# Service difficulty reports: N258JB, cancelled Dec 22, 2025

A list on [N258JB, cancelled Dec 22, 2025](https://openairdocs.org/deregistered/N258JB-2025-12-22.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 3 · 101 reports

- [SDR EE4Y2025111423461](https://openairdocs.org/sdr/EE4Y2025111423461.md): Skin · nicked · Nov 14, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, SKIN WITH NICKS WERE FOUND AT FWD FUSELAGE FROM FR18+85MM / FR19+150MM, BTWN STR26L / 27L+80MM. THE NICKS REPORTED EXCEED THE LIMITS FOR NON-SIGNIFICANT DAMAGE AND THE ALLOWABLE DAMAGE PER SRM53-10-01 AD51, DUE TO THEIR LOCATION W
- [SDR EE4Y2025111423448](https://openairdocs.org/sdr/EE4Y2025111423448.md): Skin · damaged · Nov 14, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGESKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE WITH SRM 51-10-03(BLEND-OUT TYPES A AND D). THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-9307
- [SDR EE4Y2025111423446](https://openairdocs.org/sdr/EE4Y2025111423446.md): Skin · damaged · Nov 14, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES WERE FOUND ONTHE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. 3 LSDS WERE REMOVED BY DRILLING THE SKIN. THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-930784 AND DOCUMENTED P
- [SDR EE4Y2025111323455](https://openairdocs.org/sdr/EE4Y2025111323455.md): Skin · dented · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, A DENT WAS IDENTIFIED ON THE CENTER FUSELAGE LOWER SKIN AT FRAME 27 AND BETWEEN STRINGERS 27LH-28RH. ACCORDING TO DOCUMENTATION FROM THE PREVIOUS OPERATOR, THE DENT WAS ASSESSED UNDER REFERENCE ETD2017-190-094601. THE AREA IS C
- [SDR EE4Y2025111323452](https://openairdocs.org/sdr/EE4Y2025111323452.md): Inlet · dented · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Engine Air Intake System
  > DURING THE STRUCTURE INSPECTION, WAS IDENTIFIED AN EXISTING DENTS REPAIR LOCATED ON THE ENGINE NR 2, INLET COWL, INNER BARREL. ACCORDING TO DOCUMENTATION PROVIDED BY THE PREVIOUS OPERATOR, THE REPAIR WAS PERFORMED IN ACCORDANCE WITH CV20-09120. THE CONDITION R
- [SDR EE4Y2025111323451](https://openairdocs.org/sdr/EE4Y2025111323451.md): Inlet · dented · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Engine Air Intake System
  > DURING THE STRUCTURE INSPECTION, WAS IDENTIFIED AN EXISTING DENTS REPAIR LOCATED ON THE ENGINE NR 1, INLET COWL, INNER BARREL. ACCORDING TO DOCUMENTATION PROVIDED BY THE PREVIOUS OPERATOR, THE REPAIR WAS PERFORMED IN ACCORDANCE WITH CV20-09114 REV B. HOWEVER,
- [SDR EE4Y2025111323457](https://openairdocs.org/sdr/EE4Y2025111323457.md): Skin · damaged · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, NICKS WERE FOUND ON THE FUSELAGE SKIN AT FR 26 AND STRINGER 27L. THE DAMAGE WAS REMOVED VIA BLEND-OUT IN ACCORDANCE WITH SRM 51-10-03. THE RESULTING BLENDED AREA WAS EVALUATED PER SRM 53-21-01 AD51 AND DETERMINED TO BE OUT OF LI
- [SDR EE4Y2025111323456](https://openairdocs.org/sdr/EE4Y2025111323456.md): Skin · nicked · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, NICKS WERE IDENTIFIED ON THE FUSELAGE SKIN FROM FR 32 TO FR 32 + 175 MM, BETWEEN STRINGERS 27R AND 28R. THE DAMAGE WAS REMOVED VIA BLEND-OUT IN ACCORDANCE WITH SRM 51-10-03. WHILE MOST OF THE BLENDED AREA WAS CLASSIFIED AS NON-S
- [SDR EE4Y2025111323450](https://openairdocs.org/sdr/EE4Y2025111323450.md): Skin · cracked · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Vertical Stabilizer, Plate/Skin
  > DURING INSPECTION, A CRACK WAS FOUND ON THE LH SKIN PANEL OF THE VERTICAL STABILIZER, LOCATED NEAR THE AFT EDGE JUST BELOW RIB 06. THE AFFECTED AREA FALLS WITHIN A NON-REPAIRABLE ZONE AS DEFINED IN SRM 55-30-01/REPAIR 58P. THE CONDITION REPORTED WAS REPAIRED I
- [SDR EE4Y2025111323449](https://openairdocs.org/sdr/EE4Y2025111323449.md): Skin · damaged · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS FOUND ON THE FUSELAGE SKIN AT FR 97 + 25 MM, STR-27LH, DUE TO ITS PROXIMITY TO THE STRINGER 27L FASTENER ROW, THREE FASTENERS WERE REMOVED. AFTER DAMAGE REMOVAL VIA BLEND-OUT IN ACCORDANCE WITH
- [SDR EE4Y2025111323447](https://openairdocs.org/sdr/EE4Y2025111323447.md): Skin · damaged · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE WITH SRM 51-10-03 (BLEND-OUT TYPES A AND D). THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-93
- [SDR EE4Y2025111323445](https://openairdocs.org/sdr/EE4Y2025111323445.md): Skin · damaged · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. SIX (6) LSDS WERE REMOVED BY DRILLING THE SKIN. THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-930784 AND
- [SDR EE4Y2025111323444](https://openairdocs.org/sdr/EE4Y2025111323444.md): Skin · cracked · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Leading Edge Devices
  > DURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE RH WING LEADING EDGE SKIN CUTOUTBETWEEN RIBS 19 AND 20. THE AFFECTED AREAWAS TRIMMED IN ACCORDANCE WITH SRM 57-49-01 REP51. THE FINAL DIMENSIONS AFTER REWORK EXCEED THE MINIMUM ALLOWABLE LIMITS. THECONDI
- [SDR EE4Y2025111323443](https://openairdocs.org/sdr/EE4Y2025111323443.md): Skin · cracked · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Leading Edge Devices
  > DURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE LH WING LEADING EDGE SKIN CUTOUT BETWEEN RIBS 19 AND 20. THE AFFECTED AREA WAS TRIMMED IN ACCORDANCE WITH SRM 57-49-01 REP 51. HOWEVER, THE FINAL DIMENSIONS AFTER REWORK EXCEED THE MINIMUM ALLOWABLE LIMI
- [SDR EE4Y2025111323442](https://openairdocs.org/sdr/EE4Y2025111323442.md): Skin · damaged · Nov 13, 2025 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, CUSTOMER IDENTIFIED AN EXISTING SKIN REPAIR LOCATED BETWEEN FR23 AND FR24, AND BETWEEN STRINGERS 16L AND 17L. ACCORDING TO DOCUMENTATION PROVIDED BY THE PREVIOUS OPERATOR, THE REPAIR WAS PERFORMED IN ACCORDANCE WITH ETD2014-190-
- [SDR YENA2024103101420](https://openairdocs.org/sdr/YENA2024103101420.md): Battery Pack · no test · Oct 30, 2024 · N258JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE: EMERGENCY LIGHT BATTERY PACK #5 FAILED OPERATIONAL CHECK; REF EAMS WO H9782, NR00001 REPLACED LIGHT BATTERY PACK #5 PER E190 AMM 33-50-01-400-801-A. OPS TEST REF AMM 33-50-00- 710-801-A. TEST PASSED.
- [SDR YENA2023091801107](https://openairdocs.org/sdr/YENA2023091801107.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR 86 TO FR 89 AND Y=250 LH (W2); (RESOLVED ON W/O: 1228947 TASKCARD: NR-00001) CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR 86 TO FR 89 A
- [SDR YENA2023091801106](https://openairdocs.org/sdr/YENA2023091801106.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR12 TO FR13 AND Y = 460 LH (W1); (RESOLVED ON W/O: 1228947 TASKCARD: NR-00003) CORROSION ON FLOOR BEAM BTW FR12 TO FR13 AND Y=460 LH (W1) WAS REMOVED PER EMB-190 SRM 51-12-01, EMB 190 SRM 51-10-03 AND WAS
- [SDR YENA2023091801105](https://openairdocs.org/sdr/YENA2023091801105.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM AT FR 16 AND Y= 280 LH (W1); (RESOLVED ON W/O: 1228947 TASKCARD: NR-00004) CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM AT FR 16 AND Y= 280 LH (W1) WAS REMOVED PER EMB-190 51-12-01, EM
- [SDR YENA2023091801104](https://openairdocs.org/sdr/YENA2023091801104.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: AFTER FASTENERS REMOVAL: CORROSION ON STGR 25LH BTW FR82/83 WAS FOUND; REF TOMX WO 2265 NR# 00234 STRINGER 25LH FROM FR74 TO FR90 WAS REPLACED PER EMB 190 SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03.
- [SDR YENA2023091801103](https://openairdocs.org/sdr/YENA2023091801103.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM, LOCATED BTW FR12 TO FR19 AND Y= 280 RH (W1); EF TOMX WO 2265 NR # 00141 BTW FR13 TO FR14 AND Y= 280 RH (W1) OUT LIMITS PER EMB190 SRM 53-10-10/AD51 THE
- [SDR YENA2023091801102](https://openairdocs.org/sdr/YENA2023091801102.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: JETBLUE CUSTOMER N/R: LAV SERVICE PANEL CUTOUT, FUSELAGE SKIN HAS CORROSION; (RESOLVED ON W/O: 1206076 TASKCARD: NR-00013) SKIN AND DOUBLER OF LAV SERVICE PANEL AREA WERE REPAIRED PER EMB-190 SRM 53-23-60 REPAIR 51. ALL WORK ACCOMPLI
- [SDR YENA2023091801101](https://openairdocs.org/sdr/YENA2023091801101.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Horizontal Stabilizer Structure
  > DURING HEAVY MAINTENANCE: AFTER RH ELEVATOR BEARING REMOVAL FROM HINGE, FITTING #2 WAS FOUND CORROSION IN HOUSING; REPLACED HOUSING AT RH ELEVATOR HINGE FITTING #2 PER EMB-190 SRM 51-43-03. REF TOMX NR 0323.
- [SDR YENA2023091801100](https://openairdocs.org/sdr/YENA2023091801100.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Nacelle/Pylon Structure
  > DURING HEAVY MAINTENANCE: REPLACE THE INBOARD AND OUTBOARD SPAR AT THE RH PYLON DUE TO AFT LUG CORROSION; REF TOMX W/O 2265 NR00306: INBD AND OUTBD SPARS AT RH PYLON WERE REPLACED PER EMB-190 SRM 51-43-03, 51-43-04, EMBRAER ANNEX A SPAR REPLACEMENT PROCEDURE R
- [SDR YENA2023091801099](https://openairdocs.org/sdr/YENA2023091801099.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Nacelle/Pylon Structure
  > DURING HEAVY MAINTENANCE: REPLACE THE INBOARD AND OUTBOARD SPAR AT THE LH PYLON DUE TO AFT LUG CORROSION; REF TOMX W/O 2265 NR00305: INBD AND OUTBD SPARS AT LH PYLON WERE REPLACED PER EMB-190 SRM 51-43-03, 51-43-04, EMBRAER ANNEX A SPAR REPLACEMENT PROCEDURE R
- [SDR YENA2023091801098](https://openairdocs.org/sdr/YENA2023091801098.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: MAJOR REPAIR: REPLACE THE EXISTING REPAIR DOUBLER IN LH WING THAT INTERFERES WITH THE INSTALLATION OF SB190-57-0056, LH WING REAR LOWER SKIN PANEL REINFORCEMENTS; REF TOMX W/O NR-00318: REPAIRED INTERFERENCE BETWEEN EXISTING REPAIR DO
- [SDR YENA2023091801097](https://openairdocs.org/sdr/YENA2023091801097.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM, LOCATED BTW FR12 TO FR19 AND Y= 280 RH (W1); REF TOMX WO 2265 NR # 00141 BTW FR13 TO FR14 AND Y= 280 RH (W1) OUT LIMITS PER EMB190 SRM 53-10-10/AD51 TH
- [SDR YENA2023091801096](https://openairdocs.org/sdr/YENA2023091801096.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: WINGS / RH & LH WING / FWD LWR SKINS / SB IMPLEMENTATION / FWD FITTINGS / BOLT INSTALLATION / WASHER DEVIATION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801095](https://openairdocs.org/sdr/YENA2023091801095.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / LOWER SKIN PANEL SB APPLICATION / DISCREPANT FASTENER - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801094](https://openairdocs.org/sdr/YENA2023091801094.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: WINGS / LH WING / LOWER SKIN PANEL BETWEEN RIB 9-10 / EXISTING REPAIR & SB 57-0056 DOUBLER INTERFERENCE - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801093](https://openairdocs.org/sdr/YENA2023091801093.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE AT FR 13-14 AND Y= 280 RH / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801092](https://openairdocs.org/sdr/YENA2023091801092.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 88 / BETWEEN STRINGER 27R AND 28R / EXISTING MISDRILLED HOLE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801091](https://openairdocs.org/sdr/YENA2023091801091.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: WINGS / LH AND RH WING / REAR LOWER SKINS / SB 190-57-0056 / REPAIR WASHER INSTALLATION - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023091801090](https://openairdocs.org/sdr/YENA2023091801090.md): Unknown · unknown · Sep 13, 2023 · N258JB · Emb ERJ190100IGW · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: WINGS / RH WING / WING MAIN BOX / LOWER SKIN PANEL SB APPLICATION / DISCREPANT FASTENER - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023011300039](https://openairdocs.org/sdr/YENA2023011300039.md): Hinge Pin · out of position · Jan 10, 2023 · N258JB · Emb ERJ190100IGW · Fuselage, Door Hinge
  > FLT#23, DCA-MCO. 'COCKPIT DOOR HINGE PIN POPPED OUT OF POSITION; REPLACED COCKPIT DOOR LOWER HINGE AND ADJUSTED COCKPIT DOOR IAW AMM 52-51-01. A/C OK FOR SERVICE.'
- [SDR YENA202301040011](https://openairdocs.org/sdr/YENA202301040011.md): Pressure Switch · faulted · Dec 26, 2022 · N258JB · Emb ERJ190100IGW · Engine Bleed Air System
  > FLT 726, BWI - BOS. AIRCRAFT PERFORMED AN AIR TURN BACK TO BWI, BLEED 1 OVERPRESSURE MSG APPEARED ON CLIMB AFTER TAKEOFF. RAN QRH PROCD, MSG RETURNED. DISPATCH ADVISED RETURN TO BWI; ACCOMPLISHED FIM TASK 36 14 00 810 867A. REMOVED AND REPLACED LH BLEED OVER
- [SDR YENA2022121901269](https://openairdocs.org/sdr/YENA2022121901269.md): A/C Pack · odor · Dec 16, 2022 · N258JB · Emb ERJ190100LR · Cabin Cooling System
  > FLT 1182, RIC-BOS. ODOR OF EXHAUST IN FLIGHT DECK ONLY. DURING THE LAST PART OF THE CLIMB, CRUISE, AND DESCENT. MILD, EXHAUST SMELL THROUGH FLIGHT DECK VENTS WOULD COME AND GO DURING WAVES. OVERALL LASTING ABOUT 30 MINUTES. WHEN PACK 1 WAS TURNED OFF THE ODOR
- [SDR YENA2022081200793](https://openairdocs.org/sdr/YENA2022081200793.md): A/C Pack · dirty · Aug 8, 2022 · N258JB · Emb ERJ170200LR · Air Distribution Fan
  > FLT#2028, MCO-EWR. 'ODOR DIRTY SOCKS DETECTED ON TAKE-OFF ROLL LEVEL 1 DURATION OF 5 MINUTES MODERATE INTENSITY DETECTED IN COCKPIT ONLY NO REPORT OF ODOR FROM FLIGHT ATTENDANTS SUSPECTED SUSPECTED SOURCE IS AIR SUPPLY VENTS APU WAS OFF; PERFORMED PACK BURN PE
- [SDR YENA2022021400062](https://openairdocs.org/sdr/YENA2022021400062.md): None · failed · Feb 13, 2022 · N258JB · Emb ERJ190100IGW · Engine Indicating System
  > FLT # 733, MCO-SJU (AIRTURN BACK TO MCO). CLIMBING THROUGH FL230 ENG 2 LP VIBRATION WAS 4.1 FOLLOWED QRH PROCEDURE; PER FIM 77-31-00-810-816A R/R EVM MODULE PER AMM 77-31-01. BITE CK GOOD.
- [SDR YENA2020120700565](https://openairdocs.org/sdr/YENA2020120700565.md): Power Supply · failed · Dec 1, 2020 · N258JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 932, IAH-BOS. EMERGENCY LIGHT AT CEILING PANEL 11 INOPERABLE. R & R EMERGENCY LIGHT POWER UNIT NR 6, IAW AMM 33-50-01. OPERATIONS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR YENA2020090800453](https://openairdocs.org/sdr/YENA2020090800453.md): Battery · failed · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT POWER UNIT AT MID CABIN P/N 3400-22-10 S/N 001995 IN PASSENGER CABIN. RESOLVED ON W/O: 1050580 TASKCARD: NR-00009. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT AT MID CABIN, IAW 3190 AMM 33-50-01-000-80
- [SDR YENA2020090800452](https://openairdocs.org/sdr/YENA2020090800452.md): Light · inoperative · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE EXTERNAL SKIN LT FWD EMERGENCY LIGHT ON UPPER FUSELAGE (1EA). R & R FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY LT SIDE, IAW E190 AMM 33-50-25-000-802-A AND E190 AMM 33-50-25-400-802-A. PERFORMED OPERATIONAL TEST EXTERNAL EMERG
- [SDR YENA2020090800451](https://openairdocs.org/sdr/YENA2020090800451.md): Skin · corroded · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Aerodynamic Fairings
  > DURING HEAVY MAINTENANCE, CORROSION INTERNAL SKIN ON ACCESS PANEL 351GL IN TAIL COMPARTMENT. ACCOMPLISHED REPAIR OF CORROSION DAMAGE FOUND ON THE TAIL CONE ( S/N: 0200001, P/N 170-50005-421) APU BAY FWD ACCESS PANEL 351GL IN ACCORDANCE WITH EA 53-0571-20 COVE
- [SDR YENA2020090800450](https://openairdocs.org/sdr/YENA2020090800450.md): Skin · damaged · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR 96 TO FR 97 AT STGR 23R LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR96 TO FR97 AT LEVEL STGR 23R LOWER FUSELAGE, IAW E190 SRM 53-30-01, REPAIR 63, ITEM
- [SDR YENA2020090800449](https://openairdocs.org/sdr/YENA2020090800449.md): Skin · dented · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE DENT EXTERNAL SKIN FR 96 TO FR 97 AT LEVEL STR23L LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR96 TO FR97 AT LEVEL STGR 23L LOWER FUSELAGE, IAW E190 SRM 53-30-01, REPAIR 63, ITEM 5. DETAILED VISUAL INSPECTIO
- [SDR YENA2020090800448](https://openairdocs.org/sdr/YENA2020090800448.md): Rib · cracked · Sep 4, 2020 · N258JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, CRACK RIB 10 WING MAIN BOX LOWER SKIN SPAR 2 TRAILING EDGE RT WING. PERFORMED PERMANENT REPAIR ON RIB 10 WING MAIN BOX LOWER SKIN SPAR 2 TRAILING EDGE RT WING IAW E190 SRM 57-10-01, REPAIR 54 ITEM 9 FIGURE 201 SHEET 6. NO FURTHER AC
- [SDR YENA201809220942](https://openairdocs.org/sdr/YENA201809220942.md): Skin · cracked · Sep 22, 2018 · N258JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, B6 CHECK AT (SAL), A CRACK (LENGTH: 2.627 INCHES) WAS FOUND ON LT WING REAR LOWER SKIN (P/N 190-33065-013) AT RIB 10+1". SEE THE REF /1/ EA FOR MORE DETAILS. THE DAMAGE IS FOUND TO BE OUTSIDE OF REF /3/ SRM LIMITS. THEREFORE, CONTACTE
- [SDR YENA2018092620359](https://openairdocs.org/sdr/YENA2018092620359.md): Structure · corroded · Sep 22, 2018 · N258JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR TIE FLOOR STRUCTURE AT FR 76 BTWN STR 28R TO STR 29R ON AFT CARGO COMPARTMENT; REPLACED SHEAR TIE FLOOR STRUCTURE LOCATED AT LEVEL FR 76 BTWN STR 28R TO STR 29R ON AFT CARGO COMPARTMENT. IAW E190 SRM-
- [SDR YENA201708260704](https://openairdocs.org/sdr/YENA201708260704.md): Mount · damaged · Aug 26, 2017 · N258JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT 1479, DCA-FLL. FOUND AFT ESCAPE DOOR SLIDE BUSTLE BRACKET DAMAGED(AFT). REMOVE SLIDE FOR REPAIR, REPLACED SHOCK MOUNT ON SLIDE AND REINSTALLED SLIDE ASSY IAW 25-65-01. ALL CHECKS NORMAL.
- [SDR YENA20160620569](https://openairdocs.org/sdr/YENA20160620569.md): Panel Support · corroded · Jun 20, 2016 · N258JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT AT FRAME 90, RBL 42". R & R RT PANEL SUPPORT IAW SRM 51-42-01 & 51-43-03.

Next page: https://openairdocs.org/deregistered/N258JB-2025-12-22/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 = 'N258JB' AND deregistration_id = 'N258JB-2025-12-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N258JB-2025-12-22/reports

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