N339JB

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,694 hrs · 20,598 cycles

FLT#481, DCA-RSW. (AIRCRAFT DIVERTED TO BWI) 'MULTIPLE GEESE STRUCK AT ROTATION. THE NOSE GEAR DOOR ARM WAS FOUND BROKEN ON POST-FLT; PERFORMED INSP IN REF TO AMM 05-50-02-200-801-A. FOUND RH NLG AFT DOOR LINKAGE ROD BROKEN AND AFT DOOR FWD SEAL BENT. NO SIGN OF INGESTION ON BOTH ENGINES. NO DAMAGE WAS NOTED ON SLATS AND FLAPS. NO DAMAGE NOTED ON MLGS.'

Part: PRESSURE SWITCH — FAILED (324409-01-10-2) · airframe 29,715 hrs · 19,893 cycles

FLT#2160, PHL-BOS.(AIRCRAFT DECLARED AN EMERGENCY INTO BOS) 'PRKG BRK NOT RELEASED ON EICAS IN FLIGHT; T/S PER FIM 32-41-00-810-852A. REMOVED AND REPLACED #2 EMERGENCY/PARKING BRAKE PRESS SWITCH PER AMM 32-44-09. OP'S CHECK'S OK.'

Part: NONE — NONE · airframe 29,498 hrs · 19,734 cycles

FLT#640, CLE-BOS. 'R1 DOOR ASSIST BOTTLE DISC RUPTURED; REPLACED R1 DOOR ASSIST BOTTLE DISC AND SERVICED IAW AMM 52-41-53. OPS CHECK GOOD.'

Part: SLIDE — DEPLOYED (R1-SLIDE) · airframe 29,498 hrs · 19,734 cycles

FLT#640, CLE-BOS. 'R-1 DOOR SLIDE BLOWN; REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-65-01. OPS CHECK GOOD.'

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: CRACK: NLG WHEELWELL FR15 AT HORIZONTAL RH UPPER WEB INTERNAL SIDE OF FUSELAGE L= 1.400"; REF TOMX WO: N339JB/2012/E190/B5 CHECK NR 00292: FR15 AT HORIZONTAL RH UPPER WEB WAS REPAIRED PER JETBLUE E/C E22-729-01, TOMX ETI-190-22-644 REV 3, AND ETD2022-190-026938 REV A.

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FUSELAGE / FRAME 15 / WEB / BETWEEN STGR 24R - 25R / CRACK - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: INOPERATIVE AFT PASSENGER DOOR EMERGENCY EXIT IDENTIFIER SIGN WAS FOUND; REF. TOMX WO: N339JB/2012 NR 00371 - T/S OF THE EMERGENCY LIGHT POWER UNIT #5 WAS PERFORMED PER EMB 190 FIM 33-50-00-810-810-A. ELPU WAS REMOVED AND SERVICEABLE ELPU WAS INSTALLED PER EMB - 190 AMM 33-50-01. SATISFACTORY TEST.

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: AFTER MID-SEAL REST REMOVAL, FOUND CORROSION IN LWR BEAM-BAG DOOR FR, AL. LOCATED BETWEEN FR 77/80 AFT CARGO DOOR CUTOUT; REF. TOMX WO N339JB/2012 NR-00321 -: CORROSION IN LWR BEAM-BAG DOOR AT AFT CARGO DOOR CUTOUT WAS REMOVED AND EVALUATED, THEREFORE ITS OUT LIMITS. LWR BEAM BAG DOOR WAS REPLACED PER EMB190 SRM 51-40-08 PAR 3 AND 5, SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03.

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / FLOOR STRUCTURE / RH FLOOR TRACK BTW FR 12-14 /CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP, LOCATED BTW FR 90 AND STGR 29L / 29R AT AFT CARGO COMPARTMENT INTERNAL STRUCTURE; REF TOMX WO 2012 N/R 00226 SHEAR CLIP, LOCATED BTW FR 90 AND STGR 29L / 29R AT AFT CARGO COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER EMB 190 SRM 51-41-02, SRM 51-41-01, SRM 51-43-01 AND DWG 170-66324-001 REV A.

