N355JB
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.
25 reports on file, 2013-05-03 – 2023-12-11.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 25,672 hrs · 17,988 cycles
FLT#381, BOS-ORH. 'SEVER TURBULENCE ENCOUNTER AT 3000 FEET 10 MILES WEST OF KRIC WHILE IN IMC ALTITUDE DEVIATIONS +500/-200 FEET AIRSPEED DEVIATION +60/- KTS SPEED AT TIME OF ENCOUNTER 230 KTS. ENCOUNTER LASTED APPROXIMATELY 30 SECONDS UNABLE TO READ INSTRUMENTS NO INJURIES; DVDR FOR SEVERE TURBULENCE WAS WITHIN LIMITS. NO FURTHER ACTION REQUIRED. REF AMM 05-50-28. MDDR CLEAR. MX-4 UPDATED PLACARD REMOVED.'
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,865 hrs · 17,324 cycles
FLT#582, RSW-DCA. 'RH CTR EMERGENCY LIGHT INOP; REMOVED AND REPLACED RH FWD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. PROBLEM NO FIX. FOUND EMERGENCY LIGHT ASSY. THE CONNECTOR NOT SECURED. SECURED CONNECTOR IAW AMM 33-50-25. OPS CHECK GOOD. NO DEFECTS NOTED.'
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 23,569 hrs · 16,342 cycles
FLT#1287, PVD-PBI. 'DESCENDING THRU 14,000 STRONG EXHAUST FUME SMELL BEGAN INFLIGHT COULDN'T SMELL IT. AN ODOR ISOLATION PROCEDURE FOR PACK 1 WAS PERFORMED AND THE SMELL WENT AWAY. WE TURNED THE PACK BACK ON A FEW MINUTES LATER AND IT CAME BACK. WE TURNED OFF PACK 1 FOR THE REST OF FLIGHT; ACCOMPLISHED FIM TASK 21-20-00-810 TRANSITORY CONDITION FOUND COULD NOT DUPLICATE ON GROUND. SYSTEM OPS CHECK NORMAL.'
Earlier reports · 2013–2022 · 22 reports
2022
Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON CUT-OUT STRUCTURE AT WASTE SERVICE PANELL; CUTOUT STRUCTURE AT WASTE SERVICE PANEL WAS REPAIRED PER EMB/190 SRM 53-23-60/REPAIR51. ALL WORK ACCOMPLISHED ON TOMX N/R# 00013.'
Part: HINGE FITTING — CRACKED · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: REF TC NDT-55-40-00-211-801 CRACK AND MIGRATED BUSHINGS IN HINGE FITTING # 3 LOCATED IN FWD FRONT SPAR OF RUDDER; REF TOMX WO 1989 NR -00145 RUDDER WAS REPLACED PER AIPC 27-21-05 ITEM 10, AMM 51-60-02-820-801-A AND AMM 27-21-05-000-801-A, 27-21-05-400-801-A.
Part: FLOOR SUPPORT — CORRODED · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION "CPCP FINDING": CORROSION IN LATERAL FLOOR SUPPORT LOCATED FROM Y= -1100 TO Y= -1270.0 AND FROM FR12 TO FR 16 IN PASSENGER CABIN FLOOR STRUCTURE W1; LATERAL FLOOR SUPPORT LOCATED FROM Y=-1100.0 TO Y=-1270 AND FR 12-16 PAX CABIN FLOOR STRUCTURE W1 WAS REPLACED PER EMB 190 SRM 51-41-02;51-43-04'
Part: NONE — NONE · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER & RH LATERAL SKIN PANEL BETWEEN FR 1-3 & STRG 18-22R / DENTS - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR.)
Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION "CPCP FINDING". CORROSION IN FLOOR SUPPORT LOCATED IN Y= -420.0 AND FR 12/13 IN PASSENGER CABIN FLOOR STRUCTURE W1; FLOOR SUPPORT LOCATED IN Y= -420.0 AND BETWEEN FR 12/13 IN PASSENGER CABIN FLOOR STRUCTURE W1 WAS REPLACED PER EMB 190 SRM 51-40-08. ALL WORK ACCOMPLISHED ON TOMX N/R# 00129, TECHOPSMX TECH # 201635937, TECHOPSMX RII INSPECTOR # 200002656.'
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION "CPCP FINDING": CORROSION FROM MODERATE TO SEVERE ON LONGITUDINAL FLOORBEAM LOCATED IN Y= -280.0 AND FROM FR 12 TO FR 16 IN PASSENGER CABIN FLOOR STRUCTURE W1; FLOOR BEAM LOCATED IN Y= - 280.0 AND FROM FR 12 TO FR 16 IN PASSENGER CABIN FLOOR STRUCTURE W1 WAS REPAIRED PER ETI-190-22-667 REV.1, EC: E22-801-01 AND ETD2022-190-029311. ALL WORK ACCOMPLISHED IN TOMX N/R# 00130. FLOOR B AND ETD 2022-190-029311EAM LOCATED IN Y=-280.0 AND FROM FR 12-16 IN PASSENGER CABIN FLOOR STRUCTURE W1 WERE REPAIRED PER ETI-190-22-667 REV. 1; EC E22-801-01.
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: IN REF. NRC 00131(CPCP FINDING) CORROSION IN PREVIOUS DOUBLER REPAIR LONGITUDINAL FLOORBEAM LOCATED IN Y=330.0 FROM FR 13-14 IN PAX FLOOR STRUCTURE W1; DOUBLER IN LONGITUDINAL FLOORBEAM LOCATED IN Y=330.0 FROM FR13-14 IN PAX FLOOR STRUCTURE W1 WAS REPLACED PER EMB-190 SRM 53-10-10/ REPAIR 51 AND ETD 2017-190-04-1003 REV. A. (CONSIDERED AS A MAJOR REPAIR.)
Part: BRACKET — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION"CPCP FINDING" CORROSION IN BRACKET FLOOR SUPPORT LOCATED IN Y=-1140.0 AND FR 16 IN PAX CABIN FLOOR STRUCTURE W1; BRACKET FLOOR SUPPORT LOCATED IN Y=-1140.0 AND FR 16 IN PAX CABIN FLOOR STRUCTURE W1 WAS REPLACED PER EMB-190 SRM 51-43-01. REF. TOMEX NR 00126 FOR DETAILS. (CONSIDERED AS A MAJOR REPAIR.)
Part: RIB — CRACKED · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: CRACK ON LOWER SKIN PANEL RIB 10 LH WING; REF TOMX WO 1989- NR 00163; ACCOMPLISHED REPAIR OF SKIN PANEL RIB 10 LH WING E190-SRM 57-10-01 / REPAIR 54.
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION "CPCP FINDING": CORROSION FROM MODERATE TO SEVERE IN LONGITUDINAL FLOORBEAM LOCATED IN Y= -280.0 AND FROM FR 12 TO FR 16 IN PASSENGER CABIN FLOOR STRUCTURE W1; FLOORBEAM LOCATED IN Y= - 280.0 AND FROM FR 12 TO FR 16 IN PASSENGER CABIN FLOOR STRUCTURE W1 WAS REPAIRED PER ETI-190-22-667 REV.1, EC: E22-801-01 AND ETD2022-190-029311. ALL WORK ACCOMPLISHED IN TOMX N/R# 00130. FLOOR B AND ETD 2022-190-029311EAM LOCATED IN Y=-280.0 AND FROM FR 12-16 IN PASSENGER CABIN FLOOR STRUCTURE W1 WERE REPAIRED PER ETI-190-22-667 REV. 1; EC E22-801-01.
Part: SPAR — CRACKED · airframe 22,910 hrs · 15,919 cycles
DURING HEAVY MAINTENANCE: REF TC 190-54-0014-02' CRACK AT INBOARD SPAR OF RH PYLON; REF TOMX WO 1989- NR 00241, REMOVED AND REPLACED INBOARD SPAR AT RH PYLON IAW SRM 51-41-02 PAR 4, PAR 6, SRM 51-43-03 PAR 4/5 AND SRM 51-43-04 PAR 4-5.
Part: TRANSMITTER — FAILED (720001-01-001-LH) · airframe 21,558 hrs · 14,975 cycles
FLT # 1704, CTG-FLL(DIVERTED TO MBJ). IN FLT # 1 OIL PRESSURE INDICATION AMBER AT PSI SLOWLY BLEED DOWN TO 0 IN LESS THAN FEW MINUTES. ENGINE VIBRATION MEER 1.3=1.4 STEADY UNITL SHUTDOWN, FOLLOWED QRH PROCEDURE 6-25 FOR ENG OIL PRESSURE ABNORMAL INDICATION AN SHUTDOWN OF ENGINE; R/R ENG # 1 OIL PRESS. TRANSMITTER IAW EMM 77-00-00-050-806. LEAK CK AND OPS CK GOOD
2020
Part: MAU — FAILED (NR 2)
EMERGENCY DECLARED. AVNX MAU FAIL IN FLT; A/C ARRIVED AT GATE WITH NO ACTIVE FAULTS. REF FIM 45-45-00-810-941-A PERFORMED MAU 2 NIC 3 MODULE RESET TEST, TEST PASSED. CONSIDERED TRANSITORY CONDITION, A/C OK FOR SVC. NO HISTORY IN AHEAD OF ITEM. SUPPLEMENTAL INFORMATION TO FOLLOW.
2018
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 14,310 hrs · 9,718 cycles
CENTER CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-50-01. OPS CHECKED GOOD.
2017
Part: DISPLAY — FAILED (NR 2) · airframe 12,020 hrs · 8,042 cycles
ACFT POWERED BY STATION, PFD OVERHEAT, MFD FAIL EICAS MESSAGE. BURNING PLASTIC ODOR IN COCKPIT & GALLEY NOTICED BY CREW. R & R THE NR 5 DISPLAY IAW AMM 31-61-01, OPS OK.
Part: DISPLAY — FAILED (COCKPIT) · airframe 12,020 hrs · 8,042 cycles
A/C POWERED BY STATION, PFD OVERHEAT, MFD FAIL EICAS MESSAGE. BURNING PLASTIC ODOR IN COCKPIT AND GALLEY NOTICED BY CREW. R & R THE NR 5 DISPLAY IAW AMM 31-61-01, OPS OK.
Part: FLOOR SUPPORT — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 11,967 hrs · 8,008 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT BETWEEN FRAMES 13 AND 14. BLENDED THE FLOOR SUPPORT IAW SRM 51-10-03, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-10. FABRICATED A REPAIR AND FILLER. REMOVED DAMAGE AREA IAW SRM 53-10-10, AND ETD 2017-190-041003. APPLIED PROTECTIVE TREATMENT IAW SRM 53-10-10. INSTALLED THE REPAIR IAW SRM 53-10-10, AND ETD 2017-190-041003. OPEN
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,967 hrs · 8,008 cycles
DURING HEAVY MAINTENANCE, THE L2 DOOR LOWER EMERGENCY EXIT SIGN DID NOT ILLUMINATE. R & R THE BATTERY IAW AMM 33-50-01, OPS CHECKED GOOD IAW AMM 33-50-00.
Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 11,967 hrs · 8,008 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE LT FLOORBEAM AT FRAME 87 +5, LBL 10 ON THE UPPER SURFACE. REMOVED CORROSION, FOUND TO OUT OF LIMITS. INSTALLED DOUBLER REPAIR, TREATED, PRIMED, AND TOPCOATED IAW 51-10-03, 53-23-10, 51-23-04, 51-23-05, 51-23-06, 51-41-02, 51-40-04 & NDTM PART 1 51-00-00-916-803-A.
2016
Part: COMPUTER — FAILED · airframe 8,372 hrs · 5,538 cycles
STEER OFF EICAS DISPLAYED UPON LANDING. UNABLE TO ENGAGE OR RESET; PERFORMED FIM TASK 45-45-00-810-941-A AND FOUND NIC/PROC, MOD 3, MAU 2, NIC1, AT FAULT. R & R NIC 1 IAW AMM 31-41-04. TARGET LOAD ACCEPTED. NAV DATABASE UPDATED. ACFT TAXIED WITH NO STEERING FAULT AND NO EICAS RELATED MSG NOTED. ACFT OK FOR CONTINUED SERVICE.
2014
Part: MAU — FAILED (NR 1) · airframe 4,150 hrs · 2,744 cycles
FLIGHT DIVERTED, PILOT REPORTED DURING FLIGHT, AUTOPILOT DISENGAGED 3 DIFFERENT TIMES WITH VIBRATION FELT IN LATERAL AXIS WHILE HAND FLYING. VIBRATION ONLY FELT WHILE TURNING ACFT. ACCOMPLISHED VISUAL INSPECTION OF ACFT IAW AMM 05-50-27-210-007A IAW ENGINEERING REQUEST. NO DEFECT NOTED. FOUND AILERONS OUT OF RIG. PERFORMED LT AND RT AILERON SURFACE POSITION SENSOR RIG IAW AMM 27-13-02, RIG COMPLETED AND OPS NORMAL. ACCOMPLISHED AUTOPILOT OPS TEST IAW AMM 22-11-00. NO FAULTS NOTED. R & R AIOP MODULE 1 IAW AMM 31-41-10, OPS NORMAL.
2013
Part: FCU — FAILED (FUEL SYSTEM) · airframe 62 hrs · 50 cycles
FLT 1903, BOS-MSY. AIRCRAFT DIVERTED TO JFK DUE TO LOSS OF FUEL QTY INDICATIONS AFTER LEVEL OFF AT FL360 . REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW AMM TASK 28-41-03. FCU SELF TEST ACCOMPLISHED IAW AMM TASK 28-41-00-710-801-A/500. SYSTEM OPS NORMAL, INDICATIONS OK. A/C OK TO CONTINUE SERVICE.