# Service difficulty reports: N318JB

A list on [N318JB](https://openairdocs.org/aircraft/N318JB.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 · 89 reports

- [SDR YENA2024072501046](https://openairdocs.org/sdr/YENA2024072501046.md): Shear Tie · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP FR76 STGR 28RH/29RH AT AFT CARGO; REF: TOMX W/ 2563 N/R 00198 SHEAR CLIP WAS REPLACED PER EMB190 SRM 51-41-01 AND SRM 51-41-02.
- [SDR YENA2024072501045](https://openairdocs.org/sdr/YENA2024072501045.md): Rib · cracked · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE: CRACK ON RIB 17 AT FIXED LEADING EDGE LH WING; REF: TOMX W/O 2563 N/R-00106 RIB 17 WAS REPLACED PER EMB190 SRM 51-43-03, SRM 51-43-04 AND SRM 51-41-02.
- [SDR YENA2024072501044](https://openairdocs.org/sdr/YENA2024072501044.md): Beam · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON BEAM BTW FR13 AND Y:250 LH APPROX AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO 2563 NR 00125. BEAM BTW FR13 AND Y:250 LH APPROX AT CABIN FLOOR STRUCTURE (W1) WAS REPLACED PER EMB190 SRM 51-43-03, SRM 51-43-04, SRM 51-40-01
- [SDR YENA2024072501043](https://openairdocs.org/sdr/YENA2024072501043.md): Beam · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON BEAM BTW FR12/14 AND Y:250 RH APPROX AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO 2563 NR 00123. CORROSION AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED PER EMB-190 SRM 51-10-03, SRM 51-12- 01, EVALUATED OUT LIMITS PER EMB 19
- [SDR YENA2024072501042](https://openairdocs.org/sdr/YENA2024072501042.md): Stringer · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION ON STRINGER 29RH AND FASTENERS BTW FR78/81 AND STRG 29R; REF TOMX WO 2563 NR 00205. CORROSION ON STRINGER 29RH BTW FR78/81 AND STRG 29R WAS REMOVED AND EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER EMB 190 SRM 51-12-01,
- [SDR YENA2024072501041](https://openairdocs.org/sdr/YENA2024072501041.md): Skin · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: AFTER REMOVAL STRINGER 29RH CORROSION ON SKIN BTW FR73-74RH WAS FOUND; REF TOMX WO 2563 NR 00273. SKIN BTW STRINGER 29RH FR73-74 WAS REPAIR PER EMB 190 ETI-190-24-211 REV.: 1, ETD2024-190-018554 REV.: /, EC: E-24-895-01. COMPLETED BY:
- [SDR YENA2024072501040](https://openairdocs.org/sdr/YENA2024072501040.md): Skin · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CPCP FINDING: CORROSION ON SKIN BTW FR 73/74 AND STGR 28R/28L AT AFT CARGO; REF TOMX WO 2563 NR 00158. CORROSION ON SKIN BTW FR 73/74 AND STGR 28R/28L AT AFT CARGO WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB 190 SRM 51-12-01, SRM
- [SDR YENA2024072501039](https://openairdocs.org/sdr/YENA2024072501039.md): Doubler · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON DOUBLER RIGHT -COCKPIT FLOOR OVER FR-8/FR-12; "REF TOMX WO 2563 NR 00277. CORROSION ON DOUBLER RIGHT -COCKPIT FLOOR OVER FR-8/FR-12 WAS REMOVED PER EMB 190 SRM 51-10-03, SRM 51-12-01 EVALUATED WITHIN LIMITS PER EMB-190
- [SDR YENA2024072501038](https://openairdocs.org/sdr/YENA2024072501038.md): Crossbeam · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: [CPCP FINDING]: CORROSION IN CROSS BEAM LOCATED BETWEEN Y = - 280.0 AND Y = 280.0 AND FR 11 AT COCKPIT FLOOR STRUCTURE; "REF TOMX WO 2563 NR 00093. NRC 00093: CORROSION IN CROSS BEAM LOCATED BETWEEN Y = - 280.0 AND Y = 280.0 AND FR
