N353JB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
14 reports on file, 2015-07-26 – 2022-05-28.
Part: CONNECTOR — INOPERATIVE · airframe 24,859 hrs · 46,816 cycles
FLT#1120, DTW-JFK. (AIRCRAFT DIVERTED TO EWR) 'BLEED 1 LEAK AT CRUISE ALTITUDE (ENGINE BLEED SYS - SINGLE - ICING OK); PERFORMED T/S IAW FIM 36-21-00-810-813-A, NO ACTIVE FAULTS. ELECTRICAL CHECKS OF LOOP 3 IAW AMM 36-21-02, SHOWED FAULT AT LOOP 3 CONNECTORS IN WTB FAIRING. REPLACED CERAMIC PINS IAW AMM 36-20-01. OPS CHECKS GOOD, THIS CLEARS MDDR #474084, PLACARD REMOVED, MX-4 UPDATED, MCC NOTIFIED DAR, DISPATCH #94123.'
Part: NONE — NONE · airframe 24,286 hrs · 16,446 cycles
FLT#618, MSP-JFK. 'MODERATE ODOR ON DEPARTURE WITH APU ON DUE TO REF ECS OFF TAKEOFF WITH BLEED 1 INOP. IMPROVED WHEN THE APU WAS TURNED OFF AS PART OF THE AFTER TAKEOFF CHECKLIST. ODOR SMELLED LIKE EXHAUST; PERFORMED FIM TASK 21-20-00-810-801-A + 21-20-00-810-803-A FOUND NO DEFECTS OR ODORS INSPECTED APU COMPARTMENT + OPERATED APU + ENGINE #2 NO ODORS PRESENT AT THIS TIME A/C OK FOR CONTINUED SERVICE.'
Earlier reports · 2015–2021 · 12 reports
2021
Part: PRESSURE SWITCH — FAILED (324409-01-10-2) · airframe 23,352 hrs · 15,824 cycles
FLT #10, JAX-BOS. PARKING BRAKE ON CAUTION MSG DURING FLIGHT AFTER LANDING. EMR BRK FAULT MESS. ILLUMINATED; R+R EMERGENCY/PARKING BRAKE PRESSURE SWITCH 2 IN REF TO AMM 32-44-09. OPS CHECK GOOD. NO MESSAGES AT THIS TIME. OK FOR FURTHER SERVICE
2020
Part: FRAME — CRACKED (FRM 52) · airframe 21,980 hrs · 14,993 cycles
DURING HEAVY MAINTENANCE, CRACK FRAME 52 ON WEB RH SIDE ON LOWER FUSELAGE (1EA); (RESOLVED ON W/O: 1052659 TASKCARD: NR-00006 ) ACCOMPLISH THE REPAIR OF THE CRACK AT THE WING TO FUSELAGE FAIRING FRAME 52 IN ACCORDANCE WITH AEROMAN EA 53-052-20 (COVER , PART 1) AND EMBRAER EDT 2020-190-022068 REV. A AND EC NO. E20-540-01.
Part: SKIN — CRACKED (RT WING) · airframe 21,980 hrs · 14,993 cycles
DURING HEAVY MAINTENANCE, CRACK LOWER SURFACE SKIN LOC RIB 9 TO RIB 10 ON RH WING; (RESOLVED ON W/O: 1052659 TASKCARD: NR-00005 ) PERFORMED PERMANENT REPAIR ON LOWER SURFACE SKIN BTW RIB 9 RO RIB 11 ON RH WING IAW E190 SRM 57-10-01 REPAIR 54, ITEM 9, FIGURE 201 SHEET 6, NO FURTHER ACTION REQUIRED
2018
Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,421 hrs · 10,997 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR CUT OUT, FWD LWR CORNER SEAL REST. CORR OUT OF LIMITS REF SRM 53-23-11 AD52 SEAL REST RPL IAW AMM 20-10-01/200.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,421 hrs · 10,997 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD FUSELAGE FLOOR STRUC BET FR13-14 RBL 11, TRACK BEAM PREV RPR DOUBLER; RPL PER SRM 51-41-02 REV37 & JB EC 16-167-01.
Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,421 hrs · 10,997 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR CUT OUT STRUCT LWR MID SEAL REST. CORR OUT OF LIMITS REF SRM 53-23-11 AD52 SEAL REST RPL IAW SRM 51-41-01.
Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,421 hrs · 10,997 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR CUT OUT AFT LWR CORNER SEAL REST. CORR OUT OF LIMITS REF SRM 53-23-11 AD52 SEAL REST RPL IAW AMM 20-10-01/200.
2017
Part: BLEED VALVE — FAILED (HYDRAULIC SYS) · airframe 12,919 hrs · 8,512 cycles
FT 1170, MCO-RIC, RETURN TO FIELD. ENROUTE, CREW REPORTED SYSTEM 2 HYDRAULICS INDICATED LOW QUANTITY ON EICAS, QUANTITY DROPPED TO 0; FOUND NR 2 HYD SYS FOUND RESERVOIR ECOLOGY BOTTLE OVERFLOWING. R&R HYD SYS RESERVOIR RELIEF/BLEED/SAMPLE VALVE IAW AMM 29-11-10. LEAK WAS RESOLVED. OPS CHECK PASSED.
2016
Part: BRAKE ASSY — FAILED (MLG) · airframe 10,802 hrs · 7,038 cycles
AFTER LANDING AND CLEAR OF RUNWAY, NR 4 BRAKE SEEMED TO BE STICKING PARTIALLY. TEMP ROSE TO APPROX 350 DEGREES. NO MESSAGES APPEARED ON EICAS. ACCOMPLISHED INSPECTION FOR OVERHEATED WHEELS/BRAKES IAW AMM 05-50-16-200-801A. R & R MLG, CARBON BRAKE ASSEMBLY. ACCOMPLISHED OPS BRAKE TEST IAW AMM 34-41-00, OPS NORMAL. ACFT OK FOR SERVICE.
Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,236 hrs · 6,666 cycles
AFT CARGO FWD FINGER PLATE CORRODED AT FRAME 77 +2.0", RBL 15; REPLACED DOUBLER IAW SRM REF 51-43-03, REF EAMS NR H4884-00203.
Part: SEAT TRACK — CORRODED (FRAME 13) · corrosion level 2 · airframe 10,236 hrs · 6,666 cycles
SEAT TRACK CORRODED BETWEEN 4.25" TO 5.25" AFT OF FRAME 13 AND FROM RBL 10.0" TO 10.25"; REPAIRED AND COMPLIED WITH EA E16-167-01 ON WO 761579 TALLY 5045.
2015
Part: MODULE — MALFUNCTIONED (FLIGHT CONTROL) · airframe 8,424 hrs · 5,453 cycles
RETURN TO DEPARTURE. FLIGHT CONTROL SHUTTER WITH MANUAL CONTROL DURING TURNS, WITH AP ON NO ISSUES. R & R MAU 2 PROCESSOR MODULE 3 IAW MM 31-41-04.