N864AS

Part: BRACKET — FAILED (PROXIMITY SENSOR) · airframe 40,320 hrs · 35,812 cycles

AFTER TAKEOFF, AFTER SELECTING GEAR UP. WE RECEIVED A WARNING MESSAGE GEAR DISAGREE AND NOSE DOOR OPEN. WE COMPLIED WITH THE QRH. WARNING MESSAGES CLEARED AND WE RETURNED TO FIELD LANDING WAS UNEVENTFUL. (FLT#3133) FO: 02/26/2019 CLOSED REMOVED AND REPLACED WHEEL CENTERING PROX SENSOR BRACKET, NLG SELECTOR VALVE IAW AMM. PERFORMED OPS CHECK OF LANDING GEAR IAW AMM. SWUNG GEAR SEVERAL TIMES OPS CHECK GOOD AT THIS TIME.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

RT FLOOR SILL AT FS562 TO FS589 CORRODED. (C-CHECK) RO: 11/02/2018 REMOVED AND REPLACED THE RT FLOOR SILL AT FS562.00 TO FS621.00. IAW REO.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

CORROSION ON CROSS BEAM CAP, 27RBL AT FS589.0 (C-CHECK) RO: 11/02/2018 REMOVED CORROSION FROM CROSS BEAM CAP, 27RBL AT FS589.0 IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

RT SILL ADJACENT TO FWD SERVICE DOOR CUTOUT HAS CORROSION. (C-CHECK) RO: 11/02/2018 REMOVED AND REPLACED RT SILL LOCATED BETWEEN FS 280 AND FS 319.70 WITH NEW IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

FLOOR SUPPORT BEAM 27 LBL CORRODED AT FS559.0+112. (C-CHECK) RO: 11/02/2018 REMOVED AND REPLACED FLOOR BEAM SECTION FROM 559+10 TO FS 559+112 AT LBL 27 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

RT SILL JUST AFT OF SERVICE DOOR CUTOUT HAS CORROSION AROUND NUTPLATE HOLES. (C-CHECK) RO: 11/02/2018 REMOVED AND REPLACED CORRODED SECTION OF RT FLOOR SILL AFT OF SERVICE DOOR CUT-OUT, BETWEEN FS 349.00 - FS 379.00, RBL 42 WITH NEW RT FLOOR SILL SECTION IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

RT FLOOR SUPPORT SILL FROM FS559.0+80 TO FS589.0 HAS CORROSION AROUND THE FASTENER HOLES. (C-CHECK) RO: 11/02/2018 REPAIRED RT FLOOR SILL FROM FS559.0+80 TO FS562 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,700 hrs · 35,216 cycles

SERVICE DOOR SILL ANGLE HAS CORROSION. (C-CHECK) RO: 11/02/2018 REMOVED AND REPLACED SERVICE DOOR SILL ANGLE IAW SRM.

Part: SKIN — DENTED (LT WING) · airframe 39,700 hrs · 35,216 cycles

THERE ARE TWO DENTS ON THE LT WING LEADING EDGE 48" FROM INBD EDGE. (C-CHECK) RO: 11/02/2018 DRESSED 3 DENTS ON THE LT I/B L/E, IAW REO.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 39,465 hrs · 35,002 cycles

ON TAKEOFF, RECEIVED AN ANTI SKID INBD AND PARK BRAKE SOV CAUTION MESSAGE AFTER GEAR HANDLE SELECTED UP. LANDING GEAR NEVER CAME UP. RAN QRH PROCEDURE. CYCLED THE LANDING GEAR HANDLE TO DOWN POSITION AND EVERYTHING WENT BACK TO NORMAL. RETURNED TO FIELD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM. OPS CHECKED GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. PERFORMED OPS CHECK FOR ANTI-SKID CAUTION MESSAGE IAW FIM. OPS CHECKED GOOD. NO DEFECTS FOUND. PERFORMED OPS CHECK FOR PARK BRAKE SOV IAW AMM. OPS CHECKED GOOD AT THIS TIME. NO FAULTS FOUND.

Part: THRUST REVERSER — NOT REPORTED (ENGINE) · airframe 38,281 hrs · 33,870 cycles

CREW HEARD A LOUD BANG AND STRONG AIRFRAME VIBRATIONS FELT. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. (FLT 3133) REMOVED AND REPLACED UPPER TRANSLATING COWL AND UPPER AND LOWER CORE COWLS IAW AMM. REPAIRED DENTS IAW SRM AND REO.

Part: ENGINE — FAILED (NR 2) · airframe 37,885 hrs · 33,484 cycles

IN FLIGHT, NR 2 ENGINE OBSERVED LOUD NOISE FOLLOWED BY N2 ROLLBACK AND NOTED HIGH VIBRATION. COMPLIED WITH QRH AND SHUT ENGINE DOWN. REMOVED AND REPLACED THE NR 2 ENGINE. OK FOR SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 37,512 hrs · 33,049 cycles

VISIBLE SMOKE IN THE CABIN. FA REPORTS SMOKE SEEMED TO BE MID CABIN NEAR OVERHEAD EXIT SIGN. RECEIVED SMOKE TOILET CAUTION. DECLARED AN EMERGENCY. FLT 2954, WORK IN PROGRESS.

Part: LIGHT — SHORTED (LAVATORY) · airframe 37,423 hrs · 32,946 cycles

AIRCRAFT RETURNED TO THE FIELD WITH THE A LAVATORY SMOKE ALARM ACTIVATED. FLT ATTENDANT FOUND NO SMOKE IN THE LAVATORY. JUST AFTER TAKEOFF. TROUBLESHOT AND FOUND LAVATORY LIGHTED ORDINANCE SIGN TO BE SHORTING TO A FRAME SCREW. REMOVED AND REPLACED THE THE SIGN IAW AMM. OPS CHECKED GOOD. FOUND THE LAVATORY FA CALL LIGHT DAMAGED. REMOVED AND REPLACED THE CALL LIGHT IAW AMM. OPS CHECKED GOOD. REMOVED AND REPLACED LAVATORY LIGHT BALLAST AS A PRECAUTION. OPS CHECKED GOOD. PERFORMED ENGINE RUNS AND OPERATED PACKS FOR AN EXTENDED PERIOD OF TIME. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 37,188 hrs · 32,663 cycles

SMOKE TOILET CAUTION MESSAGE. WITH VISIBLE SMOKE IN THE AFT END OF THE CABIN. REMOVED AND REPLACED LT AND RT COALESCER BAGS IAW AMM. NO FURTHER DEFECTS FOUND AT THIS TIME.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,580 hrs · 31,961 cycles

DENT FOUND ON SKIN LT SIDE AFT FUSELAGE JUST AFT OF CARGO COMPARTMENT DOOR. REPAIRED DENT IAW EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,580 hrs · 31,961 cycles

DENT ON RIGHT FUSELAGE SKIN JUST FWD OF AFT EQUIPMENT ACCESS . REPAIRED IAW EA.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 34,928 hrs · 30,171 cycles

RECEIVED SMOKE TOILET CAUTION MSG DURING FLIGHT. COULD NOT DUPLICATE. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (AFT CABIN & LAV) · airframe 34,239 hrs · 29,534 cycles

SMOKE NOTED IN THE CABIN AFTER TAKEOFF. SMOKE TOILET CAUTION MESSAGE. SMOKE FILLED BACK OF CABIN. LAVATORY SMOKE ALARM GOING OFF. CREW FOLLOWED QRH. OPERATED BOTH PACKS WITH BOTH APU AND ENGINE BLEEDS FOR EXTENDED PERIOD IAW AMM. NO SMOKE DETECTED IN CABIN OR COCKPIT AT THIS TIME.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 34,069 hrs · 29,381 cycles

CABIN EMERGENCY LIGHTS DO NOT STAY ON. R & R EMERGENCY LIGHT BATTERY PACK NR 1, NR 2, NR 3 AND NR 4 IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 32,912 hrs · 28,264 cycles

CABIN ALTITUDE WARNING AT FL220 UNABLE TO CONTROL CABIN IN AUTO OR MANUAL. DIVERTED. PRESSURIZED ACFT IAW AMM. DISPLAY COOL MESSAGE REMAINED OFF. ACFT PRESSURIZES AND DEPRESSURIZED SMOOTHLY.

Part: SENSOR — OUT OF ADJUST (MLG) · airframe 32,401 hrs · 27,753 cycles

MLG WOULD NOT RETRACT. ADJUSTED NOSE GEAR CENTERED/EXTENDED PROX SENSOR IAW AMM. SWUNG GEAR MULTIPLE TIMES. ALL CHECKS GOOD.

