N819AY

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,270 hrs · 28,215 cycles

FOUND EXTERIOR EMERGENCY LIGHT 2 INOPERATIVE. REPLACED THE LAMPS, AND PERFORMED OPS TEST OF THE MERGENCY LIGHTS IAW AMM 33-51-00. TESTED NORMAL.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,720 hrs · 25,450 cycles

FS 621 AFT PRESSURE BULKHEAD REQUIRES GREO 601R-53-61-1240 MOD TO BE PERFORMED DUE TO THE AMOUNT OF CRACKS AND PREVIOUS REPAIRS DAMAGED REMOVED IAW CRJ 200 REO 601R-53-61-1240 REV D

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 27,720 hrs · 25,450 cycles

MID CABIN FWD FACING EMERGENCY LIGHT INOP. CONNECTED CONNECTOR P63/J63, P56/J56 IAW CRJ 200 WDM 33-51-00 AND ESPM 20-17-00 RESEATED EMER LIGHT CHARGER BATTERY CONNECTOR IAW CRJ 200 WDM 33-51-00 AND ESPM 20-17-00 OPS TEST GOOD IW CRJ 200 AMM 33-51-00. AAR TECH RE-13, INSP A-330

Part: ATTACH ANGLE — CORRODED (BS 333) · airframe 27,720 hrs · 25,450 cycles

ANGLE CLIP HAS CORROSION ON THE O/B SIDE OF INTERCOSTAL THAT SITS ON STGR 23R AND FWD SIDE OF FRAME 333, IN THE FWD E & E BAY. REMOVED/REPLACED ANGLE CLIP AT FS333 AND STRG 23R IAW CRJ 200 SRM 51-42-06

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

CORROSION ON STRAP OTBD STR 23R FWD FS333 GOING FWD APPROXIMATELY FIVE INCHES. REPAIRED DAMAGE IAW EA 253-08071 REV IR.

Part: SKIN — CHAFED (TE FLAP) · airframe 27,720 hrs · 25,450 cycles

RT IB FLAP VANE L/E CHAFED IN 3 LOCATIONS. REMOVED AND REPLACED 3 EA RT INBOARD FLAP VANE L/E SKINS IAW SRM 51-42-10.

Part: STRIKER — CRACKED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

AFT EQUIP COMPARTMENT DOOR SEAL STRIKER IS BENT ON FWD RT CORNER. REMOVED AND REPLACED AFT EQUIP COMPARTMENT DOOR SEAL STICKER IAW SRM 51-42-06.

Part: RIB — CRACKED (RT FAIRING) · airframe 27,720 hrs · 25,450 cycles

RIGHT ENGINE TAIL PIPE FAIRING INTERNAL RIB HAS EVIDENCE OF CRACK. REMOVED AND REPLACED TAIL PIPE FAIRING INTERNAL RIB (STIFFENER) IAW CMM 20-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SEAT TRACK 4 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 27,720 hrs · 25,450 cycles

PAX DOOR HAS CRACK IN CORNER UNDER THIRD STEP REMOVED AND REPLACED STIFFNER

Part: FRAME — CORRODED (BS 333) · airframe 27,720 hrs · 25,450 cycles

FRAME 333 HAS CORROSION ON THE AFT SIDE BETWEEN STGR 26L AND 26R, IN THE E&E BAY REMOVED DAMAGED FRAME SECTOR AND REPLACED WITH NEW FRAME SECTOR I.A.W. CRJ-200 SRM 57-42-06

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 6 IAW AMM 53-01-11.

Part: SPLICE PLATE — CORRODED (BS 319.7) · airframe 27,720 hrs · 25,450 cycles

SPLICE PLATE HAS CORROSION ON THE FWD I/B SIDE OF THE SERVICE DOOR OPENING AT FS 319.70 JUST ABOVE THE FLOOR, IN THE CABIN. REMOVED AND REPLACED SPLICE PLATE ANGLE AT FS319.7 IAW CRJ 200 SRM 51-42-06, 51-42-13 AND 51-42-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SIDEWALL SEAT RACK STICK 7 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 7 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS, IN THE CABIN. INSTALLED NEW SEAT TRACK STICK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS, IN THE CABIN. REMOVED & REPLACED NEW SIDEWALL SEAT TRACK IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF LBL 27 AT FS 473.15, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF RBL 27 AT FS 473.15. REMOVED AND REPLACED CRACKED CUP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 2 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 4 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 3 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED R/H SIDEWALL SEAT TRACK STICK 2 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 27,720 hrs · 25,450 cycles

