N413AW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,366 hrs · 42,103 cycles

LOW SPEED ABORT FOR IDG 2 CAUTION MSG CLEARED WHEN POWER REDUCED. ******AIRCRAFT REMOVED FROM SERVICE******** C/W M ACTION FOR MEL 24-11-01-01 REF 363019/2 FOR MEL. T.S. PER FIM 24-10-00. FOUND #2 IDG OIL LEVEL LOW. PERFORMED LEAK CHECK OF RH IDG OIL SYSTEM. REF AMM 24-12-00-210-803. NO EVIDENCE OF LEAKS NOTED. SERVICED RH IDG AND PERFORMED OPS/LEAK CHECKS. ALL CHECKS GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: EEC — UNKNOWN (FLAPS) · airframe 44,070 hrs · 41,780 cycles

FLAP FAIL CAUTION MESSAGE ON APPROACH WHEN EXTENDING TO 45 DEGREES. GAUGS INDICATED 45 DEGREES. QRH C/W AND NORMAL LANDING. PREFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ******AIRCRAFT REMOVED FROM SERVICE********** TROUBLE SHOT IAW FIM 27-50-00. FOUND FECU MOST LIKELY AT FAULT. R&R FECU IAW AMM 27-51-05-04. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,946 hrs · 41,650 cycles

ON TO RCVD GEAR DISAGREE AND NLG DOOR OPEN WARNING MSGS C/W QRH FOR NLG DOOR OPEN BOTH MSGS DISAPPEARED. RETURNED DAYTON.NO EMER DECLARED. **********AIRCRAFT REMOVED FROM SERVICE********* SERV NLG IAW AMM 12-12--32-03 AND AWAC SUP 09-055 PERF GEAR SWING OPS CK GOOD

Part: ENGINE — DAMAGED (RIGHT) · airframe 43,902 hrs · 41,598 cycles

ITT ON RIGHT ENGINE INCREASED TO 840C ON 85% N1 ON BOTH ENGINES, WITH VIBRATIONS AT FLIGHT LEVEL 190. REDUCED POWER VIBRATION ON N2 TWICE FOR 1 SEC EACH. AND N1 VIBE AT 2.7MIL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RH ENGINE COLD SECTION STAGES ON THROUGH TEN PER AMM 72-00. FOUND STAGE SIX MISSING A BLADE. STAGE FIVE SPINDLES THROUGH STAGE TEN BLADES ALL HAVE DAMAGE FROM LOOSE BLADE GOING THROUGH COMPRESSOR SECTION. R&R RH ENGINE.

Part: NONE — NONE · airframe 42,022 hrs · 39,739 cycles

ON T/O RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSG'S. C/W QRH LOWERED GEAR AND RETURNED TO FIELD. AFTER SELECTING HANDLE UP WARNING CAME ON IMMEDIATELY. RECEIVED INBD A-SKID AND NWS INOP MSG'S BRIEFLY. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS CHECK GOOD. REMOVED PLACARD REMOVED FROM MEL P/N: 750006000, S/N OFF: 1945, S/N ON: 0365T ARW

Part: NONE — NONE · airframe 42,019 hrs · 39,735 cycles

AFTER SELECTING LANDING GEAR UP, GOT GEAR DISAGREE MSG, C/W QRH LANDING GEAR DOWN 3 GREENS. NLG DID NOT COME UP. RETURNED TO ORIGINATING AIRPORT. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS CHECK GOOD. REMOVED PLACARD REMOVED FROM MEL P/N: 750006000, S/N OFF: 1945, S/N ON: 0365T ARW

Part: CONTROL UNIT — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 40,981 hrs · 38,640 cycles

RECEIVED LT AND RT WING ANTI-ICE CAUTION MESSAGES DURING CRUISE. C/W QRH, MESSAGES PERSISTED. WING ANTI-ICE ON ADVISORY MESSAGE NOT PRESENT. DIVERTED TO PIT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TEMP CONTROL UNIT, IAW AMM 30-12-19. OPERATIONS CHECK GOOD. P/N 1151336-1, S/N OFF 103C-1687, S/N ON 021C-0711. - LN.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 40,922 hrs · 38,581 cycles

PAX DOOR UPPER STEP PLATFORM TO SILL HINGE CORRODED. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND DRILLED NEW HINGE. REMOVED AND REPLACED UPPER STEP PLATFORM TO HINGE, IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 40,922 hrs · 38,581 cycles

CABIN FLOOR SEAT TRACK CORRODED AT LBL 9 FS 364 THRU FS 409. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK. INSTALL NEW SEAT TRACK AT LBL 9.00 FS 364 THRU FS 409, IAW REO 601R-53-00-764.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 40,922 hrs · 38,581 cycles

CABIN FLOOR SEAT TRACK AT RIGHT BUTT LINE 9 FS 364-FS 409. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW REO-601R-53-00-764 REPAIR B STEP 1.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 40,922 hrs · 38,581 cycles

CABIN FLOOR SEAT TRACK CORRODED AT LBL 9 FS 409 THRU FS 559. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SEAT TRACK, PER REO 601R-53-00-764 REPAIR B STEP 1.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 39,568 hrs · 37,251 cycles

SERVICE DOOR UPPER FORWARD CORNER INNER SKIN DAMAGED. REPAIRED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,979 hrs · 36,674 cycles

INTERCOSTAL IS CORRODED JUST AFT OF FS 310 FRAME AT STGR 21L.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 38,979 hrs · 36,674 cycles

PAX DOOR HINGE ON FUSELAGE SIDE HAS MULTIPLE HOLES OUT OF ROUND.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,979 hrs · 36,674 cycles

SERVICE DOOR LOWER FLOOR SILL ANGLE IS CORRODED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,979 hrs · 36,674 cycles

LT PRESSURE FLOOR SILL IS CORRODED AT F.S.449.85.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,979 hrs · 36,674 cycles

FS 333.00 FRAME IS CRACKED AT STRINGER 0.

Part: FLOOR SUPPORT — CORRODED (FS 559) · airframe 38,979 hrs · 36,674 cycles

LH FLOORBOARD SUPPORT ANGLE OVER THE PRESSURE FLOOR SILL IS CORRODED AT FS 559.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 38,979 hrs · 36,674 cycles

LH FWD EQUIPMENT COMPARTMENT FLOOR IS CRACKED AT FS 193.00.

Part: VALVE — LEAKING (APU) · airframe 38,548 hrs · 36,265 cycles

ON APPROACH APPROXIMATELY 10 MINUTES AFTER APU START WITH LCV OPEN RECEIVED FUEL SMELL IN COCKPIT. ON GROUND APU DOOR SHOWED DASHES. BOTH PACKS RUNNING WITH BLEEDS ON ENGINES. AFTER APU SHUTDOWN SMELL WENT AWAY. INSPECTED AND FOUND FUEL SHUTOFF VALVE/SOLENOID LEAKING AROUND VALVE BODY. REMOVED AND REPLACED APU FUEL VALVE/SOLENOID IAW AMM 49-31-05, SUPP 10-023A. OPS AND LEAK CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: WIRE HARNESS — CRUSHED (NLG) · airframe 37,903 hrs · 35,662 cycles

UPON SELECTING LANDING GEAR UP RECEIVED GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING MESSAGES. C/W QRH MESSAGES CLEARED ON GEAR EXTENSION PLAN TO CHANGE CRUSHED NLG HARNESS.

Part: WIRE HARNESS — CRUSHED (NLG) · airframe 37,903 hrs · 35,662 cycles

UPON SELECTING LANDING GEAR UP RECEIVED GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING MESSAGES C/W QRH MESSAGES CLEARED ON GEAR EXTENSION. PLAN TO CHANGE CRUSHED NLG HARNESS.

Part: CONTROL UNIT — MALFUNCTIONED (ADG) · airframe 37,123 hrs · 34,873 cycles

AFTER TAKEOFF, THE AIR DRIVEN GENERATOR DEPLOYED UNCOMMANDED. COMPLIED WITH QRH, GENERATORS DID NOT PICK UP THE LOAD, AND POWER TRANSFER OVERRIDE SWITCH DID NOT WORK. DIVERTED. THE GENERATOR TRANSFER OCCURRED BELOW 80 KNOTS AFTER LANDING. REPLACED ADG AUTO DEPLOY CONTROL PANEL UNIT. CHECKED GOOD. REPLACED CONTROL PANEL CONNECTOR.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 35,569 hrs · 33,404 cycles

3843 ON APPROACH SWITCHING FROM NAV TO HEADING TO APPROACH MODE A/C TRIED TO CLIMB IN PITCH MODE WITH AUTO PILOT ON FOLLOWED BY C-CORD AURAL ALERT TURNED AUTO PILOT OFF AND BACK ON A/C BEGAN TO CLIMB IN PITCH MODE AGAIN. AUTO PILOT DISCONTINUED FOR APPROACH. AURAL WARNING CONTINUED BOTH PFD'S SHOWED MATCHING DATA, A/C SEEMED NORMAL AND CONTROLLABLE REF MXC QRH FOR DCU DISAGREEMENT NO DISSIMILAR MSGS SHOWN APR AND CAS MIS COMP MSGS. INFLIGHT ONLY CAS MIS COMP ONLY MSG DISPLAYED. F/O NOTICED AT ONE POINT ALT HEADING HAD DROPPED AFTER CORRECTING AURAL ALERT CONTINUED BUT A/C HANDLED NORMALLY WITH AUTO PILOT ENGAGED. ON GROUND WITH AUTOPILOT DISCONNECTED NO AURAL WARNING PRESENT AND NO CAS MISCOMP CAUTION PRESENT. WITH AUTOPILOT ENGAGED AIRCRAFT GOES LWD WITH AP TRIM IS LWD CAUTION WITH NO MODES SELECTED. FCC INPUT MODE SHOWS CRSDAT L-79.4 R-35.4 R&R FCP IAW AMM 22-11-07 NO FIX, REINSTALLED ORIGINAL FCP.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 35,569 hrs · 33,404 cycles

ON APPRACH SWITCHING FROM NAV TO HEADING TO APPROACH MODE A/C TRYED TO CLIMB IN PITCH MODE WITH AUTO PILOT ON FOLLOWED BY C-CORD AURAL ALERT TURNED AUTO PILOT OFF AND BACK ON A/C BEGAN TO CLIMB IN PITCH MODE AGAIN. AUTO PILOT DISCONTINUED FOR APPROACH. AURAL WARNING CONTINUED BOTH PFD'S SHOWED MATCHING DATA,A/C SEEMED NORMAL AND CONTROLLABLE REF MXC QRH FOR DCU DISAGREEMENT NO DISSIMILAR MSGS SHOWN APR AND CAS MIS COMP MSGS. INFLIGHT ONLY CAS MIS COMP ONLY MSG DISPLAYED. F/O NOTICED AT ONE POINT ALT HEADING HAD DROPPED AFTER CORRECTING AURAL ALERT CONTINUED BUT A/C HANDLED NORMALY WITH AUTO PILOT ENGAGED. ON GROUND WITH AUTOPILOT DISCONNECTED NO AURAL WARNING PRESENT AND NO CAS MISCOMP CAUTION PRESENT. WITH AUTOPILOT ENGAGED AIRCRAFT GOES LWD WITH AP TRIM IS LWD CAUTION WITH NO MODES SELECTED. FCC INPUT MODE SHOWS CRSDAT L-79.4 R-35.4 R&R FCP IAW AMM 22-11-07 NO FIX, REINSTALLED ORIGINAL FCP.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 36,640 hrs · 34,383 cycles

RECEIVED AN UNCOMMANDED YAW IN FLIGHT, 2 BALL WIDTHS ON THE SIDE SLIP INDICATOR. COMPLIEC WITH QRH. YD 1 AND 2 OFF UNCOMMANDED YAW CONTINUED FOR 10 MINUTES THEN CLEARED. COULD FEEL YAW MOTION IN RUDDER PEDALS. REMOVED AND REPLACED THE NR 1 YAW DAMPER ACTUATOR IAW AMM 22-22. OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 605) · airframe 36,534 hrs · 34,280 cycles

FOUND A DENT UNDER CARGO DOOR. BS 605 FRAME WAS CRACKED

Part: UNKNOWN — ODOR (A/C PACK) · airframe 35,850 hrs · 33,640 cycles

STRONG BURNING ODOR FROM PACKS, WHILE ON APU BLEED, RIGHT AFTER TAKEOFF, IN CABIN AND COCKPIT.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 35,694 hrs · 35,502 cycles

TWO NUT PLATE LOCATIONS ON THE FLOORBEAM CORRODED AT LBL 27, BS 559+90 TO 559+112. REPAIRED THE FLOORBEAM IAW SRM 53-00-43, REPAIR 2.

