# Service difficulty reports: N267JB

A list on [N267JB](https://openairdocs.org/aircraft/N267JB.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 · 92 reports

- [SDR YENA2025011500047](https://openairdocs.org/sdr/YENA2025011500047.md): Oxygen Mask · unwanted deploy · Jan 14, 2025 · N267JB · Emb ERJ190100IGW · Passenger Oxygen System
  > FLT#1155, BOS-DCA. 'PRESN AUTO FAIL WITH OXYGEN MASK DEPLOYMENT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024013000156](https://openairdocs.org/sdr/YENA2024013000156.md): Actuator · failed · Jan 25, 2024 · N267JB · Emb ERJ190100IGW · Aileron Control System
  > FLT#483, BOS-RDU. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO BOS) 'AUTO PILOT FAIL INFLIGHT AILERONS VERY DIFFICULT TO MOVE MANUALLY; FOUND AILERON TRIM ACTUATOR SLOW TO MOVE - OCCAISONALLY UNRESPONSIVE. REMOVED AND REPLACED AILERON TRI
- [SDR YENA2024011600040](https://openairdocs.org/sdr/YENA2024011600040.md): Pcu · failed · Jan 12, 2024 · N267JB · Emb ERJ190100IGW · Aileron Control System
  > AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AND AIR TURN BACK TO BOS. AIRCRAFT FLIGHT CONTROLS STIFF AND DIFFICULT TO TURN. AIRCRAFT WOULD NOT MAINTAIN LATERAL COURSE WITH AUTO PILOT ON. AUTO PILOT FAILED. NO ABNORMAL INDICATIONS ON ANY SYSTEMS PAGE. BOTH CA
- [SDR YENA2023112701458](https://openairdocs.org/sdr/YENA2023112701458.md): Anti-Ice Valve · failed · Nov 26, 2023 · N267JB · Emb ERJ190100IGW · Airfoil Anti/De-ice System
  > FLT#2783, BOS-RDU. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) 'A-I WING FAIL MULTIPLE OCCASIONS. COMPLIED WITH QRH. MESSAGE PERSIST; REMOVED AND REPLACED LH WING ANTI-ICE VALVE AND WING LH A-I PRESSURE SENSOR IAW AMM 30-11-01 AND AMM 30-11-03. RESPECTEVELY.
- [SDR YENA2023031700250](https://openairdocs.org/sdr/YENA2023031700250.md): Shutoff Valve · failed · Mar 13, 2023 · N267JB · Emb ERJ190100LR · Pneumatic System
  > FLT#2231, BOS-LGA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) 'DURING CLIMBOUT IN ICING CONDITIONS BLEED 2 FAILED UNABLE TO RESET PER QRH RETURNED TO BOS TO AVOID ICING CONDITIONS; REMOVED AND REPLACED PRSOV IAW AMM 36-11-03. OPS GOOD. AT THIS TIME NO FAULTS
- [SDR YENA2022080800755](https://openairdocs.org/sdr/YENA2022080800755.md): Floor Splice · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING": CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 76 AND STGR 28RH/29RH; SUMMARY OF NRC 00272: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 76 AND STGR 28RH/29RH WAS REMOVED A
- [SDR YENA2022080800770](https://openairdocs.org/sdr/YENA2022080800770.md): Light · inoperative · Jul 29, 2022 · N267JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DURING INTERIOR LIGHTS CHECK, EMERGENCY LIGHTS FROM CEILING PANEL 227BLC, 233ALC, 243CLC, 243GLF, AND 243ELC ARE INOPERATIVE; REF TOMX WO # 1997 N/R# 00465. TROUBLESHOOTING WAS PERFORMED PER EMB-190 FIM 33-50-00-810--813-A AND EMB-190
- [SDR YENA2022080800769](https://openairdocs.org/sdr/YENA2022080800769.md): Slat Track · cracked · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Leading Edge Slat Control System
  > DURING HEAVY MAINTENANCE: CRACK ON SLAT TRACK #5 CUTOUT AT LH WING FIXED LEADING EDGE UPPER SKIN; REF TOMX WO # 1997 N/R# 00208. SLAT TRACK #5 CUTOUT AT LH WING FIXED LEADING EDGE UPPER SKIN WAS REPAIRED PER.EMB-190 ETI-190-22-600 REV ORIGINAL, EC E22-532-01 A
- [SDR YENA2022080800768](https://openairdocs.org/sdr/YENA2022080800768.md): Spar · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: CORROSION ON SHARE CLIP BTW FR 16 AT STGR 28R AND STGR 28L ON FWD CARGO COMPARTMENT; REF TOMX WO# 1997 N/R# 00314. SHARE CLIP BTW FR 16 AT STGR 28R AND STGR 28L ON FWD CARGO COMPARTMENT WAS REPLACED PER EMB 190 SRM 51-43-01 AND SRM 5
- [SDR YENA2022080800767](https://openairdocs.org/sdr/YENA2022080800767.md): Spar · cracked · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: A 0.343” LENGTH CRACK WAS FOUND AT RH PYLON INBOARD SPAR AFT BUSHING BORE; REF TOMX WO# 1997 N/R# 00403. RH PYLON INBOARD SPAR WAS REPLACED PER EMB-190 S.R.M. 51-43-03 AND S.R.M. 51-43-04..
