N538EG

Part: HYDRAULIC LINE — LEAKING (BRAKE) · airframe 32,764 hrs · 25,460 cycles

LOSS OF HYD PRESSURE ON SYS 2.QTY @ 0%. FOUND HYDRAULIC SYSTEM 2 LEAK COMING FROM FWD OUTBOARD BRAKE ACCUMULATOR LINE. OUTBOARD BRAKE ACCUMULATOR LINE TORQUED IAW CRJ 700 AMM 32-43-16-400-801-A01-PSA. HYDRAULIC SYSTEM #2 BLED AND SERVICED IAW CRJ 700 AMM 29€“10€“00€“870€“801.

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 31,586 hrs · 24,466 cycles

CA WINDSHIELD CRACKED IN FLIGHT, REMOVE AND REPLACED LH WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: WINDOW — SPARKS (ZONE 200) · airframe 29,732 hrs · 22,897 cycles

L WINDOW HEAT CAUTION WITH ELECTRICAL ARCING / REMOVED AND INSTALLED LH SIDE WINDOW IAW CRJ 700 AMM 56-12-01-000/400-801. PERFORM OPS TEST OF WINDOW HEAT CONT IAW CRJ 700 AMM 30-41-06-710-810. PRESSURIZED AND LEAK TEST A/C IAW CRJ 700 AMM 21-31-00-910-801 . ALL CHECK OK

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 1-1, 1-3 UPPER SURFACE & SLAT TRACK 1-2 UPPER/LOWER SURFACE; SLAT #1, RH WING

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 2-1, 2-3 UPPER SURFACE & SLAT TRACK 2-2 UPPER/LOWER SURFACE; SLAT #2 RH WING.

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 1-1, 1-3 UPPER SURFACE & SLAT TRACK 1-2 UPPER/LOWER SURFACE; SLAT #1 LH WING

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 2-1, 2-3 UPPER SURFACE & SLAT TRACK 2-2 UPPER/LOWER SURFACE; SLAT #2 LH WING.

Part: SKIN — DENTED · airframe 26,187 hrs · 191,783 cycles

DENT ON EXTERNAL FUSELAJE SKIN BTW FS STA 394 AND FS STA 409 BTW STGR 20RH AND STGR 19RH

Part: SKIN — NONE · airframe 26,187 hrs · 191,783 cycles

WEAR ON LOWER SKIN, BELOW FLAP HINGE BOX ACCESS PANELS, LH WING. (REF. WS 68, WS128, WS220 APROX).

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 3-1, 3-2 UPPER SURFACE, SLAT #3 RH WING

Part: CANISTER — CRACKED (ZONE 500) · airframe 26,187 hrs · 19,783 cycles

CRACK ON CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT CHORD INNER (3) BELOW LOWER SILL BTW FS1000 TO FS1047 AT AFT CARGO COMPARTMENT

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON STGR 26LH BTW . FS: 265 TO FS: 250 AT AVIONICS COMPARTMENT

Part: EXHAUST DUCT — BENT · airframe 26,187 hrs · 19,783 cycles

BENT APU EXHAUST DUCT AFT EDGE, SEVERAL LOCATIONS.

Part: ACCESS PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON ACCESS PANEL 699BB,542AZ

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

NICKS AND CORROSION ON SEVERAL AREAS OF SEAT RAIL LBL9 BTW FS677.00/863.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT RBL9 SEAT RAIL BETWEEN FS 677 AND FS 581(CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT SEAT RAIL BETWEEN FS 379 AND FS 485, STRG 15RH (CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,187 hrs · 19,783 cycles

NICKS, CORROSION & SCRATCHES ON LH SIDE SEAT RAIL (SEVERAL LOCATIONS), PAX CABIN. (REF. BTW FS379-FS469).

