# Service difficulty reports: N279JB

A list on [N279JB](https://openairdocs.org/aircraft/N279JB.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 · 69 reports

- [SDR YENA2025031900269](https://openairdocs.org/sdr/YENA2025031900269.md): Girt Bar · unsecure · Mar 17, 2025 · N279JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT#2732, LGA-BOS. 'R1 SERVICE DOOR WON'T CLOSE AND ARM PROPERLY PER F1; RESECURED R1 DOOR GIRT BAR IAW AMM 52-11-41 AND RESECURED METAL RETAINING SEAL TAB AS REQ. OPS CHECK OK.'
- [SDR YENA2025031900268](https://openairdocs.org/sdr/YENA2025031900268.md): Unknown · odor · Mar 17, 2025 · N279JB · Emb ERJ190100IGW · Air Distribution System
  > FLT#2732, LGA-BOS. 'F2 INDICATED SHE SMELLED A FOUL ORDER THAT BOTHERED HER EYES AND NOSE; T/S PER FIM 21-20-00-810-801A NO SMOKE NOTED AND F2 SAID ODOR DISSIPATED AND NO SMELL IN FLIGHT OK FOR SVC.'
- [SDR YENA2023080800913](https://openairdocs.org/sdr/YENA2023080800913.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING" CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO2268 NRC 00151 CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED AND EVA
- [SDR YENA2023080800912](https://openairdocs.org/sdr/YENA2023080800912.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON DOUBLER REPAIR IN L/H BEAM BTW FR 15/17 AND Y=300 LH AT CABIN FLOOR STRUCTURE (W1); (RESOLVED ON W/O: 1241004 TASKCARD: NR-00011) REF: TOMX W/O 2268 N/R 00152. REPAIRED IAW ETI -190-23-601 REV 1 AND ETD 223-
- [SDR YENA2023080800911](https://openairdocs.org/sdr/YENA2023080800911.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Wing Structure
  > DURING HEAVY MAINTENANCE: CPCP FINDING: CORROSION ON RIB 3 IN ALL CONNECTORS SETTLEMENT AREA, BTW SPAR 2-3 WING LH AND RH; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00017)REF: TOMX W/O 2268 N/R 00204 CORROSION ON RIB 3 IN ALL CONNECTORS SETTLEMENT AREA, BTW SPAR
- [SDR YENA2023080800910](https://openairdocs.org/sdr/YENA2023080800910.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE: CICI FINDING: CORROSION ON RIB 3 IN ALL CONNECTORS, SETTLEMENT AREA, BTW SPAR 2-3 WING RIGHT MLG; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00018) REF: TOMX W/O 2268 N/R 00204 CORROSION WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER EMB
- [SDR YENA2023080800909](https://openairdocs.org/sdr/YENA2023080800909.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Escape Slide
  > DURING HEAVY MAINTENANCE: DURING R2 DOOR EVACUATION SLIDE REMOVAL, THE SAFETY PIN WAS FOUND OUT OF POSITION; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00023) R2 DOOR EVACUATION SLIDE WAS VERIFIED PER EMB 190 AIPC 25-65-01 (FIG-02.ITEM 10) AND REPLACED PER EMB 1
- [SDR YENA2023080800908](https://openairdocs.org/sdr/YENA2023080800908.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: CRACK ON LOWER EXTERNAL SKIN SPAR II AND RIB 10 AT LH WING; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00024) CRACK ON LOWER EXTERNAL SKIN SPAR II AND RIB 10 AT LH WING WAS REPAIRED PER EMB-190 SRM 57-10-01 REPAIR 54P. ALL WORK ACCOMPL
- [SDR YENA2023080800907](https://openairdocs.org/sdr/YENA2023080800907.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT AREA COVERED BY LIVE TV RADOME; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00025) CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT THE AREA COVERED BY LIVE TV RADOME WAS REMOVED AN
- [SDR YENA2023080800906](https://openairdocs.org/sdr/YENA2023080800906.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON DOUBLER REPAIR IN L/H BEAM BTW FR 15/17 AND Y=300 LH AT CABIN FLOOR STRUCTURE (W1); REF: TOMX W/O 2268 N/R 00152 REPAIRED IAW ETI -190-23-601 REV 1 AND ETD 223-190-017761 REV:/ (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023080800905](https://openairdocs.org/sdr/YENA2023080800905.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING" CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO2268 NRC 00151 CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED AND EVA
