# Service difficulty reports: N247JB, cancelled Oct 23, 2025

A list on [N247JB, cancelled Oct 23, 2025](https://openairdocs.org/deregistered/N247JB-2025-10-23.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 · 68 reports

- [SDR EE4Y2025092723176](https://openairdocs.org/sdr/EE4Y2025092723176.md): Skin · damaged · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF SB 190-57-0056 AT RH WING AFT REINFORCEMENT AREA, WAS FOUND FIVE OVERSIZED FASTENER HOLES LOCATED AT THE AREA AFFECTED BY THE REINFORCEMENT DOUBLERS AND FITTING. THIS CONDITION WAS REPORTEDAND REPAIRED IAW ETD2025-190-927169 DTD AU
- [SDR EE4Y2025092723175](https://openairdocs.org/sdr/EE4Y2025092723175.md): Skin · damaged · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF SB 190-57-0056 AT THE LH WING FORWARD REINFORCEMENT AREA, ALLIANCE AIRLINES FOUND TWO OVERSIZED FASTENER HOLES LOCATED IN THE AREA AFFECTED BY THE REINFORCEMENT DOUBLERS. THE FIRST ONE FASTENER HOLE (HOLE A) IS COMMON TO THE SRGT22
- [SDR EE4Y2025092723174](https://openairdocs.org/sdr/EE4Y2025092723174.md): Skin · delaminated · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Trailing Edge Flaps
  > CUSTOMER REPORTS DELAMINATION DAMAGE AFFECTING THE LH INBOARD AFT FLAP LOWER SKIN. THE DAMAGE IS LOCATED AT SPAR 2 AND RIB 5A +50MM. THE DAMAGE AREA WAS EVALUATED AS PER SRM 57-52-00 AD51, HOWEVER, THE DELAMINATION IS LOCATED AT THE ZONE 1 AREA AND TABLE 101.
- [SDR EE4Y2025FA0000667](https://openairdocs.org/sdr/EE4Y2025FA0000667.md): Skin · worn · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Engine Thrust Reverser
  > DURING THE INSPECTION WAS FOUND ON ENGINE NR 2 OUTBD THRUST REVERSER TRANSLATING COWL, EXTERNAL SKIN WITH WORN AT 1 O’CLOCK POSITION. DUE TI THIS, WAS REPORTED AND REPAIRED TO BOWDEN (ENGINEERING SOLUTIONS PTY LDT) WITH THE ENGINEERING ORDER ESE-ERJ190-78-006
- [SDR EE4Y2025092723172](https://openairdocs.org/sdr/EE4Y2025092723172.md): Repair · misinstalled · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND ON THE FUSELAGE SKIN AT FR19 BETWEEN STR-27R. ACCORDING TO PREVIOUS OPERATOR DOCUMENTATION, THE REPAIR WAS PERFORMED UNDER ETD2025-190-000892 GUIDELINES. DUE TO ITS CONDITION (TOOL MARKS AND POORLY DRI
- [SDR 2025FA0000651](https://openairdocs.org/sdr/2025FA0000651.md): Skin · damaged · Sep 17, 2025 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE STRUCTURE INSPECTION IT WAS FOUND THE FORWARD FUSELAGE, AT FR18+50MM, AND S27LH + 155MM (JUST 8.0MM FROM THESTR 28L FASTENER ROW), THE EXTERNAL SKIN WITHLIGHTNING STRIKE WITH EXISTING BLEND OUT. THE BLEND OUT WAS EVALUATED AND CLASSIFIED ASNON-SIGNI
- [SDR EE4Y2025091723171](https://openairdocs.org/sdr/EE4Y2025091723171.md): Skin · damaged · Sep 17, 2025 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE EXTERNAL SKIN OF THE FWD FUSELAGE, LOCATED AT FRAME 20+85MM, STRINGER 27RH+115MM. THE DAMAGE EXCEEDS 50% OF THE SKIN THICKNESS. A 3.97MM HOLE WAS DRILLED TO INSTALL A THROUGH DAMAGE REPAIR IN ACCORDANCE
- [SDR YENA2024061300868](https://openairdocs.org/sdr/YENA2024061300868.md): Power Supply · failed · Jun 11, 2024 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT#2254, DCA-BOS.' WHILE PERFORMING TASK CARD E190-33-50-25-710-801 FWD RH EXT EMERG LIGHT WILL NOT ILLUMINATE. ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT); REMOVED AND REPLACED ELPU OPS CHECKS OK PER AMM 30-50-01. THIS CLEARS MDDR 550483 MEL 33-50-25A
- [SDR YENA2023122101639](https://openairdocs.org/sdr/YENA2023122101639.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: AFTER LATCH FITTINGS REMOVAL IN REF WITH NRC 071,CORROSION ON LOWER BEAM IN CUTOUT AT FWD CARGO DOOR; REF TOMX WO # 2404 NR # 00144 CORROSION ON LOWER BEAM IN FWD CARGO DOOR CUTOUT WAS REMOVED PER EMB-190 SRM 51-12-01 AND SRM 51-10-0
- [SDR YENA2023122101638](https://openairdocs.org/sdr/YENA2023122101638.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CRACK AT END OF STRG 9R IN FR 73, LOCATED AT INTERNAL STRUCTURE OF CF II; REF TOMX WO #2404 TOMX NR # 00051Y:STRG 9R IN FR 73, LOCATED AT INTERNAL STRUCTURE OF CF II WAS REPLACED PER EMB 190 SRM 51-43-03 AND SRM 51-43-04.
- [SDR YENA2023122101637](https://openairdocs.org/sdr/YENA2023122101637.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: AFTER STRG 29R REMOVAL, FOUND CORROSION AT INNER FUSELAGE SKIN LOCATED BETWEEN FR73/74 IN AFT CARGO COMPARTMENT; REF TOMX WO # 2404 NR # 00168 CORROSION AT INNER FUSELAGE SKIN LOCATED BETWEEN FR73/74 IN AFT CARGO COMPARTMENT WAS REMOV
- [SDR YENA2023122101636](https://openairdocs.org/sdr/YENA2023122101636.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DURING AFT FUS FAIRING 199ML INSTALLATION, UPPER EMERGENCY LIGHT WAS FOUND INNOPERATIVE; REF TOMX WO #2404 NR # 00176 UPPER EMERGENCY LIGHT WAS REPLACED PER EMB-190 AMM 33-50-25--000-802-A AND PER EMB-190 AMM 33-50-25--400-802-A.
- [SDR YENA2023122101635](https://openairdocs.org/sdr/YENA2023122101635.md): None · none · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Standard Practices/Structures
  > DURING HEAVY MAINTENANCE: # 2 ENGINE REMOVED TO FOM; # 2 ENGINE REINSTALLED IAW E190 AMM 71-00-01.
- [SDR YENA2023122101634](https://openairdocs.org/sdr/YENA2023122101634.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON STRINGER ON AFT COMPARTMENT STRUCTURE BTW FR 76/78 AND STRG 29R; "REF TOMX WO # 2404 NR # 00091 CORROSION ON STRINGER ON AFT COMPARTMENT STRUCTURE BTW FR 76/78 AND STRG 29R WAS REMOVED PER EMB-190 SRM 51-12-0
- [SDR YENA2023122101633](https://openairdocs.org/sdr/YENA2023122101633.md): Shear Tie · corroded · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ON AFT COMPARTMENT STRUCTURE BTW FR87 AND STRG 28R/27R; "REF: TOMX W/O 2404 N/R 00097 REPLACED SHEAR CLIP PER EMB190 SRM 51-43-03 AND SRM 51-41-02".
- [SDR YENA2023122101632](https://openairdocs.org/sdr/YENA2023122101632.md): Shear Tie · corroded · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLPI ON AFT COMPARTMENT STRUCTURE BTW FR88 AND STRG 28R/27R; "REF: TOMX W/O 2404 N/R 00096 REPLACED SHEAR CLIP PER EMB-190 SRM 51-41-02 AND SRM 5143-03"
- [SDR YENA2023122101631](https://openairdocs.org/sdr/YENA2023122101631.md): Shear Tie · corroded · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ON AFT COMPARTMENT STRUCTURE BTW FR83 AND STRINGER 28L/29L; "REF: TOMX W/O 2404 N/R 00090 STRINGER CLIP WAS REPLACED PER EMB-190 SRM 51-41-02 AND SRM 51-43-01".
- [SDR YENA2023122101630](https://openairdocs.org/sdr/YENA2023122101630.md): Shear Tie · corroded · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSTION ON SHEAR CLIP IN AFT COMPARTMENT STRUCTURE BTW FR82 AND STRINGER 28R/29R; "REF: TOMX W/O 2404 N/R 00089SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-41-02 AND SRM 51-43-03".
- [SDR YENA2023122101629](https://openairdocs.org/sdr/YENA2023122101629.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION ON RH SEAT TRACK LOCATED BTW RE 17/18 AND Y:300RH AT CABIN FLOOR STRUCTURE (W1); REF: TOMX W/O 2404 N/R - 00060 SEAT TRACK WAS REPLACED PER EMB-190 SRM 51-12-01, SRM 51-10-03, SRM 51-75-16, SRM 53-10-10/AD51, SRM 51-41-01, S
- [SDR YENA2023122101628](https://openairdocs.org/sdr/YENA2023122101628.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FLOOR STRUCTURE / RH SEAT TRACK / FR84 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023122101627](https://openairdocs.org/sdr/YENA2023122101627.md): Unknown · unknown · Dec 20, 2023 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II / LOWER SKIN / AT STR 29R BETWEEN FR73 – FR74 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023092601127](https://openairdocs.org/sdr/YENA2023092601127.md): Battery · damaged · Sep 24, 2023 · N247JB · Emb ERJ190100IGW · Emergency Locator Beacon
  > FLT#2754, DCA-BOS. 'ELT BATTERY ??? AND FOUND ELT WIRES DAMAGED; REPLACED ELT BATTERY REPAIRED C/P PER 25-61-01. CHECK SYSTEM OK.PER 25-61-00.'
- [SDR YENA2022121901271](https://openairdocs.org/sdr/YENA2022121901271.md): Link · malfunctioned · Dec 17, 2022 · N247JB · Emb ERJ190100LR · Landing Gear Retraction/Extension System
  > FLT 1340, NAS-MCO. AFTER LIFT OFF LANDING GEAR UP LOCK SELOIND CYCLE REPEATEDLY. GEAR HAND WOULD NOT GO UP MOMENTARILY. OCCURRED ON BOTH LEGS. THE GEAR EXTENDED NORMALLY. SEE PREVIOUS WRITE UP(12/14); REF LP 3457854, ITEM 2. REPLACED HARDWARE OF RH MAIN GEAR
- [SDR YENA2022031500212](https://openairdocs.org/sdr/YENA2022031500212.md): Skin · cracked · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE, CRACK: LOWER SKIN RH WING AT WING SPAR 2 AND RIB 9A +3.00"; REF TOMX NR 00373:ACCOMPLISHED REPAIR IAW EMBRAER SRM 57-10-01 PAR 11(P)(Q)(R)(T), FIG 202 SHEET 4 AND SRM 51-43-01 PAR 5, FIG 2. TOMAX R.S. 4TOY762C TECH 89307 QC RII 23691
- [SDR YENA2022031500211](https://openairdocs.org/sdr/YENA2022031500211.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF TOMX NR 00301 FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB
- [SDR YENA2022031500210](https://openairdocs.org/sdr/YENA2022031500210.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB 190 SRM 51-40-08 AND S
- [SDR YENA2022031500209](https://openairdocs.org/sdr/YENA2022031500209.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF TOMX NR 00301 MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PE
- [SDR YENA2022021600071](https://openairdocs.org/sdr/YENA2022021600071.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE, CRACK: LOWER SKIN RH WING AT WING SPAR 2 AND RIB 9A +3.00"; REF TOMX NR 00373:ACCOMPLISHED REPAIR IAW EMBRAER SRM 57-10-01 PAR 11(P)(Q)(R)(T), FIG 202 SHEET 4 AND SRM 51-43-01 PAR 5, FIG 2. TOMAX R.S. 4TOY762C TECH 89307 QC RII 23691
- [SDR YENA2022021600070](https://openairdocs.org/sdr/YENA2022021600070.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF TOMX NR 00301 FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB
- [SDR YENA2022021600069](https://openairdocs.org/sdr/YENA2022021600069.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; ALL WORK ACCOMPLISHED REF TOMX NR 00301 MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PE
- [SDR YENA2022021600068](https://openairdocs.org/sdr/YENA2022021600068.md): None · none · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB 190 SRM 51-40-08 AND S
- [SDR YENA2022021600067](https://openairdocs.org/sdr/YENA2022021600067.md): Seal Rest · corroded · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; "ALL WORK ACCOMPLISHED REF TOMX NR 00301 FWD SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB
- [SDR YENA2022021600066](https://openairdocs.org/sdr/YENA2022021600066.md): Seal Rest · corroded · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN AFT SEAL REST IN LOWER EDGE OF AFT CARGO; "ALL WORK ACCOMPLISHED REF TOMX NR 00301 AFT SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PER EMB 190 SRM 51-40-08 AND
- [SDR YENA2022021600065](https://openairdocs.org/sdr/YENA2022021600065.md): Door Frame · corroded · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, "FROM TOMX NR 00300, INITIAL INSPECTION: ""CPCP FINDING"" CORROSION IN FASTENER PERIPHERY LOCATED OVER MACHINED BEAM BETWEEN STRG 27R/28R AND FR 77 IN AFT CARGO DOOR CUTOUT STRUCTURE"; "FROM TOMX NR 00300, INITIAL INSPECTION: ""CPCP
- [SDR YENA2022021600064](https://openairdocs.org/sdr/YENA2022021600064.md): Door Frame · corroded · Dec 21, 2021 · N247JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; "ALL WORK ACCOMPLISHED REF TOMX NR 00301 MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED P
- [SDR YENA2021102100707](https://openairdocs.org/sdr/YENA2021102100707.md): Diaphragm · blown · Oct 20, 2021 · N247JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > FLT # 628, CHS-EWR. R1 DOOR REQ. SERVICING AND DOOR DIAPHRAM BLOWN.; REPLACED R-1 SERVICE DOOR PNEUMATIC ASSY DIAPHRAM AND SHEAR PIN IAW AMM 52-41-53/400. SERVICE R-1 DOOR PNEUMATIC ASSY IAW AMM 52-41-51. LEAK CHECK OK.
- [SDR YENA2021102100706](https://openairdocs.org/sdr/YENA2021102100706.md): Slide · deployed · Oct 20, 2021 · N247JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > FLT # 628, CHS-EWR. A/C OOS DUE TO R1 DOOR SLIDE BLOWN; R/R OF R1 DOOR SLIDE IAW AMM 52-11-40. OPS CHECK GOOD A/C OK FOR SVC.
- [SDR YENA2021072900489](https://openairdocs.org/sdr/YENA2021072900489.md): Control Module · failed · Jul 25, 2021 · N247JB · Emb ERJ190100IGW · Landing Gear Brake System
  > FLT 2155, JFK-FLL. IN CRUISE, GOT "BRK FH FAULT" AND "BRK LH FAULT". AFTER LANDING, GOT "LG NO DISPATCH" WITH BRK FAULT MESSAGES. NOTICED HYDRAULIC SYSTEM 1 QUANTITY SHOWED DASHES MOMENTARILY; R & R #2 BCM SLOT 16 MAU#2 IAW AMM32-41-07 SOFTWARE LOAD GOOD.OPS
- [SDR YENA2021020400083](https://openairdocs.org/sdr/YENA2021020400083.md): Warning Message · false activation · Jan 31, 2021 · N247JB · Emb ERJ190100IGW · Central Warning
  > FLIGHT 663, EWR-JAX. AILERON RT HAND FAIL MSG APPEARED AT CRUISE; TROUBLESHOT IAW FIM REFERENCE 27-03-00-810-926-A. PERFORMED RETURN TO SERVICE TEST IAW AMM 27-00-00 AND AILERON RT HAND FAIL MESSAGE CLEARED. NO FURTHER DEFECTS NOTED.
- [SDR YENA201909120525](https://openairdocs.org/sdr/YENA201909120525.md): Power Unit · failed · Sep 12, 2019 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 1979, DCA-FLL. WHILE PERFORMING T/C E190-33-50-01-720-801-AFT. FOUND AFT ELPU 5+6 FAILS FUNCTIONAL TEST; R & R ELPU 5 + 6 IAW AMM 33-50-01. OPS CK OK. A/C OK TO CONT SVC.
- [SDR YENA201902259090](https://openairdocs.org/sdr/YENA201902259090.md): Unknown · odor · Feb 19, 2019 · N247JB · Emb ERJ190100IGW · Air Distribution System
  > FT # 2133, DESCENDING THRU 12K, GOT STRONG JET EXHAUST SMELLING FUMES IN COCKPIT. GOT VERY STRONG SMELLING BOTH PILOTS WENT ON O2. TURNING RECIRCS OFF BRIEFLY HELPED, BUT STRONG FUMES CONTINUED. NO SMELL DETECTED IN CABIN; PER FIM 21-20-00-810-801A & 803A PER
- [SDR YENA2018092090352](https://openairdocs.org/sdr/YENA2018092090352.md): Battery · discharged · Sep 19, 2018 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 2680, EWR-BOS. 2 EACH EMERGENCY LIGHT POWER UNITS FAILED OPERATIONAL TEST. REPLACED 2 EACH EMERGENCY POWER UNITS IAW AMM 33-50-01.
- [SDR YENA2018092090351](https://openairdocs.org/sdr/YENA2018092090351.md): Battery · discharged · Sep 19, 2018 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 2680, EWR-BOS. 2 EACH EMERGENCY LIGHT POWER UNITS FAILED OPERATIONAL TEST. REPLACED 2 EACH EMERGENCY POWER UNITS IAW AMM 33-50-01.
- [SDR YENA201807270935](https://openairdocs.org/sdr/YENA201807270935.md): Skin · damaged · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE ( BASIC 6 CHECK AT SAL) FOR A/C N247JB, WHILE ACCOMPLISHING JACKING PROCEDURES, CREASE DAMAGE WAS A RESULT OF IMPROPERLY FOLLOWING PROCEDURES. THE DAMAGE IS COMMON TO THE REAR FUSELAGE SKIN (P/N 190-61701-003) AT FR 92/FR93 & STR 29L-2
- [SDR YENA2018100970579](https://openairdocs.org/sdr/YENA2018100970579.md): Support Bracket · corroded · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222180 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR76 AND BETWEEN S29R TO S-29L (2EA) ON AFT CARGO COMPARTMENT; REPLACED SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR76 AND BETWEEN S29R TO S29L
- [SDR YENA2018100970578](https://openairdocs.org/sdr/YENA2018100970578.md): Support Bracket · corroded · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222179 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR74 AND S-29L ON AFT CARGO COMPARTMENT; REPLACED SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR74 AND STR29L ON AFT CARGO COMPARTMENT IAW SRM 51
- [SDR YENA2018100970577](https://openairdocs.org/sdr/YENA2018100970577.md): Support Bracket · corroded · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222184 SUPPORT BRACKET FLOOR STRUCTURE AT FR81 ANFD SR-29R ON AFT CARGO COMPARTMENT; REPLACED SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR81 AND S-29R ON AFT CARGO COMPARTMENT IAW SRM 51-40-08.
- [SDR YENA2018100970576](https://openairdocs.org/sdr/YENA2018100970576.md): Support Bracket · corroded · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222183 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S29L-S29R (2EA) ON AFT CARGO COMPARTMENT; REPLACED SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S29L & 29R (2EA) ON AFT
- [SDR YENA2018100970575](https://openairdocs.org/sdr/YENA2018100970575.md): Support Bracket · corroded · Jul 27, 2018 · N247JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF NR 2018-222183 SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S29L TO S29R (2EA) ON AFT CARGO COMPARTMENT; REPLACED SUPPORT BRACKET FLOOR STRUCTURE LOCATED AT FR80 BETWEEN S 29L TO S29R (2EA) O
- [SDR YENA201712131000](https://openairdocs.org/sdr/YENA201712131000.md): Battery Pack · failed · Dec 13, 2017 · N247JB · Emb ERJ190100IGW · Emergency Lighting
  > FT # 1282, RIC-BOS. EMERGENCY LIGHT OVER L1 DOOR INOP; R & R #1 EMERGENCY POWER UNIT PER AMM 33-50-01. OPS CHECK GOOD.

Next page: https://openairdocs.org/deregistered/N247JB-2025-10-23/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 = 'N247JB' AND deregistration_id = 'N247JB-2025-10-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N247JB-2025-10-23/reports

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