N216JB

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,781 hrs · 28,462 cycles

FLT#1432, LGA-BOS. 'STRONG BURNING OIL SMELL WHEN THROTTLES ARE ADVANCED. MORE PRONOUNCED ON F/O'S SIDE AND FWD GALLEY; PERFORMED T/S PER FIM 21-20-00. INSPECTED #1 ENG BLEED LINES AT PRSOV FOR EVIDENCE OF OIL. NO OIL WAS FOUND. REPLACED BOTH RECIRCULATION FILTERS AND RAN PACKS FULL HOT FOR 30 MIN AND FULL COLD FOR 30 MIN. NO ODOR EVENT. RAN #1 ENG AT IDLE FOR 15 MIN W/#1 PACK RUNNING. NO ODOR EVENT. A/C OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,780 hrs · 28,460 cycles

FLT#654, DCA-BOS. 'BURNT OIL SMELL IN FLIGHT DECK ON BOTH LEGS ON TAKE OFF, SMELL CLEARED DURING CLIMB; T/S PER FIM TASK 21-20-00-810-801A AND UNABLE TO DUPLICATE. A/C OK FOR SERVICE AS NO ODOR NOTED.'

Part: SHEAR TIE — CORRODED (FRM 86) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR86 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR86 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01 PAR. 5,EMB 190 SRM 51-41-02 PAR. 6 AND EMB 190 SRM 51-41-01 PAR. 6 REF. TECHOPSMX WO N216JB/2075/E190/BRIDGE CHECK NRC 00058 TECH: CORONADO LOPEZ 201217491 INSP: JIMENEZ DE LA CRUZ 202268641 (CONSIDERED AS A MAJOR REPAIR)

Part: FITTING — CRACKED (LT NACELLE) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INDICATION OF CRACK ON BUSHING HOUSING AT LH PYLON AFT INBOARD FITTING. INBOARD SPAR OF LH PYLON WAS REPLACED PER EMB 190 SRM 51-43-03 PAR 4&5 AND SRM 51-43-04 PAR.4 AND 5 AND SRM 51-41-02 PAR.4 AND 6 & AMM 20-10-01-910-801-A.'

Part: SHEAR TIE — CORRODED (FRM 82 S27-28R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR82 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY OF NRC 00060: SHEARCLIP ON FR82 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01, SRM 51-41-02- AND SRM 51-41-01. WORK ACCOMPLISHED ON TECHOPS WORK ORDER N216JB/2075/E190/BRIDGE CHECK NRC: 00060 TECH: CORONADO LOPEZ 201217491 INSP: NIEVES GARRIDO 201635713. (CONSIDERED AS A MAJOR REPAIR)

Part: FRAME — CORRODED (FRM 80 S27-28R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON FR80 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: FR80 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPAIRED PER EC NO E22-930-01, ETI-190-22-698 REV. 4, ETD2022-- 190-033239 REV.:C.

Part: STRINGER — CORRODED (FR 77-78 S29R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON STGR 29R BETWEEN FR78 / FR77 AT AFT CARGO; SUMMARY: STGR 29R BETWEEN FR75 / FR78 AT AFT CARGO WAS REPAIRED PER EMB190 SRM 53-23-03/R51.

Part: NOT REPORTED — CORRODED · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR80 & STGR 27R-28R / CORROSION. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: WASTE PANEL INTERNAL DOUBLER WAS FOUND OUT OF LIMITS, DOUBLER THICKNESS 0.098IN, REMAINING THICKNESS 0.061 IN & MATERIAL LOSS 0.037IN; REF. TOMX W/O: N216JB / 2075 NR-00136 - CUT OUT STRUCTURE AT WASTE SERVICE PANEL WAS REPAIRED PER EMB / 190 SRM 53-23-60 REPAIR 51.'