Part: BULKHEAD — GOUGED (BS 621) · airframe 32,330 hrs · 27,691 cycles

GOUGE CAUSED BY SCREW ON THE BS 621 BULKHEAD RBL 41, WL 76 REQUIRES REPAIR. C-CHECK REPAIRED THE BULKHEAD IAW REO.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 32,330 hrs · 27,691 cycles

PRESSURE BULKHEAD, FS 621 AT RBL 41, WL 76 DAMAGED. C-CHECK, REPAIRED PRESSURE BULKHEAD IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 32,330 hrs · 27,691 cycles

LEFT SIDE FLOOR SUPPORT CORRODED FROM BS 349 - 364, LBL 36. C-CHECK, REMOVED CORROSION IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 32,330 hrs · 27,691 cycles

PASSENGER DOOR HINGE LANDS CHAFED. C-CHECK, BLENDED CHAFES TO A SMOOTH FINISH, IAW REO.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 32,330 hrs · 27,691 cycles

PASSENGER DOOR HINGE, FUSELAGE SIDE, AFT LUG LANDING HAS GOUGE FROM DRIVE PIN. C-CHECK, REMOVED DAMAGE FROM PASSENGER DOOR HINGE, FUSELAGE SIDE, AFT LUG LANDING GOUGE FROM DRIVE PIN IAW REO.

Part: SKIN — CHAFED (LT WING) · airframe 32,330 hrs · 27,691 cycles

LEFT WING LOWER PLANK HAS CHAFE DAMAGE AT WS 124, APPROXIMATELY 30 " FROM T/E. C-CHECK, REPAIRED CHAFE DAMAGE ON LT WING LOWER PLANK AT 30" FROM T/E AT WS 124, IAW STS EA.

Part: SKIN — CHAFED (RT WING) · airframe 32,330 hrs · 27,691 cycles

RIGHT WING LOWER PLANK HAS CHAFE DAMAGE AT WS 124, APPROXIMATELY 30" FROM T/E. C-CHECK, REPAIRED CHAFE DAMAGE ON RT WING LOWER PLANK AT 30" FROM T/E AT WS 124 IAW EA.

Part: SKIN — CHAFED (RT WING) · airframe 32,330 hrs · 27,691 cycles

RT WING LOWER PLANK HAS CHAFE DAMAGE AT BL 45, AT T/E, APPROXIMATELY 3" IN LENGTH WITH 2 EA SMALL CHAFE MARKS JUST FORWARD OF THE T/E. C-CHECK BLENDED OUT CHAFING DAMAGE ON RT WING LOWER PLANK, BL 45 JUST FWD OF T/E IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,330 hrs · 27,691 cycles

RT WING PLANK AROUND OPENING FOR PANEL 640BB HAS SURFACE CORROSION. C-CHECK, BLENDED CORROSION ON RT WING PLANK AROUND OPENING FOR PANEL IAW REO C.

Part: SKIN — CORRODED (LT WING) · airframe 32,330 hrs · 27,691 cycles

LEFT WING PLANK AROUND OPENING FOR PANEL 550BB HAS SURFACE CORROSION. C-CHECK, BLENDED CORROSION ON LT WING PLANK AROUND OPENING FOR PANEL 550BB IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 32,330 hrs · 27,691 cycles

RIGHT WING PLANK AROUND OPENING FOR PANEL 650EB HAS SURFACE CORROSION. C-CHECK, BLENDED CORROSION ON RT WING PLANK AROUND OPENING FOR PANEL 650EB IAW REO.

Part: SKIN — CRACKED (LT WING) · airframe 32,330 hrs · 27,691 cycles

LEFT LOWER WING SKIN WING DRAIN HOLES CRACK INDICATIONS NOTED. C-CHECK, REPAIRED IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 32,330 hrs · 27,691 cycles

LT WING PLANK AROUND OPENING FOR PANEL 550DB HAS SURFACE CORROSION. C-CHECK, BLENDED CORROSION ON LT WING PLANK AROUND OPENING FOR PANEL 550DB IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,330 hrs · 27,691 cycles

BS 559+96, LBL 9 SEAT TRACK CORRODED. C-CHECK, INSTALLED A NEW SEAT TRACK IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,330 hrs · 27,691 cycles

BS 280 OTBD OF RBL 9 LOWER FLOORBEAM SPLICE CRACKED. C-CHECK, R & R LOWER FLOORBEAM SPLICE IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 461.5-599) · airframe 32,330 hrs · 27,691 cycles

