N832AY

Part: FAIRING — DAMAGED (RT NACELLE) · airframe 26,592 hrs · 27,212 cycles

"ON POST FLIGHT WALK AROUND, RH UPPER STANG FAIRING DAMAGED/ MISSING. KITH CONTROL TOWER ADVISED ACFT OF POSSIBLE MISSING PART WHICH THEY FOUN ON THE RUNWAY IN KITH. "REMOVED & REPLACED RH ENG UPPER STANG FAIRING. DONE IAW AMM 78-34-15 OPS CHECK GOOD. P/N 228-50253-806. "

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,555 hrs · 27,166 cycles

EMERGENCY LIGHTS (ALL) WILL NOT ILLUMINATE. REMOVED AND REPLACED ALL EMERGENCY BATTERY IAW CRJ200 AMM 33-51-04. OPS CHECKS GOOD. "

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,346 hrs · 24,520 cycles

CABIN EMERGENCY LIGHTS NOT WORKING DEFERRED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1A. PLACARD INSTALLED MM02 UPDATED MOC MOC NOTIFIED 100888...CHARGED CABIN EMERGENCY POWER SUPPLY BATTERIES IAW CMM 25-60-03. CABIN EMERGENCY LIGHTS OP CHECK GOOD IAW AMM 33-51-04 TS#006276. REMOVED FROM MM02 MXC NOTIFIED 100888

Part: BATTERY — INOPERATIVE (EXTEROR LIGHTS) · airframe 24,346 hrs · 24,520 cycles

EXTERIOR EMERGENCY LIGHTS NOT WORKING DEFERRED EXTERIOR EMERGENCY LIGHTS IAW MEL 33-52-2B. PLACARD INSTALLED MM02 UPDATED MOC NOTIFIED 100888... CHARGED EXTERIOR EMERGENCY POWER SUPPLY BATTERIES IAW CMM 25-60-03. EXTERIOR EMERGENCY LIGHTS OP CHECK GOOOD IAW AMM 33-51-04 TS#005276 REMOVED FROM MM02 MXC NOTIFIED 100888

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,858 hrs · 22,986 cycles

DURING FA CABIN PRE-FLIGHT, SHE FOUND THE CABIN EMERGENCY LIGHT-FLOOR LEVEL LIGHTED EXIT SIGN IN THE GALLEY BY THE SERVICE DOOR INOPERATIVE. DEFERRED CABIN EMERGENCY LIGHTS PER MEL 33-51-1A CAT "A" ENTERED IN MM02 PLACARD APPLIED MC 96579 NOTIFIED*******REMOVED & REPLACED GALLEY EMERGENCY FLOOR LIGHT & RE-SECURED GROUND WIRE IAW AMM 33-51-19, OPS CHECK GOOD. MM02 UPDATED, PLACARD REMOVED. MOC NOTIFIED #96183

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 394, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-4-11A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

FUSELAGE SKIN CRACKED AT LT FWD NOSE AVIONICS PANEL / DOOR BELOW AFT LATCH. REPAIRED FUSELAGE SKIN AT LT AVIONICS PANEL IAW EA NR CRJ253-08386 IR 2/6/19.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

FOUND 2EA INTERCOSTALS CRACKED LBL 27 FLOORBEAM FS 589. REMOVED & REPLACED 2EA INTERCOSTALS FS589 - FS605 @ LBL 27 IAW SRM 51-42-06 & 51-42-21.

Part: ACCESS PANEL — DAMAGED (TE FLAP VANE) · airframe 22,794 hrs · 22,918 cycles

RT IB FLAP VANE CENTER ACCESS PANEL ON THE ZONE 6 PANEL RACK HAS A BLOWN OUT FASTENER HOLE MARKED BY GREASE PENCIL AND DOT. LOCATED AND DRILLED ACCESS PANEL IAW SRM 51-40-11 TR 51-42.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,794 hrs · 22,918 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. PAX DOOR DRAG ANGLE WAS REPAIRED IAW REO# 601R-52-11-513.

Part: FITTING — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LBL 9 O/B FLOOR PANEL LANDING HAS CORROSION SPOT BETWEEN FS 605 AND FS 621, IN THE CARGO BAY. REPAIRED FLOOR PANEL LANDING IAW EA #CRJ253-08402.

Part: STIFFENER — CRACKED (EXHAUST FAIRING) · airframe 22,794 hrs · 22,918 cycles

RT EXHAUST FAIRING NR 2 STIFFENER FROM FWD END IS CRACKED AT TOOLING HOLE. REPAIRED STIFFENER ON RT EXHAUST FAIRING IAW CMM 78-11-00.