Part: SHEAR TIE — CORRODED (FRM 78 S28-29L) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. MAJOR REPAIR

Part: STRINGER — CORRODED (FRM 88 S28R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: AFTER WASTE SERVICE PANEL REMOVAL, CORROSION ON STGR 28 AT FR88; REF.TOMX W/O: N216JB / 2075 NR-00139 - REPAIR ACCOMPLISHED PER EMB 190 SRM 53-23-03 REP 51 & ETI-190-22-709, EC. 22-939-01.

Part: SHEAR TIE — CORRODED (FRM 83) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR83 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR83 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01 PAR. 5 AND 51-41-02 PAR. 6 REF.

Part: SHEAR TIE — CORRODED (FRM 81 S28-29R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR81 BETWEEN STRG 29R / 28R AT AFT CARGO; SUMMARY: SHEARCLIP ON FR81 BETWEEN STGR 28R / 28R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-41-01 AND SRM 51-41-02 WORK ACCOMPLISHED ON TECHOPS W/O N216JB/ 2075/E190/BRIDGE CHECK. NRC: 00057 TECH: CORONADO LOPEZ 201217491 INSP RII: SANCHEZ GILBERTO 201534008 NRC: 00057. (CONSIDERED AS A MAJOR REPAIR)

Part: SHEAR TIE — CORRODED (FRM 88 S27-28R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: FROM TECHOPS MX NR 00140, AFTER WASTE SERVICE PANEL REMOVAL, CORROSION ON SHEAR CLIP BTW STGR 28R/27/R AND FR 88; SHEARCLIP BTW STGR 28R/27R AND FR 88 AT AFT CARGO WAS REPLACED PER EMB SRM 51-41-01 AND SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 81 S27-28R) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: THIS NRC IS ISSUED IN REF NRC 00057: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR81 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEARCLIP ON FR81 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-41-01 AND SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 78 S28-29L) · airframe 42,903 hrs · 27,818 cycles

DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16; SUMMARY OF NRC 00055: CORROSION ON SHEARCLIP ON FR78 BETWEEN STRG 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. WORK ACCOMPLISHED ON TECHOPS W/O N216JB/2075/E190/BRIDGE CHECK NR 00055. (CONSIDERED AS A MAJOR REPAIR)

Part: TRANSDUCER — FAILED (324105-01-10-3) · airframe 41,841 hrs · 27,034 cycles

FLT#206, BNA-BOS. (AIRCRAFT DECLARED AN EMERGENCY). 'WE RECEIVED BKR RH AND LH FAULT MESSAGE DURING THE APPROACH. OUTBOARD BRAKES DID NOT WORK DURING LANDING; T/S REF E190 FIM 32-41-00-810-850-A. FOUND BRAKE PRESSURE XDCR #4 READING 100PSI MORE THAN THE OTHER 3. REMOVED AND REPLACED BRAKE PRESSURE XDCR #4 REF E190 AMM 32-41-05. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME.'

Part: MAU — FAILED · airframe 41,676 hrs · 26,931 cycles

FLT # 1423, FLL-MSY. (EMERGENCY WAS DECLARED). AVIONICS MAU 1A FAIL IN FLIGHT WITH ASSOCIATED EICAS MESSAGE.; PERFORMED POWER UP AND POWER DOWN MSG CLEARED C/W OPS CKS OPS CHECK GOOD REF FIM 31-41-00 AC OK FOR SERVICE

Part: RIB — CRACKED (RT WING LE) · airframe 39,130 hrs · 25,216 cycles

DURING HEAVY MAINTENANCE, CRACK RIB 17 FIXED LEADING EDGE ON RT WING. RESOLVED ON W/O: 1062723 TASKCARD: NR-00013, REF AEROMAN NR 2020-277-068 WO 2020 293/1. REMOVED AND REPLACED RIB 17 AND FASTENERS LOCATED AT LEADING EDGE ON RT WING, IAW E190 SRM 51-40-08, DWG 191-03201-433. PERFORMED LEAK CHECK ON FRONT SPAR LOCATED ON RIB 17, IAW E190 AMM 28-11-00-790-801-A ON RT WING. NOT FOUND LEAK TOOL USED DIGITAL CALIPER PN: 500-197-30 SN: 15319560 ACCOMPLISHED BY AEROMAN TECH 8611312 INSPECTED BY QC 141 DUE DATE: MAY-25-2021.

Part: SKIN — DENTED (FRAMES 23-24) · airframe 39,130 hrs · 25,216 cycles

DURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN BETWEEN FR 23/FR 24 AND BETWEEN STR 27L/STR 28L LOWER FUSELAGE. RESOLVED ON W/O: 1062723 TASKCARD: NR-00010, REF AEROMAN NR W/O 2020-293/1 WCC 2020-277060. ACCOMPLISHED REPAIR ON EXTERNAL SKIN BETWEEN FR 23 TO FR 24 AND BETWEEN STGR 27L TO STGR 28L LOWER FUSELAGE, IAW AEROMAN EA 53-0646-20 (COVER, PART 1-3), EMBRAER ETD2020-190-027963 REV C AND EC E20-672-01. TOOL USED: CALIPER P/N: 700-113-10, S/N: 0002956 DUE DATE: APR-21-2021. P/N: NORTEC 500D, S/N: N500X12101V022235, DUE DATE: 20-JUL-2021. P/N: 25 DL PLUS, S/N: 071504410, DUE DATE: OCT-18-2020. AEROMAN TECH 8619800; RJEY598H QC STAMP 153; RJEY598H.

Part: SKIN — CRACKED (LT WING) · airframe 39,130 hrs · 25,216 cycles

DURING HEAVY MAINTENANCE, CRACK UPPER SKIN PANEL AT LEVEL SLAT TRACK 5 CUT OUT FIXED LEADING EDGE ON LT WING. RESOLVED ON W/O: 1062723 TASKCARD: NR-00011, REF AEROMAN NNR W/O 2020-293/1 WCC 2020-277033. ACCOMPLISHED REPAIR ON UPPER SKIN PANEL AT LEVEL SLAT TRACK 5 CUT OUT FIXED LEADING EDGE ON LT WING, IAW AEM EA 57-0641-20, ETD2020-190-027268 AND EC E20-664-01. TOOL USED: CALIPER P/N: 700-113-10, S/N: 0002956, DUE DATE: APR-21-2021. RADIUS GAGE P/N: S167C, S/N: AE-28448, DUE DATE: JUN-17-2021. ET EQUIPMENT P/N: NORTEC 600D, S/N: 60009161631, DUE DATE: NOV-06-20. AEROMAN TECH 8619800; RJEY598H QC STAMP 153; RJEY598H.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 39,130 hrs · 25,216 cycles

DURING HEAVY MAINTENANCE, INOPERABLE DOOR FRAME EXIT LIGHT RT SIDE AT FWD GALLEY AREA. RESOLVED ON W/O: 1062723 TASKCARD: NR-00012, REF AEROMAN NR W/O 2020-293/1 WCC 2020-277311. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT 1, IAW E190 AMM 33-50-01/400, AIPC 33-50-01-01. PERFORMED OPERATIONAL TEST RELATED EMERGENCY-LIGHT POWER UNIT, IAW E190 AMM 33-50-01-710-801-A AND 33-50-00-710-801-A, TEST ARE OK. TOOL USED: MILLIOHMMETER P/N:M1-G-KIT S/N:DC005518. DUE DATE:DEC-03-2020AEROMAN TECH 8605813; RJEY598H QC STAMP 163; RJEY598H.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 39,128 hrs · 25,215 cycles

FLT 6102, JFK-BUF. WHEN TESTING EMERGENCY LIGHTS RECIEVED LH MIDDLE BATTERY FAULT; R & R LH MIDDLE EMERGENCY BATTERY PER MM 33-50-01.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 38,775 hrs · 24,975 cycles

FT # 1582, RSW-DCA. L1 PAX DOOR EMERG LIGHTS INOP; REMOVED 7 REPLACED EMERGENCY LIGHT POWER UNIT AT FRAME 17 - 18. OPS CHECK GOOD REF AMM 33-50-01