LH AISLE SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT AISLE SEAT TRACK STICK 4 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT AISLE SEAT TRACK STICK 4 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 55-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED RT AISLE SEAT TRACK STICK 1 IAW AMM 53-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

LT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS, IN THE CABIN. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

SEAT TRACK ON LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK LBL9 IN CARGO BAY IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

SEAT TRACK ON RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK RBL 9 IN CARGO BAY IAW AMM 53-00-49.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,550 hrs · 25,278 cycles

DAMAGE REQUIRES CUT OUT. CUT OUT DAMAGE IAW SRM 51-70-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,776 hrs · 24,415 cycles

MID EXTERNAL EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP ON RH FUSELAGE. IAW CMM 33-41-41. CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,558 hrs · 24,142 cycles

ON WAKE UP, FOUND THE FIRST OFFICER`S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02, OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,123 hrs · 23,662 cycles

CAPTAIN`S SIDE FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 25,772 hrs · 23,270 cycles

FORWARD WARDROPE EMERGENCY FLASHLIGHT NOT INDICATING CHARGING. REPLACED THE FLASHLIGHT ASSY AND OPS CHECK GOOD IAW AMM 25-61-02

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 24,702 hrs · 22,161 cycles

FIRST OFFICER`S SIDE EMERGENCY FLASHLIGHT BATTERY LOW. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 25-61-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,933 hrs · 21,393 cycles

LEFT EXTERNAL EMERGENCY LIGHT JUST FWD OF WING INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 23,789 hrs · 21,243 cycles

FLOOR SUPPORT IS CORRODED ON I/B SIDE AT NUT PLATE HOLES FROM BS 310 - 349. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21.

Part: HOUSING — CRACKED (E/E DOOR HANDLE) · airframe 23,789 hrs · 21,243 cycles

AVIONICS BAY DOOR HANDLE HOUSING CRACKED (NDT VERIFIED). REMOVED AND REPLACED THE HOUSING IAW SRM 51-40-11. OPS CHECKED GOOD IAW AMM 52-42-00-710-801 STEP 2A AND 52-70-08-710-801 STEP 3.

Part: BULKHEAD — GOUGED (BS 621) · airframe 23,789 hrs · 21,243 cycles

AFT PRESSURE BULKHEAD BS 621 LBL 18 IS GOUGED OUT OF LIMITS. REPAIRED IAW REO 601R-53-61-1286.

Part: BULKHEAD — GOUGED (BS 621) · airframe 23,789 hrs · 21,243 cycles

AFT PRESSURE BULKHEAD BS 621, RBL 18 GOUGED OUT OF LIMITS. REPAIRED IAW REO 601R-53-61-1286.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 23,789 hrs · 21,243 cycles

FLOOR SUPPORT ATTACHMENT ON LBL 27 HAS CORROSION ON BOTH THE INBD AND OTBD LANDINGS BETWEEN BS 605 - 621 IN THE CARGO BAY. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT ATTACHMENT IAW SRM 51-42-06, 51-42-34, 51-41-04.

Part: BULKHEAD — GOUGED (BS 621) · airframe 23,789 hrs · 21,243 cycles

AFT PRESSURE BULKHEAD BS 621, RBL 36 FOUND GOUGED OUT OF LIMITS. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1286.

Part: STRUCTURE — CRACKED (NR 2 EXHAUST) · airframe 23,789 hrs · 21,243 cycles

NR 2 ENGINE EXHAUST NOZZLE FAIRING DOOR CUT OUT CRACKED. REMOVED AND REPLACED THE NR 2 EXHAUST NOZZLE FAIRING DOOR CUT OUT LANDING IAW CMM 78-11-00.

Part: FAIRING — CRACKED (NR 1 EXHAUST) · airframe 23,789 hrs · 21,243 cycles

NR 1 ENGINE EXHAUST NOZZLE FAIRING DOOR CUTOUT AT LOWER ATTACH POINT FOUND CRACKED IN TWO PLACES. REPAIRED THE EXHAUST FAIRING DOOR CUTOUT IAW CMM 78-11-00.

