N451CA

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,280 hrs · 22,680 cycles

INTERIOR EMERGENCY CEILING LIGHT OUT AT 5ABCD. LAMPED THE EMERGENCY LIGHT AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 23,691 hrs · 22,062 cycles

CABIN EMERGENCY TRACK LIGHT COVER IS CRACKED. REPLACED EMERGENCY LIGHT COVER IAW AMM 33-51-01-400-801. OPS CHECK GOOD AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 621) · airframe 23,691 hrs · 22,062 cycles

CARGO BAY FLOOR SUPPORT AT LBL 27 BETWEEN FS 621.00 ON OTBD EDGE HAS CORROSION AROUND NUTPLATES. CORROSION IS BEYOND LIMITS OF SRM 53-00-00, FIG 101, SHEET 3 AND REO 601R-53-00-005 REV B. R & R CARGO FLOOR SUPPORT IAW SRM 51-42-21 AND REO 601R-53-61-3778.

Part: STRAP — CORRODED (BS 559) · airframe 23,691 hrs · 22,062 cycles

STRAP AT FS 559 LBL 27 IS CORRODED BEYOND LIMITS. REMOVED STRAP IAW SRM 51-42-06. INSTALLED STRAP IAW SRM 51-42-06. BLENDED CORRSION ON STRAP BOTH SIDES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 AND 53-41-43. DRILLED NEW SERVICEABLE STRAP IAW SRM 51-40-11.

Part: STRAP — CORRODED (BS 559) · airframe 23,691 hrs · 22,062 cycles

STRAP AT BS 559 LBL 27 IS CORRODED BEYOND LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 499-529) · airframe 23,691 hrs · 22,062 cycles

LEFT FLOOR SUPPORT BETWEEN FS 499 AND 529 HAS AREAS OF CORROSION. REPAIRED IAW REO 601R-53-41-1577.

Part: ANGLE — CRACKED (BS 484) · airframe 23,691 hrs · 22,062 cycles

RIGHT FS 484.00 INTERCOSTAL ANGLE AT RBL27 IS CRACKED. REPLACED CRACKED INTERCOSTAL ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 23,691 hrs · 22,062 cycles

PAX DOOR AFT DOOR ANGLE PREVIOUS REPAIR CRACKED APPROX .5" LONG. NO WITHIN SERVICEABLE LIMITS IAW SRM 52-00-00. REMOVED PAX DOOR AFT DRAG ANGLE. LOCATED & DRILLED NEW AFT DRAG ANGLE IAW SRM 51-42-06 AND SRM 51-40-11. INSTALLED THE NEW AFT DRAG ANGLE IAW SRM 51-42-06.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 23,691 hrs · 22,062 cycles

FS 621.00 FWD FACE OF THE REAR PRESSURE BULKHEAD LT OTBD SIDE HAS AN ISOLATOR MISSING. REPLACED BROKEN ISOLATOR AT FS 621.00 FWD FACE OF REAR PRESSURE BULKHEAD IAW SRM 51-42-13 PN SL2337-3.

Part: ANGLE — CRACKED (BS 484) · airframe 23,691 hrs · 22,062 cycles

LEFT FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IS CRACKED. REPLACED CRACKED INTERCOSTAL ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 570-621) · airframe 23,691 hrs · 22,062 cycles

CARGO BAY FLOOR SUPPORT CAP AT LBL27 BETWEEN FS 570.00 AND FS 621.00 ON OTBD EDGE HAS CORROSION AROUND NUTPLATES. FURTHER INVESTIGATION FOUND CORROSION MORE THAN 75 PERCENT OF MATERIAL THICKNESS. CORROSION IS BEYOND LIMITS OF SRM 53-00-00, FIG 101, SHEET 3 AND REO 601R-53-00-005, REV B.

Part: POST — CRACKED (BS 409) · airframe 23,691 hrs · 22,062 cycles

FOUND FS 409.00+128 VERTICAL POST BL 0.0 HAS CRACK INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE. RADIUS FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. DRILLED & LOCATED NEW POST AND LT & RT ANGLES IAW SRM 51-40-11 & 51-42-06. INSTALLED NEW POST IAW REO 601R-53-41-889 & SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 23,691 hrs · 22,062 cycles

FOUND FS 409.00+128 VERTICAL POST LBL 18 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE. RADIUS FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. DRILLED & LOCATED NEW POST IAW SRM 51-40-11 & 51-40-06. INSTALLED POST IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,392 hrs · 21,743 cycles

FORWARD LIGHTED CEILING EXIT SIGN, MID CABIN INOPERATIVE. R & R NR 2 EMERGENCY BATTERY PACK IAW AMM 33-51-04-000/400-801. PERFORMED OPS TEST IAW AMM 33-51-04-740-801. OPS CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 23,391 hrs · 21,742 cycles

RIGHT WING LOWER SKIN IS CRACKED AT WS 148.019, APPROX .4" LONG. CRACK IS RADIATING FROM THE WING SKIN T/E FORWARD. CRACK IS OUT OF ALLOWABLE LIMITS OF MFG ALERT S/B A601R-57-031, REV A. JOINT STRAP FAILS NDT WITH AN INDICATION FULL SCREEN HEIGHT IAW NDTM 51-20-06. R & R JOINT STRAP PN 601R10336-44 IAW SRM 51-42-06. ECTC REQUIRED FOR REO 601R-57-51-578. REO 601R-57-51-578 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTD AND SIGNED FOR ON A NRI WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 3-3 PROCEDURES, PRIOR TO THE ACFT BEING RETURNED TO SERVICE. FUEL PANELS 640FB AND 650HB DUE LEAK CHECK. FUEL PANELS 640FB & 650HB LEAK CHECKED GOOD IAW AMM 28-11-00-790-802.

Part: PSEU — FAILED (MLG) · airframe 22,688 hrs · 20,982 cycles

PROXIMITY SYS CHANNEL MASTER CAUTION IN FLIGHT RAN QRH. EMERGENCY DECLARED. NORMAL LANDING. R & R PSEU IAW AMM 32-61-01. OPS CHECKED GOOD.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,288 hrs · 20,540 cycles

EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT CABLE IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,336 hrs · 18,381 cycles

FWD INTERIOR CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED CABIN FWD MOST CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,299 hrs · 18,340 cycles

LEFT FWD, EMERGENCY LIGHT INOP. RELAMPED LT FWD EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,851 hrs · 17,852 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW IAW AMM 33-51-16 / ITEM: 1. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW AMM 33-51-16.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,345 hrs · 17,280 cycles

NR 7 EXIT EMERGENCY LIGHT IS INOP. RELAMPED NUMBER 7 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21 OPERATIONAL CHECK GOOD.

Part: CABIN PRESSURE — FAILED · airframe 19,017 hrs · 16,918 cycles

AT 29000' CABIN ALT CAUTION AT 8500' THEN WENT TO RED WARNING AND ALL MASKS DROPPED AND HAD ALL GREEN DOOR INDICATIONS. (EMERGENCY DECLARED -- ENROUTE, ACFT DIVERTED DUE TO MX).

Part: FLOORBEAM — CRACKED (BS 621) · airframe 19,014 hrs · 16,912 cycles

RT FS 621.0 FLOORBEAM CRACKED. REPAIRED RT FS621.0 FLOOR ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT SEAT TRACK CORRODED APPROX. FS 559.0+111 TO FS 574.0 AT LBL 9.0 (MARKED).

Part: STOP FITTING — CORRODED (CARGO DOOR FRAME) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT DOOR CUTOUT FWD AND LWR STOP FITTINGS CORRODED AT FS 589.0 AND FS 605.0.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT SEAT TRACK CORRODED APPROX. FS559.0+111 TO FS574.0 AT RBL 9.0 (MARKED).

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT SEAT TRACK CORRODED APPROX. FS559.0+79 TO FS559.0+96 AT RBL 27.0 (MARKED).

Part: FLOORBEAM — CORRODED (BS 589) · airframe 19,014 hrs · 16,912 cycles

CORROSION DAMAGE ON FLOORBEAM FS 589.0 BETWEEN LBL 9.0 AND RBL9.0 (MARKED).

Part: FRAME — CRACKED (BS 559) · airframe 19,014 hrs · 16,912 cycles

FRAME CAP ANGLE CRACKED IN BEND RADIUS AT FS 559.00, LBL 18.00 AND RBL 18.00.

Part: SILL — CRACKED (BS 589) · airframe 19,014 hrs · 16,912 cycles

ANGLE BELOW CARGO COMPT DOOR SILL LANDING AT FS589.0 CRACKED. REMOVED AND REPLACED ANGLE BELOW CARGO COMPT DOOR SILL IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT SEAT TRACK CORRODED APPROX FS559.0+85 TO FS559.0+94 AT RBL 9.0 (MARKED).

Part: FLOORBEAM — CRACKED (BS 621) · airframe 19,014 hrs · 16,912 cycles

LEFT FS 621.0 FLOORBEAM CRACKED. REMOVED AND REPLACED REPAIR ANGLE AT LTS FS 621.0 IAW SRM 51-42-06, 51-42-20, 51-23-00 AND 51-21-16.

Part: SEAT TRACK — CORRODED (BS 615-618) · airframe 19,014 hrs · 16,912 cycles

CARGO COMPT SEAT TRACK CORRODED APPROX. FS 615.0 TO FS 618.0 AT LBL 9.0 (MARKED).

Part: SILL — CORRODED (FUSELAGE) · airframe 19,014 hrs · 16,912 cycles

CORROSION DAMAGE ON PAX DOOR SILL AREA MARKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 19,014 hrs · 16,912 cycles

CARGO BAY ALL SEAT TRACK SECTIONS CORRODED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,810 hrs · 16,695 cycles

EMER EXIT SIGN NEAR PAX DOOR FWD BULKHEAD WALL NOT ILLUMINATED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,447 hrs · 16,305 cycles

RT WING EXTERIOR OVERWING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,088 hrs · 15,945 cycles

RT REAR EXTERIOR EMERGENCY LIGHT WILL NOT WORK.

Part: WIRE — DAMAGED (CABIN) · airframe 1 hrs · 1 cycles

EMERGENCY FLOOR LIGHTING STRIP HAS DAMAGED WIRING AT CENTER WING BOX AREA, AIRFRAME SIDE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,504 hrs · 15,374 cycles

EN ROUTE FROM LGA TO CHS, RECEIVED RT REV UNLOCK MSG. RAN QRH, A/C DIVERTED TO BWI LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01.

Part: THRUST REVERSER — MALFUNCTIONED (RIGHT) · airframe 17,381 hrs · 15,281 cycles

DURING CLIMB RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO IND. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 16,710 hrs · 14,741 cycles

ON APPROACH, RECEIVED TWO MASTER WARNINGS, ONE FOR NOSE GEAR OPEN, THE OTHER FOR GEAR DISAGREE. ABORTED APPROACH, RAN QRH, MANUALLY EXTENDED GEAR, LANDED WITHOUT INCIDENT WITH GEAR INDICATING GREEN. REPLACED NLG SELECTOR VALVE. NO FURTHER DEFECTS.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 16,205 hrs · 14,314 cycles

FLIGHT 5531 - RIGHT ENGINE OIL PRESSURE ERRATIC IN FLIGHT AT NORMAL T/O THRUST SETTING. AIRCRAFT RETURNED BACK TO CVG LANDED SAFELY. FOUND RIGHT ENGINE OIL SERVICED. SERVICED RIGHT ENGINE, GROUND RAN A/C, OPS CHECK GOOD.

Part: BPSU — FAILED (T/E FLAP) · airframe 15,882 hrs · 14,069 cycles

FLIGHT 5440 - ON CLIMBOUT FROM JFK RECEIVED FLAPS FAIL CAUTION MESSAGE AT 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT RETURNED BACK TO JFK AND LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,355 hrs · 13,672 cycles

INBOARD BRACKET AT FS 280 RBL 9 CRACKED. REPLACED INBOARD BRACKET IAW CRJ SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 15,355 hrs · 13,672 cycles

INTERCOSTAL ATTACH ANGLE CRACKED IN UPPER CORNER FS 484 RBL 27. REPLACED ANGLE IAW CRJ SRM 51-42-21.

Part: PUMP — FAULTY (LT ENGINE) · airframe 13,433 hrs · 12,115 cycles

FLIGHT 9476 - EN ROUTE CVG-GRR LEFT ENGINE OIL PRESSURE INDICATION WAS ERRATIC, CREW DECLARED AN EMERGENCY AND PERFORMED AN IN-FLIGHT SHUTDOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE LUBRICATION MODULE.

Part: CHECK VALVE — FAULTY (LT ENG OIL PUMP) · airframe 13,429 hrs · 12,111 cycles

FLIGHT 9456 - EN ROUTE LGA-CVG RECEIVED A LEFT ENGINE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND PERFORMED AN INFLIGHT SHUTDOWN OF THE LEFT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE OIL PUMP CHECK VALVE.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 13,130 hrs · 11,875 cycles

FLIGHT 5222 - ANTI-ICE DUCT WARNING IN CLIMB. LEFT FUSELAGE DUCT ON EICAS WAS RED. CLEANED CONNECTORS FOR 14TH STAGE BLEED AIR LOOP IN LEFT WHEEL WELL. NO FURTHER DEFECTS.

Part: CAUTION MESSAGE — ACTIVATED (IDG) · airframe 12,787 hrs · 11,575 cycles

FLIGHT 5067 - EN ROUTE CVG-MYR RECEIVED AN IDG NR 1 CAUTION MESSAGE, FLIGHT DIVERTED TO CVG. PERFORMED RECONNECT OF NR 1 IDG, PERFORMED AN OPERATIONAL CHECK WITH NO DISCREPANCIES NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,617 hrs · 11,416 cycles

FLIGHT 5320 - LEFT WINDSHIELD CRACKED DURING CLIMB, DECLARED AN EMERGENCY AND RETURNED WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 11,363 hrs · 10,179 cycles

FLIGHT 5268- DURING TEST OF THE EMERGENCY LIGHTING, CABIN LIGHTS WOULD NOT ILLUMINATE. REPLACED THE EMERGENCY BATTERY PACKS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 11,363 hrs · 10,179 cycles

FLIGHT 5268 - DURING TEST OF THE EMERGENCY LIGHTING, CABIN LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 11,363 hrs · 10,179 cycles

FLIGHT 5268 - DURING TEST OF THE EMERGENCY LIGHTING, CABIN LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACK.

Part: CONTROL SYSTEM — MALFUNCTIONED (SPOILERS) · airframe 10,735 hrs · 9,616 cycles

FLIGHT 5045- FLIGHT SPOILER FAULT. DEFERRED MAINTENANCE PER MEL.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 11,363 hrs · 10,179 cycles

FLIGHT 5268 - DURING TEST OF THE EMERGENCY LIGHTING, CABIN LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS.

Part: PRESSURE PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 6,543 hrs · 5,947 cycles

FLIGHT 5096 CABIN ALTITUDE CAUTION DURING CLIMB. PERFORMED SYSTEM RESET OPERATIONAL CHECK OF PRESSURIZATION SYSTEM NORMAL.

Part: VALVE — MALFUNCTIONED (LEFT ANTI ICE) · airframe 5,851 hrs · 5,352 cycles

FLIGHT 5612 LEFT COWL ANTI-ICE MESSAGE. REPLACED THE ANTI-ICE VALVE.

Part: CONTACTOR — BURNED (UTILITY BUSS) · airframe 4,450 hrs · 4,137 cycles

FLIGHT 5374 DURING CRUISE FLIGHT THE ADG AUTO DEPLOYED, RECEIVED AN AC NR 1 TRU MESSAGE FOLLOWED BY SMOKE IN THE COCKPIT, AIRCRAFT DIVERTED TO RDU AND LANDED SAFELY. IT IS BELIEVED THAT THE UTILITY BUS CONTACTOR IK4XD OVERHEATED CAUSING COLLATERAL DAMAGE TO THE LT CONTACTOR TRAY AND WIRING.

Part: TRIM SWITCH — MALFUNCTIONED (INST PANEL) · airframe 3,962 hrs · 3,712 cycles

RUDDER TRIM WENT TO FULL NOSE LEFT WITH NO CREW COMMAND. REPLACED THE RUDDER TRIM CONTROL PANEL.

Part: ELEMENT — FALSE INDICATION (LT ANTI ICE DUCT) · airframe 3,420 hrs · 3,250 cycles

FLIGHT 5335 ANTI ICE DUCT WARNING MESSAGE. REPLACED THE LT WHEEL WELL DUCT LEAK SENSING ELEMENT.

Part: LAMP — BURNED OUT (CABIN) · airframe 3,211 hrs · 3,081 cycles

FLIGHT 5267 SERVICE DOOR EMERGENCY LIGHT IS INOP.REPLACED THE LIGHT BULB.

Part: SEAL RING · airframe 2,507 hrs · 2,471 cycles

FLIGHT 5667 LOUD SQUEAL FROM CABIN DOOR. F/A COULD SEE DAYLIGHT THROUGH DOOR SEAL.REPAIRED DOOR SEAL NIBS, PER SRM.

Part: ENGINE · airframe 878 hrs · 840 cycles

FLIGHT 5740 DURING LANDING APPROACH INTO AZO THE AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE RESULTING IN FLAMING OUT THE #1 ENGINE.PERFORMED A LIGHTNING STRIKE INSPECTION, REPAIRED MINOR AIRFRAME SKIN BURN MARKS AND PERFORMED SUCCESSFUL ENGINE RUNS.

Part: BUSS TIE · airframe 750 hrs · 800 cycles

FLIGHT 5117 AUTO XFER FAIL MESSAGE.RESET A/C BUSS 1 - MESSAGE CLEARED.