Part: SKIN — CHAFED (BS 544-559) · airframe 35,694 hrs · 35,502 cycles

FOUND CHAFE DAMAGE THAT EXCEED ALLOWABLE LIMITS IAW EO E16/011/453 REV:A ON RT APRON SKIN PANEL.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 35,694 hrs · 35,502 cycles

LEFT OTBD FLOOR SUPPORT CORRODED AT BS 559+80 TO 559+112. REMOVER AND REPLACED THE FLOOR SUPPORT IAW EA 253-00638 REV-IR.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,694 hrs · 35,502 cycles

RIGHT INBD FLAP VANE LE CHAFED IN MULTIPLE AREAS. REPLACED THE FLAP VANE.

Part: SKIN — DENTED (RUDDER) · airframe 35,694 hrs · 35,502 cycles

RUDDER IS DENTED ON RT SIDE. REPAIRED IAW SRM 55-40-00.

Part: DOUBLER — CORRODED (BS 310) · corrosion level 2 · airframe 35,694 hrs · 35,502 cycles

AFT INBD DOUBLER ON WARDROBE IS CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-10.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,694 hrs · 35,502 cycles

LT WING TE FLAP VANE CTR LE IS CHAFED.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,694 hrs · 35,502 cycles

LEFT WING TE FLAP VANE IS CHAFED

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 35,694 hrs · 35,502 cycles

1013972-3000-0023 - INTERCOSTAL AT STGR 13L AND FS 625 IS CRACKED

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 35,694 hrs · 35,502 cycles

INTERCOSTAL AT STRINGER 14L, BS 625 CRACKED.

Part: SEAT TRACK — CORRODED (BS 394-409) · corrosion level 2 · airframe 35,694 hrs · 35,502 cycles

RIGHT AISLE SEAT TRACK NR 2 HAS CORROSION BETWEEN BS 394 THRU 409+128

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 35,694 hrs · 35,502 cycles

LEFT AISLE SEAT TRACK NR 3 HAS CORROSION AND IS GOUGED BETWEEN BS 409+128 AND 559.

Part: ANGLE — CRACKED (BS 280) · airframe 35,694 hrs · 35,502 cycles

ANGLE ON THE OTBD SIDE OF RBL 9 AND AFT SIDE OF FLOORBEAM BS 280 IS CRACKED

Part: ANGLE — CRACKED (BS 473) · airframe 35,694 hrs · 35,502 cycles

ANGLE INBD SIDE OF RBL 36 AT BS 473.15 CRACKED. REPLACED THE ANGLE.

Part: BRACKET — CRACKED · airframe 35,694 hrs · 35,502 cycles

STANDOFF BRACKET AT 7 O'CLOCK POSITION ON RH ENGINE NOSE INLET COWL

Part: BRACKET — CRACKED · airframe 35,694 hrs · 35,502 cycles

STANDOFF BRACKET AT 8 O'CLOCK POSITION ON LH ENGINE NOSE INLET COWL IS CRACKED

Part: DOOR — BINDING (SERVICE) · airframe 35,494 hrs · 33,341 cycles

SERVICE DOOR IS DIFFICULT TO OPEN FROM INSIDE.

Part: ENGINE — UNSERVICEABLE (RIGHT) · airframe 35,428 hrs · 33,287 cycles

APROXIMATELY 10500 FT, HEARD A LOUD BANG WITH VIBRATION. RT ENGINE ITT PEGGED. RETARDED THROTTLE ITT REMAINED PEGGED. CW QRH FOR SEVERE ENGINE DAMAGE. ENGINE WAS SHUT DOWN BY FLIGHT CREW. DIVERTED TO LGA. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. LANDING WEIGHT 49,000 LBS. LANDING WAS SMOOTH AND NORMAL. MAX BTMS READING WERE 8,7,6,6

Part: TORQUE LINK — NOT REPORTED (NLG) · airframe 34,472 hrs · 32,419 cycles

ABORTED TAKEOFF DUE TO STRONG PULL TO THE RIGHT. BTMS READS 4,5,3,2. ABORTED AT 50 KNOTS. REMOVED AND REPLACED NLG LOWER TORQUE LINK IAW AMM 32-21-10 AND AWAC SUP 10-102. TAXI CHECK WITH CREW GOOD AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 34,472 hrs · 32,419 cycles

GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR OPEN WARNING MESSAGE AFTER GEAR SELECTED UP. NOSE GEAR REMAINED DOWN. NWS CAUTION MESSAGE. COMPLIED WITH QRH.

Part: WARNING MESSAGE — MULTIPLE FAIL (MLG) · airframe 34,472 hrs · 32,418 cycles

AFTER TAKEOFF, SELECTED GEAR UP AND RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. NLG WAS DOWN AT THE TIME. WITHIN 6 SECONDS OF GEAR UP SLECTION. ALSO RECEIVED STEERING INOPERATIVE, WOW INPUT AND WOW OUTPUT CAUTION MESSAGES. COMPLIED WITH THE QRH, AND SLECTED NR 2BH AND 3B HYD PUMPS ON, NO CHANGE. SELECTED ALTERNATE EXTENSION, GEAR SHOWED ALL 3 GREEN. MESSAGES CLEARED EXCEPT STEERING INOPERATIVE AND WOW INPUT. MC SELECTED NORMAL GEAR HANDLE DOWN, LANDED WITHOUT INCIDENT AND AFTER A COMPLETE STOP CYCLED THE NOSE GEAR STEERING SELECTOR SWITCH. ALL MESSAGES CLEARED. TAXIED TO GATE.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 33,968 hrs · 31,944 cycles

3790 CLIMBING OUT AROUND 7000 FT, RECEIVED PAX DOOR OUTER HANDLE CAUTION MSG. COMPLIED WITH ARH, FLIGHT ATTENDANT REPORTED HANDLE LOCK INDICATOR SHOWED RED. DIVERTED, LANDED AT 46,500 LBS, BRAKING WAS NORMAL. GND CREW REPORTS HANDLE WAS POPPED OUT UPON ARRIVAL. INSPECTED PAX DOOR OUTER HANDLE, NO DEFECTS FOUND. COMPLIED WITH OPERATIONS TEST OF PAX DOOR OUTER HANDLE. DOOR OPENS, CLOSES & LOCKS IN PROPER FASHION. ALL WITNESS MARKS ALIGN CORRECTLY IAW AMM 52-11-03. OPERATIONS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (DOOR HANDLE) · airframe 33,968 hrs · 31,944 cycles

CLIMBING OUT AROUND 7000 FT, RECEIVED OAX DOOR OUTER HANDLE CAUTION MESSAGE. C/W ARH, F/A REPORTED HANDLE LOCK INDICATOR SHOWED RED. DIVERTED, LANDED AT 46,500 LBS BRAKING WAS NORMAL. GROUND CREW REPORTS HANDLE WAS POPPED OUT UPON ARRIVAL. INSPECTED PASSENGER DOOR OUTER HANDLE NO DEFECTS FOUND. CW OPS TEST OF PASSENGER DOOR OUTER HANDLE. DOOR OPENS, CLOSES LOCKS IN PROPER FASHION ALL WITNESS MARKS ALIGN CORRECTLY IAW AMM 52-11-03. OPS CK GOOD.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 33,968 hrs · 31,944 cycles

CLIMBING OUT AROUND 7000 FT, RECEIVED PAX DOOR OUTER HANDLE CAUTION MSG. COMPLIED WITH QRH, FLIGHT ATTENDANT REPORTED HANDLE LOCK INDICATOR SHOWED RED. DIVERTED & LANDED AT 46,500 LBS. BRAKING WAS NORMAL. GND CREW REPORTS HANDLE WAS POPPED OUT UPON ARRIVAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,459 hrs · 31,466 cycles

FRONT ORANGE FLOOR TRACK EMER LIGHT NOT WORKING, ALL OTHERS ARE WORKING.

Part: APU — SHUTDOWN (APU BAY) · airframe 32,154 hrs · 30,217 cycles

APU FAULT MSG, AFTER TAKEOFF APU AUTO SHUTDOWN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 31,854 hrs · 29,928 cycles

ANTI-SKID INBD & OTBD MSGS CAME ON WHEN LANDING GEAR WAS LOWERED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,231 hrs · 29,336 cycles

CAPTAIN`S WINDSHIELD CRACKED AT CRUISE AFTER RECEIVING WINDSHIELD HEAT CAUTION MSG. EMERGENCY DECLARED & ACFT DIVERTED. R & R CAPTAIN`S WINDSHIELD IAW AMM 56-11-01. OPS & LEAK CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 31,192 hrs · 29,296 cycles

FWD ATTACH ANGLE FOR LT BATTERY RIB IS CRACKED.

Part: SUPPORT — CRACKED (TAIL PIPE) · airframe 31,192 hrs · 29,296 cycles

LEFT TAIL PIPE FAIRING NR 3 SUPPORT HAS CRACK NEAR 8 POSITION.

Part: DOOR SILL — DAMAGED (FUSELAGE) · airframe 31,192 hrs · 29,296 cycles

HOLE IN RT OTBD FLOOR SILL NEAR FS 409+96.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,192 hrs · 29,296 cycles

CORROSION ON RT OTBD FLOOR SILL NEAR FS 320.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,192 hrs · 29,296 cycles

SEVEN SEAT TRACKS CORRODED IN CARGO BAY.

Part: MOUNT BRACKET — CRACKED (LT WING) · airframe 31,193 hrs · 29,296 cycles

LEFT WING LE UPPER MOUNT BRACKET FOR DE-ICE DUCT TRANSITION PANEL IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,193 hrs · 29,296 cycles

LOWER U BRACKET CRACKED AT FS 574, TIE IN FOR CARGO DOOR TRACK SUPPORT.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 31,193 hrs · 29,296 cycles

LT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,193 hrs · 29,296 cycles

RIGHT UPPER OBLIQUE ANGLE CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 31,193 hrs · 29,296 cycles

RIGHT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 31,193 hrs · 29,296 cycles

LEFT MLG WW BRAKE VOLUMETRIC FUSE FWD MOUNT BRACKET IS CRACKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,193 hrs · 29,296 cycles

STRINGER ATTACH ANGLES CRACKED STRINGER 3L & FS 280.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,193 hrs · 29,296 cycles

PAX DOOR LOWER SILL FLOOR SUPPORT LOWER ANGLE CORRODED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,193 hrs · 29,296 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED ON LOWER FLANGE AT LBL 11.

Part: SKIN — DENTED (TE FLAP) · airframe 31,193 hrs · 29,296 cycles

LEFT INBD FLAP LOWER SKIN DENTED.

Part: PLATE — CRACKED (FUSELAGE) · airframe 31,193 hrs · 29,296 cycles

CARGO DOOR FLOOR SILL LANDING PLATE CRACKED AT FLOORBEAM AT FS 589.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,193 hrs · 29,296 cycles

CORROSION ON THE FS 349 FLOOR SUPPORT AT RBL 30 TO 42.

Part: RECEPTACLE — DAMAGED (EXTERNAL POWER) · airframe 31,054 hrs · 29,167 cycles

EXTERNAL POWER OUTLET DAMAGE, RECEPTACLE.

Part: WARNING MESSAGE — ACTIVATED (LANDING GEAR) · airframe 30,930 hrs · 29,049 cycles

AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING MESSAGE. NLG INDICATED DOWN, LOCKED & GREEN. LT & RT MLG UP, LOCKED, WHITE. GEAR LEVER IN UP POSITION. COMPLIED WITH QRH FOR GEAR UP DISAGREE. PULLED LANDING GEAR MANUAL EXTENSION & ALL THREE GEAR CAME DOWN & LOCKED. ACFT WOW, BRAKES WERE NOT APPLIED BEFORE NLG WOW. WITH ACFT WOW, ELEVATOR TRAVEL NOSE DOWN WAS NOT GREATER THAN 75% BEFORE NLG WOW. RECEIVED NWS INOPERATIVE CAUTION MESSAGE & NWS DID NOT WORK ON LANDING. DID NOT ATTEMPT TO RESET. COMPLIED WITH FIM RESET. MESSAGE CLEARED.

Part: WARNING MESSAGE — ACTIVATED (LANDING GEAR) · airframe 30,925 hrs · 29,043 cycles

AFTER TAKEOFF, RECEIVED A GEAR DISAGREE WARNING MESSAGE. AT THAT TIME NLG INDICATED DOWN & LOCKED. MAINS WERE WHITE IN TRANSIT. ALSO RECEIVED ANTI-SKID INBD, PARK BRAKE SOV NWS & WOW INPUT CAUTION MESSAGES ALONG WITH NOSE DOOR OPEN WARNING MESSAGE. COMPLIED WITH QRH FOR GEAR DISAGREE, GEAR UP DISAGREE. HYD 2 & 3 B PUMPS SELECTED TO ON, LANDING GEAR MANUAL RELEASE PULLED, SELECTOR LEVER DOWN. GEAR EXTENDED & MANUAL RELEASE LEVER WAS STOWED. WOW INPUT & NWS CAUTION MESSAGES ALONG WITH WOW OUTPUT FAIL STATUS MESSAGE. CYCLED NWS SWITCH. NWS CAUTION MESSAGE CLEARED. OTHER MESSAGES CLEARED ON LANDING. DECLARED EMERGENCY. ALL STRUT HEIGHTS LOOK APPROPRIATE & EVEN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,881 hrs · 28,054 cycles

ANTI-SKID OTBD CAUTION MSG ON TAKEOFF AT 120 KNOTS. INSPECTED ANTI-SKID HARNESS & CONNECTIONS, NO DEFECTS NOTED. PERFORMED FUNCTION TEST OF ANTI-SKID SYS IAW AMM 32-44-00 NOM, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 29,098 hrs · 27,311 cycles

AFTER ENG START SELECTED GEN 1 & GEN 2 HEARD LOUD BANG FOLLOWED BY AC 2 AUTO TRANSFER & AUTO TRANSFER FAIL CAUTION MSG. BURNING ODOR NOTED AFTER FAULT. COMPLIED WITH SEVERAL GEN TRANSFER CYCLES IAW AMM 24-20-00 NO DEFECTS NOTED. ALL TRANSFERS SMOOTH NO ODOR AROUND, OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (STAB TRIM) · airframe 28,859 hrs · 27,098 cycles

STAB TRIM & MACH TRIM CAUTION MSG IN FLT. COMPLIED WITH QRH, RESET STAB TRIM 1 & 2, MSGS PERSISTED. AIR RETURN TO HSV LANDED AT 44500 LBS. COMPLIED WITH FIM FAULT RESET, MSGS CLEARED THEN RETURNED WITH TRIM OPERATION.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 28,468 hrs · 26,707 cycles

3722 ON SHORT FINAL RECEIVED NLG CAUTION MESSAGE, HORN, COMPLIED WITH QRH CYCLED GEAR ALL INDICATION NORMAL. REPLACED HARNESS & ADJUSTED RVDTS.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 26,200 hrs · 24,492 cycles

UPON GEAR RETRACTION, RECEIVED NOSE DOOR OPEN WARNING WITH ASSOCIATED AUAL WARNING. AFTER GEAR EXTENSION WARNING REMAINS. ON GROUND DOOR FOUND PHYSICALLY OPEN. REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM 32-22-20, OPS CHECKS GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.

Part: SMOKE DETECTOR — UNSECURE (LAVATORY) · airframe 25,826 hrs · 24,131 cycles

REQUEST INSPECTION OF LAV SMOKE DETECTOR - WENT OFF IN FLIGHT, NO SMOKE NOTED. FOUND TO BE HANGING FROM CEILING. REMOVED LAV SMOKE DETECTOR, RE-ADJUSTED HOLDING BRACKET IAW 26-16-01, RE-SECURED HOLDING BLOCK, OPS CHECK GOOD AT THIS TIME. RE-INSTALLED SAME DETECTOR, NO DEFECTS.

Part: STRINGER — DAMAGED (FS 210-280) · airframe 23,670 hrs · 21,974 cycles

SKIN DAMAGED BY A BIRD STRIKE, STRINGER UNDER SKIN DEFORMED BY IMPACT AS WELL AS SKIN, PN 601R33010-66, STRINGER PN 600-33011-198, 12R ON RT SIDE. R & R SKIN AND STRINGER USING THE SRM AND MM.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 22,059 hrs · 20,213 cycles

AFTER TAKEOFF, WHILE SELECTING GEAR UP RECEIVED GEAR DISAGREE MSG APPROX 6 SECONDS AFTER SELECTION. NOSE GEAR SHOWED RED INDICATION. TROUBLESHOT NLG DISAGREE REF FIM 32-60-09 AND 32-60-05 ADJUSTED NLG WOFW AND NLG OLEO CENTERED AND EXTENDED PROX SENSORS NLG DOOR UPLOCK SENSORS CK OK REF AMM 32-61-05. CYCLED GEAR CKS OK, THIS CLEARS MEL.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

DAMAGED PAX DOOR SIDE STAIR PANEL 601R-52-11-1906. REPAIRED PAX DOOR SIDE STAIRS IAW REO 601R-52-11-1906, REV A.

Part: COVER — CRACKED (APU ENCLOSURE) · airframe 21,944 hrs · 20,099 cycles

APU COVER 311BZ CRACKED AT WELD TOP CENTER OF COVER. REPAIRED APU ENCLOSURE COVER 311BZ IAW REO 601R-49-11-070, REV A.