Part: BEAM — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LBL 27 I/B AND O/B FLOOR PANEL LANDINGS HAS CORROSION SPOTS BETWEEN FS 574 THRU FS 621, IN THE CARGO BAY. REPLACED LBL27, FS 574 TO FS621 BEAM CAP IAW SRM 51-42-21 & 51-42-22.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 22,794 hrs · 22,918 cycles

RT WINDSHIELD SIDE POST LWR OTBD TRANSITION FITTING CRACKED IN RADIUS. REPLACED RT WINDSHIELD SIDE POST LWR OTBD TRANSITION FITTING IAW SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

AFT PRESSURE BULKHEAD CLIP AT FS 625 STR 14L CRACKED. REMOVED AND REPALCED CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LT SIDE SEAT RAIL FROM FS409.00+16 TO FS409.00+112 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: STRAP — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

FLOOR SUPPORT STRAP AT FS 559.00 RBL 27 TO RBL 39 HAS MINOR SURFACE CORROSION. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT STRAP AT FS 559.00 RBL 27 TO RBL 39 IAW SRM 51-42-03.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 22,794 hrs · 22,918 cycles

LT WINDSHIELD SIDE POST LWR OTBD TRANSITION FITTING CRACKED IN RADIUS. REPLACED LT WINDSHIELD SIDE POST LWR OTBD TRANSITION FITTING IAW SRM 51-42-21 & TR 51-42.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LT SIDE SEAT RAIL FROM FS364.00 TO FS409.00+16 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 394, IN THE CABIN. REMOVED AND REPALCED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LT SIDE SEAT RAIL FROM FS409.00+112 TO FS449.00.85 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT SIDE SEAT RAIL FROM FS449.00.85 TO FS449.00 IS CORRODED. REMOVED/REPLACED RT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT SIDE SEAT RAIL FROM FS364.00 TO FS409.00+16 IS CORRODED. REMOVED AND REPLACED RT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION SPOTS BETWEEN FS 559+112 THRU FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49. RESTORED FINISHES IAW SRM 51-21-11, SRM 51-25-06, SRM 51-25-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

LT AISLE SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 394 THRU FS 409, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT SIDE SEAT RAIL FROM FS544.00 TO FS559.00+80 IS CORRODED. REMOVED AND REPLACED RT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT SIDE SEAT RAIL FROM FS409.00+16 TO FS409.00+112 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT SIDE SEAT RAIL FROM FS449.00.85 TO FS544.00 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,794 hrs · 22,918 cycles

RT AISLE SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 394 THRU FS 409, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,942 hrs · 20,833 cycles

EXTERIOR LEFT AFT EMERGENCY LIGHT INOPERATIVE.

Part: PBE — DEFECTIVE (CABIN) · airframe 20,863 hrs · 20,748 cycles

DURING INSPECTION NOTED AFT CABIN PBE PACK TO BE SOFT. VACUUM SEAL LOST. REMOVED & REPLACED AFT CABIN PBE IAW AMM CH 35-30-00.

Part: OXYGEN MASK — INOPERATIVE (CABIN) · airframe 20,324 hrs · 20,156 cycles

OXYGEN BOTTLE MASK QD BALLS STICK RETRACTED. R & R THE OXYGEN MASK, OP'S CHECKED GOOD IAW 35-900-700.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 18,940 hrs · 18,730 cycles

LAVATORY SMOKE TOILET INDICATION, PULLED BREAKERS IAW THE QRH, AND DIVERTED. NO EVIDENCE OF SMOKE OR FIRE IN THE LAVATORY. R & R AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,624 hrs · 18,406 cycles

NR 2 AND NR 4 EMERGENCY CEILING LIGHTS ARE INOPERATIVE. REF W/O 1013379, CARD NR 9000-0020. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,624 hrs · 18,406 cycles

559 CAP ANGLE IS CRACKED IN RADIUS BELOW THE POST AT BL 18 LT. WORK WAS ACCOMPLISHED ON W/O 1013379 1000 0041, SN 4859218. REPAIRED CAP ANGLE IAW REO 601R-53-41-260 AND EO P53025.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 18,624 hrs · 18,406 cycles

221 AFT FLOORBOARD SUPPORT, AFT ANGLE HAS CORROSION AT FS 280, BL 0. R & R ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: OXYGEN MASK — KINKED (CABIN) · airframe 18,624 hrs · 18,406 cycles

PASSENGER PSU OXYGEN MASK HOSE KINKED ON LT ROW 11, MARKED. R & R 1 LT ROW 11, O2 MASK IAW AMM 35-21-09-020-801/35-21-09-420-801 PERFORMED OPS CHECK IAW AMM 35-20-00-710-803, CHECKS GOOD.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 18,624 hrs · 18,406 cycles

NR 2 ENGINE THRUST REVERSER TORQUE BOX IS CRACKED ON AFT FLANGE AT 5 O'CLOCK POSITION. REPAIRED THRUST REVERSER TORQUE BOX AFT FLANGE IAW REO NR 601R-78-30-2531.

Part: STRIP — CHAFED (LT COWLING) · airframe 18,624 hrs · 18,406 cycles

LEFT ENGINE NOSE COWL 432AT T/E HAS CHAFING DAMAGE. R & R AFT EDGE STRIP ON NOSE COWL 432AT IAW CMM 71-14-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,624 hrs · 18,406 cycles

FLOOR SUPPORT AT FS 559.0 BETWEEN LT SILL AND RBL 27 HAS CORROSION. R & R FLOOR SUPPORT AT FS 559.0 BETWEEN LT FLOOR SILL AND LBL27 IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,624 hrs · 18,406 cycles

CARGO DOOR SUPPORT STRUCTURE HORIZONTAL MEMBER TO 621 BULKHEAD CLIP IS CRACKED AT FWD FACE OF FS 621 BULKHEAD. R & R BULKHEAD CLIP IAW SRM 51-42-21.

Part: SUPPORT ANGLE — CRACKED · airframe 18,624 hrs · 18,406 cycles

ENTRY DOOR INERTIA REEL ASSY UPPER SUPPORT ANGLE POSSIBLY CRACKED ON O/B RADIUS. REMOVED AND REPLACED ENTRY DOOR INERTIA REEL POWER ASSIST MOTOR ASSY UPPER SUPPORT ANGLE IAW SRM 51-42-06, AND 51-42-13 AND 51-41-04.

Part: SMOKE DETECTOR — OUT OF ADJUST (LAVATORY) · airframe 17,496 hrs · 17,217 cycles

LAVATORY SMOKE DETECTOR INOPERATIVE. ADJUSTMENT & TEST OF SMOKE DETECTOR PUSH BUTTON MECHANISM DONE IAW CMM 25-40-43. OPERATIONS CHECKED GOOD. THIS CLEARS DM 002950 MMO2 UPDATED & PLACARD REMOVED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 17,080 hrs · 16,781 cycles

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

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 16,588 hrs · 16,269 cycles

FIRST OFFICER'S LIFE VEST BAG TORN. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.

Part: OXYGEN MASK — OUT OF POSITION (CABIN) · airframe 16,500 hrs · 16,173 cycles

OXYGEN MASK AT FLIGHT ATTENDANT STATION & ROW 1CD HAVE FALLEN. RESTOWED O2 MASKS AT FLIGHT ATTENDANT STATION & AT ROW 1CD IAW AMM 35-21-09.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 16,360 hrs · 16,023 cycles

CAPTAIN`S EMERGENCY FLASHLIGHT FOUND INSTALLED IMPROPERLY AND WHEN REMOVED, NON-FUNTIONAL. REPLACED BATTERY ON CAPTAIN SIDE FLASHLIGHT IAW AMM 25-61-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 16,137 hrs · 15,788 cycles

SMOKE TOILET INDICATION ON SHORT FINAL. NOTICED NOTHING UNUSUAL WHEN INSPECTING LAV. NOTED NO RESIDUAL ODOR PRESENT. RAN BOTH PACKS AT FULL HOT VIA APU SOURCE. NO SMOKE, HAZE, ODOR PRESENT. NOTED TOILET SMOKE DETECTOR ELECT CONNECTOR LOOSE DUE TO SLIDE LATCH NOT LOCKED. AS A PRECAUTION, REPLACED DETECTOR IAW 200 AMM 26-16-01. OPS CHECKS GOOD. ACFT OK FOR CONTINUED SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 16,133 hrs · 15,783 cycles

TOILET SMOKE MESSAGE DURING FLIGHT. F/A FOUND NO SMOKE IN LAVATORY F/A RESET, MESSAGE CLEARED. NEVER RECEIVED MESSAG EAGAIN. OPS TEST OF LAV SMOKE DETECTON SYSTEM IAW AMM 26-16-00-710-803. OP'S CHECKED IS GOOD, OK FOR SERVICE.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 15,718 hrs · 15,357 cycles

FWD MOST CEILING EMER LIGHT INOPERATIVE. DEFERRED CLEARED DM 008768 BY REPLACING FUSE ON NR 1 EMER BATTERY CHARGER IAW CMM 33-21-70. UPDATED MM02.

