N530EA

Part: BULKHEAD WEB — CORRODED (ZONE 200) · airframe 32,335 hrs · 25,219 cycles

FOUND CORROSION ON FS 280 R/H LOWER WEB. UPON FURTHER INVESTIGATION FOUND CORROSION ON FS 280 R/H LOWER WEB FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-11-10-201-003-A01. FABRICATED, LOCATED AND DRILLED FS 280 RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" PO# 5-22986 IAW CRJ 700 SRM 53-11-10-201-004-A01. COMPLIED WITH CRJ 700 SRM 53-11-10-201-004-A01 FS 280 LOWER BULKHEAD WEB REPAIR

Part: TRANSCOWL — TEMP REPAIR (ZONE 400) · airframe 32,335 hrs · 25,219 cycles

EA 54-2025-0682 (140FH PERM REPAIR - SPEED TAPE APPLIED - RH ENGINE TRANS COWL ACCES PANEL FWD LATCH OPENS IN FLIGHT) WITHIN 140 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PERFORMED PERMANENT REPAIR BY COMPLYING WITH BOMBARDIER REO 670-54-21-1207 REV.-A DATED 2015-08-27. OPERATIONAL CHECK OF THE RIGHT TRANSCOWL IAW CRJ AMM 78-30-00-720-801-A01, CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: PULLEY BRACKET — CHAFED (ZONE 100) · airframe 32,335 hrs · 25,219 cycles

HN00246730 DISCREPANCY: FOUND RH SIDE FS280 AILERON PULLEY BRACKET TO BE CHAFED AND REQUIRE REPLACEMENT. CORRECTIVE ACTION: LOCATED AND DRILLED NEW BRACKET P/N CC670-94802-7-01, AND TRANSFERRED BRACKET FROM OLD PULLEY IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 51-42-06-001-001-A01

Part: BULKHEAD WEB — CORRODED (ZONE 100) · airframe 32,335 hrs · 25,219 cycles

FOUND CORROSION ON FS 280 L/H LOWER WEB. UPON FURTHER INVESTIGATION FOUND CORROSION ON FS 280 L/H LOWER WEB FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-11-10-201-003-A01. FABRICATED, LOCATED AND DRILLED FS 280 LH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" PO# 5-22986 IAW CRJ 700 SRM 53-11-10-201-004-A01. COMPLIED WITH CRJ 700 SRM 53-11-10-201-004-A01 FS 280 LOWER BULKHEAD WEB REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 32,335 hrs · 25,219 cycles

FOUND CORROSION ON FS 280 "J" ANGLE. UPON FURTHER INVESTIGATION ON FS 280 "J" ANGLE FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01. LOCATED AND DRILLED NEW J ANGLE P/N CC670-34095-1SB IAW CRJ-700-SRM-51-40-11-001-001-A01. INSTALLED FS 280 NEW "J"ANGLE P/N CC670-34095-1SB IAW CRJ SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. RESTORED TO FINISH IAW CRJ 700 SRM 51-25-16-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 32,335 hrs · 25,219 cycles

FOUND CORROSION @ L/H F.S.280 BEAM. INSTALLED NEW FS 280 LH CROSSBEAM P/N CC670-34094-2 AND INSTALLED NEW LH CORROSION CAP ANGLE PN CC670-34096-1 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 32,335 hrs · 25,219 cycles

FOUND CORROSION ON FS 280 R/H CROSS BEAM. UPON REMOVAL OF R/H CROSS BEAM FOUND R/H CORROSION CAP ANGLE DAMAGE REQUIRES REPLACEMENT. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH CORROSION CAP ANGLE P/N CC670-34096-2 IAW CRJ 700 SRM 51-42-06-001-001- A01.AND 51-40-13-001-001-A01, WITH INCORPORATION OF SB670BA-53-041 REV M

Part: TERMINAL BLOCK — SMOKE (ZONE 200) · airframe 31,980 hrs · 24,911 cycles

CA FRONT WINDSHIELD LOWER TERMINAL BLOCK SMOKING ON FINAL. TURNED OFF WINDSHIELD HEAT SMOKE WENT AWAY. NO MEDICAL ATTENTION WAS REPORTED. / REMOVED AND REPLACED WINDSHIELD IAW CRJ700 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: SELECTOR VALVE — UNSERVICEABLE (ZONE 700) · airframe 31,138 hrs · 24,243 cycles

STEERING INOP CAUTION MSG ON T/O / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801. OPS CHECK GOOD. NO STEERING CAUTION MSG AT ANY POINT.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,950 hrs · 23,241 cycles

FUME SMELL IN THE CABIN / INSPECTED CABIN FOR FUMES/SMELL WITH SAME CONFIG AS REPORTED, COULD NOT DUPLICATE FAULT IAW CRJ700 FIM 21-22-00-810-806-A01.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,951 hrs · 23,242 cycles

ELECTRICAL BURNING SMELL/ODOR REQUIRES FTS. / PERFORMED T/S IAW CRJ700 FIM 21-21-00-810-806-A01 / FIM 21-22-00-810-806-A01 TRIED TO DUPLICATE FAULT AND IDENTIFY THE SOURCE OF THE SMELL BY CHECKING THE CABIN THROUGHLY WITH APU RUNNING, LH/RH ENGINE RUNNING ON IDLE, PACK ON/OFF, MAX CABIN TEMP, RECIRC FAN ON/OFF UNABLE TO DUPLICATE FAULT, NORMAL CABIN SMELL OBSERVED. NO ABNORMAL NOISE WHILE PACK 1/2 OPERATES. PERFORMED OPS TEST OF THE DISPLAY SUPPLY FAN AND CHECK VALVE IAW CRJ700 AMM 21-24-12-710-801-A01-PSA, TEST GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,613 hrs · 22,956 cycles

FA REPORTS BURNING SMELL IN FIRST CLASS, BOTH PACKS ON, DURING PREFLIGHT / TROUBLESHOT ABNORMAL SMELL IAW CRJ700 FIM 21-22-00-810-806 CAUSE 12. FOUND CHECKS TO BE NORMAL AND NO ABNORMAL SMELLS OR FUMES. SUSPECT BURNING COFFEE IN COFFEE MAKER TO BE ROOT CAUSE.

Part: WARNING MESSAGE — FALSE INDICATION (NLG STEERING) · airframe 29,597 hrs · 22,940 cycles

STEERING INOP CAUTION MSG ON ROTATION. / PERFORMED OPS CHECK OF THE NOSE WHEEL STEERING IAW CRJ700 AMM 32-51-00-710-801-A01. OPS CHECK GOOD AT THIS TIME.

Part: FUSE — UNSERVICEABLE (700) · airframe 28,045 hrs · 21,583 cycles

IB GND SPLRS, HYD 3 LO PRESS, IB BRAKE PRESS. LOST HYD SYSTEM 3 UPON LANDING. REMOVED AND REPLACED RH SYSTEM 3 VOLUMETRIC FUSE IAW CRJ700 AMM 32-43-21-000/400-801-A01. LEAK CHECK GOOD. HYD 3 SYSTEM SERVICED IAW CRJ700 AMM 12-12-29-611-801-A01

Part: SKIN — DAMAGED (BS 1015-1051) · airframe 27,589 hrs · 21,191 cycles

GOUGE & DENT DAMAGE TO FUSELAGE SKIN BTW FS1015.00 - FS1051.30 AND STR21R - STR26R. PERMANENT REPAIR WAS PERFORMED IAW EA 22-C7-53-0942.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 26,419 hrs · 20,120 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 693 TO 863.

Part: STUB FRAME — CORRODED · corrosion level 2 · airframe 26,419 hrs · 20,120 cycles

DESCRIPTION OF DAMAGE: FWD BAGGAGE BAY DOOR FWD LOWER STUB FRAME AT F.S. 549 IS CORRODED.

Part: FRAME — CORRODED · corrosion level 2 · airframe 26,419 hrs · 20,120 cycles

FS 333.0 IS CORRODED FROM STR 26R TO STR 27.

Part: STUB FRAME — CORRODED · corrosion level 2 · airframe 26,419 hrs · 20,120 cycles

DESCRIPTION OF DAMAGE: FWD BAGGAGE BAY DOOR AFT LOWER STUB FRAME AT F.S. 565 IS CORRODED.

Part: FRAME — GOUGED · airframe 39,973 hrs · 38,705 cycles

CREW ESCAPE HATCH SURROUND STRUCTURE L/H FRAME IS GOUGED

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,419 hrs · 20,120 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 693 TO 863.

Part: FRAME — CORRODED (F310) · corrosion level 2 · airframe 25,849 hrs · 19,591 cycles

F 310 CONTAINS CORROSION ON FRAME BETWEEN STR 25 L TO STR 25 R

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 25,849 hrs · 19,591 cycles

FS319 FRAME SHEAR TIE CONTAINS CORROSION BETWEEN STRINGER 26L TO STRINGER 25R.

Part: STRINGER — CORRODED (ZONE 100) · airframe 25,849 hrs · 19,591 cycles

FS295 CONTAINS CORROSION ON FRAME SPLICE REPAIR, BETWEEN STR25L TO STR25R

Part: GCU — FAULTED (NR 2) · airframe 25,917 hrs · 19,646 cycles

WHILE ON APPROACH TO PHL A/C LOST RIGHT GENERATOR CAUSING A FLAPS FAILURE MESSAGE CAUSING CA TO DECLARE AN EMERGENCY. FLIGHT LANDED SAFELY IN PHL TRUCKS WERE ROLLED AND EMERGENCY CANCELLED UPON LANDING. PLANE ABLE TO TAXI TO GATE UNDER OWN POWER. (TRFKE007VT4F). FOR TROUBLESHOOTING PURPOSES SWAPPED GCU 2 WITH GCU 3 IAW CRJ 700 AMM 24-22-03-000/400-801( A01) OPS CHECK GOOD, NO DISCREPANCIES NOTED AT THIS TIME.

Part: STRAP — CORRODED (BS 333 S26-27R) · corrosion level 2 · airframe 25,849 hrs · 19,591 cycles

FS 333 CIRCUMFERENTIAL SPLICE STRAP CORRODED BETWEEN STR 26R AND STR 27

Part: ANGLE — CORRODED (BS 310 S26-27L) · corrosion level 2 · airframe 25,849 hrs · 19,591 cycles

ANGLE AT FS 310 CORROSION FROM STR 26L STR 27

Part: STRAP — CORRODED (BS 280 S24R-25L) · corrosion level 2 · airframe 25,849 hrs · 19,591 cycles

FS 280 CIRCUMFERENTIAL SPLICE STRAP CORROSION BETWEEN STR 24R AND 25L

Part: COMPASS — FAILED (COCKPIT) · airframe 25,409 hrs · 19,182 cycles

ARCED THE SUN SHADE IN THE STANDBY COMPASS LIGHT, REPORTS SPARK, SMOKE, AND VISIBLE SLIGHT DAMAGE TO THE STANDBY COMPASS HOUSING. WHILE PUTTING UP THE SUN SHADE, PART OF SUNSHADE SPARKED AGAINST STANDBY COMPASS. LIGHT WAS ON DIM. SPARKED WITH LITTLE SMOKE, AND LIGHTS IN CABIN FLICKERED. SLIGHT DAMAGE TO MAG COMPASS HOUSING. REMOVED AND REPLACED DAMAGED STANDBY COMPASS BRACKET. REMOVED AND REPLACED STANDBY COMPASS. PERFORMED OPS TEST OF WINDOW/WINDSHIELD HEAT TEMP CONTROLLERS. OPS TEST GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 25,406 hrs · 19,178 cycles

DURING TRANSITION FROM ARRIVAL TO APPROACH, THE FLIGHT CREW OBSERVED AN OUTBOARD SPOILERON WARNING. THE CREW DECLARED AN EMERGENCY, BUT DID NOT CALL FOR EMERGENCY VEHICLES. NO CALL FOR BRACE WAS ISSUED TO THE PASSENGERS EITHER. THE CREW CANCELLED THEIR EMERGENCY STATUS ONCE THEY WERE SAFELY OFF THE RUNWAY. OB SPOILERONS AND OB FLT SPOILERS CAUTION MSGS IN FLIGHT. COMPLIED WITH SELF TEST OF THE SPOILER AND STABILIZER CONTROL UNITS IAW CRJ700 AMM 27-61-05-740-801. OPS CHECK GOOD NO DEFECTS NOTED. STATUS MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 24,279 hrs · 18,147 cycles

DESCENDING IINTO PHL CREW RECEIVED OB SPOILER ON MESSAGE AND SPOILER ON MESSAGE. PERFORMED OPERATIONAL CHECK OF MFS, IAW CRJ 700 AMM 27-62-01-710-801-A01. OPS CHECK GOOD. PERFORMED LEAK CHECK OF MFS PCU, IAW CRJ 700 AMM 27-62-01-790-801-A01. LEAK CHECK GOOD. NO FURTHER FAULTS FOUND.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 24,144 hrs · 18,027 cycles

WHILE ON CLIMBOUT FROM MHT, CREW RECEIVED A NOSEWHEEL STEERING INOP CAUTION MESSAGE. CREW RAN THE QRH AND CONTINUED TO DCA. THE CREW DECLARED AN EMERGENCY AS A PRECAUTION GOING INBOUND. THE FLIGHT LANDED ON RUNWAY 19 IN DCA AND WAS ABLE TO MAKE A TURN OFF THE RUNWAY TO RUNWAY 22 UNDER THEIR OWN POWER AND CANCELED THE EMERGENCY. CREW WAS ABLE TO RESET THE SYSTEM WITH MAINTENANCE AND TAXIED TO THE GATE WITH NO ISSUES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,996 hrs · 17,896 cycles

BOTH AFT OUTSIDE EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS PAST EMERGENCY DOORS ARE OUT. REMOVED AND REPLACED NR 4 EMER LIGHTS BATTERY. OPS CHECK GOOD. (PN: 2013-1ASMI SN: 76332)

Part: CONTROL UNIT — FAILED (ZONE 100) · airframe 23,905 hrs · 17,820 cycles

IB FLIGHT SPOILER AND IB SPOILERON CAUTION MESSAGES - REMOVED AND REPLACED SSCU 1, OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,277 hrs · 17,280 cycles

CAPTAINS WINDSHIELD CRACKED. MX REPLACED WINDSHIELD.

Part: ENGINE — VIBRATION (LEFT) · airframe 20,731 hrs · 14,928 cycles

ON INITIAL CLIMB OUT OF JFK THERE WAS A SEVERE ENGINE VIBRATION. EMERGENCY DECLARED AND RETURN TO FIELD IMMEDIATELY. EMERGENCY CANCELED AFTER EXITING RUNWAY. EMERGENCY EQUIPMENT WAS STANDING BY BUT DID NOT RESPOND TO AIRCRAFT. THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LH ENGINE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 20,078 hrs · 14,313 cycles

ELECTRICAL BURNING ODOR IN GALLEY. MX COMPLIED WITH AN OPS CHECK OF AIR COND DISTRIBUTION SYS AND DID NOT NOTE ANY BURING ODOR. OPS CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,311 hrs · 13,578 cycles

MAIN AVIONICS COMPARTMENT FRAME FS295.00 HAS CORROSION. COMPLETED REPAIR FRAME FS295.00 IAW SRM TEMP REVISION 53-0098.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WINDOW) · airframe 18,766 hrs · 13,133 cycles

L WINDOW HEAT CAUTION MSG AT FL260-C/A-RESETED L/H WINDOW C.B. PERFORMED WINDOW TEMP CONTROLLER OPERATIONAL TEST & FOUND WORKING PROPERLY NO DEFECTTS NOTED AT THIS TIME IAW CRJ MM 30-41-06

Part: STRUT — FAILED (NLG) · airframe 18,490 hrs · 12,930 cycles

ON SELECTING THE GEAR DOWN, RECEIVED A STEERING INOP CAUTION MESSAGE. DURING GO AROUND, SELECTED GEAR UP AND HEARD A BANG FROM NOSE AREA AND A GEAR DISAGREE WITH RED DASHES, IN TRANSIT FROM NOSE GEAR. RAN CHECKLIST TO GET THREE GREEN. REMOVED AND REPLACED NLG PISTON AND AXLE ASSEMBLY IAW AMM 32-21-20, LEAK CHECKED GOOD. PERFORMED NOSE WHEEL STEERING OPS CHECK IAW AMM 32-51-00. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,304 hrs · 12,775 cycles

OVERWING CEILING EMERGENCY EXIT SIGN LENS MISSING. REPLACED THE LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 18,194 hrs · 12,695 cycles

STEERING INOPERATIVE CAUTION MESSAGE POSTED DURING DECENT. NORMAL LANDING AFTER QRH CHECKLIST. PERFORMED A RESET OF THE SYSTEM IAW FIM 32-50-00-810-802-A01, NO MESSAGES POSTED. CREW PERFORMED A TAXI CHECK OF THE AIRCRAFT, NO MESSAGES POSTED, AIRCRAFT OK FOR SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 17,722 hrs · 12,316 cycles

EXTERIOR EMERGENCY LIGHT NR 4, JUST AFT OF THE RT OVERWING EXIT IS ALWAYS ILLUMINATED. REMOVED AND REPLACED THR NR 3 EPSU IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,825 hrs · 10,786 cycles

INBD FLT SPOILERS CAUTION MSG, COMPLIED WITH ETN-CR-27-093. OPS CHECKS GOOD, NO DEFECTS NOTED.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 15,778 hrs · 10,750 cycles

PAX DOOR FWD SIDE SKIN HAS A CRACKED REPAIR DOUBLER NEAR THE THIRD STEP FROM THE TOP. APPROX. 1/2 INCH LONG. REMOVED AND REPLACED THE DOUBLER IAW SRM 52-44-04.

Part: DOUBLER — CRACKED (PAX DOOR SKIN) · airframe 15,778 hrs · 10,750 cycles

PAX DOOR AFT SIDE SKIN HAS A CRACKED REPAIR DOUBLER NEAR THE THIRD STEP FROM THE TOP. APPROX 1.2 INCH LONG. REMOVED AND REPLACED AFT SKIN DOUBLER IAW ETN-CR-52-039.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,778 hrs · 10,750 cycles

PAX DOOR AFT DRAG ANGLE HAS 2 CRACKS 2 INCHES LONG NEAR THE POWER ASSIST PULLEY BRACKET. INSTALLED A NEW DRAG ANGLE IAW AMM TASK 52-11-04.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 15,778 hrs · 10,750 cycles

RIGHT OVERWING EMERGENCY EXIT UPPER SIGN AND ISLE SIGN ARE ILLUMINATED AND WILL NOT EXTINGUISH. REMOVED AND REPLACED THE NR 3 BATTERY PACK AND POWER SUPPLY. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,432 hrs · 10,489 cycles

DURING DESCENT, WHEN DEPLOYED THE FLIGHT SPOILER RECEIVED INBD FLT SPOILER AND INBD SPOILERONS CAUTION MESSAGE. EMERGENCY LANDING MDT ACCT FLT SPOILERS CAUTION MESSAGE. INTERGRATED MDC, FOUND RT INBD MFS PCU JAM, PERFORMED S POST 1, RESET PERFORMED. OPS CHECK IAW ETN-CR-27-093, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,620 hrs · 9,880 cycles

FIRST OFFICERS FLASHLIGHT INOPERATIVE. R & R FIRST OFFICERS FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 13,960 hrs · 9,376 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARD, FWD FLIGHT ATTENDANT FLASHLIGHT IAW MEL 25-14.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,610 hrs · 9,101 cycles

DURING CLIMB OUT AT 5000 FT, FIRST OFFICER NOTICED CRACK IN WINDSHIELD. RETURNED, EMER DECLARED FLIGHT CONTINUED. TRANSFERRED TO NRWC 530-ORD-01533. REMOVED DAMAGED WINDSHIELD & SEALANT IAW AMM 56-11-01. REPLACEMENT WINDSHIELD IS BAD FROM STOCK, FOUND DAMAGE TO SEVERAL NUTPLATES & IMPACT DAMAGE TO TRANSPARENCY. REPAIRED CORNER SEALANT BEDS IAW TR 56-0057. COMPLIED WITH STEPS 1 - 3H OF TR 56-0057.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 13,502 hrs · 9,003 cycles

FLIGHT ATTENDANT NR 2 REPORTS THAT HER FLASHLIGHT WILL NO LONGER INDICATE IF IT IS CHARGING, ITEM DEFERRED. REPAIRED NR 2 FLIGHT ATTENDANTS FLASHLIGHT CHARGER WIRE IAW AMM 20-44-05. OPERATIONS CHECKED GOOD MEL RESTORED.

Part: ENGINE — VIBRATION (NR 1) · airframe 13,188 hrs · 8,757 cycles

DIVERTED EMER DUE TO UNCONTROLLABLE EXCESSIVE NR 1 ENG VIBRATION AT 17000, NR 1 1.5%, NR 2 .3%, ABOVE FL 250 NR 1 1.8 - 2.0. PULLED NR 1 THRUST LEVER BACK TO KEEP IN GREEN. AT FL 340 UNABLE TO MAINTAIN AIRSPEED & ALT WITH NR 1 THRUST LEVER & NR 2 NEEDED TO BE IN MCT. NO PRECAUTIONARY ENG SHUTDOWN, WAS ABLE TO MAINTAIN VIBRATION ON DESCENT & THROUGH LANDING PHASE. PERFORMED INSPECTION FOR STIFF FAN BLADES IAW AMM 72-21-02. PERFORMED OPERATIONS CHECK IAW AMM 72-00-00. OPERATIONS CHECKED GOOD. VIBRATION WORK SCOPE REQUIRED WITHIN 50 FLIGHT CYCLES, REF LOG PAGE 3898273 ITEM 1.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,167 hrs · 8,001 cycles

LEFT WING ANTI-ICE CAUTION WITH THRUST LEVERS IN CLIMB. PERFORMED OPS CHECK IAW MM 30-12-08. OPS CHECKED OK .

Part: CONTACT — OUT OF ADJUST (FLASHLIGHT) · airframe 12,000 hrs · 7,871 cycles

FIRST OFFICER'S FLASHLIGHT INOPERATIVE & HAS A ELEC SMELL. INSPECTED FLASHLIGHT & CONTACT ADJUSTED IAW AMM 25-61-02. OPERATIONAL CHECKED GOOD.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 11,302 hrs · 7,315 cycles

UPON FLIGHT SPOILER DEPLOYMENT DURING THE DESCENT THE OTBD FLIGHT SPOILERS OTBD SPOILERONS CAUTION MSGS POSTED ON EICAS. ON THE FLIGHT CONTROL SYNOPTIC PAGE THE LT OTBD SPOILER TURNED AMBER & FAILED TO PROPERLY DEPLOY IN FLIGHT & DURING LANDING. THE RT OTBD SPOILER TURNED WHITE. PERFORMED SPOST 1 & SPOST 2 TESTED IAW AMM 27-61-05. OPERATIONS CHECKED GOOD. NO FURTHER MSG DISPLAYED.

Part: HOLDER — INOPERATIVE (FLASHLIGHT) · airframe 11,014 hrs · 7,116 cycles

FORWARD FLIGHT ATTENDANTS FLASHLIGHT HOLDER INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-61-01. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,630 hrs · 6,815 cycles

FLIGHT 3301 DIVERSION CREW REPORTED STAB TRIM FAULT & AURAL WARNING RUNAWAY TRIM. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED TEST OF STAB CONTROL IAW AMM 27-61-05. OPERATIONS CHECKED GOOD AT THIS TIME. THE ACFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 10,582 hrs · 6,778 cycles

LEFT INBD FLIGHT SPOILER FAIL INFLIGHT. COMPLIED WITH DVI OF LT INBD MFS. RESET SSCU'S & COMPLIED WITH SELF-TEST IAW CRJ700 27-61-05. COMPLIED WITH MFS OPERATIONS CHECK IAW CRJ700 27-62-01. ALL WITH NO DEFECTS NOTED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 10,581 hrs · 6,777 cycles

EMERGENCY FLOOR PATH LIGHT STRIP BETWEEN 2A & 3A REQUIRES REPLACEMENT. REPLACED THE EMERGENCY FLOOR PATH LIGHT STRIP BETWEEN 2A & 3A IAW AMM 33-51-01.

Part: LIGHT — UNKNOWN (CABIN) · airframe 10,581 hrs · 6,777 cycles

LEFT EMERGENCY FLOOR LIGHT STRIP NR 1 REQUIRES REPLACEMENT. CUT & TAPED STRIP AS REQUIRED IAW BOW 154906 FOR INSTALLATION.

Part: PLATE — CRACKED (FUSELAGE) · airframe 10,581 hrs · 6,777 cycles

RIGHT FWD EQUIPMENT BAY PLATE UNDER ADG RETRACTION PUMP IS CRACKED. REPAIRED IAW ETN-CR-53-099

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 10,581 hrs · 6,777 cycles

STIFFENER ON STRINGER 26L BETWEEN FS 349.00 - 364.00 IS CORRODED. INSTALLED NEW STIFFENER ON STRINGER 26L BETWEEN FS 349.00 - 364.00 IAW SRM 51-42-06 & 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,581 hrs · 6,777 cycles

RIGHT EMERGENCY FLOOR LIGHT STRIP 1 & 2 REQUIRE REPLACEMENT. CUT & TAPED NEW STRIPS IAW BOW154906 FOR INSTALLATION.

Part: DETECTOR LOOP — OUT OF POSITION (BLEED AIR SYS) · airframe 9,779 hrs · 6,213 cycles

LEFT BLEED DUCT CAUTION MESSAGE. REPOSITIONED LT BLEED AIR LEAK DET LOOPS MT 138 & 141 IAW AMM 36-21-01. PERFORMED BLEED AIR LEAK INITIATION TEST IAW AMM 36-21-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — FAULTY (BLEED AIR SYS) · airframe 9,734 hrs · 6,184 cycles

DURING CLIMB OUT ON FLIGHT 3049 LT BLEED DUCT WARNING FOLLOWED BY BLEED DUCT CAUTION FOLLOWING AOM. SYS ISOLATED ALL CAUTIONS & WARNINGS EXTINGUISHED. THE ACFT WAS REMOVED FROM SERVICE. R & R 90 DEGREE ELEC CONNECTOR MT 203 & CERAMIC INSERT IAW CRJ-700 AMM 36-21-01. OPERATIONS CHECKED OF THE BLEED LEAK DETECTION SYSTEM B, OPERATIONS CHECKED GOOD. IAW AML PG 3469877 ITEM 3 FOR WORK DONE ON SYS A, THE ACFT RETURN TO SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 7,068 hrs · 4,533 cycles

FOR FLIGHT 3676 THE CREW REPORTED THE EMERGENCY EXIT SIGN OVER ROW 13 CAME OFF DURING CLIMBOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED EMERGENCY EXIT SIGN COVER AT ROW 13 AS REQUIRED IAW CRJ-700 AMM 33-51-05. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,735 hrs · 3,721 cycles

DURING C-CHECK FOUND LEFT FLOOR SUPPORT ANGLE IN COCKPIT ENTRY CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR IAW EO CR-53MR-295. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,735 hrs · 3,721 cycles

DURING C CHECK INSPECTION FOUND LEFT FLOOR SUPPORT ANGLE IN COCKPIT ENTRY CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW EO CR-53MR-296. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 5,735 hrs · 3,721 cycles

RIGHT FLOOR SUPPORT ANGLE IN COCKPIT ENTRY IS CRACKED. REPAIRED IAW EO CR-53MR-295.

Part: TRANSMITTER — MALFUNCTIONED (RT ELEVATOR) · airframe 2,433 hrs · 1,625 cycles

ON FLIGHT 3833 THE CREW REPORTED THAT DURING THE CLIMBOUT AT APPROXIMATELY 15000 FEET, RECEIVED AN "ELEVATOR SPLIT" CAUTION MESSAGE. THE CREW PERFORMED THE AIRCRAFT OPERATIONS MANUAL VOL 1 PROCEDURES AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ELEVATOR POSITION TRANSMITTER IAW AMM 27-34-10. A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DCU — MALFUNCTIONED (NR 1) · airframe 2,421 hrs · 1,618 cycles

ON FLIGHT 9801 THE CREW REPORTED THAT ON APPROACH WHILE ON DOWNWIND TO RUNWAY 16 RIGHT THEY RECEIVED AN "ELEVATOR SPLIT" CAUTION MESSAGE. NO ADVERSE HANDLING ENCOUNTERED. THE CREW DECLARED AN EMERGENCY AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 DATA CONCENTRATION UNIT. THE PARAMETERS ARE WITHIN LIMITS IAW CRJ AMM 27-34-10. THE AIRCRAFT WAS RETURNED TO SERVICE.