Part: SEAT TRACK — GOUGED · airframe 26,187 hrs · 19,783 cycles

GOUGES ON LATERAL SIDE RAIL STGR 15 LH BTW FS873.00/939.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT RBL9 SEAT RAIL BETWEEN FS 349 AND FS 485(CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AND GOUGES LATERAL SIDE RAIL STGR 15RH BTW FS 785.00/847.00

Part: RIB — CRACKED (ZONE 500) · airframe 26,187 hrs · 19,783 cycles

CRACK ON RIB LEADING EDGE SS57.16 AT LH WING

Part: SEAT TRACK — GOUGED (ZONE 100) · airframe 26,187 hrs · 19,783 cycles

GOUGES ON LATERAL SIDE RAIL STGR 15 LH BTW FS677.00/801.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT SEAT RAIL BETWEEN FS 677 AND FS 581, STRG 15LH

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT SEAT RAIL BETWEEN FS 485 AND FS 581, STRG 15RH (CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT RBL9 SEAT RAIL BETWEEN FS 485 AND FS 581(CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT LBL9 SEAT RAIL BETWEEN FS 581 TO FS 677.(CPAX)

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT LBL9 SEAT RAIL BETWEEN FS 485TO FS 581.

Part: FORMER — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD1 AND LOWER EDGE OF PASSENGER DOOR

Part: FORMER — CORRODED (ZONE 800) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD1 AND DD1A AT PASSENGER DOOR

Part: FORMER — CORRODED (ZONE 800) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION IN SEVERAL AREAS ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD6 AND DD5 AT PASSENGER DOOR.

Part: CANISTER — CRACKED (ZONE 600) · airframe 26,187 hrs · 19,783 cycles

CRACK AT CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

NICS AND CORROSION ON SEVERAL AREAS OF SEAT RAIL LBL9 BTW FS863.00/985.00.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

NICKS AND WEAR ON SEVERAL AREAS OF SEAT RAIL RBL9 BTW FS677.00/863.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT SEAT RAIL BETWEEN FS 581 AND FS 661, STRG 15RH

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION AT SEAT RAIL BETWEEN FS 573AND FS 485, STRG 15LH (CPAX)

Part: CANISTER — CRACKED (ZONE 600) · airframe 26,187 hrs · 19,783 cycles

CRACK AT CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON LATERAL SIDE RAIL STGR 15 RH BTW FS713.00/742.00

Part: SKIN — DAMAGED (ZONE 100) · airframe 26,187 hrs · 19,783 cycles

DAMAGED ANCHORED NUT BTW FS985 / FS1000 AND STGR 16LH / STGR 17LH AT AFT BAGGAGE BAY COMPARTMENT (CCT)

Part: STRINGER — CRACKED (ZONE 100) · airframe 26,187 hrs · 19,783 cycles

CRACK ON STRINGER 03L & FS280, INTERNAL STRUCTURE, PAX CABIN.

Part: STRINGER — CRACKED (ZONE 200) · airframe 26,187 hrs · 19,783 cycles

CRACK ON STRINGER 03L & FS280, INTERNAL STRUCTURE, PAX CABIN.

Part: SUPPORT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON PLATES SUPPORT FLOOR BTW FS1000 / FS1047 AND LBL 35.16 / LBL 40.74 AT AFT BAGGAGE BAY COMPARTMENT (CCT)

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON AFT CLOSING FITTING, PAX SURROUND STRUCTURE FUSELAGE FRAME (REF. SILL AREA ).

Part: COWLING — WORN (ZONE 500) · airframe 26,187 hrs · 19,783 cycles

WEAR (2 EAS) ON LOWER COWLING OF LH ENGINE. (MOT1)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 196AR AND 196DR.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON UPPER & LOWER SURFACE OF KEEL BEAM IN MLG WHEEL WELL.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON LH INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT.

Part: SLAT TRACK — CORRODED (ZONE 500) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

PITTING CORROSION ON SLAT TRACKS 3-1 UPPER SURFACE & SLAT TRACK 3-2 LOWER SURFACE; SLAT #3, LH WING.

Part: FLOORBEAM — GOUGED (ZONE 100) · airframe 26,187 hrs · 19,783 cycles

GOUGES ON FLOOR BEAM 27RBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY. (CCT)

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON FLOOR BEAM 9LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY. (CCT)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON FRAME (FWD/AFT SIDE) ON FS565.00 BTW STGRS 17-18LH.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,187 hrs · 19,783 cycles

CORROSION ON FRAME (FWD/AFT SIDE) ON FS565.00 BTW STGRS 17-18LH.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 21,900 hrs · 15,928 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR CRACKED. R/R SERVICE DOOR EMERGENCY EXIT SIGN LENS NO FURTHER DEFECTS NOTED. P/N: BF5-0830-905 S/N: BN117033

Part: SKIN — DAMAGED (BS 969-985) · airframe 21,898 hrs · 15,925 cycles

EXTERIOR FUSELAGE SKIN HAS 3 AREAS OF DAMAGE AT STR 27 BETWEEN FS969.00 AND FS985.00-C/A-COMPLETED REPAIR IAW ERS-CR-53MR-3979.

