N304JB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
77 reports on file, 2009-11-08 – 2026-03-09.
Part: SKIN — CRACKED (ZONE 500) · airframe 39,175 hrs · 26,111 cycles
CRACKS (2EA) AND ONE ELONGATED HOE WERE FOUND AFFECTING THE LH WING LOWER SKIN AFT SPAR 2 BTWN RIB 10/11. SRM PART II 57-10-01 REP. 54 WAS EVALUATED. THE CRACK #1 IS NOT REPAIRABLE DUE TO THE LOCATION OF THE CRACK AND CRACK #2 IS REPAIRABLE PER SRM AND THE ELONGATED IS REPAIRABLE PER SRM (FREEZE PLUG). THE CUSTOMER REQUIRES TO REPAIR IAW ETD2023-190-008554 REV. B DTD APR 02 2023. JOB A1Q328 ITEM 21-31.
Part: SKIN — DAMAGED (ZONE 100) · airframe 39,175 hrs · 26,111 cycles
CUSTOMER REPORTS TWO LIGHTNING STRIKE DAMAGES AFFECTING THE CENTER FUSELAGE I SKIN, LOCATED AT FR33 + 242 MM (DAMAGE #1) AND FR33 + 394 MM (DAMAGE #2) ON STR 26L. DAMAGE #1 WAS COMPLETELY REMOVED BY BLEND-OUT. DAMAGE #2, DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, SO IT WAS REMOVED BY DRILLING A HOLE THROUGH THE SKIN. THE BLEND-OUT AREA (DAMAGE #1) WAS EVALUATED PER SRM 53-21-01 AD51 AND FOUND TO BE OUT OF LIMITS, AS IT IS LOCATED IN A NON-PERMISSIBLE ZONE (GREY AREA) AND EXCEEDS 10% OF THE SKIN THICKNESS. THIS CONDITION REPORTEDWAS REPAIRED IAW ETD2026-190-001960 DTD JAN 31 2026 AND DOCUMENTED UNDER COOPESA EOCOO-EO-2026-23835-R00. JOB A1Q328 ITEN 21-7
Part: SKIN — DAMAGED (ZONE 100) · airframe 39,175 hrs · 26,111 cycles
DURING THE STRUCTURAL INSPECTION, DAMAGE CAUSED BY A LIGHTNING STRIKE WAS FOUND ON THE EXTERNAL SKIN OF THE CENTER FUSELAGE I, AT FR24 + 327MM, STR-27LH + 8MM. AFTER PERFORMING A LIGHT BLEND-OUT, IT WAS DETERMINED THAT IN A POINT, THE DAMAGE EXCEEDED 50% OF THE SKIN THICKNESS. THE AFFECTED AREA WAS REMOVED BY DRILLING A 2.38MM HOLE THROUGH THE SKIN ONLY. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2026-190-001780 DTD FEB 03 2026 AND DOCUMENTED UNDER COOPESA EOCOO-EO-2026-23843-R00. JOB A1Q328 ITEN 21-5
Part: SKIN — DAMAGED (ZONE 100) · airframe 39,175 hrs · 26,111 cycles
WAS REPORTED THAT DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR32 AND JUST ABOVE STR-26LH. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT EXCEEDS THE LIMITS SPECIFIED IN SRM 53-21-01 AD51. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2026-190-001983 DTD FEB 02 2026 AND DOCUMENTED UNDER COOPESA EO COO-EO-2026-23839-R00. JOB A1Q328 ITEN 21-2
Part: SKIN — DAMAGED (ZONE 100) · airframe 39,175 hrs · 26,111 cycles
DURING THE STRUCTURAL INSPECTION, AN EXISTING BLEND-OUT WAS FOUND IN THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 86-87 AND STRINGERS 27R-28R. SINCE NO PREVIOUS RECORD OF THIS BLEND-OUT EXISTS, IT WAS INSPECTED AND EVALUATED. THE CONDITION WAS FOUND TO BE OUTSIDE THE LIMITS DEFINED IN SRM 53-23-01/AD51, AS THE BLEND DEPTH EXCEEDS 10% OF THE SKIN THICKNESS. THE MINIMUM REMAINING THICKNESS IS 1.35MM (15.62% THICKNESS REDUCTION) WHERE THE NOMINAL THICKNESS IS 1.6MM. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2026-190-001937 REV. A DTD FEB 02 2026 AND DOCUMENTED UNDER COOPESA EO COO-EO-2026-23836-R00. JOB A1Q328 ITEM 21-19