RIGHT FUSELAGE BS 461.5 - 599, RBL 47 HAS CORROSION ALONG FLOOR SUPPORT. C-CHECK, BLENDED CORROSION IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,330 hrs · 27,691 cycles

BS 621 AFT PRESSURE BULKHEAD AT LBL 36.2 LOWER WEB CRACK INDICATION NOTED. C-CHECK, REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,330 hrs · 27,691 cycles

BS 280, RBL 9, OTBD FLOORBEAM ANGLE CRACKED. C-CHECK, R & R IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,330 hrs · 27,691 cycles

SEAT TRACK BS 559+112, RBL 9 IS CORRODED. C-CHECK, INSTALLED A NEW SEAT TRACK IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,330 hrs · 27,691 cycles

LEFT FUSELAGE SEAT TRACK BS 559 - 559+80, LBL 9 CORRODED. C-CHECK, REPLACED THE SEAT TRACK IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 32,330 hrs · 27,691 cycles

FWD AVIONICS BAY FRAME BS 333 FROM S26R - 26L CORRODED. C-CHECK, REMOVED CORROSION FROM THE FRAME IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,330 hrs · 27,691 cycles

BS 280, LBL 9 OTBD FLOORBEAM ANGLE CRACKED. C-CHECK, REPLACED THE FLOORBEAM ANGLE IAW SRM AND REO.

Part: FRAME — CRACKED (BS 605) · airframe 32,330 hrs · 27,691 cycles

FRAME CRACKED S10L, FS 605. C-CHECK, REPAIRED FRAME IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 32,330 hrs · 27,691 cycles

FWD FACE OF BULKHEAD BS 621 GOUGED MID TO LOWER LT AND RT SIDES. C-CHECK, REPAIRED IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 32,330 hrs · 27,691 cycles

PAX DOOR HINGE HALF UPPER SIDE OF HINGE LUGS HAS GOUGING AND WEAR DAMAGE. C-CHECK, BLENDED GOUGES ON PAX DOOR HINGE LUGS, DOOR SIDE IAW REO.

Part: STRUCTURE — DAMAGED · airframe 32,330 hrs · 27,691 cycles

AFT CARGO ABOVE DOOR, LEFT ENGINE THROTTLE CABLE AT PYLON PASS THROUGH BOOT NOT COVERING FAIRLEAD TUBE. C-CHECK, COMPLIED WITH REPAIR OF THE LT FUSELAGE AFT THROTTLE CABLE ABOVE AFT CARGO DOOR IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

LEFT WING INBD FLAP, INBD VANE ACTUATOR, FLAP INNER SKIN CHAFED AT BONDING WIRE CONNECTION. C-CHECK, REPAIRED CHAFING ON LT WING INBD FLAP, INBD VANE ACTUATOR FLAP, INNER SKIN IAW SRM AND REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,330 hrs · 27,691 cycles

AVIONICS DOOR CUTOUT SURROUND STRUCTURE INNER SKIN HAS SEVERAL AREAS WITH CORROSION. C-CHECK, REPAIRED IAW REO.

Part: FASTENER — LOOSE (RT NACELLE) · airframe 32,330 hrs · 27,691 cycles

RT ENGINE NOSE INLET COWL HAS ONE LOOSE RIVET ON INSIDE ATTENUATING PANEL AT APPROXIMATELY 1 O'CLOCK POSITION. C-CHECK, REMOVED & INSTALLED NEW RIVET ON RT ENGINE NOSE INLET COWL, INSIDE ATTENUATING PANEL AT APPROXIMATELY 1 O'CLOCK IAW STS EA.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 32,330 hrs · 27,691 cycles

RIGHT MLG DOOR HAS A CHAFE ON L/E BY THE BRUSHES. C-CHECK, REPAIRED RT MLG DOOR INNER SKIN IAW REO.

Part: PANEL — CHAFED (UNKNOWN) · airframe 32,330 hrs · 27,691 cycles

PANEL 699CB CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699CB IAW REO.

Part: PANEL — CHAFED (UNKNOWN) · airframe 32,330 hrs · 27,691 cycles

PANEL 699BB CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699BB IAW REO.

Part: SHROUD — CHAFED (LT AILERON) · airframe 32,330 hrs · 27,691 cycles

LEFT AILERON UPPER SKIN SHROUD CHAFED. C-CHECK, BLENDED CHAFE AREA IAW REO.

Part: SHROUD — CHAFED (RT AILERON) · airframe 32,330 hrs · 27,691 cycles

RIGHT AILERON LOWER SKIN SHROUD FROM A STA323.843 TO A STA329.875 IS CHAFED. C-CHECK, BLENDED CHAFED AREA ON RT AILERON LOWER SKIN SHROUD FROM A STA323.843 TO A STA329.875 IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

RIGHT INBD FLAP VANE SKIN CHAFED, INBD CAP. C-CHECK, REPAIRED FLAP VANE SKIN IAW REO.

Part: SHROUD — CHAFED (RT AILERON) · airframe 32,330 hrs · 27,691 cycles

RIGHT AILERON LOWER SKIN SHROUD IS CHAFED. C-CHECK, BLENDED CHAFED AREA IAW REO.

Part: PANEL — CHAFED (UNKNOWN) · airframe 32,330 hrs · 27,691 cycles

PANEL 699AB, CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699AB IAW REO.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 32,330 hrs · 27,691 cycles

LEFT MLG DOOR HAS CHAFE ON INNER SKIN. C-CHECK, CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA.

Part: SHROUD — CHAFED (LT AILERON) · airframe 32,330 hrs · 27,691 cycles

LEFT AILERON LOWER SKIN SHROUD IS CHAFED. C-CHECK, BLENDED CHAFED AREA IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

RIGHT INBD FLAP VANE SKIN CHAFED, CENTER OTBD CAP. C-CHECK, REPAIRED CHAFE IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

LEFT INBD FLAP VANE SKIN CHAFED, OTBD CAP. C-CHECK, BLENDED CHAFE IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

LEFT INBD FLAP VANE SKIN CHAFED, CENTER OTBD CAP. C-CHECK, BLENDED CHAFE IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,330 hrs · 27,691 cycles

RIGHT AILERON UPPER SKIN SHOURD CHAFED, OTBD OF INBD HINGE TO OTBD EDGE. C-CHECK, BLENDED CHAFE ON RT AILERON UPPER SKIN SHROUD IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,330 hrs · 27,691 cycles

LEFT INBD FLAP VANE SKIN CHAFED, INBD CAP. C-CHECK, BLENDED CHAFE IAW REO.

Part: SKIN — DENTED (BS 605) · airframe 32,330 hrs · 27,691 cycles

BELOW AFT CARGO DOOR IS DENTED, APPROX 12" DOWN, NEAR BS 605. C-CHECK, REPAIRED DENT APPROXIMATELY 12" BELOW CARGO DOOR NEAR FS 605.00 IAW REO.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 32,016 hrs · 27,383 cycles

RT ENGINE OVER TEMPED FOR APPROXIMATELY 30 SECONDS DURING A GO AROUND. PERFORMED OVER TEMP INSPECTION AND BOROSCOPE. NO ISSUES FOUND AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,322 hrs · 26,693 cycles

SERVICE DOOR AND RT EMERGENCY EXIT DOOR EXIT SIGNS EACH HAVE BULBS BURNED OUT. REPLACED BULBS IAW AMM.

Part: WARNING MESSAGE — FALSE INDICATION (CABIN COOLING) · airframe 31,006 hrs · 26,387 cycles

OVERBOARD COOL CAUTION AND INBD COOL FAIL STATUS MESSAGE. CABIN WOULD NOT PRESSURIZE. INSPECTED OVERBOARD EXHAUST VALVE AND INBD EXHAUST VALVE IAW AMM. BOTH VALVES MOVED TO CORRECT POSITIONS, PERFORMED SELF TEST OF BOTH CABIN PRESSURE CONTROLLERS. NO FAULTS FOUND. PRESSURIZED ACFT TO 4P IAW AMM. OPS CHECKED GOOD AT THIS TIME.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 28,966 hrs · 24,275 cycles

FOUND A 2" DEEP SCRATCH AND DENT ABOUT 12" BELOW METAL PLATE IN THE CARGO BIN. REPAIRED SCRATCH AND DENT ON LEFT AFT FUSELAGE ABOVE STRUNGER 20L AND FOWARD OF FS. 621.00. IAW REO.

Part: SCISSOR LINK — DISCONNECTED (NLG) · airframe 27,741 hrs · 22,890 cycles

GEAR DISAGREE, NOSE GEAR STAYED DOWN, NO STEERING AVAILABLE UPON LANDING. (FLT 2617) RECONNECTED NOSE SCISSOR LINKS.

Part: SKIN — CRACKED (LT WING) · airframe 27,642 hrs · 22,781 cycles

ON LEFT WING LOWER PLANK HOLES 4TH AND 7TH FROM AFT EDGE OF STEEL STRAP COMMON TO MLG TRUNNION HAVE CRACKS. (C-CHECK) REPAIRED LEFT POWER WING PLANK FOURTH AND SEVENTH HOLES.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 27,642 hrs · 22,781 cycles

CRACK ON FS 202 LEFT SIDE AT PARKING BRAKE ROD. (C-CHECK) REPAIRED CRACK ON FS 202 AT PARKING BRAKE ROD IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 27,642 hrs · 22,781 cycles

CRACKS NOTED ON FS 409.0 +128 VERTICAL POST AT BL 0.0 AT LEFT AND RIGHT SIDES. (C-CHECK) REPLACED THE FS 409.0 +128 VERTICAL POST AT BL 0.0 AT LEFT AND RIGHT SIDES IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 27,642 hrs · 22,781 cycles

CRACKS NOTED ON FS 409.0 +128 VERTICAL POSTS AT RBL 18.0. INBOARD AND OUTBOARD SIDES. (C-CHECK) REPLACED THE FS 409.0 +128 VERTICAL POST AT RBL 18.0 IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,106 hrs · 22,260 cycles

OVERHEAD EMERGENCY EXIT ROW SIGN MID CABIN IS BURNED OUT ON ONE SIDE. (FLT 4476) REPLACED NR 2 ELBP IN REFERENCE TO AMM. P/N: AD-2013-1A, SN: 71061

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,035 hrs · 22,193 cycles

LEFT GALLEY NEAR FLOOR EMERGENCY LIGHT IS OUT. (FLT 4622) RELAMPED EMERGENCY LIGHT.

Part: FCU — FAILED (TE FLAP) · airframe 26,376 hrs · 21,506 cycles

AIRCRAFT PITCHED UP. (FLT 4826) REPLACED THE FLAP CONTROL UNIT, THE LEFT FLAP POSITION TRANSMITTER, AND THE NR 1 DCU. PN: 622-9820-010 SN OFF: 14BD, PN: 860D100-18ABCD SN OFF: 1151.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,276 hrs · 21,412 cycles

LOWER EMERGENCY CABIN DOOR LIGHT IS OUT. (FLT 4768) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,191 hrs · 21,332 cycles

LEFT FORWARD AND AFT 2 RIGHT OVERWING EMERGENCY EXIT LIGHTS ARE OUT. (FLT 4595) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,368 hrs · 20,548 cycles

RIGHT OVERWING MIDDLE EMERGENCY LIGHT IS OUT. (FLT 4541) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,352 hrs · 20,532 cycles

SERVICE DOOR EMERGENCY LIGHT NOT WORKING. (FLT 4541) REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT SERVICE DOOR IN THE CABIN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,183 hrs · 20,381 cycles

MOST FORWARD EMERGENCY LIGHT ON EXTERIOR OVERWING ON LEFT AND RIGHT SIDE ARE OUT. (FLT 4557) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CRACKED (WING) · airframe 24,371 hrs · 19,695 cycles

BOTH WING LOWER PLANKS AT WS 148 CRACKED AT AFT AREA. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,371 hrs · 19,694 cycles

FS 621 BULKHEAD CRACKED ON FORWARD FACE ABOVE UPPER CARGO TRACK FITTING. (C-CHECK) REPAIR PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 24,561 hrs · 19,847 cycles

FS 409+128 VERTICAL POST CRACKED AT OUTBOARD AFT RADIUS. (C-CHECK) REPAIRED PER REO.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 23,510 hrs · 18,960 cycles

LEFT FORWARD YOKE MOUNT CORRODED. (ENG CHANGE) REPLACED YOKE MOUNT.

Part: FLAP — OBSTRUCTED (RT WING) · airframe 22,141 hrs · 17,790 cycles

WHEN FLAPS 45° ARE DEPLOYED AIRCRAFT ROLLS TO THE RIGHT. (FLT 4740) REMOVED EXCESSIVE SEALANT ALONG RIGHT FLAPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,296 hrs · 17,119 cycles

CEILING EMERGENCY LIGHT INOP. (FLT 4514) RELAMPED EMERGENCY LIGHT.

Part: OIL SYSTEM — OVERTEMP (APU) · airframe 21,226 hrs · 17,065 cycles

APU HIGH OIL TEMP EN ROUTE WITH NR 1 IDG DEFERRED INOPERATIVE. (FLT 4869) CONFIRMED OIL LEVEL AND OPERATION CHECK NORMAL.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 20,400 hrs · 16,435 cycles

DURING C-CHECK, AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REPAIRED PER REO.

Part: PRESSURE BLKHD — CRACKED (BS 559) · airframe 20,400 hrs · 16,435 cycles

DURING C-CHECK, FS 559 PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.

Part: ATTACH BRACKET — CRACKED (BS 280) · airframe 20,400 hrs · 16,435 cycles

C-CHECK, FS 280 FLOORBEAM ATTACH BRACKETS CRACKED. REPLACED PER REO.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 20,400 hrs · 16,435 cycles

DURING C-CHECK, CLIP COMMON TO PRESSURE BULKHEAD AND CARGO DOOR CRACKED. REPLACED PER SRM.

Part: A/C PACK — SMOKE (LEFT) · airframe 16,133 hrs · 13,170 cycles

LEFT PACK TEMPERATURE WILL NOT COOL DOWN AND SMELLS OF SMOKE. REPLACED LEFT PACK IAW AMM 21-57-10. OPS CHECK GOOD.

Part: CONNECTOR — SHORTED (ELECTRICAL) · airframe 15,445 hrs · 12,636 cycles

AFTER TAKEOFF ACCESS BUSS CAUTION MESSAGE AND FOLLOWED BY SEVERAL CAUTIONS MESSAGES. FOUND ADG XFER K2XD CONTACTOR HAD A SHORTED TERMINAL. REPLACED CONTACTOR, TERMINAL AND ESSENTIAL TRU 1. OPERATIONAL CHECKS GOOD.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 15,445 hrs · 12,636 cycles

RT T/R NR 4 MAIN TRACK CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT THRUST REVERSER LOWER I/B MAIN TRACK PER CRJ200 MM TASK 78-34-11-400-801.

Part: STEP — CRACKED (PAX DOOR) · airframe 15,445 hrs · 12,636 cycles

FWD PAX DOOR STEPS 4/5 CRACKS FOUND IN CORNERS, DISCOVERED DURING C-CHECK INSPECTION. C/W CRJ200 REO 601R-52-11-702 REV A REPAIR FOR MULTI SITE DAMAGE ZONES 2 AND 3.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,445 hrs · 12,636 cycles

FS 280 FLOORBEAM IS CRACKED AT LBL10 (LWR), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON FLOORBEAM STA 280 LBL10 PER REO 601R-53-11-176 REV C.

Part: ANGLE — CRACKED (BS 280) · airframe 15,445 hrs · 12,636 cycles

FS 280 9L AND 9R BRACKETS ANGLES CRACKED INBOARD AND OUTBOARD (ALL 4, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AND FILLER PER CRJ200 SRM 51-40-2 AND BOMBARDIER REO 601R-53-11-171 REV C.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,445 hrs · 12,636 cycles

FS 280 FLOORBEAM IS CRACKED AT RBL TO (LWR), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS FS 280 FLOORBEAM PER REO 601R-53-71-171 REV C.

Part: NOSE COWL — CRACKED (RT ENGINE) · airframe 15,445 hrs · 12,636 cycles

RT ENGINE NOSE COWL HAS A CRACKED BRACKET AT 4 O'CLOCK POSITION AND XN122.72, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET RT ENGINE NOSE COWL AT 4 O'CLOCK POSITION PER ENGINEERING ORDER 601R-71-11031.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,445 hrs · 12,636 cycles

PAX DOOR EXTERNAL HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR EXTERNAL HANDLE P/N 601R31763-1 IAW CRJ200 SRM 51-42-21 PG 1-21. OPERATIONAL CHECKS GOOD.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 15,445 hrs · 12,636 cycles

LT ENG FWD MOUNT UPPER LINK HAS CORROSION ON UPPER BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT UPPER LINK P/N 601-37016-5 S/N 5064.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 15,445 hrs · 12,636 cycles

DOUBLER CRACKED INSIDE PNL832AR OF PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALL NEW PAX DOOR DOUBLER PER CRJ200 SRM 51-42-06 PG 11, 51-42-21 PG 17 AND 51-23-00 PG 21.

Part: STEP — CRACKED (PAX DOOR) · airframe 15,445 hrs · 12,636 cycles

AFT PAX DOOR STEPS CRACKED CORNERS 4/5, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS, PAX DOOR AFT WEB PER REO 601R-52-11-702 REV A.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 15,445 hrs · 12,636 cycles

LT ENG FWD YOKE MOUNT HAS CORROSION IN BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD YOKE MOUNT P/N 601-37015-7 S/N RJ SWA/070301BTAC03.

Part: NUT CLIP — CRACKED (BS 484) · airframe 15,445 hrs · 12,636 cycles

RT 484 INBOARD/OUTBOARD CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP 601R31171-9 AND 601R-53-41-059-2 TO RT FS 484 AT RBL 27 AND 36 PER CRJ200 SRM 51-42-06 P11 AND 51-42-21 P17.

Part: BOLT — CORRODED (FUSELAGE) · airframe 15,445 hrs · 12,636 cycles

FOUND CORROSION ON WARDROBE FLOOR BOLTS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 4 WARDROBE FLOOR BOLTS IAW CRJ200 AMM 20-21-00-910-801.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 15,445 hrs · 12,636 cycles

LEFT ENGINE T/R BOX UPPER INBOARD CRACKED AT LOWER FORWARD CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LEFT ENGINE UPPER INBOARD CASCADE PER CRJ200 MM SUBTASK 78-33-01-869-001 AND 78-33-01-920-001 TUC 1233

Part: NUT CLIP — CRACKED (BS 484) · airframe 15,445 hrs · 12,636 cycles

LT 484 INBOARD AND OUTBOARD CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP P/N 601R31171-17 ST LT STA 484 BL 27.00 PER REO 601R-53-41-059 AND ANGLE AT LT STA 484 BL 36.00 PER REO 601R-53-41-059.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 13,201 hrs · 10,964 cycles

ABORTED TAKEOFF FOR "TAKEOFF CONFIG SPOILER" WARNING AND "R FLT SPOILER" CAUTION MESSAGE. REPLACED NR 1 SECU IAW MM 27-62-01. OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 13,180 hrs · 10,948 cycles

RECEIVED FLT SPLRS FAULT MESSAGE IN FLIGHT RT FLIGHT SPOILER IB PCU FAILED. REPLACED SECU NR 2. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 13,161 hrs · 10,935 cycles

"FLT SPLR FAULT" STATUS MESSAGE. REPLACED RIGHT IB FLIGHT SPOILER PCU. OPERATIONAL CHECK GOOD IAW 27-52-01.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 12,451 hrs · 10,402 cycles

FLAPS FAIL 0 DEG INFLIGHT. REPLACED ALL 8 FLAP ACTUATORS IAW AMM 27-53-05. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING AN A-CHECK IN BTR, THE LEFT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT WING EMERGENCY EXIT LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED AND THE LOWER STEP SUPPORT ROD (P/N 601R317198-1) REQUIRING ADJUSTMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP AND ADJUSTED THE LOWER STEP SUPPORT ROD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURNIG A C-CHECK IN MCN, THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURNG A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD CLIP AT FS 280, RBL 9. (M)

Part: SUPPORT — CRACKED (CARGO DOOR SILL)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562-72-589 IAW ASA EO 600-53-0095. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRAKET IAW SRM 51-42-06. (M)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, AN EMERGENCY EXIT ILGHT LENS AND TRIM WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING AN EMERGENCY EXIT LIGHT ASSEMBLY. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M)

Part: BULB — BURNED OUT (FUSELAGE)

DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A SCHEDULED INSPECTION IN XNA, THE GALLEY AND FORWARD ORANGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4236 - DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THAT THE FORWARD FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE CLEANED A DIRTY CONNECTOR ON THE FLOOR TRACK EMERGENCY LIGHTING. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR INSPECTION IN MCN, THE FORWARD FLOOR TRACK EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE FLOOR LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4453 - BEFORE DEPARTURE OUT OF DFW, CAPTAIN NOTICED A CRACK IN THE LEFT SIDE WINDSHIELD. MAINTENANCE REMOVED AND REPLACED CRACKED WINDSHIELD. A PRESSURIZATION CHECK WAS PERFORMED AND NO LEAKS WERE NOTED. THE SEALANT WAS PROPERLY CURED. AIRCRAFT RETURNED TO SERVICE. (M)