N403AW

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 39,727 hrs · 36,131 cycles

AFTER TAKEOFF, WHEN GEAR WAS RETRACTED, NOSE GEAR FAILED TO RETRACT. GEAR DISAGREE WARNING & NOSE DOOR WARNING. WOW INPUT CAUTION MSGS'S DISPLAYED. COMPLIED WITH QRH, MANUALLY DEPLOYED GEAR, LANDED NORMALLY, WEIGHT 43,000 LBS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 39,725 hrs · 36,127 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING. NOSE GEAR NEVER SHOWED UP, CREW SELECTED GEAR DOWN & DIVERTED.

Part: PSU — UNSECURE (CABIN) · airframe 39,325 hrs · 35,756 cycles

DURING TAKEOFF PSU 1DF FELL DOWN. O2 GENERATORS DID NOT ACTIVATE. ACFT RETURNED TO FIELD.

Part: PIVOT ASSY — BINDING (PAX DOOR) · airframe 38,468 hrs · 34,917 cycles

RECEIVED PAX DOOR OUTER HANDLE CAUTION. WHILE PERFORMING QRH, PAX DOOR WARNING MSG APPEARED FOR APPROX 3 MINUTES. WARNING MSG CLEARED WITH NO CREW ACTION. EMERGENCY DECLARED & FLIGHT RETURNED. ON LANDING, OUTER HANDLE WAS FOUND OUT. COMPLIED WITH OPS CHECK OF PAX DOOR IAW AMM 52-11-00. FOUND DOOR TO BE DIFFICULT TO OPERATE FROM THE OUTSIDE, ALL OTHER INDICATIONS NORMAL. FOUND UPPER PIVOT ASSEMBLY FOR PAX DOOR LINKAGE BINDING. REMOVED, CLEANED & REINSTALLED PAX DOOR UPPER PIVOT ASSEMBLY IAW AMM 52-11-21. OPS CHECKED GOOD.

Part: FUEL CONTROL — FAILED (LT ENGINE) · airframe 37,762 hrs · 34,246 cycles

DURING CLIMB OUT, FELT AN AIRFRAME VIBRATION. LT N1, N2, ITT & FUEL FLOW ERRATIC. LT VIBRATION 0.5. LT ENGINE PARAMETERS FLUCTUATED +/- 2% & FF 300LBS. DECLARED AN EMERGENCY & RETURNED. R & R LT FUEL CONTROL ASSEMBLY IAW AMM 73-21-00. PERFORMED OPS, LEAK, RIG CHECKS & POWER RUN CHECKS. ALL CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 37,744 hrs · 34,227 cycles

RECEIVED SMOKE IN TOILET CAUTION AFTER TAKEOFF. DECLARED EMER & COMPLIED WITH QRH. PULLED CB P2, C5, D14, D15, S2 & U2. RETURNED & DID NOT LAND OVERWEIGHT. INSPECTED LAVATORY, NO DEFECTS NOTED. NO SIGNS OF SMOKE OR FIRE FOUND. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. SN OFF 09140, ON ADN2617.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,587 hrs · 34,068 cycles

EMERGENCY LIGHTS FROM ROWS 8-13 INOPERATIVE & ROW 12 - 13 FLOOR LIGHT SECTION MISSING CONNECTOR.

Part: LIGHT — INOPERATIVE (ROWS 8-12) · airframe 37,555 hrs · 34,039 cycles

EMERGENCY LIGHTING FROM ROW 8 - 12 FOUND INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,259 hrs · 33,758 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 9 & 10.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

FORWARD EQUIPMENT BAY FLOOR SKIN CRACKED ON LT SIDE OTBD OF GAUGES. REPAIRED IAW REO 601R-53-11-081 REV NC.

Part: RIB — CRACKED (LT WING) · airframe 36,011 hrs · 32,588 cycles

LEFT MLG WW BATTERY RIB CRACKED AFT RADIUS. R & R EXISTING REPAIR DOUBLER IAW REO 601R-57-51-046 REV B DATED 2002-02-28.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 36,011 hrs · 32,588 cycles

PAX DOOR STAIR AFT DRAG ANGLE IS CRACKED AT PULLEY BRACKET. R & R EXISTING REPAIR ANGLE FROM PN 601R31907-301 IAW REO 601R-52-11-513 REV A DATED 09 MAR 05.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

FS 621 BULKHEAD FWD SIDE CRACKED ISOLATOR MOUNT BRACKET. R & R WITH SERVICEABLE PN 601R45156-75 IAW SRM 51-40-11 & 51-42-06.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 36,011 hrs · 32,588 cycles

LEFT MLG WW DRAG ANGLE CRACKED. R & R ANGLE PN 600-10389-1 IAW SRM 51-40-11 & 51-42-21.

Part: ANGLE — CRACKED (RT WING) · airframe 36,011 hrs · 32,588 cycles

UPPER ANGLE BEHIND RT WING LE TRANSITION PANEL 620ML IS CRACKED ON OTBD CORNER. R & R WITH SERVICEABLE PART IAW SRM 51-40-11, 51-24-16 & 51-42-13.

Part: RETAINER — CRACKED (NACELLE) · airframe 36,011 hrs · 32,588 cycles

SEAL RETAINER CRACKED ON PANEL 412AT. R & R WITH SERVICEABLE PN 601-37003-39 IAW SRM 51-40-11 & 51-42-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

NLG CUT OUT LT & RT AFT RADIUS CRACKS AT FS 235. REPAIRED NLG CUT OUT AFT RADIUS SURROUND SKIN ON LT & RT SIDES IAW REO 601R-53-121-048 REV C DATED 2008-10-01.

Part: FITTING — CORRODED (CABIN) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

WARDROBE AFT FEET CORRODED. R & R AFT WARDROBE FEET WITH SERVICEABLE PARTS IAW SRM 51-40-11 & 51-41-02.

Part: FITTING — CORRODED (GALLEY) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

GALLEY INBD AFT FOOT CORRODED. R & R INBD AFT GALLEY FOOT WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-41-02.

Part: MOUNT FITTING — CRACKED (WING) · airframe 36,011 hrs · 32,588 cycles

PRESS REFUEL PORT MOUNT ANGLE IS CRACKED. R & R MOUNT ANGLE PN 600-62441-13 IAW SRM 51-40-11 & 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

LEFT OBLIQUE ANGLE CRACKED AT FS 621 - 625 NEAR STRINGER 13L. R & R WITH SERVICEABLE ANGLE IAW REO 601R-53-61-100 REV A DATED 2008-01-23 & SRM 51-40-11 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

INBD CLIP CRACKED AT FS 280 RBL 9. R & R CRACKED CLIP AT FS 280 RBL 9 IAW REO 601R-53-11-171 REV D.

