N358JB
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.
22 reports on file, 2014-12-18 – 2023-12-25.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,314 hrs · 18,673 cycles
FLT#134, JFK-BTV. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO JFK) ' LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. QRH ALTERNATE METHOD USED TO RETRACT. (GEAR RETRACTED WITH ALTERNATIVE METHOD); PERFORMED 3 GEAR SWINGS, OP CHECK OK AND MEASUREMENT R/R LMLG WOFW 2 SENSOR AS PRECAUTION IAW 32-62-03. SINCE IT SQUACK ON PFR FAULT CODE 32611305PSS, PERFORMED 3 MORE GEAR SWINGS AND OPS CHK OK, A/C OK FOR SVC.'
Part: UNKNOWN — UNKNOWN · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: THE LEFT INBD PYLON SPAR CRACKED; REF TOMX NRC 00283 WO 2162 INBD SPAR AT LH PYLON WAS REPLACED PER EMB-190 SRM 51-43-03 AND SRM 51-43-04, ETI-190-23-516 REV. 2, ETD2023-190-003959 REV. A & E23-131-01.'
Part: NONE — NONE · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: DURING POWER ON, AFT RH EMERGENCY LIGHT WING FAIRING AND CELLING PNL 11 CENTER FUS III WERE FOUND INOPERATIVE; REF TO TOMX WO 2162 NR 00350, EMERGENCY-LIGHT POWER UNIT (ELPU) P/N: 3400-22-10 S/N: 002987 WAS REMOVED PER EMB 190 AMM 33-50-01-000-801-A AND EMERGENCY-LIGHT POWER UNIT (ELPU) P/N: 3400-22-10 S/N: 010038 WAS INSTALLED PER EMB 190 AMM 33-50-01-400-801-A. SATISFACTORY TEST.
Part: NONE — NONE · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: DURING LIGHTS CHECK IN REFERENCE TO R.C. 004:J3K-190-D-E190 SERVICE CHECK, RH EXTERNAL MIDDLE EMERGENCY LIGHT WAS FOUND INOPERATIVE; REF TO TOMX WO 2162 NR 00346, RH EXTERNAL MIDDLE EMERGENCY LIGHT P/N: 2LA006954-11 WAS REMOVED PER EMB-190 A.M.M. 33-50-25-000-802-A AND RH EXTERNAL MIDDLE EMERGENCY LIGHT P/N: 2LA006954-11 WAS INSTALLED PER EMB-190 AMM 33-50-25-400-802-A. SATISFACTORY TEST.
Part: NONE — NONE · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: A CRACK OF 0.150IN LENGTH AT FRAME 15 FLOOR STRUCTURE BEAM Y=270 RH AT FWD PASSENGER CABIN WAS FOUND; REF TO TOMX WO 2162 NR 00335, CRACK OF 0.150IN LENGTH AT FRAME 15 FLOOR STRUCTURE BEAM Y=270 RH AT FWD PASSENGER CABIN WAS REPAIRED PER EMB-190 SRM 53-10-10/REP51 AND THIS REPAIR DOES NOT AFFECT AN FCS. THEREFORE, THERE IS NO CHANGE IN THE MAINTENANCE PLAN DUE TO THIS PROCEDURE.
Part: NONE — NONE · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: CRACK ON FIXED LEADING EDGE BTW RIB 19/20 AT LH WING; CRACK ON FIXED LEADING EDGE BTW 19/20 AT LH WING WAS REPAIRED PER EMB190 SRM 57-49--1. REPAIR 51P AND SDR ARE REQUIRED. O REF TOMX WO 2162 NR 00015 FOR WORK PERFORMED).
Part: NONE — NONE · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: CRACK ON FIXED LEADING EDGE BTW RIB 19/20 AT RH WING; REF TOMX WO#2162 NR 00013 FOR WORK PERFORMED FIXED LE BTW RIB 19/20 AT RH WING WAS REPAIRED PER EMB190 SRM 57-49-01 REPAIR 51P SDR REQUIRED.
Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 24,401 hrs · 17,180 cycles
DURING HEAVY MAINTENANCE: CORROSION ON SEAT TRACK BEAM FLOOR STRUCTURE LOCATED AT FR 84 BTW +Y 300 RH SIDE ON W2; REF TOMEX NRC 00312, WO 2162, SEAT TRACK BEAM FLOOR STRUCTURE LOCATED AT FR 84 BTW +Y 300RH SIDE ON W2 WAS REPAIRED PER EMB-190 SRM 53-00-10/REP. 51 AND THIS REPAIR DOES NOT AFFECT AN FCS.THEREFORE, THERE IS NO CHANGE IN THE MAINTENANCE PLAN DUE TO THIS PROCEDURE. (CONSIDERED AS A MAJOR REPAIR)
Earlier reports · 2014–2022 · 14 reports
2022
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 23,965 hrs · 16,894 cycles
FLT#1719, JFK-ATL. 'AFTER THE MAIN BOARDING DOOR WAS DISARMED AND OPENED FROM THE EXTERIOR, THE #1 FA SAW THE GIRT BAR STILL ENGAGED WITH THE INTERIOR OF THE PLANE. THE SLIDE BEGAN TO FALL OUT FROM STORAGE BUT DID NOT BLOW; REPLACED L1 DOOR W/ NEW EMERGENCY SLIDE IAW AMM 25-65-01. THE DOOR INDICATION CHECK IS GOOD. A/C OK TO RETURN TO SERVICE.
Part: NONE — FAILED (EMER-BATT-AFT-RH) · airframe 23,352 hrs · 16,342 cycles
FLT#2152, MCO-BOS. 'L2 EMERGENCY EXIT SIGN INOP; REMOVED AND REPLACED AFT L2 ELPU IAW AMM 33-50-01.'
Part: BLEED AIR SYS — FAULT MESSAGE · airframe 23,164 hrs · 16,212 cycles
FLT#1755, BOS-DCA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' AFTER TAKEOFF AND CLIMBING THROUGH 800', BLEED 1 OVERPRESS CAUTION. QRH COMPLETE. PSI OVER 120 UNTIL THRUST LEVER IDLE. AT IDLE PSI 20. RETURNED FOR NORMAL LANDING, BLEED 1 FAIL CAUTION. CABIN PRESSURE IS NORMAL. (ENGINE BLEED VLVS- SINGLE- SECURED CLSD)' (SUPPLEMENTAL TO FOLLOW)
Part: FAN — FAILED (RECIRC-FAN-LH) · airframe 22,681 hrs · 15,866 cycles
FLT#1250, SAV-BOS. ' STRONG ODOR IN FLIGHT DECK; PERFORMED INSPECTION IN CABIN/COCKPIT PER FIM 21-20-00. FOUND A BAD RECIRCULATION FAN. REMOVED AND REPLACED RECIRC. FAN PER AMM 21-24-01. OPS CHECK SATISFACTORY. A/C OK FOR SERVICE.'
