N8543F

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 26,911 hrs · 23,742 cycles

OBSERVER`S LIFE VEST HAS HOLE IN BAG. R & R OBSERVER`S LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,535 hrs · 23,351 cycles

EMERGENCY FLOOR LIGHTING AT ROW 2 INOPERATIVE. R & R IAW AMM 33-51-01.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 26,492 hrs · 23,306 cycles

EMERGENCY LIGHT EXIT ROW INOPERATIVE. R & R TRACK EMERGENCY LIGHT STRIP AND CABLE IAW AMM 33-51-01. OPC EMERGENCY LIGHTING IAW AMM 33-51-00. OK FOR SERVICE.

Part: SEAL — TORN (EMERGENCY EXIT) · airframe 26,474 hrs · 23,279 cycles

RIGHT OVERWING EMERGENCY EXIT SEAL IS TORN. REMOVED TORN SEAL AND REPLACED RT OVERWING EMERGENCY EXIT SEAL IAW MM 52-21-07-946-004.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,135 hrs · 22,941 cycles

CEILING LEVEL EMERGENCY LIGHT NR 1 BURNED OUT. R & R EMERGENCY FLOOD LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: HINGE — GOUGED (TE FLAP) · airframe 25,863 hrs · 22,682 cycles

RIGHT INBOARD FLAP OUTBOARD HINGE ARM GOUGED IN 2 PLACES. REPAIRED IAW BOMBARDIER REO 601R-57-54-237.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,319 hrs · 22,141 cycles

FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERABLE. REMOVED AND REPLACED FORWARD EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-50-01. OPS CHECK GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 25,060 hrs · 21,891 cycles

FLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED LIFE VESTS IAW AMM 25-61-03.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,894 hrs · 21,727 cycles

EMERGENCY FLOOR TRACK LIGHTING FROM ROWS 2-5CD INOPERABLE, AND LEFT OVERWING FLOOR PROX LIGHT INOPERABLE. TROUBLESHOOT PER WM 33-51-00. FOUND NR 2 EMERGENCY LIGHT BATTERY INVERTER INOPERABLE. REMOVED AND REPLACED INVERTER IAW AMM 33-51-07. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,752 hrs · 21,589 cycles

FORWARD 3 SECTIONS OF EMERGENCY FLOOR-TRACK LIGHTING INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW AMM 33-51-04. OPS CHECK GOOD.

Part: THRUST REVERSER — INOPERATIVE (LEFT) · airframe 24,687 hrs · 21,515 cycles

LEFT THRUST REVERSER INOPERATIVE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 24,649 hrs · 21,482 cycles

EMERGENCY FLASHLIGHT IN FLIGHT ATTENDANT SEAT CLOSET, LED INDICATOR INOPERATIVE. REPLACED FLASHLIGHT BATTERY IAW CMM 25-60-02.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 24,574 hrs · 21,410 cycles

LEFT THRUST REVERSER INOPERATIVE. REMOVED AND REPLACED RELAY 1K2KE AT JB-10 IAW WM 91-32-10. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 24,528 hrs · 21,366 cycles

LEFT FLOOR SUPPORT OVERWING BOX AREA CORRODED. REPAIRED IAW REO 610R-53-41-666.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 24,528 hrs · 21,566 cycles

AFT PRESSURE BULKHEAD FWD FACE HAS MULTIPLE AREAS WITH SMALL CHAFES AND BARE MATERIAL. REPAIRED IAW SRM 53-00-31/53-61-19.

Part: STRIP — MISSING (CABIN) · airframe 24,132 hrs · 20,981 cycles

ORANGE STRIP MISSING FROM EMERGENCY EXIT FLOOR STRIP LIGHT AT SEAT 1C. REMOVED AND REPLACED ORANGE LIGHT STRIP AT ROW 1C IAW AMM 33-51-01. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 23,970 hrs · 20,826 cycles

LEFT THRUST REVERSER WILL DEPLOY (AND GET GREEN REV ICON) BUT THROTTLES WILL NOT ADVANCE. LEFT THRUST REVERSER OPS CHECKED NORMAL IAW AMM 78-30-00

Part: CONTROL SYSTEM — OUT OF RIG (THROTTLE SYS) · airframe 23,970 hrs · 20,826 cycles

LT & RT ENGINES HAVE MORE THAN 1/2 KNOB SPLIT AT THROTTLES AT POWER OF DAY. /R LT MAIN FUEL CONTROL IAW AMM 73-21-01. OP/C & LEAK CHECK GOOD. PROBLEM CONTINUED. FOUND RT THROTTLE CONTROL SYSTEM OUT OF RIG RIGGED PER AMM 76-10-00 AND VG FEEDBACK RIGGED PER AMM 75-31-03. ALL OP/C, FUNC/CHECK GOOD. ALL PARAMETERS WITHIN AMM LIMITS IAW AMM 71-00-00.

