# N178JB: 2005 Embraer ERJ 190-100 IGW, registration cancelled 2024-09-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 21, 2024
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw) (registry code 3260408)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A57NM](https://openairdocs.org/tcds/A57NM) (OpenAirDocs)
- Serial number: 19000004
- Year built: 2005
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 2005
- Certificate issued: April 28, 2023
- Last registry action: September 25, 2023
- Mode S code: A137AF
- Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N178JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=178JB
- Page: https://openairdocs.org/deregistered/N178JB-2024-09-21

From the FAA registry file of November 7, 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 (42)

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

- [SDR YENA2022021600062](https://openairdocs.org/sdr/YENA2022021600062), Feb 13, 2022: NONE. NONE. FLT 1052, RSW-HPN. ENG 1 SPOOLED DOWN TO UNDER 50% N1 DURING CRZ FLT. LP VIBE 1.4, NO OTHER INDICATIONS. ENG 1 SPOOLED BACK UP AFTER 5 SECONDS TL'S DID NOT MOVE
- [SDR YENA2020020430142](https://openairdocs.org/sdr/YENA2020020430142), Jan 31, 2020: LINE. BLOCKED. FT # 427, BOS-BWI. RETURNED TO FIELD. FUEL 2 LOW LVL; SUSPECTING THE MOTIVE FLOW RETURN LINE FROM EDP BACK TO BE BLOCKED AND PREVENTING COLLECTOR TANK FROM FILL
- [SDR YENA201911183649](https://openairdocs.org/sdr/YENA201911183649), Nov 13, 2019: WEB. CRACKED. DURING HEAVY MAINTENANCE, CRACK BELLY FAIRING WEB AT LEVEL FR 52 LH SIDE MLG COMPARTMENT ON LOWER FUSELAGE; REF AEROMAN NR WO 2019-238/1 WCC 2019-332147 ACCOMPL
- [SDR YENA201907090398](https://openairdocs.org/sdr/YENA201907090398), Jul 9, 2019: POWER UNIT. FAILED. FLT 1589, BOS-DCA. L2 DOOR EMERGENCY LIGHTS, ROW 24-25 CENTER ISLE EMERGENCY LIGHT AND AFT GALLEY CEILING EMERGENCY LIGHT INOP; REMOVED AND REPLACED #5 EMERGENC
- [SDR YENA201906280379](https://openairdocs.org/sdr/YENA201906280379), Jun 28, 2019: POWER UNIT. FAILED. FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8
- [SDR YENA201906280378](https://openairdocs.org/sdr/YENA201906280378), Jun 28, 2019: POWER UNIT. FAILED. FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8
- [SDR YENA201906280377](https://openairdocs.org/sdr/YENA201906280377), Jun 28, 2019: POWER UNIT. FAILED. FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8
- [SDR YENA201906280376](https://openairdocs.org/sdr/YENA201906280376), Jun 28, 2019: POWER UNIT. FAILED. FLT 1479, DCA-FLL. WHILE PERFORMING TASK CARD E-190-33-50-01-720-801 FWD, MID & AFT FROM WO 1001155. EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST FAILED ON STEP 8
- [SDR YENA201806076235](https://openairdocs.org/sdr/YENA201806076235), Jun 6, 2018: BATTERY PACK. FAILED. LEFT MIDDLE EMERGENCY LIGHT ON THE WTB FAIRING WAS INOPERATIVE. R & R THE EMERGENCY LIGHT BATTERY PACK. PERFORMED AN OPS CHECK, ALL CHECKED GOOD IAW AMM 33-50-8