Part: CHECK VALVE — UNKNOWN (FAN BYPASS) · airframe 38,308 hrs · 24,653 cycles

FLT 1423, EMERGENCY DECLARED. SMOKE FUMES VISIBLE IN THE CABIN, STARTED DOWN LOW IN THE FT CABIN AT 15000 FT MSL. IAW QRH FOR CABIN SMOKE REACHED 11000 FT, CABIN CALL INDICATED THAT SMOKE WAS DISSIPATING. PERFORMED FIM 21-20-00-810-801-A, FOUND THE NR 2 PACK AT FAULT. ACCOMPLISHED THE MAINTENANCE OPERATIONAL TEST OF THE ELECTRONIC EQUIPMENT RACK VENTILATION SYSTEM IAW AMM 21-28-00/500, VERIFIED VENT SHUTOFF VALVE AND GROUND SHUTOFF VALVE OPERATED NORMALLY. REMOVED & REPLACED FAN BYPASS CHECK VALVE IAW AMM 21-51-09 OPS. CHK GOOD, NO SMOKE ODOR DETECTED.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 34,013 hrs · 21,517 cycles

DURING HEAVY MAINTENANCE, WAS FOUND WITH A CRACK IN THE LT WING LOWER FWD SKIN PANEL P/N 190-33061-009 AT RIB 9 AND STR 19/STR 20 AREA. THE CRACK MEASURES 2.725 INCH. THIS CRACK RESULTED IN FUEL LEAK IN THIS AREA. SEE REF/2/ ETD FOR MORE DETAILS. REFER TO EC E18-516-01. WINGS / LT WING / MAIN BOX LOWER SKIN / RIB 9 & 10 / CRACK DAMAGE / TEMPORARY REPAIR; THIS EC HAS BEEN APPROVED PER THE REF/6/ ANAC FORM AND THE REF/7/ SB-AD DEVIATIONS HAVE BEEN APPROVED VIA THE REF/8/ AMOC LETTER. THIS IS CLASSIFIED AS A MAJOR PERMANENT REPAIR. REPORTED THAT AFTER THE INSTALLATION OF THE PYLON AFT FARING AN INTERFERENCE CONDITION WAS FOUND BETWEEN THE SEAL SUPPORT PYLON CHANNEL 1 AND THE PROTRUDING HEADS OF FASTENERS COMMON TO THE REPAIR DOUBLERS OF THE REF /1/ EA (REV 0) AND REF /2/ ETD. THIS WAS REPORTED TO WHO PROVIDED THE REF /10 ETD WHICH PROVIDES ADDITIONAL INSTRUCTIONS IN PARAGRAPH N. TO TRIM /REWORK THE EDGES OF THE LATERAL AND AFT FAIRINGS (SEE FIGURE 32-28 OF THE REF /10/ ETD). THESE ADDITIONAL INSTRUCTIONS ARE ADDED IN PART 18 OF THE REF /9/ EA. ALL OTHER PARTS, 1-17, HAVE NO CHANGES REQUIRED BASED ON THE ISSUANCE OF THE REF /10 ETD. THIS EC IS REVISED TO INCLUDE THE ADDITIONAL INSTRUCTIONS TO REWORK THE FAIRINGS AND COMPLIES WITH THE REF /10/ ETD WITHOUT DEVIATION. THIS EC HAS BEEN APPROVED PER THE REF/11/ ANAC FORM AND THE REF/7/ SB-AD DEVIATIONS HAVE BEEN APPROVED VIA THE REF/8/ AMOC LETTER. THIS IS CLASSIFIED AS A MAJOR PERMANENT REPAIR.

Part: SKIN — CRACKED (LT WING) · airframe 33,404 hrs · 21,137 cycles

BASIC 6 CHECK AT SAL, REPORTED A CRACK ON THE LT WING LOWER SKIN (P/N 190-33065-009) AT RIB 10+1", AS SHOWN IN THE REF /1/ EA. THE CRACK WAS REMOVED BY MEANS OF REF. /4/ SRM, HOWEVER, CUTOUT DIMENSIONS WERE NOT WITHIN THE LIMITS. ADDITIONALLY, WHILE ACCOMPLISHING HFEC INSPECTION PER E190 NDT PART 1, 51-00-00-916-802-A, TWO ADDITIONAL CRACKS WERE FOUND COMMON TO HOLES OF A REPAIR AREA. AFTER OVER-SIZING THE HOLES, CRACKS WERE REMOVED. SEE REF. /1/ EA FOR ADDITIONAL INFORMATION. WAS CONTACTED TO ASSESS THE WORK ACCOMPLISHED AND INFORM IF ACCEPTABLE. PROVIDED REF. /2/ ETD WHICH PROVIDES INSTRUCTIONS TO REMOVE AND DISCARD ALL AFFECTED FASTENERS, CUT OUT THE DAMAGE (AS WAS ALREADY DONE), PERFORM HFEC INSPECTION, FABRICATE A FILLER AND A DOUBLER AND INSTALL; THIS REPAIR IS APPROVED PER REF. /2/ ETD. THIS REPAIR IS CATEGORIZED AS PERMANENT REPAIR AND IS CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,400 hrs · 21,136 cycles

DURING HEAVY MAINTENANCE, A CRACK WAS FOUND IN THE EXTERNAL SKIN ON THE LOWER FUSELAGE. REPAIRED THE SKIN IAW EA 57-0004-18, AND EC E18-043-01.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 32,425 hrs · 20,426 cycles

EMERGENCY LIGHT POWER UNIT IN FWD RT GALLEY BY THE R1 SERVICE DOOR FAILED CAPACITY TEST. FAILED AFTER 6 MIN. R & R EMERGENCY LIGHT POWER UNIT IAW MM 33-50-01. OPS CHECKED GOOD.

Part: BOTTLE — EMPTY (PAX DOOR) · airframe 31,477 hrs · 19,723 cycles

DURING A WEEKLY CHECK, FOUND FWD PASSENGER DOOR PRESSURE GAUGE AT 0 PSI. INSPECTED FWD PASSENGER DOOR PNEUMATIC ASSEMBLY AND FOUND THE PNEUMATIC ASSEMBLY DIAPHRAGM PUNCTURED. R & R THE DIAPHGRAM IAW 52-11-53 AND SERVICE DOOR IAW 52-11-51. ACFT OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 30,474 hrs · 19,048 cycles

R2 DOOR LOWER RED EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY EXIT SIGN & EPSU BATTERY. OPS TEST PASSED IAW AMM 33-50-01 & 33-50-15.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 28,209 hrs · 17,447 cycles

DURING PRE-DEPARTURE CHECK LIST FOUND EMERGENCY LIGHT OVER L1 DOOR INOPERATIVE. R & R FORWARD ELPU IAW 33-50-01. OPS CHECK OK.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 26,988 hrs · 16,642 cycles

DIVERTED DUE TO FLAP FAIL UPON EXTENSION. FLAPS NEVER EXTENDED BEYOND 2. FLAPS LOCKED AT ZERO. FOUND LT SIDE NR 2 FLAP ACTUATOR JAMMED. R & R LT SIDE NR 2 FLAP ACTUATOR IAW AMM 27-51-01. RIG AND OPS FOUND GOOD.

Part: SEAL REST — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER DOOR CUTOUT LOWER CENTER SEAL REST IS CORRODED. REPLACED SEAL DEPRESSOR IAW SRM REF 51-41-01. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SEAL REST — CORRODED (FRAME 85) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER DOOR CUTOUT LOWER CENTER SEAL REST IS CORRODED AT FRAME 85+7" AT LBL 49. REPLACED SEAL IAW SRM REF 51-40-01. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE FOUND SHEAR TIE AT FRAME 82 BETWEEN STR 27-28R CORRODED. REPLACED THE SHEAR TIE IAW SRM REF 51-10-03.

Part: SEAL REST — CORRODED (FRAME 86) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER DOOR CUTOUT LOWER CENTER SEAL REST CORRODED AT FRAME 86+1" AT LBL 49". REPLACED SEAL IAW SRM REF 51-41-01.