Part: UNKNOWN — MALFUNCTIONED (AILERON TRIM) · airframe 23,710 hrs · 20,581 cycles

AILERON TRIM WILL NOT TRIM TO LEFT WORKS TO RIGHT BUT NOT LEFT. COULD NOT DUPLICATE PERFORMED OPC OF AILERON TRIM. NO DEFECTS NOTED. OPC GOOD IAW CRJ 200 AMM 27-11-00. OK FOR SVC. ALL IND NORMAL.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 23,694 hrs · 20,563 cycles

FRONT 3 FORWARD EMERGENCY LIGHTS UNPLUGGED AND CAME LOOSE FROM FLOOR TRACK. RE-SECURED LIGHT STRIP SECTION AS REQUIRED. OP'S CHECK OF LIGHTS GOOD IAW CRJ200 AMM 33-50-00. ALL CHECKS GOOD.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 23,446 hrs · 20,328 cycles

FLAPS FAIL AT 16 DEGREES ON DEPARTURE. T/S PER FIM 27-50-00. FOUND NR 2, 3, 4, 1 ACTUATORS ON RT WING BAD.  REMOVED AND REPLACED ACTUATORS IAW AMM 27-53-01, AMM 27-53-05. OK FOR SVC.  XFER TO AML PAGE 2230543 C/W PA AD 27-052G.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 23,437 hrs · 20,320 cycles

AIR RETURN FOR FLAPS FAIL IN FLT AT 16 DEGREES. REMOVED AND REPLACED ACTUATOR, OPS CHECK GOOD.

Part: FLEX DRIVE — DAMAGED (TE FLAP) · airframe 23,407 hrs · 20,284 cycles

AIR RETURN FOR FLAP FAIL CAUTION MESSAGE FLAPS 13 INDICATION QRH FLAPS FAIL COMPLETE. 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 DECEMBE 18, 2009 AND PA AD 27-052G. FOUND LT FLAP ACTUATOR FLEX SHAFTS 1-5 DAMAGED AND RT FLAP ACTUATOR FLEX SHAFTS&5 DAMAGED, LT + RT FLEX SHAFTS WERE REPLACED IAW AMM 27-53-10. ALSO PERFORMED FLAP SYSTEM LUBE IAW CHECKLIST PROVIDED. FLAP SYS CHECKS NORMAL IAW AMM 27-50-00.

Part: FLEX DRIVE — MALFUNCTIONED (TE FLAP) · airframe 23,327 hrs · 20,676 cycles

FLAPS FAIL AT 16 DEGREES DURING FLAP RETRACTION RETURN LANDING AT MSP VSI LESS THAN 100 FPM UPON LANDING. REMOVED, INSPECTED, LUBRICATED, AND RE-INSTALLED FLEXIBLE SHAFTS NR 1, 2, AND 5 IAW CRJ AMM 27-53-10. REMOVED, INSPECTED, LUBRICATED, AND RE-INSTALLED FLEXIBLE SHAFTS NR 1, 2, AND 5 IAW CRJ AMM 27-53-10. COMPLIED WITH P.A. AD27-025G BY T/S PER FIM, REMOVED AND REPLACED RT BPSU SEE AML 2234142, INSPECTED, AND LUBRICATED LEX SHAFTS NR 3, AND NR 4 SEE AML 2234142 BLOCK NR 2, AND FOR FLEX SHAFTS NR 1, 2, AND 5. OPS CHECKED AND RIG CHECKED OF FLAPS NORMAL. INVESTIGATED PSEU AND FOUND CODES REMOVED AND REPLACED RT BPSU PER AMM 27-51-10. OPS CHECKED AND RIG CHECKED OF FLAPS NORMAL.

Part: STRIP — DAMAGED (CABIN) · airframe 23,218 hrs · 20,161 cycles

ORANGE FLOOR EMERGENCY STRIP DAMAGED. REMOVED AND REPLACED ORANGE FLOOR STRIP IAW AMM 33-51-01. OPS CHECK GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 23,174 hrs · 20,121 cycles

AP TRIM IS LWD CAUTION MSG IN FLIGHT FOLLOWED BY AP DISCONNECTING. RETRIMMED RE ENGAGED AP AND 1 MIN LATER IT DISCONNECTED AGAIN. PERFORMED OPS CHECK OF AUTOPILOT IAW AMM 22-11-00. ALL OPS CHECKS NORMAL. NO CODES STORED IN FCC. OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,228 hrs · 20,114 cycles

RT FUEL LO PRESS CAUTION IN FLT COMES ON WHEN RT THRUST LEVER IS AT IDLE. PERFORMED OPC OF RT FUEL PSI SWITCH IAW AMM 73-31-06. OPC GOOD. OK FOR SVC.