Part: HINGE — CHAFED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR HINGE (ON FUSELAGE SIDE) IS CHAFED FROM ROLL PIN NEXT TO AFT LUB. REPAIRED IAW REO 601R-53-11-2090.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 21,944 hrs · 20,099 cycles

INSPECT QEC FOR DAMAGE INCURED WHEN ENGINE STAND BROKE AND REPAIR AS NECESSARY- FIXED CORE COWL OUTER SKIN AND STIFFENER DAMAGED WHEN REAR MOUNT BROKE DURING TRANSITION ON TRUCK. REPAIRED ENGINE ASSY CF34-381, SN 873714. FIXED CORE COWL OUTER SKIN AND STIFFENER IAW REO 601R-71-13-3895, REV A.

Part: FLOORBEAM — CORRODED (BS 569) · corrosion level 2 · airframe 21,944 hrs · 20,099 cycles

LBL 27 AFT FLOORBEAM HAS CORROSION AT NUTPLATE. REMOVED DAMAGED FLOORBEAM AT LBL 27 & REPLACED WITH SERVICEABLE PART MADE FROM N126-1577 EXTENSION IAW SRM 51-42-21 & REO 601R-53-61-3778.

Part: RISER — CRACKED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR FWD STEP RISER CRACKED. REPAIRED IAW REO 601R-53-11-702.

Part: PANEL — CHAFED (LT AILERON) · airframe 21,944 hrs · 20,099 cycles

AILERON L/E PANEL 599BB HAS CHAFING DAMAGE. R & R PANEL IAW SRM 51-40-11.

Part: SKIN — CHAFED (LT AILERON) · airframe 2,194 hrs · 20,099 cycles

LT AILERON UPPER L/E SKIN IS CHAFED. R & R UPPER L/E SKIN IAW SRM 51-42-06.

Part: LATCH — WORN (LT NACELLE) · airframe 21,944 hrs · 20,099 cycles

LT LWR CORE COWL AFT OF FWD DOOR LATCH IS WORN. REPAIR IAW CMM 71-12-01.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR LOWER AFT SUPPORT STRUCTURE CRACKED. REPAIRED IAW REO 601R-52-11-279.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 21,944 hrs · 20,099 cycles

RT FLAP T/E GOUGED ON LOWER SURFACE. REPAIR IAW SRM 57-52-00.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 21,944 hrs · 20,099 cycles

LT INBD FLAP VANE CHAFED ON INBD L/E. R & R PN 601R14303-535 IAW SRM 51-42-13.

Part: SKIN — CHAFED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR ICE DOOR CHAFED BY CABLE BLENDED OUT CHAFING IAW REO 601R-52-11-1040 & SRM 51-12-00.

Part: LEVER — WORN (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR FWD PULL IN LEVERS WORN (PN 601R318968-3). REPAIRED IAW REO 601R-52-11-524, REV A.

Part: PLATE — GOUGED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR FWD STRIKER PLATE GOUGED. BLENDED GOUGE FROM FWD STRIKER PLATE OF PAX DOOR IAW REO 601R-52-11-296 AND SRM 51-12-00.

Part: PLATE — GOUGED (PAX DOOR) · airframe 21,944 hrs · 20,099 cycles

PAX DOOR AFT STRIKER PLATE GOUGED BLENDED GOUGE FROM AFT STRICKER PLATE OF PAX DOOR IAW REO 601R-52-11-296 AND SRM 51-12-20.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 21,944 hrs · 20,099 cycles

RT AILERON UPPER L/E SKIN CHAFING. REPAIRED IAW REO 601R-57-60-013.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 21,944 hrs · 20,099 cycles

RT OTBD FLAP, FLAP VANE L/E HAS DENT ON OTBD END. UPON EVALUATION OF RT OTBD FLAP VANE L/E ON OTBD END FOUND TO BE WITHIN LIMITS IAW REO 601R-57-53-030.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,944 hrs · 20,099 cycles

LBL 9 & RBL 9 SEAT TRACKS AT FS 559+112 CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS ON LBL 9 & RBL 9 AT FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACKS IAW AMM 53-01-11.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 21,726 hrs · 19,880 cycles

GEAR DISAGREE WARNING FOR RT MLG TOOK APPROXIMATELY 40 SECONDS FOR RT MLG TO SHOWED STOWED. FAULT VERIFIED, GEAR DISAGREE WARNING TO BE REPORTING FROM BOTH DCU`S. CW INSTALLED RT MLG STAY ACTUATOR MASSY OPS CK GOOD GEAR SWING GOOD LK CHECK GOOD IAW AMM 32-32-01.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 21,103 hrs · 19,210 cycles

"LT REV UNLOCKED" CAUTION MSG IN FLIGHT. FOLLOWED QRH PROCEDURES. NO CHANGE TO AC HANDLING CHARACTERISTICS. DID NOT SHUTDOWN ENGINE. DIVERTED. IN FLT LANDING WEIGHT CALCULATED AT 46990. R & R LT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CHECK GOOD, REMOVED PLACARD AND MEL REACTIVATED LT T/R IAW AMM 78-30.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 19,986 hrs · 18,069 cycles

WHILE WAITING TO CAPTURE GLIDE SLOPE, AP PITCHED UP 15 DEGREES, TURNED OFF AUTO PILOT AND RETUREND TO NORMAL FLIGHT. REENGAGED AP AND AP FUNCTIONED NORMALLY. PERFORMED ELEVATOR SERVO SPIN TEST IAW AMM 22-11-00. SERVO SPIN TEST GOOD AT THIS TIME, AUTOPILOT REMOVED FROM MEL AND PLACARDS.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 17,329 hrs · 15,493 cycles

FLAPS FAILED AT 41 DEGREES WHEN SELECTED TO 45 DEGREES. BRAKE TEMPS 4,3,4,4. REMOVED AND REPLACED RT INBD OUTER FLAP ACTUATOR. (K)

Part: RETAINER — CORRODED (E/E DOOR SEAL) · corrosion level 2 · airframe 17,310 hrs · 15,474 cycles

MAIN AVIONICS DOOR SEAL RETAINERS (4EA) FOUND CORRODED. MAIN AVIONICS DOOR SEAL RETAINERS (4 EA) REPLACED IAW SRM 51-42-06. (K)

Part: FAIRING — WORN (LT WING TE FLAP) · airframe 17,310 hrs · 15,474 cycles

LT WING, FLAP STUB FAIRING WORN LT WING, FLAP STUB FAIRING REPLACED IAW SRM 51-42-06. (K)

Part: STIFFENER — DAMAGED (PAX DOOR) · airframe 17,310 hrs · 15,474 cycles

PASSENGER DOOR AFT WEB + AFT TEE STIFFENER FOUND BUCKLED AND BENT. NEW PASSENGER AFT WEB + AFT TEE STIFFENERS INSTALLED IAW SRM 51-42-06. (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 17,310 hrs · 15,474 cycles

SERVICE DOOR LOWER SILL, STEP PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL, STEP PLATE REMOVED IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-21-23, SERVICE DOOR LWR SILL STEP PLATE REPLACED IAW SRM 51-41-04. (K)

Part: SKIN — CORRODED (WING) · corrosion level 1 · airframe 17,310 hrs · 15,474 cycles

CORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 540AT REO 601R-57-21-1076. (K)

Part: SKIN — CORRODED (WING) · corrosion level 1 · airframe 17,310 hrs · 15,474 cycles

CORROSION ON UPPER PLANK ACCESS DOOR CUT OUT OF 640BT. REO 601R57-21-1076.

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,310 hrs · 15,474 cycles

CORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 640AT REO 601R-57-21-1076. (K)

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 17,309 hrs · 15,747 cycles

CARGO DOOR HSG FOUND CRACKED 2 PLACES. CARGO DOOR HANDLE HSG REMOVED IAW SRM 51-42-21. CARGO DOOR HANDLE HSG INSTALLED IAW SRM 51-42-21. (K)

Part: MOUNT — CRACKED (DOOR MOTOR) · airframe 17,310 hrs · 15,474 cycles

PAX DOOR POWER ASSIST MOTOR STIFFENER MOUNT CRACKED. PAX DOOR POWER ASSIST MOTOR STIFFENER MOUNT REPLACED IAW SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,310 hrs · 15,474 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 (CRACK LENGTH .500) CRACK ON PILOT BULKHEAD AT FS 280, RBL 9. REPAIRED IAW REO 601R-53-11-171, REV D. EDDY CURRENT PERFORMED ON CUT-OUT AND FABRICATD PARTS IAW REO 601R-53-11-171, REV D. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 17,310 hrs · 15,474 cycles

CRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71 AROUND PARKING BRAKE CABLE (CRACK LENGTH 1.000) CRACK ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71. REPAIRED IAW CRJ 200 601R-53-11-563. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,832 hrs · 15,030 cycles

MWC 6 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED APPROX 1" LONG. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-61-1230 REV D.

Part: WIRE HARNESS — UNKNOWN (ANTI SKID SYS) · airframe 15,533 hrs · 13,801 cycles

RT OUTBOARD MLG TIRE FLAT. SUSPECT ANTI-SKID PROBLEM. REMOVED AND REPLACED RIGHT OUTBOARD GEAR HARNESS ASSEMBLY IAW AWAC SUPP 06-051, OPS CHECK GOOD AT THIS TIME. (A)

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 14,674 hrs · 12,980 cycles

RT PACK PRESSURE UNCONTROLLABLE, FOLLOWS ENGINE POWER SETTINGS, FALLS OFF LINE AT HIGH POWER SETTINGS. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .5 INCH IN LENGTH. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601R35056-109 IAW CRJ SRM 51-42-21. (M)

Part: ANGLE — CRACKED (FUSELAGE)

AFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON LEFT SIDE CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE)

AFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON RIGHT SIDE CRACKED .5 INCH LONG. MAINTENANCE CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M)

Part: SKIN — CORRODED (LT WING)

LEFT WING OUTBOARD FUEL PANEL 550BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING INBOARD FUEL PANEL 640BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING OUTBOARD FUEL PANEL 650B FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LEFT FS 280 INBOARD AND OUTBOARD FLOOR ANGLES CRACKED APPROX .1 INCH LONG AT LBL 9.0. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES P/N 601R31113-57 IAW CRJ SRM 51-42-06 AND 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT FS 280 INBOARD AND OUTBOARD FLOOR SUPPORT ANGLES CRACKED APPROX .1 INCH LONG AT RBL 9.0. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FS 280 AFT FLOOR SUPPORT ANGLE P/N 600-34017 CRACKED APPROX .3 INCH LONG OUTBOARD OF LBL 9.0. MAINTENANCE REPAIRED CRACKED FLOOR SUPPORT ANGLE P/N 600-34017 BY CUTTING OUT DAMAGE AND INSTALLING REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-138 REV C. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FABRICATED ANGLE IAW BSC STANDARD REPAIR 601R53-0030A AND BOMBARDIER REO 601R-53-41-059A REV A. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT FS 460 FLOOR SUPPORT FITTING P/N 600-31068-19 CRACKED APPROXIMATELY .3 INCH LONG AT OUTBOARD SIDE RBL 9. MAINTENANCE REMOVED CRACKED FITTING RIGHT FS 460 OUTBOARD SIDE RBL 9. DRILLED UP AND ALODINED NEW FITTING PART NR 600-31068-19. FITTING AND FASTENERS SHOT WET USING PS 870 C-12 SEALANT. (M)

Part: ANGLE — CRACKED (FUSELAGE)

RIGHT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT RBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FABRICATED ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND BOMBARDIER REO 601R-53-121-059 REV A. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LEFT FS 484 INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FAB`D ANGLE IAW BSC STANDARD REPAIR 601R.

Part: EXTINGUISHER — LOW (CARGO BAY)

FOUND CARGO BOTTLE LOW CAUTION MESSAGE ON TAXI, COMPLIED WITH QRH. REMOVED AND REPLACED CARGO FIRE EXTINGUISHER PER AMM 26-25-01. (M)

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 10,451 hrs · 8,927 cycles

ABORTED TAKEOFF DUE TO RT PACK HIGH PRESSURE. ABORTED BELOW 40 KNOTS. CREW PERFORMED ENGINE RUN IAW MEL. NO RT PACK HIGH PRESSURE OCCURRED. AIRCRAFT OK FOR RETURN TO SERVICE. (K)

Part: WARNING SYSTEM — ACTIVATED (PAX DOOR)

PASSENGER DOOR MASTER CAUTION AND AURAL `DOOR` CAME ON AFTER TAKEOFF AT APPROXIMATELY 500 AGL. COMPLIED WITH QRH AND RETURNED TO LAND. INTERROGATED PSEU, FOUND CODES D116, D117 AND D113. ALL INDICATIONS NORMAL. ALL ALIGNMENT MARKS NORMAL. NO FAULTS NOTED. (M)

Part: COALESCER BAG — DIRTY (AFT FUSELAGE)

JET FUEL ODOR IN COCKPIT. SUSPECT DIRTY COALESCER BAG FOR NR 1 PACK, PLACED ON MEL AND PLACARDED. REMOVED AND REPLACED NR 1 COALESCER SOCK IAW 21-51-13. OPS CHECK GOOD. REMOVED FROM MEL AND REMOVED PLACARD. (M)

Part: BUSHING — OUT OF POSITION (LT WING)

LEFT AFT MLG TRUNNION BUSHING MIGRATED .006. REMOVED AND REPLACED LEFT AFT MLG TRUNNION BUSHING WITH 2ND OVERSIZED BUSHING P/N 601R-57-21-003-23 IAW BOMARDIER REO 601R-57-21-0003 REV B. (M)

Part: SPAR — MISDRILLED (RT WING) · airframe 7,533 hrs · 6,241 cycles

DUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NR 46952/7 IAW BRAS 601R-57-6125. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

RIGHT INTERCOSTAL AT FS 484 AT RBL 36 CRACKED 1 INCH LONG. (M) PERFORMED A REPAIR AT FS484, RBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K)

Part: RIB — CRACKED (LT MLG WW) · airframe 7,533 hrs · 6,241 cycles

LT HAND MLG WHEEL WELL AT SS 48.30, FS 523.8, BATT RIB IS CRACKED 1.2500 INCH LONG. REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

LEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT 1 INCH. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 LT AND INSTALLED REPAIR ANGLE IAW MFG REO. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

RIGHT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED .5 INCH LONG. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 RT AND INSTALLED REPAIR ANGLE IAW MDG REO. (K)

Part: RIB — CRACKED (LT MLG WW)

LEFT MLG WHEEL WELL AT SS 48.30 FS 523.8 BATT RIB IS CRACKED 1.25 INCH LONG. (M) REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,533 hrs · 6,241 cycles

LT INTERCOSTAL AT FS 484.0 AT LBL 36 CRACKED, .5 INCH LONG. PERFORMED A REPAIR AT 484.0 LBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,533 hrs · 6,241 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A BY CUTTING OUT (CRACKED ANGLE AND INSTALLING NEW ANGLE).

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,533 hrs · 6,241 cycles

LT FS 625, WO OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED LT 621.00 ANGLE AT STR 14 LT IAW SRM. (K)

Part: ANGLE — CRACKED (WING)

RT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED RT 621-00 ANGLE AT STRINGER 14 IAW CRJ SRM 57-42-06. (M)

Part: YAW DAMPER — DEFECTIVE (VERTICAL STAB)

ON DESCENT THROUGH 9000 FEET, LOUD REPEATED BANGING SOUND FROM AIRCRAFT. COMBINED WITH SHARP REPEATED LEFT YAW MOTIONS. C/W SECU CHECKS, SPOILER AND SPOILERON CHECKS. CHECKED HYD SYSTEM HEAT EXCHANGER. CHECKED RUDDER AND RUDDER TRIM SYSTEM. COMPLIED WITH ACCEL AND DECCEL ENGINE CHECKS AND C/W VIBE CHECKS. FOUND INTERMITTENT FAILING YAW DAMP ACTUATOR NR 2. REMOVED AND REPLACED YAW DAMP ACTUATOR NR 2. (M)

Part: SUPPORT BRACKET — CRACKED (GPU RECEPTICAL) · airframe 7,230 hrs · 5,980 cycles

GPU RECEPTACLE IS BENT EXTERNAL DOOR WILL NOT CLOSE. REMOVED CRACKED SUPPORT ASSY AND INSTALLED NEW SUPPORT ASSY (PN 600-33283-33) IAW CRJ SRM, PAINTED IAW SRM. SOLID RIVETS INSTALLED IAW SRM. (K)

Part: ODOR — DETECTED (RT A/C PACK)

AFTER TURNING ON RT PACK, CABIN FILLED WITH SMOKE AND SMELLED LIKE OIL. INSPECTED SYSTEM AND RT PACK FOUND NO DEFECTS. PERFORMED OPS OF SYSTEM. SYSTEM OPS NORMAL. (M)

Part: FASTENER — LOOSE (T/E FLAP)

LEFT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO THE LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER EO 601R-57-4131. (M)

Part: STRUCTURE — CHAFED (STUBWING)

LT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER. EO 601R-57-4131 AS APPROVED BY FAA 8110-3. (M)

Part: ADG — INOPERATIVE (ELETRICAL) · airframe 2,896 hrs · 2,312 cycles

MAINTENANCE CHECK FLIGHT REQUIRED FOR INFLIGHT DEPLOYMENT OF ADG. ADG TEST FLIGHT UNSATISFACTORY. REMOVED AND REPLACED GCU (S/N OFF: 0570, S/N ON: 0212). OPERATIONAL CHECK OF GCU GOOD. ADG TEST FLIGHT GOOD. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, PASSED INCOMING ATP TEST WITH NO ERRORS.

Part: DOOR — OPEN (OXYGEN DOOR)

O2 DOOR OPENED IN FLIGHT. PRODUCED STALL WARNING CAS MESSAGE. MAINTENANCE FOUND O2 DOOR OPEN, DISRUPTED AIR FLOW OVER AOA VAIN CAUSING FAIL MESSAGE. INSPECTED DOOR NO DAMAGE NOTED. TESTED STALL WARNING SYSTEM OPS CHECK GOOD.