- [SDR YENA2022080800766](https://openairdocs.org/sdr/YENA2022080800766.md): Bushing · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: CORROSION ON BUSHING HOUSING AT RH FITTING ASSY FRAME 100 INBD/OUTBD LUG; REF TOMX WO# 1997 N/R# 00424. BUSHING HOUSING AT RH FITTING ASSY FRAME 100 INBD/OUTBD LUG WERE REPAIRED PER ETI-190-22-612 REV. 7, ETD2022-190-021932 REV. ORIG
- [SDR YENA2022080800765](https://openairdocs.org/sdr/YENA2022080800765.md): Stringer · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: CORROSION ON STGR21L BTW FR83/FR82 AFT CARGO COMPARTMENT; REF TOMX N/R 00381 WO 1997 STGR22L BTW FR83/FR82 AFT CARGO COMPARTMENT WAS REPLACED PER EMB-190 SRM 53-23-00 REPAIR 51, THERE IS NO CHANGE TO THE MAINTENANCE PLAN DUE TO THIS R
- [SDR YENA2022080800764](https://openairdocs.org/sdr/YENA2022080800764.md): Floorbeam · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: CORROSIÓN ON FLOOR STRUCTURE RH WEB BTW FR 87-88, W2; REF TOMX NR 00241 WO 1997 WEB FLOOR STRUCTURE RH BTW FR 87-88, W2 WAS REPLACED PER EMB-190 SRM 51-42-01..
- [SDR YENA2022080800763](https://openairdocs.org/sdr/YENA2022080800763.md): Floorbeam · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE: CORROSIÓN ON FLOOR STRUCTURE CENTRAL WEB BTW FR 87-88; W2; REF. TOMX WO.1997 NR-00240 - FLOOR STRUCTURE CENTRAL WEB BTW FR 87-88; W2 WAS REPLACED PER.EMB-190 SRM 51-42-01.