Part: WEB — CRACKED (BS 193) · airframe 23,789 hrs · 21,243 cycles

TRU FLOOR HAS A CRACK ON THE LT SIDE AT FWD FRAME BS 193.0. REPAIRED THE FLOOR WEB IAW REO 601R-53-11-111.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 23,789 hrs · 21,243 cycles

FLOORBEAM ANGLE AT BS 621 LBL 43 IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW REO 601R-53-61-117.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,789 hrs · 21,243 cycles

NOSE HYD COMPARTMENT HAS POSSIBLE CRACK ON AFT BULKHEAD AT PARKING BRAKE CABLE BS 202.75. REPAIRED THE BULKHEAD IAW REO 601R-53-11-563 TYPE IV BA REPAIR.

Part: PLATE — CRACKED (RT WING TE FLAP) · airframe 23,789 hrs · 21,243 cycles

RIGHT OTBD FLAP MID HINGE ASSY INBD SIDE, GUIDE PLATE IS CRACKED. REMOVED AND REPLACED THE GUIDE PLATE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,789 hrs · 21,243 cycles

FLOOR SUPPORT LBL 27 HAS CORROSION BETWEEN BS 559+112 - 621, IN THE CARGO BAY. REPAIRED THE FLOOR SUPPORT IAW EA CRJ253-04424.

Part: DOUBLER — CRACKED (ACCESS PANEL) · airframe 23,789 hrs · 21,243 cycles

DOUBLER FOR NUTPLATE ON ACCESS PANEL 446BR IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW NUTPLATE DOUBLER IAW CMM 20-42-06.11

Part: BULKHEAD — NOT REPORTED (BS 559) · airframe 23,789 hrs · 21,243 cycles

PRESSURE BULKHEAD AT BS 559 BL 23L-23R. REPAIRED BULKHEAD IAW GREO 601R-53-41-260, GREO 601R53-41-609 AND REO 601R53-41-2068.

Part: STRUT — FLAT (NLG) · airframe 22,997 hrs · 20,425 cycles

AFTER TAKEOFF AT GEAR UP, GOT GEAR DISAGREE & GEAR DOOR OPEN WARNINGS. RAN THE QRH FOR GEAR DOOR OPEN & ALL LG SHOWED DOWN & LOCKED. RETURNED & DID NOT LAND OVERWEIGHT. WHEN WE GOT THE WARNINGS THE NOSE GEAR SHOWED DOWN & LOCKED, THE MAINS SHOWED YELLOW. NLG STRUT COMPLETELY FLAT. IAW NRWC 529784 FOR REPAIR OF NOSE STRUT ASSEMBLY. LG EXTENSION & RETRACTION OPERATIONS CHECKED GOOD IAW AMM 32-30-00, AFTER STRUT WAS REPAIRED, SEE ALSO NRWC 531421 & NRCC FOR DETAILS.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 22,758 hrs · 20,180 cycles

FLIGHT ATTENDANTS FWD FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL 25-61-04, PLACARD INSTALLED & ENTERED IN MMO 2. R & R FLIGHT ATTENDANTS FLASHLIGHT BATTERY PACK IAW AMM 25-61-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE. THIS CLEARS DM 002750. PLACARD REMOVED & MM02 UPDATED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,737 hrs · 20,158 cycles

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

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 21,921 hrs · 19,321 cycles

TWO EACH CABIN EMER PHOTO LUMINESCENT FLOOR LIGHTS DAMAGED. R & R LT SIDE AFT TWO EMER PHOTO LUMINESCENT LIGHTS IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE · airframe 21,815 hrs · 19,205 cycles

THREE BULBS INOPERATIVE IN THE EMER LIGHTS OFF, LIGHT ON THE OH PANEL. ONE BULB INOPERATIVE ON THE RT 10TH SOV BLEED CLOSED POSITION. RELAMPED ASSOCIATED LIGHTS IAW AMM 33-11-00. OPERATIONS CHECKED GOOD.