Part: POST — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

LBL 18 OTBD VERTICAL POST AT FS 409+128 IS CRACKED AT BOTTOM. REPAIRED IAW REO 601R-53-41-056 REV F DATED 2011-09-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,011 hrs · 32,588 cycles

INBD & OTBD CLIPS ARE CRACKED AT LBL 9 FS 280. R & R INBD & OTBD CLIPS AT FS 280, LBL 9.

Part: DOUBLER — CORRODED (WINDSCREEN) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

LEFT WINDSCREEN KICK PLATE DOUBLERS CORRODED, FWD & AFT. R & R WITH SERVICEABLE DOUBLERS IAW CMM 25-22-89.

Part: MOUNT BRACKET — CORRODED (CABIN) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

LEFT & RIGHT WINDSCREEN CORROSION ON MOUNT FEET. R & R FEET ON LT & RT WINDSCREENS IAW CMM 25-22-89.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

SERVICE DOOR LOWER SILL FLOOR SUPPORT LOWER ANGLE CORRODED. R & R ANGLE WITH SERVICEABLE PART IAW SRM 51-40-11, 51-42-13 & 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

LEFT FLOOR SILL FROM FS 349 TO 356 CORRODED. REPAIRED IAW EA 15-2014-094 DATED 4-24-2014 & REO 601R-53-00-530 DATED 06-JUN-2013.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

FLOOR SUPPORT CROSSBEAM AT FS 349 HAS CORROSION FROM RBL 36 TO RBL 45. CLEANED CORROSION & REPLACED AFT FLOOR SUPPORT ANGLE ON FS 349 CROSSBEAM RT SIDE IAW SRM 51-40-11 & 51-40-06.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

PAX DOOR SILL FWD & AFT CLEAT FITTINGS, FS 316 & 343 CORRODED. R & R WITH SERVICEABLE PARTS PN 601R31527-217 IAW SRM 51-40-11 & 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,011 hrs · 32,588 cycles

LBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE LOCATIONS BETWEEN FS 561 & 564. REPAIRED FLOORBEAM CAP LBL 27 AT FS 561 - 564 IAW SRM 53-00-43 REPAIR NR 2 FLOORBEAM SPLICE REPAIR.

Part: COWLING — CRACKED (LT ENGINE) · airframe 36,011 hrs · 32,588 cycles

LEFT ENG LOWER CORE COWL FWD CORNER CRACKED. REPAIRED LT ENG LOWER CORE COWL FWD CORNER IAW CMM TASK 71-12-01-300-826-A01.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 34,520 hrs · 31,144 cycles

ON FINAL, RECEIVED HYD 2 LOW PRESS CAUTION HYD 2 QTY READS 5 PERCENT. MESSAGE APPEARED APROX 30 SECONDS AFTER GEAR SELECTD DOWN, COMPLIED WITH QRH TURNED ACMP2 OFF, EDP 2 WAS RUNNING FOR APROX 20 MIN WITH LOW PRESSURE MESSAGE (INCLUDING TAXI TIME). REPLACED PACKING FOR NR 2 ACMP BALL ATTENUATOR ASSY IAW AMM 29-11-03. OPS CHECKED GOOD, NO LEAKS NOTED

Part: COMPUTER — FAILED (FCC) · airframe 31,713 hrs · 28,436 cycles

ON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786. TROUBLESHOT SYSTEM AND FOUND FCC2 FAILING. REPLACED FCC 2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS TIME.

Part: COMPUTER — FAILED (FCC2) · airframe 31,713 hrs · 28,436 cycles

ON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786, TROUBLESHOT SYS AND FOUND FCC 2 FAILING. REPLACED FCC2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS TIME.

Part: ANGLE — CRACKED (FS 280) · airframe 31,504 hrs · 28,237 cycles

RBL 9 OTBD CLIP AT FS 280.00 CRACKED. REMOVED UNSERVICEABLE CLIP ON RBL 9 AT FS 280.00 IAW SRM 51-42-21 AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-11-171, REV D.

Part: SKIN — CHAFED (WS 45) · airframe 31,504 hrs · 28,237 cycles

WING PLANK CHAFED FROM FAIRING AT WS 45 WING REAR FACE RT SIDE BLENDED AREA AT WS 45 MEASURED DEPTH .045 WITHIN LIMITS IAW REO 601R-57-21-1673.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 31,504 hrs · 28,237 cycles

RT WING INBD L/E OTBD ATTACH BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-41-02/ 51-40-11.

Part: FLOOR SUPPORT — CORRODED (FS 589-621) · corrosion level 2 · airframe 31,504 hrs · 28,237 cycles

LBL 9 FLOOR SUPPORT CAP FS 529-610 HAS CORROSION ON OTBD SIDE. REPAIR BY SPLICING IN NEW MEMBER IAW SRM 53-00-43.

Part: PULLEY BRACKET — CHAFED (PAX DOOR) · airframe 31,504 hrs · 28,237 cycles

PAX DOOR MOTOR PULLEY BRACKET CHAFED AREA ON PAX DOOR MOTOR PULLEY BRACKET. BLENDED CHAFE ON PAX DOOR MOTOR PULLEY BRACKET WITHIN LIMITS ORIG .165. REMOVED .015 REMAINING .090 NDT, ALODINED, PRIMED AND TOP COATED IAW REO 601R-52-11-2077.

Part: COVER — CHAFED (LT MLG) · airframe 31,504 hrs · 28,237 cycles

LT MLG BATTERY RIB COVER CHAFED FROM LT MLG HARNESS. BLENDED CHAFED AREA ON TL MLG BATTERY RIB COVER ORIG THICKNESS .080, REMOVED .023 REMAINING .057 IAW SRM 51-12-00 USING THICKNESS GAUGE. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16, REO 601R-57-21-1676, FOUND TO BE OUT OF LIMITS.

Part: PANEL — CRACKED (NACELLE) · airframe 31,504 hrs · 28,237 cycles

PANEL 412AT CRACKED. REMOVED UNSERVICEABLE RETAINER & SEAL. REPLACED WITH SERVICEABLE RETAINER AND SEAL IAW SRM 51-40-11, 51-42-06, AMM 54-63-01.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 31,504 hrs · 28,237 cycles

FOUND CARGO BAY DOOR HANDLE HOUSING CRACKED ABOVE CENTER OF HANDLE. REMOVED UNSERVICEABLE CARGO DOOR HANDLE AND REPLACED WITH SERVICEABLE HANDLE IAW AMM CMM 52-31-03 AND SRM 51-40-03, AND SRM 51-40-11, 51-42-06.

Part: BULKHEAD — GOUGED (FS 280 RT) · airframe 31,504 hrs · 28,237 cycles

RT AFT SIDE OF 280 BULKHEAD HAS 2 GOUGES ON THE INBD SIDE FROM MAKING CONTACT WITH GALLEY STORAGE COMPARTMENT DOOR.

