# N216JB: 2006 Embraer ERJ 190-100 IGW, registration cancelled 2025-02-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 25, 2025
- Exported to: Lithuania
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw) (registry code 3260408)
- Engine: [GE CF34-10E6](https://openairdocs.org/engine/ge-cf34-10e6) (registry code 30023)
- Data sheets: [TCDS A57NM](https://openairdocs.org/tcds/A57NM), [TCDS E00070EN](https://openairdocs.org/tcds/E00070EN) (OpenAirDocs)
- Serial number: 19000026
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 27, 2006
- Certificate issued: September 3, 2024
- Last registry action: September 3, 2024
- Mode S code: A1D096
- Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N216JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=216JB
- Page: https://openairdocs.org/deregistered/N216JB-2025-02-25

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer ERJ 190-100 IGW: https://openairdocs.org/model/embraer-erj-190-100-igw.md

## Service difficulty reports (62, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR YENA2024012900155](https://openairdocs.org/sdr/YENA2024012900155), Jan 26, 2024: STRINGER. CRACKED. DURING HEAVY MAINTENANCE: DURING ATTENTION T.C.53-23-006-0418 FOUND A CRACK IN STRG 10L UNDER FR 74 AT INTERNAL STRUCTURE OF CF III; (RESOLVED ON W/O: 1299067 T
- [SDR YENA2024012900154](https://openairdocs.org/sdr/YENA2024012900154), Jan 26, 2024: FLOOR SUPPORT. CORRODED. DURING HEAVY MAINTENANCE: [CPCP FINDING]: CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED BETWEEN FR 86/90 AND Y= 300.0 MM IN CTR FUS III PASSENGER CABIN FLOOR STR
- [SDR YENA2024012900153](https://openairdocs.org/sdr/YENA2024012900153), Jan 26, 2024: FLOOR SUPPORT. CORRODED. DURING HEAVY MAINTENANCE: CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED BETWEEN FR 13/17 AND Y= 300.0 MM IN FWD FUSELAGE PASSENGER CABIN FLOOR STRUCTURE; REF TOM
- [SDR YENA2024012900152](https://openairdocs.org/sdr/YENA2024012900152), Jan 26, 2024: FLOOR SUPPORT. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED AT Y = - 300.0 MM IN FR 17 AND FR 19, FWD FUSELAGE PAS
- [SDR YENA2023033100302](https://openairdocs.org/sdr/YENA2023033100302), Mar 30, 2023: UNKNOWN. UNKNOWN. 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. INSPECTE
- [SDR YENA2023032700281](https://openairdocs.org/sdr/YENA2023032700281), Mar 26, 2023: UNKNOWN. UNKNOWN. 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 DUPLICA
- [SDR YENA2022112901177](https://openairdocs.org/sdr/YENA2022112901177), Nov 27, 2022: FITTING. CRACKED. 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
- [SDR YENA2022112901176](https://openairdocs.org/sdr/YENA2022112901176), Nov 27, 2022: STRINGER. CORRODED. 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 19
- [SDR YENA2022112901175](https://openairdocs.org/sdr/YENA2022112901175), Nov 27, 2022: DOUBLER. DAMAGED. 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;
- [SDR YENA2022112901174](https://openairdocs.org/sdr/YENA2022112901174), Nov 27, 2022: SHEAR TIE. CORRODED. 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 2
- [SDR YENA2022112901173](https://openairdocs.org/sdr/YENA2022112901173), Nov 27, 2022: SHEAR TIE. CORRODED. 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 CAR
- [SDR YENA2022112901172](https://openairdocs.org/sdr/YENA2022112901172), Nov 27, 2022: FRAME. CORRODED. 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 CA
- [SDR YENA2022112901171](https://openairdocs.org/sdr/YENA2022112901171), Nov 27, 2022: STRINGER. CORRODED. 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 
- [SDR YENA2022112901170](https://openairdocs.org/sdr/YENA2022112901170), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR83 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR83 BETWE
- [SDR YENA2022112901169](https://openairdocs.org/sdr/YENA2022112901169), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR86 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR86 BETWE
- [SDR YENA2022112901168](https://openairdocs.org/sdr/YENA2022112901168), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN 
- [SDR YENA2022112901167](https://openairdocs.org/sdr/YENA2022112901167), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN 
- [SDR YENA2022112901166](https://openairdocs.org/sdr/YENA2022112901166), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR81 BETWEEN STRG 29R / 28R AT AFT CARGO; SUMMARY: SHEARCLIP ON FR81 BETWEE
- [SDR YENA2022112901165](https://openairdocs.org/sdr/YENA2022112901165), Nov 27, 2022: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR82 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY OF NRC 00060: SHEARCLIP O
- [SDR YENA2022112901164](https://openairdocs.org/sdr/YENA2022112901164), Nov 27, 2022: NOT REPORTED. CORRODED. DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR80 & STGR 27R-28R / CORROSION. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022030400115](https://openairdocs.org/sdr/YENA2022030400115), Feb 28, 2022: MAU. FAILED. 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 
- [SDR YENA2020100900472](https://openairdocs.org/sdr/YENA2020100900472), Oct 3, 2020: RIB. CRACKED. 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. RE
