# Service difficulty reports: N216JB, cancelled Feb 25, 2025

A list on [N216JB, cancelled Feb 25, 2025](https://openairdocs.org/deregistered/N216JB-2025-02-25.md).

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

Page 1 of 2 · 62 reports

- [SDR YENA2024012900155](https://openairdocs.org/sdr/YENA2024012900155.md): Stringer · cracked · Jan 26, 2024 · N216JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > 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 TASKCARD: NR-00008) REF TOMEX WO 2488, NR 00034, STRG 10L UNDER FR 74 AT INTERNAL STRUCTURE OF CF II
- [SDR YENA2024012900154](https://openairdocs.org/sdr/YENA2024012900154.md): Floor Support · corroded · Jan 26, 2024 · N216JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > 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 STRUCTURE; REF TOMEX WO 2488, NR 00051, CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED BETWEEN FR 86/-90
- [SDR YENA2024012900153](https://openairdocs.org/sdr/YENA2024012900153.md): Floor Support · corroded · Jan 26, 2024 · N216JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > 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 TOMEX WO 2488, CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED BETWEEN FR 13/17 AND Y= 300.0 MM IN FWD FU
- [SDR YENA2024012900152](https://openairdocs.org/sdr/YENA2024012900152.md): Floor Support · corroded · Jan 26, 2024 · N216JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > 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 PASSENGER CABIN FLOOR STRUCTURE; REF TOMX WO# 2488 NR# 00043 CORROSION ON LONGITUDINAL FLOOR BEAM LOCAT
- [SDR YENA2023033100302](https://openairdocs.org/sdr/YENA2023033100302.md): Unknown · unknown · Mar 30, 2023 · N216JB · Emb ERJ190100LR · Air Conditioning System
  > 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. INSPECTED #1 ENG BLEED LINES AT PRSOV FOR EVIDENCE OF OIL. NO OIL WAS FOUND. REPLACED BOTH RECIRCULATION FIL
- [SDR YENA2023032700281](https://openairdocs.org/sdr/YENA2023032700281.md): Unknown · unknown · Mar 26, 2023 · N216JB · Emb ERJ190100LR · Air Conditioning System
  > 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 DUPLICATE. A/C OK FOR SERVICE AS NO ODOR NOTED.'
- [SDR YENA2022112901177](https://openairdocs.org/sdr/YENA2022112901177.md): Fitting · cracked · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Nacelle/Pylon, Main Frame
  > 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 PAR 4&5 AND SRM 51-43-04 PAR.4 AND 5 AND SRM 51-41-02 PAR.4 AND 6 & AMM 20-10-01-910-801-A.'
- [SDR YENA2022112901176](https://openairdocs.org/sdr/YENA2022112901176.md): Stringer · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Main, Longeron/Stringer
  > 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 190 SRM 53-23-03 REP 51 & ETI-190-22-709, EC. 22-939-01.
- [SDR YENA2022112901175](https://openairdocs.org/sdr/YENA2022112901175.md): Doubler · damaged · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Main, Structure
  > 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; REF. TOMX W/O: N216JB / 2075 NR-00136 - CUT OUT STRUCTURE AT WASTE SERVICE PANEL WAS REPAIRED PER E
- [SDR YENA2022112901174](https://openairdocs.org/sdr/YENA2022112901174.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > 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 28R/27R AND FR 88 AT AFT CARGO WAS REPLACED PER EMB SRM 51-41-01 AND SRM 51-41-02.
- [SDR YENA2022112901173](https://openairdocs.org/sdr/YENA2022112901173.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > 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 CARGO; SUMMARY: SHEARCLIP ON FR81 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-
- [SDR YENA2022112901172](https://openairdocs.org/sdr/YENA2022112901172.md): Frame · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Main, Frame
  > 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 CARGO WAS REPAIRED PER EC NO E22-930-01, ETI-190-22-698 REV. 4, ETD2022-- 190-033239 REV.:C.
- [SDR YENA2022112901171](https://openairdocs.org/sdr/YENA2022112901171.md): Stringer · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Main, Longeron/Stringer
  > 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 CARGO WAS REPAIRED PER EMB190 SRM 53-23-03/R51.
- [SDR YENA2022112901170](https://openairdocs.org/sdr/YENA2022112901170.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR83 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR83 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01 PAR. 5 AND 51-41-02 PAR. 6 REF.
- [SDR YENA2022112901169](https://openairdocs.org/sdr/YENA2022112901169.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR86 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY: SHEAR CLIP ON FR86 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01 PAR. 5,EMB 190 SRM 51-41-02 PA
- [SDR YENA2022112901168](https://openairdocs.org/sdr/YENA2022112901168.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16. MAJOR REPAIR
- [SDR YENA2022112901167](https://openairdocs.org/sdr/YENA2022112901167.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR78 BETWEEN STGR 29L / 28L AT AFT CARGO. WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03, AND SRM 51-75-16; SUMMARY OF NRC 00055: CORROSION ON
- [SDR YENA2022112901166](https://openairdocs.org/sdr/YENA2022112901166.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR81 BETWEEN STRG 29R / 28R AT AFT CARGO; SUMMARY: SHEARCLIP ON FR81 BETWEEN STGR 28R / 28R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-41-01 AND SRM 51-41-02 WORK ACCOMPLIS
- [SDR YENA2022112901165](https://openairdocs.org/sdr/YENA2022112901165.md): Shear Tie · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEARCLIP ON FR82 BETWEEN STGR 28R / 27R AT AFT CARGO; SUMMARY OF NRC 00060: SHEARCLIP ON FR82 BETWEEN STGR 28R / 27R AT AFT CARGO WAS REPLACED PER EMB 190 SRM 51-43-01, SRM 51-41-02- AND
- [SDR YENA2022112901164](https://openairdocs.org/sdr/YENA2022112901164.md): Not Reported · corroded · Nov 27, 2022 · N216JB · Emb ERJ190100LR · Fuselage Structure (General)
  > 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.md): Mau · failed · Feb 28, 2022 · N216JB · Emb ERJ190100IGW · Central Display
  > 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 OPS CKS OPS CHECK GOOD REF FIM 31-41-00 AC OK FOR SERVICE
- [SDR YENA2020100900472](https://openairdocs.org/sdr/YENA2020100900472.md): Rib · cracked · Oct 3, 2020 · N216JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > 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. REMOVED AND REPLACED RIB 17 AND FASTENERS LOCATED AT LEADING EDGE ON RT WING, IAW E190 SRM 51-40-08,
- [SDR YENA2020100900471](https://openairdocs.org/sdr/YENA2020100900471.md): Battery · failed · Oct 3, 2020 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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 2020-293/1 WCC 2020-277311. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT 1, IAW E190 AMM 33-50-01/400, A
- [SDR YENA2020100900470](https://openairdocs.org/sdr/YENA2020100900470.md): Skin · cracked · Oct 3, 2020 · N216JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > 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 AEROMAN NNR W/O 2020-293/1 WCC 2020-277033. ACCOMPLISHED REPAIR ON UPPER SKIN PANEL AT LEVEL SLAT T
- [SDR YENA2020100900469](https://openairdocs.org/sdr/YENA2020100900469.md): Skin · dented · Oct 3, 2020 · N216JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > 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 AEROMAN NR W/O 2020-293/1 WCC 2020-277060. ACCOMPLISHED REPAIR ON EXTERNAL SKIN BETWEEN FR 23 TO FR
- [SDR YENA2020090700447](https://openairdocs.org/sdr/YENA2020090700447.md): Battery · failed · Sep 2, 2020 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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.md): Battery · failed · Feb 14, 2020 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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.md): Check Valve · unknown · Dec 17, 2019 · N216JB · Emb ERJ190100IGW · Cabin Cooling System
  > 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, CABIN CALL INDICATED THAT SMOKE WAS DISSIPATING. PERFORMED FIM 21-20-00-810-801-A, FOUND THE NR 2
- [SDR YENA201806280931](https://openairdocs.org/sdr/YENA201806280931.md): Skin Panel · cracked · Jun 28, 2018 · N216JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > 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 INCH. THIS CRACK RESULTED IN FUEL LEAK IN THIS AREA. SEE REF/2/ ETD FOR MORE DETAILS. REFER TO EC E
- [SDR YENA201802040897](https://openairdocs.org/sdr/YENA201802040897.md): Skin · cracked · Feb 4, 2018 · N216JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > 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 REF. /4/ SRM, HOWEVER, CUTOUT DIMENSIONS WERE NOT WITHIN THE LIMITS. ADDITIONALLY, WHILE ACCOMPLISH
- [SDR YENA201802040064](https://openairdocs.org/sdr/YENA201802040064.md): Skin · cracked · Feb 4, 2018 · N216JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > 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.md): Power Supply · no test · Sep 1, 2017 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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. OPS CHECKED GOOD.
- [SDR YENA201704230295](https://openairdocs.org/sdr/YENA201704230295.md): Bottle · empty · Apr 23, 2017 · N216JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > DURING A WEEKLY CHECK, FOUND FWD PASSENGER DOOR PRESSURE GAUGE AT 0 PSI. INSPECTED FWD PASSENGER DOOR PNEUMATIC ASSEMBLY AND FOUND THE PNEUMATIC ASSEMBLY DIAPHRAGM PUNCTURED. R & R THE DIAPHGRAM IAW 52-11-53 AND SERVICE DOOR IAW 52-11-51. ACFT OK FOR SERVI
- [SDR YENA201612261107](https://openairdocs.org/sdr/YENA201612261107.md): Battery Pack · failed · Dec 26, 2016 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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.md): Power Supply · failed · Mar 15, 2016 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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.md): Actuator · failed · Oct 18, 2015 · N216JB · Emb ERJ190100IGW · Trailing Edge Flap Actuator
  > 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 ACTUATOR IAW AMM 27-51-01. RIG AND OPS FOUND GOOD.
- [SDR YENA20150909414](https://openairdocs.org/sdr/YENA20150909414.md): Shear Tie · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > 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.md): Seal Rest · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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.md): Seal Rest · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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 ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150909411](https://openairdocs.org/sdr/YENA20150909411.md): Seal Rest · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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 ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150909410](https://openairdocs.org/sdr/YENA20150909410.md): Seal Rest · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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 CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150909409](https://openairdocs.org/sdr/YENA20150909409.md): Shear Tie · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > 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.md): Seal Rest · corroded · Sep 9, 2015 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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 BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150506099](https://openairdocs.org/sdr/YENA20150506099.md): Sensor · failed · May 6, 2015 · N216JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > 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 SYS, ELECTRCAL, RIGGING IAW AMM 27-80-00. OPS CK GOOD AT THIS TIME WITH NO MESSAGES NOTED. ACFT OK
- [SDR YENA20150506098](https://openairdocs.org/sdr/YENA20150506098.md): Sensor · failed · May 6, 2015 · N216JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > 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 SYS, ELECTRCAL, RIGGING IAW AMM 27-80-00. OPS CK GOOD AT THIS TIME WITH NO MESSAGES NOTED, ACFT OK
- [SDR YENA20140716135](https://openairdocs.org/sdr/YENA20140716135.md): I/O Card · failed · Jul 16, 2014 · N216JB · Emb ERJ190100IGW · Smoke Detection
  > 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 CUSTOM I/O & NR 1 GENERIC I/O CARDS IAW AMM 31-41-06-04 & 31-41-07-04. ALL CKS NORMAL.
- [SDR YENA20140115011](https://openairdocs.org/sdr/YENA20140115011.md): Power Supply · failed · Jan 15, 2014 · N216JB · Emb ERJ190100IGW · Emergency Lighting
  > 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 NORMAL.
- [SDR YENA20131228252](https://openairdocs.org/sdr/YENA20131228252.md): Circuit Card · failed · Dec 28, 2013 · N216JB · Emb ERJ190100IGW · Cabin Temperature Control System
  > 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.md): Crossbeam · corroded · Oct 16, 2013 · N216JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > 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. HFEC INSPECTION AND INSTALLED A (LT) ANGLE AND FILLER AS PERMANENT REPAIR IAW EA E13-647-01.
- [SDR YENA20130802167](https://openairdocs.org/sdr/YENA20130802167.md): Pressure Switch · failed · Aug 2, 2013 · N216JB · Emb ERJ190100IGW · Engine Fuel Indicating System
  > 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 PAGE GREEN AC PUMP BUT WHITE FUEL LINE TO ENGINE. INDICATIONS NORMAL EXCEPT ENG 2 JUST A LITTLE SLO

Next page: https://openairdocs.org/deregistered/N216JB-2025-02-25/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N216JB' AND deregistration_id = 'N216JB-2025-02-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N216JB-2025-02-25/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.