- [SDR YENA2023080800904](https://openairdocs.org/sdr/YENA2023080800904.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE / FR63 - FR64 & STGR 01L-02L / SKIN /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023080800903](https://openairdocs.org/sdr/YENA2023080800903.md): Unknown · unknown · Aug 5, 2023 · N279JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / FLOOR STRUCTURE / LH FLOOR TRACK / BTW FR 15 - 17 AND Y= -300 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023061600663](https://openairdocs.org/sdr/YENA2023061600663.md): Module · failed · Jun 12, 2023 · N279JB · Emb ERJ190100IGW · Detection System
  > FLT#1780, FLL-DCA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'LAV SMOKE MASTER WARN AT 10K UPON DEP CAME ON AT LEAST 3X DURING FLT, AIR RETURN FLL; FOUND #MAU 3 9/10 MODULE AT FAULT. REMOVED AND REPLACED IAW AMM GENERIC I/O MODULE IAW AMM 31-41-06. LOAD ANS
- [SDR YENA2022121601261](https://openairdocs.org/sdr/YENA2022121601261.md): Engine · failed · Dec 12, 2022 · N279JB · Emb ERJ190100LR · Engine (Turbine/Turboprop)
  > FLT 1555, BOS-DCA. AFTER LANDING, NR 1 ENGINE FAIL MESSAGE APPEARED AND THE ENGINE AUTO SHUTDOWN WITH ENGINE RUN SWITCH IN RUN. OPEN
- [SDR YENA2022122101280](https://openairdocs.org/sdr/YENA2022122101280.md): Anti-Ice Valve · faulted · Dec 11, 2022 · N279JB · Emb ERJ190100LR · Airfoil Anti/De-ice System
  > FLT#79, BOS-EWR. (AIRCRAFT DIVERTED TO BWI) ' WING A/I FAIL AFTER TAKEOFF WITH MFD SHOWING LEFT A/I VALVE FAILED CLOSED AND RIGHT NORMAL; ACCOMPLISHED LH WAI VALVE RESET IAW FIM TASK 30-11-00-810-808-A WITH NO FAULTS PRESENT. A/C OK FOR SERVICE. MCC BOB WAS N
- [SDR YENA2022031600259](https://openairdocs.org/sdr/YENA2022031600259.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ADJACENT TO FWD AND AFT LATCH FITTING LOCATED AT STRG 27R BETWEEN FR 77/80 IN AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 00072, CORROSION ON BEAM-BAG DOOR LOCATED AT
- [SDR YENA2022031600258](https://openairdocs.org/sdr/YENA2022031600258.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP OVER FR 88 BTWN STGR 28-29 RH AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00146, CORROSION ON SHEAR CLIP LOCATED IN FR 88 BETWEEN STRG 28R/29R AT AFT CARGO
- [SDR YENA2022031600257](https://openairdocs.org/sdr/YENA2022031600257.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN SHEAR CLIP LOCATED IN FR 87 BETWEEN STRG 27R/28R IN CF III INTERNAL STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 00075, CORROSION ON SHEAR CLIP LOCATED ON FR 87 BETWEEN STRG 27R/28R AT AF
- [SDR YENA2022031600256](https://openairdocs.org/sdr/YENA2022031600256.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP OVER FR 84 BTWN STGR 27-28 RH AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00142, CORROSION ON OVER FR 84 BTWN STGR 27-28 RH AT AFT CARGO COMPARTMENT WAS REMOV
- [SDR YENA2022031600255](https://openairdocs.org/sdr/YENA2022031600255.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN DOUBLER OF WASTE PANEL LOCATED IN FR 88 AND STRG 27R / 28R IN CF III INTERNAL STRUCTURE; ALL WORK WAS ACCOMPLISHED ON TOMEX NRC 000151, CORROSION ON INTERNAL DOUBLER OF PANEL BOX WASTE BTW
- [SDR YENA2022031600254](https://openairdocs.org/sdr/YENA2022031600254.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON FRAME 88 BTWN STGR 26-29 RH AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 000147, CORROSION ON FRAME 88 BTWN STGR 26-29 RH AT AFT CARGO COMPARTMENT WAS REMOVED AND EVALUAT
- [SDR YENA2022031600253](https://openairdocs.org/sdr/YENA2022031600253.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON FRAME 88 BTWN STGR 26-29 RH AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 000147, CORROSION ON FRAME 88 BTWN STGR 26-29 RH AT AFT CARGO COMPARTMENT WAS REMOVED AND EVALUAT
