N542EA

Part: TRANSCEIVER — FLUCTUATES (ZONE 200) · airframe 31,234 hrs · 24,346 cycles

IN-FLIGHT AT FL20.0 WE EXPERIENCED THE RA START TO MAKE 25.00FT, 500FT, 100FT CALL OUTS AND FLUCTUATE. / REMOVED AND REPLACED RAD ALT #1 IAW CR7 AMM 34-44-01-000/400-801-A02-PSA. BIT CHECKS GOOD.

Part: HOSE — CHAFED (ZONE 100) · airframe 31,043 hrs · 24,176 cycles

HYD SYSTEM 2 LOW PRESSURE CAUTION MESSAGE IN FLIGHT WITH 0% QUANTITY. FOUND HYD 2 DAMPENER FLEX HOSE TO BE CHAFED THROUGH BY ADEL CLAMP. REMOVED AND REPLACED HOSE AND CLAMP IAW AMM 29-11-59-000/400-801. OPS CHECK/LEAK CHECK GOOD.

Part: STEERING SYS — MALFUNCTIONED (ZONE 700) · airframe 30,245 hrs · 23,503 cycles

STEERING INOP AFTER TAKEOFF. / PERFORMED OPS CHECK OF THE NOSEWHEEL STEERING IAW CRJ700 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.

Part: SKIN — DENTED (ZONE 100) · airframe 29,984 hrs · 23,290 cycles

DENT ON LH FUSELAGE AFT OF AFT NLG DOOR. / REPAIRED LH FUSELAGE BETWEEN FS250.00- FS265.00 STR24L-STR23L IAW REO 670-53-11-2096 AND CRJ700 SRM REF 51-42-21.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,334 hrs · 22,737 cycles

SMOKE CONDITION IN CABIN, CONDITION IMPROVED WHEN PACKS SHUT OFF. / INSPECTED AIRCRAFT IAW CRJ700 FIM 21ˆ’21/22ˆ’00ˆ’810ˆ’806-A01 AND FOUND B1 CODE 211943--RH PACK AUTOFAILED CAUTION MSG DISPLAYED. ISOLATED ISSUE TO THE RH PACK, VENTIALATED AIRCRAFT CABIN AS REQUIRED, RAN LH PACK ON APU AND R ENGINE (ONLY ENGINE RUNNING AT THE TIME OF FAULT) AS A BLEED SOURCE, NO SMOKE, SMELL OR FUMES NOTED

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON STRINGER 27 BTW FS 349.00 TO FS 353.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION WAS FOUND ON STRINGER SPLICE FS 333.00 ON STRINGER 23RH AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 27,711 hrs · 19,595 cycles

CRACK ON STRINGER ATTACHED ANGLE ON STGR 7LH FS1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON STRINGER 24RH BTW FS 333.00 TO FS 364.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON FRAME AT STGR 26LH & FS1031.00 AT AFT BAGGAGE BAY.

Part: STRIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON METALIC STRIP (1EA) AT FORWARD UNDERWING FAIRNG 193AB.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS863 - FS969

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS 581 - FS 661

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS708+5 - FS 761.00

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS581.40 - FS677.0

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS349.0 - FS485.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS485.0 - FS581.0

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL BETWEEN FS847+5 - FS967 ON STRINGER 15RH

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION WAS FOUND ON INTERCOSTAL AT STRINGER 20R, BTW FS 310.00 AND FS 319.70 ON MAIN AVIONICS COMPARTMENT

Part: NONE — GOUGED (ZONE 100) · airframe 25,711 hrs · 19,595 cycles

SCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17RH

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL BETWEEN FS708+4 - FS761 ON STRINGER 15RH

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION AT SEAT RAIL BETWEEN FS785+4 - FS847+15 ON STRINGER 15RH

Part: NONE — CORRODED (ZONE 100) · airframe 25,711 hrs · 19,595 cycles

CORROSION ON WHEEL BINS ATTACHMENT ANGLES (2 EA) BTW FS 797.00 TO FS 830.40 RBL 16 AND LBL 49 ON MAIN WHEEL WELL

Part: NONE — GOUGED (ZONE 100) · airframe 25,711 hrs · 19,595 cycles

SCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17LH

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION WAS FOUND ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,711 hrs · 19,595 cycles

CORROSION ON STRINGER 22RH BTW FS 333.00 TO FS 349.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE

Part: NONE — CRACKED (ZONE 600) · airframe 27,711 hrs · 19,595 cycles

CRACK ON AFT BACKING OF REFUEL DUCT SUPPORT STRUCTURE ON FS 679.00, BTW STGR 22RH AND 21RH.

Part: NONE — CRACKED (ZONE 800) · airframe 25,711 hrs · 19,595 cycles

CRACKS ON LOWER PRESSURE SEAL RETAINER BOTH CORNERS AT FWD BAGGAGE BAY DOOR

Part: GUST LOCK — FALSE INDICATION · airframe 24,633 hrs · 18,647 cycles

AS PILOT FYING ON SHORT FNAL INTO RWY 16 AT HPN (<500'AGL), GOT A GLD RELATED MASTER CAUTION MSG. DUE TO THE SHORT RUNWAY AND DOWNHILL SLOPE, I COMMENCED A GO-AROUND. MESSAGE EXTINGUISHED DURING THE CLIMB OUT BEFORE I COULD ASCERTAIN THE EXACT MESSAGE. GOT DELAY VECTORS, AND REVIEWED THE QRC/QRH FOR GLD MESSAGES. DISCUSSED WITH FO, AND BECAUSE WE HAD PLENTY OF FUEL (6,000LBS OF TANKER) CONCURRED IN MAKING A SECOND APPROACH, BUT BREAKING IT TO IF THE MESSAGE REAPPEARED. ON SECOND APPROACH, MESSAGE REAPPEARED AND WE WENT AROUND. THIS TIME, FO WAS ABLE TO VERIFY THAT IT WAS GLD NOT ARMED. REVIEWED THE QRH AGAIN, AND MESSAGED DISPATCH TO DISCUSS WHETHER TO DIVERT AND PREFERRED DIVERSION ?ELD (PHL WAS ?LED ALTERNATE DUE TO WEATHER). GIVEN THE REASONS MENTIONED BEFORE (SHORT, DOWNHILL RUNWAY AND TIGHT LANDING NUMBERS) DECIDED TO DIVERT TO PHL FOR: 1) LONGER RUNWAY, 2) ON FIELD PRESENCE OF CONTRACT MX, 3) LIKELY CHANCE OF SWAPPING PLANES IS NEEDED, AND 4) IT WAS THE ?LED ALTERNATE. TROUBLESHOT GLD NOT ARMED CAUTION IAW CRJ700 FIM 27-64-00-810-802-A01. OPS TEST OF GROUND LIFT DUMPING GOOD. CAUTION MESSAGE NOT PRESENT AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,074 hrs · 16,367 cycles

STRONG BURNING ODOR IN AFT ROWS WHEN AC POWER APPLIED - INSPECTED AFT EQUIP. BAY , AND CAB LIGHTING, CYCLED AC POWER FROM CAT AND APU , AND CYC RH PACK NO DEFECTS NOTED SMELL NOT PRESENT. GVI NO DEFECTS NOTED

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 21,877 hrs · 16,190 cycles

HYDRAULICS SYSTEM FAILURE. FLIGHT CREW RAN THE QRH, AND DECLARED AN EMERGENCY. HYD PUMP 3A LOW PRESSURE CAUTION IN FLIGHT. REMOVED AND REPLACED NR 3A HYD ACMP. SERVICED 3A HYD SYS TO 55% AT 49 DEGREES C. PERFORMED OPERATIONAL AND LEAK CHECK. NO LEAKS AT THIS TIME OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 969-985) · airframe 21,309 hrs · 15,697 cycles

EXT. FUSELAGE SKIN HAS AREA OF DAMAGE BETWEEN FS 969.00 AND 985.00 AT STR 27.-C/A-C/W REPAIR IAW ERS-CR-53MR-4025

Part: ANGLE — CRACKED · airframe 21,309 hrs · 15,697 cycles

"L" ANGLE AT BL 26.0 ON RH SIDE IS CRACKED ON LOWER END. -C/A-FOUND STANCHION TO BE CRACKED BEHIND THE RH BULKHEAD. REMOVED AND REPLACED STANCHION BEHIND THE RH BULKHEAD IAW SRM 5-42-12. CHECK NRWC E767449 FOR INSTALLATION OF NEW "L" ANGLE.

Part: BULKHEAD — CORRODED (BS 280) · airframe 21,309 hrs · 15,697 cycles

RH BULKHEAD WALL AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION AT FLOOR LEVEL-C/A-COMPLETED RH BULKHEAD LOWER WEB REPAIR @ FS280.00 IAW SRM 53-11-10-201-004.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,309 hrs · 15,697 cycles

RH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-REMOVED AND REPLACED RH FLOOR BEAM AT FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 21,309 hrs · 15,697 cycles

PASSENGER DOOR AFT SIDE HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR. -C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW 52-11-04-201-004-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,309 hrs · 15,697 cycles

LH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-RAR'D LH FLOOR BEAM AT FS2800.00 IAW SRM 51-42-06 AND 51-42-13

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,309 hrs · 15,697 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04.

Part: SKIN — CRACKED (PAX DOOR) · airframe 21,309 hrs · 15,697 cycles

PASSENGER DOOR AFT SIDE SKIN HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW SRM 52-11-04-201-004-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,309 hrs · 15,697 cycles

LH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.

Part: WEB — UNKNOWN (BS 193) · airframe 21,309 hrs · 15,697 cycles

RH WEB/FLOOR AT FS 193.00 OUTBD OF THE ADG RETACTION PUMP HAS 3/8" CRACK ON THE PREVIOUS REPAIR DOUBLER. -C/A-REPLACED REPAIR DOUBLER FROM PREVIOUS REPAIR IAW SRM 53-11-43 AND ETN-CR-53-099.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,309 hrs · 15,697 cycles

RH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 21,309 hrs · 15,697 cycles

EMERGENCY LIGHTING BATT P/N 2013-1 S/N 109524 AND POWER SUPPLY P/N 11-0049 S/N 24464 A110 REQ TO BE REMOVED AND REPLACED.-C/A-FOUND BATTERY S/N 109524 AND CHARGER S/N 24464 IN THE #3 POSITION. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND CHARGER IAW CRJ 700 W/C 33-002. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 109524

Part: UNKNOWN — ODOR (AFT LAVATORY) · airframe 21,286 hrs · 15,670 cycles

OUT OF 12,000 FT SMELLED A PLASTIC BURNING SMELL FOLLOWED BY SMOKE AFT LAV EICAS FOLLOWED GRH PROCEDURE SMOKE AFT LAV RETURNED ORD EMERGENCY DECLARED-C/A-C/W FIM TASK 21-22-00ABNORMAL SMOKE/ SMELL AFTER MAIN ENG COMPRESSOR WASH, GROUND RAN BOTH ENGS AND BLEED SYS AS PER CRJ MM TASK 72-00-00-100-801 UNTILL ALL FUMES NO LONGER PRESENT NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,126 hrs · 15,487 cycles

LH AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LH AFT EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-15. OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,845 hrs · 14,302 cycles

STEERING INOP CAUTION MESSAGE AFTER EXTENDING LANDING GEAR. STEERING INOP CAUTION RESET PER AOM VOLUME 1 RESET PROCEDURES PAGE 130.13.

Part: CHARGER — FAILED (CABIN) · airframe 19,065 hrs · 13,630 cycles

AFT EMERGENCY LIGHT (EXIT) WILL NOT SHUT OFF. -C/A-REMOVED AND REPLACED NR 3 EMERGENCY LIGHT CHARGER/CRADLE ASSY IAW AMM 33-51-07; OPS CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 18,984 hrs · 13,557 cycles

AFTER LANDING ON TAXI LOSS OF NOSE WHEEL STEERING CONTROL FOLLOWED BY HYD 3 LO PRESS, STEERING INOP AND SYSTEM 3 QUANTITY AT 0% FLUID REPORTED PUDDLED AROUND NOSE GEAR AND BEHIND AIRCRAFT ON TAXIWAY TOWED TO GATE. REF NRWC 542-ORD-02159 FOR THE R&R OF HYD LINE NR 2 ON NLG RETRACT ACTUATOR IAW AMM 32-32-09. OPS CHECK GOOD. NO LEAKS FOUND.

Part: ACM — SEIZED (NR 1) · airframe 18,429 hrs · 13,098 cycles

WHEN LEFT PACK WAS TURNED ON AFTER A FEW SECONDS WE'VE GOT SMOKE IN THE CABIN AND 'L PACK AUTOFAIL CAUTION MSG WAS POSTED'. HAD PAX ALREADY ON BOARD AND DEPLANED IMMEDIATELY. DEFERRED PER MEL PERFORMED FIM TASK 21-21-00 AND 21-22-00. SMOKE AND ABNORMAL SMELL IN THE COCKPIT AND SMOKE SMELL ABNORMAL SMELL IN THE CABIN. CONFIRMED NR 1 DUCT TEMP UNCONTROLLABLE WHEN PACK NR 1 SELECTED. FOUND NR 1 ACM SIEZED. REMOVED AND REPLACED LT ACM IAW AMM 21-51-08. OPC GOOD.

Part: WIRE — BROKEN (CALL PANEL) · airframe 16,601 hrs · 11,659 cycles

EMERGENCY EXIT FA CALL BUTTON LIGHT INOPERATIVE. REMOVED AND REPLACED BOTH LIGHT BULBS AT EXTERIOR LAVATORY WALL, AND CIRCUIT BOARD PANEL IAW AMM 33-23-01 AND AMM 23-31-17 NEITHER COMPONENTS CORRECTED PROBLEM WITH LIGHT DIMMING. REPAIRED BROKEN GROUND WIRE PLZ-L9011 20N IAW ESPM 20-16-53. OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,475 hrs · 11,548 cycles

LEFT FORWARD EQUIPMENT BAY FLOOR CRACKED IN CORNER. REPAIRED LEFT FORWARD EQUIPMENT BAY FLOOR IAW ETN-CR-53-099.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 15,496 hrs · 10,771 cycles

LEFT UPPER TRANSLATING COWL FORWARD INBOARD ANGLE IS CRACKED, REPLACED ANGLE IAW ETN-CR-54-015R1.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 15,496 hrs · 10,771 cycles

LEFT UPPER TRANSLATING COWL FWD OUTBD ANGLE IS CRACKED. REPLACED THE ANGLE IAW ETN-CR-54-015R1.

Part: STAND OFF — DAMAGED (LT NACELLE) · airframe 15,496 hrs · 10,771 cycles

LEFT LOWER TRANSLATING COWL FWD INBD ANGLE IS CRACKED. REPLACED THE STANDOFF IAW SRM 51-42-14, 51-42-21 AND ETNCR-54-015R1.

Part: HANDLE — OBSTRUCTED (PAX DOOR) · airframe 13,988 hrs · 9,603 cycles

PASSENGER ENTRY (MAIN CABIN DOOR) DIFFICULT TO OPEN. CLEANED DEBRIS FROM INTERIOR LOCK HANDLE ROLLER BEARING IAW STANDARD MAINTENANCE PRACTICES. OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,938 hrs · 9,570 cycles

WHEN RETRACTING SPOILERS DURING APPROACH, RECEIVED OTBD SPOILERONS AND OTBD FLT SPOILERS CAUTION MSG. C/W QRH CHECKLIST. INTERROGATED MDC, FOUND LT OTBD MFS PCU, PCU JAM MESSAGE. PERFORMED SPOST1 REST. PERFORMED OPS CK IAW ETN CR-27-093. OPS CK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,676 hrs · 9,400 cycles

IN DESCENT DOWNWIND, UPON STOWING THE FLIGHT SPOILER HANDLE, THE OTBD SPOILERS & OTBD FLIGHT SPOILERS CAUTION MSG POSTED. RAN THE AOM 1 CHECKLIST & DECLARED AN EMER. ON THE FLIGHT CONTROLS SYNOPTIC PAGE THE LT OTBD FLIGHT SPOILER BOX IS AMBER, RT OTBD FLIGHT SPOILER IS BOXED WHITE. COMPLIED WITH ETN-CR-27-093, RESET PROCEDURES FOR LT & RT INBD & OTBD MFS PCU & PCU JAM MDC MSGS. NO FURTHER DEFECTS NOTED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 13,048 hrs · 8,956 cycles

FLASHLIGHT HOLDER FOR NR 1 FLIGHT ATTENDANT BROKEN. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,969 hrs · 8,904 cycles

EMERGENCY LIGHTS FOR BATTERY PACK 3 STAY ON. TROUBLE SHOT & FOUND NR 3 EMER BATTERY & CHARGER BAD. R & R NR 3 EMER BATTERY & EMER BATTERY CHARGER. OPERATIONS CHECKED GOOD IAW AMM 33-51-00. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 13314.

Part: RELAY — FAILED (CABIN) · airframe 12,966 hrs · 8,901 cycles

EMERGENCY LIGHTS ON EXIT ROW CAPTAIN'S SIDE ARE STAYING ON. R & R RELAY K198 IAW MM 33-51-19. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,789 hrs · 8,758 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT NOT CHARGING. REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT IAW AMM 25-61-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 10,836 hrs · 7,138 cycles

RIGHT SIDE FLOOR IN FWD EQUIP COMPARTMENT HAS A 3/8" CRACK THAT RUNS UNDER ADG PUMP. REPAIRED RT SIDE FLOOR IN FWD EQUIP COMPARTMENT IAW ETN-CR-53-099.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,836 hrs · 7,138 cycles

MAIN AVIONICS UNDERFLOOR FRAME AT FS 295.00 IS CORRODED BETWEEN STRINGERS 26 LT - 26 RT. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15 - 27.

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 10,836 hrs · 7,138 cycles

RIGHT SUPPORT WEB BETWEEN FS 1144.00 & 1162.00, AT STRINGER 9 IS CHAFED. REPAIRED IAW ERS-CR-53MR-1125.

Part: COVER — DAMAGED (CABIN) · airframe 10,836 hrs · 7,138 cycles

CABIN EMER FLOOR LIGHT STRIPS RT SIDE SECTIONS 1, 9 & OVERWING EXIT HAVE CRACKED, BROKEN OR UNSERVICEABLE COVERS. R & R CRACKED, BROKEN OR UNSERVICEABLE CABIN EMER FLOOR LIGHT STRIPS RT SIDE SECTIONS 1, 9 & OVERWING EXIT IAW AMM 33-51-01.

Part: BRACKET — CRACKED (AC BAY) · airframe 10,836 hrs · 7,138 cycles

RIGHT HEAT EXCHANGER WATER INJECTION LINE BRACKET BETWEEN FS 1144.00 & 1162.00 AT STRINGER 9 IS CRACKED. R & R BRACKET IAW SRM 51-24-06.

Part: PANEL — CRACKED (PAX DOOR) · airframe 10,836 hrs · 7,138 cycles

PASSENGER DOOR AFT SIDE PANEL AT UPPER MIDDLE STEP IS CRACKED. REPAIRED PAX DOOR AFT SIDE PANEL AT UPPER MIDDLE STEP IAW SRM 52-11-04.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,836 hrs · 7,138 cycles

MAIN AVIONICS UNDERFLOOR FRAME AT FS 319.70 IS CORRODED BETWEEN STRINGERS 26 LT - 27. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15 - 27.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,836 hrs · 7,138 cycles

MAIN AVIONICS UNDERFLOOR FRAME AT FS 310.00 IS CORRODED BETWEEN STRINGERS 26 LT - 26 RT. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15 - 27.

Part: BRACKET — CRACKED (AC BAY) · airframe 10,836 hrs · 7,138 cycles

RIGHT HEAT EXCHANGER WATER INJECTION LINE BRACKET BETWEEN FS 1144.00 & 1162.00 AT STRINGER 7 IS CRACKED. R & R BRACKET IAW SRM 51-42-06.

Part: LIGHT — MISSING (CABIN) · airframe 9,994 hrs · 6,481 cycles

EMERGENCY LIGHT MISSING ON MAIN CABIN DOOR. INSTALLED NEW LIGHT STRIP IAW SMP. NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 9,988 hrs · 6,474 cycles

PASSENGER DOOR WARNING IN FLIGHT. FOLLOWED AOM VOL 1 PROCEDURES. PERFORMED OPS CHECK OF THE PAX DOOR INDICATION IAW AMM 52-11-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: HAND RAIL — DEFECTIVE (PAX DOOR) · airframe 9,289 hrs · 5,937 cycles

UNABLE TO OPEN PAX DOOR FROM EITHER INSIDE OR OUTSIDE. R & R FWD & AFT STUDS HANDRAIL IAW AMM 52-11-05. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,687 hrs · 5,529 cycles

NR 1 FLIGHT ATTENDANT FLASHLIGHT & MOUNT FELL OFF WALL & WILL NOT CHARGE. REPLACED NR 1 FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 25-61-02, OPERATIONS GOOD.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 7,491 hrs · 4,739 cycles

AFT EXTERIOR EMERGENCY LIGHTS CONTINOUSLY ILLUMINATED. R & R EMERGENCY LIGHT CHARGER AND BATTERY AT NR 4 POSITION IAW AMM 33-51-17. OPS CHECK GOOD.

Part: ENGINE — VIBRATION (LEFT) · airframe 7,294 hrs · 4,620 cycles

LEFT ENGINE, HIGH VIBATION ON CLIMBOUT WENT UP TO 1.8 BEFORE WE LEVELED OFF AND BROUGHT BACK THE POWER. PREFORMED FIM TASK 72-00-00-810-011. ALL VIBRATIONS WITHIN LIMITS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,219 hrs · 4,567 cycles

BATTERY POWER SUPPLY UNSERVICEABLE. R & R NR 4 BATTERY POWER SUPPLY IAW WORK CARD 33-002. OPS CHECKED GOOD.

Part: FLASHLIGHT — INTERMITTENT (COCKPIT) · airframe 4,555 hrs · 2,862 cycles

ON FLIGHT 3785 - THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT ONLY WORKED WHEN SHAKEN. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW CRJ 700 AMM 25-6102. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE ASSY — BROKEN (PAX DOOR) · airframe 2,773 hrs · 1,746 cycles

DURING FLIGHT 4590 THE MAIN PASSENGER DOOR HAS LOUD AIR LEAK NOISE WHILE IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ICE BREAK CABLE BROKEN BETWEEN VENT FLAP & DOOR ASSY PREVENTING DOOR (FLAP VENT) TO SEAL. REPLACED ICE BREAK CABLE IAW AMM 52-11-15. PERFORMED LEAK TEST OF MAIN DOOR IAW AMM 52-00-00. LEAK OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — FAULTY (RT MLG) · airframe 25,743 hrs · 1,627 cycles

FOR FLIGHT 3745 THE CREW REPORTED THAT WHILE ON APPROACH THEY RECEIVED AN ANTI-SKID OUTBAORD MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WTHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR PRXIMITY SENSOR HARNESS IAW CRJ 700 AMM 32-61-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — FAULTY (ANTISKID SYS) · airframe 2,481 hrs · 1,569 cycles

ON FLIGHT 4588 THE CREW REPORTED THAT ON SHORT FINAL THEY RECEIVED AN ANTI-SKID INBOARD INOPERABLE CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY. UPON TOUCHDOWN THE MESSAGE EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT INBOARD ANTI - SKID WIRING HARNESS IAW CMM 32-61-01. PERFORMED EXTENSION AND RETRACTION OF MAIN LANDING GEAR IAW AMM 32-30-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRU — MALFUNCTIONED (NR 1) · airframe 134 hrs · 96 cycles

ON FLIGHT 3712 SMOKE WAS OBSERVED COMING FROM THE NOSE CLAM SHELL DOORS. (WHEN DISCOVERED-UNKNOWN) THE CAPTAIN ELECTED TO RETURN TO ORD. REMOVED AND REPLACED THE NUMBER 1 TRANSFORMER RECTIFIER UNIT IAW CRJ 700 AMM 24-31-01. THE OPERATIONAL CHECK WAS GOOD NO SMOKE NOTED P/N OFF TRU3502 S/N OFF 3522 P/N ON TRU 3502 S/NON 1590. THE AIRCRAFT WAS RETURNED TO SERVICE.