- [SDR YENA2022080800762](https://openairdocs.org/sdr/YENA2022080800762.md): Stringer · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION “CPCP FINDING”: CORROSION LOCATED ON SPLICE STRG 21L AND BETWEEN FR 88/89 INTERNAL STRUCTURE CF III; IN COMPLEMENT WIP # 14. A NEW SPLICE WAS INSTALLED ON STRG 21LH AND BETWEEN FR 88/89 INTERNAL STRUCTURE CF III PER
- [SDR YENA2022080800761](https://openairdocs.org/sdr/YENA2022080800761.md): Floorbeam · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 82 AND STGR 28LH/29LH; SUMMARY OF NRC 00291: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 82 AND STGR 28LH/29LH WAS REMOVED A
- [SDR YENA2022080800760](https://openairdocs.org/sdr/YENA2022080800760.md): Floor Support · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 83 AND STGR 21LH/22LH; SUMMARY OF NRC 00298:CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 83 AND STGR 21LH/22LH WERE REMOVED A
- [SDR YENA2022080800759](https://openairdocs.org/sdr/YENA2022080800759.md): Floor Support · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 73 AND STGR 27LH/28LH; SUMMARY OF NRC 00287: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 73 AND STGR 27LH/28LH WAS REMOVED A
- [SDR YENA2022080800758](https://openairdocs.org/sdr/YENA2022080800758.md): Shear Restraint · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 22LH/23LH; SUMMARY OF NRC 00266: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 22LH/23LH WAS REMOVED A
- [SDR YENA2022080800757](https://openairdocs.org/sdr/YENA2022080800757.md): Floor Skin · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 23LH/24LH; SUMMARY OF NRC 00265: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 23LH/24LH WAS REMOVED A
- [SDR YENA2022080800756](https://openairdocs.org/sdr/YENA2022080800756.md): Shear Tie · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: “CPCP FINDING”: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 24LH/25LH; SUMMARY OF NRC 00264: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 78 AND STGR 24LH/25LH WAS REMOVED A
- [SDR YENA2022080800754](https://openairdocs.org/sdr/YENA2022080800754.md): Flap Track · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Leading Edge Devices
  > DURING HEAVY MAINTENANCE: WING / LH WING / FIXED LEADING EDGE / SKIN PANEL / RIB 19 - 20 / CRACK. PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2022080800753](https://openairdocs.org/sdr/YENA2022080800753.md): Hinge · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / H. STABILIZER HINGE / FR 100 / RH FITTING/ MISALIGNMENT - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2022080800752](https://openairdocs.org/sdr/YENA2022080800752.md): Floor Skin · corroded · Jul 29, 2022 · N267JB · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR82-83 & STGR 22L / CORROSION. PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2022031800280](https://openairdocs.org/sdr/YENA2022031800280.md): Exhaust Duct · leaking · Mar 16, 2022 · N267JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT#1527, EWR-FLL. "BLEED 2 LEAK AT FL 150 ON ARRIVAL; ACCOMPLISHED ENG#2 PRECOOLER EXHAUST DUCT RE-SEAL AS PER M.M 54-50-25 & EMBRAER ETD2010/190-10969. ACCOMPLISHED ENG 2 IDLE RUN AND ENG 2 BLEED SYS LEAK/OPS CHECK AS REQUIRED PER M.M. 36-00-00. ALL OPS/IND.
- [SDR YENA2021100700660](https://openairdocs.org/sdr/YENA2021100700660.md): Engine · faulted · Oct 5, 2021 · N267JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > FLT# 1355, BOS-DCA (RETURNED BACK BOS). ENG 1 CONTROL FAULT ITT INDICATION WENT AMBER AND FUEL FLOW WAS 500PPHABOVE #2 DURING CLIMB. ENGINE WOULD NOT MAKE CLIMB 1 THRUST WITHIN ITT LIMITS; R & R # 1 ENGINE IAW AMM 71-00-01
- [SDR YENA2020120900585](https://openairdocs.org/sdr/YENA2020120900585.md): Rib · cracked · Nov 29, 2020 · N267JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, REF NDT 57-40-00-211-802, CRACK RIB 17 WING MAIN BOX LEADING EDGE AREA LT WING, REF AEROMAN WO 2020-388/1, NR 2020-360940. REMOVED AND REPLACED RIB 17 LOCATED LEADING EDGE ON LT WING, IAW E190 SRM 51-40-08 DWG 190-31005-409.
- [SDR YENA2020120900584](https://openairdocs.org/sdr/YENA2020120900584.md): Rib · cracked · Nov 29, 2020 · N267JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, REF NDT 57-40-00-211-802 CRACK RIB 17 WING MAIN BOX LEADING EDGE AREA RT WING, REF AEROMAN WO 2020-388/1, NR 2020-360939. REMOVED AND REPLACED RIB 17 LOCATED LEADING EDGE ON RT WING, IAW E190-SRM 51-40-08 AND DWG 190-31005-409.
- [SDR YENA2020120900583](https://openairdocs.org/sdr/YENA2020120900583.md): Rib · cracked · Nov 29, 2020 · N267JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, REF NDT 57-40-00-211-802, CRACK RIB 22 WING MAIN BOX LEADING EDGE AREA LT WING, REF AEROMAN WO 2020-388/1, NR 2020-360941. REMOVED AND REPLACED RIB 22 AND FASTENERS LOCATED LEADING EDGE AREA LT WING, IAW SRM 51-40-08 AND DRAWING 190-
- [SDR YENA2020120900582](https://openairdocs.org/sdr/YENA2020120900582.md): Power Supply · failed · Nov 29, 2020 · N267JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT BATTERY AFT RT, REF AEROMAN N/R 2020-360931. REMOVED AND REPLACED ELPU, IAW E190-AMM 33-50-01-400-801-A. OPERATIONS CHECK GOOD, IAW E190 AMM 33-50-01-710-801-A.
- [SDR YENA2020120900581](https://openairdocs.org/sdr/YENA2020120900581.md): Power Supply · failed · Nov 29, 2020 · N267JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT POWER UNIT AFT RT INBOARD, REF AEROMAN N/R 2020-360932. REMOVED AND REPLACED ELPU, IAW E190 AMM 33-50-01-400-801-A. OPERATIONS CHECK GOOD, IAW E190- 33-50-00-710-801-A.
- [SDR YENA201912160701](https://openairdocs.org/sdr/YENA201912160701.md): Skin · cracked · Dec 12, 2019 · N267JB · Emb ERJ190100IGW · Nacelle/Pylon, Plate/Skin
  > FT # 526, TPA-JFK. #1 ENGINE INBOARD PYLON CRACK (REF ORIGINAL INSP LP 2766591-1); AEROMAN WO# 2019-414/1 WCC# 2019-414201 PERFORMED PROCEDURE TO LH PYLON IB UPPER SPAR LINK SPAR REPLACEMENT ALTERNATE TOOLING PER AEROMAN EA 54-50-76-19 REV 0(COVER 1 PART 1) AN
- [SDR YENA201812030960](https://openairdocs.org/sdr/YENA201812030960.md): Diverter · broken · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · APU Oil System
  > DURING HEAVY MAINTENANCE AT YRQ FOUND WITH A SECTION OF APU OIL COOLER AIR INLET DIVERTER (P/N: 170-50258-005) FOUND BROKEN AND MISSING. ALSO, WHILE INVESTIGATION OF AFFECTED AREA, YRQ FOUND APU COMPARTMENT RT UPPER PANEL CRACKED AT 6 PLACES. DVI AND HFEC INSP
- [SDR YENA201812030956](https://openairdocs.org/sdr/YENA201812030956.md): Skin · damaged · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Rudder, Plate/Skin
  > DURING BASIC 6 CHECK AT YRQ DATED 11/18, OBJECT IMPACT AND PERFORATION DAMAGE WAS FOUND ON THE RUDDER P/N 190-09910-431 S/N 0000261387 RT SKIN PANEL P/N 190-63064-409. SEE REF. (1) FOR DETAILS. ULTRASONIC INSPECTION WAS ACCOMPLISHED ON THE AREAS SURROUNDING TH
- [SDR YENA2018120730834](https://openairdocs.org/sdr/YENA2018120730834.md): Shear Tie · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CNTR FUSE III BELOW CABIN FLOOR CORR SHEAR CLIP FR89; REF NRC FOR ALL WORK ACP. SHEAR CLIPS RPL IAW SRM 51-41-01, -02, & 51-43-03.
- [SDR YENA2018120730833](https://openairdocs.org/sdr/YENA2018120730833.md): Doubler · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RH TRANSPONDER ANTENNA DOUBLER CORRBET FR19 -FR20; REF NRC FOR ALL WORK ACP. RH TRANSPONDER ANT DOUBLER RPL IAW SRM 51-41-02
- [SDR YENA2018120730832](https://openairdocs.org/sdr/YENA2018120730832.md): Shear Tie · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR CLIP FR87; REF NRC FOR ALL WORK ACP. SHEAR CLIP RPL AT FR 87 STGR 29L-29R IAW SRM 51-41-01,02,03.
- [SDR YENA2018120730831](https://openairdocs.org/sdr/YENA2018120730831.md): Threshold · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DR CUTOUT CORR THRESHOLD FINGER PLATE; REF NRC FOR ALL WORK ACP. THRESHOLD FWD FINGER PLATE RPL IAW SRM 51-43-03, 51-43-04
- [SDR YENA2018120730830](https://openairdocs.org/sdr/YENA2018120730830.md): Seal Rest · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DR CUT OUT MID LWR SEAL REST; REF NRC FOR ALL WORK ACP: MIDDLE LWR SEAL REST RPL PER SRM 51-41-01
- [SDR YENA2018120730829](https://openairdocs.org/sdr/YENA2018120730829.md): Seal Rest · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR CUT OUT LWR CRNR SEAL REST; REF NRC FOR ALL WORK ACP: RPL SEAL REST IAW SRM 53-23-29 FIG20
- [SDR YENA201812030828](https://openairdocs.org/sdr/YENA201812030828.md): Gusset · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PAX CABIN GUSSET PLATE FR90 RBL23; REF NRC FOR ALL WORK ACP. RPL GUSSET PLATE IAW SRM 51-41-02
- [SDR YENA2018120730827](https://openairdocs.org/sdr/YENA2018120730827.md): Gusset · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PAX CABIN FR90 RBL11 GUSSET PLATE; REF NRC FOR ALL WORK ACP. RPL GUSSET PLATE IAW SRM 51-41-02
- [SDR YENA2018120930826](https://openairdocs.org/sdr/YENA2018120930826.md): Doubler · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PAX CABIN FLR DOUBLER FR16; REF NRC FOR ALL WORK ACP. RPL FLR DOUBLER IAW SRM 51-41-02.
- [SDR YENA2018120730825](https://openairdocs.org/sdr/YENA2018120730825.md): Doubler · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CNTR FUSE BELOW FLR PNL WASTE PAN DOUBLER; REF NRC FOR ALL WORK ACP. RPL FWD PAN DOUBLER IAW SRM 51-43-04
- [SDR YENA2018120730824](https://openairdocs.org/sdr/YENA2018120730824.md): Shear Tie · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CNTR FUSE 111 BELOW CABIN FLR SHEAR CLIP FR88; REF NRC FOR ALL WORK ACP. SHEAR CLIP RPL SRM 51-41-01, 51-41-02
- [SDR YENA2018120730823](https://openairdocs.org/sdr/YENA2018120730823.md): Shear Panel · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PAX CABIN RH SHEAR PNL FR87-88; REF NRC FOR ALL WORK ACP. RH SHEAR PNL RPL IAW SRM 51-42-01, 51-42-03
- [SDR YENA2018120730822](https://openairdocs.org/sdr/YENA2018120730822.md): Seat Track · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RH INBD TRACK FR17; REF NRC FOR ALL WORK ACP. SEAT TRACK RPL PER SRM 51-41-01/02, 51-43-03
- [SDR YENA2018120730821](https://openairdocs.org/sdr/YENA2018120730821.md): Doubler · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PASS CABIN FR18-19 FLR SUPP DOUBLER; REF NRC FOR ALL WORK ACP. FLR SUPP DOUBLER CORR RPL IAW SRM 51-41-02, 51-43-04
- [SDR YENA2018120730820](https://openairdocs.org/sdr/YENA2018120730820.md): Seat Track · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PASS CABIN RH INBD SEAT TRACK CORR FR17; REF NRC FOR ALL WORK ACP. SEAT TRACK RPL IAW SRM 51-41-01/02, 51-43-03
- [SDR YENA2018120730819](https://openairdocs.org/sdr/YENA2018120730819.md): Crossbeam · corroded · Dec 3, 2018 · N267JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON PASS CABIN UPR FLANGE CR BEAM FR17; REF NRC FOR ALL WORK ACP: RPL SUPP ANGLE PER SRM 51-43-03.

Next page: https://openairdocs.org/aircraft/N267JB/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 = 'N267JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N267JB/reports

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