N431AW

Part: SWITCH — DEFECTIVE (THRUST REVERSER) · airframe 45,012 hrs · 43,457 cycles

LEFT THRUST REVERSER CAUTION IN FLIGHT - AIR RETURN "AIRCRAFT REMOVED FROM SERVICE" REF WORK ORDER 293027 FOR R/R OF STOW SWITCH AND OPS TEST ON WORK CARDS 15-THROUGH 19. REMOVED PLACARD, REMOVED FROM MEL

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 44,993 hrs · 43,439 cycles

L REV UNLOCK CAUTION IN FLIGHT. C/W IAC AND QRH. EMER STOW DID NOT CLEAR MESSAGE. REVERSER NOT USED ON LANDING. CAUTION REMAINS WITH ENGINE SHUT DOWN. AIRCRAFT REMOVED FROM SERVICE. R/R LH TR PDU IAW AMM 78-32-03 OPS CHECK GOOD AT THIS TIME.

Part: PDU — FAULTY (THRUST REVERSER) · airframe 44,562 hrs · 43,003 cycles

SUPPLEMENTAL INFORMATION, DURING CLIMB OUT RECIEVED LT T/R UNLOCK CAUTION MSG. C/W QRH EMERG STOW WAS PRESSED. T/R STOWED VISUALLY VERIFIED ON GROUND. REV ICON AMBER, DID NOT EXTINGUISH. AIRCRAFT AIR RETURNED TO KORD FOR MX. REVERSER WAS DE-ACTIVATED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. R&R LT TR PDU IAW AMM 78-31. OPS CHECK GOOD, REMOVED PLACARD REMOVED FROM MEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,435 hrs · 42,880 cycles

L/H LWR EMERGENCY LIGHT BY OVERWING EXIT WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE FOUND BATTERY PACK PS2LY TO HAVE LOW VOLTAGE. CHARGED DEPLETED EMERGENCY BACK REF AWAC SUPPLEMENT 15-220B. PERFORMED SELF TEST OF EMERGENCY BATTERY PACK/CHARGER ASSY IAW CRJ-200 AMM 33-51-04-740-005 NO DEFECTS NOTED.

Part: SKIN — DENTED (BS 733) · airframe 44,435 hrs · 42,880 cycles

SMALL DENT ON R/H AFT FUSELASGE TAIL SECTION APPROX FS 733 & R/H STRINGER 19 AIRCRAFT REMOVED FROM SERVICE REWORKED DENT ON R/H AFT FUSELAGE TAIL SECTION AT APPROX FSS 733 AND ABOVE S19R IN AN AREA OF 1" X 1" X .002"D FROM ORIGINAL DEPTH OF .012"D FOUND TO BE WITHIN LIMITS REF EA# AWAC-CRJ253-01363 ISSUE DATE 10-29-2019 REV B AND SUPPLEMENT NO: 19-299A ISSUED 10-30-2019.

Part: INTERCOSTAL — CRACKED (BS 654-672) · airframe 44,435 hrs · 42,880 cycles

APU DOOR INTERCOSTAL AT FS 654 TO FS 672.20 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED DOOR INTERCOSTAL AT FS654 TO FS 672.20 REF AIR WISCONSIN SUPPLEMENTAL NO. 13-0851B AND BOMBARDIER PL601R-53-62-225 AT STRINGER 4L. CUT OUT DAMAGED AREA, HFEC NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR DOUBLER REF BOMBARDIER PL601R-53-62-225.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,435 hrs · 42,880 cycles

R/H PRESSURE FLOOR SILL ASSY ON PAD UP AREA AT STA 449.88 & RBL 43 AND STA 461 & RBL 43 HAS SURFACE CORROSION AIRCRAFT REMOVED FROM SERVICE REMOVED SURFACE CORROSIONBY HAD AT BOTH STA 449.85 AND STA 461 & RBL 43. STA 449.85 HAD AN AREA OF 1.0" X 1.0" X .002" REMOVED LEAVING .076" MATERIAL REMAING AT STA 449.85 OF .078" FROM ORIGINAL THICKNESS AND STA 461 HAD AN AREA OF 1.0" X 1.0" X .002" REMOVED AT STA 461 LEAVING .077" FROM ORIGINAL THICKNESS. REF BOMBARDIER REO 601R-53-41-666

Part: SEAL — DAMAGED (EMEGENCY EXIT) · airframe 44,435 hrs · 42,880 cycles

R/H OVERWING EMERGENCY EXIT DOOR SEAL HAS 2" TEAR ON BOTTOM SIDE AIRCRAFT REMOVED FROM SERVICE REPLACED SEAL ON R/H OVERWING EMERGENCY EXIT DOOR SEAL REF CRJ AMM 52-21-07

Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 44,435 hrs · 42,880 cycles

#1 I/B REVERSER STING FAIRING HAS MULTIPLE DAMAGE AND CRACKS AIRCRAFT REMOVED FROM SERVICE #1 ENG I/B REVERSER STING FAIRING HAS MULTIPLE DAMAGES AND CRACKS BEYOND LIMITS AND PART HAD TO BE REPLACED

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 44,290 hrs · 42,751 cycles

DURING CLIMB WHEN TRANSFERRING BLEEDS TO ENGINES RECEIVED RT PACK HIGH PRESS. C/W QRH PACK WORKED ON APU (NOT ON ENGINE) DER: ON CLIMB OUT WHEN TRANSFERRING BLEEDS TO ENGINE RECEIVED RT PACK HI PRESS CAUTION MESSAGE COMPLIED WITH QRH AND THE MESSAGE CLEARED. TRIED TRANSFERRING AGAIN AND RECEIVED MESSAGE AGAIN, PACK WOULD RESET ON APU ONLY. CREW MADE THE DECISION TO DIVERT BACK TO ORD DUE TO NO OPERATIVE PACKS. (LT PACK WAS ON MEL) NO EMERGENCY WAS DECLARED AND THE PLANE LANDED SAFELY AND TAXIED TO THE GATE. THE PLANE WAS TAKEN OUT OF SERVICE FOR INSPECTION.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,094 hrs · 42,558 cycles

CARGO FIRE BOTTLE LOW INDICATION- WHILE AT FLT LEVEL 280 ENROUTE, RECEIVED AMBER CARGO BLT LO MESSAGE. C/W QRH & LANDED AT 47400 LBS LANDING WEIGHT. BTMS READS 3343. MESSAGE CLEARED BY ITSELF AT 3000 FEET. LANDING WAS NORMAL AND SMOOTH.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,094 hrs · 42,559 cycles

WHILE FLT LEVEL 250 IN ROUTE RECIEVED "AMBER CARGO BOTTLE LOW CAUTION MSG". C/W QRH DIVERTED TO KMSN FOR NORMAL LANDING. MSG CLEARED AT PARKING. PLACARED AND PLACED ON MEL.

Part: UNKNOWN — UNKNOWN · airframe 43,575 hrs · 42,061 cycles

ON APPROACH, THE AIRCRAFT EXPERIENCED AN UN-COMMANDED YAW MOTION. THE FLIGHT CREW REFERENCED THE QRH, STABILIZED THE AIRCRAFT, CONTACTED ATC AND DISPATCH, DECLARED AN EMERGENCY AND DIVERTED.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

FRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 22R AND 23R

Part: BRACKET — CRACKED (HYD RESERVOIR) · airframe 40,869 hrs · 39,406 cycles

DURING LEAK CHECK OF #3 HYD RESERVOIR FOUND RESERVOIR AFT MOUNT BRACKET TO BE CRACKED

Part: POST — CRACKED (BS 409) · airframe 40,869 hrs · 39,406 cycles

BS 409+128 VERTICAL POST AT RBL 18 CRACKED ON INBD SIDE IN AFT RADIUS.

Part: SKIN — CRACKED (BS 646-654) · airframe 40,869 hrs · 39,406 cycles

FUSELAGE SKIN PUNCTURED AT BS 640 - 654 AND STRINGERS 26R - 27R.

Part: FRAME — CORRODED (BS 574) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

FRAME BS 574 HAS CORROSION ON THE FWD AND AFT SIDE AROUND STRINGER 21L, IN THE CARGO BAY.

Part: RIB — CRACKED (RT PYLON) · airframe 40,869 hrs · 39,406 cycles

RIGHT PYLON LEADING EDGE FWD INTERNAL RIB CRACKED. REPAIRED IAW 14-252A.

Part: ANGLE — CRACKED (BS 621) · airframe 40,869 hrs · 39,406 cycles

ANGLE AT THE CARGO DOOR BEAM, AFT SIDE OF BS 621 IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 40,869 hrs · 39,406 cycles

EMERGENCY LIGHT BATTERY PACK NR 3 FAILED OPERATIONAL TEST. REPLACED THE BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD IAW AMM 33-51-04-740-801.

Part: STRINGER — CORRODED (BS 574-589) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

STRINGER 21L HAS CORROSION BETWEEN FRAMES BS 574 AND 589.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 40,869 hrs · 39,406 cycles

REAR PRESSURE BULKHEAD AFT SIDE HAS A CRACKED OBLIQUE ANGLE AT STRINGER 14R. REPLACED THE ANGLE IAW SRM 51-42-21, 51-40-11, 51-21-11, AND 51-25-06.

Part: ANGLE — CRACKED (BS 621 FLOORBEAM) · airframe 40,869 hrs · 39,406 cycles

FLOORBEAM ANGLE CRACKED AT BS 621 AT OTBD FLOOR SILL. REPLACED THE FLOORBEAM ANGLE IAW REO 601R-53-61-117, REV-D.

Part: ANGLE — CRACKED (STRINGER 3L) · airframe 40,869 hrs · 39,406 cycles

ANGLE ON STRINGER 3L IS CRACKED, AFT OF BS 280. REPLACED THE ANGLE IAW SRM 51-24-16, AND 51-42-06.