Part: DOUBLER — MISINSTALLED (ZONE 200) · airframe 39,175 hrs · 26,111 cycles
DURING STRUCTURAL INSPECTION, THE CUSTOMER FOUND AN EXTERNAL REPAIR DOUBLER AT FR74 + 105 MM AND STR 24L + 85 MM, REPORTEDLY INSTALLED IN ACCORDANCE WITH EMB IC2009-190/05358C DATED 09-JUL-2009. ONCE THE AVAILABLE DOCUMENTATION LACKED ESSENTIAL INFORMATION, THE REPAIR WAS REMOVED, EXPOSING AN EXISTING SKIN CUTOUT BENEATH THE DOUBLER. A NEW REPAIR WAS ATTEMPTED FOLLOWING SRM 53-23-01, REPAIR 62, BUT THE REQUIRED DOUBLER FOOTPRINT EXTENDED INTO THE NONREPAIRABLE âGREY ZONEâ IDENTIFIED IN FIGURE 205 OF SRM 53-23-01. TO RESOLVE THIS, A NEW REPAIR SKETCH WAS DEVELOPED USING THE CRITERIA OF SRM 53-23-01 AND SRM II 51-75-00, APPLYING THE âNO-FINGERâ METHOD DEFINED IN SRM 51-75-17. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2026-190-001344 DTD JAN 27 2026 AND DOCUMENTED UNDER COOPESA EO COO-EO-2026-23824-R00. JOB A1Q328 ITEM 21-30
Part: RIB — CORRODED (ZONE 500) · airframe 39,175 hrs · 26,111 cycles
DURING A STRUCTURAL INSPECTION, CORROSION WAS FOUND AT A FASTENER HOLE LOCATED ON THE LH WINGLET LOWER SURFACE, AT THE SUPPORT STRUCTURE OF ACCESS PANEL 551AB, SEE FIGURE 1 FOR DAMAGE OVERVIEW. THE AFFECTED FASTENER HOLE INVOLVES BOTH THE WING SPAR II AND WINGLET RIB 1 FLANGES. ALL CORROSION WAS REMOVED BY REAMING THE FASTENER HOLE (INCREASING ITS DIAMETER). AFTER REMOVAL, THE FINAL HOLE DIAMETER MEASURED 9.80 MM. THIS CONDITION REPORTEDWAS REPAIRED IAW ETD2026-190-001038 REV. A DTD JAN 29 2026 AND DOCUMENTED UNDER COOPESA EO COO-EO-2026-23831-R00. JOB A1Q328 ITEM 5-41
Part: SKIN — DAMAGED (ZONE 100) · airframe 39,175 hrs · 26,111 cycles
CUSTOMER REPORTS LIGHTNING STRIKE DAMAGE AFFECTING THE CENTER FUSELAGE III SKIN, LOCATED AT FR74 AND STR 28L. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT IS OUTSIDE THE LIMITS SPECIFIED IN SRM 53-23-01 AD51. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2026-190-001961 DTD JAN 31 2026 AND DOCUMENTED UNDER COOPESA EO COO-EO-2026-23837-R00. JOB A1Q328 ITEN 21-11
Earlier reports · 2009–2023 · 69 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,556 hrs · 24,150 cycles
DURING HEAVY MAINTENANCE: LH WING TE AREA, LOWER SKIN HAS 2 EACH CRACK O/B PYLON; REF: TOMX W/O 2191 NR-00014 REPAIRED PER ETI-190-23-535 REV 3 AND ETD-2023-190-008554 REV B. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. TOMX MECH 10000726 INSP 325718.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,556 hrs · 24,150 cycles
DURING HEAVY MAINTENANCE: WINGS/ LH WING MAIN BOX / TRAILING EDGE LOWER SKIN AT AFT SPAR 2 BETWEEN RIB 10 AND RIB 11/ CRACK AND ELONGATED HOLES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
2022
Part: FINGER DOUBLER — CORRODED · corrosion level 2 · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR79/80, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. REMOVED AND REPLACED FINGER PLATE PER EMB 190 SRM 51-12-01, 51-10-01, 53-23-11/AD53, 51-43-01, AND 51-43-02. WORK ACCOMPLISHED ON TOMX NR 00210. (SUPPLEMENTAL ADDED TO STRUCTURE CAUSING DIFFICULTY).
Part: SEAL REST — CORRODED · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, CORROSION ON LOWER FORWARD SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FWD SEAL REST PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/AD52 AND 51-40-08. WORK ACCOMPLISHED ON TOMX NR 00206. (SUPPLEMENTAL INFORMATION TO STRUCTURE CAUSING DIFFICULTY).
Part: SKIN — CORRODED · corrosion level 2 · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, CORROSION ON INTERNAL SKIN BTW FR86/FR87 AND STGR 29L/28L; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. PER EMB 190 SRM 53-23-01/ADS51. PERFORMED REPAIR PER EC E22-324-01, ETI 190-22-561 REV 6 AND EDT2022-190-015055 REVD. WORK ACCOMPLISHED ON TOMX NR 00411.
Part: SKIN — CORRODED · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, FUSELAGE / CENTER FUSELAGE III / LOWER SKIN / BTW FR86 - FR87 AND STGR 29LH - 29RH / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR).
Part: FINGER DOUBLER — CORRODED · corrosion level 2 · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR77/78, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. REMOVED AND REPLACED FINGER PLATE PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/ AD53, 51-43-01 AND 51-43-02. WORK ACCOMPLISHED ON TOMX NR 00209. (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION).
Part: SEAL REST — CORRODED · corrosion level 2 · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, CORROSION ON LWR CENTRAL SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION, EVALUATED AND FOUND OUT OF LIMITS. REMOVED AND REPLACED CENTRAL SEAL REST PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/AD52 AND 51-41-01. WORK ACCOMPLISHED ON TOMX NR 00207.
Part: SKIN — DAMAGED · airframe 34,537 hrs · 22,733 cycles
DURING HEAVY MAINTENANCE, PROTUBERANCE EXTERNAL SKIN FR 30-31 STR 26-27; MAJOR REPAIR REF TOMX NR 1894-00330 - EVALUATED AND REPAIRED PROTUBERANCE IAW EMB 190 SRM 53-21-01/AD52, SRM 53-21-01/R62P, 51-75-13 PAR. 5 AND SRM 51-75-00F.
Part: CONTROLLER — FAILED (SPDA-2) · airframe 34,341 hrs · 22,598 cycles
FLT#384, MCO-MCO.'BLEED 2 LEAK CLIMBING THROUGH FL 290; PER FIM 36-21-00-810-804-A PERFORMED BLEED LEAK CHECK ON ENG #2 NO LEAK NOTED INSPECTION ODS LOOP ELECTRICAL CONNECTOR NO FOUND CONTAMINATION AND FAILURE NEXT STEP REMOVED AND REPLACED AMS CONTROLLER PROCESSOR BOARD ON SLOT 18 IAW E190 AMM 21-00-01-000-801-A. NO FAULT NOTED AT THIS TIME.'
2021
Part: CLAMP — MIGRATED · airframe 33,832 hrs · 22,261 cycles
FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTACT WITH PYLON STRUCTURE. PERFORMED ESPM REPAIR 20-41-20ON PIGTAIL AND RESECURED CLAMP AS REQUIRED. FOUND FAULTED ISOLATOR AT EVENT LOCATION 25. SECURED AS REQUIRED AND VERIFIED BOTH CHANNELS ARE NOW CLEAR. PERFORMED SATIFACTORY OPS CHECK OF BLEED 2 SYS IAW AMM 36-11-00.
Part: CLAMP — MIGRATED · airframe 33,832 hrs · 22,261 cycles
FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTACT WITH PYLON STRUCTURE. PERFORMED ESPM REPAIR 20-41-20ON PIGTAIL AND RESECURED CLAMP AS REQUIRED. FOUND FAULTED ISOLATOR AT EVENT LOCATION 25. SECURED AS REQUIRED AND VERIFIED BOTH CHANNELS ARE NOW CLEAR. PERFORMED SATIFACTORY OPS CHECK OF BLEED 2 SYS IAW AMM 36-11-00.