Part: FRAME — CORRODED (BS 310) · airframe 21,898 hrs · 15,925 cycles

FRAME AT FS310.00 CORRODED BETWEEN STR 25 LT TO STR 25 RT-C/A-REAPIRED FS310.00 BEWTEEN STR 25LT AND 25RT IAW ERS-CR-53MR-3982.

Part: FRAME — CORRODED (BS 319) · airframe 21,898 hrs · 15,925 cycles

FRAME AT FS319.00 CORRODED BETWEEN STRINGER 26 LT AND 27 LT.-C/A-REPAIRED FS319.00 BETWEEN STR 26LT AND 27LT IAW ERS-CR-53MR-3980.L

Part: FRAME — CORRODED (BS 295) · airframe 21,898 hrs · 15,925 cycles

FRAME AT FS295.00 BETWEEN STRINGERS 26 LEFT TO 26 RIGHT IS CORRODED.-C/A-REPAIRED FRAME AT FS295.00 IAW CRJ SRM CH. 53-00-06-201-006.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,898 hrs · 15,925 cycles

RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IS CRACKED, LOCATED JUST FWD OS FS280.00. -C/A-REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IAW SRM CH. 53-11-43-200-003.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,898 hrs · 15,925 cycles

LH CROSSBEAM AT FS280.00 IS CORRODED IN NUMEROUS PLACES BETWEEN DRIP TRAY AND UPPER L ANGLE.-C/A-COMPLETED INSTALL OF NEW LH FS280.00 CROSSBEAM IAW CRJ SRM CHS. 51-42-06 AND 51-42-13.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,898 hrs · 15,925 cycles

LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IS CRACKED, LOCATED JUST FWD OS FS280.00. -C/A-REPAIRED LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS280.00 IAW SRM 53-11-43.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,898 hrs · 15,925 cycles

RH CROSSBEAM AT FS280.00 IS CORRODED IN NUMEROUS PLACES BETWEEN DRIP TRAY AND UPPER L ANGLE.-C/A-COMPLETED INSTALL OF NEW RH FS280.00 CROSSBEAM IAW CRJ SRM CHS. 51-42-06 AND 51-42-13.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,215 hrs · 15,193 cycles

SUPPLEMENTAL AFT CARGO CAUTION MESSAGE IN FLIGHT. C/A-DEFERRED DOOR IND PER MEL 52-09. EXP 7/6/19. C/W OPS CK 52-31-00 OPS CK GOOD REF FIM 52-70-02 NO DEFECTS NOTED AT THIS TIME (AMM ) MEL RESTORED

Part: CONTROL MODULE — FAILED (NLG STEERING) · airframe 21,110 hrs · 15,087 cycles

NWS STEER INOP MESSAGE ON EICAS JUST AFTER TAKEOFF IN GSP. NORMAL LANDING IN ORD UNDER 61,000 LBS. UNABLE TO RESTORE NWS ON GROUND. EICAS MESSAGE STEERING INOP, BIT CODE: B1-007464/ B1-007466. T/S FIM TASK 32-51-50-810-801, POSSIBLE CAUSE NOSEWHEEL STEERING MANIFOLD UNSERVICEABLE. REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD IAW CRJ700 AMM 32-51-50. OPS CHECK AND LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,012 hrs · 15,001 cycles

FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. C/A-REMOVED AND REPLACED FLASHLIGHT ASSY IAW AMM CH. 25-61-02. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,344 hrs · 14,469 cycles

NR 1 FA FLASHLIGHT NOT CHARGING. C/A-REMOVED AND REPLACED NR 1 FA FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD. NO FURTHER DEFECTS.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 19,754 hrs · 13,958 cycles

DVT ALB LOW OIL PRESS (NO 1 ENG) EMERGENCY DECLARED. FLIGHT CXLD.-C/A-PENDING CORRECTIVE ACTIONS. REMOVED AND REPLACED LH ENG ASSY IAW WC-71-001 AND WC-71-002. SEE AML#4373191. NEW ENG CAME WITH ITS OWN HARNESS.

Part: WIRE HARNESS — SHORTED (OIL SYSTEM) · airframe 19,754 hrs · 13,958 cycles

SUPPLEMENTAL CLIMBING OUT OF PWM THRU ABOUT 20,000 FT L OIL LEVEL LO STATUS WENT FROM 57% TO 25%. CONTINUED TO DECREASE AFTER A SHORT TIME AND HELD AT 15% SLOWLY STARTED TO GET AMBER OIL PRESS FOLLOWED BY ENG OIL PRESS WARNING MSG. AS PER EPC AND CHECKLISTS SHUTDOWN LEFT ENGINE AND DIVERTED.-C/A-FOUND MDC MSG L OIL LO PRES SW/ LO PRESS & ENG RUNNING B21-007481. REF FIM 79-30-00-810-803. FOUND OIL TANK LEVEL INDICATOR CONNECTOR A87P46 SHORTED AND POPPING OIL IND BREAKER. REMOVED AND REPLACED W5 GREEN INDICATING HARNESS ON LT ENG IAW AMM 77-41-01 UP TO BUT NOT INCLUDING STEP 5. E OF CLOSE-OUT. BREAKER NO-LONGER POPPING AND OIL LEVEL IND POWERED. REMOVED AND REPLACED BOTH LT AND RT ENG OIL LEVEL TANK INDICATORS IAW AMM 79-31-09. OPC OF RT ENG GOOD. OIL TANK OIL LEVEL INDICATOR P/N 4121T65P02 S/N EEDE0413(LT) AND EEDE2187 (RT).REMOVED MAGNETIC ELECTRICAL CHIP DETECTOR AND RE-INSTALLED IAW AMM 79-21-05. FOUND LARGE AMOUNT OF DEBRIS ON DETECTOR. TOOK PICTURES AND SENT TO ENGINE GROUP. FOUND VISIBLY LOW OIL IN OIL TANK WITH NO SIGNS OF OIL LEAKS DURING DVI. REMOVED AND REPLACED LT ENG ASSY IAW WC-71-001 AND WC-71-002. SEE AML#4373191. NEW ENG CAME WITH ITS OWN HARNESS. ENGINE P/N CF34-8C5B1 S/N GEE965310

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,119 hrs · 13,445 cycles

RT AFT OVERWING EMERGENCY LIGHT INOP. R&R RT AFT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-51-15 OPC GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 19,112 hrs · 13,438 cycles

FA REPORTED THAT THE FLASHLIGHT BASE UNDER THE JUMPSEAT HAD BROKEN OFF, WILL NOT HOLD THE FLASHLIGHT IN PLACE. R & R THE FLASHLIGHT MOUNT ASSY IAW AMM 25-61-02. OPS CHECKED GOOD.

Part: A/C PACK — FAILED (NR 2) · airframe 18,995 hrs · 13,338 cycles

SMOKEY HAZE REPORTED DURING LANDING WITH SULFIRIC ODOR, ENGINE BLEEDS ONLY IN CABIN, EMERGENCY DECLARED. PERFORMED FIM 21-22-00, FOUND THE NR 2 PACK IN AUTOFAIL WITH NO OTHER DEFECTS NOTED. OK FOR SERVICE. REMOVED AND REPLACED THE NR 2 PACK IAW AMM 21-51-08. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,729 hrs · 13,112 cycles

FLOOR EMERGENCY LIGHT ADJACENT TO THE GALLEY WAS FOUND DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,492 hrs · 11,377 cycles

MID CABIN EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-17. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 16,492 hrs · 11,377 cycles

PORT SIDE, OVERWING EMERGENCY LIGHT DIM. REPLACED THE POWER SUPPLY. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM33-51-17. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 16,138 hrs · 11,097 cycles

STEERING INOPERATIVE CAUTION POST. RESET THREE TIMES AND FAILED ALL TIMES. REMOVED AND REPLACED STEERING MANIFOLD IAW AMM 32-51-50. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING) · airframe 16,116 hrs · 11,072 cycles

STEERING INOPERATIUVE CAUTION MESSAGE AFTER TAKE OFF. UNABLE TO RECOVER SYSTEM AFTER LANDING. TROUBLESHOT IAW FIM 32-50-00-810-802. NO CURRENT FAULTS NOTED. PERFORMED OPS CHECK OF THE NWS IAW AMM 32-51-00-710-801. OPS CHECKED GOOD. ACFT OK FOR CONTINUED SERVICE.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 16,076 hrs · 11,035 cycles

PAX DOOR AFT SIDE STEPSHELL ATTACH ANGLE HAS A ONE INCH CRACK BY THE BRACKET FOR ACTUATOR CABLE PULLEY. REPAIRED IAW SRM 52-11-04 AND TEMPORARY REVISION 52-0026.

Part: STEP — CRACKED (PAX DOOR) · airframe 16,076 hrs · 11,035 cycles

PAX DOOR FWD SIDE STEPSHELL HAS A .750 INCH CRACK ON PREVIOUS REPAIR BY SECOND STEP FROM BOTTOM. REPAIRED IAW SRM 52-11-04-201-004.

Part: STEP — CRACKED (PAX DOOR) · airframe 16,076 hrs · 11,035 cycles

PASSENGER DOOR AFT STEP SIDE SKIN HAS A CRACK AT PREVIOUS REPAIR BETWEEN TOP STEP AND MID-TOP STEP REPAIRED IAW SRM 51-11-04-201-004.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,076 hrs · 11,035 cycles

LT AND RT AFT OVERWING EMERGENCY LIGHTS BEHIND EMERGENCY EXITS AND AFT INTERIOR CEILING EMERGENCY LIGHTS BEHIND EMERGENCY EXITS NOT TURNING ON. REMOVED AND REPLACED NR 4 EPSU BATTERY AND CHARGER IAW AMM 33-51-17. OPS CHECK GOOD.

Part: QUICK DISCONNECT — LOOSE (BRAKE LINE) · airframe 16,014 hrs · 10,979 cycles

AFTER LANDING, NR 2 BRAKE TEMP AT 7. NR 1 BRAKE TEMP 0. NR 2 WAS SMOKING. NR 1 IS COLD TO TOUCH. INSPECTED AND FOUND THE 1 BRAKE QUICK DISCONNECT LOOSE. REINSTALLED IAW AMM 32-43-26, OPS CHECKED GOOD

Part: ECU — FAILED (NLG STEERING) · airframe 15,994 hrs · 10,958 cycles

STEERING INOPERATIVE MESSAGE ON EICAS CLIMBING THROUGH 400 FT . RETURN TO DEPARTURE. RESET SYSTEM IAW AOM 1 PROCEDURE. THE MESSAGE WENT AWAY. REMOVED AND REPLACED NWS ECU. OPS CHECKED GOOD IAW AMM 32-51-10

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 14,436 hrs · 9,785 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT BROKEN IN PIECES, INOPERATIVE. R & R AFT FLASHLIGHT IAW SMP.

Part: DOOR — DIRTY (CABIN) · airframe 14,151 hrs · 9,576 cycles

MAIN CABIN DOOR WILL NOT OPEN EITHER FROM INSIDE OR OUTSIDE OF ACFT. CLEANED & LUBED MAIN CABIN DOOR IAW STANDARD PRACTICES. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: ACTUATOR — MALFUNCTIONED (LT WING) · airframe 13,930 hrs · 9,409 cycles

OTBD SPOILERONS FAIL MSG. INTERROGATED MDC FOUND LT OTBD MFS PCU JAM. PERFORMED SPOST 1 RESET & OPERATIONS CHECKED IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD. DEFERRED LT OTBD MFS PCU ACTUATOR IAW ETN-CR-27-093. R & R LT OTBD MFS PCU ACTUATOR IAW AMM 27-62-01. OPERATIONS CHECKED GOOD & LEAK CHECKED GOOD. TDMI RESTORED.

Part: DCU — FAILED (WARNING SYSTEM) · airframe 13,642 hrs · 9,202 cycles

DURING CLIMB OUT ELEVATOR SPLIT CAUTION MSG POSTED ALONG WITH CAS MISCOMP STATUS MSG. COMPLIED WITH AOM 1 PROCEDURES. DETERMINED TO BE IND ISSUE. R & R BOTH DCU'S IAW AMM 31-41-04. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE. DATA DCU-4004 UNIT, PN 822-1310-106 & SN 2TFDP RFWD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,640 hrs · 9,200 cycles

TRANSFERRED FROM AML 3998257 ITEM 1 FOUND DAMAGE, BETWEEN FS 1031 & 1051, BETWEEN STRINGERS 21R & 26R, MAJOR REPAIR. REPAIRED SKIN IAW ERS-CR-53MR-1923.

Part: PCU — FAILED (SPOILER) · airframe 13,146 hrs · 8,796 cycles

EN-ROUTE CREW LOST ENG HYD PUMP 2A & HYD SYS 2 FLUID QTY BEGAN TO DROP. CREW DIVERTED WITHOUT INCIDENT. REMOVED AND REPLACED LT OB MFS PCU IAW AMM 27-62-01. PERFORMED OPS CHK IAW ETN-CR-27-093. TDMI RESTORED.

Part: TRANSCEIVER — FAILED (COCKPIT) · airframe 11,966 hrs · 7,820 cycles

ON APPROACH FIRST OFFICER`S RADAR ALTIMETER FAILED, CAUSING GLD UNSAFE CAUTION & SPOILER STAB FAULT STATIC MSG. GEAR AMBER INDICATIONS & TOO LOW GEAR AURAL MSG. MEL 34-48 M PROCEDURES COMPLIED WITH. EXPIRATION DATE 06 07 15. DEFERRED RAD ALT NR 2 FIRST OFFICERS. R & R NR 2 RADAR ALTIMETER TRANSCEIVER IAW AMM 34-44-01. OPERATIONS CHECKED GOOD.

Part: DUCT — BLOCKED (CABIN) · airframe 11,619 hrs · 7,536 cycles

FLIGHT ATTENDANT 2 REPORTS BURNT PLASTIC SMELL AFTER LANDING. SMELL WAS IN REAR PORTION OF CABIN. SMELL REMAINED FOR 2 MINUTES & POSSIBLY STARTED WHEN BLEEDS WERE SWITCHED TO THE APU. REFERENCE NRWC 8EG-DFW-01305 ITEM 2 & 3. REMOVED BLOCKAGE IN CABIN SPLITTER & CLEANED TEMP SENSORS. OPERATIONS CHECKED GOOD IAW MM 21-51-00.

Part: FAN — FAILED (RECIRCULATION) · airframe 11,610 hrs · 7,526 cycles

UNUSUAL ODOR DURING TAXI IN WHEN POWERING APU & THE BLEEDS SWITCH OVER TO APU. ODOR IS SIMILAR TO HOT ELEC EQUIP OR HOT DRYER VENT. R & R NR 1 RECIRCULATION FAN. PERFORMED OPS CHECK OF AIR CONDITIONING SYS WITH APU RUNNING IAW AMM 21-51-00. NO FAULTS NOTED & NO ODORS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,608 hrs · 7,523 cycles

STRONG SCENT OF BURNING ODOR AFTER LANDING & AFTER BLEED CHANGE OVER FROM ENGINES TO APU. REPAIRED RISER DUCT BETWEEN 16CD AND 17CD IAW ERS-CR-25-047 PTA.VERIFIED THAT NR 2 RECIRCULATION FAN CHECK VALVE IS INSTALLED PROPERLY IAW AMM 21-22-10. OPS AND LEAK CHECKED GOOD. NO BLOCKAGE OR OBSTRUCTIONS NOTED IN RT RECIRCULATION FAN DUCTING IAW AMM 21-23-34. OPS AND LEAK CHECKED GOOD. INSPECTED RT RECIRCULATION FAN INLET IAW AMM 21-23-25. NO OBSTRUCTIONS NOTED WITH STRONG AIRFLOW GOING INTO INLET.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 11,605 hrs · 7,521 cycles

STRONG PLASTIC BURNING ODOR IN THE COCKPIT & CABIN AFTER PARKING AT THE GATE. NO VISIBLE SMOKE NOTED. TROUBLESHOT SYS , FOUND GALLEY EXHAUST FAN INOPERATIVE, CONNECTOR DISCONNECTED. RECONNECTED GALLEY EXHAUST FAN CONNECTOR. OPERATIONS CHECKED GOOD. FOUND PAPER & FOAM IN DUCTING AT SEAT 2 CD PSU GASPER. PERFORMED ENG RUNS WITH BLEED AIR & PACKS IAW FORM OPC OF INTERIOR LIGHTING, COULD NOT DUPLICATE ODOR ON THE GND, ALL WORK IAW AMM TASKS 21-23-93, 25-28-01 & 71-00-00. CHECKED RECIRC FILTERS, FOUND NR 1 RECIRC FILTER HOUSING UNATTACHED & MOUNTING BOLTS LAYING ON THE FLOOR. ATTACHED FILTER HOUSING IAW AMM 21-22-10.

Part: CARPET — DIRTY (CABIN) · airframe 11,603 hrs · 7,519 cycles

STRONG PLASTIC BURNING SCENT WHILE TAXING, APPROACH & LANDING FOR ABOUT 1 MINUTE EACH TIME. FLIGHT ATTENDANT 1 SAID IT WAS IN CABIN FOR ABOUT 5 MINUTES. INSPECTED COCKPIT & CABIN TO IDENTIFY SOURCE OF ODOR OR SMELL. COCKPIT FLOOR TO BE DIRTY & STINKY WITH FOOD RESIDUE & CABIN CARPET AT 14BC SPILL STAIN WITH BURN PLASTIC ODOR. SEE ITEMS 3 & 4 FOR FURTHER CORRECTIVE ACTION. PERFORMED A CLEANING OF CARPET STAIN, SPILL & SMELLING OF LIKE BURNT PLASTIC IAW AMM 25-25-00-110-801. NO ODOR OR SMELL NOTED AT THIS TIME. PERFORMED AIR DISTRIBUTION LEAK TEST IAW AMM 21-20-00-790-801. NO LEAKS, ABNORMAL NOISES OR ODORS NOTED AT THIS TIME FROM AIR DISTRIBUTION SYS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,262 hrs · 6,449 cycles

EMERGENCY BATTERY INOPERATIVE. REMOVED EMER BATTERY PN 2013-1A & SN 68591.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

NUMEROUS EMER LIGHTS INOPERATIVE FROM BATTERY PACK NR 1. R & R NR 1 EPSU BATTERY CHARGER & OPERATIONS CHECKED GOOD IAW AMM 33-51-17.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

BATTERY POWER SUPPLY NO POWER OUTPUT. REMOVED BATTERY POWER SUPPLY PN 11-0049 & SN 13109.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

BATTERY POWER SUPPLY NUMEROUS LIGHTS FROM BATTERY & CHARGER NR 1 INOPERATIVE. REMOVED BATTERY POWER SUPPLY PN 11-0049 & SN 18892.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

NUMEROUS EMER LIGHT INOPERATIVE FROM BATTERY PACK NR 2. R & R NR 2 EPSU BATTERY CHARGER & OPERATIONS CHECKED GOOD IAW AMM 33-51-17.

Part: EPSU — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

EMERGENCY LIGHTS DS55 & DS54 ARE INOPERATIVE. R & R EPSU NR 4 & BATTERY PACK FOR EMER LIGHTS DS55 & DS54 IAW AMM 33-51-17. ALSO FOUND LOOSE CONNECTIONS. RECONNECTED & OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 10,262 hrs · 6,449 cycles

BATTERY POWER SUPPLY NUMEROUS LIGHTS FROM BATTERY & CHARGER NR 2 INOPERATIVE. REMOVED BATTERY POWER SUPPLY PN 11-0049 & SN 24457.

Part: HOLDER — INOPERATIVE (FLASHLIGHT) · airframe 10,166 hrs · 6,382 cycles

NUMBER 1 FLIGHT ATTENDANT FLASHLIGHT HOLDER INOPERATIVE. R & R FLIGHT ATTENDANT NR 1 FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — MISINSTALLED (CABIN) · airframe 10,101 hrs · 6,333 cycles

NUMBER 1 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. FOUND FLASHLIGHT INSTALLED WRONG. RE POSITION AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 25-61-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 9,596 hrs · 6,008 cycles

FLIGHT ATTENDANT 1 FLASHLIGHT INOPERATIVE, WILL NOT CHARGE IN EITHER HOLDER. R & R FLIGHT ATTENDANT 1 FLASHLIGHT BATTERY AS REQUIRED, OPERATIONS CHECKED GOOD.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 8,929 hrs · 5,588 cycles

FLIGHT ATTENDANT NR 1 REPORTS PAX DOOR HANGING UP WHEN OPENED HAS TO PULL IT BACK IN & PUSH OUT, WORKED ON 3RD TRY. DEFERRED DOOR ASSIST IAW MEL 52-1 AUTH 010163DM-C MTX PROCEDURES COMPLIED WITH.

Part: SWITCH — INOPERATIVE (TRIM UP) · airframe 8,122 hrs · 5,071 cycles

CAPTAIN'S NOSE UP STAB TRIM FAILED. NOSE DOWN TRIM NORMAL. F/O'S SIDE NORMAL. R & R PITCH TRIM SWITCH IAW AMM 27-41-05.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 7,130 hrs · 4,456 cycles

THE CREW REPORTED THE F/O`S FLASHLIGHT HOLDER WAS CRACKED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O’S FLASHLIGHT HOLDER IAW AMM 3 25-61-02. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (SPOILER) · airframe 6,995 hrs · 4,361 cycles

ON FLIGHT 4657 DURING CRUISE AT LIGHT LEVEL 3400 THE CREW REPORTED THEY RECEIVED A RUDDER, INBOARD FLIGHT SPOLIER AND INBOARD SPOILERS MESSAGE ON ED 1. THE CREW FOLLOWED THE APPROPRIATE CHECKLIST AND AOM VOL 1 AND DECLARED AN EMERGENCY AND RETURNED TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 SSCU IAW CRJ AMM 27-61-05. THE OPERATIONAL CHECK WAS GOOD NO MSG ON EICAS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 6,428 hrs · 4,025 cycles

ON FLIGHT 3876 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT FELL OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW CRJ-700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 5,821 hrs · 3,645 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY FLASHLIGHT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BROKEN FLASHLIGHT WITH A NEW UNIT IAW CRJ AMM 25-61-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LE SLAT) · airframe 5,574 hrs · 3,487 cycles

ON FLIGHT 3650 ON LANDING THE CREW REPORTED, RECEIVED A SLATS FAIL CAUTION MESSAGE UPON FLAP EXTENSION. THE SLATS STUCK IN THE 1 DEGREE POSITION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK AND VISUAL CHECK OF SLAT SYSTEM IAW CRJ 700 FIM 27-81-09-810-802. NO DEFECTS NOTED ON SLAT SYSTEM. AIRCRAFT OK FOR SERVICE. MESSAGE CLEARED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (FLASHLIGHT) · airframe 5,206 hrs · 3,256 cycles

ON FLIGHT 3777 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT RECHARGER WAS INOPERABLE. COMPLIED WITH MAINTENANCE PROCEDURES. FOUND A BREAK IN THE POWER WIRE GOING TO THE FORWARD CHARGER. REPAIRED IAW SWPM. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (FLASHLIGHT)

DURING B-INSPECTION, FOUND COPILOTS FLASHLIGHT CHARGER BROKEN, WILL NOT HOLD FLASHLIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED COPILOTS FLASHLIGHT AND CHARGER ASSEMBLY IAW AMM 25-61-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 3,222 hrs · 2,016 cycles

DURING MAINTENANCE BASE CHECK FOUND THAT THE FIRST OFFICER’S FLASHLIGHT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED FIRST OFFICER’S FLASHLIGHT AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAILED (MLG BRAKE) · airframe 2,232 hrs · 1,416 cycles

ON FLIGHT 4642 THE CREW REPORTED THAT ON DESCENT INTO YYZ GOT BRAKE OVERHEAT WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY INTO YYZ LANDED SAFELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MDC DOWNLOAD WITH MFD VERIFIED NR 3 TEMPERATURE SENSOR INTERNAL FAILURE CRJ-700 AMM 45-45-00. REMOVED AND REPLACED NR 3 IAW AMM 32-46-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECEPTACLE — FIRE (LAVATORY) · airframe 153 hrs · 87 cycles

ON FLIGHT 3703 DURING DESCENT THE FLIGHT ATTENDANT REPORTED A FIRE IN THE LAVATORY TRASH RECEPTACLE AND HAD TO USE THE FIRE EXTINGUISHER TO PUT OUT FIRE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED AT ATL WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FIRE EXTINGUISHER IAW CRJ MM 26-23-01. THE AIRCRAFT WAS RETURNED TO SERVICE.