Part: CARGO TRACK — CORRODED · airframe 31,504 hrs · 28,237 cycles

CORROSION FOUND ON CARGO TRACK. R & R CARGO TRACK WITH SERVICEABLE IAW 51-40-11, SRM 51-21-11, AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (FS 559-621) · airframe 31,504 hrs · 28,237 cycles

RT SIDE FLOOR SILL CORRODED AROUND NUTPLATES FS 559+112, FS 621. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR SILL AT FS 559+112 TO FS 621 IAW REO 601R-53-61-4497.

Part: FLOOR SUPPORT — CRACKED (FS 589) · airframe 31,504 hrs · 28,237 cycles

FLOOR SUPPORT CLIP AT FS 589, LBL 45 CRACKED. REMOVED, FABRICATION AND INSTALLATION OF SERVICE CLIP IAW CRJ 200 51-24-16, 51-40-11, 51-42-21.

Part: PANEL — CHAFED (WS 54.848)

PANEL 684BB & 684AB IS CHAFED. BLENDED PANEL 684BB MAT LOSS.003. REMAINING MAT .077 WITHIN LIMITS IAW SRM 57-52-00. BLENDED PANEL 684AB MAT LOSS .017 REMAINING MAT .063 WITHIN LIMITS IAW REO 601R-57-52-1910.

Part: SKIN — CHAFED (MLG DOOR) · airframe 31,504 hrs · 28,237 cycles

LEFT MLG DOOR INNER SKIN AND FASTENER CHAFED. BLENDED CHAFE AREA WITHIN LIMITS ORG .040, REMOVED .002, REMAINING .038 IAW SRM 52-82-00, FIG 101. BLENDED AREA NR 5 FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R-52-82-337, R & R CHAFE FASTENER.

Part: FLOOR SUPPORT — CORRODED (FS 310-349) · corrosion level 2 · airframe 31,504 hrs · 28,237 cycles

CORROSION ON FLOOR SUPPORT ANGLE AT PAX DOOR CUT OUT PN 601R31527-205S. R & R FLOOR SUPPORT ANGLE AT PAX DOOR CUT OUT WITH SERVICEABLE PN 601R-31527-205S IAW SRM 51-48-11, SRM 51-42-06, SRM 51-45-00, SRM 51-42-13.

Part: HANDLE — CORRODED (PAX DOOR) · airframe 31,504 hrs · 28,237 cycles

CORROSION ON PAX DOOR HANDLE CLEAT WAS BEYOND SERVICEABLE LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE PAX DOOR CLET ANGLE IAW SRM 53-00-00, 51-21-11, 51-40-11, 51-25-06, 51-25-16.

Part: BRACKET — BROKEN (WS 252) · airframe 31,504 hrs · 28,237 cycles

LT OTBD L/E INBD MOUNTING BRACKET BROKE. REMOVED UNSERVICEABLE LT OTBD L/E INBD MOUNTING BRACKET AND INSTALLED SERVICEABLE INBD MOUNTING BRACKET IAW SRM 51-40-11, 51-41-00 & 51-42-10.

Part: ANGLE — CRACKED (FS 484) · airframe 31,504 hrs · 28,237 cycles

ANGLE CRACKED AT FS 484, RBL 36 OTBD OF FLOORBEAM INTERCOSTAL. REMOVED ANGLE IAW REO 601R-53-41-054, REV B AND REPLACED WITH SERVICEABLE ANGLE AT FS 484, RBL IAW REO 601R-53-41-059, REV B.

Part: BRACKET — BROKEN (WS 232-252) · airframe 31,504 hrs · 28,237 cycles

LT OTBD L/E INBD MOUNTING BRACKET BROKE. REMOVED UNSERVICEABLE LT OTBD L/E INBD MOUNTING BRACKET AND INSTALLED SERVICEABLE INBD MOUNTING BRACKET IAW SRM 51-40-11, 51-41-00, 51-42-10.

Part: ATTACH FITTING — CORRODED (FS 289-310) · airframe 31,504 hrs · 28,237 cycles

FWD AND AFT WARDROBE ATTACH PARTS ON FUSELAGE FLOOR AT FS 310 AND FS 289, LBL 36 CORRODED. REMOVED AFT WARDROBE ATTACH POINT AND REPLACED WITH SERVICEABLE ATTACH JOINT AT FS 310, LBL 36. BLENDED FWD WARDROBE ATTACH POINT AT FS 289, LBL36. FOUND TO BE IN LIMITS TROUBLED AREA.

Part: TRUNNION — DAMAGED (MLG) · airframe 31,504 hrs · 28,237 cycles

DURING COMPLIANCE WITH AWAC`S EO E10/016/457 FOUND 5 EA TOTAL OVERSIZED HOLES IN MLG TRUNNION LOWER FLANGES 4 ON LT 1 ON RT. REPAIRED 5 EA OVERSIZED HOLES ON MLG LOWER FLANGES IAW REO 601R-57-21-1667.

Part: ANGLE — CRACKED (BS 700) · airframe 31,504 hrs · 28,237 cycles

LT CENTER OF AEB DOOR CUT OUT HAS CRACKED CLIP ON OTBD SIDE. REMOVED UNSERVICEABLE AND REPLACED WITH SERVICEABLE CLIP ON OTBD SIDE OF AFB DOOR CUTOUT IAW SRM 51-42-06, 51-24-16.

Part: SKIN — DAMAGED (BS 618-630) · airframe 30,028 hrs · 26,662 cycles

ACFT HAS DAMAGE TO TAIL BETWEEN FS 618 & 630, FS 618. (.145 BOT 24L & 25L) FS 619 (.100 BET 25L AND 26L) FS 626 (.110LH AND .071 RT OF 27 CL) FS 629.50 (.032 BET 27CL AND 26R) 24" L X 1.3750 W X .145D). R & R BELLY SKIN IAW SRM 51-42-06, 51-40-11 & REO 601R-53-61-4175.

Part: COWLING — MISSING (LT ENGINE) · airframe 30,255 hrs · 26,906 cycles

LT LOWER FORWARD COWL MISSING, (FOUND COWL ON RUNWAY). INSTALL LEFT LWR NOSE COWL W/SERV COWL. INSTALL LEFT LOWER NOSE COWL WITH SERV COWL. S/N OFF C0360 S/N ON SB/RJNAC/C0791.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 30,062 hrs · 26,701 cycles

IN CRUISE AT FL 220 RECEIVED HYD 1 LOW PRESSURE CAUTION. HYD 1 QTY 5 PERCENT DROPPED TO ZERO. NR 1 PUMP RAN 25 MIN WITH NO QTY. R & R PRESSURE HOSE ASSY AND CLAMP.