- [SDR YENA2024072501037](https://openairdocs.org/sdr/YENA2024072501037.md): Doubler · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: [CPCP FINDING]: CORROSION ON DOUBLER RIGHT/LEFT -COCKPIT FLOOR OVER FR-8/FR-12; "REF TOMX WO 2563 NR 00092. CORROSION ON DOUBLER RIGHT/LEFT -COCKPIT FLOOR OVER FR-8/FR-12 WAS REMOVED PER EMB 190 SRM 51-10-03, SRM 51-12-01 EVALUATED W
- [SDR YENA2024072501036](https://openairdocs.org/sdr/YENA2024072501036.md): Skin · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II & III / FR 73-74 / STGR 28 RH TO 29 LH / LOWER SKIN / CORROSION – PERMANENT REPAIR; REFERENCES: /1/ TOMX ETI-190-24-211 REV 01 /2/ EMBRAER ETD2024-190-018554. DESCRIPTION: AT CURRENT (7/2024) BASIC 6 CHEC
- [SDR YENA2024072501035](https://openairdocs.org/sdr/YENA2024072501035.md): Seat Track · corroded · Jul 24, 2024 · N318JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR STRUCTURE / RH TRACK BTWN FR12-14 AND Y= 300 / CORROSION - PERMANENT REPAIR; REFERENCE: /1/ TOMX ETI-190-24-200 R2 /2/ EMBRAER ETD2024-190-017662 REV. A /3/ ANAC FOR ETD2024-190-017662-A (ATTACHED I
- [SDR YENA2022122301293](https://openairdocs.org/sdr/YENA2022122301293.md): Light · inoperative · Dec 26, 2022 · N318JB · Emb ERJ190100LR · Emergency Lighting
  > FLT#2355, BOS-DCA. 'DURING CABIN CONDITION CHECK, FOUND FORWARD LT PASSAGEWAY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-05. OPS CHECKEDS GOOD. OK FOR SERVICE.
- [SDR YENA2022081200788](https://openairdocs.org/sdr/YENA2022081200788.md): Eicas · fault message · Aug 9, 2022 · N318JB · Emb ERJ170200LR · Door Warning System
  > FLT#1231, BOS-LGA. (REJECTED TO TAKEOFF) 'RTO @ 70KTS DO TO A MASTER WARNING TRIPPLE CLIME " SERVICE DOOR OPEN"; PERFORMED HIGH ENERGY STOP, INSP REF AMM 05-50-12 NO DEFECTS NOTED.'
- [SDR YENA2022081200789](https://openairdocs.org/sdr/YENA2022081200789.md): Eicas · fault message · Aug 8, 2022 · N318JB · Emb ERJ170200LR · Door Warning System
  > FLT#159, BOS-PHL. (REJECT TO TAKEOFF) 'DOOR PAX AFT OPEN INDICATION ON TAKE OFF ROLL, REJECTED TAKE OFF AT 60 KNOTS. RTO DOOR INDICATION INOP ( DOOR POS IND ON MFD & ASSC EICAS-PAX (L1/L2) AND SERVICE (R1/R2)).' (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022081200790](https://openairdocs.org/sdr/YENA2022081200790.md): A/C Pack · dirty · Jul 1, 2022 · N318JB · Emb ERJ170200LR · Passenger/Crew Doors
  > FLT#494, MCO-EWR. 'ON TAXI GOT INTERMITTENT L2 PASSENGER DOOR OPEN INDICATION CYCLED DOOR HANDLES WITH NO EFFECT. ( DOOR POS IND ON MFD & ASSC EICAS-PAX (L1/L2) AND SERVICE (R1/R2)); PERFORMED ADJUSTMENT CHECK OF THE L2 DOOR SENSOR IAW E190 AMM 52-72-21. CHECK
- [SDR YENA2022042900425](https://openairdocs.org/sdr/YENA2022042900425.md): None · none · Apr 27, 2022 · N318JB · Emb ERJ170200LR · Landing Gear/Wheel Fairing
  > FLT#1131, FLL-CHS (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO CHS). 'LG WOW SYS FAIL (AMBER) PERFORMED QRH AND RETURN TO CHS. THE GEAR WOULD NOT RETRACT; INSPECTION OF NLG FOUND THE NITRO SHRADER VALVE DAMAGED. REMOVED AND REPLACED NITRO
- [SDR YENA2021112400787](https://openairdocs.org/sdr/YENA2021112400787.md): Girt Bar · dirty · Nov 23, 2021 · N318JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT 656, MCO-SYR. R2 DOOR WILL NOT DISARM (MULTIPLE WRITE UPS OF THIS CONDITION); CLEANED GIRT ON HOLDS AND REMOVED DEBRIS R2 DOOR CHECKED SERVAL TIMES AND CHECKS GOOD.
