAFT RETURNED TO BASE AND LANDED SUCCESSFULLY. REDESIGN OF LANDING GEAR HANDLE WAS DONE AND AWAITING APPROVAL FROM CANADAIR. (X)

Part: HANDLE — BROKEN (MLG)

LANDING GEAR CONTROL HANDLE BROKE OFF IN PILOT''S HAND WHILE ATTEMPTING TO RETRACT GEAR. GEAR DID NOT RETRACT. REMOVED AND REPLACED GEAR HANDLE ASSEMBLY. (M)