Part: FLAP — FAILED (WING) · airframe 22,477 hrs · 19,408 cycles

FLAPS FAILED ON DESCENT. PRIOR TO LANDING FLAPS SELECTED TO 30 WITH THEM AT 20 HANDLE SLIPPED TO ALMOST 40 THEN MOVED BACK TO 30 AND GOT THE FF MSG. DEFERRED PER MEL 27-50-00 AUTH 47470.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,826 hrs · 18,804 cycles

FOUND FS 559 SEMI PRESSURE BULKHEAD HAS INDICATION NOTED AT RT WEB RBL 18 AND LBL 18 CAP ANGLE, ALL GREATER THAN 50 PERCENT SCREEN HEIGHT, FAILED NDT INSPECTION. REPAIR IAW BOMBARIDER REO 601R-53-41-260 REV E, BOMBARDIER REO 601R-53-41-609 REV B DEVIATION E, AND BOMBARDIER SERVICE CORPORATION EO 601R-53-21039 AND SR 601R-53-0114.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,654 hrs · 18,670 cycles

SUSPECTED DE-ICE FLUID IN CABIN AIR SYSTEM. BURNING TYPE 1 SMELL OCCURRED ABOUT 10 SECONDS AFTER TAKEOFF WITH SMOKE TOILET CAUTION MESSAGE. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTURE POINT. POST LANDING INVESTIGATION DID NOT REVEAL EVIDENCE OF FIRE. CREW SUSPECTS EXCESSIVE DE-ICE FLUID SPRAYED ON THE REAR OF THE AIRCRAFT. NO RELATED DISCREPANCIES INDICATED.

Part: COALESCER BAG — CONTAMINATED (AC BAY) · airframe 21,496 hrs · 18,500 cycles

SMOKE TOILET AIRCRAFT DE-ICED PRIOR TO FLIGHT CAUTION CAME ON AFTER TAKEOFF FOUND LT AND RT COALESCER BAGS CONTAMINATED. REMOVED AND REPLACED LT AND RT COALESCER BAGS IAW CRJ AMM 21-51-13, RAN ENGS LEAK AND OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 21,305 hrs · 18,355 cycles

L COWL A ICE CAUTION WITH SWITCH SELECTED OFF ON CLIMBOUT. REMOVED AND REPLACED LT COWL ANT-ICE VALVE IAW AMM 30-22-01, OPS CHECKS GOOD.

Part: SKIN — DAMAGED (BS 640-682) · airframe 21,056 hrs · 18,093 cycles

THE FUSELAGE SKIN AT FS 640 TO FS 682 AND BETWEEN STRINGERS 15L AND 20L IS DAMAGED. REPAIRED FUSELAGE SKIN AT FS 640 TO 682 IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-53-19713.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,056 hrs · 18,093 cycles

SIDE SEAT TRACK CORRODED BELOW RT AND LT OVERWING EXITS BETWEEN FS 473.15 AND FS 513.00. REMOVED AND REPLACED SIDE SEAT TRACKS IAW CRJ 200 AMM 53-01-11-400-802.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,056 hrs · 18,093 cycles

THE FUSELAGE SKIN AT FS 625.3 TO FS 640 AND BETWEEN STRINGERS 19L AND 20L IS DAMAGED. REPAIRED FUSELAGE SKIN AT FS 625.3 TO 640 IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-53-19741.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,056 hrs · 18,093 cycles

THE FUSELAGE SKIN AT FS 589 TO FS 605 AND BETWEEN STRINGERS 21R AND 26R IS DAMAGED. REPAIRED FUSELAGE SKIN AT FS 589 TO 605 IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-53-19742.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,056 hrs · 18,093 cycles

FLOOR SEAT TRACK CORRODED AT FS 379.00 RBL 9. REMOVED AND REPLACED FLOOR SEAT TRACK BETWEEN FS 364.00 AND FS 399.50 AT RBL 9 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,066 hrs · 17,185 cycles

REAR PRESSURE BULKHEAD FS 621.00 AT LINTEL FITTING FOUND CRACK .200 INCH LONG, 90 PERCENT FSH, FAILED NDT. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230 REV D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,026 hrs · 17,159 cycles

CRACKED REAR PRESSURE BULKHEAD FS 621.00, LBL 27.50, WL 130.00, APPROX .200 INCH LONG AT TOP OF CARGO DOOR AFT TRACK. NDT INSPECTION FAILED. REPAIRED CRACK IAW BOMBARDIER REO 601R-53-61-1541 REV B.

Part: UNKNOWN — UNKNOWN (LANDING GEAR)

ON CLIMB OUT RECEIVED GEAR DISAGREE WHEN GEAR SELECTED UP. QRH FOLLOWED AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. PERFORMED TROUBLESHOOTING PER FIM AND AMM GEAR SWINGS PERFORMED WITH NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER)

DURING DESCENT TO DTW THE LT THRUST REVERSER UNLOCKED MSG ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH PROCEDURES AND DECLARED AN EMERGENCY. THERE WERE NO ADVERSE ACFT HANDLING ISSUES. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KDTW. MX INSPECTED THE THRUST REVERSER AND FOUND NO PROBLEMS WITH IT. AFTER AN OP CHECK OF THE REVERSER, THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL SYSTEM — FAILED (TE FLAPS) · airframe 8,593 hrs · 8,443 cycles

FLAP FAILURE ON TAXI-OUT. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.