Part: SEAL REST — CORRODED (FRAME 86) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER ENTRANCE 3.5" AFT OF FR 86 UNDER CENTER SEAL REST CORRODED, BLENDED AND TOPCOATED IAW EC E15-853-01 THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE FOUND SHEAR TIE AT FR 87 BETWEEN STR 27-28R AT AFT DRAIN CORRODED REPLACED SHEAR TIE IAW SRM IAW 51-41-01.

Part: SEAL REST — CORRODED (FRAME 85) · corrosion level 2 · airframe 26,702 hrs · 16,439 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER DOOR CUTOUT LOWER CENTER SEAL REST CORRODED AT FRAME 85+9", LBL 49. REPLACED SEAL REST IAW SRM REF 51-41-01. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SENSOR — FAILED (SLATS) · airframe 25,883 hrs · 15,877 cycles

ON CLIMB, RECEIVED SLAT FAIL AFTER APPROXIMATELY 400 AGL. DIVERTED. R & R RT OTBD SLAT SKEW SENSOR 2 & 3 AND 3 & 4 IAW AMM 27-83-01 AND PERFORMED SLAT CONTROL SYS, ELECTRCAL, RIGGING IAW AMM 27-80-00. OPS CK GOOD AT THIS TIME WITH NO MESSAGES NOTED. ACFT OK FOR SERVICE.

Part: SENSOR — FAILED (SLATS) · airframe 25,883 hrs · 15,877 cycles

ON CLIMB, RECEIVED SLAT FAIL AFTER APPROXIMATELY 400 AGL. DIVERTED. R & R RT OTBD SLAT SKEW SENSOR 2 & 3 AND 3 & 4 IAW AMM 27-83-01 AND PERFORMED SLAT CONTROL SYS, ELECTRCAL, RIGGING IAW AMM 27-80-00. OPS CK GOOD AT THIS TIME WITH NO MESSAGES NOTED, ACFT OK FOR SERVICE.

Part: I/O CARD — FAILED (NR 1) · airframe 23,469 hrs · 14,367 cycles

CREW DECLARED AN EMERGENCY AND ACFT DIVERTED. CARGO FWD SMOKE AT FL 270, 12 MIN AFTER T/O PUSHED AFFECTED CARGO SMOKE, THE LIGHT NEVER WENT OUT. R & R NR 1 CUSTOM I/O & NR 1 GENERIC I/O CARDS IAW AMM 31-41-06-04 & 31-41-07-04. ALL CKS NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 21,961 hrs · 13,454 cycles

DURING MAINTENANCE CHECK, FOUND OVERWING FWD RT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT POWER UNIT NR 3, MID CABIN IAW AMM 33-50-01. OPS CHECKED NORMAL.

Part: CIRCUIT CARD — FAILED (SPDA 2) · airframe 21,806 hrs · 13,364 cycles

AIRCRAFT DIVERTED, FLIGHT DECK TEMP UNCONTROLLABLE, COCKPIT TEMP 3C CABIN TEMP 17C. R & R AMS CONT CARD SPDA 2 SLOT REF AMM 21-00-03. OPS CK GOOD.

Part: CROSSBEAM — CORRODED (CABIN) · airframe 21,227 hrs · 13,003 cycles

DURING HEAVY CHECK, FOUND FWD CABIN CROSSBEAM FRAME 14 RT CORRODED, REMOVED CORROSION IAW EAMS NR H4029/1546, CUTTING OUT AREAS WITH OVER 40 PERCENT CORROSION. HFEC INSPECTION AND INSTALLED A (LT) ANGLE AND FILLER AS PERMANENT REPAIR IAW EA E13-647-01.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE FUEL) · airframe 20,781 hrs · 12,674 cycles