- [SDR YENA2021112400786](https://openairdocs.org/sdr/YENA2021112400786.md): Girt Bar · out of alignment · Nov 23, 2021 · N318JB · Emb ERJ190100IGW · Service Doors
  > FLT 495, R2 DOOR WILL NOT DISARM.; SECURED R2 DOOR GIRT BAR IN POSITION ON THE DOOR AND ALIGN THE GIRT BAR BEELCRANKS WITH THE FRAME BELLCRANKS IAW AMM 52-12-41. OPS. CHECK GOOD.
- [SDR YENA2021112400785](https://openairdocs.org/sdr/YENA2021112400785.md): Door · dirty · Nov 23, 2021 · N318JB · Emb ERJ190100IGW · Service Doors
  > FLT 1294, MCO-HPN. R2 DOOR WILL NOT DISARM; CLEANED GIRT ON HOLDS AND REMOVED DEBRIS R2 DOOR CHECKED SERVAL TIMES AND CHECKS GOOD
- [SDR YENA2021113000825](https://openairdocs.org/sdr/YENA2021113000825.md): Skin · dented · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, DENT ON FWD FUSELAGE SKIN BETWEEN FR-10 / FR-11 AND STRG-14LH / STGR 15LH; (RESOLVED ON W/O: 1126567 TASKCARD: NR-00007) REF TOMX 1708-00491; DENT ON FWD FUSELAGE SKIN BETWEEN FR-10 / FR-11 AND STGR-14LH / STGR-15LH WAS MEASURED WI
- [SDR YENA2021113000824](https://openairdocs.org/sdr/YENA2021113000824.md): Skin · dented · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, DENT ON FWD FUSELAGE SKIN BETWEEN FR10-FR 11 STR 14LH / 15LH; REF TOMAX NR 1708-00491, ACCOMPLISHED REPAIR IAW SRM 51-41-01 PAR 6 AND SRM 51-42-02 PAR 6. REPETITIVE INSPECTION ASSIGNED BY FUR E190-53-0174.
- [SDR YENA2021113000823](https://openairdocs.org/sdr/YENA2021113000823.md): Floorbeam · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION(CPCP FINDING RELATED R.C. 53-23-005-0417): CORROSION IN CF III PASSENGER CABIN FLOOR BEAM STRUCTURE LOCATED IN FR 84 FROM Y=400.0 TO Y= 1100.0; SUMMARY OF TOMEX WO 1708 NRC 00412: CFIII PASSENGER CABIN FLOOR BEAM ST
- [SDR YENA2021113000822](https://openairdocs.org/sdr/YENA2021113000822.md): Doubler · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION(CPCP FINDING): CORROSION ON DOUBLER FLOOR STRUCTURE W1 (UNDER FWD. LAVATORY).; SUMMARY OF TOMEX WO 1708 NRC 00371: DOUBLER FLOOR STRUCTURE W1 (UNDER FWD. LAVATORY) WAS REPLACED PER EMB 190 SRM 51-41-02 PAR.4 &PAR.6;
- [SDR YENA2021113000821](https://openairdocs.org/sdr/YENA2021113000821.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000820](https://openairdocs.org/sdr/YENA2021113000820.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000819](https://openairdocs.org/sdr/YENA2021113000819.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000818](https://openairdocs.org/sdr/YENA2021113000818.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000817](https://openairdocs.org/sdr/YENA2021113000817.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000816](https://openairdocs.org/sdr/YENA2021113000816.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, 10 EA. SHEAR CLIPS BETWEEN FR 80-83 AT FOLLOWING STRINGER LOCATIONS 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 10 EA. SHEAR CLIPS REPLACED
- [SDR YENA2021113000815](https://openairdocs.org/sdr/YENA2021113000815.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, 5EA SHEAR CLIPS BETWEEN FR 77-79 AT FOLLOWING STRINGERS: 27-28L;28-29L REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 5EA. SHEAR CLIPS BETWEEN FR 77-79 AT FOLLOWING STRINGER LOCATION
- [SDR YENA2021113000814](https://openairdocs.org/sdr/YENA2021113000814.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, 5EA SHEAR CLIPS BETWEEN FR 77-79 AT FOLLOWING STRINGERS: 27-28L;28-29L REQUIRE REPLACEMENT DUE TO CORROSION BEYOND LIMITS PER EMB 190 SRM 51-12-01;51-10-03;51-75-16.; 5EA. SHEAR CLIPS BETWEEN FR 77-79 AT FOLLOWING STRINGER LOCATION
- [SDR YENA2021113000813](https://openairdocs.org/sdr/YENA2021113000813.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, 4EA. SHEAR CLIPS BETWEEN FR 74-76 AT STRINGERS: 27-28L;28-29L;28-29R REQUIRE REPLACEMENT PER EMB 190 SRM 51-12-01;51-10-03;51-75-16 CORROSION BEYOND LIMITS.; 4EA. SHEAR CLIPS REPLACED DUE TO CORROSION BETWEEN FR 74-76 @ FOLLOWING ST
- [SDR YENA2021113000812](https://openairdocs.org/sdr/YENA2021113000812.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, 4EA. SHEAR CLIPS BETWEEN FR 74-76 AT STRINGERS: 27-28L;28-29L;28-29R REQUIRE REPLACEMENT PER EMB 190 SRM 51-12-01;51-10-03;51-75-16 CORROSION BEYOND LIMITS.; 4EA. SHEAR CLIPS REPLACED DUE TO CORROSION BETWEEN FR 74-76 @ FOLLOWING ST
- [SDR YENA2021113000811](https://openairdocs.org/sdr/YENA2021113000811.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, 4EA. SHEAR CLIPS BETWEEN FR 74-76 AT STRINGERS: 27-28L;28-29L;28-29R REQUIRE REPLACEMENT PER EMB 190 SRM 51-12-01;51-10-03;51-75-16 CORROSION BEYOND LIMITS.; 4EA. SHEAR CLIPS REPLACED DUE TO CORROSION BETWEEN FR 74-76 @ FOLLOWING ST
- [SDR YENA2021113000810](https://openairdocs.org/sdr/YENA2021113000810.md): Floor Support · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP: CORROSION ON FLOOR SUPPORT FR 16 Y=-1150 MM APROX. W1 AREA (UNDER FWD. LAV.); SUMMARY: CORROSION ON FLOOR SUPPORT FR 16 Y=-1150MM W1 AREA (UNDER FWD LAV.) WAS REMOVED AND EVALUATED. FOUND TO BE OUT OF LIMITS
- [SDR YENA2021113000809](https://openairdocs.org/sdr/YENA2021113000809.md): Seat Track · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: (CPCP FINDING RELATED R.C. 53-23-005-0417).CORROSION IN FASTENERS PERIPHERY OF CENTER SEAT TRACK LOCATED @ Y=300 AND BTWN FR 84-85 IN C.F.III PASSENGER CABIN FLOOR STRUCTURE.; SUMMARY: SEAT TRACK LOCATED AT Y=300.0
- [SDR YENA2021113000808](https://openairdocs.org/sdr/YENA2021113000808.md): Stringer · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: INTERGRANULAR CORROSIONAT CF III INTERNAL STRUCTURE LOCATED OVER STRG23L BETWEEN FR 85-86.; REF TOMX WO# 1708 NR# 00431 STRINGER 23L BETWEEN FR 85/FR86 WAS REPAIRAIRED PER EMB190 SRM 53-23-03 REPAIR 51P.
- [SDR YENA2021113000807](https://openairdocs.org/sdr/YENA2021113000807.md): Stringer · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, LATE FINDING: CORROSION ON FUSELAGE INTERNAL STRUCTURE STR 23L FR 90.;REF TOMX WO# 1708 NR# 00594 SECTION OF STRINGER 23LH BTW FR89 TO FR90 WAS REPAIRED PER EMB190 SRM 53-30-03 / REPAIR 51P.
- [SDR YENA2021113000806](https://openairdocs.org/sdr/YENA2021113000806.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CORROSION - LATE FINDING ON SHEAR CLIP AT FRAME 90 BETWEEN STGR 21LH - STGR 23LH; REF TOMX WO# 1708 NR# 00588 SHEARCLIP AT FR90 STRG 21-23LH WAS REPLACED PER EMB190 SRM 51-41-02 AND SRM 51-43-01.
- [SDR YENA2021113000805](https://openairdocs.org/sdr/YENA2021113000805.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION; CORROSION IN SHEAR CLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 86 BETWEEN STGR 27L & 28L; REF; TOMX WO# 1708 NR# 00430 SHEAR CLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 86 BETWEEN STRG 27L AND 28L WAS REP
- [SDR YENA2021113000804](https://openairdocs.org/sdr/YENA2021113000804.md): Stiffener · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: CORROSION IN STIFFENER OF CF III INTERNAL STRUCTURE LOATED BETWEEN FR 86/87 AND BETWEEN STRG 27R-28R; REFERENCE; TOMX WO# 1708 NR# 00427 STIFFENER OF CF III INTERNAL STRUCTURE LOCATED BETWEEN FR 86 / 87 AND BETWE
- [SDR YENA2021113000803](https://openairdocs.org/sdr/YENA2021113000803.md): Stringer · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, SECONDARY NRC IN REF NRC 00427 -CORROSION WAS FOUND OVER STRG 28R BETWEEN FR 86/87 AT CF III INTERNAL STRUCTURE STRINGER 28R BETWEEN FR 86/87 AT CFIII INTERNAL STRUCTURE WAS REPAIRED PER EMB190 SRM 53-23-03 / REPAIR 51P.
- [SDR YENA2021113000802](https://openairdocs.org/sdr/YENA2021113000802.md): Angle · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION; CORROSION IN ANGLE AT CF III INTERNAL STRUCTURE LOCATED BETWEEN FR 85 AND STRG 19L; REFERENCE; TOMX WO# 1708 NR# 00428 ANGLE AT CF III INTERNAL STRUCTURE LOCATED BETWEEN FR 85 STGR 19L WAS REPLACED PER EMB190 SRM
- [SDR YENA2021113000801](https://openairdocs.org/sdr/YENA2021113000801.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION; CORROSION IN SHEAR CLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 84 BETWEEN STRG 27R-28R; REFERENCE TOMX WO# 1708 NR# 00433 SHEARCLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 84 BETWEEN STRG 27R-28R WAS REPL
- [SDR YENA2021113000800](https://openairdocs.org/sdr/YENA2021113000800.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION; CORROSION IN SHEAR CLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 75 BETWEEN STRG 28L/ 29L; REFERENCE TOMX WO# 1708 NR# 00452 SHEARCLIP AT CF III INTERNAL STRUCTURE LOCATED IN FR 75 BETWEEN STRG 28L -29L WAS RE
- [SDR YENA2021113000799](https://openairdocs.org/sdr/YENA2021113000799.md): Shear Tie · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, SECONDARY CORROSION ON SHEAR CLIP AT FR 86 BETWEEN STGR 22LH - STGR 23LH; REFERENCE TOMX WO# 1708 NR# 00524 SHEARCLIP OVER FR86 BETWEEN STGR 22LH - STGR 23LH WAS REPLACED PER EMB-190 SRM 51-41-01 AND SRM 51-41-02 TOMX MX# 201000259 QC
- [SDR YENA2021113000798](https://openairdocs.org/sdr/YENA2021113000798.md): Floor Support · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION: (CPCP FINDING): CORROSION ON DOUBLER FLOOR STRUCTURE W1 (UNDER FWD. LAVATORY).; SUMMARY TOMEX WO 1708 NRC 00371: DOUBLER FLOOR STRUCTURE W1 ( UNDER FWD LAVATORY) WAS REPLACED PER EMB 190 SRM 51-41-02 PAR.4 & PAR.6.
- [SDR YENA2021113000797](https://openairdocs.org/sdr/YENA2021113000797.md): Floorbeam · corroded · Nov 19, 2021 · N318JB · Emb ERJ190100IGW · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, INITIAL INSPECTION(CPCP FINDING RELATED R.C. 53-23-005-0417): CORROSION IN CF III PASSENGER CABIN FLOOR BEAM STRUCTURE LOCATED IN FR 84 FROM Y=400.0 TO Y= 1100.0; SUMMARY OF TOMEX WO 1708 NRC 00412: CFIII PASSENGER CABIN FLOOR BEAM ST
- [SDR YENA201806270929](https://openairdocs.org/sdr/YENA201806270929.md): Skin · cracked · Jun 27, 2018 · N318JB · Emb ERJ190100IGW · Horizontal Stabilizer, Plate/Skin
  > DURING HEAVY MAINTENANCE, A CRACK WAS FOUND ON HORIZONTAL STABILIZER. REFER TO EC E18-512-01. STABILIZERS - HORIZONTAL STABILIZER / LOWER REAR HORIZONTAL SPLICE SKIN (P/N 190-09772-003) / CRACK DAMAGE - TEMPORARY REPAIR; THIS REPAIR IS APPROVED PER REF. /1/ ET

Next page: https://openairdocs.org/aircraft/N318JB/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 = 'N318JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N318JB/reports

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