Part: NONE — NONE · airframe 28,664 hrs · 19,159 cycles

DURING HEAVY MAINTENANCE: FROM TECHOPS MX WO2012, NRC00208. (CPCP FINDING): CORROSIÓN ON BEAM FLOOR STRUCTURE UNDER FWD GALLEY, BTW FR 12 AND FR 14; APPROX. Y+ 290 MM; REF TECHOPSMX WORK ORDER # 2012 N/R# 00208, TECHOPSMX TECH #201532129, TECHOPSMX RII INSPECTOR #200701413. SUMMARY OF NRC 00208: BEAM FLOOR STRUCTURE UNDER FWD GALLEY, BTW FR 12 AND FR 14; APPROX. Y+ 290 MM WAS REPAIRED PER N° EC E22-722-01, ETI-190-22-650 REV: 3 AND ETD2022-190-027200. (CONSIDERED A MAJOR REPAIR)

Part: NONE — FAILED (TRIM-AIR-FWD) · airframe 28,580 hrs · 19,089 cycles

FLT#2480, EWR-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) 'AFTER TAKEOFF ECS SYSTEM ONLY BLEW HOT AIR. CABIN TEMPS REACHED 43C. TEMP CONTROLS SET TO FULL COLD/18C AND ECS IS UNRESPONSIVE TO CHANGES. SLIGHT DECREASE IN TEMPS WITH REDUCED THROTTLE TRIED JUST PACK 1 AND JUST PACK 2 BUT SAME RESULT; REMOVED AND REPLACED FWD TRIM BYPASS VALVE IA AMM 21-62-05. SYS OPS CHECK NORMAL.'

Part: ANTENNA — FAILED (RA-2-RECEIVE) · airframe 26,897 hrs · 17,932 cycles

FLT 2618, FLL-JAX(AIR TURN BACK). LANDING GEAR WARNING ANNUNCIATED WITH GEAR UP AT 5000 DURING THE CLIMB. THE WARNING COULD NOT BE SILENCED.; REPLACED #2 R/A RECEIVER ANTENA IAW M/M 34-31-02, ACCOMPLISHED OPS CHECK, FOUND TO BE NORMAL. SEE L/P# 3241737 ITEM #1 FOR AURAL WARNING SYSTEM.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,276 hrs · 16,967 cycles

FLT 102, JFK-BUF. PERSISTENT FUEL SMELL OBSERVED BY FLIGHT ATTENDANTS AND CUSTOMER DURING CRUISE AND DESCENT PHASES OF FLIGHT. TEST FLIGHT INSPECTION REVEALED NO FUEL SMELL BY FLIGHT CREW; CREW DID NOT COMPLETE MX271 GROUND RAN APU NO SMELL NOTED #1 AND 2 ENG NO SMELL NOTED A/C OK FOR SERVICE PER FIM 21-20-00-810-803-A.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 24,960 hrs · 16,762 cycles

FLT 1633, BTV-JFK. COCKPIT EMERGENCY LIGHT INOPERABLE. REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY, REF AMM 33-50-03, NO HELP. INSTALLED ORIGINAL ASSEMBLY. REPLACED EMERGENCY LIGHT POWER UNIT NR 1, REF AMM 33-50-01. OPERATIONS TEST OK.

Part: SKIN — CRACKED (RT WING) · airframe 23,219 hrs · 15,428 cycles

DURING HEAVY MAINTENANCE, CRACK LOWER RH WING PANEL BTW RIB 9 AND RIB 10 TRAILING EDGE AREA; REF AE NR 2019-278012 WCC 2019-195/1 PERFORMED REPAIR TO RH WING SKIN BTW RIB90RIB10 PER AEROMAN EA 57-0412-19 COVER R0 PARTS 1-4 AND ETD 2019-190-127021 REV B. TOOLS USED CALIPER PN 700-113-10 S/N 0096657 DUE 12/28/19, NORTEC500D, S/N N500X12101V022240 DUE 4/8/20. PN CBG-10-2-N-1, S/N AE 39299 DUE 10-25-19. PN CBG-8-2-N-1 S/N AE 24086 DUE 6/21/20 MICROMETER 293-340-S/N 25201548 DUE 6/23/20.

Part: SKIN — CRACKED (RT WING) · airframe 23,219 hrs · 15,428 cycles

DURING HEAVY MAINTENANCE, N339JB (MSN 490) WAS REPORTED WITH A VISIBLE CRACK WAS DETECTED AFFECTING THE RIGHT HAND WING AFT REAR SPAR LOWER SKIN P/N 190-33065-032 AFT EDGE, BETWEEN RIB 10/RIB 11 (SEE REF /1/ EA). THE DAMAGE WAS OUT OF THE SRM’S SCOPE. FURTHER INSPECTIONS FOUND THREE ADDITIONAL CRACKED HOLES COMMON TO THE WING AFT REAR SPAR, AFFECTING THE LOWER SKIN ONLY. EMBRAER WAS CONTACTED AND INSTRUCTED TO TRIM OUT TWO CRACKED SKIN SECTIONS, OVERSIZING THE REMAINING TWO AFFECTED HOLES, PERFORMING NDT INSPECTIONS, FABRICATING AND INSTALLING TWO REPAIR BUSHINGS, FABRICATING AND INSTALLING ALUMINUM REPAIR FILLER, AND INSTALLING A DOUBLER PN 191-34897-001. THIS EC E19-744-01 WILL PROVIDE TEMPORARY REPAIR INSTRUCTIONS VALID FOR 12 MONTHS. EC E19-744-02 WILL TRACK THE 12-MONTH DTA; EMBRAER APPROVED THIS REPAIR PER REF /2/ ETD AND IS CLASSIFIED AS MAJOR.

Part: FITTING — CRACKED (RT PYLON) · airframe 23,219 hrs · 15,428 cycles

DURING HEAVY MAINTENANCE, CRACKED FITTING UPPER SPAR INBOARD SIDE ON RH PYLON; REF AEROMAN NR 2019-278043 WCC 2019-195/1 ACCOMPLISHED PART REPLACEMENT ON INBOARD UPPER SPAR ON RH PYLON IN ACCORDANCE WITH AEROMAN EA 54-0421-19 AND EMBRAER ETD 2019-124080 REV A. TOOLS USED: MICROMETER PN 103-178 S/N 67151664 DUE 7/13/20 TORQUE PN QD2R150 S/N 1211501831 DUE 4/19/20, TORQUE PN 1QDR2R200 S/N 0117001279 DUE 4/19/20 TORQUE QD2R1000 S/N 0611043847 DUE 6/20/20. MILLIOHMMETER PN M1-G-KIT S/N DC005518 DUE 6/13/20. TORQUE PN QD2RFR75B S/N 0219112550 DUE 2/22/20 TORQUE PN QD2R200 S/N 0117001450 DUE 5/8/20, MILLIOHM METER C15292 S/N 1693 DUE 10/30/19. ALSO ACCOMPLISHED IAW JB EC E19-760-01.

Part: SKIN — CRACKED (LT WING) · airframe 23,219 hrs · 15,428 cycles

DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL BTW RIB 9 TO RIB 10 TRAILING EDGE ON LH WING; (REFENCED AEROMAN WO 2019-195/1 WCC 2019-278011) PERFOMED PERMANENT REPAIR LOWER SKIN PANEL BTW RIB 9 TO RIB 10 TRAILING EDGE ON LH WING IAW E190 SRM 57-10-01 REPAIR 54 ITEM 9 FIG 201 SHEET 2.

Part: SENSOR — FAILED (LE SLAT) · airframe 22,419 hrs · 14,866 cycles

FLT 1786, PIT-BOS. EMERGENCY DECLARED. SLAT FAIL EICAS ENROUTE. WHEN FLAPS EXTENDED GOT EICAS MESSAGES "SPOILER FAULT" " AOA LIMIT FAILURES" SHAKER ANTICIPATED"; THESE MESSAGES GENERATED DUE TO "SLAT FAIL" ON DEFECT 2248055 ITEM 1. THESE MESSAGES HAVE BEEN CLEARED DUE TO RESOLUTION OF SLAT FAIL. TROUBLE SHOT PER FIM 27-83-00-810-829. REMOVED AND REPLACED RIGHT WING SLAT SCREW SENSORS PER AMM 27-83-02. OPERATION OF SLATS NORMAL AND NO FAULTS NOTED.

Part: SENSOR — FAILED (LE SLAT) · airframe 22,419 hrs · 14,866 cycles

FLT 1786, PIT-BOS. EMERGENCY DECLARED. SLAT FAIL EICAS ENROUTE. WHEN FLAPS EXTENDED GOT EICAS MESSAGES "SPOILER FAULT" " AOA LIMIT FAILURES" SHAKER ANTICIPATED"; THESE MESSAGES GENERATED DUE TO "SLAT FAIL" ON DEFECT 2248055 ITEM 1. THESE MESSAGES HAVE BEEN CLEARED DUE TO RESOLUTION OF SLAT FAIL. TROUBLE SHOT PER FIM 27-83-00-810-829. REMOVED AND REPLACED RIGHT WING SLAT SCREW SENSORS PER AMM 27-83-02. OPERATION OF SLATS NORMAL AND NO FAULTS NOTED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 21,250 hrs · 14,091 cycles

FLT 1186, RDU-JFK. L1 DOOR ESCAPE SLIDE INADVERTENTLY UNRAVELED; R & R L1 DOOR ESCAPE SLIDE IAW AMM 25-65-00. OPS CK GOOD. R & R DOOR ASSIST BOTTLE DIAPHRAGM IAW AMM 52-11-53 + SERVICED IAW AMM 52-11-51 OPS CK GOOD. HOLDS PRESSURE.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUCTURE, FR 16 LBL 45, ON FWD FLOOR SILL; R & R FWD FLOOR SILL IAW SRM 51-41-02 REV.34.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FORWARD FUSELAGE FLOOR STRUCTURE, AT RBL 16 AND BETWEEN FR 12 AND FR 13 ON FLOORBEAM FWD; REPLACED GALLEY SUPPORT BEAM IAW SRM 51-41-02 REV 34.

Part: SEAT TRACK — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUCTURE, ON RT SEAT TRACK BETWEEN FRAMES 12 AND 14. R & R THE SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-03, & 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT PASSENGER CABIN FWD WET AREA FRAME 16, LBL45, FLOOR SUPPORT BRACKET UPPER SURFACE; R & R FLOOR BRACKET AT FR 16 LBL 45.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUCTURE, ON RH TRACK AT FR 17; R & R SEAT TRACK.

Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT AFT CARGO DOOR CUTOUT, ON AFT LOWER CORNER SEAL REST. R & R SEAL REST IAW SRM 20-10-01.

Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 16,438 hrs · 10,600 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT AFT CARGO DOOR CUTOUT, ON LOWER UPPER SEAL REST SURFACE; R & R SEAL REST IAW SRM 20-10-01.

Part: SHUTOFF VALVE — LEAKING (CABIN PRESSURE) · airframe 11,011 hrs · 6,999 cycles

RETURNED TO DEPARTURE. BLEED 1 FAILED CLIMBING THROUGH 21,500'. AIRCRAFT LOST PRESSURIZATION, CABIN CLIMBED TO 6900'. FOUND NR 1 NAPRSOV AT FAULT, LEAKING. R & R NR 1 NAPRSOV IAW AMM 36-11-02, OPS LEAK CK GOOD. ACCOMPLISHED CABIN PRESS TEST IAW AMM 21-31-00-720-802-A. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 10,452 hrs · 6,611 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOORBEAM FRAME 87, LBL 9.5"-LBL 12". REMOVED CORROSION AND INSTALLED DOUBLER IAW SRM 51-10-03 & 51-23-10.

