N178JB

Part: LINE — BLOCKED (FUEL FLOW) · airframe 38,696 hrs · 25,151 cycles

FT # 427, BOS-BWI. RETURNED TO FIELD. FUEL 2 LOW LVL; SUSPECTING THE MOTIVE FLOW RETURN LINE FROM EDP BACK TO BE BLOCKED AND PREVENTING COLLECTOR TANK FROM FILLING PROPERLY. REMOVED AND REPLACED PER LMM 73-00-00 REMOVAL 001 SUBTASK 73-00-00-440-001. ALL LEAKS CHECKED NORMAL ALL INDICATIONS NORMAL.

Part: WEB — CRACKED (FRAME 52) · airframe 38,113 hrs · 25,765 cycles

DURING HEAVY MAINTENANCE, CRACK BELLY FAIRING WEB AT LEVEL FR 52 LH SIDE MLG COMPARTMENT ON LOWER FUSELAGE; REF AEROMAN NR WO 2019-238/1 WCC 2019-332147 ACCOMPLISHED CRACK REPAIR OF CENTER FUSELAGE II WING TO FUSELAGE FAIRING FR 52 WEB IN ACCORDANCE WITH AEROMAN EA 57-0491-19 REV1 AND EMBRAER ETD 2019-190-144625 AND EC NO. E19-836-01. THIS IS CLASSIFIED AS MAJOR.

Part: POWER UNIT — FAILED (CABIN) · airframe 37,400 hrs · 24,231 cycles

FLT 1589, BOS-DCA. L2 DOOR EMERGENCY LIGHTS, ROW 24-25 CENTER ISLE EMERGENCY LIGHT AND AFT GALLEY CEILING EMERGENCY LIGHT INOP; REMOVED AND REPLACED #5 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECK GOOD AT THIS TIME.

Part: POWER UNIT — FAILED (CABIN) · airframe 37,326 hrs · 24,171 cycles

FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8-C-A-A-3. (15 MIN STEP) ONLY THE CENTER FUSELAGE EMERGENCY EXIT SIGNS STAYED ON FOR 15 MINUTES. ALL OTHERS LASTED LESS THAN 2 MINUTES; REF LG PG #2479616 I#1+2, ALSO REF LG PG#2479617 I#1+2 FOR R & R OF ALL ELPU'S. ACCOMPLISHED ELPU'S FUNCTIONAL TEST IAW AMM 33-50-01. TEST GOOD. A/C OK FOR CONT.

Part: POWER UNIT — FAILED (CABIN) · airframe 37,326 hrs · 24,171 cycles

FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8-C-A-A-3. (15 MIN STEP) ONLY THE CENTER FUSELAGE EMERGENCY EXIT SIGNS STAYED ON FOR 15 MINUTES. ALL OTHERS LASTED LESS THAN 2 MINUTES; REF LG PG #2479616 I#1+2, ALSO REF LG PG#2479617 I#1+2 FOR R & R OF ALL ELPU'S. ACCOMPLISHED ELPU'S FUNCTIONAL TEST IAW AMM 33-50-01. TEST GOOD. A/C OK FOR CONT.

Part: POWER UNIT — FAILED (CABIN) · airframe 37,326 hrs · 24,171 cycles

FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8-C-A-A-3. (15 MIN STEP) ONLY THE CENTER FUSELAGE EMERGENCY EXIT SIGNS STAYED ON FOR 15 MINUTES. ALL OTHERS LASTED LESS THAN 2 MINUTES; REF LG PG #2479616 I#1+2, ALSO REF LG PG#2479617 I#1+2 FOR R & R OF ALL ELPU'S. ACCOMPLISHED ELPU'S FUNCTIONAL TEST IAW AMM 33-50-01. TEST GOOD. A/C OK FOR CONT.

Part: POWER UNIT — FAILED (CABIN) · airframe 37,326 hrs · 24,171 cycles

FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8-C-A-A-3. (15 MIN STEP) ONLY THE CENTER FUSELAGE EMERGENCY EXIT SIGNS STAYED ON FOR 15 MINUTES. ALL OTHERS LASTED LESS THAN 2 MINUTES; REF LG PG #2479616 I#1+2, ALSO REF LG PG#2479617 I#1+2 FOR R & R OF ALL ELPU'S. ACCOMPLISHED ELPU'S FUNCTIONAL TEST IAW AMM 33-50-01. TEST GOOD. A/C OK FOR CONT.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 34,220 hrs · 21,956 cycles

LEFT MIDDLE EMERGENCY LIGHT ON THE WTB FAIRING WAS INOPERATIVE. R & R THE EMERGENCY LIGHT BATTERY PACK. PERFORMED AN OPS CHECK, ALL CHECKED GOOD IAW AMM 33-50-80.

Part: DOUBLER — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 32,099 hrs · 20,419 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INTERNAL FUSELAGE ON WASTE PAN INNER DOUBLERS BETWEEN FRAMES 88-89, STRINGERS 27-28R. R & R DOUBLER IAW SRM 51-43-03, AND 51-43-04.

Part: DOUBLER — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 32,099 hrs · 20,419 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INTERNAL FUSELAGE ON WASTE PAN INNER DOUBLERS BETWEEN FRAMES 88-89, STRINGERS 27-28R. R & R DOUBLER IAW SRM 51-43-03, AND 51-43-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 31,702 hrs · 20,104 cycles

BRAKE RT FAULT, AND BRAKE LT FAULT ON EICAS AFTER GEAR CAME DOWN. MESSAGES REMAINED AFTER GO AROUND. IAW FIM 32-41-00-810-824-A, PERFORMED PULSE PRESSURE BIT TEST FOR BMC 1 & 2. INSPECTED LANDING GEAR AND BRAKE HARNESS FOR CONDITION AND PIN CONNECTION FOR SECURITY. NO FAULTS NOTED ON EICAS. NO MAINTENANCE MESSAGE NOTED IN CMC (ACTIVE). SUSPECT TRANSITORY CONDITION OF THE MAIN BRAKE CONT MODULES. ACFT OK FOR SERVICE.

Part: CABLE — UNKNOWN (R2 SLIDE ARMING) · airframe 31,698 hrs · 20,101 cycles

R2 DOOR ARMING LEVER VERY DIFFICULT TO MOVE. R & R THE R2 DOOR EMERGENCY EVACUATION SLIDE MECHANISM CONTROL CABLE IAW AMM 52-42-40. OPS CHECKED GOOD. THE ACFT OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 29,808 hrs · 18,845 cycles

THE FWD LEFT OVERHEAD ENTRY DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED & REPLACED FWD THE LT ENTRY EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. PERFORMED OPS CHECK. OPS CHECK PASSED.

Part: PCU — LEAKING (NR 4 SPOILER) · airframe 27,247 hrs · 17,076 cycles

AIR TURNBACK TO DEPARTURE. AFTER TAKEOFF, LOST ALL HYD 1 QUANTITY AND HYD 1 SYSTEM. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. R & R RT NR 4 SPOILER PCU DUE TO LEAKING IAW AMM 27-65-01. REF LOG PAGE 1734048, ITEM NR 2. OPS AND LEAK CHECK GOOD.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE AT FRAME 17 AND STRINGERS 27- 28R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-43-03.

Part: BEAM — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND FWD CARGO DOOR LOWER BEAM CORRODED AT THE AFT SEAL REST CORNER. R & R THE BEAM, IAW SRM 51-41-01, 51-41-02, 51-43-03, 51=43-04. PERFORMED PRESSURIZATION CHECK OF ACFT IAW AMM 21-31-00. LEAK CHECKED GOOD.

Part: SHEAR TIE — CORRODED (FRAME 18) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE AT FRAME 18 AND STRINGERS 27 -28R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-41-01 AND 51-41-02.

Part: STRINGER — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND CORROSION ON STRINGER 29R, 1.5" FWD OF FRAME 77. REMOVED CORROSION FROM THE STR, AND PERFORMED AN HFEC INSPECTION, NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE TREATED, PRIMED AND INSTALLED THE REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE CORRODED AT FRAME 87 BETWEEN STRINGERS 27-28R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01 AND 51-41-02.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND FWD CABIN FLOORBEAM FRAME 17 CORRODED. CUT-OUT DAMAGE, PERFORMED A DYE-PENETRANT INSPECTION, NO DEFECTS FOUND., FABRICATED A REPAIR. INSTALLED THE REPAIR AND TOP COATED.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 26,194 hrs · 16,302 cycles

DURING HEAVY MAINATENANCE, FOUND SHEAR TIE CORRODED AT FRAME 86 AND STRINGERS 27- 28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, 51-41-02, AND SRM 51-23-06.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 24,614 hrs · 15,263 cycles

ACFT DIVERTED DUE TO BLEED 2 FAILED INFLIGHT WITH BLEED 1 ON MEL. R & R NR 2 ENG NAPRSOV VALVE IAW AMM 36-11-03. FAILURE SUSPECTED OVERLOAD ON SINGLE BLEED OPERATION. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (NLG STEERING) · airframe 19,992 hrs · 12,212 cycles

FLT 611 JFK-JAX, ON APPROACH WHEN LANDING GEAR CAME DOWN A NOSE STEER FAIL EICAS MESSAGE APPEARED. A GO AROUND WAS DONE AND MESSAGE WENT AWAY WHEN GEAR WAS LIFTED UP. MESSAGE RE-APPEARED WHEN GEAR WAS LOWERED SECOND TIME. QRH COMPLIED WITH FOR STEER FAILURE. CLEARED RUNWAY, TUG TO GATE. ACCOMPLISHED FIM TASK 32-52-00-810-802-A OK TRANSITORY CONDITION OF THE STEERING CONTROL MODULE MESSAGE CLEARED NWS OPERATION NORMAL REF AMM 32-50-00-06. NO HISTORY NOTED AND NO ASSOCIATED FAULT MESSAGE ON CODES.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 19,660 hrs · 12,028 cycles

FLT 1230 RDU-BOS, CREW REPORTED COCKPIT EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-01. CHECK OK.

Part: PUMP — DAMAGED (NR 2 ENGINE) · airframe 17,344 hrs · 10,571 cycles

FLT 1208 RSW-HPN, AIRCRAFT DIVERTED TO MCO DUE TO HYD 2 EDP FAIL ON EICAS. REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOOD. NOTE: REMOVED PUMP HAD A HOLE IN IT.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 17,277 hrs · 10,529 cycles

FLT 450 SJU-SXM, CREW DECLARED EMERGENCY DUE TO STEER FAIL ON APPROACH. RAN QRH AND LANDED WITHOUT STEERING. RESET SYSTEM IAW FIM 32-53-00-810-806A. NO FURTHER FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (STEERING SYS) · airframe 15,759 hrs · 9,661 cycles

FLT 1245 BOS-CLT, CREW EXECUTED A GO AROUND DUE TO ON GEAR EXTENSION RECEIVED A STEER FAULT. AIRCRAFT LANDED AND CLEARED RUNWAY THEN PERFORMED QRH RESET AND RECOVERED STEERING SYSTEM. PERFORMED RESET OF NIC 3 AND MESSAGE CLEARED. OPS CHECK OF STEERING NFF REF FIM 45-45-00-810-941A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,804 hrs · 9,003 cycles

FLT 1008 JFK-BOS, CREW DECLARED EMERGENCY DURING APPROACH AT APPROX 3,000 FEET DUE TO SLAT FAIL EICAS MSG. QRH PROCEDURE WAS ACCOMPLISHED. TECHNICIAN C/W TASK 27-80-00 AND RESET SF ACE INHIBITS. RAN FLAPS/SLATS AND MESSAGE CLEARED. OPS CHECK GOOD.

Part: PIN — BURNED (AC SYSTEM) · airframe 14,098 hrs · 8,580 cycles

FLT 440 MCO-BOS, CREW DECLARED EMERGENCY AND DIVERTED TO RDU DUE TO IFE SMOKE INDICATION ON EICAS. PERFORMED INSPECTION OF AFT CARGO COMPT AND DE-ACTIVATED IFE VENT SHUT OFF VALVE. COMPLIED WITH FIM 21-28-00-810-803A PER STEP 12. FOUND P604 AND J3261 HAD BURNED PINS. REPINNED C/P'S P604 REF WDM 25-31-51 AND J3261 REF 23-22-50. A/C RESTORED TO NORMAL CONFIGURATION. OPS CHECK OK.

Part: FILTER — FAILED (BLEED AIR SYS) · airframe 12,778 hrs · 7,847 cycles

FLT 107 BUF-JFK, VERY STRONG ODOR AT FRONT CABIN ON T/O AND DESCENT. REMOVED AND REPLACED NR 2 ENGINE OZONE FILTER IAW AMM 36-30-00. RAN ENGINE, NO FURTHER FAULTS NOTED.

Part: CONTROL MODULE — FAILED (SPOILER) · airframe 12,162 hrs · 7,484 cycles

FLT 1305 JFK-IAD DECLARED EMERGENCY DUE TO SPOILER FAULT AT 4000FT ON DOWNWIND INTO IAD. LANDED LONG, NO GROUND SPOILERS ON GRD LEFT DUMP ON ROLL OUT DEGRADED/SLOW RESPONSIVENESS TO AILERON INPUT ON FINAL APPROACH. REMOVED AND REPLACED FCM 3 PER AMM 27-03-02. PERFORMED FCM RIGGING PER 27-03-02-820-801. FAULTS CLEARED. OPS CHECK NORMAL.

Part: BLEED AIR SYS — CONTAMINATED · airframe 12,052 hrs · 7,421 cycles

FLT 408 FLL-FLL FUMES IN THE COCKPIT IN FLIGHT, TURN PACKS OFF FUMES CLEARED (NOT ELECTRICAL SMELL). SUSPECT DUE TO NR 1 ENGINE COMPRESSOR BOROSCOPE INSPECTION BORO PLUG ANTI SEIZE COMPOUND. CONTAMINATED BLEED SYSTEM CAUSING FUMES IN THE CABIN. PERFORMED HIGH POWER RUN PER AMM 72-00-00 AND PACK BURN, NO FUMES OR SMELL NOTED, PERFORMED INSPECTION PER AMM 21-20-00-810-801-A, NO DEFECTS NOTED, OK FOR SERVICE.

Part: DRIVE UNIT — FAULTY (WX RADAR ANTENNA) · airframe 11,635 hrs · 7,182 cycles

FLT JB1761-- AIR TURN BACK AFTER TAKEOFF, LOUD CLUNKING NOISE UNDER FLOOR OF COCKPIT ASSOCIATED "THUD" NOISE FELT IN FLOORBOARD, NOT CONTINUOUS BUT EVERY FEW SECONDS NOISE CONTINUED UNTIL SHORT FINAL. SJU MX PERFORMED VIBRATION/NOISE TASK AMM 05-50-00 ALSO PERFORMED RADAR SYSTEM TEST AMM 34-42-00. FOUND WEATHER RADAR ANTENNA MOTOR CAUSING SOUND EVERY 20 SECONDS UNIT PLACED ON MEL 34-42-00 COD 1 CAT C. ACFT FLEW TO FLL AND MX REMOVED AND REPLACED WX RADAR DRIVE UNIT PER AMM 34-42-01 OPS CK GOOD MEL CLEARED AIRRAFT RETURNED TO SERVICE.

Part: TRANSCEIVER — FAILED (RADAR ALTIMETER) · airframe 11,272 hrs · 6,980 cycles

FLT JB1207 HPN-RSW CREW DIVERTED TO JFK DUE TO UNCOMMANDED LANDING GEAR ORAL WARNING AT 7000/9000/13000/17000 FT, COULD NOT CANCEL WARNING IT WOULD CONTINUE FOR SEVERAL MINUTES EACH OCCURRENCE. JFK MX RETRIEVED FHDB AND DVDR DATA, DATA NOTED NR 2 RADAR ALTIMETER SYSTEM FAULTED AT APPROX 400 FT CAUSING A/C TO BELIEVE IT WAS AT 400 FT AND ASKED FOR THE GEAR TO BE EXTENDED. PERFORMED AMM FIM 34-31-00-810-810, VERIFIED TRANSMIT COAX OF SYS NR 2 HAS GOOD INSULATION AND GOOD CONTINUITY. REMOVED AND REPLACED NR 2 RADAR ALTIMETER TRANSCEIVER IAW AMM 34-31-01, ALL OPS CHECK GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 8,430 hrs · 5,250 cycles

FLT NR 1433, LGB-SFO, LOST HYD NR 2 EDP IN FLIGHT ALONG WITH LOSS OF ALL HYD QTY IN FLIGHT. DUE TO LOSS OF HYD NR 2 QTY, GEAR WAS MANUALLY LOWERED, GEAR REF QRH PROCEDURE. R&R NR 2 ENG DRIVEN HYDRAULIC PUMP, RAN ENGINE LEAK CHECK OK. NO LEAK NOTED.

Part: ACM — CONTAMINATED (NR 2) · airframe 4,959 hrs · 3,275 cycles

FLT 1047, JFK-BNA, AT APRX 21:40 PM RETURNED TO JFK, SMOKE/FUMES/HAZE IN CABIN & COCKPIT PASSING 8K FEET, GOT WORSE AS CLIMB CONTINUED. LANDED ASAP. FUMES SEEMED TO CLEAR A BIT DESCENDING THROUGH 2K FEET ON DESCENT. PERFORMED SMOKE/ABNORMAL SMELL IN PASSENGER, CABIN AND COCKPIT PER AMM 21-20-00-810-801A. NO FAULTS FOUND, NO SMELL PRESENT IN A/C. REPLACED NR 2 AIR CYCLE MACHINE & TURBINE BYPASS VALVE DUE TO COFFEE CONTAMINATION. OPS CHECK OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 4,907 hrs · 3,232 cycles

FLT 1016, JFK-, EXPERIENCED DUSTY/HAZY/BURNING ODOR IN CABIN ON TAKEOFF ROLL. ENTIRE CABIN HAZY, WARM RUSH OF AIR ON FLT DECK, LIGHTS ON FLT ATTENDANT WERE INOP. PERFORMED VISUAL INSPECTION OF NR 1 & 2 ENGINE BLEED AIR LINES. FOUND 1 BLANKING CAP MISSING FROM NR 1 ENGINE NAPRSOV. INSTALLED NEW BLANKING CAP PER AMM 36-11-031, NO OTHER DEFECTS FOUND ON NR 1 AND 2 ENGINE BLEED AIR LINES. PERFORMED VISUAL INSPECTION OF SPDA 1 PER AMM 24-61-01. NO DEFECTS NOTED, REMOVED ACCESS PANELS 191 EL AND 191 AR AND PERFORMED GENERAL VISUAL INSPECTION OF LT AND RT COOLING PACKS PER AMM 21-51-00. LEAK CHECK OF LT AND RT COOLING PACKS PER AMM 21-51-00, NO DEFECTS NOTED. REINSTALLED ACCESS PANELS 191 EL AND 191 AR PER AMM 06-41-00, PERFORMED IDLE ENGINE RUN ON LT AND RT ENGINES PER EMM 72-00-00-760-122, NO FAULTS NOTED. PERFORMED FIM PROCEDURES AS SPECIFIED IN FIM 21-20-00-810-801. UNABLE TO LOCATE OR DUPLICATE SMOKE OR ODOR ON A/C. CHECKED RECIRCULATION AIR FILTERS AMM 21-24-02, NO EVIDENCE OF CONTAMINATION FOUND, PERFORMED HI POWER ENG 1 & 2 RUN IAW EMM 71-00-00, OPERATED PACKS 1 & 2 WITH ONE ENGINE BLEED AT A TIME AND ONE PACK AT A TIME, NO ABNORMAL OPERATION OR ODOR NOTED. A/C OK TO CONTINUE SERVICE.

Part: CONTROL VALVE — FALSE INDICATION (NR 1) · airframe 3,582 hrs · 2,399 cycles

BRAKE RT & LT FAULT EICAS MESSAGES AT GEAR EXTENSION, TEMPS INDICATE O/B BRAKES FAILED. T/S PER FIM 32-41-00-810-848-A. REMOVED AND REPLACED MAIN BRAKE CONTROL VALVE NR 1 PER AMM 32-41-02/401. ALSO REPLACED MAIN BRAKE SOV 1 PRECAUTIONARY PER AMM 32-41-03. OPS CHECK GOOD, ALSO PERFORMED INFO NOTICE 2006-TO19B, OPS CHECK GOOD, NO LEAKS NOTED.

Part: WIRE HARNESS — INTERMITTENT (SLATS) · airframe 2,523 hrs · 1,711 cycles

SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (RT HARNESS INTERMITTENT). REMOVED AND REPLACED RT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-810-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A, OPS CHECK OK, NO FAULTS FOR SLAT FAIL MSGS ON EICAS.

Part: WIRE HARNESS — INTERMITTENT (LT WING SLAT) · airframe 2,523 hrs · 1,711 cycles

SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (LT HARNESS INTERMITTENT). REMOVED AND REPLACED LT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A OPS CHECK OK. NO FAULTS FOR SLAT FAIL MSG ON EICAS.

Part: CLEVIS — BROKEN (ACTUATOR) · airframe 2,200 hrs · 1,472 cycles

ON POWER APPLICATION FOR TAKEOFF NR 2 ENG WOULD NOT ADVANCE PAST 58.7 PERCENT. NR 1 ENG ADVANCE NORMALLY. NO EICAS MSGS ASSOCIATED WITH POWER APPLICATION WHEN ATTEMPTED, WAS ON AUTO THROTTLE. THIS WAS A LOW SPEED REJECT AT APPROX 45 KTS. REPLACED LEFT VSV ACTUATOR SHAFT/TORQUE LINKS, & RIGHT ACTUATOR CLEVIS PER EA E06-598, REV NEW. PERFORMED POBIT AND PWR ASSURANCE RUN PER EMM 72-00-00-760-13 AND EMM 72-00-00-760-118. OPS CKS NORMAL.