Part: BATTERY — FAILED (EMER-BATT-CTR-RH) · airframe 22,022 hrs · 15,379 cycles
FLT # 818, JFK-BOS. REMOVED EMERGENCY LIGHT POWER UNIT BATTERY 3 (ELPU3) AT FRAME 45-46 TO BE USED ON A/C N274JB. PULLED AND COLLARED CB'S EMR FWD BATT HTR LHCBP (DC BUS1 LIGHTS), EMER LT BAT HRT- LICC (DC BUS1), AND EMER AFT BAT HTR- RICC (DC BUS2) PER THE AMM BATTERY REMOVAL PROCEDURE; R&R ELP#3 PER AMM 33-50-01/400
2021
Part: ANTI-ICE VALVE — FAILED · airframe 21,451 hrs · 14,990 cycles
FLT #2291, JFK-ACK(DIVERTED TO BOS). A-I ENG (2) FAIL MULTIPLE TIMES W/ ICING CONDITION. FIRST TIME, RESET SECOND DIDN'T HAD TO EXIT ICING PER THE QRH ( ENGINE ANTI-ICE VALVES -- SECURED OPEN ) ; PLACED ENG 2 ANTI-ICE ON MEL 30-21-01B CAT C MDDR 452092 MCC NOTIFIED. MX-4 UPDATED PLACARD INSTALLED + SECURED (RH) ENGINE ANTI-ICE VALVE OPEN IAW AMM TASK 30-21-01-040-801A. DISP. NOTIFIED (SUPPLEMENTAL INFORMATION TO FOLLOW)
2019
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 18,996 hrs · 13,293 cycles
DURING HEAVY MAINTENANCE, FAULT FWD SERVICE DOOR ELPU ON FWD AND CENTER RH POSITION; REF AEROMAN NR WO 2019-243/1 WCC 2019-366998 REMOVED AND REPLACED ELPU AT THE FWD SERVICE DOOR AND CENTER RH POSITION IAW E190 AMM 33-50-01-400-801-A AND PERFORMED OPERATIONAL TEST E190-AMM 33-50-00-710-801-A AND IAW AMM E190 33-50-01-710-801-A/500. TEST IS O.K.
Part: POWER UNIT — FAILED (CABIN) · airframe 17,695 hrs · 12,280 cycles
FLT 535, SWF-FLL. LT AFT BOTTOM EXTERNAL EMERGENCY LIGHT INOP; R & R EMERGENCY LIGHT POWER UNIT 6, AS PER MM 33-50-01. ALL OPS/IND. NORMAL FOR LT AFT EXT. EMERGENCY LT PER MM 33-50-01-710-801-A/500.
2017
Part: LIFE RAFT — DAMAGED (FWD) · airframe 13,364 hrs · 9,163 cycles
FT # 854, DCA-BOS. FOUND FWD LIFE RAFT LACING UNRAVELED; R & R FWD LIFE RAFT REF 25-66-00.
Part: SEAT TRACK — CORRODED (FRAME 13) · corrosion level 2 · airframe 11,981 hrs · 8,134 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT SEAT TRACK AT FRAME 13 AROUND ANCHOR NUT UNDER FWD GALLEY AREA. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A REPAIR IAW ETD2017-190-044057, AND EC E17-459-01.
Part: SEAT TRACK — CORRODED (FRAME 13) · corrosion level 2 · airframe 11,981 hrs · 8,134 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT SEAT TRACK, FRAME 13+6 AROUND ANCHOR NUT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A REPAIR IAW ETD 2017 190-044057 AND EC E17-459-01.
Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 11,981 hrs · 8,134 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL AROUND AFT DOOR LATCH FITTING. REMOVED CORROSION IAW SRM 51-10-03. REMOVED & REPLACED THE LOWER SILL BEAM IAW SRM 51-43-03-04.
2014
Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 4,799 hrs · 3,235 cycles
CREW DECLARED AN EMERGENCY DUE TO BRAKE RT AND LT FAULT. IAW FIM 32-41-00. R & R MAIN BRAKE CONTROL MODULE MAU1 SLOT 5 IAW AMM 32-41-07. OPS CHECKED GOOD. THE DEFECT REPEATED AGAIN ON FLIGHT 1094. THE MAIN SHUTOFF VALVE WAS R & R IAW AMM 32-41-03-400-801-A. OPS CHECKED GOOD.
Part: CONTROL MODULE — FAULTY (BRAKE SYS) · airframe 4,792 hrs · 3,233 cycles
CREW REPORTED EICAS WARNING FOR LT AND RT BRAKE FAULT IAW FIM 32-41-00. R & R BRAKE CONTROL MODULE MAU 1 SLOT 5 IAW AMM 32-41-07. OPS CHECK GOOD.