AIR RETURN DUE TO NR 2 ENGINE FUEL LOW PRESSURE AND FUEL FEED FAULT EICAS DURING CLIMB. FOLLOWED BOTH QRH'S AND ENG 2 FUEL LO PRESS REMAINED ON EICAS. ON FUEL PAGE GREEN AC PUMP BUT WHITE FUEL LINE TO ENGINE. INDICATIONS NORMAL EXCEPT ENG 2 JUST A LITTLE SLOW TO SPOOL UP AT THROTTLE ADVANCE ON TO (JUST A LITTLE). PERFORMED FIM 73-361-00-810-804-A. FOUND NR 2 ENG FUEL LOW PRESS SWITCH FAULTY. R & R OPS CK NORMAL. PERFORMED EJECTOR PUMP SYS AND HIGH POWER RUN NO DEFECTS NOTED. OK FOR SVC. AMM 28-21-25 AND FIM 28-21-00-810-815-A.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 20,690 hrs · 12,610 cycles

CREW REPORTED BURN ODOR IN THE GALLEY. FAULT ISOLATION PERFORMED IAW FIM 21-20-00-810-801-A, PAGE 205, BLOCK 1 AND FIM 25-30-00-810-801-A, FOUND THE FORWARD LT COFFEEMAKER AT FAULT. OPEN

Part: CONVERTER — ODOR (AC BAY) · airframe 20,207 hrs · 12,277 cycles

FLT 1296 PIT-BOS, CREW REPORTED IN MOIST, AIR PACKS HAVE STRONG DIRTY SOCK ODOR. APPLIED FIM TASK 21-20-00-810-801 A, REMOVED AND REPLACED RIGHT OZONE CONVERTER AND LEAK CHECKED OK IAW 36-30-00. REPLACED 2 EACH RECIRCULATION AIR FILTERS IAW 21-24-02. PERFORMED OPS CHECK OF LEFT AND RIGHT AIR CONDITIONING PACKS INDIVIDUALLY WITH APU, NR 1 ENGINE AND NR 2 ENGINE BLEEDS IAW 21-00-00. NO SMELL NOTED.

Part: CONTACT — LOOSE (EMERGENCY LIGHTS) · airframe 17,882 hrs · 10,876 cycles

FLT 1758 SJU-FLL, DURING WEEKLY CHECK, LEFT AFT MAIN DOOR EMERGENCY EXIT IDENTIFIER INOP. TROUBLESHOT PER WDM 33-50-50, SHT 4, FOUND LOOSE CONTACT AT SPLICE SP0904. RECONNECTED AND OPS CHECK NORMAL PER MM 33-50-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 16,288 hrs · 9,848 cycles

FLT 6409, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN FRAME 17 CORRODED ALONG LEADING EDGE OUTBOARD OF RIGHT SEAT TRACK. COMPLIED WITH TASK CARD EC E12-052-01 REFERENCE EAMS NON ROUTINE H2767-2521. THE CORROSION DAMAGE WAS BLENDED OUT AND THE FABRICATED "L" SHAPED REPAIR ANGLES INSTALLED ON FRAME 17 RT SIDE OF THE CABIN AREA. (MFG P/N 170-21769-403)

Part: EPSU — FAILED (CABIN) · airframe 16,240 hrs · 9,809 cycles

FLT 1223, EMERGENCY LIGHTS OUT IN CENTER OF CABIN. REMOVED AND REPLACED ELPSU PER FIM 33-50-00-810-816 AND AMM 33-50-01, OPS CHECK GOOD.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 14,747 hrs · 8,863 cycles

FLT 571 HPN-PBI, CREW EXECUTED EMERGENCY LANDING DUE TO ENG (1) ENG (2)FIRE, APU FIRE, AFT AND FWD CARGO FIRE INDICATIONS. TECHNICIAN REMOVED AND REPLACED FIRE EXTINGUISHER PANEL IAW AMM 26-20-01. ALSO REPLACED GENERIC I/O MODULE NR 1 IAW AMM 31-11-06. OPS CHECK NORMAL.

Part: SPLICE — DISCONNECTED (CABIN) · airframe 13,757 hrs · 8,264 cycles

FLT 6417 JFK-BNA, DURING MAINTENANCE CHECK AT BNA THE AFT PAX DOOR EMERGENCY LIGHT WAS INOP. RECONNECTED SPLICE AT AFT PAX DOOR LIGHT IAW SWPM 20-41-20 REFERENCE NR 2522 AND OPS CHECK GOOD.

Part: DUCT — LOOSE (INTAKE)

AIR RETURN TO DEPARTURE DUE SOUND IN COCKPIT AS IF N1 OR NX SYNC WAS OFF. ENG INDICATIONS NORMAL. FOUND AIR INTAKE FOR BOTH RT AND LT DUCT ON 191FL LOOSE, TIGHTENED CLAMPS AND SECURED, OPS CHECK OK. (K)

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 5,724 hrs · 3,650 cycles

FLT 426, PBI-BOS, ON APPROACH AFTER SELECTING LDG GEAR DOWN, RECEIVED A STEER FAIL EICAS.INTERROGATED STEER FAIL MESSAGE IN CMC. NO CORRELATED FAULTS FOUND. COMPLIED WITH FIM TASK 32-53-00-810-806A. ALL FAULTS CLEARED. PERFORMED CHECK OF STEERING SYSTEM PER AMM 32-52-00-720. ALL CHECK GOOD. TAXIED AIRCRAFT AND STEERING SYSTEM OPERATES NORMALLY. NO DEFECTS NOTED AT THIS TIME.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 4,441 hrs · 2,941 cycles

FLT NR 141, JFK TO RSW, RETURNED TO JFK, LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. FOLLOW QRH PROCEDURES INCLUDING WOW SWITCH FAILURE. NORMAL LANDING, ALL OTHER WOW AFFECTED SYSTEMS, OPERATED NORMALLY. TROUBLESHOT AS PER FIM REF 32-33-00-810-802-A. NO LDG WOW SENSOR TGT DISAGREE MESSAGES NOTED ON CMC. ACCOMPLISHED OPS TEST OF LDG CONTROL LEVER AMM REF 32-33-00-710-801-A. CHECKS GOOD. ACCOMPLISHED SEVERAL EXTENSION AND RETRACTIONS OF THE LDG GEAR HANDLES OPERATED NORMAL AND NO FAULTS NOTED. CHECKED NLG AND MLG SHOCK STRUT H DIMENSIONS. ALL WITHIN LIMITS AS PER AMM REF'S 12-12-07 AND 12-12-09. FAULT CONSIDERED TRANSITORY CONDITION OF THE LDG CONTROL LEVER.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 4,441 hrs · 2,941 cycles

FLT NR 141, JFK TO RSW, RETURNED TO JFK, LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. FOLLOW QRH PROCEDURES INCLUDING WOW SWITCH FAILURE. NORMAL LANDING, ALL OTHER WOW AFFECTED SYSTEMS, OPERATED NORMALLY. TROUBLESHOT AS PER FIM REF 32-33-00-810-802-A. NO LDG WOW SENSOR TGT DISAGREE MESSAGES NOTED ON CMC. ACCOMPLISHED OPS TEST OF LDG CONTROL LEVER AMM REF 32-33-00-710-801-A. CHECKS GOOD. ACCOMPLISHED SEVERAL EXTENSION AND RETRACTIONS OF THE LDG GEAR HANDLES OPERATED NORMAL AND NO FAULTS NOTED. CHECKED NLG AND MLG SHOCK STRUT H DIMENSIONS. ALL WITHIN LIMITS AS PER AMM REF'S 12-12-07 AND 12-12-09. FAULT CONSIDERED TRANSITORY CONDITION OF THE LDG CONTROL LEVER.

Part: MODULE — FAILED · airframe 1,897 hrs · 1,317 cycles

ON CLIMB-OUT, EICAS DISPLAYED AVNX ASCB FAULT AND SEVERAL OTHER MESSAGES THAT COULDN'T READ IN TIME DROPPED AUTO PILOT, AUTO THROTTLES, ETC. REMOVED AND REPLACED NIC/PROC MODULE NR 5 IAW E190 TASK 31-41-04. ALL OPS NORMAL.