Part: SKIN — DAMAGED (BS 559-625) · airframe 30,028 hrs · 26,662 cycles

MULTIPLE ELONGATED HOLES TO SKIN AT FS 559.00+112 TO FS 625 BETWEEN STRINGER 20L TO 20R. REPAIRED IAW REO 601R-53-61-4175.

Part: RIB — CRACKED (RT NACELLE) · airframe 30,028 hrs · 26,662 cycles

RT NACELLE PYLON L/E FAIRING ATTACH RIB AT FS605 IS CRACKED AT LOWER BUT PLATE HOLE. REPAIRED CRACKED ATTACH RIB AT FS 605 IAW SRM 51-71-12.

Part: SKIN — DAMAGED (BS 559) · airframe 30,028 hrs · 26,662 cycles

SKIN FOR AFT LOWER FUSELAGE HAS MULTIPLE ELONGATED HOLES FROM DRILL UP PROCESS. REPAIRED ELONGATED HOLES IAW REO 601R-53-61-4175.

Part: SKIN — SCRATCHED (BS 229-316) · airframe 30,028 hrs · 26,662 cycles

RT FUSELAGE OUTER SKIN AT FS 299, STR 20, 17" X .25" X.008" DEEP SCRATCH C/W REO 601R-53-21-1340 C/T BLENDING AND SMOOTHING AWAY SCRATCH.

Part: SKIN — SCRATCHED (BS 299) · airframe 30,028 hrs · 26,662 cycles

FUSELAGE SKIN FS 299, S20R, 17" X .25 X .008" DEEP SCRATCH COMPLIED WITH REO 601R-53-21-1340.

Part: SKIN — DAMAGED (FS 654) · airframe 30,028 hrs · 26,662 cycles

ACFT HAS SKIN DAMAGE AT FS 655 (.033 BET 27 CL AND 26L) (9.25" L X .1250 W X .033 D). REPAIRED SKIN AT FS 655 IAW REO 601R-53-61-4149 & R & R FS 654 FRAME, LOWER SECTION, PN 601-36002-3 IAW SRM 51-42-06 & 51-40-11.

Part: SKIN — DAMAGED (BS 589) · airframe 27,190 hrs · 23,693 cycles

MUSTIPLE DENTS, GOUGES AND TEARS IN FUSELAGE BELOW CARGO DOOR. DAMAGE IS ISOLATED TO SKIN. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTALLED FILLER AND DOUBLER IAW REO 601R-53-61-3678.

Part: RELAY — MALFUNCTIONED (DC BUSS) · airframe 27,496 hrs · 24,010 cycles

DC BUSS 2 CAUTION MSG. R & R CONTACTOR K3PA, RELAY K21PA AND DIODE NR CR28PA IAW 24-50-00. OPS CK GOOD OF DC BUSS 2 AT THIS TIME.

Part: BPSU — FAILED (TE FLAPS) · airframe 27,078 hrs · 23,587 cycles

AIR RTN- AFTER T/O FLAPS RETRACTED 20 TO 8, FLAPS FAILED AS 10 (LT = 8/RT=10) C/W QRH. NORMAL LANDING AT 46400 LBS GROSS. R & R LT AND RT BRAKE POSITION SENSOR UNIT.

Part: ECU — FAILED (E&E BAY) · airframe 27,069 hrs · 23,578 cycles

FLAPS FAILED AT 12 DEGREES DURING RETRACTION AFTER TAKEOFF. C/W QRH DIVERTED, LANDED AT 44360. C/W FLAP RESET PROCEDURE (98-018D) FLAPS FAILED AGAIN. REPLACED FECU IAW AMM 27-51-05. OPS AND FUNCTIONAL TEST CK OK.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 27,048 hrs · 23,553 cycles

FLAPS FAIL MSG DURING CLIMB-OUT. FAILED AT 13 DEGREES. C/W QRH, DIVERTED, LANDED AT 46370 LBS. ATTEMPTED FLAP RESET IAW SUPP 98-018C (AMOC) FLAPS FAILED AGAIN. R & R FLAP ELECTRONIC CONTROL UNIT.

Part: UNKNOWN — SMOKE (CABIN) · airframe 27,023 hrs · 23,526 cycles

ELECTRICAL SMOKE SMELL IN COCKPIT. INSPECTED CB`S WITH NO FAULTS FOUND. STARTED APU RAN BOTH PACS FOUND LT PAC TEMP UNCONTROLABLE IN BOTH AUTO AND MANUAL. SHUT LT PACK OFF WITH RT PACK ON NO FURTHER SMOKE SMELL IN COCKPIT.

Part: DUCT — BENT (PRECOOLER) · airframe 27,023 hrs · 23,526 cycles

AT FL240, RECEIVED CABIN ALT CAUTION MSG FOLLOWED BY WARNING. ALL CABIN PRESSURE WAS LOST. PERFORMED EMERG DESCENT & C/W ALL QRH`S. LANDED UNPRESSURIZED. RT PACK INDICATED 43 PSI WITH NO AIR FLOW. ARINC COOL CAUTION MSG IN FLIGHT ALSO. FOUND BOTH DUCTS AT PRECOOLER BENT, PREVENTING CORRECT INSTALLATION R & R BOTH PRECOOLER DUCTS AND COUPLINGS. INSTALLED DUCTS FROM PRECOOLER TO HEAT EXCHANGER.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 26,943 hrs · 23,449 cycles

PAX DOOR CAM COVER AFT BRACKET CRACKED. REMOVED, FABRICATED NEW BRACKET AND INSTALLED.

Part: BRACKET — CRACKED (BS 324) · airframe 26,943 hrs · 23,449 cycles

PAX DOOR CAM COVER FWD BRACKET IS CRACKED, REMOVED, FABRICATED NEW BRACKET AND INSTALLED.

Part: PANEL — DAMAGED (RT WING) · airframe 26,943 hrs · 23,449 cycles

FUEL PANEL 640BB HAS GRINDING MARKS IN THE RED SEAL AREA. REPAIRED FUEL PANEL 640BB IAW REO 601R-52-21-1263.

Part: LINK — DISPLACED (FS 513) · airframe 26,943 hrs · 23,449 cycles

LT/RT FS 513 WING LINKS ROTATED AND TOUCHING AIRFRAME REPAIR DEFERED 5000 HRS WITH 1000 HR REINSPECTS IAW REO 601R-53-41-1191, DUE TO NO TOOLING AVAILABLE.

Part: FRAME — CORRODED (BS 330) · corrosion level 2 · airframe 26,943 hrs · 23,449 cycles

FRAME 333.00 HAS MINOR SURFACE CORROSION BETWEEN STR 26L & 26R. REMOVED SURFACE W CORROSION, TREATED, PRIMED & PAINTED REPAIR AREA, IAW SRM 51-21-06, 51-25-00, 51-25-06.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 26,943 hrs · 23,449 cycles

FLOOR SUPPORT AT FS 280 CRACKED AT RBL 10 AND LBL 10 REPAIR IAW REO 601R-53-11-137 REV A AND 601R-53-11-138NC.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,943 hrs · 23,449 cycles

CORRODED ANGLE AND BRACKET IN PAX DOOR OPENING. FABRICATED NEW ANGLE AND REPLACED ALONG WITH BRACKETS.