- [SDR YENA2022031600252](https://openairdocs.org/sdr/YENA2022031600252.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN SHEAR CLIP LOCATED IN FR 88 BETWEEN STRG 27R/28R IN CF III WASTE ACCESS DOOR CUTOUT INTERNAL STRUCTURE EVA; ALL WORK ACCOMPLISHED ON TOMEX NRC 00080, CORROSION ON SHEAR CLIP LOCATED IN
- [SDR YENA2022031600251](https://openairdocs.org/sdr/YENA2022031600251.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION OVER STRG 21L LOCATED BETWEEN FR 88/89 IN CF III INTERNAL STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 000150, CORROSION OVER STRG 21L LOCATED BETWEEN FR 88/89 IN CF III INTERNAL STRUCTURE
- [SDR YENA2022031600250](https://openairdocs.org/sdr/YENA2022031600250.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP OVER FR 85 BTWN STGR 27-28 RH AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 000144, CORROSION ON SHEAR CLIP LOCATED IN FR 85 BETWEEN STRG 27R/28R AT AFT CARGO
- [SDR YENA2022031600249](https://openairdocs.org/sdr/YENA2022031600249.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP OVER FR-83 BTW STGR-27L / STGR-28L AT AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00143, CORROSION ON OVER FR 83 BTWN STGR 27-28 RH AT AFT CARGO COMPARTMENT WAS
- [SDR YENA2022031600248](https://openairdocs.org/sdr/YENA2022031600248.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN SHEAR CLIP LOCATED IN FR 86 BETWEEN STGR 27R/28R AT CF III INTERNAL STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 00076, CORROSION ON SHEAR CLIP LOCATED IN FR 86 BETWEEN STGR 27R/28R AT
- [SDR YENA2022031600247](https://openairdocs.org/sdr/YENA2022031600247.md): Rib · cracked · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Wing, Attach Fittings
  > DURING HEAVY MAINTENANCE, CRACK RIB #17 AT RH WING FIXED LEADING EDGE; REF TOMX WO 1847 NR-00062, WING FIXED LEADING EDGE WAS REPLACED FOR A NEW RIB PER EMB-190 SRM 51-41-01PAR. 6, SRM 51-41-02 PAR. 6 SRM 51-43-03 PAR. 5 AND SRM 51-43-04 PAR. 5
- [SDR YENA2022031600246](https://openairdocs.org/sdr/YENA2022031600246.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN FWD AND MIDDLE SEAL REST LOCATED NEAR TO STRG 27R AND BETWEEN FR 77/78 IN AFT CARGO DOOR CUTOUT STRUCTURE; CORROSION IN FWD AND MIDDLE SEAL REST LOCATED NEAR TO STRG 27R AND BETWEEN FR 77/
- [SDR YENA2022031600245](https://openairdocs.org/sdr/YENA2022031600245.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN FINGER PLATE-CTLIII, AL IN AFT CARGO DOOR CUTOUT STRUCTURE LOCATED IN STRG 27R, BETWEEN FR 77 AND FR 78; CORROSION IN FINGER PLATE-CTL III, AT AFT CARGO DOOR CUTOUT STRUCTURE LOCATED IN ST
- [SDR YENA2022031600244](https://openairdocs.org/sdr/YENA2022031600244.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION IN SHEAR CLIP LOCATED IN FR 89 AND STRG 25L IN CF III INTERNAL STRUCTURE; CORROSION ON SHEAR CLIP OVER FR 89 BETWEEN STGR 25 LH AND STGR 25 LH AT AFT CARGO COMPARTMENT WAS BLENDED OUT AND EVA
- [SDR YENA2022031600243](https://openairdocs.org/sdr/YENA2022031600243.md): None · none · Mar 13, 2022 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP OVER FR 85 BTWN STGR 27-28 LH AT AFT CARGO COMPARTMENT; CORROSION ON SHEAR CLIP OVER FR 85 BETWEEN STGR 27-28 LH AT AFT CARGO COMPARTMENT WAS BLENDED OUT AND EVALUATED, THEREF
- [SDR YENA2020020750160](https://openairdocs.org/sdr/YENA2020020750160.md): Battery · no test · Feb 5, 2020 · N279JB · Emb ERJ190100IGW · Emergency Lighting
  > FT # 102, JFK-BUF. EMERGENCY LIGHT POWER UNIT #1 FAILS OPERATIONAL CHECK; REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT #1 PER E190MM 33-50-01,OPS CHECK GOOD.
- [SDR YENA2020010210720](https://openairdocs.org/sdr/YENA2020010210720.md): Girt Bar · fod · Dec 31, 2019 · N279JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT 1418, F-2 WAS UNABLE TO DISARM THE L2 DOOR. REMOVED DEBRIS FROM THE GIRT BAR. OPS CHECKEDKS GOOD. OK TO CONTINUE.
- [SDR YENA2019101620593](https://openairdocs.org/sdr/YENA2019101620593.md): Rib · cracked · Oct 12, 2019 · N279JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, A CRACK (L=3.109”) WAS FOUND ON THE RH WING LEADING EDGE RIB 27 (PN: 190-31277-002). SEE REF /1/ EA FOR DETAILS. THE DAMAGE IS FOUND TO BE OUTSIDE OF SRM SCOPE. EMBRAER WAS CONTACTED & PROVIDED REPAIR INSTRUCTIONS VIA REF /2/ ETD WHIC
- [SDR YENA201905280292](https://openairdocs.org/sdr/YENA201905280292.md): Acm · damaged · May 28, 2019 · N279JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 1986, PIT-BOS. EMERGENCY DECLARED. RETURNED TO FIELD. SMOKE IN COCKPIT AND CABIN AT FL 190 PERFORMED FULL QRH PROCEDURE IMMEDIATE RETURN TO FIELD. ALL ASSOCIATED EQUIPMENT USED INCLUDING COCKPIT O2, RAT, ETC; ACCOMPLISHED FIM TASK 21-20-00 FOUND #1 ACM TO
- [SDR YENA201905280291](https://openairdocs.org/sdr/YENA201905280291.md): Acm · faulty · May 28, 2019 · N279JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 1986, PIT-BOS. EMERGENCY DECLARED. RETURNED TO FIELD. SMOKE IN COCKPIT AND CABIN AT FL 190 PERFORMED FULL QRH PROCEDURE IMMEDIATE RETURN TO FIELD. ALL ASSOCIATED EQUIPMENT USED INCLUDING COCKPIT O2, RAT, ETC; ACCOMPLISHED FIM TASK 21-20-00 FOUND #1 ACM TO
- [SDR YENA201703030146](https://openairdocs.org/sdr/YENA201703030146.md): Module · failed · Mar 3, 2017 · N279JB · Emb ERJ190100IGW · Smoke Detection
  > DURING CLIMB OUT AT 500 FT, CREW RECEIVED AN EICAS MESSAGE FOR FWD CARGO SMOKE. CARGO FIRE BOTTLE WAS ARMED THEN FIRED. CREW INITIATED AIR TURN BACK TO DEPARTURE, AND LANDED UNEVENTFULLY. R & R ALL FWD CARGO SMOKE DETECTORS PER AMM 26-15-01. ALL OPS TEST NOR
- [SDR YENA201703030145](https://openairdocs.org/sdr/YENA201703030145.md): Smoke Detector · failed · Mar 3, 2017 · N279JB · Emb ERJ190100IGW · Smoke Detection
  > DURING CLIMB OUT AT 500 FT, CREW RECEIVED AN EICAS MESSAGE FOR AFT CARGO SMOKE. CARGO FIRE BOTTLE WAS ARMED THEN FIRED. CREW INITIATED AIR TURN BACK TO DEPARTURE, AND LANDED UNEVENTFULLY. R & R ALL FWD CARGO SMOKE DETECTORS IAW AMM 26-15-01. ALL OPS TEST NORM
- [SDR YENA201703030144](https://openairdocs.org/sdr/YENA201703030144.md): Smoke Detector · failed · Mar 3, 2017 · N279JB · Emb ERJ190100IGW · Smoke Detection
  > DURING CLIMB OUT AT 500 FT, CREW RECEIVED AN EICAS MESSAGE FWD CARGO SMOKE. CARGO FIRE BOTTLE WAS ARMED THEN FIRED. CREW INITIATED AIR TURN BACK TO DEPARTURE, AND LANDED UNEVENTFULLY ON THE FIELD. R & R ALL FWD CARGO SMOKE DETECTORS IAW AMM 26-15-01. ALL OPS
- [SDR YENA201703030143](https://openairdocs.org/sdr/YENA201703030143.md): Smoke Detector · failed · Mar 3, 2017 · N279JB · Emb ERJ190100IGW · Smoke Detection
  > DURING CLIMB OUT AT 500 FT, CREW RECEIVED EICAS MESSAGE FOR FWD CARGO SMOKE. CARGO FIRE BOTTLE WAS ARMED THEN FIRED. CREW INITIATED AIR TURN BACK AND LANDED UNEVENTFULLY ON THE FIELD. R & R ALL FWD CARGO SMOKE DETECTORS IAW AMM 26-15-01. ALL OPS TEST NORMAL
- [SDR YENA201703030142](https://openairdocs.org/sdr/YENA201703030142.md): Smoke Detector · failed · Mar 3, 2017 · N279JB · Emb ERJ190100IGW · Smoke Detection
  > DURING CLIMB OUT AT 500 FT, CREW RECEIVED EICAS MESSAGE FOR FWD CARGO SMOKE. CARGO FIRE BOTTLE WAS ARMED THEN FIRED. CREW INITIATED AIR TURN BACK AND LANDED UNEVENTFULLY ON THE FIELD. R & R ALL FWD CARGO SMOKE DETECTORS IAW AMM 26-15-01. ALL OPS TEST NORMAL
- [SDR YENA20160804677](https://openairdocs.org/sdr/YENA20160804677.md): Battery · discharged · Aug 4, 2016 · N279JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS FOR THE PASSENGER DOOR AND CABIN CEILING PANELS WOULD REMAIN ON WHEN ACFT WAS POWERED DOWN AND EMERGENCY LIGHTS NOT ARMED. IN ADDITION, EICAS DISPLAYED AN EMERGENCY LIGHT BATTERY FAULT.
- [SDR YENA20160607546](https://openairdocs.org/sdr/YENA20160607546.md): Battery · failed · Jun 7, 2016 · N279JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MAINTENANCE, MIDDLE LT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE; R & R EMERGENCY BATTERY IAW AMM 33-50-01-401. OPS CHECK GOOD
- [SDR YENA20150727291](https://openairdocs.org/sdr/YENA20150727291.md): Girt Bar · out of position · Jul 27, 2015 · N279JB · Emb ERJ190100IGW · Emergency Equipment
  > AT GATE F/A REPORTS RT SERVICE DOOR WILL NOT DISARM AND RED LOWER INDICATOR WILL NOT SHOW ARMED. DISARMED LEVER APPEARS STUCK IAW AMM 52-41-40. SECURED THE GIRT BAR INTO PLACE AND OPS CHECKED OK.
- [SDR YENA20150709261](https://openairdocs.org/sdr/YENA20150709261.md): Acm · failed · Jul 9, 2015 · N279JB · Emb ERJ190100IGW · Cabin Cooling System
  > DURING CLIMBOUT, AT ABOUT 20K NOTICED ODOR F/O SAW SMOKE FROM HIS VENT PACK 1, FAILED MESSAGE ON EICAS. APPLIED QRH PROCEDURES AND A LITTLE BIT MORE ODOR CONTINUED AT FLIGHT LEVEL 310. ODOR RETURNED ON DESCENT THROUGH 20K PACK, FAILED AT 15K, SWITCHED OFF NR
- [SDR YENA20150305039](https://openairdocs.org/sdr/YENA20150305039.md): Stringer · corroded · Mar 5, 2015 · N279JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE CHECK, IT WAS NOTED STR 28 RT BETWEEN FRAMES 88 AND 89 IS CORRODED. ACCOMPLISHED A DETAIL INSPECTION OF DAMAGED AREA IAW E190 NDT INTRODUCTION PARA 5.B. NO OTHER FAILURES NOTED. REMOVED STR 28 RIGHT, CUT A NEW STR AT 28 RT. SPLICED
- [SDR YENA20150302037](https://openairdocs.org/sdr/YENA20150302037.md): Shear Tie · corroded · Mar 2, 2015 · N279JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE CHECK, IT WAS DISCOVERED THAT THE SHEAR CLIP AT FR 87, STR 27R & 28R WAS CORRODED. REMOVED CORRODED SHEAR CLIP AT FR 87, STR 27R & 28R. REF SRM 51-41-01, 51-41-02. DRILLED, ALODINED AND, INSTALLED NEW SHEAR CLIP AT FR 87, STR 27R-28
- [SDR YENA20150227032](https://openairdocs.org/sdr/YENA20150227032.md): Skin · corroded · Feb 27, 2015 · N279JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > ON HEAVY MAINTENANCE CHECK, FOUND INTERNAL STRUCTURE BETWEEN FR 80 & 81, STRINGERS 28L & 27L CORRODED. BLENDED & REWORKED THE CORROSION DAMAGE, FABRICATED DOUBLER, SHIM, INSTALLED PARTS AND REPLACED FASTENERS. ALL WORK ACCOMPLISHED AND COMPLIED WITH EA E15-1

Next page: https://openairdocs.org/aircraft/N279JB/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 = 'N279JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N279JB/reports

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