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 40,869 hrs · 39,406 cycles

RIGHT FLIGHT DECK WINDOW LOWER AFT ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CORRODED (BS 621 FLOORBEAM) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

FLOORBEAM ANGLE CORRODED AT BS 621, RBL 9 TO RBL 27. REPAIRED THE FLOORBEAM ANGLE IAW EA CRJ253-00753 REV-IR.

Part: ANGLE — CRACKED (BS 605) · airframe 40,869 hrs · 39,406 cycles

LEFT PYLON ACCESS PANEL SUPPORT ANGLE CRACKED AT 605. REPAIRED IAW 14-252A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,869 hrs · 39,406 cycles

STR 3L IS CRACKED JUST FWD OF FRAME 379.00. REPAIRED STRINGER 3L FWD OF FRAME 379.00 IAW SRM 53-00-03, 51-42-06, 51-25-16.

Part: POST — CRACKED (BS 409) · airframe 40,869 hrs · 39,406 cycles

CRACKED VERTICAL POST AT BS 409+128, BL 0. REPLACED VERTICAL POST IAW SRM 51-42-06, AND REO 01R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 40,869 hrs · 39,406 cycles

VERTICAL POST AT BS 409+128, LBL 18 IS CRACKED. REPLACED THE VERICAL POST IAW SRM 53-41-19, AND REO 601R-53-41-889 REV-B.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,869 hrs · 39,406 cycles

FLOORBEAM ANGLE CRACKED AT BS 280, LBL 9, OTBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, 51-41-11, 51-21-11, AND 51-25-06.

Part: STRAP — CORRODED (BS 559-560) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

FLOOR SUPPORT STRAP CORRODED AT FS 559 TO 560, RBL 30 TO RBL 42. REPAIRED THE FLOOR STRAP IAW SRM 51-42-06, AND EA 00754, REV-IR.

Part: SEAT TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

CARGO SEAT TRACK CORRODED AT FS 559+80 TO 559+96, LBL9. REPLACED CARGO SEAT TRACK IAW AMM 53-00-49, REO 601R-53-00-485 REV-B.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 40,869 hrs · 39,406 cycles

LT FLOOR SILL CRACKED AT FS 589.00 IN THE CARGO BAY. REPAIRED LT FLOOR SILL REO 601R-53-61-433 REV-C.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,869 hrs · 39,406 cycles

FLOOBEAM ANGLE CRACKED AT BS 280, RBL 9- INBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 40,869 hrs · 39,406 cycles

RT OVERWING ACCESS PNL SUPPORT BRACKET AT FS 449.85 IS CRACKED.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 40,869 hrs · 39,406 cycles

RT OVERWING ACCESS PNL SUPPORT BRACKET AT FS 461.0 IS CRACKED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,869 hrs · 39,406 cycles

FLOORBEAM ANGLE CORRODED AT BS 280, LBL 9 TO RBL 9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,869 hrs · 39,406 cycles

MAIN CABIN FLOORBEAM AT BS 280, RBL 9 HAS CRACKED ATTACH ANGLE. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, 51-40-11, 51-24-36, 51-25-16, AND 51-25-06.

Part: ATTACH ANGLE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

MAIN CABIN FLOOR SILL ATTACH ANGLE CORRODED AT THE SERVICE DOOR. REPLACED ATTACH ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21, AND 51-40-11.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 40,869 hrs · 39,406 cycles

LEFT INBD FLAP LOWER SKIN DAMAGED. REPLACED THE SKIN IAW SRM 51-42-13, 57-52-00, AND 51-40-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,869 hrs · 39,406 cycles

FLOORBEAM ANGLE CRACKED AT BS 280.00, LBL 9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 40,869 hrs · 39,406 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 280. LBL 9 TO RBL 9. REPAIRED THE FLOORBEAM IAW REO 601R-53-11-136 REV-A.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 40,869 hrs · 39,406 cycles

LEFT I/B FLAP VANE HAS A CHAFE AT THE I/B STOP. REPLACED FLAP VANE LEADING EDGE IAW SRM 51-42-13.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,115 hrs · 32,602 cycles

RECEIVED SERVICE DOOR CAUTION MESSAGE ON CLIMB OUT AT 20,000 FEET AND THEN LOUD HISSING. PRECEDED BY "THUMP" COMING FROM SERVICE DOOR AREA. PRESSURIZATION REMAINED NORMAL HOWEVER HISSING WAS INTOLERABLE. C/W QRH, DECLARED EMERGENCY, RETURNED PHL. LANDING WAS SMOOTH AND UNEVENTFUL, APPROXIMATELY 200 FOOT PER MINUTE. BRAKING NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,515 hrs · 32,077 cycles

EMERGENCY LIGHTS ROWS 8-12 INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-04. AND R & R THE INVERTER IAW AMM 33-51-07 OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (SERVICE DOOR) · airframe 32,056 hrs · 31,645 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.

Part: SKIN — DENTED (BS 280-333) · airframe 38,929 hrs · 37,646 cycles

FUSELAGE SKIN BETWEEN BS 280 - 333, STRINGERS 8 - 16R IS DENTED AT MULTIPLE LOCATIONS

Part: AUTOPILOT SYS — DISCONNECTED · airframe 31,867 hrs · 31,470 cycles

AUTOPILOT INTERMITTENTLY DISCONNECTS AFTER BEING ENGAGED.

Part: HANDLE — OUT OF ADJUST (SERVICE DOOR) · airframe 38,046 hrs · 36,839 cycles

UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, DOOR OPENS FROM THE INSIDE NORMALLY. ADJUSTED SERVICE DOOR HANDLE, OUTER LOCK PIN & SECURED HANDLE IAW AMM 52-41-03, OUTER HANDLE OPERATIONS CHECKED GOOD.

Part: PDU — DEFECTIVE (THRUST REVERSER) · airframe 37,981 hrs · 36,776 cycles

RECEIVED RT REV UNLOCK CAUTION MSG, PASSING THROUGH 23,700 FT. COMPLIED WITH QRH, MSG REMAINS, AMBER REV ICON. REVERSERS WERE NOT ARMED. RT REV APPEARS TO BE STOWED AT THE GATE. DEACTIVATED RT TR IAW SUP 15-046. COMPLIED WITH M ACTION. R & R PDU FOR RT TR IAW AMM 78-32-03. OPERATIONS CHECKED GOOD. REMOVED PLACARD & MEL.

Part: SKIN — CRACKED (PAX DOOR) · airframe 37,908 hrs · 36,709 cycles

COMPLIED WITH PERMANENT REPAIR TO PAX DOOR INNER SKIN CRACKS, REPLACED.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 37,908 hrs · 36,709 cycles

MAIN ENTRY DOOR FWD FRAME UPPER END CRACKED, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,908 hrs · 36,709 cycles

LEFT AISLE SEAT TRACK STICK 3, BETWEEN FS 409+128 & 559 HAS CORRODED AREAS, REPLACED.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 37,908 hrs · 36,709 cycles

FORWARD BULKHEAD AT FS 169.00, FWD SIDE IS CHAFED AT 3,6 & 9 O CLOCK. REMOVED CHAFED FS 169.00 BULKHEAD ANGLE & INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: FITTING — CHAFED (TE FLAP) · airframe 37,908 hrs · 36,709 cycles

LEFT WING OTBD FLAP, INBD GUIDE BEARING, LANDING IS CHAFED, REPLACED.

Part: ANGLE — CRACKED (RT WING) · airframe 37,908 hrs · 36,709 cycles

RIGHT WING LE SHROUD UPPER ANGLE CRACKED AT WS 143.180, REPLACED.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 37,908 hrs · 36,709 cycles

MAIN ENTRY DOOR AFT FRAME IS CRACKED ON UPPER END. REPAIRED MAIN ENTRY DOOR AFT FRAME IAW REO 601R-52-11-402.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,908 hrs · 36,709 cycles

FRAME 529.00 CRACKED, AT STRINGER 6L IN THE PAX CABIN. REPAIRED FRAME 529.00, AT STRINGER 6L IAW EA CRJ253-00274 REV IR DATED 2 9 2016.

Part: RIB — CRACKED (LT WING) · airframe 37,908 hrs · 36,709 cycles

LEFT WING TE RIB AT WS 130.10 CRACKED, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,908 hrs · 36,709 cycles

LEFT AISLE SEAT TRACK STICK 4 HAS CORROSION, BETWEEN FS 559 & 559+80, REPLACED.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 37,908 hrs · 36,709 cycles

CARGO DOOR FWD TRACK LOWER U CHANNEL IS CRACKED, REPLACED.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 37,908 hrs · 36,709 cycles

CARGO DOOR LOWER AFT CORNER HAS CRACKED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,908 hrs · 36,709 cycles

LEFT SIDEWALL SEAT TRACK STICK 6, BETWEEN FS 559 & 559+80, CORRODED, REPLACED.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 37,908 hrs · 36,709 cycles

LEFT FWD EQUIPMENT BAY FLOOR CRACKED AT FS 193.00. REPAIRED IAW REO 601R-53-11-081 REV NC.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 37,908 hrs · 36,709 cycles

RIGHT FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 CRACKED, REPAIRED.

Part: ANGLE — CRACKED (BS 484) · airframe 37,908 hrs · 36,709 cycles

BS 484 ANGLE AT LBL 27 FOUND CRACKED. R & R THE ANGLE IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,908 hrs · 34,709 cycles

LEFT AISLE SEAT TRACK STICK 1 HAS CORROSION, BETWEEN FS 364.00 & 394.00 IN CABIN. R & R SEAT TRACK 1 LT AISLE IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,908 hrs · 36,709 cycles

LEFT FLOOR SEAT RAIL SECTION AT LBL 9.0 IN CARGO AREA HAS CORROSION FROM FS 559.00+110 TO FS 570.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,805 hrs · 30,488 cycles

AFTER TAKEOFF, GEAR SELECTED UP, RECEIVED GEAR DISAGREE AT APPROX 5 SECONDS, NOSE SHOWED RED. COMPLIED WITH QRH, MANUAL EXTENSION SELECTED, RECEIVED 3 GREEN DOWN. LANDED AT 46,760 LBS, NORMAL BRAKING. HYD PUMPS WERE IN AUTO IAW QRH, 2 & 3B WERE SELECTED TO ON WITH NO CHANGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,713 hrs · 30,406 cycles

EMERGENCY LIGHTS BETWEEN ROW 6 & 7 NOT ILLUMINATING.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,324 hrs · 30,048 cycles

FLIGHT SPOILERS STATUS MSG INFLIGHT, WHEN FLIGHT SPOILERS WERE DEPLOYED. ACFT HAD UNCOMMANDED ROLL MOMENTARILY WITH NO FURTHER ISSUES.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 37,068 hrs · 35,905 cycles

APPEARS FUEL IS LEAKING FROM RT TANK TO CTR TANK. GAINED 250 LBS OF FUEL IN CTR TANK IN CRUISE FLIGHT. NOTED FUEL QUANTITIES & DEPOWERED ACFT FOR 35 MINUTES. ON REPOWER, NOTED FUEL QUANTITIES, NO SIGNIFICANT CHANGE. VERIFIED NO STATIC LEAKS BETWEEN TANKS. ACFT OK FOR SERVICE.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 29,476 hrs · 29,211 cycles

FLIGHT 3745 STRONG SMELL OF FUEL IN FLIGHT DECK WHILE EN-ROUTE. INSPECTED AFT EQUIPMENT BAY & APU COMPARTMENT FOR FUEL LEAKS. NO LEAKS FOUND. R & R LT COALECSOR SOCK IAW AWAC SUPP 14-192. ACCOMPLISHED SUP 09-037A, NO SMELL OR ODOR NOTED & WIPED DOWN FLIGHT DECK AREA.

Part: O-RING — DAMAGED (APU) · airframe 29,467 hrs · 29,203 cycles

FLIGHT 3779 COCKPIT & GALLEY HAVE STRONG FUEL SMELL. INSPECTED APU & FOUND LEAKING LINE ON APU FCU. R & R O RING ON LEAKING LINE AS REQUIRED. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD. CLEANED APU ENCLOSURE & FUEL SMELL NO LONGER PRESENT INSIDE OF ACFT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 36,422 hrs · 35,275 cycles

STRINGER 23R & TIE CLIP CRACKED IN ASSOCIATION WITH DAMAGED POWER RECEPTACLE BRACKET & SURROUND SKIN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,422 hrs · 35,275 cycles

SURROUNDING SKIN & MOUNT BRACKET FOR THE ACFT GND POWER RECEPTACLE DAMAGED.

Part: BEAM — CRACKED (NLG WW) · airframe 36,422 hrs · 35,275 cycles

RIGHT BEAM WEB ON NLG WW HAS DAMAGED HOLES ASSOCIATED WITH POWER RECEPTACLE MOUNT DAMAGE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 36,422 hrs · 35,275 cycles

FS 621 PRESS BULKHEAD HAS DISCREPANT HOLES FROM CARGO LINER INSTALL ON LT SIDE, AFT OF CARGO DOOR.

Part: ANGLE — GOUGED (FUSELAGE) · airframe 36,422 hrs · 35,275 cycles

FS 621 BULKHEAD ANGLE GOUGED AFT OF CARGO DOOR.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 36,048 hrs · 34,918 cycles

LAVATORY SMOKE DETECTOR FALSE ALARM. NO EVIDENCE OF SMOKE OR FIRE. INTERMITTENT COCKPIT INDICATION. VERIFIED NO EVIDENCE OF SMOKE OR FIRE IN LAVATORY. PULLED & COLLARED CBP1-K1. R & R SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 36,048 hrs · 34,918 cycles

LAVATORY SMOKE DETECTOR FALSE ALARM. NO EVIDENCE OF SMOKE OR FIRE. NO COCKPIT INDICATION. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. NO FIRE DAMAGE NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,627 hrs · 28,390 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 1 & 2.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,612 hrs · 28,378 cycles

PASSENGER DOOR & SERVICE DOOR GREEN EXIT SIGNS & ROW 1 FLOOR TRACK LIGHTING INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,242 hrs · 28,023 cycles

EMERGENCY LIGHT FROM ROW 2 - 5 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,149 hrs · 34,059 cycles

FLOOR TRACK LIGHTING INOPERATIVE AT ROW 6 - 8.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,861 hrs · 27,681 cycles

STRIP OF EMER FLOOR LIGHTS BETWEEN ROWS 6 - 8 DO NOT ILLUMINATE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,804 hrs · 27,632 cycles

EMERGENCY LIGHTS ROW 5 -8 INOPERATIVE. EMER EXIT SIGN INOPERATIVE ON RT SIDE AT ROW 8. R & R BATTERY PACK IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 27,777 hrs · 27,609 cycles

FIRST FLIGHT OF THE DAY, PAX DOOR FWD EXIT SIGN WAS FOUND INOPERATIVE. FOUND BROKEN WIRES BEHIND THE FLIGHT ATTENDANT`S SEAT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,717 hrs · 27,548 cycles

EXPERIENCED A MALFUNCTION OF A SECTION OF FLOOR TRACK LIGHTING & A SIDEWALL EXIT LIGHT AT AN OVERWING EXIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,734 hrs · 33,688 cycles

EMERGENCY LIGHTING ROW 8 & FLOOR TRACKS LIGHTING ROW 6 - 8 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,616 hrs · 27,515 cycles

EMERGENCY FLOOR LIGHTING ROW 6 - 8 INOPERATIVE. WINDOW LIGHTING 8D,F INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,661 hrs · 27,501 cycles

EMERGENCY LIGHTING FLOOR TRACK UNLIT ROW 6 - 8.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,657 hrs · 27,494 cycles

FLOOR TRACK EMER LIGHT INOPERATIVE FROM ROW 6 - 8.

Part: WIRE — PULLED (CABIN) · airframe 27,608 hrs · 27,450 cycles

EMERGENCY LIGHTS BETWEEN ROWS 9 - 12 INOPERATIVE. INSPECTED FLOOR TRACK LIGHTING & FOUND WIRING PULLED FROM CONNECTOR AT ROW 13. APPLIED TAPE TO BARE WIRE & APPLIED MEL. CONNECTOR TO BE REPLACED AT MX BASE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,576 hrs · 33,539 cycles

FLOOR EMER LIGHTS ROW 6 - 9 INOPERATIVE & LOWER RT EMER EXIT LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,510 hrs · 27,361 cycles

EMERGENCY LIGHTS FLOOR TRACK OUT BETWEEN ROWS 6 - 8.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,180 hrs · 32,193 cycles

PRE-EXISTING DOUBLER AT FS 250, STRINGER 25L TO STRINGER 27L BE REMOVED. REPAIRED PRE-EXISTING DOUBLER IAW BA REO 601R-53-1102630 DATED 2-20-2014.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

PAX DOOR LOWER SILL IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR LOWER SILL THEN INSTALLED SERVICEABLE FLOOR SILL IAW SRM 51-42-06 & 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 33,180 hrs · 32,193 cycles

RT FLOOR SILL AT FS 621 TO 559 & 96 HAS CORROSION IAW BA REO 601R-53-00-526. REMOVED UNSERVICEABLE RT FLOOR SILL & FABRICATED SERVICEABLE FLOOR SILL 2 FS 559 & 96 TO FS 621.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,180 hrs · 32,193 cycles

AIRCRAFT GND POWER PLUG MOUNT BRACKET IS CRACKED ON FWD OTBD CORNER. REMOVED CRACKED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-42-21, 51-42-13 & 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

CORROSION ON CARGO BAY FLOOR SUPPORT BEAM NEAR FS 600.00 LBL 30. REPAIRED CARGO BAY FLOOR SUPPORT IAW REO.601R-53-00-005REV B, SRM 51-42-21, 51-42-06, 51-25-06, 51-25-16 & 51-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

CORROSION UNDER RT LIGHTNING PANEL FWD OTBD MOUNT AT FS 349.00, RBL 40. R & R RT FLOOR SUPPORT AT FS FS349.00 WITH NEW SERVICEABLE PART IAW EA 15-2014-019 REV A DATED 2/7/14.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

CORROSION ON TOP & BOTTOM OF RT OTBD FLOOR SILL AT FS349.00. R & R WITH NEW SERVICEABLE FLOOR SILL IAW STS EA 15-2014-326 REV A DATED 2-13-14.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 33,180 hrs · 32,193 cycles

CARGO BAY DOOR HANDLE HOUSING CRACKED. REMOVED CRACKED HANDLE, THEN INSTALLED NEW HOUSING IAW CRJ200 SRM51-40-1151-25-16 & AMM 52-70-02.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 33,180 hrs · 32,193 cycles

CARGO BAY DOOR SUPPORT FWD CLIP IS CRACKED. REMOVED CRACKED CLIP THEN FABRICATED NEW CLIP & INSTALLED IAW SRM 51-11-20, 51-25-06 & 51-25-16.

Part: STRUT — CHAFED (NLG) · airframe 33,180 hrs · 32,193 cycles

NLG PROX SWITCH WIRE HARNESS HAS WORN THROUGH PAINT ON NLG STRUT. BLENDED OUT CHAFING ON NLG STRUT IAW REO 601R-32-21-796, AMM32-61-05, SRM 51-42-02, 51-24-11, 51-21-11 & 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

LT & RT FLOOR SEAT TRACK 409 & 128 THROUGH 379 CORRODED. REMOVED UNSERVICEABLE SEAT TRACK & REPLACED WITH NEW SERVICEABLE TRACK.

Part: SILL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

CARGO DOOR LOWER SILL CRACKED AT AFT STOP. REMOVED CRACKED FLOOR SILL, THEN FABRICATED NEW SERVICEABLE SILL IAW REO 601R-53-61-690REV D.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

PAX DOOR TOP STEP HINGE CORRODED. R & R WITH SERVICEABLE PART, PN 601R31980-41 IAW SRM 51-40-11 & 51-42-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

RT OTBD FLOOR SILL AT FS 319 IS CORRODED. R & R SILL PLATE & STIFFENER WITH SERVICEABLE PARTS IAW SRM 51-42-06, 51-42-13 & 51-40-11.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

TWO EACH CARGO TIE DOWNS ON RBL 9 AT FS 559 & 112 THROUGH 559 & 96 HAS CORROSION. CRJ200 53-61-49 & 51-21-06, REMOVED CORRODED TIE DOWNS, TWO EACH & INSTALLED NEW SERVICEABLE TIE DOWNS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,180 hrs · 32,193 cycles

RIGHT OBLIQUE ANGLE CRACKED. R & R RT OBLIQUE ANGLE IAW SRM 51-40-11, 51-21-11 & 51-42-21.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

FIVE EACH CARGO TIE DOWN AT FS 621 THROUGH 559 & 96. REMOVED CORROSION FROM THREE EACH CARGO TIE DOWN TRACKS. R & R TWO EACH CARGO TIE DOWN CLEATS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,180 hrs · 32,193 cycles

LT HAND UNDER FLOOR SUPPORT AT FS 484, INBD CLIP CRACKED. R & R WITH SERVICEABLE CLIP IAW SRM 51-40-11, 51-42-06 & 51-42-21.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

THREE EACH TIE DOWNS ON LBL 27 CARGO AREA HAVE CORROSION. R & R THREE EACH TIE DOWNS ON LBL 27 IN CARGO AREA.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,180 hrs · 32,193 cycles

TOP OF LATERAL FLOOR SUPPORT AT FS 559 & LBL 27 - 43 CORRODED. R & R SUPPORT STRAP IAW SRM 51-40-11 & 51-42-06.

Part: SEAL — CRACKED (RT SPOILER) · airframe 33,180 hrs · 32,193 cycles

RT FLIGHT SPOILER OTBD SPRING SEAL CRACKED. R & R SPRING SEAL PN 601R10226-130 IAW SRM 51-40-11 & 51-42-06.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 29,843 hrs · 29,844 cycles

AFTER TAKEOFF SMOKE BEGAN COMING OUT OF THE VENTS IN THE COCKPIT AND AT ROW 8 IN THE CABIN. THE SMOKE CONTINUED UNTIL THE AC WAS ON THE GROUND. AIRCRAFT HAS A BURNING SMELL IN CABIN AND COCKPIT. CAME BACK AROUND AND LANDED WITHOUT INCIDENT. LANDING WEIGHT 45,000 LBS. RAN AIRCRAFT WITH APU AIR AND ENGINE AIR. ENGINE AIR RUNS CLEAR. APU AIR IS CONTAMINATED. SUSPECT DEICE FLUID. SEE 238190/4 FOR MEL.

Part: LANDING GEAR — MALFUNCTIONED · airframe 22,169 hrs · 22,188 cycles

AFTER TAKE OFF, AFTER 10 MINUTES, BROUGHT GEAR UP AT 22 IAS. RECEIVED GEAR DISAGREE AURAL MESSAGE FOLLOWED BY NOSE DOOR MESSAGE. THEN GEAR WENT UP AND LOCKED. NO GEAR MESSAGES (ENTIRE EVENT LASTED ABOUT 20 SECONDS). COMPLIED WITH OVERSPEED INSPECTION, NO DEFECTS NOTED IAW AMM 05-51-04.

Part: LANDING GEAR — MALFUNCTIONED · airframe 29,293 hrs · 28,429 cycles

AFTER TAKE OFF, BROUGHT GEAR UP AT 220 KIAS. RECEIVED GEAR DISAGREE AURAL MESSAGE FOLLOWED BY NOSE DOOR MESSAGE. THEN GEAR WENT UP AND LOCKED. NO GEAR MESSAGES, ENTIRE EVENT LASTED ABOUT 20 SECONDS. COMPLIED WITH OVERSPEED INSPECTION. NO DEFECTS NOTED IAW AMM 05-51-04.

Part: WARNING LIGHT — FALSE ACTIVATION (WING OVERHEAT) · airframe 21,679 hrs · 21,717 cycles

WING OVERHEAT WARNING ON TAKE OFF. HIGH SPEED ABORT. ACARS REPORTING 139 KIAS. WING ANTI-ICE WAS SELECTED NORMAL. WITH ASSISTANCE FROM CREW, RAN ENG AND OPS CHECKED IAW AMM 30-11-01. OPS CHECKED GOOD.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 28,334 hrs · 27,473 cycles

RT OTBD FLAP OTBD GIMBLE FITTING CHAFED. BLENDED CHAFED AREA ON RT OTBD FLAP OTBD GIMBLE FITTING IAW SRM 51-12-00.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYS) · airframe 21,353 hrs · 21,378 cycles

RECEIVED LEFT WING ANTI ICE CAUTION MESSAGE IN FLT. COMPLIED WITH QRH, MESSAGE REMAINED. FOUND OVERHEAD PANEL HEAT SWITCH WITH HIGH RESISTANCE THRU CONTACTS, R & R SWITCH IAW CMM 30-12-21. OPS CHECKED GOOD.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 28,334 hrs · 27,473 cycles

FWD INBD TORQUE TUBE COVER ATTACH BRACKET ON PAX DOOR CRACKED. R & R BRACKET IAW SRM 51-41-02.

Part: FRAME — CORRODED (FS 349) · airframe 28,334 hrs · 27,473 cycles

FWD AND AFT SIDE OF FS 349 FRAME BETWEEN STRINGER 26R AND 26L IS CORRODED. R & R FRAME.

Part: HINGE — GOUGED (PAX DOOR) · airframe 28,334 hrs · 27,473 cycles

PAX DOOR HINGE (FUSELAGE SIDE) HAS GOUGED LUGS AFT NR2 AND NR15. REPAIRED IAW REO 601R-53-21-814.

Part: SKIN — CHAFED (FS 484-544) · airframe 28,334 hrs · 27,473 cycles

LEFT FUSELAGE SKIN BEHIND LT STAB FAIRING IS CHAFED FOUND AREA TO BE OUT OF LIMITS IAW REO 601R-53-41-341. BLENDED CHAFED AREA ON LT SKIN BEHIND LT STUB FAIRING. REPAIR AREA LT FUSELAGE SKIN BEHIND LT STUB FAIRING IAW REO 601R-53-41-341, REV C.

Part: SKIN — CRACKED (FS 235) · airframe 28,334 hrs · 27,473 cycles

CRACK IN NLG CUT OUT REQUIRED REO 601R-53-11-048, REV C.

Part: SKIN — DAMAGED (FS 589-605) · airframe 28,334 hrs · 27,473 cycles

TEMPOARY REPAIR TO FUSELAGE SKIN BETWEEN FS 589 & 605 BETWEEN STR 21R-26R MULTIPLE DAMAGE CAUSED BY GROUND AIR DOOR. REPAIRED IAW REO 601R-53-61-4359, REV A.

Part: HINGE BRACKET — CRACKED (LT WING) · airframe 28,334 hrs · 27,473 cycles

LEFT OTBD FLAP CENTER HINGE AREA CRACKED ON INBD FAIRING GUID. R & R LT OTBD FLAP CENTER HINGE AREA FAIRING GUIDE BRACKET.

Part: FITTING — GOUGED (FS 349-355) · airframe 28,334 hrs · 27,473 cycles

UNDER SERVICE DOOR THRESHOLD FITTING IS GOUGED AT FS 349.00. BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW SRM 51-12-00.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 28,334 hrs · 27,473 cycles

FWD CARGO DOOR STOP FITTING FWD LWR CLIP CRACKED UNDER DOOR SILL AT FS 587, STR 17 LT. INSTALLED SERVICEABLE FWD CARGO STOP FITTING IAW SRM 51-40-11, 51-42-10, 51-42-21, 51-41-04.

Part: HINGE FITTING — SCRATCHED (RT ELEVATOR) · airframe 28,334 hrs · 27,473 cycles

RIGHT ELEVATOR HAS A SCRATCH ON LOWER INBD CORNER NR 2 HINGE FITTING. BLENDED AREA ON RT ELEVATOR AT LOWER INBD CORNER NR 2 HINGE FITTING.

Part: FITTING — GOUGED (FS349-355) · airframe 28,334 hrs · 27,473 cycles

UNDER SERVICE DOOR THRESHOLD FITTING IS GOUGED AT FS 349.00. BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW SRM 51-12-00.

Part: HINGE FITTING — GOUGED (RT ELEVATOR) · airframe 28,334 hrs · 27,473 cycles

RT ELEVATOR NR2 HINGE FITTING HAS GOUGES LWR SIDE. REPAIRED IAW REO 601R-55-21-351.

Part: PANEL — CRACKED (RUDDER)

LIGHTNING PANEL STRUCTURE BELOW RUDDER CRACKED. R & R PART IAW SRM 51-41-06.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 28,334 hrs · 27,473 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED. REMOVED UNSERVICEABLE PAX DOOR AFT ANCHOR FITTING AND REPLACED WITH SERVICEABLE PAX DOOR AFT ANCHOR FITTING.

Part: SKIN — CHAFED (FS 516.85-559) · corrosion level 1 · airframe 28,334 hrs · 27,473 cycles

RT FUSELAGE SKIN IS CHAFED BEHIND STUB FAIRING. REPAIR COMPLIED WITH REO 601R-53-41-341.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 28,334 hrs · 27,473 cycles

FOUND INDICATION OF CORROSION ON FWD INBD END OF FUEL PANEL 540AB BLENDED AREA ON FWD INBD END OF FUEL PANEL 540AB IAW SRM 51-12-00.

Part: ATTACH FITTING — CRACKED (FS 605) · airframe 28,334 hrs · 27,473 cycles

ATTACH FITTING CRACKED AT UPPER RADIUS STR 17 AT FS 605. INSTALLED SERVICEABLE CARGO DOOR SILL ANGLE AT FS 605 IAW SRM 51-41-00, 51-42-21 & 51-41-04.

Part: ACTUATOR — DAMAGED (INBD FLAP VANE) · airframe 28,334 hrs · 27,473 cycles

LEFT INBD FLAP, LT INBD FLAP VANE ACTUATOR DAMAGE BLENDED DAMAGE AREA ON LT FLAP INBD, FLAP VANE ACTUATOR IAW SRM 51-12-00.

Part: ANGLE — CRACKED (WS 149.58) · airframe 28,334 hrs · 27,473 cycles

LEFT WING UPPER ANGLE CRACKED AT OTBD CORNER. REMOVED AND FABRICATED ANGLE IAW SRM 51-40-11, 51-31-06.

Part: FLOOR SUPPORT — CORRODED (FS 449.85-473.15) · airframe 28,334 hrs · 27,473 cycles

RT OTBD FLOOR SUPPORT IS CORRODED IN TWO PLACES ALONG RBL 47 AT FS 449.85 AND FS 473.15. BLENDED RT OTBD FLOOR SUPPORT ALONG RBL47 AT FS 449.85 AND FS 473.15. FOUND TO BE WITHIN LIMITS WITH DEEPEST BLEND .003 MAX BLEND DEPTH OF .015 IAW REO 601R53-41-666, REV B.

Part: FRAME — DENTED (FS 672.20) · airframe 28,334 hrs · 27,473 cycles

FRAME FS 672.20 DENTED. REPAIRED DENT ON FRAME FS 672.20 IAW REO 601R-53-61-4353.

Part: DOOR — CRACKED (APU BAY) · airframe 28,334 hrs · 27,473 cycles

APU ENCLOSURE BOX HAS MULTIPLE CRACKS AND APU ENCLOSURE BOX DOOR HAS CRACKED. REPAIRED IAW REO 601R-49-11-070, REV A.

Part: ATTACH BRACKET — CRACKED (FS 574) · airframe 28,334 hrs · 27,473 cycles

CARGO TRACK FWD LOWER ATTACH BRACKET CRACKED. R & R ATTACH BRACKET IAW SRM 57-42-06, 51-40-11.

Part: RIB — CRACKED (WS 53 - 53.6) · airframe 28,334 hrs · 27,473 cycles

LEFT AND RIGHT RIBS ARE CRACKED. REPAIRED LT AND RT BATT RIBS IAW REO 601R-57-51-016.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 28,334 hrs · 27,473 cycles

RT NR 3 SEAT TRACK CORRODED AT FS 409.00+112-FS 559.00+16. BLENDED CORRODED AREA ON RT NR 3 SEAT TRACK DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 51-21-49. REMOVED UNSERVICEABLE SEAT TRACK IAW SRM 51-41-00. FABRICATED SERVICEABLE SEAT TRACK.

Part: MOUNT — BROKEN (RT STAB FAIRING) · airframe 28,334 hrs · 27,473 cycles

RT STUB FAIRING FWD MOUNT LOOP BROKEN. R & R IAW SRM 51-42-21.

Part: ANGLE — CRACKED (WS 143.189) · airframe 28,334 hrs · 27,473 cycles

LEFT WING AT WS 143.189, INBD ANGLE IS CRACKED UNDER PANEL 520ML. R & R IAW SRM 51-41-02.

Part: SUPPORT — GOUGED (FS 682-700) · airframe 28,334 hrs · 27,473 cycles

RT FRAME SUPPORT AT FS 700 AT AEB DOOR OPENING IS GOUGED INSIDE AEB COMPARTMENT. BLENDED DAMAGED AREA TO A SMOOTH PROFILE.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,334 hrs · 27,473 cycles

RT INBD FLAP VANE IS CHAFED IN 3 PLACES. BLENDED RT INBD FLAP VANE IN 3 AREAS IAW REO 601R-57-52-004.

Part: FAIRING — CHAFED (RT STAB) · airframe 28,334 hrs · 27,473 cycles

RT STUB FAIRING CHAFED & GOUGED FROM FLAP. BLENDE CHAFED AREA ON RT STUB FAIRING IAW REO 601R-53-82-003 & SRM 51-12-00 TO WITHIN ALLOWABLE LIMITS.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,334 hrs

LT INBD FLAP VANE HAS 3 CHAFES. BLENDED DAMAGED AREAS IAW REO 601R-57-52-004.

Part: CLEAT — CORRODED (BS 300-340) · corrosion level 2 · airframe 28,334 hrs · 27,473 cycles

PAX DOOR CLEAT (AFT) CORRODED BEYOND SERVICEABLE LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE PAX DOOR CLEAT IAW SRM 51-42-06 & 52-42-21.

Part: DRAG ANGLE — CRACKED (BS 347.25) · airframe 28,334 hrs · 27,473 cycles

AFT DRAG ANGLE ON PAX DOOR CRACKED ABOVE DOOR ASSIST PULLEY BRACKET. REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513.

Part: SKIN — CHAFED (RT AILERON) · airframe 28,334 hrs · 27,473 cycles

RT WING AILERON PANEL 699CB IS CHAFING. REPAIRED RT WING AILERON PANEL 699CB IAW SRM 51-12-00 AND SRM 57-60-00.

Part: HINGE — GOUGED (BS 317-349) · airframe 28,334 hrs · 27,473 cycles

PAX DOOR HINGE (DOOR SIDE) HAS GOUGED LUGS NR6 & NR13. BLENDED DOOR HINGE ON NR 6 AND NR 13 LUGS IAW REO 601R-52-11-1347, ORIG MAT .110". REMOVED .002" WITH .108 MAT REMAINING ON NR6 LUG, NR13 LUG, ORIG MAT .113". REMOVED .002 MAT WITH .111 MAT REMAINING, BOTH ARE WITHIN LIMITS IAW REO 601R-52-11-1347.

Part: PANEL — CHAFED (LT AILERON) · airframe 28,334 hrs · 27,473 cycles

RT WING AILERON PANEL 699BB IS CHAFING. REPAIRED RT WING AILERON PANEL 699BB IAW SRM 51-12-00 AND SRM 57-60-00.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 28,334 hrs · 27,473 cycles

CARGO DOOR OUTER HANDLE HOUSING GUGED IN MULTIPLE. REPAIRED IAW REO 601R-52-31-086.

Part: WIRE — SPARKS (CIRCUIT BREAKER) · airframe 25,840 hrs · 24,871 cycles

WHILE GETTING DE-ICED, PILOTS HEARD STRANGE SOUND IN COCKPIT, GOT UP FROM SEAT, SAW WIRES FROM CB PANEL 2 GLOWING AND SPARKING. HAD F/O TURN NR 2 GEN OFF, SELECTED AUTO TRANSFER SWITCH OFF, GRABBED COCKPIT FIRE EXTINGUISHER, PUT GLOWING AND SPARKED WIRES (REF 233651) COCKPIT FLOOR WET FROM MELTED SNOW, NO FIRE OR SMOKE RETURNED TO GATE. REMOVED RESIDUAL FIRE EXT AGENT AND CLEANED AFFECTED AREA OF COCKPIT, VISUALLY INSPECTED COCKPIT & CBP2 FOR EVIDENCE OF ELECTRICAL DAMAGE. NO DAMAGE FOUND. UPON FURTHER INVESTIGATION, FOUND DAMAGED CONDUIT AND WIRING RUNNING TO OBS SEAT HEADSET JACK AND O2 MASK LT SW ON JACK PANEL. INSULATED WITH HEAT SHRINK AND NEW PROTECTIVE SLEEVE.

Part: SENSOR — SHORTED (TEMP) · airframe 25,596 hrs · 24,615 cycles

"ANTI-ICE DUCT" WARNING MESSAGE INFLIGHT. SYNOPTIC PAGE SHOWED RT WING RED. C/W QRH AND MESSAGE CLEARED. FOUND SHORT TO GROUND ON RT WING OTBD L/E SENSOR S28WK. REPLACED TEMP SENSOR IAW AMM 36-21-03. OPS TEST GOOD AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (TEMP) · airframe 25,626 hrs · 24,650 cycles

ANTI-ICE DUCT WARNING MESSAGE INFLIGHT. SYNOPTIC PAGE SHOWED RT WING RED. COMPLIED WITH QRH AND MESSAGE CLEARED. FOUND SHORT TO GROUND ON RT WING OTBD L/E SENSOR S28WK. REPLACED TEMP SENSOR IAW AMM 36-21-03. OPS TEST GOOD AT THIS TIME.

Part: FITTING — MISALIGNED (RT ELEVATOR ACT) · airframe 24,783 hrs · 23,769 cycles

RT ELEVATOR INDICATES HALF SCALE PITCH DOWN. INSTALLED NEW LOCK FASTENER IN LOWER POSITION ON AFT ACTUATOR FITTING ASSY, ON ELEVATOR RT SIDE IAW DWG NR 601R-24-05-6.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 24,538 hrs · 23,509 cycles

ACFT RT WING TIP STRUCK WING OF PARKED ACFT DURING TAXI. R & R RT WINGLET AFT/FWD SPAR CHANNEL REF DWG NR 600-15108, SRM 51-42-2, 51-42-26, 51-40-11 AND DWG NR 600-15102.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 23,935 hrs · 22,860 cycles

SERVICE DOOR THRESHOLD ANGLE CORRODED. R & R THRESHOLD ANGLE IAW SRM 51-24-16, 51-42-21, 51-42-13.

Part: SEAT TRACK — DAMAGED (BS 235) · airframe 23,935 hrs · 22,860 cycles

DOUBLE DRILLED HOLE ON PILOT SEAT TRACK INBD TRACK COMPLIED WITH REPAIR OF DOUBLE DRILLED HOLE ON PILOT INBD SEAT TRACK IAW DWG CAS-CRJ-534702.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 23,935 hrs · 22,860 cycles

FS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED FS 202.75 PRESSURE BULKHEAD IAW REO 601R53-11-563.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 23,935 hrs · 22,860 cycles

FS559 PRESSURE BULKHEAD REG`S REO 601R-53-41-260. REPAIRED FS559.00 IAW REO 601R-53-41-260.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

280 AFT FLOOR SUPPORT ANGLE CRACKED LBL 9 REPAIRED IAW REO 601R-53-11-138.

Part: SEAL — DAMAGED (LT ENGINE) · airframe 23,935 hrs · 22,860 cycles

LT JET PIPE UPPER AND LOWER SEALS REQUIRE REPLACEMENT. R & R UNSERVICEABLE SEALS ON LT JET PIPE UPPER AND LOWER IAW CMM 78-11-00.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 23,935 hrs · 22,860 cycles

CORROSION ON RT WING OTBD L/E WHERE PICCOLO TUBE ATTACHES. R & R UNSERVICEABLE RIB PN 601R12063.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

FS280, RBL 9 INBD CLIP CRACKED. REMOVED DAMAGED CLIP, DUPLICATED PART AND INSTALLED NEW SERVICEABLE CLIP.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

FS 280, RBL 9 OTBD ATTACH CLIP CRACKED. REMOVED DAMAGED CLIP. DUPLICATED PART, AND INSTALLED NEW SERVICEABLE CLIP.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,935 hrs · 27,860 cycles

MWC 51552-2000-0130 FS 280 FLOOR SUPPORT CRACKED AT RBL 9. COMPLIED WITH REO 601R-53-11-1842.

Part: STIFFENER — DAMAGED (BS 621) · airframe 23,935 hrs · 27,860 cycles

VERTICAL STIFFENER AT RBL 18 HAS DRILL START DAMAGED DUMMY 621 MOD REPAIRED IAW REO NR 601R53-61-3529, REV A.

Part: PANEL — CRACKED (PAX DOOR) · airframe 23,935 hrs · 27,860 cycles

REPAIR CRACK ON PAX DOOR TOP PANEL UNDER TOP STEP AFT SIDE AND REQUIRED. REMOVED DAMAGED PAX DOOR EDGE MEMBER UNDER TOP STEP AND INSTALL SERVICEABLE EDGE MEMBER IAW SRM 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,935 hrs · 22,860 cycles

PAX DOOR AFT INNER AND OUTER CORNER ANGLES AT DATUM 8 CORRODED. R & R AFT INNER AND OUTER CORNER ANGLES IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,935 hrs · 22,860 cycles

PAX DOOR FWD INNER AND OUTER CORNER ANGLES AND DATUM 8 CORRODED. R & R FWD INNER AND OUTER CORNER ANGLES IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS461) · airframe 23,935 hrs · 22,860 cycles

FITTING AT RBL 10, FS 461.0, ON FLOOR SUPPORT BEAM CRACKED (BATH TUB) PN 600-31068-19. R & R FITTING IAW SRM.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

FS 280, LBL 9, INBD CLIP CRACKED. FABRICATED NEW CLIP AND INSTALLED IAW REO 601R-53-11-171 REV D.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

FLOORBOARD SUPPORT (OTBD) ANGLE CRACKED ATTACHED TO FS 280 FRAME AT LBL 9. FABRICATED NEW CLIP AND INSTALLED IAW REO 601R-53-11-171, REV D.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 23,935 hrs · 22,860 cycles

WHILE REMOVING BRACKET IN LT WW FOR 559 REPAIR, FOUND PREVIOUS DOUBLE DRILLED HOLES UNDER BRACKET. 2 EA DOUBLE DRILLED HOLES LT WHEEL WELL AT FS 559, BL 18.00. REPAIRED BY PO NR 961789.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,935 hrs · 22,860 cycles

FS 280 FLOOR SUPPORT CRACKED AT LBL 9 AT ALT RELEASE CABLE MOUNT BRACKET. PERMANENT REPAIR INCORPORATED IAW GENERIC REO 601R-53-11-171, REV D.

Part: ANGLE — CORRODED (BS 338.968) · corrosion level 2 · airframe 23,935 hrs · 27,860 cycles

PAX DOOR FS 338.968 AT DATUM 8 INBD AND OTBD ANGLES ARE CORRODED. R & R INBD & OTBD ANGLES IAW SRM 51-42-06, 51-42-13, 51-42-21.

Part: ANGLE — CORRODED (BS 320.163) · corrosion level 2 · airframe 23,935 hrs · 27,860 cycles

PAX DOOR FS 320.163 AT DATUM 8 INBD & OTBD ANGLES ARE CORRODED. R & R INBD AND OTBD ANGLES IAW SRM 51-42-06, 51-42-13, 51-42-21.

Part: ANGLE — CORRODED (BS 329.503) · corrosion level 2 · airframe 23,935 hrs

PAX DOOR FS 329.503 AT DATUM 8 ANGLE IS CORRODED. R & R ANGLE IAW SRM 51-42-06, 51-42-13 & 51-42-21.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,935 hrs · 22,860 cycles

RT INBD FS 484, RBL 27 CLIP CRACKED. REPAIRED IAW REO 601R-53-41-059 REV A.

Part: SKIN — GOUGED (LT WING) · airframe 23,935 hrs · 27,860 cycles

LT WING OTBD L/E INNER SKIN AT INBD END GOUGED. TRIMMED EDGE IAW SRM 57-00-31.

Part: STIFFENER — CRACKED (BS 559) · airframe 23,935 hrs · 22,860 cycles

VERT STIFFENER AT RBL 9 CRACKED ON 559 PRESSURE BULKHEAD. REPLACED DURING REO 601R-53-41-260 INCORPORATION.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,935 hrs · 22,860 cycles

INTERCOSTAL CLIP CRACKED AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 625) · airframe 23,935 hrs · 22,860 cycles

LT OBLIQUE ANGLE AT FS 625 CRACKED. R & R IAW SRM.

Part: ANGLE — CRACKED (BS 625) · airframe 23,935 hrs · 22,860 cycles

RT OBLIQUE ANGLE CRACKED AT FS 625.0, R & R IAW SRM.

Part: FRAME — CRACKED (PAX DOOR) · airframe 23,935 hrs · 22,860 cycles

PAX DOOR UPPER FRAME CRACKED AT FS 338.90. REPAIR IAW REO 601R-52-11-402.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 23,935 hrs · 22,860 cycles

CRACKED ATTACH ANGLE UNDER 326CL LT TOP SIDE OF VERT STAB PN 600-21137-5. DUPLICATE AND REPLACE IAW SRM.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 23,935 hrs · 22,860 cycles

CRACKED ATTACH ANGLE UNDER PANEL 326C, PN 60021137-5. R & R IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 23,935 hrs · 22,860 cycles

CENTER L/E ON RT WING INBD ATTACH FLANGE CRACKED. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 23,935 hrs · 27,860 cycles

FLOOR SUPPORT AT FS 621 LT END CRACKED AT PREVIOUS REPAIR. (LBL 36) REPLACED FILLER IAW REO 601R-53-61-117.

Part: SKIN — CRACKED (RT WING) · airframe 23,935 hrs · 22,860 cycles

INNER SKIN OF RT OTBD WING L/E CRACKED. REPLACED WEB IAW SRM 51-42-10.

Part: ANGLE — CRACKED (LT WING) · airframe 23,935 hrs · 22,860 cycles

ATTACH ANGLE AT INBD END OF WING L/E 530JL CRACKED (PN 600-12045-11).

Part: STRUCTURE — CRACKED (NLG DOOR) · airframe 23,707 hrs · 22,624 cycles

NLG DOOR MECH BASE IS CRACKED AT LOWER AFT PIVOT OF HYD ACTUATOR RT SIDE. R & R RT SIDE NLG DOOR MECH ASSY. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 22,829 hrs · 21,777 cycles

EDDY CURRENT INSPECTION SHOWS STRONG DISCONINUITY INDICATION OF FWD FACE OF AFT PRESSURE BULKHEAD AT APPROX LBL 11.0 AND WL 116.0. INDICATION IS APPROX 0.5" IN LENGTH AND RUNS ROUGHLY VERTICALLY. EO 601R-53-61-3301, REV A AND GREO 601R-53-61-1285 TO REAR PRESSURE BULKHEAD. (K)

Part: CHECK VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 22,011 hrs · 20,992 cycles

291717/3 -14TH STAGE BLEED AIR CHECK VALVE REMOVED FOR INSPECTION. FOUND BUTTERFLY VALVE PARTS MISSING. REF LOG 201715/1 - RT WING ANTI-ICE OVERHEAT. ENGINE NR 2, 14TH STAGE BLEED AIR CHECK VALVE REPLACED IAW AMM 30-12-01 MISSING PIECES FOUND IN REMOVED RT PICCOLO TUBE. REF 201715/3. LEAK AND OPS TEST OF BLEED AIR CHECK VALVE OK. IAW AMM 30-12-00. (K)

Part: PICCOLO TUBE — DAMAGED (RIGHT) · airframe 21,982 hrs · 20,962 cycles

ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT WITH ANTI-ICE SELECTED ON. RT WING L/E SHOWED RED ON SYNOPTIC PAGE. REMOVED AND REPLACED RT OTBD PICCOLO TUBE IAW AMM 30-11-14. (K)

Part: WINDOW — CRACKED (COCKPIT) · airframe 21,859 hrs · 20,846 cycles

THE RT COCKPIT WINDOW CRACKED. REMOVED AND REPLACED F/O`S WINDOW IAW AMM 56-12-01. OPS AND LEAK CHECK GOOD. (K)

Part: FITTING — LOOSE (FUEL LINE) · airframe 21,470 hrs · 20,466 cycles

LOG 188378/2 AND 3 - ACFT LEAKING FUEL FROM AFT DRAIN MAST AT TAIL. ACFT SMELLS LIKE FUEL INSIDE CABIN. VERIFIED LEAK COMING FROM APU AND STOPPED WITH APU SHUTDOWN AND ODOR IN CABIN DISSAPATED, REF 188378/3 FOR MEL. RESECURED LOOSE FITTING BETWEEN FCU AND SOLENOID SOV IAW 49-31-05. APU OPS CHECK AND LEAK CHECKS GOOD. REMOVED FROM MEL. (K)

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 21,875 hrs · 20,860 cycles

A SKID IB CAUTION MSG ON GEAR EXTENSION. T/S IAW FIM 32-40-00, SHEET 7 BLK 9 ASCU BITE SKID CHECK W/N PASS, REMOVED AND REPLACED ASCU IAW AMM 32-44-06. OPS TEST GOOD. (K)

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYSTEM) · airframe 21,318 hrs · 20,320 cycles

LOG 188366/3 ANTI-SKID INBD CAUTION MSG ON GEAR EXTENSION. T/S PER FIM 32-40-00. ASCU BITE SKID CHECK W/N PASS, R&R ANTI-SKID CONTROL UNIT IAW AMM 32-44-06. OPS TEST GOOD.

Part: FLAP SYSTEM — OUT OF RIG (TE FLAPS) · airframe 20,293 hrs · 19,369 cycles

AIRCRAFT ROLLS LT WITH THRUST, EVEN IN DESCENT AND CRUISE. APPROXIMATELY 50% TRIM RWD. CAPTAIN YOKE HAS FREE PLAY (LT AND RT), FIRST OFFICERS YOKE NORMAL. FLAPS FOUND OUT OF RIG. FLAPS HAVE BEEN RIGGED USING AMM 27-51-00. BOTH LT AND RT CONTROL WHEEL QUADRANTS CABLE TENSIONS FOUND OUT OF TOLERANCE, BOTH QUADRANTS CORRECT CABLE TENSIONS USING AMM 27-11-00. FOUND SYS OK AT THIS TIME. (A)

Part: TARGET — OUT OF ADJUST (MLG UPLOCK) · airframe 20,010 hrs · 19,101 cycles

GEAR DISAGREE LT MLG SHOWS HATCHED. COMPLIED WITH QRH, RETURNED TO PHL. SECURED LT MLG UPLOCK TARGET REF AMM 32-32-05, OPS CHECK AND GEAR SWINGS GOOD.

Part: THROTTLE — OUT OF ADJUST (RT ENGINE) · airframe 19,835 hrs · 18,930 cycles

UPON ENGINE SHUTDOWN, RIGHT ENGINE CONTINUED TO RUN WITH THRUST LEVER IN SHUTOFF POSITION. WORKED THROTTLE LEVER, ENGINE EVENTUALLY SHUTDOWN. ADJUSTED THROTTLE CONTROL RIGHT ENGINE IAW 76-11-17. PERFORMED IDLE SPEED CHECK IAW 70-00-00. OPS CHECK GOOD. (A)

Part: FAN — MISINSTALLED (INSTRUMENT PNL) · airframe 19,658 hrs · 18,766 cycles

CAPTAIN AND F/O RECEIVED DISPLAY TEMP MESSAGE ON PFD`S. BOTH ATTITUDE INDICATORS SHOW BLACK. FOUND COCKPIT DISPLAY COOL GROUND FAN CONNECTOR LOOSE. SECURED CONNECTOR AS REQUIRED. ALSO FOUND COCKPIT DISPLAY COOL FLIGHT FAN INSTALLED BACKWARDS. RE-INSTALLED FLIGHT FAN IAW AMM 21-24-19. DISPLAY COOL SYSTEM OPS CHECK GOOD IAW AMM 21-24-19. CAPT AND F/O`S PFD DISPLAY TEMP CAUSED BY FAULTY DISPLAY COOLING SYSTEM. BOTH PFD`S OPS CHECK GOOD IAW AMM 31-61-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,640 hrs · 18,750 cycles

ABORTED TAKEOFF DUE TO CONFIG FLAP WARNING. FLAP INDICATION SHOWED 3 DEGREES WHEN SELECTED TO 8 DEGREES. TAKEOFF ABORTED AT 60 KNOTS. BTMS INDICATED 3-3-5-3. INTERROGATED FECU PER AMM 27-50-00. NO DEFECTS NOTED. RESET FLAP SYSTEM IAW FIM PROCEDURES. OPS CHECK OF FLAP SYSTEM GOOD IAW AMM 27-51-01. ACFT OK FOR RETURN TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 19,646 hrs · 18,756 cycles

DISPLAY COOL MSG IN FLIGHT, FOLLOWED QRH MSG STAYED ON IN STANDBY FAN POSITION DIVERTED TO PHL MSG WENT OUT INBOUND OF PHL AFTER 10-15 MINUTES. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (WING DUCT) · airframe 19,475 hrs · 18,579 cycles

WING DUCT FAIL WARNING ON EICAS/WITH MASTER WARNING. COMPLIED WITH QRH. MESSAGE CLEARED. OPS CHECK OF WING ANTI-ICE GOOD IAW AMM 30-12-00. CHECKED RESISTANCE TO GROUND AT CONTROLLERS OF 14TH STAGE LEAK DETECTION SYSTEM, NO DEFECTS FOUND.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,210 hrs · 18,324 cycles

PILOTS BULKHEAD WEB IS CRACKED AT FS 280.00, WL 85.00 LBL 27.00. (K) REPAIRED WEB IAW SRM 51-71-28 FIGURE 2. (M)

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 19,210 hrs · 18,324 cycles

SERVICE DOOR PLATE ASSY CORRODED. (K) SERVICE DOOR PLATE ASSY REPLACED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 19,210 hrs · 18,324 cycles

AT FS 574.00, WL 73.50 CARGO TRACKS LT AND RT SIDE INNER OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 1 · airframe 19,210 hrs · 18,324 cycles

AT FS 559.96 WL 73.50 CARGO TRACK LT AND RT SIDE INNER, OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)

Part: SUPPORT — CRACKED (GROUND POWER) · airframe 19,210 hrs · 18,324 cycles

AC GROUND POWER RECEPTACLE SUPPORT MEMBER IS CRACKED. (K) SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)

Part: PLATE — CORRODED (FUSELAGE) · airframe 19,210 hrs · 18,324 cycles

TWO CRACKS ON FLOOR LANDING PLATE AT FS 589 AND FS 605. (K) REPAIRED IAW REO 601R-53-61-433. (M)

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 19,210 hrs · 18,324 cycles

FLOOR LANDING PLATE CORRODED BETWEEN FS 559 + 112 TO FS 621, AROUND NUT PLATE HOLES. (K) CORROSION ON FLOOR LANDING PLATE BETWEEN FS 559 PLUS 112 TO FS 621 AROUND NUT PLATE HOLES, BENDED IAW SRM 51-21-06. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,210 hrs · 18,324 cycles

FLOOR SUPPORT CORRODED AT FS 589.0 TO 605.0 NL 73.50 LBL 10.0. (K) REPAIRED IAW REO 601R-53-00-027 REV C. (M)

Part: OIL SYSTEM — LOW (APU)

APU OIL CAUTION MESSAGE IN FLIGHT. SERVICED APU OIL IAW AMM 12-13-49. ADDED 1 PINT. PERFORMED, OPS TEST OF APU IAW 49-10-01, OPS CHECK GOOD. (M)

Part: PUSH-PULL ROD — OUT OF POSITION (PAX DOOR) · airframe 17,685 hrs · 16,836 cycles

PASSENGER DOOR WILL NOT OPEN/CLOSE FROM OUTSIDE. OPCV NORMAL FROM INSIDE. PLACARDED AND PLACED ON MEL. REPOSITIONED OUTER DOOR HANDLE PUSHPULL TUBES IAW CMM. OPS CHECK GOOD. REMOVED FROM MEL. (K)

Part: A/C PACK — MALFUNCTIONED (LEFT)

LEFT PACK HIGH PRESSURE, YELLOW AMBER CAUTION MESSAGE ON TAKEOFF. ABORTED TAKEOFF BELOW 80 KNOTS (30 KNOTS), MAX BTMS READING 3, TAKEOFF WEIGHT 44,000 LBS. PLACARDED AND PLACED ON MEL, NO RTO/HES INSPECTION REQUIRED. REMOVED AND REPLACED PRESSURE SWITCH S1HG, OPERATIONAL CHECK GOOD, IAW 21-30-00. REMOVED PLACARD, REMOVED OFF MEL. (M)

Part: RIB — CRACKED (RT WING)

RIGHT WING BATT RIB IS CRACKED 1 INCH ALONG TOP AFT CORNER AT WS 53.60. MAINTENANCE TRIMMED OUT CRACK, INSTALLED FILLER AND REPAIR ANGLE IAW REO 601R-57-51-046 REV B. (M)

Part: RIB — CRACKED (LT WING)

FOUND LEFT WING BATT RIB IS CRACKED 1 INCH LONG AT TOP AFT CORNER. MAINTENANCE REPAIRED LEFT WING BATT RIB ASSEMBLY IAW REO 601R-57-51-046 REPAIR NR 2. (M)

Part: TORQUE TUBE — OUT OF ADJUST (PAX DOOR) · airframe 15,293 hrs · 14,541 cycles

MAIN PASSENGER DOOR WOULD NOT OPEN WITH PASSENGERS ONBOARD. FUNCTION NORMAL WITH AIRCRAFT EMPTY.. PLACARDED AND PLACED ON MEL. COMPLIED WITH INSPECTION AND FUNCTION CHECK OF PASSENGER DOOR IAW AMM. PERFORMED ADJUSTMENT OF UPPER TORQUE TUBE IAW AMM. OPS CHECK GOOD. (K)

Part: HANDLE — DIRTY (PAX DOOR)

PAX DOOR WILL NOT OPEN. CLEANED PAX DOOR HANDLE ASSY AND LUBED SHOOT BOLTS PER AMM CHAPTER 12, PAX DOOR CHECKS GOOD PER AMM CHAPTER 52. (M)

Part: MOTOR — FAILED (CABIN DOOR)

UNABLE TO OPEN PAX DOOR INTERNALLY OR EXTERNALLY. INSPECTED AND FOUND PAX DOOR ASSIST CABLE NOT RETRACING AND TANGLED INHIBITING DOOR FROM OPENING. REPLACED ASSIST MOTOR IAW 52-11-08. (M)

Part: PSU — DISLODGED (CABIN)

PSU IN ROW 6 AND 7 LEFT SIDE INOPERATIVE, FELL DOWN. CREW DECLARED EMERGENCY AND COMPLIED WITH EMERGENCY LANDING. REPLACED SILICONE CHORD ON ON LT PSU AT ROW 6 AND 7 IAW CRJ AMM 25-28-01. (M)

Part: AILERON — UNKNOWN (LT & RT) · airframe 13,844 hrs · 13,168 cycles

REQUEST INSPECTION OF RT AND LT AILERONS. THAWED ICE FROM AILERON, INSPECTED SURFACE MOVEMENT AND SURFACES. NO DEFECTS NOTED. (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

SMOKE CARGO MESSAGE AFTER PUSHBACK, GROUND INSPECTION OF CARGO HOLD. NO SMOKE FOUND. MEL`D NR 1 CARGO SMOKE DETECTOR. REMOVED AND REPLACED CARGO SMOKE DETECTOR. OPS CHECK GOOD IAW CRJ MM 26-15-00. REMOVED OFF MEL. S/N OFF 1719, S/N ON 2222. (M)

Part: CHECK VALVE — STICKING (RT ENGINE)

LOW OIL ENGINE PRESSURE WARNING IN FLIGHT (RED). INDICATED LOW ON GAUGE LOW PRESSURE, COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. REMOVED AND REPLACED ENGINE NR 2 GEARBOX BB CARBON SEAL AND MATING RING. ALSO, REMOVED AND REPLACED ENGINE NR 2 REPLENISHMENT CHECK VALVE. ALL UNITS LEAK CHECKED GOOD. (M)

Part: ENGINE — MALFUNCTIONED

LOW OIL ENGINE PRESSURE WARNING. INDICATED LOW ON GAGE LOW PRESSURE. COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. (M)

Part: STRUT — DISCHARGED (NLG)

AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. SERVICED HYDRAULIC FLUID AND NITORGEN TO THE NOSE STRUT. ADJUSTED THE NOSE OLEO CENTER EXTEND SENSOR WITHIN LIMITS. (M)

Part: ACM — ODOR (LEFT)

VERY STRONG ACRID SMELL COMING FROM AIR CONDITIONING PACKS. GOT WORSE WHEN TEMP CHANGES. REMOVED AND REPLACED LEFT ACM IAW AMM 21-51-10. (M)

Part: FRAME — CRACKED (FUSELAGE)

FRAME FLANGE BETWEEN STRINGER 11-12 HAS A CRACK COMING FROM A RIVET HOLE. TRIMMED OUT CRACKED PORTION OF FRAME FLANGE. PERFORMED LPI OF CUTLINE TO ENSURE NO CRACKS EXIST. FABRICATING REPAIR FLANGE FROM FRAME SECTOR PN 600-36030-23 INSTALLED IAW REO 601R-53-61-193 REV. A.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FLOOR ANGLE AT FS 484, RBL 27 RIGHT INBOARD IS CRACKED. REMOVED CRACKED RT INBOARD FLOOR ANGLE AT FS 484 WL 73.5 AND FABRICATED NEW ANGLE FROM S6144-14 AND INSTALLED IAW REPAIR NUMBER 601R-53-0029. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND FLOORBEAM ANGLES CRACKED AT FS 280, WL 73.50, LBL 9 AND RBL 9, FLOOR LEVEL. REMOVED OLD FLOOR SUPPORT ANGLES AT FS 280 WL 73.50 INBOARD SIDE OF LBL 9 AND RBL 9. INSTALLED NEW ANGLES PART NR RH 601R31113-58, LH 601R31113-57. ALL WORK IAW CRJ200 SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16, AND 51-42-06. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLES CRACKED AT FS 280, WL 73.5 LBL 9 AND RBL 9, BOTH INBOARD ANGLES. REMOVED LEFT ANGLE, P/N 601R31113-57 AND RT ANGLE P/N 601R31113-58 AND INSTALLED NEW SAME P/N ANGLES LEFT AND RT AND TREATED AND PAINTED. ALL WORK PERFORMED IAW SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16 AND 51-42-06. (M)

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY)

CARGO SMOKE WARNING, FIRE BOTTLES BLOWN, WHILE AIRCRAFT ON GROUND WITH CARGO AND PASSENGER DOOR OPENED. INSPECTED CARGO COMPARTMENT, NO HEAT OR SMOKE DAMAGE. COMPLIED WITH MAINTENANCE ACTION TASK 26-15-00-040-801. DEACTIVATED BOTH CARGO SMOKE DETECTORS. REMOVED AND REPLACED RIGHT FIREX BOTTLE, P/N 34600037-1, S/N OFF 14773F1, REMOVED AND REPLACED LEFT FIREX BOTTLES, P/N 36500018-3, S/N OFF 45875D1. (M)

Part: CONTROL UNIT — MALFUNCTIONED (ADH SENSOR)

TAT PROBE HEAT CAUTION ILLUMINATED INFLIGHT AFTER TAKEOFF. REPLACED AIR DATA HEAT SENSOR CONTROL UNIT. (M)

Part: A/C PACK — CONTAMINATED (AIR CONDITIONING)

SMOKE FROM LEFT PACK ON ROTATION UPON INVESTIGATION FOUND SMOKE TO BE FROM RESIDUAL DE-ICE FLUID. OPERATED ENGINE AT POWER WITH BLEEDS OPEN AND CLEARED COCKPIT AND CABIN FROM SMOKE. NO FURTHER DEFECTS AT THIS TIME. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

ONE LIGHTENING STRIKE DAMAGE AREA IN OPEN BAY AT FS 250 BETWEEN STRINGERS L25 AND L26. TRIMMED OUT DAMAGED AREA OF SKIN PANEL. COMPLIED WITH EDDY CURRENT INSPECTION OF CUT LINE FROM DAMAGE REMOVAL. NO INDICATION NOTED AT THIS TIME. FABRICATED FILLER. COMPLIED WITH WVAC RO 601R-53-3910. COMPLIED WITH STEP 15 OF WVAC EO 601R-53-3910. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

ONE LIGHTENING STRIKE DAMGED AREA IN OPEN BAY AT FS 265, BETWEEN STRINGERS L25 AND L26 TRIMMED OUT DAMAGED AREA OF SKIN PANEL. COMPLIED WITH EDDY CURRENT OF CUT LINE FROM DAMAGE REMOVAL. NO INDICATIONS NOTED AT THIS TIME. FABRICATED FILLER. COMPLIED WITH WVAC EO 601R-53-3909 STEPS 3 THROUGH 9 AND 11. OK TO INSTLAL. COMPLIED WITH STEPS 12. (M)

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)

RIGHT ENGINE INFLIGHT FLAMED OUT WITH RIGHT ENGINE OIL PRESSURE CAS MESSAGE ON ED1. REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT. NO DEFECTS NOTED. REPLACED FUEL FILTER, RIG CHECKED, TANKS SUMPED, NO DEFECTS. (M)

Part: WINDOW — CRACKED (LT COCKPIT)

DEN - AIRCRAFT WAS IN-FLIGHT EN ROUTE TO DEN WHEN PILOT NOTICED HIS SIDE WINDOW (LEFT) HAD CRACKED. AIRCRAFT PROCEEDED DEN WHERE THE WINDOW WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE ASSY — BROKEN (AIRSTAIR DOOR)

AIRSTAIR DOOR CABLE HAD BROKEN AT TERMINAL END DURING NORMAL SERVICE. AFTER REMOVAL OF OLD TERMINAL END IT WAS NOTED THAT THE INNER BEARING WAS EXCESSSIVELY TIGHT AND WOULD NOT ALLOW ROTATION. CABLE WAS REPLACED. (M)

Part: BRACKET — CRACKED (RT MLG)

DURING INSPECTION OF AIRCRAFT, FOUND A PROBABLE FRETTING CONDITION EXISTED AT THE RT MLG RETRACTION ACTUATOR SUPPORT BRACKET. THE BRACKET WAS REMOVED AND INSPECTED IAW AD CF91-25R2. A POSSIBLE CRACK INDICATION WAS VERIFIED BY MPI. IT SHOULD BE NOTED THAT THE BRACKET WAS POST MOD 8/1830 AND PRE MOD 8/2049 WHICH IS PART OF THE TERMINATING ACTION OF AD CF91-25R2. THE BRACKET WAS REPLACED PER MOD 8/2049 AND SB 8-54-27 ON FIELD AVIATION COMPANY WORK ORDER NR 21968.

Part: CONTROL CABLE — WORN (RT AILERON)

DURING INSPECTION, FOUND THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL POSITION. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21968 AT C-CHECK.

Part: AUTOFEATHER — MALFUNCTIONED (RT ENGINE)

DURING CRUISE AT 16,000 FEET WITH POWER AT APPROX 45 PERCENT TORQUE, CREW SELECTED AUTOFEATHER ARMED AND WHEN CONDITION LEVERS ADVANCED FROM MIN RPM TO MAX RPM TO RT ENGINE, EXPERIENCED AUTOFEATHER CONDITION. CREW SELECTED AUTOFEATHER OFF AND ENGINE RETURNED TO NORMAL PARAMETER. ACFT LANDED UNEVENTFULLY AT RAP. PERFORMED MAINTENANCE GROUND RUN IN RAP WITH AUTOFEATHER OFF. FERRIED AIRCRAFT TO GJT FOR INVESTIGATION. DOWNLOADED FDR AND FOUND ALL ENGINE PARAMETERS NORMAL FOR AUTOFEATHER OPERATION. PERFORMED GROUND RUN-UP AND OPS CHECK OF AUTOFEATHER SYSTEM. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE.