N528CA

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,902 hrs · 20,126 cycles

FWD ORANGE SEGMENT OF EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT FLEXIBLE LAMP NR 1 IAW AMM 33-51-01. OPS CHECK GOOD. SDR CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,669 hrs · 19,891 cycles

CABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP, ORANGE, INOPERATIVE. PERFORMED THE OPS TEST OF THE EMERGENCY FLOOD LIGHTS IAW AMM 33-51-00. OPS CHK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 20,683 hrs · 18,846 cycles

EMERGENCY LIGHT STRIP ABOVE PAX DOOR DOES NOT ILLUMINATE. REINSTALLED CONNECTOR FOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 19,945 hrs · 18,070 cycles

EMERGENCY LIGHT AT ROW 5 INOPERATIVE. FOUND BATTERY PACK TO BE DISCHARGED. CHARGED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 19,928 hrs · 18,052 cycles

RT OTBD FLAP DAMAGED ON T/E. 41" FROM INBD END, DAMAGE IS APPROX 10" L. COMPLIED WITH MAJOR REPAIR IAW REO 601R-57-53-041, REV A, DATED 2004/05/07. COMPLIED WITH EC/TC EO 600-57-0128 02.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 19,928 hrs · 18,052 cycles

AT FS 621.00 BULKHEAD LBL 30 WL 135 THERE IS A DRILL START .150" WIDE .031" DEEP AND .150" FROM CENTER OF FIRE BLOCK HOLE/NUTPLATE AT .1562" TO CENTER OF DRILL START. COMPLIED WITH MAJOR REPAIR IAW REO 601R-53-61-4873, DATED 2013/04/11. COMPLIED WITH EC/TC REO 601R-53-61-4873.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 19,928 hrs · 18,052 cycles

PRESSURE FLOOR SKIN HAS 1 EA DENT MEASURING 4.256" LONG X 1.980" WIDE X .015" DEEP AND HAS 5 EA GOUGES WITH MAX DAMAGE BEING .730" LONG X .062" WIDE X .008" DEEP WITH HIGH METAL AT FS 553 BETWEEN LBL 0 AND LBL 9 AND IS NOT WITHIN REPAIRABLE LIMITS IAW SRM 53-41-45. REPAIRED IAW REO 601R-53-44-1679, 601R-53-41-1680.

Part: BUSHING — DAMAGED (HORIZONTAL STAB) · airframe 19,920 hrs · 18,043 cycles

LT BUSHINGS AT HORIZONTAL STAB HINGE ARE DAMAGED. REPAIRED IAW REO 601R-55-00-045 REV B, 2013/04/27. MAJOR REPAIR

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 19,902 hrs · 18,020 cycles

FS 621.00 CRACKED INTERCOSTAL STRINGER 13L,. REMOVED CRACKED INTERCOSTAL IAW SRM 51-42-21. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (AFT) · airframe 19,902 hrs · 18,020 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,902 hrs · 18,020 cycles

FOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E, DATED: 08/24/2010, REO 601R-53-41-609, REO 601R-53-41-609 01, AND REO 601R-53-41-609, REV B (SHEET 3 TO 11 REV A) FOR DEVIATION D.

Part: POST — CRACKED (BS 409) · airframe 19,902 hrs · 18,020 cycles

FOUND FS 409.00+128 VERTICAL POST BL 0.00 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED LT & RT POST BL 0 FS 409+128 IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: CIRCUIT CARD — UNSERVICEABLE (FCC) · airframe 19,608 hrs · 17,704 cycles

UNCOMMANDED FULL RT RUDDER DEFECTION IN FLT ON A/P, NO EICAS MSG OVER POWERED, DISCONNECTED A/P AND YD, WERE ABLE TO RETRIM (ENROUTE, ACFT DIVERTED TO GSO DUE TO MX) R & R NR 1 AND NR 2 FCC CARDS IAW AMM 22-12-14 , OPS CHECK GOOD IAW AMM 22-12-14 IOC REF 22-12-14 ITEM 5 . R & R AILERON/RUDDER TRIM PANEL IAW AMM 27-12-10, OPS CHECK GOOD IAW AMM 27-22-00.

Part: SWITCH — ILLUMINATED (THRUST REVERSER) · airframe 18,681 hrs · 16,760 cycles

LEFT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. R & R STOW SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD.

Part: SENSING ELEMENT — BROKEN (OVERHEAT LOOP) · airframe 18,195 hrs · 16,220 cycles

LT 10TH DUCT IN FLIGHT FOLLOWED CHECK LIST IT DID NOT GO OUT. DELCARED EMERGENCY AND RETURNED TO ATC (AFTER T/O ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND SENSING ELEMENT A48WK BROKEN. R & R SENSING ELEMENT A48WK IAW AMM 36-21-04. OPS TEST OF BLEED AIR LEAK DETECTION AND WARNING SYS GOOD IAW AMM 36-21-00. NO FURTHER DEFECTS NOTED AT THIS TIME. (SDR CLOSED)

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 17,971 hrs · 15,984 cycles

REAR PRESSURE BULKHEAD CRACKED AT RBL 36.20. REPAIRED IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-1285 REV D.

Part: FITTING — CRACKED (PRESSURE BLKHD) · airframe 17,971 hrs · 15,984 cycles

REAR PRESSURE BULKHEAD CRACKED AT MACHINE FITTING (LINTEL FITTING) AT CARGO DOOR CUTOUT. REPAIRED IAW REO 601R-53-61-1230, REV C.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 17,971 hrs · 15,984 cycles

WIRE BROKEN ON EMERGENCY FLOOR TRACK LIGHTING AT FWD END. REPLACED CRIMP CONNECTOR ON RT FWD EMERGENCY LIGHT FLOOR STRIP LIGHTING WIRE IAW ESPM 20-17-00. OPS TESTED IAW AMM 33-51-00-710-801. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 16,899 hrs · 14,814 cycles

EMERGENCY LIGHTS INOPERATIVE, CENTER TWO SECTIONS AND FWD WHITE SECTION AT FLOOR POSITIONS. R & R FWD WHITE EMERG LIGHT SECTION IAW AMM 33-51-01-000-801 AND 33-51-01-400-801. FOUND 2 SETS OF CONNECTORS (MALE/FEMALE) NOT TERMINATED ON LIGHT STRIP INSTALLED CONNECTOR IAW ESPM 20-17-10. R & R CABLE CONNECTOR AT POSITION C IAW AMM 33-51-01-000-801 AND 33-51-01-600-801. OPS TESTED EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. TESTED GOOD.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 16,893 hrs · 14,806 cycles

CARGO DOOR FWD TRACK LOWER C-CHANNEL ANGLE CRACKED. R & R DAMAGED C-CHANNEL IAW SRM 51-41-06 & 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,893 hrs · 14,806 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRE IAW REO 601R-52-11-513 AND REO NR 610R-52-11-513, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,893 hrs · 14,806 cycles

FS 280 TRANVERSE BEAM UPPER AFT J-ANGLE CRACKED OTBD OF LBL 9 AND RBL 9. REPAIRED IAW REO 601R-53-11-926 REV B.

Part: BEAM — CRACKED (BS 280) · airframe 16,893 hrs · 14,806 cycles

FS 280 TRANSVERSE BEAM CRACKED IN WEB OTBD OF RBL 9. THIS DISCREPANCY AND THE AFT J-ANGLES ON JOB 8784121, OP 159 IS BEING REPAIRED AS ONE IAW REO 601R-53-11-926.

Part: WEB — CRACKED (PAX DOOR) · airframe 16,893 hrs · 14,806 cycles

PASSENGER DOOR FWD WEB CRACKED AT 4TH RISER. REPAIRED IAW REO 601R-52-11-702.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 16,893 hrs · 14,806 cycles

PASSENGER DOOR CUTOUT LOWER ANGLE HAS CORROSION AROUND HOLE FOR PROXIMITY SENSOR. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND THE REMOVED MATERIAL (0.003) WITHIN THE LIMIT IAW SRM 53-00-00 AND SRM 53-21-023.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 16,893 hrs · 14,806 cycles

CLIP AT FS 484.00, RBL 27 CRACKED. R & R A NEW CLIP AT FS 484.00, RBL 27 IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: DOOR — NONE (EMERGENCY EXIT) · airframe 16,893 hrs · 14,806 cycles

LEFT EMERGENCY OVERWING EXIT FAILS FUNCTION TEST, FORCE TO OPERATE HANDLE EXCEEDS 40 LBS. PERFORMED FUNCT TEST OF THE LT EMERGENCY EXIT IAW AMM 52-21-00-720-801. FUNCTION TEST GOOD AT 35LBS.

Part: DOUBLER — CRACKED (BS 640) · airframe 2,794 hrs · 2,414 cycles

LT SIDE FS 640.00 DOUBLER CRACKED AT CUTOUT RADIUS FOR ENGINE SUPPORT BEAM ATTACH POINT. REPAIRED.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 2,799 hrs · 2,418 cycles

FS 625, OBLIQUE CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-42-20. COMPLIED WITH EDDY CURENT INSP IAW NDTM 51-20-06, PART 1 53-00-096, PART 6 AND COMFIRMED CRACK. INSTALLED NEW CLIP IAW REO 601R-53-61-100 AND REO 601R-53-61-422.

Part: WARNING SYSTEM — ACTIVATED (NLG) · airframe 16,094 hrs · 13,965 cycles

GEAR DISAGREE NOSE DOOR WARNING NOSE GEAR NEVER CAME UP DEFERRED PER MEL 32-30-01.

Part: CONNECTOR — DIRTY (FIRE BOTTLE) · airframe 15,502 hrs · 13,388 cycles

DURING CLIMB, PASSING 27000FT CARGO BOTTLE LOW CAUTION MESSAGE CAUTION MESSAGE EXTINGUISHED DESCENDING THROUGH 11000FT. REMOVED, CLEANED, RESECURED CONNECTOR ON CARGO BOTTLES, TEST GOOD PER CRJ AMM 26-20-00.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 15,198 hrs · 13,096 cycles

FUMES IN COCKPIT/CABIN LED TO DIVERSION. APU OFF/BLEEDS ON ENGINES/SMELLED LIKE CIGARETTE BURNING/NO VISIBLE SMOKE. PERFORMED GROUND RUNS WITH BLEEDS ON ENGINES AND APU NO FUMES OR SMOKE NOTED. PER 71-00-00 OPS CHECKED 1 AND 2 PACKS PER 21-50-00 OPS GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 1,106 hrs · 1,029 cycles

UPON CLIMBOUT AFTER THE CLIMB CHECK, HAD A GEAR DISAGREE MSTR WARNING. THE NOSE GEAR WAS THE ONE IN DISAGREEMENT. THE F/O START THE QRH, THE WARNING WENT AWAY. A/C RETURNED TO DTW AND MAINTENANCE REMOVED AND REPLACED THE NLG SELECTOR VALVE IAW AMM 32-20-00.

Part: ECU — FAULTY (TE FLAPS) · airframe 9,721 hrs · 8,530 cycles

FLIGHT 5011 - FLAP FAIL CAUTION RECEIVED ON TAXI OUT. RETURNED TO GATE. REPLACED FECU. NO FURTHER DEFECTS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,967 hrs · 7,918 cycles

CAPTAIN'S WINDSHIELD INNER PANEL SHATTERED. PROCEEDED TO CVG WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,738 hrs · 7,738 cycles

FLIGHT 5115 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: SHAFT — DAMAGED (TE FLAPS) · airframe 8,671 hrs · 7,685 cycles

FLIGHT 5510 - FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046 AD INCLUDING FLAP SHAFT REJUVENATION. NO FURTHER DEFECTS.

Part: SKIN PANEL — CRACKED (DOOR) · airframe 7,827 hrs · 6,899 cycles

PAX DOOR SECOND STEP DOWN FORWARD AND AFT SKINS CRACKED UNDER BRACKETS WHERE HAND RAILS STOW WHEN DOWN. AFT SKIN ALSO CRACKED THIRD STEP DOWN IN RADIUS OF TREAD/RISER. REMOVED DAMAGED AREAS OF PAX DOOR FORWARD AND AFT SKINS SECOND STEP, AND THIRD STEP AFT SKIN IAW EA 10-5211-01344.

Part: GENERATOR — FAULTY (AVIONICS BAY) · airframe 6,750 hrs · 5,841 cycles

FLIGHT 5104 - CLIMBING OUT OF AUS DURING GEAR RETRACTION, THE AIR DRIVE GENERATOR DEPLOYED, FLIGHT RETURNED TO THE FIELD. REPLACED THE ADG AUTO DEPLOY CONTROL PANEL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 4,436 hrs · 3,844 cycles

FLIGHT 5380 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW.

Part: HYDRAULIC SYSTEM — LOW (NR 3) · airframe 3,983 hrs · 3,441 cycles

FLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. SERVICED THE NR 3 HYDRAULIC SYSTEM.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 1,795 hrs · 1,591 cycles

FLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PITOT SYSTEM LINE.

Part: CONTROL UNIT — MALFUNCTIONED (AVIONICS) · airframe 946 hrs · 858 cycles

FLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU.

Part: ENGINE — FLUCTUATES · airframe 828 hrs · 758 cycles

FLIGHT 5732 N1 AND N2 AND F/F FLUCTUATING. COULD NOT DUPLCIATE. GROUND RUNS WERE NORMAL AND SATISFACTORY.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 13 hrs · 23 cycles

DURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES.