N412AW

Part: THERMAL SWITCH — FAILED (WING DEICE) · airframe 41,404 hrs · 39,264 cycles

DURING ARRIVAL AND ENTERING ICING CONDITION RECEIVED ANTI-ICE DUCT WARNING MESSAGE. DECLARED EMERGENCY AND DIVERTED TO SB. SYNOPTIC PAGE SHOWS LEADING EDGE LEFT WING RED, EVEN WITH ALL BLEED AIR TURNED OFF AND ON THE GROUND. C/W QRH. AIRCRAFT REMOVED FROM SERVICE. R & R LT WING ANTI-ICE DUCT THERMAL SWITCH S43WK, REF AMM 36-21 AND AMM SUP 11-031. OPERATIONS CHECK GOOD.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,402 hrs · 39,263 cycles

SEAT TRACK LOCATED ON RBL 9 FROM FS 394 TO FS 559+80 FOUND TO HAVE CORROSION OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, PER REO 601R-53-00-764.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,402 hrs · 39,263 cycles

FOUND CORROSION AT SEAT TRACK AT LBL 27 FS 559+88. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, PER REO 601R-53-00-764.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,402 hrs · 39,263 cycles

FOUND CORROSION ON SEAT TRACK FROM FS 364 TO 559+16. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK ON LBL 9 FROM FS 364 TO 559+16, PER SRM 51-42-02 AND REO 601R-53-00-764.

Part: WARNING MESSAGE — MULTIPLE FAIL (MLG) · airframe 39,099 hrs · 37,057 cycles

ON CLIMBOUT SELECTING GEAR UP, RECIEVED NOSE DOOR OPEN WARNING, GEAR DISAGREE WARNING, WOW INPUT CAUTION, STEERING INOP CAUTION, AND WOW OUTPUT FAIL STATUS, MESSAGES CLEARED AFTER LANDING. TAKEOFF WAS IN ICING CONDITIONS AND ALL HYDRAULICS NORMAL

Part: HINGE — UNSERVICEABLE (PAX DOOR) · airframe 39,040 hrs · 36,996 cycles

PAX DOOR HINGE ON FUSELAGE SIDE HAS FOUR GOUGED LUGS ON AFT END. REMOVED AND REPLACED PAX DOOR HINGE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,040 hrs · 36,996 cycles

RT FLOOR SILL FROM FS 589 TO FS 619 NUT PLATE LOCATIONS HAVE CORROSION. REPAIRED.

Part: PLUG — DEFECTIVE (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

RT FWD PRESSURE PANEL 132AL HAS 2 BAD FREEZE PLUGS. REPLACED.

Part: LANDING — CRACKED (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

LT TRU DOOR LAND CRACKED AT LATCH CUTOUT. REPLACED.

Part: SKIN — CHAFED (RT AILERON) · airframe 39,040 hrs · 36,996 cycles

RT AILERON LEADING EDGE UPPER SKIN CHAFFED. REPLACED.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 39,040 hrs · 36,996 cycles

FS193.00, LBL30 ELECTRICAL BAY FLOOR IS CRACKED AT INSIDE CORNER. REPAIRED FS193.00 LBL30 ELECTRICAL BAY FLOOR IAW REO 601R-53-11-111 REV -NC.

Part: BRACKET — CRACKED (BS 621) · airframe 39,040 hrs · 36,996 cycles

CARGO DOOR BEAM MEMBER BRACKET CRACKED ON 621 BULKHEAD. REPLACED CARGO DOOR BEAM MEMBER BRACKET IAW CRJ200 SRM 51-42-21.

Part: BEAM — CORRODED (BS 569-621) · corrosion level 2 · airframe 39,040 hrs · 36,996 cycles

DURING INCORPORATION OF E.O. E17/005/425 STEP 7, LBL FLOOR BEAM CAP CORRODED AT FS569.00-621.00, LBL27, WL73. REPLACED CAP IAW CRJ200 SRM 51-40-11, 51-42-21, 51-42-22.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 39,040 hrs · 36,996 cycles

LEFT MLG WHEEL WELL VOLUMETRIC FUSE TRANSDUCER BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 39,040 hrs · 36,996 cycles

RH FLAP IB LOWER SKIN HAS NUMEROUS SMALL GOUGES. REPLACED

Part: ATTACH BRACKET — CRACKED (BS 449.85) · airframe 39,040 hrs · 36,996 cycles

FS449.85 L/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 39,040 hrs · 36,996 cycles

FS461 L/H FAIRING ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 39,040 hrs · 36,996 cycles

FS461.00 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06,

Part: ATTACH BRACKET — CRACKED (BS 449.85) · airframe 39,040 hrs · 36,996 cycles

FS449.85 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 468) · airframe 39,040 hrs · 36,996 cycles

FS468 R/H FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06, 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,040 hrs · 36,996 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL36, WL78. BULKHEAD CRACK REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0043 SN:6781395.

Part: SKIN — DENTED (BS 700-718) · airframe 39,040 hrs · 36,996 cycles

EXTERIOR LOWER SKIN PANEL REPAIR DOUBLER FROM FS 700-718 STGR 23R TO 24R DENTED. REPAIRED

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,040 hrs · 36,996 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL27, WL 130, TAIL END OF CARGO DOOR TRACK. BULKHEAD CRACK REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0034 SN:67813 95.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,040 hrs · 36,996 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL27, WL 106. REPAIR ACCOMPLISHED ON AAR WORK ORDER 1016496-2000-0043 SN:6781395 ITEM #6.

Part: ATTACH ANGLE — CRACKED (WINDOW POST) · airframe 39,040 hrs · 36,996 cycles

FLIGHT DECK WINDSHIELD RIGHT O/B LOWER POST ATTACH CLIP IS CRACKED. REPLACED CLIP IAW CRJ 200 SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (WINDSHIELD) · airframe 39,040 hrs · 36,996 cycles

FLIGHT DECK LEFT WINDSHIELD POST O/B ATTACH CLIP CRACKED. REPLACED CLIP IAW CRJ200 SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

STR 14R OBLIQUE ANGLE IS CRACKED IN AEB. REPLACED STR14R OBLIQUE ANGLE IAW SRM 51-42-21, 51-25-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

STR 14L OBLIQUE ANGLE IS CRACKED IN THE AEB. REPLACED STR14L OBLIQUE ANGLE IAW SRM 51-42-21, 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

FS 193.00 LBL9 POST O/B CLIP CRACKED. REPLACES CLIP IAW CRJ200 SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,040 hrs · 36,996 cycles

FS193.00, RBL9 VERTICAL POST TOP O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 39,040 hrs · 36,996 cycles

RIGHT MLG WHEEL WELL Z ANGLE FWD OF TRANSDUCER BRACKET IS CRACKED. REPLACED Z BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 39,040 hrs · 36,996 cycles

RIGHT MLG WHEEL WELL VOLUMETRIC FUSE TRANSDUCER MOUNT IS CRACKED. REPLACED MOUNT IAW SRM 51-42-06.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 39,040 hrs · 36,996 cycles

PAX DOOR EDGE MEMBER CRACKED. REPAIRED EDGE MEMBER IAW REO 601R-52-11-279 REV-NC.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,277 hrs · 36,289 cycles

PAX DOOR AFT INNER SKIN DAMAGE. (DRAG ANGLE) REPAIRED PAX DOOR INNER SKIN (DRAG ANGLE) IAW REO601R-52-11-513 REV-B.