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 32,046 hrs · 21,110 cycles
DURING HEAVY MAINTENANCE, ELPU NR 2 FAILED OPERATIONS CHECK. R & R ELPU NR 2, IAW AMM 33-50-01-000-801-A AND 33-50-01-801-A. REF TO MX NR 00033.
2019
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 29,775 hrs · 19,457 cycles
FT # 2167, RH AFT OVERWING EMERGENCY LIGHT INOP; REMOVED AND REPLACED ELPSU # 4 IAW AMM 33-50-01 OPS CHECK NORMAL.
Part: REPAIR — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 28,344 hrs · 18,480 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON (141-57) CENTER FUSELAGE III FLOOR STRUCTURE, CORROSION FOUND ON PREVIOUS SEAT TRACK REPAIR BTW FR 84-85 AND LBL 11''; REF NRC 4000173-2000-0173, SEAT TRACK REPAIR BTW FR 84-85 AND LBL11'' IAW SRM II 53-23-10, REPAIR 54, NO FURTHER ACTION REQUIRED, EC E14-349-01 APPLIED FOR ID PURPOSE.
2018
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 26,363 hrs · 16,986 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA MIDDLE SHEAR PANEL AT FRAME 87 - 88. REPLACED THE SHEAR PANEL IAW SRM IAW 51-42-01, AND 51-42-03, REV 37.
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 26,363 hrs · 16,986 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA FLOOR PANEL CORRODED AT FRAME 78. REPLACED THE FLOOR PANEL IAW SRM 51-42-01, AND 51-42-03.
2017
Part: PUMP — FAILED (HYD SYSTEM) · airframe 14,663 hrs · 23,172 cycles
FLIGHT CREW REPORTED EDP 2 FAIL FOLLOWED BY COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM. DIVERTED. EMERGENCY DECLARED. REPLACED NR 2 ENGINE EDP HYDRAULIC PUMP IAW AMM 29-11-01. PERFORMED OPS CHECK. OPS CHECK TEST PASSED.
2016
Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LOWER SKIN FRAME 88 BET STRG 27R-28R SHEAR CLIP. REF EAMS NR 00413; REPLACED SHEAR CLIP IAW SRM 51-41-01, 51-41-02.
Part: SUPPORT — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR87, LBL 44". REF EAMS NR 00179; REMOVED CORROSION AND REPLACED LT SUPPORT PANEL, REF SRM 51-10-03 AND SRM 51-75-16.
Part: STRUCTURE — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 8" AFT FR17, 49.5" RBL, REF EAMS NR 00217, REPLACED RT AFT SILL, REF SRM 51-41-02.
Part: SEAT TRACK — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK FR 87, RBL 12. SEAT TRACK REPLACED IAW SRM 51-41-01, 51-42-01, AND 51-43-03.
Part: STRUCTURE — CORRODED (FRAME 13) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON FWD RT SILL 8" AFT FR13, 49" RBL. REF EAMS NR 00209. REPLACED SILL. REF SRM 51-41-02.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FRAME 84, RBL 12", CORROSION WAS REMOVED. NEW DOUBLER WAS FABRICATED AND INSTALLED.
Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LOWER SKIN FRAME 87, BETWEEN STRG 27R-28R SHEAR CLIP. REF EAMS NR 00415; REPLACED SHEAR CLIP. REF SRM 51-41-01, 51-41-02.
Part: STRUCTURE — CORRODED (FRAME 20) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 20 49" RBL. UAW EAMS NR 00221. REPLACED SILL REF SRM 51-41-02.
Part: STRUCTURE — CORRODED (FRAME 18) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 2" AFT FRAME 18, 49" RBL; REPLACED AFT RT SILL IAW SRM 51-41-02.
Part: SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 89, RBL 43"; REPLACED PANEL SUPPORT. REF SRM 51-41-02, 51-43-01.
Part: FRAME — CORRODED (FRM 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON FR 17, 7" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES REF E16-346-01.
Part: FRAME — CORRODED (FRM 14) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK BS, CORROSION WAS FOUND ON FRAME 14 RBL 23"; CORROSION WAS R & R DOUBLERS WERE INSTALLED.
Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT CARGO LWR SKIN FR82 BET STGR 27R-28R, SHEAR CLIP. REF EAMS NR 00405; REPLACED SHEAR CLIP REF SRM 51-41-01, 51-41-02.