- [SDR YENA201708110658](https://openairdocs.org/sdr/YENA201708110658), Aug 11, 2017: DOUBLER. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INTERNAL FUSELAGE ON WASTE PAN INNER DOUBLERS BETWEEN FRAMES 88-89, STRINGERS 27-28R. R & R DOUBLER IAW SR
- [SDR YENA201708110657](https://openairdocs.org/sdr/YENA201708110657), Aug 11, 2017: DOUBLER. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INTERNAL FUSELAGE ON WASTE PAN INNER DOUBLERS BETWEEN FRAMES 88-89, STRINGERS 27-28R. R & R DOUBLER IAW SR
- [SDR YENA201705280425](https://openairdocs.org/sdr/YENA201705280425), May 28, 2017: WARNING MESSAGE. FALSE ACTIVATION. BRAKE RT FAULT, AND BRAKE LT FAULT ON EICAS AFTER GEAR CAME DOWN. MESSAGES REMAINED AFTER GO AROUND. IAW FIM 32-41-00-810-824-A, PERFORMED PULSE PRESSURE BIT TE
- [SDR YENA201705270422](https://openairdocs.org/sdr/YENA201705270422), May 27, 2017: CABLE. UNKNOWN. R2 DOOR ARMING LEVER VERY DIFFICULT TO MOVE. R & R THE R2 DOOR EMERGENCY EVACUATION SLIDE MECHANISM CONTROL CABLE IAW AMM 52-42-40. OPS CHECKED GOOD. THE ACFT O
- [SDR YENA20161005906](https://openairdocs.org/sdr/YENA20161005906), Oct 5, 2016: BATTERY PACK. FAILED. THE FWD LEFT OVERHEAD ENTRY DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED & REPLACED FWD THE LT ENTRY EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.
- [SDR YENA20151201612](https://openairdocs.org/sdr/YENA20151201612), Dec 1, 2015: PCU. LEAKING. AIR TURNBACK TO DEPARTURE. AFTER TAKEOFF, LOST ALL HYD 1 QUANTITY AND HYD 1 SYSTEM. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. R & R RT NR 4 SPOILER PCU DUE T
- [SDR YENA20150716280](https://openairdocs.org/sdr/YENA20150716280), Jul 16, 2015: SHEAR TIE. CORRODED. DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE CORRODED AT FRAME 87 BETWEEN STRINGERS 27-28R. REMOVED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01 AND 51-41-0
- [SDR YENA20150716279](https://openairdocs.org/sdr/YENA20150716279), Jul 16, 2015: FLOORBEAM. CORRODED. DURING HEAVY MAINATENANCE, FOUND FWD CABIN FLOORBEAM FRAME 17 CORRODED. CUT-OUT DAMAGE, PERFORMED A DYE-PENETRANT INSPECTION, NO DEFECTS FOUND., FABRICATED A RE
- [SDR YENA20150716278](https://openairdocs.org/sdr/YENA20150716278), Jul 16, 2015: BEAM. CORRODED. DURING HEAVY MAINATENANCE, FOUND FWD CARGO DOOR LOWER BEAM CORRODED AT THE AFT SEAL REST CORNER. R & R THE BEAM, IAW SRM 51-41-01, 51-41-02, 51-43-03, 51=43-04.
- [SDR YENA20150716277](https://openairdocs.org/sdr/YENA20150716277), Jul 16, 2015: STRINGER. CORRODED. DURING HEAVY MAINATENANCE, FOUND CORROSION ON STRINGER 29R, 1.5" FWD OF FRAME 77. REMOVED CORROSION FROM THE STR, AND PERFORMED AN HFEC INSPECTION, NO DEFECTS N
- [SDR YENA20150716276](https://openairdocs.org/sdr/YENA20150716276), Jul 16, 2015: SHEAR TIE. CORRODED. DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE AT FRAME 17 AND STRINGERS 27- 28R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND 51-43-03.
- [SDR YENA20150716275](https://openairdocs.org/sdr/YENA20150716275), Jul 16, 2015: SHEAR TIE. CORRODED. DURING HEAVY MAINATENANCE, FOUND SHEAR TIE CORRODED AT FRAME 86 AND STRINGERS 27- 28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, 51-41-02, AND SRM 51
- [SDR YENA20150716274](https://openairdocs.org/sdr/YENA20150716274), Jul 16, 2015: SHEAR TIE. CORRODED. DURING HEAVY MAINATENANCE, FOUND THE SHEAR TIE AT FRAME 18 AND STRINGERS 27 -28R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-41-01 AND
- [SDR YENA20141209273](https://openairdocs.org/sdr/YENA20141209273), Dec 9, 2014: SHUTOFF VALVE. FAILED. ACFT DIVERTED DUE TO BLEED 2 FAILED INFLIGHT WITH BLEED 1 ON MEL. R & R NR 2 ENG NAPRSOV VALVE IAW AMM 36-11-03. FAILURE SUSPECTED OVERLOAD ON SINGLE BLEED OPER
- [SDR YENA20130419079](https://openairdocs.org/sdr/YENA20130419079), Apr 19, 2013: WARNING SYSTEM. FALSE ACTIVATION. FLT 611 JFK-JAX, ON APPROACH WHEN LANDING GEAR CAME DOWN A NOSE STEER FAIL EICAS MESSAGE APPEARED. A GO AROUND WAS DONE AND MESSAGE WENT AWAY WHEN GEAR WAS LIFT
- [SDR YENA20130314060](https://openairdocs.org/sdr/YENA20130314060), Mar 14, 2013: BATTERY PACK. DISCHARGED. FLT 1230 RDU-BOS, CREW REPORTED COCKPIT EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-01. CHECK OK.
- [SDR YENA20120520504](https://openairdocs.org/sdr/YENA20120520504), May 20, 2012: PUMP. DAMAGED. FLT 1208 RSW-HPN, AIRCRAFT DIVERTED TO MCO DUE TO HYD 2 EDP FAIL ON EICAS. REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOO
- [SDR YENA20120512496](https://openairdocs.org/sdr/YENA20120512496), May 12, 2012: STEERING SYS. MALFUNCTIONED. FLT 450 SJU-SXM, CREW DECLARED EMERGENCY DUE TO STEER FAIL ON APPROACH. RAN QRH AND LANDED WITHOUT STEERING. RESET SYSTEM IAW FIM 32-53-00-810-806A. NO FURTHER 
- [SDR YENA20111025372](https://openairdocs.org/sdr/YENA20111025372), Oct 25, 2011: UNKNOWN. MALFUNCTIONED. FLT 1245 BOS-CLT, CREW EXECUTED A GO AROUND DUE TO ON GEAR EXTENSION RECEIVED A STEER FAULT. AIRCRAFT LANDED AND CLEARED RUNWAY THEN PERFORMED QRH RESET AND REC
- [SDR YENA20110610268](https://openairdocs.org/sdr/YENA20110610268), Jun 10, 2011: WARNING SYSTEM. FALSE ACTIVATION. FLT 1008 JFK-BOS, CREW DECLARED EMERGENCY DURING APPROACH AT APPROX 3,000 FEET DUE TO SLAT FAIL EICAS MSG. QRH PROCEDURE WAS ACCOMPLISHED. TECHNICIAN C/W TASK 2
- [SDR YENA20110309211](https://openairdocs.org/sdr/YENA20110309211), Mar 9, 2011: PIN. BURNED. FLT 440 MCO-BOS, CREW DECLARED EMERGENCY AND DIVERTED TO RDU DUE TO IFE SMOKE INDICATION ON EICAS. PERFORMED INSPECTION OF AFT CARGO COMPT AND DE-ACTIVATED IFE 
- [SDR YENA20100725102](https://openairdocs.org/sdr/YENA20100725102), Jul 25, 2010: FILTER. FAILED. FLT 107 BUF-JFK, VERY STRONG ODOR AT FRONT CABIN ON T/O AND DESCENT. REMOVED AND REPLACED NR 2 ENGINE OZONE FILTER IAW AMM 36-30-00. RAN ENGINE, NO FURTHER FAUL
- [SDR YENA20100509068](https://openairdocs.org/sdr/YENA20100509068), May 9, 2010: CONTROL MODULE. FAILED. FLT 1305 JFK-IAD DECLARED EMERGENCY DUE TO SPOILER FAULT AT 4000FT ON DOWNWIND INTO IAD. LANDED LONG, NO GROUND SPOILERS ON GRD LEFT DUMP ON ROLL OUT DEGRADED/S
- [SDR YENA20100422064](https://openairdocs.org/sdr/YENA20100422064), Apr 22, 2010: BLEED AIR SYS. CONTAMINATED. FLT 408 FLL-FLL FUMES IN THE COCKPIT IN FLIGHT, TURN PACKS OFF FUMES CLEARED (NOT ELECTRICAL SMELL). SUSPECT DUE TO NR 1 ENGINE COMPRESSOR BOROSCOPE INSPECTION 
- [SDR YENA20100305027](https://openairdocs.org/sdr/YENA20100305027), Mar 5, 2010: DRIVE UNIT. FAULTY. FLT JB1761-- AIR TURN BACK AFTER TAKEOFF, LOUD CLUNKING NOISE UNDER FLOOR OF COCKPIT ASSOCIATED "THUD" NOISE FELT IN FLOORBOARD, NOT CONTINUOUS BUT EVERY FEW SE
- [SDR YENA20100117008](https://openairdocs.org/sdr/YENA20100117008), Jan 17, 2010: TRANSCEIVER. FAILED. FLT JB1207 HPN-RSW CREW DIVERTED TO JFK DUE TO UNCOMMANDED LANDING GEAR ORAL WARNING AT 7000/9000/13000/17000 FT, COULD NOT CANCEL WARNING IT WOULD CONTINUE FOR
- [SDR YENA200812230131](https://openairdocs.org/sdr/YENA200812230131), Dec 19, 2008: PUMP. LEAKING. FLT NR 1433, LGB-SFO, LOST HYD NR 2 EDP IN FLIGHT ALONG WITH LOSS OF ALL HYD QTY IN FLIGHT. DUE TO LOSS OF HYD NR 2 QTY, GEAR WAS MANUALLY LOWERED, GEAR REF QRH
- [SDR YENA2007109](https://openairdocs.org/sdr/YENA2007109), Nov 26, 2007: ACM. CONTAMINATED. FLT 1047, JFK-BNA, AT APRX 21:40 PM RETURNED TO JFK, SMOKE/FUMES/HAZE IN CABIN & COCKPIT PASSING 8K FEET, GOT WORSE AS CLIMB CONTINUED. LANDED ASAP. FUMES SEEME
- [SDR YENA2007101](https://openairdocs.org/sdr/YENA2007101), Nov 16, 2007: UNKNOWN. ODOR. FLT 1016, JFK-, EXPERIENCED DUSTY/HAZY/BURNING ODOR IN CABIN ON TAKEOFF ROLL. ENTIRE CABIN HAZY, WARM RUSH OF AIR ON FLT DECK, LIGHTS ON FLT ATTENDANT WERE INOP
- [SDR YENA2007043](https://openairdocs.org/sdr/YENA2007043), Jun 1, 2007: CONTROL VALVE. FALSE INDICATION. BRAKE RT & LT FAULT EICAS MESSAGES AT GEAR EXTENSION, TEMPS INDICATE O/B BRAKES FAILED. T/S PER FIM 32-41-00-810-848-A. REMOVED AND REPLACED MAIN BRAKE CONTROL 
- [SDR YENA2007003](https://openairdocs.org/sdr/YENA2007003), Jan 13, 2007: WIRE HARNESS. INTERMITTENT. SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (LT HARNESS INTERMITTENT). REMOVED AND REPLACED LT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-81
- [SDR YENA2007002](https://openairdocs.org/sdr/YENA2007002), Jan 13, 2007: WIRE HARNESS. INTERMITTENT. SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (RT HARNESS INTERMITTENT). REMOVED AND REPLACED RT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-81
- [SDR YENA200687](https://openairdocs.org/sdr/YENA200687), Nov 23, 2006: CLEVIS. BROKEN. ON POWER APPLICATION FOR TAKEOFF NR 2 ENG WOULD NOT ADVANCE PAST 58.7 PERCENT. NR 1 ENG ADVANCE NORMALLY. NO EICAS MSGS ASSOCIATED WITH POWER APPLICATION WHEN A

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