- [SDR YENA2020100900471](https://openairdocs.org/sdr/YENA2020100900471), Oct 3, 2020: BATTERY. FAILED. 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/
- [SDR YENA2020100900470](https://openairdocs.org/sdr/YENA2020100900470), Oct 3, 2020: SKIN. CRACKED. 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 A
- [SDR YENA2020100900469](https://openairdocs.org/sdr/YENA2020100900469), Oct 3, 2020: SKIN. DENTED. 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 AE
- [SDR YENA2020090700447](https://openairdocs.org/sdr/YENA2020090700447), Sep 2, 2020: BATTERY. FAILED. FLT 6102, JFK-BUF. WHEN TESTING EMERGENCY LIGHTS RECIEVED LH MIDDLE BATTERY FAULT; R & R LH MIDDLE EMERGENCY BATTERY PER MM 33-50-01.
- [SDR YENA2020021840178](https://openairdocs.org/sdr/YENA2020021840178), Feb 14, 2020: BATTERY. FAILED. 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
- [SDR YENA2019121970706](https://openairdocs.org/sdr/YENA2019121970706), Dec 17, 2019: CHECK VALVE. UNKNOWN. 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, CABI
- [SDR YENA201806280931](https://openairdocs.org/sdr/YENA201806280931), Jun 28, 2018: SKIN PANEL. CRACKED. 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
- [SDR YENA201802040897](https://openairdocs.org/sdr/YENA201802040897), Feb 4, 2018: SKIN. CRACKED. 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
- [SDR YENA201802040064](https://openairdocs.org/sdr/YENA201802040064), Feb 4, 2018: SKIN. CRACKED. 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.
- [SDR YENA201709010727](https://openairdocs.org/sdr/YENA201709010727), Sep 1, 2017: POWER SUPPLY. NO TEST. 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. O
- [SDR YENA201704230295](https://openairdocs.org/sdr/YENA201704230295), Apr 23, 2017: BOTTLE. EMPTY. DURING A WEEKLY CHECK, FOUND FWD PASSENGER DOOR PRESSURE GAUGE AT 0 PSI. INSPECTED FWD PASSENGER DOOR PNEUMATIC ASSEMBLY AND FOUND THE PNEUMATIC ASSEMBLY DIAPHR
- [SDR YENA201612261107](https://openairdocs.org/sdr/YENA201612261107), Dec 26, 2016: BATTERY PACK. FAILED. 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.
- [SDR YENA20160315232](https://openairdocs.org/sdr/YENA20160315232), Mar 15, 2016: POWER SUPPLY. FAILED. DURING PRE-DEPARTURE CHECK LIST FOUND EMERGENCY LIGHT OVER L1 DOOR INOPERATIVE. R & R FORWARD ELPU IAW 33-50-01. OPS CHECK OK.
- [SDR YENA20151018472](https://openairdocs.org/sdr/YENA20151018472), Oct 18, 2015: ACTUATOR. FAILED. 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 
- [SDR YENA20150909414](https://openairdocs.org/sdr/YENA20150909414), Sep 9, 2015: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE FOUND SHEAR TIE AT FRAME 82 BETWEEN STR 27-28R CORRODED. REPLACED THE SHEAR TIE IAW SRM REF 51-10-03.
- [SDR YENA20150909413](https://openairdocs.org/sdr/YENA20150909413), Sep 9, 2015: SEAL REST. CORRODED. 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.
- [SDR YENA20150909412](https://openairdocs.org/sdr/YENA20150909412), Sep 9, 2015: SEAL REST. CORRODED. 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 
- [SDR YENA20150909411](https://openairdocs.org/sdr/YENA20150909411), Sep 9, 2015: SEAL REST. CORRODED. 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 
- [SDR YENA20150909410](https://openairdocs.org/sdr/YENA20150909410), Sep 9, 2015: SEAL REST. CORRODED. 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 C
- [SDR YENA20150909409](https://openairdocs.org/sdr/YENA20150909409), Sep 9, 2015: SHEAR TIE. CORRODED. 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.
- [SDR YENA20150909408](https://openairdocs.org/sdr/YENA20150909408), Sep 9, 2015: SEAL REST. CORRODED. 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 
- [SDR YENA20150506099](https://openairdocs.org/sdr/YENA20150506099), May 6, 2015: SENSOR. FAILED. 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 S
- [SDR YENA20150506098](https://openairdocs.org/sdr/YENA20150506098), May 6, 2015: SENSOR. FAILED. 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 S
- [SDR YENA20140716135](https://openairdocs.org/sdr/YENA20140716135), Jul 16, 2014: I/O CARD. FAILED. 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 CUST
- [SDR YENA20140115011](https://openairdocs.org/sdr/YENA20140115011), Jan 15, 2014: POWER SUPPLY. FAILED. 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 NORM
- [SDR YENA20131228252](https://openairdocs.org/sdr/YENA20131228252), Dec 28, 2013: CIRCUIT CARD. FAILED. 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.
- [SDR YENA20131016215](https://openairdocs.org/sdr/YENA20131016215), Oct 16, 2013: CROSSBEAM. CORRODED. 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. 
- [SDR YENA20130802167](https://openairdocs.org/sdr/YENA20130802167), Aug 2, 2013: PRESSURE SWITCH. FAILED. 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 P

All 62: https://openairdocs.org/deregistered/N216JB-2025-02-25/reports.md

## Other aircraft with N216JB

- [Cancelled 1993-10-20](https://openairdocs.org/deregistered/N216JB-1993-10-20): Beech V35A, S/N D8856. Triennial form not returned. Owner: [Seaton John D](https://openairdocs.org/faa-owner/SEATON%20JOHN%20D), [Vienna, VA](https://openairdocs.org/faa-place/VA/Vienna)

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