Part: STRUCTURE — CORRODED (FRAME 12) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FWD RT SILL 5.5" AFT FRAME 12, 37.5" RBL. REF EAMS NR 00206, REPLACED FWD RT SILL REF SRM 51-41-02.
Part: DOUBLER — CORRODED (FRAME 15) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, FWD LT DOUBLER 6" AFT FR15, 13.5 LBL WAS FOUND TO BE CORRODED; R & R DOUBLER. TREATED NEW DOUBLER IAW SRM 53-10-10.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT SHEAR PANEL FR87, LBL 19"; REMOVED CORROSION. REPLACED SHEAR PANEL. INSTALLED AND TOP COATED NEW PANEL SUPPORT REF SRM 51-10-03.
Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FRAME 84, RBL 24", REPLACED PANEL REF SRM 51-41-02, 51-43-04.
Part: FLOOR SUPPORT — CORRODED (FRAME 15) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT 6" AFT FRAME 15, 45" LBL. REF EAMS NR 00199. REPLACED FLOOR SUPPORT. REF SRM 51-43-03.
Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 84, RBL 42". REF EAMS NR 00193. REPLACED PANEL REF SRM 51-41-02, 51-43-04.
Part: SEAT TRACK — CORRODED (FRAME 13) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON RT SEAT TRACK AT THE GALLEY MOUNT BETWEEN FRAMES 13-14 IN THE FWD CABIN. CORROSION WAS R & R WITH A DOUBLER/STRAP AND FILLER INSTALLATION.
Part: STRUCTURE — CORRODED (FRAME 13) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON FWD RH SILL 2" AFT FR13, 49" RBL, REPLACED FWD RT SILL REF SRM 51-41-02.
Part: SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR90, LBL 42". REPLACED PANEL SUPPORT REF SRM 51-41-01, 5141-02, 51-42-02, 51-43-03.
Part: FRAME — CORRODED (FRM 14) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 14 RBL 15.5; CORROSION WAS REMOVED AND REPAIRED DOUBLERS WERE INSTALLED.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA CENTER SHEAR PANEL 5" AFT FR87, LBL 4"; REPLACED CENTER SHEAR PANEL. REF SRM 51-42-01, 51-23-06.
Part: SHEAR TIE — CORRODED (FRAME 81) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT CARGO LOWER SKIN FRAME 81 BETWEEN STR 27R-28R, SHEAR CLIP, REF EAMS NR 00401. REPLACED SHEAR CLIP. REF SRM 51-41-01, 51-41-02.
Part: STRUCTURE — CORRODED (FRAME 18) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 11" AFT FRAME 18, RBL 49". REF EAMS NR 00219, REPLACED SILL, REF SRM 51-41-02.
Part: STRUCTURE — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 17, 48" RBL. REF EAMS NR 00216, REPLACED AFT RT SILL REF SRM 51-41-02.
Part: FRAME — CORRODED (FRM 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON FRAME 17, 8" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES, REF E16-346-01.
Part: STRUCTURE — CORRODED (FRAME 19) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 13.5" AFT, FR19, 49" RBL. REF EAMS NR 00220. REPLACED SILL REF SRM 51-41-02.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, AFT WET AREA RT SHEAR PANEL 5" AFT OF FRAME 87; RBL 24 WAS FOUND TO BE CORRODED; REPLACED SHEAR PANEL. REF EAMS NRS H4955- 00184 AND 00183, SRM REF 51-42-01 .
Part: FRAME — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 17, RBL 8.5"; CORROSION WAS REMOVED AND 2 L SHAPED REINFORCEMENT ANGLES WERE INSTALLED, REF E16-346-01.
Part: STRUCTURE — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL FRAME 17, 42.5" RBL. REF EAMS NR 00215, REPLACED SILL. REF SRM 51-42-01.
Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SUPPORT PANEL FR 84, RBL 24". REF EAMS NR 00192, REPLACED PANEL. REF SRM 51-41-02, 51-42-02, 51-43-04, 51-23-06.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, CORROSION WAS FOUND ON AFT WET AREA LT SHEAR PANEL FRAME 87, LBL 13. REMOVED CORROSION AND REPLACED IAW EAMS NR 00176, AND SRM 51-10-03.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, CORROSION WAS FOUND ON AFT WET AREA LT SHEAR PANEL FRAME 87, LBL 29. IAW EAMS NR 00174; REMOVED CORROSION. SHEAR PANEL REPLACED. INSTALLED AND TOP COATED NEW PANEL SUPPORT, IAW SRM 51-10-03.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FR84, RBL 10". REFERENCE EAMS NR 00187, CORROSION WAS REMOVED. NEW DOUBLER WAS FABRICATED AND INSTALLED.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT GUSSET PLATE FR 90, RBL 24, REPLACED GUSSET IAW SRM 51-41-02.
Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT CARGO LWR SKIN FR76, BETWEEN STGR 28L AND 29L, SHEAR CLIP, REF EAMS NR 00398; REPLACED SHEAR CLIP. REF SRM 51-41-01, 51-41-02.
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, AFT WET AREA RIGHT SHEAR PANEL 5" AFT OF FR87; RBL 37 WAS FOUND TO BE CORRODED. REPLACED SHEAR PANEL. IAW EAMS NRS H4955- 00184 AND 00183, SRM 51-42-01 .
Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,081 hrs · 13,123 cycles
DURING HEAVY CHECK, CORROSION WAS FOUND ON AFT WET AREA LT SHEAR PANEL FRAME 87, LBL 36. REPLACED SHEAR PANEL. IAW SRM 51-10-03. AND EAMS NR 00173.
2014
Part: FLOORBEAM — CORRODED (FRAME 84) · airframe 15,799 hrs · 9,669 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT CABIN FR 84, LBL 20 CROSSBEAM. CAREFULLY CUT OUT DAMAGED AREA AND PERFORMED DETAILED VISUAL INSPECTION OF CROSS BEAM AT FR 84, BETWEEN LBL 29 AND LBL 34. PERFORMED HFEC INSPECTION OF REWORKED AREA OF TOP FLANGE OF CROSSBEAM AT FR 84 IAW NDT PART 1 51-00-00-916-803. FABRICATED THE DOUBLER AND FILLER OF AFFECTED AREAS. APPLIED CHEMICAL CONVERSION COMPOUND AND HIGH SOLIDS EPOXY PRIMER TO REPAIRED PARTS AND REWORKED AREAS. APPLIED A COATING OF THE INTERFACE SEALANT TO THE REPAIRED PARTS. POSITIONED REPAIR PARTS AND SOAKED THE FASTENERS WITH INTERFACE SEALANT IAW SRM 51-40-00/1 AND SRM 51-21-05/1. FILLED THE GAPS AND REWORED AREA WITH HYSOL STRUCTURAL RESIN. RESTORED THE ORIGINAL FINISHING OF THE REPAIR AREA IAW SRM PART II 51-23-06/1 AND E14-359-01.
Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 15,799 hrs · 9,669 cycles
DURING HEAVY CHECK IAW EAMS NR H4307/1578, AFT CABIN LEFT SEAT TRACK FRAME 84, LBL 10 CORRODED. BLENDED CORROSION IAW SRM 51-10-03, PERFORMED HFEC IAW NDT PART 1 51-00-00-916-803, FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER.
Part: FLOORBEAM — CORRODED (FRAME 17) · airframe 15,799 hrs · 9,669 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT THE FWD CABIN FLOORBEAM FRAME 17. REMOVED CORROSION, PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION. CUTOUT DAMAGE. FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-00 AND E190 SRM 51-21-05.
Part: CABLE — BROKEN (R1 DOOR SLIDE) · airframe 15,658 hrs · 9,582 cycles
R1 DOOR SLIDE UNRAVELED AND GIRT BAR REMAINED ENGAGED WHEN CATERING ATTEMPTED TO OPEN DOOR, SLIDE WAS DISARMED. FOUND THE FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE FLEXBALL CABLES BROKEN. R & R FLEXBALL CABLE IAW AMM 52-41-40. RIG & OPS CHECKED OK.