Part: DOOR SEAL — ICED (CABIN DOOR) · airframe 21,710 hrs · 19,090 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPERATE. REMOVED ICE FROM DOOR SEAL & ICE CUBES FROM DOOR HINGE & THRESHOLD AREA. OPERATIONS CHECKED IAW 52-11-00-710-802.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,339 hrs · 18,714 cycles

EMERGENCY LIGHT 4 INOPERATIVE. R & R LIGHT IAW AMM 33-51-21.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 21,252 hrs · 18,623 cycles

AFT PBE SEAL BROKEN. DEFER FOR ONE FLIGHT CYCLE IAW PBE CMM PRM-01 PG 38 IAW CONTROL 009043 ENTERED INTO MM02. R & R AFT PBE IAW AMM 35-30-00 THI CLEAR DI 9043.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,095 hrs · 18,466 cycles

FLOOR LEVER PAX DOOR & FWD WINDSCREEN EXIT EMER LIGHTS HAVE INOPERATIVE. RELAMPED 3 BULBS IN FWD WINDSCREEN EXIT LIGHT & 2 LAMPS IN THE PAX DOOR FLOOR LEVEL EMER LIGHT IAW AMM 33-51-19.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 21,058 hrs · 18,427 cycles

FS 621 BULKHEAD FWD FACE HAS MULTIPLE SCREW HEAD CHAFES BETWEEN RBL 36.2 - LBL 36.2 & WL 87 - WL 103.5. REPAIRED IAW REO 601R-53-61-2155.

Part: FLAP — CHAFED (RT WING) · airframe 21,058 hrs · 18,427 cycles

RIGHT INBD FLAP LE CHAFED UP TO 0.010 INCHES DEEP. REPAIRED IAW REO 601R-57-52-004.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,058 hrs · 18,427 cycles

LEFT WING LOWER WING PLANK LANDING FOR FUEL ACCESS PANEL 540BB CORRODED 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 21,058 hrs · 18,427 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS MULTIPLE CHAFES BETWEEN 0.002 INCHES & 0.011 INCHES DEEP. REPAIRED IAW REO 601R-53-61-2155.

Part: RIB — CRACKED (LT WING) · airframe 21,058 hrs · 18,427 cycles

LEFT BATTERY RIB CRACKED 0.9 INCHES. REPAIRED IAW REO 601R-57-51-046.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,725 hrs · 16,116 cycles

FLIGHT 3804 AIRCRAFT DIVERTED TO BNA DUE TO CARGO FIRE BOTTLE LOW CAUTION MESSAGE. AIRCRAFT LANDED OVER WEIGHT (47,900LBS, MAX 47,000) AT LESS THAN 300 FPM. NO EMERGENCY WAS DECLARED. DEFERRED CARGO BOTTLE IAW MEL 26-25-01, NO OVERWEIGHT INSPECTION REQUIRED DUE TO TCI REQUIREMENTS. AIRCRAFT WAS THEN RELEASED FOR REVENUE FLIGHT.

Part: THRUST REVERSER — MALFUNCTIONED (LT ENGINE) · airframe 18,511 hrs · 15,910 cycles

CREW REPORTED ON LANDING THE LEFT THRUST REVERSER WOULD NOT DEPLOY, GOT THE YELLOW ICON ON N1.

Part: COVER — CRACKED (EXIT SIGN) · airframe 18,019 hrs · 15,416 cycles

SERVICE DOOR EXIT SIGN LOWER CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT COVER IAW AMM 11-30-00 DM 00132 CLOSED.

Part: SIGN — CRACKED (CABIN) · airframe 18,014 hrs · 15,412 cycles

SERVICE DOOR EXIT SIGN UPPER SIGN CRACKED. REMOVED AND REPLACED SERVICE DOOR EXIT SIGN IAW AMM 33-51-14.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,750 hrs · 15,142 cycles

FOURTEEN TOOLING MARKS AND/OR CHAFES FOUND ON THE FORWARD SIDE OF THE FS 621 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,750 hrs · 15,142 cycles

CRACKS FOUND ON RT AND LT LOWER AND UPPER FLOOR SUPPORT BEAM AND UPPER SUPPORT ANGLE OF FS 280 O/B OF LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO301R-53-11-171 REV D AND REO601R-53-11-136 REV A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,750 hrs · 15,142 cycles

TWO 1 INCH CRACKS ON FORWARD SIDE OF FS 755 BULKHEAD. REPAIRED IAW SRM TR53-28.

Part: PLACARD — MISSING (CABIN) · airframe 17,316 hrs · 14,703 cycles

PASSENGER DOOR PLACARD (EXIT) IS MISSING. INSTALLED NEW PLACARD IAW AMM 11-30-02.

Part: THRUST REVERSER — UNKNOWN (LEFT) · airframe 17,243 hrs · 14,626 cycles

LEFT THRUST REVERSER INOPERATIVE. INSPECTED LEFT THRUST REVERSER. PERFORMED OPS CHECK, IAW AMM 78-30-00. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,236 hrs · 13,643 cycles

DIVERTED TO TYS FOR L REV UNLOCKED CAUTION IN FLIGHT HAPPEND AT 15,000 FT INDICATION ONLY. NO ADVERSE FLIGHT CHARACTERISTICS. OPC LT TR IAW AMM 78-30-00. OPC GOOD.