Part: ATTACH BRACKET — CORRODED (BS 330) · corrosion level 2 · airframe 26,943 hrs · 23,449 cycles

PAX DOOR LWR CTR INTERCOSTAL CLIP CORRODED. REPLACE CLIP IAW SRM PROCEDURES.

Part: RIB — CRACKED (RT WING) · airframe 26,943 hrs · 23,449 cycles

RT BATT RIB CRACKED IN RT WHEEL WELL. REPAIRED IAW REO 601R-57-51-046.

Part: FIRE DETECTOR — MALFUNCTIONED · airframe 26,059 hrs · 22,544 cycles

ON LANDING ROLL OUT LT FIRE WARNING ILLUMINATED EXITED RUNWAY. STOPPED ACFT. IAC WAS RED FOLLOWED QRH, BOTH FIRE BOTTLES WERE FIRED. THE FIRE WARNING REMAINED ON, WE PULLED AHEAD AND PARKED IN GATE AREA AFTER TALKING TO TOWER AND DEPLANED NORMALLY. TOWER SAID NO EVIDENCE OF SMOKE OR FIRE AFTER INITIAL SMOKE, THEY SAID WHILE STOPPED. REMOVED AND REPLACED FIRE AND OVERHEAT CONTROLLER IAW AMM 26-10-01. OPS CHECKS GOOD REF LP 205914/1 AND 2 FOR ENG FIRE BOTTLE REPLACEMENT.

Part: SEAL — LOOSE (FAIRING) · airframe 25,487 hrs · 21,988 cycles

ON CLIMBOUT, NOTICED VIBRATION IN BOTH CONTROL COLUMNS AND AN ASSOCIATED LOW PITCH BUZZ. VIBRATION AND BUSS REMAINED CONSTANT REGARDLESS OF AIRSPEED PITCH OR CONTROL COLUMN MOVEMENT. FA REPORTED SIMILAR BUZZ AND VIBRATION IN PASSENGER CABIN. VIBRATION AND BUZZ WERE INTERMITTNET THROUGHOUT FLIGHT. FOUND AERODYNAMIC SEALANT OF FWD EDGE AT BELLY FAIRING 193AB DETERIORATED W/4" OF SECTION MISSING REMOVED SEALANT AND RESEALED IAW 51-23-00. (K)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 25,311 hrs · 21,819 cycles

ON DEPARTURE RUNWAY 1, WHILE MAKING 20 DEGREE LT TURN, RECEIVED FUEL INBALANCE CASS MESSAGE. LT WING INDICATED 1000 LBS MORE AND THEN MESSAGE CLEARED. AT 9000 FT, TURNED LT WITH 30 DEGREE BANK AND RECEIVED "FUEL INBALANCE" CASS MESSAGE. MESSAGE EXTINGUISHED WITH WINGS LEVEL. C/W QRH AND DIVERTED. REF W.O. 13711 FOR MX PERFORMED AND C/A OK FOR RETURN TO SERVICE. (K)

Part: ACTUATOR — FAILED (STAB TRIM) · airframe 25,287 hrs · 21,791 cycles

STAB AND MACH TRIM DISENGAGED IN FLT RE-ENGAGED AFTER 15 SEC TRIM DISENGAGED AGAIN, RECEIVED STAB TRIM, MACH TRIM AND AUTO PILOT PITCH TRIM CASS MSG. FOUND STAB TRIM ACTUATOR FAILS CHANNEL 1 REMOVED AND REPLACED HORZ STAB TRIM ACTUATOR IAW AMM 27-42-01.

Part: A/C PACK — ODOR (LEFT) · airframe 25,032 hrs · 21,538 cycles

DURING FLT, BURNING ODOR COMING FROM LT PACK. BLEEDS ON ENGINE NO AIRFLOW OUT OF LT PACK. NO ODOR AND PACK AIR FLOW NORMAL WHEN BLEEDS ON. PERFORMED OPS CHECK OF LT PACK IAW AMM 21-51-00 AND FOUND NO DEFECTS AT THIS TIME. NO ODOR NOTED WITH ENGINE BLEED AIR AND APU BLEED AIR SELECTED. REMOVED PLACARD AND REMOVED FROM MEL. (K)

Part: BLEED AIR SYS — ODOR (CABIN) · airframe 25,055 hrs · 21,564 cycles

DURING FLT BURNING ODOR COMING FROM LT PACK. BLEEDS ON ENGINE NO AIR FLOW OUT OF LT PACK. NO ODOR AND PACK AIR FLOW NORMAL WHEN BLEEDS ON. PERMORED OPS CHECK OF LT PACK IAW AMM 21-51-00 AND FOUND NO DEFECTS AT THIS TIME. NO ODOR NOTED WITH ENGINE BLEED AIR AND APU BLEED AIR SELECTED. REMOVED PLACARD AND REMOVED FROM MEL. (K)

Part: SKIN — DENTED (TE FLAP) · airframe 22,381 hrs · 19,038 cycles

DENT ON RT OUTBOARD WING FLAP. RT OUTBOARD WING FLAP REPAIRED IAW SRM 57-53-00 FIG 202 SHEET 2 REPAIR 3. (A)

Part: LENS — CRACKED (LIGHT) · airframe 22,381 hrs · 19,038 cycles

RIGHT LIGHT LENS CRACKED. (M) RT WING LIGHT LENS REPLACED IAW AMM 57-30-01-400-801 AWAC SUPPLEMENT 07-009. (A)

Part: ANGLE — BROKEN (LT WING TE FLAP) · airframe 22,381 hrs · 19,038 cycles

LEFT WING OUTBOARD FLAP, INBOARD HINGE ARM, LEFT ANGLE IS BROKEN. (M) ANGLE FABRICATED IN S6144-13 IAW SRM 51-24-36 PRIMER AND PAINT APPLIED IAW SRM 51-25-01 AND INSTALLED IAW SRM 51-42-06. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,381 hrs · 19,038 cycles

FLOOR ANGLE CRACKED ON COCKPIT TO CABIN AT FS 280 LBL 9 TO RBL 9. - - FLOOR ANGLE AT FS 280.00 LBL 9 TO RBL 9 REPLACED IAW SRM 51-42-06 . . (A)

Part: SCUFF PLATE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 22,381 hrs · 19,038 cycles

CORROSION UNDER SERVICE DOOR SCUFF PLATE. (K) CORROSION REMOVED IAW SRM 51-21-06.

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 22,381 hrs · 19,038 cycles

CARGO BAY FLOOR SILL BETWEEN FS 574 TO FS 621, ALL NUT PLATE HOLES CORRODED. CORROSION REMOVED IAW SRM 51-21-06 .

Part: BRACKET — BROKEN (RT WING TE FLAP) · airframe 22,381 hrs · 19,038 cycles

BRACKET BROKEN AT THE CENTER HINGE ARM OF THE RIGHT WING OUTBOARD FLAP. (M) BROKEN BRACKET AT CENTER HINGE ARM OF RIGHT WING OUTBOARD FLAP REPLACED IAW SRM 51-42-06.

Part: HINGE — CRACKED (PAX DOOR) · airframe 22,381 hrs · 19,038 cycles

PAX DOOR UPPER FOLDING STEP BOTTOM HINGE FOUND CRACKED FOUND NEAR FWD END. - - PAX DOOR FLODING STEP BOTTEM HINGE REPLACED IAW SRM 51-41-02. .(A)

Part: PRESSURE PANEL — CORRODED (BS 409-559) · airframe 22,381 hrs · 19,038 cycles

CORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, RBL 45. (M) CORROSION REMOVED ON PRESSURE FLOOR IAW SRM 51-21-06 .

Part: ATTACH FITTING — CORRODED (BS 589-605) · corrosion level 1 · airframe 22,381 hrs · 19,038 cycles

CARGO DOOR FITTING ATTACHMENT FS 589 AND FS 605 CORRODED. (K) CORROSION REMOVED ON CARGO DOOR FITTING ATTCHMENT AT FS 589 AND 605 IAW SRM 51-21-06 . (A)

Part: PRESSURE PANEL — CORRODED (BS 409-559) · airframe 22,381 hrs · 19,038 cycles

CORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, LBL 45. CORRSION REMOVED IAW SRM 51-21-06.

Part: SILL — DAMAGED (BS 310-340) · airframe 22,381 hrs · 19,038 cycles

LOWER SILL LONGERON OF PAX DOOR CORRODED BETWEEN FS 310 TO 340 LBL 45. (M) CORROSION ON LOWER SILL OF PAX DOOR REMOVED IAW SRM 51-21-06.

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 22,381 hrs · 19,038 cycles

AT FS 718 RT SIDE, NR2 HYDRAULIC MANIFOLD SUPPORT BRACKET FOUND CRACKED IN AFT LOWER CORNER. PERFORMED REPAIR AT FS 718.00 RT SIDE NR2 HYDRAULIC MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-031 REV A. (A)

Part: SILL — CORRODED (BS 605-621) · airframe 22,381 hrs · 19,038 cycles

CARGO FLOOR SILL CORRODED FS 605 TO 621, RBL 45. (M) CORROSION REMOVED ON CARGO FLOOR SILL IAW SRM 51-21-06.

Part: SILL — CRACKED (BS 605) · airframe 22,381 hrs · 19,038 cycles

CARGO DOOR SILL CRACK AROUND RIVET FS 605 LBL 45. OPEN.

Part: SILL — CRACKED (BS 589)

CARGO DOOR SILL CRACK AROUND RIVET FS 589 LBL 45. (M) CRACK REPAIRED IAW REO 601R-53-61-433 . (A)

Part: HINGE — CRACKED (CARGO DOOR) · airframe 22,381 hrs

FOUND CARGO DOOR STEP PLATE HINGE CRACKED. REPLACED CARGO DOOR STEP PLATE HINGERS IAW SRM 51-42-06. .

Part: COVER — CRACKED (PAX DOOR) · airframe 22,381 hrs · 19,038 cycles

PAX DOOR FORWARD AND AFT UPPER CORNER COVERS FOUND CRACK. (M) PAX DOOR FWD AND AFT UPPER CORNER COVERS REPLACED WITH SERVICEABLE ITEMS IAW SRM 51-42-13.

Part: SKIN — CRACKED (RT WING) · airframe 22,381 hrs · 19,038 cycles

CRACK FOUND ON RT WING, AFT OF LANDING EDGE AT WS 343, BTWN ACCESS PANEL 603 LZ AND 630 KZ. (K) RT WING L/E ON THE REAR SIDE AT WEB FABRICATED IAW SRM 51-24-16. RT WING L/E ON THE REAR SIDE AT WS 343 WEB INSTALLED IAW SRM 51-42-13. (A)

Part: FRAME — CRACKED (BS 280) · airframe 22,381 hrs · 19,038 cycles

CRACK EXIST ON FRAME FS 280 RBL 9. (M) PILOTS BULKHEAD AT FS 280.00 RBL 9 REPAIRED IAW REO 601R-53-11-171 REV "D". (A)

Part: SILL — CRACKED (FUSELAGE) · airframe 22,381 hrs · 19,038 cycles

CRACK EXISTS ON LOWER SILL OF CARGO DOOR FS 574 LBL 45. NEW SILL CARGO DOOR FS 574 LBL 45 INSTALLED IAW REO 601R-53-61-690 REV D. (A)

Part: BULKHEAD — CRACKED (BS 280) · airframe 22,381 hrs · 19,038 cycles

CRACK EXISTS ON PILOT BULKHEAD FS 280 LBL 9 WL 71. (M) PILOTS BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV "D". (A)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 22,381 hrs · 19,038 cycles

FOUND CRACK ON INTERCOSTAL FS 484 AND LBL 36. (M) INTERCOSTAL REPAIRED IAW REO 601R-53-41-059 REV A.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 22,381 hrs · 19,038 cycles

CRACK EXIST ON ANGLE OF INTERCOSTAL FS 484, RBL 27. (M) NEW ANGLE INSTALLED IAW SRM 51-42-20 .

Part: STRUCTURE — GOUGED (BS 625) · airframe 22,381 hrs · 19,038 cycles

GOUGE FOUND ON VERTICAL Z MEMBER AT FS 625 BL 0 WL 136. - - VERTICAL 2 MEMBER AT FS 625 BL O WL 136 REPAIRED IAW REO 601R-53-61-2573. . (A)

Part: CHANNEL — CRACKED (BS 574) · airframe 22,381 hrs · 19,038 cycles

CRACK FOUND CARGO DOOR SURROUNDING STRUCTURE CHANNEL AT FS 574 WL 79 LBL 45. (M) REPLACED IAW SRM 51-42-06. (A)

Part: BULKHEAD — CRACKED (BS 202) · airframe 22,381 hrs · 19,038 cycles

CRACK FOUND ON PRESSURE BULKHEAD FSW 202.75, LBL 23.71, AROUND PARKING BRAKE. (K) REPAIR ON FWD PRESSURE BULKHEAD IAW REO 601R-53-11-563.

Part: SUPPORT — CRACKED (EXTERNAL POWER) · airframe 22,016 hrs · 18,671 cycles

AC EXTERNAL POWER CONNECTOR BOX SUPPORT MEMBER BTW FS 193.00 - 202.00 RT SIDE IS CRACKED AT TOP FWD AND LWR AFT ATTACHMENT POINTS. TOP FWD AND LWR AFT CRACKS IN SUPPORT MEMBER TEMPORARILY REPAIRED IAW REO 601R-24-41-002 PERMANENT REPAIR TO BE CARRIED OUT AT NEXT C-CHECK SCHEDULED 3/8/08. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,016 hrs · 18,671 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 AT LINTEL FITTING AREA. AFT PRESSURE BULKHEAD AT FS 621.00 AT LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (K)

Part: TRANSDUCER — FLUCTUATES (RT ENGINE)

AT FL320, RECEIVED ENGINE NR 2 LOP PRESS FLUCTUATED 32-38 PSI, DIVERTED TO PIT, ENGINE WAS NOT SHUTDOWN, COMPLIED WITH QRH, OIL PRESSURE INCREASED AS ALTITUDE DECREASED (44 PSI MAX). REMOVED AND REPLACED OIL PRESSURE, RAN ENGINE NR 2 FOR OIL PRESSURE. NO DEFECTS OR FLUCTUATIONS ON OIL INDICATION. (M)

Part: POST — CRACKED (BS 409)

FOUND BULKHEAD POST AT FS 409 PLUS 128, RBL 18 LOWER OUTBOARD RIVET HOLE IS CRACKED APPROXIMATELY .25 INCH LONG. MAINTENANCE TRIMMED OUT CRACKED PORTION OF STIFFENER AND REPAIRED WITH A REPAIRED WITH A REPAIR ANGLE IAW BOMBARDIER AEROSPACE REO-601-53-41-056. (M)

Part: RIB — CRACKED (LWS 53)

FOUND LEFT WS 53.60 BATTERY RIB ASSEMBLY IS CRACKED 2 INCH LONG IN UPPER CORNER. MAINTENANCE REPAIRED CARRIED OUT IAW REO 601R-57-51-046. (M)

Part: BULKHEAD — CRACKED (BS 559)

FOUND BULKHEAD POST CRACKED APPROX 1 INCH LONG AT FS 559.0 RBL 9.00 OUTBOARD SIDE BOTTOM ON AFT SIDE OF BULKHEAD. MAINTENANCE REPAIRED POST AT FS 559.00 RBL 9.00 OUTBOARD SIDE BOTTOM IAW BOMBARDIER REO 601R-53-41-057. (M)

Part: ATTACH ANGLE — CRACKED (LT WING)

FOUND LEFT WING LEADING EDGE SPAR ATTACH ANGLE FOR THE INBOARD END OF THE MIDDLE LEADING EDGE SECTION IS CRACKED AT LOWER CORNER 1.0 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT WING L/E SPAR ATTACH ANGLE IAW CRJ200 SRM 51-41-00 BY INSTALLING SOME SERVICEABLE BOLTS. (M)

Part: ATTACH ANGLE — CRACKED (RT WING)

FOUND RIGHT WING LEADING EDGE SPAR ATTACH ANGLE FOR THE OUTBOARD END OF THE INBOARD LEADING EDGE SECTION IS CRACKED AT LOWER CORNER 1.0 INCH LONG (P/N 600-12025-8). MAINTENANCE REMOVED AND REPLACED ANGLE P/N 600-12025-8 IAW CRJ AMM 20-21-00-910-801 AND 57-41-01-400-803. (M)

Part: FLAP — MALFUNCTIONED (WING)

FLAP FAIL CAS AFTER DEPARTURE FLAPS AT 8 DEGREES. REMOVED AND REPLACED RT BPSU, OPS CHECK GOOD IAW AMM 27-51-10. (M)

Part: SEAL — LACK OF LUBE (SERVICE DOOR)

RIGHT FORWARD EXIT DOOR DIFFICULT TO OPEN. CLEANED AND LUBRICATED SERVICE DOOR SEAL AS REQUIRED, OPS CHECK GOOD, IAW CRJ MM 52-41-02. (M)

Part: HANDLE — UNLATCHED (PAX DOOR) · airframe 17,885 hrs · 14,717 cycles

ON CLIMB OUT (OUTER PAX DOOR HANDLE UNSTOWED MESSAGE) FOLLOWED BY DEPRESURIZATION. UPON RETURN TO GATE FOUND L1 DOOR HANDLE IN UNLATCHED POSITION. INSPECTED DOOR IAW AMM, NO DEFECTS NOTED. REF 152478/3 FOR PRESSURIZATION CHECK. REF 152478/3- PERFORMED PRESS CHECKS, NO DEFECTS NOTED. (K)

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS)

MISCONFIG MASTER WARNING MESSAGE, FLIGHT SPOILER AND GROUND SPOILER CAUTION MESSAGES DURING TAKEOFF. ABORTED TAKEOFF AT 40 KNOTS IAS, ALL MTMS IN GREEN. PERFORMED BITE CHECK ON SECU, NO FAULT NOTED. COMPLIED WITH RESET. PROCEDURES IAW CRJ FIM, RESET NORMAL. OK FOR CONTINUED SERVICE IAW AMM CRJ 27-61-00, OPS CHECK GOOD. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,475 hrs · 14,316 cycles

AFT ATTACHMENT ANGLE FOR CARGO NET BEAM IS CRACKED APPROX 2 INCHES IN RADIUS AT AFT PRESSURE BULKHEAD. CORRECTIVE ACTION IN PROGRESS. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,475 hrs · 14,316 cycles

LT AND RT INTERCOSTAL ANGLES (OBLIQUES) AT FS 625 ARE CRACKED .5 INCH LONG. CORRECTIVE ACTION IN PROGRESS. (K)

Part: ACM — SEIZED (LEFT) · airframe 17,020 hrs · 13,895 cycles

ON APPROACH GOT OIL TYPE SMELL FROM LT PACK, AND LT PACK OVERHEATED IN AUTO MODE. WHILE ON GROUND WAS UNABLE TO CONTROL LT PACK IN MANUAL MODE. INSPECTED LT PACK AND FOUND ACM SEIZED AND TO BE THE SOURCE OF THE OIL SMELL. REMOVED AND REPLACED AIR CYCLE MACHINE. (NO FURTHER OCCURRENCES). (K)A6WA200540335

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 15,135 hrs · 12,160 cycles

UPON FINAL APPROACH EXTENDED GEAR RECEIVED HYD 3 LO PRESSURE CAUTION MESSAGE. ASSOC WITH GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. EXECUTED GO AROUND. GEAR CAME UP AFTER ABOUT A MINUTE. RAN ASSOCIATED QRH PUT GEAR DOWN. ALL NORMAL. REMOVED AND REPLACED ENGINE DRIVEN MOTOR PUMP 3B. (K)

Part: COMPUTER — MALFUNCTIONED (AVIONICS BAY)

CAPTAINS SIDE 'RED MAG' INDICATION ON PFD1 PRIOR TO TAKEOFF. TAKEOFF ABORTED, AIRSPEED LESS THAN 40 KNOTS. REMOVED AND REPLACED AHRS NR 1 UNIT IAW/AMM 34-21-01, OPS CHECK GOOD. (M)

Part: HANDLE — STUCK (ESCAPE HATCH)

CREW ESCAPE HATCH OUTER HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC 33. (M)

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH)

CREW ESCAPE HATCH OUT HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC33. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTROLABLE EVEN WHEN SELECTED TO FLIGHT IDLE. COMPLIED WITH QRH, ENGINE SHUTDOWN. TAT -41C ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENGINE STATOR, GROUND RAN. ALL ENGINE INDICATIONS WITHIN LIMITS. IAW FIM 72-00-00, PG 1305.

Part: INDICATOR — MALFUNCTIONED (NR 2 ENGINE)

DURING CRUISE, NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTOLLABLE EVEN WHEN SELECTED TO FIGHT IDLE. COMPLIED WITH QRH ENGINE SHUTDOWN. TAT 41 DEGREES CELCIUS. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED ALTERNATOR AND STATOR, N2 INDICATING, IAW AMM 73-21-07, OPS CHECK DURING GROUND RUN NORMAL. (M)

Part: DRIVE ASSY — FAILED (TE FLAPS)

FOUND FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. REMOVED AND REPLACED 1 FLEX DRIVE CABLE AND 2 BPSU IAW MM 27-51-10. PERFORMED RIGGING AND OPS CHECK. OPS CHECK GOOD, S/N 5310, 0857.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. (M)

Part: SKIN — LIGHTNING STRIKE (RT ELEVATOR)

FOUND DAMAGE ON RIGHT ELEVATOR UPPER SKIN CAUSED BY LIGHTNING STRIKE. REPAIRED BY PERFORMING WVAC EO NR 601R-55-4418. BLENDED AREA, PERFORMED NDI EDDY CURRENT AND APPLIED PROTECTIVE TREATMENT. (M)

Part: SKIN — LIGHTNING STRIKE (ELEVATOR)

FOUND DAMGE ON RIGHT ELEVATOR UPPER SKIN CAUSED BY LIGHTNING STRIKE. REPAIRED BY PERFORMING WVAC EO NR 601R-55-4418. BLENDED AREA, PERFORMED NDT EDDY CURRENT AND APPLIED PROTECTIVE TREATMENT. (M)

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

AFTER TAKEOFF ON GEAR RETRACTION GOT RED GEAR DISAGREE AND RED NOSE GEAR DOORS CAS MESSAGE. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY. OPS AND LEAK CHECK GOOD. (M)

Part: GENERATOR — FAILED (NR 2)

ADG DEPLOYED IN FLIGHT AUTOMATICALLY WHEN GEN 1 WAS MANUALLY SHUT OFF WITH GEN 2 OFF LINE STOWED ADG. SQUIB FIRED. REPLACEMENT NOT AVAILABLE. AUTO DEPLOY FUNCTION PLACED ON MEL.

Part: ACCESS PANEL — MISSING (EXHAUST NOZZLE)

DURING REMOVAL AND REPLACEMENT OF LEFT LOGO LIGHT, NOTICED ACCESS PANEL MISSING ON INBOARD SIDE OF EXHAUST NOZZLE. REMOVED AND REPLACED LEFT ENGINE EXHAUST NOZZLE. (M)

Part: OVERHEAT LOOP — FAULTY (LT ENGINE)

LEFT 14TH DUCT WARNING IN FLIGHT, REDUCED POWER PER QRH, MESSAGE DISAPPEARED, ON DESCENT AT REDUCED POWER MESSAGE RETURNED, PERFORMED PRECAUTIONARY SHUTDOWN PER QRH. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE 14TH STAGE PYLON OVERHEAT DETECTION LOOP. (M)

Part: ANGLE — CHAFED (FUSELAGE)

WHILE PERFORMING SB 601R-53-059 FOUND BL0 BULKHEAD Z-MEMBER TO HAVE A CHAFE IN THE RADIOUS APPROX 12 INCHES FROM TOP AT FS 624. REPAIRED Z-MEMBER AT BL0, FS 624 IAW WEST VIRGINIA AIR CENTER EO NR 601R-53-3674A. (M)

Part: SKIN — CHAFED (FLAP VANE)

LEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT STOP CONTACT POINTS IN 3 PLACED, .010 IN TO .040 IN DEEP PERFORMED A MAJOR REPAIR TO THE LEFT INBOARD FLAP VANE LEADING EDGE IAW WVAC EO 601R-57-3659B. (M)

Part: SKIN — CHAFED (FLAP VANE)

THE RIGHT INBOARD FLAP LEADING EDGE VANE CAP INBOARD SKIN IS CHAFED (WHERE THE INBOARD VANE CAP RESTS ON THE BUMPER PADS/TEFLON STOPS. REMOVED CHAFED VANE CAP. FABRICATED AND INSTALLED A NEW VANE CAP IAW WVAC EO 601R-57-3659B. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

MWD 131 AND 132 THE ATTACH ANGLES ON THE INTERCOSTAL AT FS 484, BL 27 LEFT AND RIGHT WERE FOUND CRACKED. THE CRACKED ANGLES WERE REMOVED. NEW (REPAIR) ANGLES WERE FABRICATED AND INSTALLED IAW WVAC EO 601R-53-3663. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 6,739 hrs · 5,170 cycles

EN ROUTE THE PAX DOOR HANDLE CAUTION ILLUMINATED. PRESSURIZATION WAS NORMAL. WHILE C/W CHECKLIST THE PAX DOOR WARNING ILLUMINATED AS PRESSURIZATION WAS MANUALLY REDUCED, WARNING CHANGED BACK TO CAUTION. MAINTENANCE INSPECTED DOOR AND LOCKING MECHANISMS. NO DEFECTS NOTED. OPERATED DOOR 5 TIMES IAW MM 52-11-00, OK FOR SERVICE.

Part: GENERATOR — FAILED (NR 1)

NR 1 GENERATOR FAILS IN-FLIGHT. DURING TROUBLESHOOTING OF NR 1 GENERATOR, MAINTENANCE FOUND EVIDENCE THAT TERMINAL BLOCK GB209 (ENGINE TO AIRFRAME) AND WIRE NR 2XA73A4ORN WERE BURNT. NR 1 GENERATOR PLACED ON MEL AND ISOLATED THE DAMAGED TERMINAL BLOCK AND WIRE. (ATW). (X)