Part: PIN — NOT SEATED (BATTERY CHARGER) · airframe 15,709 hrs · 15,350 cycles

WARDROBE HAS ONE EACH EMER LIGHT INOPERATIVE & CTR AISLE FWD EMER LIGHT INOPERATIVE. FOUND RECESSED PIN AT CHARGER ASSEMBLY NR 2 RESEATED PIN IAW ESPM 20-17-10. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,689 hrs · 15,331 cycles

FLIGHT ATTENDANT FLASHLIGHT CHARGING LIGHT INOPERATIVE. R & R BATTERY IAW CMM 25-60-02 PN ON OFF P4-01-0021.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,677 hrs · 15,321 cycles

FOUND THE FUSELAGE SKIN AT APPROXIMATELY FS 253 & 0.28 INCHES ABOVE STRINGER 24L TO BE DENTED, MEASURING 1.3 INCHES IN DIAMETER & 0.045 INCHES DEEP. REPAIRED IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,375 hrs · 15,004 cycles

NUMBER 3 EMER CEILING FLOOD LIGHT INOPERATIVE. R & R NR 3 EMER CEILING FLOOD LIGHT BULB IAW AMM 33-51-16, OPERATIONS CHECKED GOOD.

Part: PUMP — FAULTY (HYDRUALIC SYS) · airframe 14,843 hrs · 14,468 cycles

HYD 3A ACMP GOT HIGH TEMP >96 DEG C CAUTION MSG. AFTER DOING QRH TURNED 3A OFF HIGH TEMP DECREASED DOWN TO 6 DEG C. DEFERRED 3A ACMP IAW MEL 29-12-01. R & R 3A ACMP IAW AMM 29-12-03, OPERATIONS CHECKED GOOD. RAN 3A PUMP CONTINUOUSLY & MOVED FLIGHT CONTROLS FOR 45 MINS, 3 HYD TEMP WAS 27C, ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 14,832 hrs · 14,458 cycles

AFTER STARTING THE RT ENGINE, RECEIVED AN AC BUSS 2 CAUTION MESSAGE FOLLOWED BY AN ARINC COOL, HYD 3B & COMPLETE ELEC FAILURE, ALSO FLAPS FAIL MSG. ALL FAULT MESSAGES OCCURRED AFTER HYD 3A CIRCUIT BREAKER TRIPPED & KICKED APU GENERATOR OFF. RESET POWER, RAN ENGINES & CYCLED FLAPS & ACFT POWER CHECKED GOOD IAW AMM 24-20-00. ALL AC POWER MESSAGES CLEARED.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 14,832 hrs · 14,458 cycles

FLAPS FAIL MESSAGE, MESSAGE CLEARED WITH RESET. CYCLED FLAPS, FOUND ASYMMETRY AT 8 DEGREES P0SITION LT 8 DEGREES & RT 9 DEGREES. R & R NR 4 FLEX SHAFT IAW AMM 27-53-10, NR 4 FLAP ACTUATOR IAW AMM 27-53-04, SHIMMED NR 3 FLAP ACTUATOR IAW AMM 27-54-00, RIGGED RT & LT FLAPS IAW AMM 27-54-00-830-801. ALL OPS CHECKED GOOD. COMPLIED WITH FLAP FAIL MINIMUM WORKSCOPE. PERFORMED TROUBLESHOOTING PER FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC.

Part: LIFE VEST — DAMAGED (CABIN) · airframe 13,335 hrs · 12,953 cycles

2 EA INFANT LIFE VEST DAMAGED. R & R 2 EA INFANT LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — DAMAGED (CABIN) · airframe 13,331 hrs · 12,949 cycles

TWO INFANT LIFE VEST DAMAGED. R & R TWO INFANT LIFE VEST IAW AMM 25-61-03.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 13,275 hrs · 12,890 cycles

GEAR UP DISAGREE RIGHT MAIN.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 12,834 hrs · 12,463 cycles

FIRST OFFICER'S FLASHLIGHT INOPERABLE. REMOVED AND REPLACED FIRST OFFICER'S FLASHLIGHT IAW CMM 25-60-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,791 hrs · 12,421 cycles