Part: BEAM — CORRODED (FRAME 23) · corrosion level 2 · airframe 10,452 hrs · 6,611 cycles

DURING HEAVY MAINTENANCE, CORROSION FOUND FORWARD CARGO DOOR LOWER BEAM. BLENDED CORROSION ON FORWARD CARGO DOOR LOWER BEAM IAW SRM E1-10-03. PERFORMED HFEC INSPECTION ALONG AREA OF CORROSION. RESTORED SURFACE PROTECTION REF SRM 51-21-04;51-21-05; 51-21-06.

Part: BEAM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 10,452 hrs · 6,611 cycles

DURING HEAVY MAINTENANCE, FOUND AFT PAX DOOR LOWER BEAM HAS CORROSION AT AFT FLOOR FITTING. ACCOMPLISH DETAILED VISUAL INSPECTION, REMOVED THE CORROSION, PERFORMED HFEC INSPECTION IAW E190 51-00-00-916-803 OF ALL REWORKED AREAS, APPLIED ALODINE IAW SRM 51-23-04. APPLIED EPOXY PRIMER IAW SRM 51-23-05. REPLACED THE AFFECTED FASTENERS AND RESTORED THE ORIGINAL FINISHING IAW SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 10,452 hrs · 6,611 cycles

DURING HEAVY MAINTENANCE FOUND CORROSION, SHEAR CLIP FRAME 88 BETWEEN STR 27R & 28R. BLENDED TO EVALUATE CORROSION ON BOTTOM INBD AFT SIDE OF SHEAR CLIP REF SRM 51-10-03. MEASURED CORROSION FROM AFT INBD EDGE AT 1.5" X 1" X 100 PERCENT MATERIAL LOSS. SHEAR CLIP NEEDS REPLACEMENT. R & R CORRODED SHEAR CLIP REF SRM 51-41-01;51-41-02. LOCATED AND DRILLED NEW SHEAR CLIP REF SRM 51-40-02. INSTALLED NEW SHEAR CLIP REF SRM 51-41-01 & 51-41-02. EDGE SEALED NEW SHAER CLIP REF SRM 51-21-02. TOP COATED FASTENERS. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: VALVE — OUT OF POSITION (L1 DOOR SLIDE) · airframe 7,459 hrs · 4,655 cycles

FOUND L1 DOOR SLIDE VALVE ACTUATOR ROTATED INBD AND IN A POSITION WHERE SAFETY PIN COULD NOT BE INSTALLED. R & R L1 DOOR SLIDE PACK ASSY IAW AMM 25-65-01. R & R DOOR PNEUMATIC ASSY DIAPHRAGM DUE TO CONTROLLED SLIDE DEPLOYMENT ACCOMPLISHED. OPS OK.

Part: PROBE — FAILED (NR 4) · airframe 6,879 hrs · 4,295 cycles

AIRCRAFT DIVERTED, ALTIMETER ERROR 280 FT DIFFERENCE BETWEEN CAPT AND F/O. R & R NR 4 INTEGRATED PROBE IAW AMM 34-13-01. OPS CK OK. ACCOMPLISHED ADS SYS FUNCTIONAL TEST IAW AMM 34-15-00, NO FAULTS FOUND.

Part: FADEC — FAILED (NR 1 ENGINE) · airframe 3,583 hrs · 2,223 cycles

FLT 525 EWR-MCO, AT THE GATE NR 1 ENGINE ONLY OPERATING-GROUND PWR ADDED BUT NOT SELECTED-ELEC DID NOT DISPLAY PROPERLY- THEN THRUST LEVERS REMAINS AT IDLE ENGINE NR 1 INCREASED N1 FROM 20.1 N1 TO 30.1 N1 NO PILOT INPUT- START/ STOP SELECTION SWITCHES SELECTED OFF-ENG SHUTDOWN NORMAL FROM THAT POINT FWD. REMOVED AND REPLACED ENGINE NR 1 FADEC. OPS CHECK GOOD REF EMM 73-00-00-800-812.