Part: SWITCH — DIRTY (THRUST REVERSER) · airframe 16,205 hrs · 13,614 cycles

AIR RETURN L REV UNLOCKED CAUTION DURING CLIMBOUT RAN IAI CARD & QRH RETURNED TO DTW NO BUFFETING/YAW ISSUES NORMAL AIRPLANE CONTROL. CLEANED L/H T/R STOW SWITCH. MSG CLEARED. OPC GOOD IAW CRJ AMM 78-30-00.

Part: VALVE — DEFECTIVE (AC BAY) · airframe 15,947 hrs · 13,417 cycles

ON CLIMB WHEN REACHED 11,000 FT RECEIVED A CABIN ALT CAUTION AND THEN RECEIVED CABIN ALT WARN AROUND 10,500 ON THE DESCENT. EMERGENCY DECLARED. COMPLIED WITH MEL 21-24-61. OPC GOOD. OK FOR SERVICE. REMOVED AND REPLACED O/B COOL VALVE IAW AMM 21-24-34. OP/C GOOD. PLACARD REMOVED. VERIFIED PART EFFECTIVITY. CLEARS DM 54966.

Part: FUEL CONTROL — OUT OF RIG (LT ENGINE) · airframe 15,939 hrs · 13,410 cycles

N2 SPLIT OF 2.7 AT IDLE. RIGGED LT FUEL CONTROL IAW AMM 76-10-00 & OPC LT ENG IAW AMM 71-00-00. OK FOR SERVICE.

Part: FUEL CONTROL — FAULTY (NR 2 ENGINE) · airframe 15,772 hrs · 13,197 cycles

NR 2 N1, N2 AND FUEL FLOW FLUXATIONS IN CLIMB AND CRUISE. N1 DEVIATED ROUGHLY 1 PERCENT AND FUEL FLOW ROUGHLY 100LBS FLUXATIONS WERE CONTINUOUS AND ASSOCIATED WITH YAW. REMOVED AND REPLACED FUEL CONTROL UNIT IAW AMM 73-21-01, PERFORMED OPS CHECK OF RT ENG FCU IAW AMM 73-21-01. A/C OK FOR SERVICE.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 14,214 hrs · 11,737 cycles

ON CLIMBOUT OF KGRR EN ROUTE TO KMEM THE RT THRUST REVERSER UNLOCKED MESSAGE ILLUMINATED. THE FLIGHT CREW PERFORMED THE QRH WHICH REQUIRED LANDING AT THE NEAREST SUITABLE AIRPORT. KFWA WAS TEN MINUTES AWAY. THE FLIGHT CREW DECLARED AN EMERGENCY AND REQUESTED TO LAND AT KFWA DUE TO CLEAR RUNWAY CONDITIONS AND BECAUSE IT WAS A COMPANY MAINTENANCE BASE. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KFWA. MAINTENANCE INSPECTED THE AIRCRAFT AND DEFERRED THE THRUST REVERSER. THE AIRCRAFT WAS RELEASED FOR SERVICE BUT WAS SCHEDULED INTO A HANGAR FOR THAT NIGHT. NIGHT MAINTENANCE AT FWA REPLACED THE RT THRUST REVERSER POWER DRIVE UNIT.

Part: TRIM SWITCH — FAULTY (RUDDER) · airframe 13,520 hrs · 11,069 cycles

RUDDER WENT FULL RIGHT DEFLECTION DURING CLIMB. AIRCRAFT ROLLED RIGHT. AUTOPILOT DISCONNECTED. RUDDER RETURNED TO NEUTRAL QRH FOR RUDDER JAM AND RUNAWAY. DECLARED EMERGENCY. REMOVED AND REPLACED RUDDER TRIM SWITCH IAW AMM 27-20-00. SEE DISCR NR 2 FOR OP/C RUDDER TRIM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY)

CARGO SMOKE WARNING IN FLIGHT, QRH FOLLOWED FIRE EXTINGUISHING SYSTEM ACTUATED. REMOVED AND REPLACED THE NR 2 CARGO SMOKE DETECTOR IAW BOMBARDIER AMM 26-10-00. (S)