PARKING BRAKE CABLE PASS THRU HOLE IS CRACKED ON FS 202.75 PRESSURE BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 12,791 hrs · 12,421 cycles

UPPER SUPPORT ANGLE AT FS 280 IS CRACKED JUST OUTBOARD OF LBL 9 AND PULLEY BRACKET. REPAIRED IAW BOMBARDIER REO 601R-53-11-137.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 12,791 hrs · 12,421 cycles

UPPER FLOOR SUPPORT ANGLE AT FS 280 IS CRACKED JUST OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-137.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,791 hrs · 12,421 cycles

FS 280 WEB LOWER ANGLE IS CRACKED JUST OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,791 hrs · 12,421 cycles

CLIP IS CRACKED AT INBOARD SIDE OF LBL 9 AT FS 280. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: SKIN — DENTED (TE FLAP) · airframe 12,791 hrs · 12,421 cycles

LEFT INBOARD FLAP LOWER SKIN IS DENTED AT TRAILING EDGE 15 INCHES FROM INBOARD AFT CORNER. REPARIED IAW SRM 57-52-00 REPAIR 3.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,460 hrs · 12,086 cycles

FLIGHT ATTENDANT'S UNDERSEAT FLASHLIGHT INOPERABLE. REMOVED & REPLACED F/A FLASHLIGHT BELOW JUMPSEAT IAW CRJ200 AMM 25-61-04 OPS CHECKED GOOD.

Part: SIGN — CRACKED (CABIN) · airframe 12,447 hrs · 12,072 cycles

FORWARD CENTER AISLE EXIT SIGN CRACKED AND NOT FITTING CORRECTLY PART NUMBER BF5-0357-901. REMOVED AND REPLACED FORWARD CENTER AISLE EXIT SIGN IAW CRJ 200 AMM 20-00-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 11,997 hrs · 11,600 cycles

PASSENGER DOOR UPPER EMERGENCY EXIT SIGN INOPERATIVE. FOUND LOOSE CONNECTOR ON PASSENGER DOOR EMERGENCY EXIT SIGN. SECURED CONNECTOR IAW AMM 33-51-10, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,813 hrs · 9,101 cycles

FOUND RT OVERWING LIGHT BURNED OUT. RELAMPED RT OVERWING LIGHT.

Part: STRUCTURE — DAMAGED (FUSLEAGE) · airframe 7,869 hrs · 6,978 cycles

WHILE TOWING THE ACFT ON AN ICY HANGAR APRON THE TUG JACKKNIFED AND CONTACTED THE RT SIDE OF THE FUSELAGE. THE FOLLOWING ITEMS WERE DAMAGED: S22R BENT FROM STA 375-389 AND SEVERED AT FS 379 AND 383; FS 379 FRAME WEB AND OUTER FLANGE BENT 6" FROM 2.5" BELOW S22R TO 3.5" ABOVE S22R; FUSELAGE SKIN DENTED AND TORN FROM STA 377-390, S21-23R. INSPECTED RT FUSELAGE SKIN IN DAMAGED AREA UNDERLYING COMPONENTS AND SYS ARE DAMAGE FREE DAMAGE CONFINED TO AREA BETWEEN APPROX FR STA 377.0 AND 391.0 AND BETWEEN STRINGERS 21 AND 23. ACFT TO BE FERRIED UNPRESSURIZED FOR REPAIRS. C/W SHEET METAL REPAIR F.S. 377-389 S21-23R IAW EO C53105. ACCOMPLISH REPAIR IAW BBD REO 601R-53-21-1093.

Part: BRACKET — DAMAGED (NLG PROX SENSOR) · airframe 5,791 hrs · 4,787 cycles

NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF WHEN GEAR WAS SELECTED UP GEAR DISAGREE AND NOSEWHEEL DOOR OPEN WARNINGS ANNUNCIATED. GEAR DID NOT RETRACT. RAN EMERGENCY CK LIST, EXTENDED GEAR MANUALLY. DECLARED EMERGENCY BACK INTO MSP LANDED BELOW 47,000 DESCENT RATE BELOW 600 FT PER MIN. AIRSPEED REMAINED AT 200 IAS NO OVERWEIGHT LANDING. COMPLETED MM409 NR 352863. REPLACED NLG OLEA CENTER/EXTENDED PROX SENSOR BRACKET PN 16215-105 AND ADJUSTED SENSOR GAP. OPS CHECK GOOD.