2012
Part: POWER UNIT — FAILED (CABIN) · airframe 10,986 hrs · 6,647 cycles
FLT 1108 RDU-JFK, ON GROUND CHECK FOUND CABIN AND EXTERIOR EMERGENCY LIGHTS AT ROWS 2, 21, 17 AND EXT LT BOTTOM LT + RT FAILED PER TC E190-33-50-01-720-801. FOUND NR 5 ELPU NOT HOLDING CHARGE. REMOVED AND REPLACED ELPU IAW AMM 33-50-01. OPS CHECK GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 10,757 hrs · 6,516 cycles
FLT 6403 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND CORROSION ON FRAME 17 AS MARKED P/N 170-21769-403. PERMANENT REPAIR ACCOMPLISHED ON CROSS BEAM FRAME 17 RBL 16 TO RBL 45. REMOVED CORROSION BY BLEND OUT / CUT OUT. PERFORMED HFEC INSPECTION, INSTALLED REINFORCEMENT ANGLES AND SHIMS, APPLIED ALODINE, PRIMER AND TOPCOAT AS PER EA E12-681-01.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 10,757 hrs · 6,516 cycles
FLT 6403 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND CORROSION ON FRAME 14 AND 17 FWD FLOOR CROSS BEAM P/N 170-21766-411. REMOVED CORROSION BY BLEND OUT / CUT OUT. PERFORMED HFEC INSPECTION, INSTALLED REINFORCEMENT ANGLES AND SHIMS. APPLIED ALODINE, PRIMER AND TOPCOAT AS PER EA E12-681-01.
Part: ACM — FAILED (AC BAY) · airframe 10,033 hrs · 6,011 cycles
FLT 1230 RDU-BOS, F/A REPORTS SMOKE SMELL IN CABIN AT 10,000 FEET. PACK 2 FAILED ON LANDING FIM TASK 21-51-00-810-A FOR SMELL OF SMOKE IN CABIN WITH ASSOCIATED PACK 2 FAIL EICAS MSG VERIFIED ACM 2 FAILED ITEM TRANSFERRED TO MEL 21-51-00 COND 1. OPS CHECK OF ELECT EQUIP RACK VENTILATION SHUTOFF VALVE, OPS NORMAL PER AMM 21-28-00-710-810A. REMOVED AND REPLACED ACM PER AMM 21-51-00. OPS CHECK GOOD.
2011
Part: BELLOWS — TORN (AC PACK) · airframe 6,845 hrs · 4,031 cycles
FLT 1115 RIC-MCO, CLIMBING THROUGH FL280 NOTICED CABIN ALT AT 9400FT IN AMBER AND CLIMBING. DESCENDED TO 10,000 FEET AND OBSERVED NORMAL CABIN ALT PARAMETERS. A/C REMAINED PRESSURIZED AT 10,000FT WITH A CABIN ALT OF NEG 200 AND A DIFF PRESSURE OF -4.7. TECHNICIAN PERFORMED TSM 21-31-00-810-824-A AND FOUND EMERGENCY BELLOWS FOR RT PACK TORN. REMOVED AND REPLACED BELLOWS AND TEST WAS SATISFACTORY REF AMM 21-31-00.
2009
Part: DIAPHRAGM — PUNCTURED (DOOR ASSIST) · airframe 2,306 hrs · 1,365 cycles
FLT JB1087, AFTER COMPLETION OF PASSENGER BOARDING DURING CLOSING OF FWD LEFT PASSENGER DOOR PNEUMATIC ASSIST BOTTLE DISCHARGED INADVERTENTLY. CANCELLED DEPARTURE, MX FOUND NITROGEN DEPLETED IN PNEUMATIC ASSIST SYSTEM, PERFORMED INSPECTION OF L1 DOOR AND ASSIST ASSY FOUND ALL NORMAL. REMOVED AND REPLACED PNEUMATIC DIAPHRAGM AND PACKINGS IN PASS DOOR PNEU ASSY AND SERVICED IAW AMM 52-11-53. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. INSPECTION OF THE L1 PASSENGER DOOR WAS ACCOMPLISHED PER E190 AMM 05-25-00-06, FOUND ALL NORMAL. AIRCRAFT OK FOR SERVICE.
Part: PIN — OUT OF POSITION (EVAC SLIDE) · airframe 1,954 hrs · 1,148 cycles
FLT JB1056 - PIT-JFK AFTER LANDING AT JFK AND AIRCRAFT AT GATE CABIN CREW COULD NOT OPEN L1 DOOR, JAMMED AND WOULD NOT DISARM. MX FOUND L1 DOOR ESCAPE SLIDE BUSTLE PIN MISSING FROM LANYARD CAUSING DOOR JAM. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE ASSY IAW AMM 25-65-01. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE.