N184JB

Part: NONE — NONE · airframe 42,955 hrs · 28,165 cycles

FLT#1232, LGA-BOS. 'R2 DOOR DIFFICULT TO ARM; REPLACED R2 DOOR FWD VISUAL LOCK INDICATOR REF AMM 52-42-22-000-802-A.'

Part: NONE — NONE · airframe 42,681 hrs · 27,994 cycles

FLT # 2028, MCO-EWR. ON DEPARTURE AT 1000 FT AGL BOTH RADIO ALTIMETERS TURNED AMBER. FO'S HUD PROVIDED ERRONEOUS DATA ; COMPLIED WITH INFO NOTICE 2022-T001, NO DEFECTS NOTED, OK FOR SERVICE SUSPECT 5G INTERFERENCE. MCC DAVID NOTIFIED PER AMM 34-31-00-710-801-A

Part: SLIDE — DEPLOYED (L2-SLIDE) · airframe 42,296 hrs · 27,747 cycles

FLT 1274, CHS-JFK. WHILE T/C C2514012-01 "DOOR SLIDE FIRING CABLE TENSION", THERE WAS A INADVERTENTLY SLIDE DEPLOYMENT ON L2 DOOR ; R/R L2 DOOR SLIDE IAW AMM 25-65-01.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 40,466 hrs · 26,626 cycles

FLT # 1141, BDL-PBI. R1 EPSU FAILED OPS TEST ; R & R R1 SVC DOOR POSITION EPSU W/SERVICEABLE ASSY PER AMM 33-50-01. OPS TEST OK (CORRECT REGISTRATION NUMBER AND DATE)

Part: RIB — CRACKED (RT WING) · airframe 39,700 hrs · 25,892 cycles

DURING HEAVY MAINTENANCE, RH WING LEADING EDGE RIB 17 HAS CRACK; REF AEROMAN 2020-56275: R & R RIB 17 ON LEADING EDGE RH WING IAW E190 SRM 51-40-08 & DRAWING 190-31005-405.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 38,014 hrs · 24,669 cycles

SUPPLEMENTAL INFORMATION: FLT 1037, SJU-SDQ. RETURNED TO FIELD. OVERWHELMING DIRTY SOCK ODOR AFTER TAKEOFF. WE BOTH FELT NAUSEOUS AND HAD HEADACHES. INFLIGHT DID NOT SMELL IT IMMEDIATELY, BUT DID AFTER ABOUT 5 MINS; PERFORMED OPERATIONAL CHECK REF 71-00-01 ALSO ACCOMPLISHED PROCEDURES ON AIRCRAFT FIM 21-20-00-810-801A. NO ABNORMAL ODOR DETECTED WITH ENGINES AND /OR APU BLEEDSOURCES. A/C IS GOOD TO CONTINUE SERVICE.

Part: UPLOCK — FAULTY (NLG) · airframe 36,647 hrs · 23,727 cycles

FT 1210, JAX-MCO. NOSE GEAR INDICATES UP, THEN EVERY 5 SECONDS AMBER, THEN UP. WE CAN FEEL IT MOVING. R&R NLG UPLOCK PER AMM 32-32-03. OPS CK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 36,288 hrs · 23,464 cycles

FT # 1354, DCA-BOS. LH LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP; R & R POWER SUPPLY #6, OPS NORMAL REF AMM 33-50-01.

Part: SEAL — CONTAMINATED (EMERGENCY EXIT) · airframe 33,153 hrs · 21,226 cycles

LOUD SQUEAL NOISE FROM OVERWING EXIT AT 12D. OCCURRED ENTIRE FLIGHT ABOVE 10,000 FT. REMOVED & REINSTALLED THE RT OVERWING ESCAPE HATCH IAW AMM 52-21-00/400. INSPECTED DOOR LOCK MECHANISM SEAL IAW AMM 52-21-20/600 & FOUND BUILD UP OF DEBRIS ON THE SEAL. REMOVED CONTAMINATE & CLEANED SEAL.

Part: PROCESSOR — FAILED (MAU 3) · airframe 33,082 hrs · 21,176 cycles

EMERGENCY DECLARED ON APPROACH HAD A CARGO SMOKE AFT ON THE EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT, CARGO AFT SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6 MAU 3 NIC 2.

Part: PROCESSOR — FAILED (MAU3) · airframe 33,082 hrs · 21,176 cycles

EMERGENCY DECLARED ON APPROACH. CARGO SMOKE AFT EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT. AFT CARGO SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6, MAU 3, NIC 2.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 32,881 hrs · 21,028 cycles

DURING HEAVY MAINTENANCE, CORROSION DISCOVERED ON THE FLOOR SUPPORT FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 32,881 hrs · 21,028 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 30,725 hrs · 19,519 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 16, BETWEEN STRINGERS 27 AND 28R. R & R THE SHEAR TIE IAW SRM 51-42-02 AND 51-43-03.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 30,725 hrs · 19,519 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 17 BETWEEN STRINGERS 27 - 28R. R & R THE SHEAR TIE IAW SRM 51-41-02, AND 51-43-03.

Part: ENGINE — VIBRATION (NR 1) · airframe 29,370 hrs · 18,563 cycles

FLIGHT CREW REPORTED HIGH ENGINE VIBRATION ON DEPARTURE. ACFT DIVERTED DUE TO HIGH VIBRATION AND ENGINE EXCEEDANCE ON NR 1 ENGINE. NR 1 ENGINE R & R.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 26,643 hrs · 16,641 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. RESET CONNECTOR AT RT EMERGENCY LIGHT BATTERY PACK. EMERGENCY LIGHT SYSTEM OK.

Part: DISPLAY — FAILED (NR 2) · airframe 26,108 hrs · 16,274 cycles

DURING FLIGHT, ODOR OF HOT PLASTIC "MFD 2 OVHT". PERFORMED AND COMPLIED WITH INSPECTION FOR ABNORMAL ODOR OF SMOKE IAW 21-20-00-810-801-A. R & R NR 2 MFD IAW AMM 31-61-01. OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FRAME 81) · airframe 25,576 hrs · 15,959 cycles

ON MAINTENANCE CHECK, FOUND FRAME 81 BETWEEN STR 27 & 28R HAS ONE CORRODED SHEAR CLIP. REF EAMS NR 4490-1611, REMOVED DAMAGE SHEAR CLIP, PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED NEW SHEAR CLIP. ALL WORK ACCOMPLISHED IAW EA E15-146-01.

Part: CIRCUIT CARD — FAILED (MAU 1) · airframe 24,053 hrs · 14,953 cycles

AIRCRAFT DIVERTED DUE TO AN INTERMITTENT FIRE INDICATION ON NR 1 ENGINE ITT GAUGE, NO ORAL WARNINGS, FIM 26-11-00-810-807A FAULT CODE 26110014UT1 GENERIC I/O MODULE 1, MAU 1 MOD 11/12, FAILED. R & R GEN I/O MOD MAU 1 SLOT 11/12. ACCOMPLISHED SUCCESSFUL TARGET LOAD IAW AMM 45-45-00. OPS CK OF CARD IAW AMM 31-41-06, OPS CK OK.

Part: VALVE — WARNING MESSAGE (PARKING BRAKE) · airframe 21,567 hrs · 13,358 cycles

PARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. R & R DUAL EMERGENCY PARK BRAKE VALVE IAW AMM 32-44-01. ALL OPS AND LEAK CHECKED OK.

Part: PRESSURE SWITCH — WARNING MESSAGE (PARKING BRAKE) · airframe 21,567 hrs · 13,358 cycles

PARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. FAULT CODE 32400001UT1. R & R EMERGENCY PARK BRAKE PRESSURE SWITCH SYS 1 IAW AMM 32-44-09. ALL OPS AND LEAK CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,323 hrs · 13,200 cycles

DURING MX L1 AND L2 LOW LEVEL EMERGENCY LIGHT IDENTIFIERS HAS SECTIONS INOPERATIVE. R & R BOTH L1 AND L2 EXIT IDENTIFIERS LIGHT ASSY IAW AMM 33-50-15. OPS CHECK OK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 21,323 hrs · 13,200 cycles

DURING MX, RT OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-01, OPS CHECKED GOOD.

Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 18,762 hrs · 11,568 cycles

FLT 1678 KIN-FLL, CREW DECLARED EMERGENCY DUE TO HYD 2 ELEC PUMP FAIL FOLLOWED BY HYD 2 LO QTY. QRH CALLED FOR CREW AWARENESS. QTY WAS 0 BUT PRESS WAS 2900. PHONE PATCH TO MX, ASKED CREW TO PUT HYD 2 ELEC SW TO ON. AT THAT POINT HYD 2 SYS FAILED. TROUBLESHOT AS PER FIM TASK 29-11-00-810-806A AND FOUND NR 2 ACMP PRESS INLET HOSE WITH RUPTURE AT NR 2 FILTER MANIFOLD CONNECTION. REMOVED AND REPLACED NR 2 ACMP INLET HOSE IAW AMM 29-11-02. OPS AND LEAK CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 18,650 hrs · 11,483 cycles

FLT 1055 JFK-PIT, HYDRAULIC SYSTEM 2 FAIL - FLUID ZERO QUANTITY AFTER NORMAL GEAR EXT / NO HYD OVERHEAT MSG. PERFORMED DETAIL VISUAL INSPECTION AND FOUND RETRACT/EXT HOSE ASSY LEAKING. REMOVED AND REPLACED HOSE ASSY IAW AMM 20-10-03. HYDRAULIC QTY LOW SERVICED TO CORRECT LEVEL IAW AMM 12-12-00. NO LEAKS NOTED, A/C OK FOR SERVICE, LEAK CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,053 hrs · 11,096 cycles

FLT 746 SJU-MCO FOUND OVERHEAD EMERGENCY LIGHT INOP ABOVE ROW 1. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-50-00, OPS CHECK NORMAL.

Part: BYPASS VALVE — FAILED (AC PACK) · airframe 16,562 hrs · 10,185 cycles

FLT 974 FLL-BOS, AIRCRAFT DIVERTED TO MCO DUE TO CABIN AND FLIGHT DECK TEMPERATURE UNCONTROLLABLE, TEMP WAS MODULATING BETWEEN HOT AND COLD. REMOVED AND REPLACED NR 2 PACK BYPASS VALVE PER AMM 21-51-10-04 OPS CHECK OF TEMP CONTROL OK.

Part: CONVERTER — FAULTY (LEFT) · airframe 16,136 hrs · 9,914 cycles

FLT 1080 CLT-JFK, BURNING OIL SMELL IN COCKPIT ON TAKEOFF. DUE TO HISTORY WITH RECIRCULATION FILTERS ALREADY REPLACED, THE TECHNICIAN REMOVED AND REPLACED LT OZONE CONVERTER PER AMM 36-30-00. LEAKS CHECK OK.

Part: DETECTOR — SHORTED (BLEED AIR SYS) · airframe 13,473 hrs · 8,275 cycles

FLT 522 MCO-EWR, AIR TURNBACK TO MCO DUE TO NR 2 ENG BLEED LEAK EICAS MESSAGE WHILE CLIMBING THROUGH FL300. CREW PERFORMED QRH PROCEDURE AND MESSAGE EXTINGUISHED. FOUND LOOP 5 LEAK DETECTOR SHORTED. REMOVED AND REPLACED AS PER AMM 36-21-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 13,472 hrs · 8,274 cycles

FLT 590 PBI-HPN, FLT CREW DECLARED EMERGENCY AND A/C DIVERTED TO MCO DUE TO BLEED 2 LEAK MSG IN FL 310. QRH PROCEDURE COMPLETED. BLEED 2 SELECTED OFF (XBLEED) CAS MSG EXTINGUISHED. INTERROGATED CMC FOUND BLEED 2 LEAK, ODS PACK LOOP 5 (RT BLD) [C1] /WRG FAULT. T/S REF FIM 36-21-00-810-802-A AND 36-21-00-810-804-A00. CMC ODS PARAMETERS CONFIRM OVERHEAT COND TRUE, EVENT LOC 11.90 AND SHORT COND TRUE FOR SYS 2 BLEED CHAN 1 AND CHAN 2. PERF BLD ODS NVM READ/RESET MSG CLEARED/ FAULT CLEARED. REMOVED ACCESS PANEL 429AT PER FIM 36-21-00. PERF VISUAL INSP OF BLEED DUCTS, CLAMPS, LINES AND THERMAL INSUL REF AMM 36-11-04. NO DEFECTS NOTED AT THIS TIME. RAN ENG AND ENG BLEED. CONFIRMED NO PHYSICAL INDICATION OF BLEED LEAK NOTED. RE-INSTALLED ACCESS PANEL 429AT REF AMM 54-50-21. RESTORED A/C TO INITIAL CONFIG. A/C OK FOR CONT SERVICE.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 11,851 hrs · 7,309 cycles

FLT JB1224 LGB-PDX FLIGHT FROM LONG BEACH TO PORTLAND OREGON DIVERTED TO OAK DUE TO ENGINE NR 1 FIRE DETECTION FAIL MESSAGE DURING CRUISE. PERFORMED QRH PROCEDURES AND LANDED UNEVENTFUL. INSPECTION OF NR 1 ENGINE FOUND LOW PRESSURE TURBINE BLADE DAMAGE LPT STG 4 ONE BLADE BROKEN OFF AND NUMEROUS OTHERS BENT. REMOVED AND REPLACED NR 1 ENGINE IAW TASK CARDS IN WO 62524 PER AMM1 71-00-01-000-801 AND 71-00-01-400-801. ACCOMPLISHED RUN UPS AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (STEERING SENSOR) · airframe 11,047 hrs · 6,840 cycles

FLT JB1401 FLL-AUS "STEER FAIL" AMBER EICAS MESSAGE DISPLAYED AT GEAR EXTENSION, LOSS OF NOSE WHEEL STEERING ON LANDING AIRCRAFT TOWED TO GATE. MX PERFORMED TROUBLESHOOTING NO FAULT CODE FOUND, RESET AIRCRAFT AND ACCOMPLISHED STEERING ELECTRONIC SYSTEM INSPECTION/CHECK, OPS CHECK GOOD PER AMM 32-53-00. AT JFK MX PERFORMED ADDITIONAL T/S IAW AMM 32-50-00-06AND FOUND LOOSE CONNECTOR ON STEERING FEEDBACK SENSOR P33, NO OTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (EL SLAT) · airframe 10,809 hrs · 6,705 cycles

FLT JB78 - MCO-JFK "SLAT FAIL" AT ZERO DURING DESCENT FOR LANDING, SLATS SELECTED AND FAILED TO MOVE. CREW NOTIFIED ATC, AIRCRAFT LANDED SAFELY. MX TROUBLESHOT PER AMM FIM 27-81-00 FOUND RIGHT WING SLAT ACTUATOR NR 4 AT FAULT, REMOVED AND REPLACED RT WING NR 4 SLAT ACTUATOR IAW AMM 27-81-01, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLEED AIR SYS — LEAKING · airframe 10,542 hrs · 6,554 cycles

FLT 1326 BWI-BOS - DEPARTED BWI WITH LEFT ENGINE BLEED DEFERRED. ON CLIMBOUT AT 19000FT THE NR 2 ENGINE BLEED LEAK EICAS MESSAGE APPEARED. LEVELED OUT AT 20000FT TO EVALUATE SITUATION. CONFIRMED BLEED LEAK INDICATION REQUESTED DESCENT TO 10000FT. AT 12000FT TRIED APU START UNSUCCESSFUL. TRIED A SECOND APU START SUCCESSFUL AND CONTINUED TO BOS AT 10000FT UNEVENTFUL. PERFORMED FIM TASK 36-21-00 VISUAL INSPECTION RUN UP AND LEAK CHECKS ALL OK. RETURNED AIRCRAFT BACK TO SERVICE.

Part: HINGE — LOOSE (COCKPIT DOOR) · airframe 10,491 hrs · 6,523 cycles

FLT 1119 - COCKPIT DOOR UNATTACHED FROM DOOR FRAME. FOUND UPPER HINGE LOOSE, SECURED UPPER HINGE AND INSTALLED COCKPIT DOOR AS PER AMM 52-51-01. OPS CHECK GOOD.

Part: PIN — DAMAGED (LEAK DETECTOR) · airframe 10,484 hrs · 6,520 cycles

FLT 1417, AT FLT 280. BLEED 2 LEAK. REMOVED AND REPLACED LEAK DETECTOR CERAMIC PINS AT (P2146) AND (J2148) LOCATED FWD TOP PYLON IAW AMM 36-20-01. CHANNEL NR2 OPS CHECK GOOD.

Part: COMPUTER — FAILED (NR 1) · airframe 10,183 hrs · 6,344 cycles

FLT 1068, AUS-JFK, DIVERTED TO BNA, "AVNX MAU 1A FAIL" IN FLIGHT AT 370, AUTO PILOT DISCONNECT AND MULTIPLE ASSOCIATED FAILURES ON EICAS. TROUBLESHOT MAU 1A FAIL FAULT CODE 45452143CMC IAW EMB 190 FIM 45-45-00-810-939-A00. MAU1 NIC PROC 1 CHECKS FAULTY, REMOVED AND REPLACED MAU1 NIC PROC 1 IAW EMB190 AMM 31-41-04 SYSTEMS OPS CHECK GOOD. NO FAULT NOTED.

Part: SENSOR — FAILED (BLEED AIR SYS) · airframe 9,843 hrs · 6,155 cycles

FLT 462, RSW-BOS - THE BLEED 2 LEAK MSG APPEARED ALONG WITH LEAK ROW ON 2 BUTTON. RAN QRH, ALL INDICATIONS REMAINED THE SAME. DIVERTED TO MCO. PERFORMED FIM TASK 36-21-00-810-804A, FOUND FAILURE OF LEAK DETECTOR LOOP 5 SEGMENT 1RT0186 CHANNEL 1. REMOVED & REPLACED LEAK SENSOR PER AMM 36-21-02, OPS CHECKS OK. MESSAGE CLEARED.

Part: CONTROLLER — FAILED (NR 2) · airframe 9,639 hrs · 6,043 cycles

FLT 1402, AUS-SFO, CLIMBING THRU FL 280, BLEED 2 LEAK AMBER EICAS MESSAGE ILLUMINATED (ENGINE BLEED SYS-SINGLE-NO ICING). RETURN TO AUS DUE NR 1 BLEED ON MEL. REF FIM 36-21-00-810-804A. REMOVED AND REPLACED BOTH AMS CONTROLLER PROCESSOR MODULES (CH A&B) AS PER AMM 21-00-01/401 MESSAGE CLEARED. NO FAULTS NOTED, RAN NR 2 ENG WITH BLEED AIR ON. NO EICAS MESSAGE NOTED. OPS CHECK OK.

Part: MODULE — FAILED (NLG STEERING) · airframe 9,556 hrs · 5,988 cycles

FLT 1068, AUS-JFK, STEER FAIL ON APPROACH WHEN DOWN LANDING GEAR. DECLARED EMERGENCY, FOLLOWED QRH. REMOVED AND REPLACED NR 2 STEERING FEEDBACK SENSOR NR 2 FOR TROUBLESHOOTING. REMOVED & REPLACED STEERING MODULE PER AMM 32-53-01. PERFORMED ADJUSTMENT & FEEDBACK SENSOR PER AMM 32-53-05. PERFORMED ADJUSTMENT OF PEDAL SENSOR PER AMM 32-52-03. PERFORMED FUNCTIONAL TEST OF STEERING HYDRAULIC SYSTEM, ALL RIGS & OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (LE SLAT) · airframe 9,340 hrs · 5,851 cycles

FLT 337, IAD-MCO, "SLAT FAIL" EICAS MESSAGE ON SLAT EXTENSION, 220 KIAS AT 6000FT (SPD BRK EXT) LANDED FLAPS "2" SLAT "0" PER QRH. APP SPEED 166 KIAS BRAKE TEMP PEAKED AT 315 DEG. FAULT DETERMINED TO BE TRANSITORY CONDITION PER E190 FIM 27-81-00-810-802-A. A/C OK FOR SERVICE AT THIS TIME. AS PRECAUTION CHECKED ALL SLAT ACTUATORS FOR TORQUE LIMIT TRIP, NONE PRESENT AT THIS TIME PER AMM 27-81-01.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 9,024 hrs · 5,666 cycles

FLT 5110, BNA-JFK - AIR RETURN TO BNA, ENG 1 FUEL LO PRESS, AMBER MSG AT 8000FT AFTER DEPARTURE, ACCOMPLISHED OPS TEST OF FUEL PRESS. SYSTEM PER 73-31-00-801-803-A. OPS TEST GOOD. ACCOMPLISHED ENG FEED EJECTOR PUMP OPS CHECK PER AMM 28-21-13, REF FIM 28-21-00-810-814-A00. OPS CHECK NORMAL, NO FAULTS NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 8,888 hrs · 5,590 cycles

FLT 115 JFK-MSY - SMOKE IN COCKPIT AFTER TAKEOFF. SMELL THROUGHOUT A/C. DOME LIGHT TURNED ON, SMOKE CONFIRMED. ACCOMPLISHED MX PROCEDURES. PERFORMED POWER ASSURANCE TEST ON BOTH ENGS PER AMM 71-00-00 AND BLEED TEST PER AMM 36-11-00, NO ODOR OR SMOKE PRESENT DURING ENG RUNS OR BLEED TESTS. NO WARNINGS OR FAULTS NOTED. PERFORMED LTV ELECTRICAL ODOR SYSTEM INTEGRITY CHECK, NO ABNORMALITIES FOUND SYSTEM DEEMED OPERABLE PER LTV AMM 44-20-10-01.

Part: UNKNOWN — ODOR (CABIN)

STRONG PLASTIC BURNING ODOR, AFTER TAKEOFF UNTIL 3000 FEET. ODOR RETURNED ON DOWN WIND AT 3000 FEET UNTIL TOUCHDOWN. PERFORMED FIM TASK 21-20-00-801A. NO FURTHER DEFECT NOTED. RAN AIR CONDITIONER (CREW) CAN NOT DUPLICATE ON THE GROUND. ACFT OK TO CONTINUE. (K)

Part: BATTERY — OVERTEMP (#2 POSITION) · airframe 4,102 hrs · 2,858 cycles

ON TAKEOFF ROLL BATTERY NR 2 OVERTEMP EICAS MESSAGE. T/S TSM 24-36-810-804-A. REMOVED AND REPLACED NR 2 MAIN BATTERY, GROUND CHECK OK.

Part: PITOT HEAD — UNKNOWN (NR 3) · airframe 515 hrs · 420 cycles

AIRCRAFT EXPERIENCED LOSS OF ADS SYSTEM NR 3 & NR 4. CMC SHOWED NR 3 & NR 4 (SMART PROBES) PITOT/STATIC AOA SENSOR. REMOVED & REPLACED NR 3 AND NR 4 INTEGRATED PITOT/STATIC AOA SENSOR IAW AMM 34-13-01, OPS CHECK. NO FAULT NOTED.

Part: CYLINDER — DAMAGED (NR 5)

WHILE IN CRUISE CONFIGURATION AT 16500 FEET, 32 INCH HG/2200 RPM THE PILOT NOTED A SHUTTER FOLLOWED BY A DROP IN MANIFOLD PRESSURE RESULTED. WITHIN 60 SECONDS THE MANIFOLD PRESSURE FLUCTUATED RAPIDLY, FOLLOWED BY A LOUD BANG. THE ENGINE WAS SECURED AND AN UNEVENTFUL LANDING FOLLOWED. INSPECTION OF THE ENGINE REVEALED THE NR 5 CYLINDER ASSEMBLY HAD SEPARATED FROM THE ENGINE. THE PISTON AND CONNECTING ROD WERE ATTACHED AND IN THE CYLINDER, THE ROD CAP HAD SEPARATED AND WAS FOUND IN THE CRANKCASE.