Part: WIRE HARNESS — DAMAGED (NLW WOW) · airframe 37,236 hrs · 35,150 cycles

INFLIGHT, RECIEVED NWS INOPERATIVE AND WOW INPUT CAS MESSAGES AND WOW OUTPUT STATUS MESSAGE, COMPLIED WITH QRH, MESSAGE PERSISTED. MESSAGES CLEARED WITH GEAR DOWN. REMOVED AND REPLACED THE NOSE LANDING GEAR WOW HARNESS NR 1 IAW 12-029D. OPS CHECKED GOOD.

Part: SKIN — PUNCTURED (BS 672.2-682) · airframe 37,101 hrs · 35,008 cycles

MAINTENANCE FOUND A PUNCTURE IN THE FUSELAGE SKIN BETWEEN FS672.20/FS682.00 AND STR1L/STR2L. DAMAGE MEASURES 1.0" X 0.4". CAN BE REPAIRED WITH A GENERIC SRM REPAIR.

Part: UNKNOWN — UNKNOWN (FLT CONTROL) · airframe 36,365 hrs · 34,320 cycles

UNCOMMANDED YAW DURING DECENT THRU 11,000 FT WITH AUTOPILOT ON AND WITH AUTOPILOT OFF ON APPROACH. YD CAUTION, HAD TO ENGAGE YD.

Part: SEAT TRACK — CORRODED (BS 569-621) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

IN AFT CARGO SEAT TRACK BEAM IS CORRODED BS 621-559+80 LBL 26

Part: FRAME — CRACKED (BS 605) · airframe 35,767 hrs · 33,779 cycles

STUB FRAME AT BS 605 CRACKED AT STRINGER 18L

Part: WEB — CRACKED (BS 589-605) · airframe 35,767 hrs · 33,779 cycles

WEB CRACKED ON INBD SIDE OF LBL 27 BETWEEN BS 589 AND 605.

Part: WEB — CRACKED (BS 574-589) · airframe 35,767 hrs · 33,779 cycles

WEB CRACKED ON INBD SIDE OF LBL 27 BETWEEN BS 574 AND 589.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

FRAME BS 605 IN CARGO BAY IS CORRODED BETWEEN STRINGERS 24R AND 24L

Part: ANGLE — CRACKED (BS 605) · airframe 35,767 hrs · 33,779 cycles

CARGO DOOR SILL TO STUB FRAME ANGLE CRACKED AT BS 605.

Part: WEB — CRACKED (BS 574-589) · airframe 35,767 hrs · 33,779 cycles

WEB CRACKED ON OTBD SIDE OF LBL 27 BETWEEN BS 574 AND 589.

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

SERVICE DOOR STEP PLATE IS CORRODED & BENT AT BOTTOM.

Part: WEB — CRACKED (BS 589-605) · airframe 35,767 hrs · 33,779 cycles

WEB CRACKED ON O/B SIDE OF LBL 27 BETWEEN BS 589 AND 605

Part: SKIN — DENTED (RT AILERON) · airframe 35,767 hrs · 33,779 cycles

RIGHT AILERON HAS A SMALL DENT IN UPPER SKIN.

Part: CARGO TRACK — CORRODED (BS 621-559) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

AFT CARGO TRACK IS CORRODED BS 621 - 559+80 AT LBL 10.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 35,767 hrs · 33,779 cycles

RIGHT INBD FLAP VANE LEADING EDGE IS CHAFED.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 35,767 hrs · 33,779 cycles

ATTACH ANGLE AT BS 625 STRINGER 13L IS CRACKED.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 35,767 hrs · 33,779 cycles

ATTACH ANGLE AT BS 625 STRINGER 14L IS CRACKED.

Part: ATTACH ANGLE — CORRODED (BS 310-319) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

SERVICE DOOR SILL FWD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,767 hrs · 33,779 cycles

FWD FLOORBEAM ANGLE AT BS 280 IS CRACKED NEAR RBL 9.

Part: SUPPORT FITTING — CRACKED (WINDOW POST) · airframe 35,767 hrs · 33,779 cycles

WINDSHIELD CENTER POST INTERNAL SIDE LOWER STRAP RT SUPPORT FITTING CRACKED. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-21.

Part: SUPPORT FITTING — CRACKED (WINDOW FRAME) · airframe 35,767 hrs · 33,779 cycles

WINDSHIELD CENTER POST INTERNAL SIDE LOWER STRAP LT SUPPORT FITTING CRACKED. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

FLOORBEAM BS 280 HAS CORROSION ON THE TOP SIDE BETWEEN LBL 9 AND RBL 9.

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

RIGHT MAIN CABIN SEAT TRACK CORRODED OUT OF LIMITS, BS 364 - 409, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

MAIN CABIN FLOOR SUPPORT ANGLE CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, AND 51-42-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 35,767 hrs · 33,779 cycles

RIGHT INBD FLAP LOWER SKIN HAS A DENT 1 1/2 INCHES FROM THE TRAILING EDGE AND 6 INCHES FROM THE INBD EDGE.

Part: BRACKET — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

PAX DOOR SILL FWD CLEAT BRACKET IS CORRODED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,767 hrs · 33,779 cycles

LBL 9, INBD ANGLE ON BS 280 FLOORBEAM IS CRACKED.

Part: BRACKET — CORRODED (PAX DOOR SILL) · corrosion level 2 · airframe 35,767 hrs · 33,779 cycles

PAX DOOR LOWER SILL AFT CLEAT BRACKET IS CORRODED.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 35,476 hrs · 33,510 cycles

EMERGENCY ROW LIGHTING BETWEEN ROW 5 AND 8 INOP. INSPECTED FLOOR TRACK LIGHTING AT ROW 5 TO 8 AND ADJUSTED CONNECTOR P39LY, AND OPS CHECK GOOD IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,331 hrs · 33,380 cycles

CREW REPORTED EMERGENCY FLOOR TRACK LIGHTS NOT WORKING FROM ROWS 5-8.

Part: SWITCH — OUT OF RIG (THRUST REVERSER) · airframe 34,089 hrs · 32,197 cycles

WHILE EN-ROUTE RECEIVED LT REVERSER UNLOCKED CAUTION. COMPLIED WITH QRH & DIVERTED. REVERSER APPEARS STOWED ON WALK AROUND. DEACTIVATED LT THRUST REVERSER IAW SUPP 15-046. COMPLIED WITH M ACTION. TROUBLE SHOT & FOUND LT THRUST REVERSER STOW SWITCH TO BE EXTREMELY FAR OUT OF RIG. RIGGED STOW SWITCH IAW AMM 78-30. OPERATIONS CHECKED GOOD. REACTIVATED LT THRUST REVERSER, REMOVED PLACARD & FROM MEL.

Part: TRIM SYSTEM — BINDING (ELEVATOR) · airframe 33,738 hrs · 31,875 cycles

WITH CAPTAIN FLYING PILOT , AUTOPILOT OFF DESCENDING THRU 1500 FT EXPERIENCED BINDING OF ELEVATOR DOWN PITCH. FREED MOVEMENT BY EXTENDING TRAVEL FARTHER FORCING YOKE FWD. BINDING CLEARED WITH A POP SOUND FROM THE FIRST OFFICERS SIDE YOKE AREA. ACFT WAS NOT DE-ICED BEFORE THE FLIGHT & WAS IN THE HANGAR ALL NIGHT PREVIOUSLY.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 32,757 hrs · 30,926 cycles

FLIGHT 3725, ELEC SMELL IN CABIN, MIDDLE TO FWD SECTION OF CABIN. R & R BALLAST BH4 IAW AMM 33-21. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WIRE — BROKEN (CABIN) · airframe 32,621 hrs · 30,791 cycles

FLIGHT 3901, 3992X2 XLD EMER FLOOR TRACK LIGHTING ROW 8 & AFT WN ILLUMINATE. REPAIRED BROKEN WIRES TO AFT SECTION OF EMER FLOOR TRACK LIGHTING IAW AMM 33-51-01 & ESPM 20-11-00. OPERATIONS CHECKED GOOD.

Part: DISPLAY — MALFUNCTIONED (MULTIPLE) · airframe 31,487 hrs · 29,714 cycles

DURING TAKEOFF ROLL, LOST ED1, ED2, FMS, RTU1, & RTU2 DISPLAY. CONTINUED DEPARTURE & AT APPROX FL 15000 ADJUSTING DISPLAY KNOB, DISPLAYS RETURNED. DECLARED AN EMERGENCY & RETURNED, LANDED APPROX 45,000 LBS.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

FS 409+128 LBL 27 STIFFENER HAS CRACK AT LOWER AFT INBD & OTBD CORNERS.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

FS 409+128 LBL 18 VERTICAL STIFFENER HAS CRACK ON LOWER AFT OTBD CORNER.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

LOWER CHANNEL ON RT MLG APRON STRUCTURE IS DAMAGED. DENTED & TORN BETWEEN FS 529 & 533.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,303 hrs · 29,533 cycles

RIGHT AILERON UPPER LE SKIN HAS CHAFING BETWEEN CTR OTBD HINGE.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

LOWER CHANNEL ON LT MLG APRON STRUCTURE DAMAGED. DENTED & TORN BETWEEN FS 529 & 533.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,303 hrs · 29,533 cycles

LBL 27 SEAT TRACK CORRODED AT APPROX FS 559+80.

Part: SEAL — CRACKED (THRUST REVERSER) · airframe 31,303 hrs · 29,533 cycles

RIGHT THRUST REVERSER SPRING SEAL CRACKED, NEAR 5 O'CLOCK POSITION.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 31,303 hrs · 29,533 cycles

LEFT MLG WW BATTERY RIB DRAG ANGLE IS CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 31,303 hrs · 29,533 cycles

RIGHT MLG WW BATTERY RIB DRAG ANGLE IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

LBL 36 FS 484 CLIP IS CRACKED ON UPPER END, OTBD CLIP.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,303 hrs · 29,533 cycles

LBL 9 BAGGAGE TIE DOWNS AT FS 583.00 ARE CORRODED & SEAT TRACK AT LBL 9 AT FS 615.00 IS CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

CLIPS AT STRINGER 4L & FS 280 ARE CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,303 hrs · 29,533 cycles

BAGGAGE COMPARTMENT SEAT TRACKS AT LBL 9 & RBL 9 AT FS 559+90 & FS 563 CORRODED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 31,303 hrs · 29,533 cycles

CRACK IN AFT LT CORNER ON NLG WW CUT OUT.

Part: CONNECTOR — DISCONNECTED (SMOKE DETECTOR) · airframe 31,170 hrs · 29,408 cycles

RECEIVED SMOKE CAUTION MSG IN FLIGHT WHILE PAX WAS IN LAVATORY. INSPECTED LAVATORY & FOUND NO EVIDENCE OF SMOKE IN LAVATORY. AFTER THOROUGH INSPECTION OF SINK & TOILET ELECTRICAL COMPONENTS. GAINED ACCESS TO LAVATORY SMOKE DETECTOR & FOUND CONNECTOR DISCONNECTED TO SMOKE DETECTOR. RECONNECTED CONNECTOR & OPERATIONS CHECKED IAW AMM 26-13-01. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 30,767 hrs · 29,025 cycles

EMERGENCY LIGHT FLOOR TRACK AT BULKHEAD ROW 1 MISSING ORANGE OVERLAY.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,903 hrs · 28,209 cycles

REQUEST INSP OF BURNING RUBBER SMELL MORE NOTICEABLE NEAR PAX DOOR. PERFORMED OPERATIONS TEST OF GALLEY HEATER SYS IAW AMM 21-23-05, INSPECTED TIRES FOR ABNORMAL WEAR IAW AWAC SUP 08-005C. PERFORMED OPERATIONS CHECK OF AIR CONDITIONING SYS IAW AMM 21-51-00, PERFORMED OPERATIONS CHECK OF AC GENERATION SYS IAW AMM 24-20-00, INSPECTED AVIONICS BAY, NO DEFECTS NOTED. PERFORMED OPERATIONS CHECK OF GCU'S IAW AMM 24-11-01. PERFORMED OPS CHECK OF CABIN & GALLEY LIGHTING SYS IAW AMM 33-21-00. ALL SYSTEMS CHECKED GOOD, NO DEFECTS NOTED. COULD NOT REPRODUCE RUBBER BURNING SMELL.

Part: AILERON SYS — MALFUNCTIONED · airframe 28,006 hrs · 26,371 cycles

ON APROACH, UNCOMMANDED AILERON MOVEMENT AND ROLL. AILERON MOVEMENT OBSERVED ON FLT CONTROL SYNOPTIC SAW LT MOVE NOT SURE ABOUT RIGHT AUTOPILOT OFF AT THE TIME. APROX 2 MIN PRIOR TO LDG. OPEN

Part: YAW DAMPER — FAULTY (AUTOPILOT SYS) · airframe 26,679 hrs · 25,108 cycles

DURING CRUISE FLT WITH A/P ON A/C YAWED SUDDENLY BOTH RT & LT YAWING MOVEMENTS LESSENED AT SPEEDS 250 KIAS OR LESS. YAWING MOVEMENTS WOULD LAST APPROXIMATELY 1-2 MINUTES THAN SUBSIDE FOR 10 MINUTES AND THAN BEGIN AGAIN. REMOVED AND REPLACED LEFT & RIGHT YAW DAMPER ACTUATORS IAW AMM 22-22-01, OPS CHECK GOOD.

Part: STRUCTURE — CHAFED (LT NACELLE) · airframe 26,646 hrs · 25,075 cycles

CHAFE ON LEFT ENGINE UPPER CORE COWL FWD AT 11 O`CLOCK POSITION. REMOVED & REPLACED REBATE DISH WITH SERVICEABLE IAW SRM 51-22-00.

Part: BRACKET — CRACKED (RT MLG TRUNNION) · airframe 26,646 hrs · 25,075 cycles

SUPPORT BRACKET ON RIGHT MLG AFT TRUNNION I/B SIDE IS CRACKED. REPLACED WITH NEW SERVICEABLE SUPPORT BRACKET P/N 601R10205-30 IAW CRJ SRM 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,646 hrs · 25,075 cycles

CORROSION ON FRAME 333 STR 26L TO 25R & AROUND GROUND LOCATIONS. REMOVED AND REPLACED FRAME SECTION (601R32004-55) IAW REO 601R-53-21-2400.

Part: SKIN — CHAFED (LT WING LE FLAP) · airframe 26,646 hrs · 25,075 cycles

LEFT I/B FLAP VANE LEADING EDGE CHAFED BY I/B & O/B PADS. REMOVED AND REPLACED I/B SKIN IAW SRM 51-40-11 & 51-42-13. O/B POSITION LIMITS PER GREO 601R-57-52-004 REV D.

Part: BRACKET — CHAFED (LT WING TE FLAP) · airframe 26,646 hrs · 25,075 cycles

LEFT WING TE FLAP VANE MOUNTING BRACKET IS CHAFED AND ON IN FRONT THE I/B EDGE. REMOVED CHAFED DAMAGE BY EDGE BLENDING.

Part: BEAM — GOUGED (LT WING TE FLAP) · airframe 26,646 hrs · 25,075 cycles

LEFT I/B FLAP VANE SLIDING BEAMS ARE GOUGED UNDER UPPER AD LOWER ROLLERS. REPAIRED PER REO 601R-57-52-1979.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,646 hrs · 25,075 cycles

SERVICE DOOR THRESHOLD CORRODED. REMOVED AND REPLACED THRESHOLD P/N: 601R38957-31.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 26,646 hrs · 25,075 cycles

CARGO DOOR LOWER SILL HAS NUT PLATES CORRODED WITH CORROSION. REPAIR CORROSION ON CARGO DOOR LOWER SILL IAW REO 601R-53-61-690 REV D AND SRMS 51-21-06, 51-24-21, 51-40-11.

Part: SKIN — GOUGED (TE FLAP) · airframe 26,646 hrs · 25,075 cycles

GOUGE ON I/B LOWER SKIN ON RIGHT I/B FLAP. REMOVED & REPLACED SKIN IAW CRJ 200 SRM 57-52-00 REPAIR 3 FIG 202 SHEET 2.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 26,646 hrs · 25,075 cycles

LEFT AND RIGHT MLG TRUNNION FOUND WEB TO HAVE TOOL MARKS. REPAIRED TRUNNION PER REO 601R-57-21-1855.

Part: STRUCTURE — DAMAGED (RT NACELLE) · airframe 26,646 hrs · 25,075 cycles

ELONGATED HOLES ON RIGHT ENGINE LOWER CORE COWL ALIGNMENT PIN HOLES. REPAIRED IAW CMM 71-12-01 REPAIR SRS109.

Part: BRACKET — BROKEN (LT WING TE FLAP) · airframe 26,646 hrs · 25,075 cycles

LEFT O/B FLAP O/B HINGE ARM HAS BROKEN MOUNT BRACKET FOR PANEL 597BB ON O/B SIDE. REMOVED AND REPLACED MOUNT BRACKET FOR PANEL 597BB.K.

Part: VANE — CHAFED (TE FLAP) · airframe 26,646 hrs · 25,075 cycles

RIGHT I/B FLAP VANE LEADING EDGE I/B, CTR & O/B AREA CHAFED FROM STOPS. REMOVED AND REPLACED I/B LEADING EDGE & BLENDED & TREATED CTR & O/B LEADING EDGE IAW REO 601R-57-52-004.

Part: BRACKET — CRACKED (BS 169-193) · airframe 26,646 hrs · 25,075 cycles

IN THE NOSE HYD COMPARTMENT, UPPER ACCUMULATOR FWD UPPER MOUNT BRACKET IS CRACKED. REMOVED UNSERVICEABLE ACCUMULATOR FWD UPPER MOUNT BRACKET AND REPLACED WITH SERVICEABLE BRACKET IAW SRM 51-42-06 AND 51-42-21.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 26,646 hrs · 25,075 cycles

RIGHT INBD FLAP VANE HAS FOUR CHAFE SPOTS. NOT BUMP STOPS. BLENDED CHAFE SPOTS IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.

Part: SEAL — CRACKED (RT SPOILER) · airframe 26,646 hrs · 25,075 cycles

RIGHT FLIGHT SPOILER OUTBD SEAL CRACKED AND BROKEN BY OUTBD SPOILER HINGE. REMOVED UNSERVCIEABLE SEAL ON RIGHT FLIGHT SPOILER O/B AND REPLACED WITH SERVICEABLE SEAL RIGHT P/N 601R10226-130 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: FITTING — CHAFED (TE FLAP) · airframe 26,646 hrs · 25,075 cycles

RIGHT OTBD FLAP ROLLER GUIDE ALIGNMENT FITTING IS CHAFED. BLENDED CHAFE PER CRJ 200 SRM 51-12-00 DEPTH WAS .008 WITHIN LIMITS IAW REO 601R-57-51-143.

Part: FITTING — CHAFED (TE FLAP) · airframe 26,646 hrs · 25,075 cycles

RIGHT OTBD FLAP ROLLER GUIDE FITTING IS CHAFED. BLENDED CHAFE ON CRJ 200 SRM 51-12-00 DEPTH OF CHAFE WAS .014 WITHIN LIMITS IAW REO 601R-57-53-039.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 26,646 hrs · 25,075 cycles

PAX DOOR POWER ASSIST MOTOR UPPER ATTACH ANGLE CRACKED IN RADIUS. REMOVED AND REPLACED ANGLE P/N 601R317745-7.

Part: ANGLE — CRACKED (BS 280) · airframe 26,646 hrs · 25,075 cycles

CRACKED ANGLE AT FS 280 RBL 9 INBRD. REMOVED & REPLACED ANGLE IAW SRM 51-42-21 & 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,646 hrs · 25,075 cycles

CRACKED CLIP FS 280 RBL 9 O/B. REMOVED AND REPLACED RBL 9 O/B CLIP AT FS 280 IAW CRJ 200 SRM 51-42-21 & 51-40-11.

Part: FRAME — DAMAGED (BS 223) · airframe 26,646 hrs · 25,075 cycles

TWO FASTENER HOLES AROUND 132AL ACCESS HOLE ARE OBLONG. REPAIR PER REO 601R-53-11-162.

Part: BULKHEAD — GOUGED (BS 280) · airframe 26,646 hrs · 25,075 cycles

AFT SIDE OF BULKHEAD FS 280 GOUGED. REPAIRED AFT SIDE FS 280 BULKHEAD IAW REO 601R-53-11-1727 REV F.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 25,948 hrs · 24,393 cycles

DURING CRUISE HEARD CRACKING SOUND AND FLASH OF LIGHT BEHIND CBP1 LEFT WINDSHEILD HEAT AND LEFT WINDOW HEAT CAUTION MSG. REMOVED AND REPLACED AIHC WINDSHEILD CONTROLLER IAW AMM 30-41-01, OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED · airframe 22,994 hrs · 21,395 cycles

FLIAPS DEGRAGED, WHITE STATUS MESSAGE APPEARED. C/W FIM FAULT RESET PROCEDURE MESSAGE CLEARED.

Part: COMPUTER — MALFUNCTIONED (RT AHRS) · airframe 22,120 hrs · 20,487 cycles

EFIS COMP MON ROLL AND PITCH, F/O PFD WENT SIDEWAYS AND A/P KICKED OFF. ACFT RETURN TO DEPARTURE, NORMAL LANDING AND NORMAL BRAKING=WD 4460. R & R NR 2 AHRS COMPUTER IAW AMM 34-21-01. OPS CK GOOD.

Part: COWLING — CHAFED (RT NACELLE) · airframe 21,808 hrs · 20,184 cycles

LT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED LT LOWER CORE COWL IAW CMM 228-50142 TASK 71-12-01-300-822 AOL.

Part: COWLING — CHAFED (RT NACELLE) · airframe 21,808 hrs · 20,184 cycles

RT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED RT LOWER CORE COWL IAW CMM 228-50142, TASK 71-12-01-300-822-A01.

Part: PANEL — DAMAGED (BS 220) · airframe 21,808 hrs · 20,184 cycles

PANEL 132AL HAS DRILL STARTS AT SCREW HOLES. LOCATED HOLES IN FWD RT PRESSURE PANEL IAW SRM 51-40-11.

Part: NUT PLATE — MISSING (LT AILERON) · airframe 21,808 hrs · 20,184 cycles

LT AILERON CTR BRACKET HAS MISSING NUTPLATE AND NUTPLATE HOLE IS DAMAGED. R & R LT AILERON CTR BRACKET IAW REO 601R-57-61-320.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 21,808 hrs · 20,184 cycles

UPPER OTBD CASCADE ON RT THRUST REVERSER CRACKED. REPAIRED RT T/R UPPER OTBD CASCADE IAW PROCESS SPEC 1 DWG AW-78-30-0711-04.

Part: SKIN — GOUGED (FUSELAGE) · airframe 21,808 hrs · 20,184 cycles

CARGO BAY DOOR CUTOUT AFT LOWER CORNER DENTED. REPAIRED DAMAGED AREA IAW REO 601R-53-61-3965.

Part: ACCESS PANEL — CRACKED (APU BAY) · airframe 21,808 hrs · 20,184 cycles

APU ENCLOSURE COVER DOOR ACCESS PANEL HAS CRACK IN CORNER EXTENDING FROM WELD. REPAIRED APU ENCLOSURE DOOR 311B2 IAW REO 601R-49-11-070, REB B.

Part: ANGLE — CRACKED (BS 625) · airframe 21,808 hrs · 20,184 cycles

CLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. TEST RT SIDE, R & R CLIP ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 625) · airframe 21,808 hrs · 20,184 cycles

CLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD, LT SIDE. R & R CLIP IAW SRM 51-42-06 & SRM 51-42-21.

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 21,808 hrs · 20,184 cycles

PAX DOOR SILL HAS CORROSION AS MARKED. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR SILL IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CRACKED (BS 559-565) · airframe 21,808 hrs · 20,184 cycles

CARGO BAY DOOR SEAL PLATE HAS CLIP CRACKED. REMOVED UNSERVICEABLE CARGO DOOR SEAL PLATE CLIP IAW SRM 51-40-11. INSTALLED SERVICEABLE CARGO DOOR SEAL PLATE CLIP SRM 51-40-11.

Part: SKIN — CHAFED (RT AILERON) · airframe 21,808 hrs · 20,184 cycles

RT AILERON L/E BUTTON SKIN CHAFE DAMAGE OTBD DEEP, RT AILERON L/E TOP SKIN CHAFE DAMAGE .006 DEEP. BLENDED CHAFE DAMAGE FROM BOTTOM SKIN BLENDED TOP SKIN WITHIN LIMITS, IAW REO 600R-57-60-020 IODIZED, PRIMED AND TOP COAT IAW SRM 51-25-16, 51-25-06.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,808 hrs · 20,184 cycles

FS 484 CRACKED CLIP AT LBL 36 INBD. R & R FS484, LBL36 CLIP IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,808 hrs · 20,184 cycles

FS 484 HAS CRACKED CLIP AT RBL 27 OTBD. R & R CLIP AT FS 484, RBL 27 IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,808 hrs · 20,184 cycles

FS 484 HAS CRACKED CLIP AT LBL 27 OB. R & R FS 484, LBL27 CLIP IAW REO 601R-53-41-059.

Part: RETAINER — CRACKED (LT NACELLE) · airframe 21,808 hrs · 20,184 cycles

BT HAS CRACKED SEAL RETAINER. R & R SEAL AND SEAL RETAINER IAW SRM 51-42-06.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 21,808 hrs · 20,184 cycles

FWD LWR TRACK OF CARGO BAY DOOR HAS CRACKED BRACKET. R & R BRACKET IAW SRM 51-42-06.

Part: ATTACH FITTING — WORN (LT PYLON) · airframe 21,808 hrs · 20,184 cycles

100 PERCENT MATERIAL LOSS WORN ALL THE WAY THROUGH FWD DIVIDER CLIP ON PANEL 412BF. DAMAGE R & R WITH NEW CLIP.

Part: SEAL — CHAFED (RT NOSE COWL) · airframe 21,808 hrs · 20,184 cycles

RT ENG UPPER NOSE COWL EDGE SEAL CHAFED. R & R EXISTING SPLICE IAW CMM 71-14-01.

Part: ATTACH FITTING — WORN (RT PYLON) · airframe 21,808 hrs · 20,184 cycles

FWD AND AFT DIVIDER CLIP ARE DAMAGED ON PANEL 422BT. R & R WITH NEW FWD AND AFT DIVIDER CLIPS.

Part: SKIN — GOUGED (RT NACELLE) · airframe 21,808 hrs · 20,184 cycles

RT LOWER COR COWL HAS (6EA) GOUGES IN NON FIRE SHIELD AREA (FWD INNERSKIN) BLENDED OUT (2EA) GOUGES IAW CMM 71-12-01. REPAIRED (2EA) GOUGES WHILE WAS OUT OF LIMITS IAW CMM 71-12-01-200-802-A01 (1EA) DENT WAS WITHIN LIMITS.

Part: SKIN — GOUGED (LT NACELLE) · airframe 21,808 hrs · 20,484 cycles

LT LOWER CORE COWL HAS (5EA) GOUGES IN NON FIRE SHIELD AREAS (FWD INNERSKIN) BLENDED (2EA) GOUGES AND REPAIRED (2EA) GOUGES IAW CMM 71-12-01 (1 DENT) FOUND TO BE WITHIN LIMITS IAW CMM 71-12-01-200-802-401.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,808 hrs · 20,184 cycles

LT MLG DOOR L/E CHOPPED. FABRICATED AND INSTALLED FILLER IAW REO 601R-52-82-034.

Part: SKIN — CHAFED (MLG DOOR) · airframe 21,808 hrs · 20,184 cycles

MLG DOOR INNER SKIN CHAFING R & R PREVIOUS FILLER IAW REO 601R-52-82-034.

Part: FRAME — CRACKED (BS 559) · airframe 20,345 hrs · 18,670 cycles

FS 559, RBL 9 HAS CRACK FROM BOTTOM OF LOWEST RIVET INCORPORATED REO 601R-53-41-260 REV D DATED 09/17/09 AND REO 601R-53-41-116, DATE 01/19/10.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 20,345 hrs · 18,670 cycles

FS 621 BULKHEAD HAS 3 CRACKED ISOLATORS. R & R WITH SERVICEABLE 3 EA ISOLATORS PN SL2337-3, PO 961376 AT FS 621 BULKHEAD ALL WORN DOWN IAW SRM 51-42-06, 51-42-06, 51-25-06.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,722 hrs · 18,029 cycles

FLAPS 45 DEGREES NORMAL APPROACH AIRSPEED (145 KNTS) ACFT REQUIRES ABOUT .5 INCH LT AILERON TRIM TO MAINTAIN LEVEL FLIGHT. ON CLIMB OUT ZERO FLAPS, NORMAL TRIM.

Part: UPLOCK ACTUATOR — FAILED (MLG) · airframe 17,844 hrs · 16,195 cycles

191172/3 - GEAR DISAGREE - WARNING ILLUMINATED APPROX 6-10 SECONDS AFTER RETRACTION SELECTION. LT MLG DID NOT RETRACT. COMPLIED WITH QRH. GEAR EXTENDED AND LOCKED NORMALLY. INSP LT MLG. FOUND NO VISUAL EVIDENCE OF HYD LK OF MECHANICAL FAILURE. INSTALLED GEAR PINS IAW AMM 10-11-00-400-801 AND 10-11-00-400-802. 191172/4 - REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR IAW AMM 32-32-05. PERFORMED LEAK CHECK AND GEAR RETRACTION AND EXTENSION SEVERAL TIMES. LEAK AND OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. (K)

Part: UPLOCK — INOPERATIVE (MLG) · airframe 17,822 hrs · 16,175 cycles

GEAR DISAGREE AFTER TAKEOFF, RED DASHES ON LT MAIN GEAR INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ASSY IAW AMM 32-32-05. OPS AND LEAK CHECK GOOD. REMOVED PLACARD, REMOVED FROM MEL. RII I-160. (K)

Part: LANDING GEAR — MALFUNCTIONED · airframe 17,776 hrs · 16,132 cycles

"GEAR DISAGREE WARNING MESSAGE APPEARED APPROX 5-10 SECONDS AFTER COMMANDED NOSE AND RT MLG INDICATED "RED" , LT MLG SHOWED "YELLOW". QRH COMPLIED WITH GEAR EXTENDED NORMALLY. C/W MX ACTION FOR MEL 32-20-01. INSTALLED NLG SAFETY AND BOTH MLG PNS IAW AMM 10-11-00-400-801 AND 802. UNABLE TO DUPLICATE CONDITION, FOUND NOSE AND LT MAIN UPLOCK PINS SEIZED, LUBED AND FREED UP LOCK PINS, RETRACTED AND EXTENDED GEAR 25 TIMES NO FAULTS FOUND IAW AMM 12-20-32 AMD MXC INPUT, REMOVED PLACARD. (K)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 17,595 hrs · 15,953 cycles

HYD LOW PRESSURE CAUTION INFLIGHT, COMPLIED WITH QRH WITH APPROX 17 MIN REMAINING IN FLIGHT. INSP AND FOUND NR 2 HYD SYS RESERVOIR SUCTION LINE LEAKING. REPAIRED HYD LINE WITH NEW FITTINGS IAW AMM 20-22-00. BLED NR HYD SYS OPS AND LEAK CHECK NORMAL IAW AMM 29-11-00. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,102 hrs · 15,503 cycles

INBD AND OTBD CLIPS AT FS 280 AND JUNCTION OF RT FLOORBEAM 9.0 ARE CRACKED. INBD AND OTBD CLIPS AT FS 280 REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)

Part: SKIN — DENTED (LT WING) · airframe 17,102 hrs · 15,503 cycles

MWC 131269/1 - 4DMI13275 REPAIR LT WING OTBD L/E AS REQUIRED DENT EXISTS IN L/E SKIN. 6.00 INCH L X 3.50 INCH W X .103 INCH DEEP. REO 601R-57-41-490 AND 601R-57-41-490 REV A LT WING OTBD L/E SKIN REPLACED IAW SRM 51-42-06 AND REO 601R-57-41-161, REV B AND DWG 601R12310. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,102 hrs · 15,503 cycles

PILOTS BULKHEAD FS 280 LBL 9 RBL 9 AFT ANGLE CRACKED. PILOTS BULKHEAD AT FS 280 AFT ANGLE REPAIRED IAW REO 601R-53-11-136 REV A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,102 hrs · 15,503 cycles

CRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 AT THE PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 REPAIRED IAW REO 53-11-1571.

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,102 hrs · 15,503 cycles

PILOTS BULKHEAD CRACKED AT FS 280.00 RBL 9 AND LBL 9. PILOTS BULKHEAD AT FS 280.00 RBL 9 AND LBL 9 REPAIRED IAW REO 601R-53-11-171 REV D,

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,102 hrs · 15,503 cycles

131226-222, SURFACE CORRODED ON LT WING PLANK FUEL ACCESS HOLES AT PANEL 540AB, 540EB, 550BB, 550DB AND 550FB. REO 601R-57-21-030, REV G. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,102 hrs · 15,503 cycles

131266221, SURFACE CORRODED ON RT WING PLANK FUEL ACCESS HOLE AT PANEL 610AB, 640CB AND 650GB, REO 601R-57-21-030, REV G. (K)

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,102 hrs · 15,503 cycles

131267-57 PAX DOOR AFT SECTION FS 338.80, CRACK FOUND ON ANGLE BETWEEN STAIRS AND DOOR FRAME LINE WITH THE POWER ASSIST MOTOR. PAX DOOR AFT SECTION DRAG ANGLE AT FS 338.80. REPAIRED IAW REO 601R-52-11-513 REV A. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,567 hrs · 15,002 cycles

AFT PRESSURE BLKHD WEB AT FS 621.00 AT THE LINTEL INSTALLATION AREA IS CRACKED. REPAIRED IAW REO 601R53-61-1230 REV D.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE SYS) · airframe 15,096 hrs · 13,607 cycles

AFTER TAKEOFF RECEIED ANTI-ICE DUCT WARNING MESSAGE. COMPLIED WITH QRH, MESSGE PERSISTED ON SYNOPTIC PAGE, SHOWS LT WING RED. (M)

Part: ELEMENT — MALFUNCTIONED (LT ANTI ICE SYS) · airframe 15,032 hrs · 13,540 cycles

FOUND LT WING ANTI-ICE DUCT WARNING MESSAGE. REMOVED AND REPLACED HEAT SENSE ELEMENT A41WK REF AMM 36-21-04, OPS CHECK GOOD. (M)

Part: CABLE — INOPERATIVE (PAX DOOR) · airframe 14,432 hrs · 12,969 cycles

LOUD WHISTLING NOISE COMING FROM MAIN CABIN DOOR, LOUDEST JUST AFTER TAKEOFF. REMOVED AND REPLACED ICE BREAK CABLE IN PRESSURE RELIEF DOOR. REF AMM 52-11-15, OPS TEST GOOD. (K)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,397 hrs · 12,936 cycles

ENTRY-WAY EMERGENCY FLOODLIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER ASSY NR 2 IAW 33-51-05, OPS CHECK GOOD. (K)

Part: CONTROLLER — MALFUNCTIONED (NR 1 HEAT) · airframe 12,582 hrs · 11,162 cycles

PITOT BASE HEAT CAUTION MESSAGE CAME ON AFTER TAKEOFF. QRH COMPLIED WITH, UPON LANDING TAT PROBE HEAT, LT STATIC HEAT, LT AOA HEAT, RT STATIC HEAT, AND RT AOA HEAT CAUTION MESSAGE ALL CAME ON. REMOVED AND REPLACED ADS NR1 HEAT CONTROLLER IAW AMM 30-13-15 AND PERFORMED OPS CHECK OF HEAT CONTROLLER 32 IAW AMM 30-31-15. ALL OPS CHECKS GOOD. (K)

Part: BULKHEAD — CRACKED (BS 202)

FOUND LEFT SIDE FORWARD FACE OF FORWARD PRESSURE BULKHEAD FS 202.75 CRACKED APPROX .2 INCH LONG AT HYDRAULIC SYSTEM NR 3 RT INBOARD BRAKE FITTING. MAINTENANCE REPAIRED CRACKED AREA IAW BOMBARDIER SERVICES CORP EO 601R-53-10650. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FS 621 FLOOR SUPPORT ANGLE IAW BOMARDIER REO 601R-53-61-117. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND RIGHT ANGLE AT FS 484 RBL 27 CRACKED APPROXIMATELY .25 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-06 AND 51-42-21. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

RIGHT INTERCOSTAL AT FS 484 RBL 36 CRACKED APPROXIMATELY .3 INCHES LONG MAINTENANCE CUT AWAY DAMAGED SECTION OF INTERCOSTAL FLANGE, PERFORMED EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: FLOOR SUPPORT — CRACKED (BS 460)

FOUND FS 460 FLOOR SUPPORT FITTING CRACKED OUTBOARD SIDE OF RBL 9, APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED FITTING P/N 600-31068-19 AT FS 460.0 RBL 9,0 IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND LEFT INTERCOSTAL AT FS 484 LBL 36 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF INTERCOSTAL FLANGE, PERFORM EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FLOOR SUPPORT IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

FOUND LEFT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-57 CRACKED APPROX .2 INCH LONG INBOARD SIDE LBL 9.0. MAINTENANCE REMOVED AND CRACKED ANGLE, FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD REPAIR 601R-53-0057A. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND LEFT ANGLE AT FS 484 LBL 27 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-06, 51-40-11 AND 51-42-21. (M)

Part: NUT CLIP — CRACKED (FS 280)

RIGHT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-58 CRACKED APPROX .3 INCHES LONG INBOARD SIDE RBL 9.0. MAINTENANCE REMOVED CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD REPAIR 601R-53-0057A. (M)

Part: FLOORBEAM — CRACKED (FS 280)

FOUND LEFT FS 280 FLOOR SUPPORT CLIP, P/N 601R31113-57 CRACKED APPROX .1 INCH LONG OUTBOARD SIDE LBL 9.0. REMOVED CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-13-51-40-11, 51-42-21 AND BSC STANDARD REPAIR 601R-53-0057A. (M)

Part: BRACKET — CRACKED (RT MLG BAY)

HYDRAULIC TRANSDUCER HOT CHANNEL IN RIGHT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-157. MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET. DRILLED UP AND INSTALLED NEW BRACKET P/N 601R-75262-15T WET USING PR1422B SEALANT AN MS20470AD5-6 SOLID RIVETS, PRIMED, PAINTED DINOTROLED REPAIR AREA IAW CRJ 200 SRM. (M)

Part: BRACKET — CRACKED (LT MLG WW) · airframe 12,127 hrs

HYDRAULIC TRANSDUCER HOT CHANNEL IN LEFT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-159. MAINTENANCE DRILLED OFF REMOVED CRACKED BRACKET, DRILLED UP AND INSTALLED NEW BRACKET P/N 601R75262-159 WET USING PR1422B SEALANT AND MS 20470AD5-6 SOLID RIVETS, PRIME, PAINTED DINOTROLED REPAIR AREA IAW CRJ 200 SRM 51-42-06. (M)

Part: IDG — FAILED (NR 2 ENGINE)

IDG CAUTION MESSAGE AT APPROXIMATELY 30 KNOTS ON TAKEOFF ROLL, ABORTED TAKEOFF. REMOVD AND REPLACED IDG NR 2. (M)

Part: DOOR — DAMAGED (MAIN PAX)

MAIN PAX DOOR DROPS 1 FOOT PRIOR TO GROUND. SOME STRUCTURAL DAMAGE INCURRED ON PAX DOOR AS A RESULT OF COMPONENT FAILURE. MAINTENANCE REPAIRED PAX DOOR IAW AMM 52-11-17-400-802, BOMBARDIER REO 601R-52-11-702, BSC EO 601R-52-9149, BSC EO 601R-52-91-46A, SRM 51-42-06, BSC EO 601R-52-9147A, AND AMM 52-11-08-710-802. (M)

Part: APU — FLAMED OUT · airframe 8,063 hrs · 6,930 cycles

APU AUTOSHUT AND GRD CREW ADVISED FLAME COME OUT OF INTAKE. LOUD BANG WHEN SHUTDOWN. DISCHARGED BOTTLES. INSP APU AREA, NO EVIDENCE OF FIRE, C/W (M) ACTION IAW MEL. (K)

Part: AILERON — OUT OF RIG (RT AILERON TRIM) · airframe 8,524 hrs · 7,406 cycles

WITH AILERON TRIM CENTERED, AIRCRAFT HAS A STRONG ROLL TO THE RT. WITH LARGE AMOUNT OF LT WING DOWN TRIM, THE AIRCRAFT CAN BE MADE TO FLY LEVEL. AUTO-PILOT WAS OFF. FOUND RT AILERON SLIGHTLY OUT OF RIG. RE-RIGGED RT AILERON IAW AMM. (K)

Part: DOUBLER — MISMANUFACTURED (RT WING) · airframe 7,402 hrs · 6,384 cycles

WHILE PERFORMING SB 601R57037 (WING SPAR MOD) IT WAS DISCOVERED THAT THE JOINT STRAP ON THE RT WING LACKS PROPER LENGTH FOR EDGE DISTANCE. COMPLIED WITH BRAS EO 601R575944A, BY FABRICATING DOUBLER FROM 2024T3, .050 INCH AND USING TO EXTEND CUTLINES TO OBTAIN EDGE DISTANCE FOR JOINT STRAP. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PAX DOOR AFT DRAG ANGLE IS CRACKED 3 INCHES LONG JUST FORWARD OF PAX DOOR ASSIST PULLEY MOUNT BRACKET. REPAIRED ANGLE IAW BRAS EO 601R-52-5929 AND BOMBARDIER, INC REO 601R-52-11-513. (M)

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH)

CREW ESCAPE HATCH OUTER HANDLE WILL NOT RELEASE. LUBRICATED HANDLE IAW CRJ 200 AMM 12-20-52-640-803. PERFORMED CHECK IAW CRJ 200 AMM 52-22-00-710-801. (M)

Part: PANEL — CORRODED (RT WING)

RT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL PANELS 640BB AND 650HB. REMOVED MINOR CORROSION FROM RIGHT WING LOWER PLANK AT FUEL TANK ACCESS PANELS 340BB AND 650 HB IAW BOMBARDIER, INC REO 601R-57-21-030 REV C. (M)

Part: ACCESS PANEL — CORRODED (LT WING)

LT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL TANK PANELS 550BB, 540ED, 540BB, 510AB. REMOVED MINOR CORROSION FROM LT WING LOWER PLANK AT FUEL ACCESS PANELS 550BB, 540FB, 540EB, 540BB AND 510AB IAW MFG REO 601R-57-21-030 REV C. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,402 hrs · 6,384 cycles

LT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. (K) REMOVED AND REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,402 hrs · 6,384 cycles

RT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. FABRICATED INTERCOSTAL FROM S6144-3 7075 T62-050 INSTALLED IAW CRJ-200 SRM 51-42-06. (M) (K)

Part: RIB — CRACKED (LT WING) · airframe 7,402 hrs · 6,384 cycles

LT WING STATION 53.6 BUTT RIB IS CRACKED, 1 INCH LONG IN UPPER AFT RADIUS. REPAIRED LT WING STATION 53.60, BATT RIB IAW MFG REPAIR EO 601R-57-51-046, REV B.

Part: RIB — CRACKED (RT WING) · airframe 7,402 hrs · 6,384 cycles

MWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B.

Part: FIRE BOTTLE — LOW (AFT CARGO BAY) · airframe 7,365 hrs · 6,358 cycles

LT ENGINE SQUIB LIGHT WILL NOT ILLUMINATE. FOUND LT ENGINE FIRE BOTTLE LOW PRESSURE. REMOVED AND REPLACED BOTTLE. (K)

Part: INDICATOR — INOPERATIVE (AIRSPEED)

ABORTED TAKEOFF AT 110 KNOTS DUE TO STANDBY AIRSPEED INDICATOR READING ZERO KNOTS. TAKEOFF WEIGHT AT 49380 LBS. NO OVERHEAT. FOUND P3 DRAIN TUBE FULL OF WATER. PURGED P3 SYSTEM IAW 34 P3 AND S3 SYSTEM LEAK CHECK GOOD. STANDBY AIRSPEED ALTITUDE. OPS CHECK GOOD. (M)

Part: CONTROL PANEL — BURNED (FMS)

FMS PAGE STUCK ON PERFORMANCE SCREEN, AFTER DETECTING ELECTRICAL BURNING ODOR IN COCKPIT AND IN FROM CABIN. PULLED CIRCUIT BREAKER H12. REMOVED AND REPLACED FMS CONTROL PANEL FOR BURNING ODOR AFTER FROZEN SCREEN. NO FURTHER ODOR NOTED WITH REPLACEMENT. OPS CHECK GOOD IAW 34-61-01. (M)

Part: BPSU — FAILED (RT BRAKE) · airframe 4,256 hrs · 3,612 cycles

FLAP FAIL WARNING INFLIGHT WITH NO MOVEMENT AFTER FLAP SELECTION. INTERROGATED FECU, RIGHT BRAKE AND POSITION SENSORING UNIT (BPSU) FAIL. REMOVED AND REPLACED RIGHT BPSU.

Part: SKIN — DENTED (SPOILER)

RIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NOTED DENT IAW WVAC EO 601R-57-4039A. (M)

Part: SKIN — DENTED (SPOILER)

RIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NDT'ED DENT IAW WVAC EO 601R-57-4039A. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 310. REPAIRED DAMAGE AT PASSENGER DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PAX DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PASSENGER DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 310. REPAIRED DAMGE AT PAX DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M)

Part: STRUCTURE — DAMAGED (TE FLAPS)

LEFT INBOARD FLAP HAS WORN RIVET HEADS ON INBOARD RIB OUTER FACE. REPLACED DISCREPANT RIVETS IAW CRJ SRM CHAP 51 AND WVAC EO 601R-57-4038. (M)

Part: A/C PACK — MALFUNCTIONED (A/C BAY)

RIGHT PACK HIGH PRESSURE 80 PSI RUNNING QRH GOT LEFT PACK HIGH PRESSURE. RETURNED TO AIRPORT. DEPOWERED AND REPOWERED AIRCRAFT. RESET PACKS CIRCUIT BREAKERS. OPS CHECK GOOD. (M)

Part: ODOR — DETECTED (CABIN)

FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN, SMELLED LIKE ELECTRICAL OR MECHANICAL SOURCE. SMOKE CLEARED AFTER FOLLOWING QRH PROCEDURES. MAINTENANCE GROUND RAN BOTH ENGINES, OPERATED PACKS AND INSPECTED GALLEY HEATER AND FAN FOR CORRECT OPERATION. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR CONTINUED SERVICE. (M)