N203JB
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.
97 reports on file, 2006-04-25 – 2024-12-05.
Part: RIB — DAMAGED (ZONE 100) · airframe 46,341 hrs · 30,443 cycles
PERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT WING TO FUSELAGE RIB FR52, (CENTER FUSELAGE II) AS PER COOPESA´S EO COO-EO-2024-21057-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2017-190-087992 REV A. THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 1-45
Part: SKIN — DAMAGED (ZONE 600) · airframe 46,341 hrs · 30,443 cycles
PERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 REINFORCEMENT AREA COMMON TO SPAR I COOPESA´S EO COO-EO-2024-21119-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-027260 REV ORIG, THE REPAIR WAS CONSIDERED MAJOR WITHOUT ADDITIONAL REQUIREMENTS, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 6-17
Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 46,341 hrs · 30,443 cycles
PERFORMED PERMANENT REPAIR AT LH WING TRAILING EDGE SLAT 4 AS PER COOPESA´S EO COO-EO-2024-21029-R00 REV 00, DUE TO CORROSION FOUND AT REAR OUTBOARD AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026436 REV ORIG. THIS REPAIR WAS CATEGORIZED AS MINOR REPAIR, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 5-1
Part: SKIN — DAMAGED (ZONE 500) · airframe 46,341 hrs · 30,443 cycles
PERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT LH WING SKIN TRAILING EDGE AT RIB 11 AREA, AS PER COOPESA´S EO COO-EO-2024-21043-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2019-190-147552 REV C. THE REPAIR WAS CONSIDERED PERMANENT ,WITH A THRESHOLD OF 7500FC AND INTERVALS OF 7500FC SINCE REPAIR EMBODIMENT, INSPECTION REQUIRED: INTERNAL AND EXTERNAL DET, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 21-64.
Part: SKIN — DAMAGED (ZONE 600) · airframe 46,341 hrs · 30,443 cycles
PERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT RH WING SKIN TRAILING EDGE AT RIB 10 AREA, AS PER COOPESA´S EO COO-EO-2024-21191-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-028502 REV ORIG. THE REPAIR WAS CONSIDERED TEMPORARY BY 12 MONTHS AND DTA IS UNDER DEVELOP, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 21-63
Part: SKIN — CRACKED (ZONE 600 SLAT) · airframe 46,341 hrs · 30,443 cycles
PERFORMED PERMANENT REPAIR AT RH WING SLAT 5 BETWEEN RIB 18 AND 21 AS PER COOPESA´S EO COO-EO-2024-21014-R00 REV 00, DUE TO CRACK FOUND AT SKIN AROUND ACTUATOR AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026551 REV ORIG, THE REPAIR WAS CONSIDERED MAJOR WITHOUT ADDITIONAL REQUIREMENTS, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 6-7.
Part: RIB — CRACKED (ZONE 500) · airframe 46,341 hrs · 30,443 cycles
PERFORMED TEMPORARY REPAIR AT LH WING RIB 6 AS PER COOPESA´S EO COO-EO-2024-21207-R00 REV 00, DUE TO CRACKS FOUND AT MLG ACTUATOR SUPPORT FITTING, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-029064 REV ORIG, THE REPAIR WAS CONSIDERED TEMPORARY BY 12 MONTHS AND DTA IS UNDER DEVELOP, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 5-17
Part: SKIN — CRACKED (ZONE 500) · airframe 46,341 hrs · 30,443 cycles
PERFORMED TEMPORARY REPAIR AT LH WING SLAT 5 BETWEEN RIB 18 AND 21 AS PER COOPESA´S EO COO-EO-2024-21017-R00 REV 00, DUE TO CRACKS FOUND AT SKIN AROUND ACTUATOR AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026548 REV ORIG, THE REPAIR WAS CONSIDERED MINOR, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 5-7.
Part: SKIN — DAMAGED (ZONE 600) · airframe 46,341 hrs · 30,443 cycles
PERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 AFT REINFORCEMENT AREA COMMON TO SPAR II COOPESA´S EO COO-EO-2024-21236-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-029313 REV ORIG, THE REPAIR WAS CONSIDERED MAJOR WITHOUT ADDITIONAL REQUIREMENTS, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 6-29
Part: SKIN — DAMAGED (ZONE 100) · airframe 46,341 hrs · 30,443 cycles
PERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT FR01+65MM STR 20L+130MM, (FWD FUSELAGE) AS PER COOPESA´S EO COO-EO-2024-21042-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-013396 REV B. THIS REPAIR WAS CATEGORIZED AS CAT B WITH A THRESHOLD OF 26600FH OR 20000FC WITH OCCURS FIRST, INSPECTION REQUIRED: LOW FREQUENCY EDDY CURRENT, THE PROCESS WAS DOCUMENTED ON COOPESAâS ITEM A1P230 21-45.
Part: SKIN — DAMAGED (ZONE 100) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: DURING CURRENT CHECK ON N203JB (MSN: 023) @ MCN, EAMS REPORTED THREE (3) BLEND-OUT SPOTS ON THE CENTER FUSELAGE I EXTERNAL SKIN @ FR30-32 & STGR 25L-26L. SEE REF /1/, ETD REV A, FOR COMPLETE INFORMATION. EMBRAER PROVIDED ENGINEERING DISPOSITION VIA REF /1/ ETD REV A, AUTHORIZING REPAIRS FOR EACH BLEND-OUT AS FOLLOWS: BLEND #1: INSPECTION OF THE BLEND OUT, PLUGGING OF THE DRILLED HOLE, APPLICATION OF CHEMICAL CONVERSION, APPLICATION OF EPOXY PRIMER, AND FINISH RESTORATION. BLEND #2: REINSTALLATION OF THE ORIGINAL RIVET TYPE, APPLICATION OF CHEMICAL CONVERSION, APPLICATION OF EPOXY PRIMER, AND FINISH RESTORATION. BLEND #3: CUT-OUT AND INSTALLATION OF A REPAIR DOUBLER, APPLICATION OF CHEMICAL CONVERSION, APPLICATION OF EPOXY PRIMER, INSTALLATION OF FASTENERS, APPLICATION OF FILLET SEALANT, AND FINISH RESTORATION. EC E24-521-01 IS ISSUED TO ACCOMPLISH THE REPAIR OF THE THREE (3) BLEND-SPOTS IAW REF /1/. EC E24-521-02 IS ISSUED TO ACCOMPLISH THE POST-REPAIR INSPECTIONS OF THE DOUBLER REPAIR OF BLEND #3 AS FOLLOWS: EXTERNAL LFEC WITH A TH = 20000 FC / 26600 FH AND INT = 20000 FC / 26600 FH SUBSTANTIATION: THIS PERMANENT REPAIR IS APPROVED PER REF /1/ ETD REV A AND REF /2/ ANAC APPROVAL FORM (INCLUDED IN THE ETD), AND IS CLASSIFIED AS MAJOR. (E/C: E24-521-01) ORIGINAL SUBMISSION DATE: 6/11/2024
Part: SKIN — CRACKED (ZONE 100) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: DURING CURRENT LEASE RETURN CHECK ON N203JB (MSN 023) AT MCN DATED 05/2024, A DENT WAS FOUND ON THE FWD FUSELAGE SKIN BETWEEN FR 1-2 & STRR 22L-24L. SEE REF /1/ ETD FOR DETAILS. THE DENT IS MEASURED TO BE 0.70â L X 0.50â W AND 0.008â DEEP. WHILE PERFORMING HFEC IN THE DENT AREA, EAMS NOTED AN INDICATION/CRACK IN THE AREA. THE DAMAGE WAS EVALUATED AGAINST SRM AND NO REPAIR NOR ADL WERE FOUND APPLICABLE. EAMS CONTACTED EMBRAER FOR REPAIR INSTRUCITON AND EMBRAER PROVIDED REF /1/ ETD TO STOP DRILL THE CRACK, CUT OUT THE DAMAGED AREA, PERFORM HFEC AFTER REMOVAL AND FABRICATE & INSTALL REPAIR FILLER AND DOUBLER AND RESTORE SURFACE PROTECTION. E24-606-01 IS ISSUED TO PERFORM PERMANENT REPAIR IAW REF /1/ ETD REV B WITHOUT DEVIATIONS. E24-606-02 IS ISSUED TO TRACK POST REPAIR LFEC/SDI INSPECITON ( THRESHOLD AND INTERVAL OF 26600FH/20000FC) SUBSTANTIATION: THIS PERMANENT REPAIR IS APPROVED VIA REF /1/ ETD AND IS CLASSIFIED AS MAJOR. (E/C:E24-606-01) ORIGINAL SUBMISSION DATE: 6/11/2024
Part: SKIN — DENTED (FUSELAGE) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: RE-EVALUATE DENT AT FR98-FR99 & STR25R-STR29R, THE DENT IS LOCATED OVER 3 BAYS AND REPAIR CROSSES OVER 1 RIVET ROW REF. EMBRAER NR-00179 W/O: H9417; REMOVED EXISTING REPAIR DOUBLER AND INSTALLED NEW REPAIR DOUBLER AND FILLER AT FR98-FR99 AND BETWEEN STRG 25R-29R REF ETD 2024-190-014202 REV AERNNOVA T1-170-24-143 REV AND JETBLUE EC E24-646-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: COMPLY WITH E24-606-01 (REV 6-5-24 ) FUSELAGE / FWD FUSELAGE / EXTERNAL SKIN BETWEEN FR1-2 & STG 22L-24L / DENT & CRACK PERMANENT REPAIR REF. EMBRAER NR-00210 WO: H9417; COMPLIED WITH E24-606-01 REV 6-5-24.
Part: SKIN — DENTED (FUSELAGE) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: PER CUSTOMER REQUEST: CENTER FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32 STGR 25L AND STGR 26L WITH DENTS (3EA) RE-EVALUATE EMBRAER NR-00097 W/O H9417; REPAIRED 3EA AREAS ON FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32, STGR25L AND STGR26L REF EMB ETD-2024-190-011449 REV A AND JETBLUE EC E24-521-01 WORK ACCOMPLISHED ON EMBRAER NR-00097 W/O: H9417.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: EMERGENCY LIGHT ON FWD PASSENGER DOOR CEILING PANEL INOP; REF EAMS WO H9417 NR 00140 REMOVED AND REPLACED FWD PAX ENTRANCE EMERGENCY/COURTESY LIGHT ASSY IAW AMM 33-26-01. OPS TEST GOOD IAW AMM 33-26-00-710-801-A.'
Part: COVER — CRACKED (ESCAPE LIGHT) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: LH WING TO BODY FAIRING LOWER EVACUATION LIGHT COVER CRACKED; REMOVED AND INSTALLED NEW LH WING TO BODY FAIRING LWR EVAC LIGHT COVER IAW EMBRAER 190 AMM 33-50-25.'
Part: LIGHT — NO TEST (CABIN) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: CABIN OVERWING EMERGENCY EXIT CEILING LIGHT INOP; PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER E190 AMM33-50-00-710-801-A. OPERATIONAL TEST IS GOOD AT THIS TIME. REF EAMS W/O H9417 NR 00139.
Part: SKIN — DAMAGED (ZONE 100) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE CHECK ON N203JB (MSN: 023) @ MCN, EAMS REMOVED THE EXISTING DOUBLER REPAIR IAW ETD2019-190-137093 REV A. THE DENT IS LOCATED OVER 3 BAYS AND THE REPAIR CROSSES OVER A ROW OF RIVETS BETWEEN FR98-99 AND STGR 25R-29R. AN HFEC INSPECTION WAS ACCOMPLISHED ON THE AFFECTED PART (PN: 190-61701-005) WITH NO FURTHER DAMAGES. PER REF /1/, ETD, THE SRM REPAIR 62P, EXTERNAL DIRECT RECTANGULAR REPAIR OF THE SKIN IS NOT ACCEPTABLE AS A PERMANENT REPAIR OPTION DUE TO THE LOCATION OF THE PREVIOUS REPAIR WHICH CROSSES OVER TWO STRINGERS AND INVOLVES THREE BAYS. EMBRAER PROVIDED ENGINEERING DISPOSITION PER REF /1/, ETD WHICH REFERENCES REF /2/ TI WITH REPAIR INSTRUCTIONS CONSISTING OF NDT, FABRICATE AND INSTALL REPAIR DOUBLER AND FILLER, AND RESTORE SURFACE PROTECTION PER SRM. THIS IS CONSIDERED A TEMPORARY REPAIR BECAUSE IT WILL REQUIRE A DAMAGE TOLERANCE ANALYSIS WITHIN 12 MONTHS AS OF MAY 23, 2024. THIS EC E24-646-01 IS ISSUED TO ACCOMPLISH THE REPAIR PER REF /1/ ETD. EC E24-646-02 IS ISSUED TO TRACK THE DTA PER REF /1/ ETD. SUBSTANTIATION: THIS TEMPORARY REPAIR IS APPROVED PER REF /1/ ETD & REF /3/ ANAC FORM AND IS CLASSIFIED AS MAJOR. (E/C: E24-646-01) ORIGINAL SUBMISSION DATE: 6/11/2024
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 46,337 hrs · 30,442 cycles
DURING HEAVY MAINTENANCE: ELPU FUNCTIONAL TEST FAILS, MULTIPLE EMERGENCY LIGHTS THROUGHOUT THE CABIN AND EXTERIOR OF AIRCRAFT ARE INOP; REMOVED AND REPLACED #4 AND #5 ELPU REF EMB190 AMM 33-50-01-000-801-A. OPERATIONAL CHECK GOOD PER EMB190 AMM 33-50-01-710-801-A.'
Earlier reports · 2006–2023 · 77 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,208 hrs · 30,362 cycles
FLT#221, BOS-PBI. 'BLEED 2 LEAK CAUTION AT FL 280 CABIN ALT HI WARNING ON DESCENT; ACCOMPLISHED FIM TASK 36-21-00-810-815-A00 R/R 1 EA. CORRODED CERAMIC PIN AT LOOP 5 CONNECTORS ICAS FAULT CLEARED SYS OP CK NORM ACCOMPLISHED HIGH POWER ENGINE ASSURANCE RUN (PRECAUTIONARY) NO LEAKS OR IEACAS MESSAGES PRESENT.'
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,197 hrs · 30,358 cycles
FLT#250, SAV-BOS. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO SAV) ' CLIMBING THROUGH APPROX 15,000 ' WE NOTICED A STRONG, SHARP ACRID SMELL IN THE COCKPIT. FA'S REPORTED THE SAME THING, STRONGEST AT MID CABIN. WE DECLARED EMERGENCY AND RETURNED TO SAV. RAN COCKPIT/ CABIN SMOKE/ FUMES QRH. FA'S REPORTED THAT SMELL DISSIPATED ON THE GROUND. AIR RETURN TO SAV. ( AIR CONDITIONING PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC IN REF NRC 00313: REPLACE INBD UPPER SPAR RH PYLON; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00027 ) REF TOMX W/O# 2362, N/R # 00350. INBD UPPER SPAR RH PYLON WAS REPLACED PER EMB-190 SRM 51-43-03 SRM 51-43-04 AND SRM 51- 41-02. ACCOMPLISHED BY TOMX TECH # 10000202, TOMX QC# 299517.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III STR28R / BWTN FR86-FR90 /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSS-BEAM LOCATED BTW FR17 AND Y=400 TO Y=810 RH IN PASSENGER FLOOR STRUCTURE W1 (PREVIOUS REPAIRED); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00021 ) REF TOMX WO# 2362. N/R# 00252.WIP: CROSS-BEAM LOCATED BTW FR17 AND Y=400 TO Y=810 RH IN PASSENGER FLOOR STRUCTURE WAS REPAIRED PER EMB-190 SRM 53-00-10 REPAIR/53. ACCOMPLISHED BY TOMX TECH # 10000939, TOMX QC#10000266.
Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ABOVE FR 87 BETWEEN STGR 28R/27R; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00037 ) REMOVED AND REPLACED SHEAR CLIP PER EMB-190 SRM 51-41-01 AND 51-41-02. REF TOMX NR 00303.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON SHARE CLIP FR 88 BTW STGR 28-29 RH AT C2. WAS FOUND;(RESOLVED ON W/O: 1260255 TASKCARD: NR-00023 ) REF TOMX WO# 2362, N/R# 00333. CORROSION ON SHARE CLIP FR 88 BTW STGR 28-29 RH AT C2 WAS REMOVED AND WAS FOUND OUT OF LIMITS OT=0.050" AND MRT=0.032" THEREFORE IT WAS REPLACED PER EMB-190 SRM 51-10-03, SRM 51-12-01,SRM 51-75-16, SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03. ACCOMPLISHED BY TOMX TECH# 400420, TOMX QC # 269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00301 CORROSION ON STGR 28 RH BTW FR 86-87 AT C2. WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00026 ) REF TOMX W/O# 2362, N/R #00335. STGR 28 RH BTW FR 86-87 AT C2 WAS REPAIRED PER EMB-190 ETI-190-23-704 REV:.2 AND ETD2023-190-026418 REV:.B. ACCOMPLISHED BY TOMX TECH # 400420, TOMX QC# 269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN AND FASTENERS AREA COVERED BY LIVE TV RADOME; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00038 ) REPAIRED PER LETBLUE EC E23-991-0. REF TOMX NR 00168.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR BEAM BTW FR87-89 AND +Y=300 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00014 ) CORROSION ON FLOOR BEAM BTW FR87-89 AND +Y=300 AT AFT FLOOR STRUCTURE WAS REMOVED AND EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER EMB-190 SRM 51-12-01, SRM 51-10-03, SRM 51-75-16, SRM 51-41-01 AND SRM 51-43-03. ALL WORK ACCOMPLISHED ON TOMX W/O # 2362, N/R# 000215. ACCOMPLISHED BY TOMX # 10001734, TOMX QC # 269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CTR BEAM LOCATED BTW FR13 TO FR19 AND Y=270 RH IN PASSENGER FLOOR STRUCTURE W1; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00017 ) REFERENCE TOMX W/O #2362, N/R# 00250. CORROSION ON CTR BEAM LOCATED BTW FR13 TO FR19 AND Y=270 RH WAS REMOVED AND EVALUATED OUT OF LIMITS OT: .071" AND RT: .032" THEREFORE IT WAS REPLACED PER EMB-190 SRM 51-12-01,SRM 51-10-03,SRM 53-10-10 AD\51,SRM 51-41-02, SRM 51-41-01,SRM 51-43-03 AND SRM 51-43-04. ACCOMPLISHED BY TOMX TECH #400420, TOMX QC #269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON SHEAR CLIP FR 86 STGR 28/27 RH AT C2. WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00025 ) REF TOMX W/O# 2362, N/R #00334. SHEAR CLIP FR 86 STGR 28/27 RH AT C2 WAS REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-41-01. ACCOMPLISHED BY TOMX TECH # 400420, TOMX QC # 269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / STR27R / BWTN FR86-FR87 /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON STGR 27 RH BTW FR 86-87 AT C2. WAS FOUND;(RESOLVED ON W/O: 1260255 TASKCARD: NR-00024 ) REF TOMX W/O# 2362 N/R# 00332. STGR 27 RH BTW FR 86-87 AT C2 WAS REPAIRED PER EMB-190 ETI-190-23-702 R2 AND ETD2023-190-026419 REV.: A. ACCOMPLISHED BY TOMX # 400420, TOMX QC # 269616.
Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER SHEAR CLIP REMOVAL IN REF TO NRC 00303, CORROSION ABOVE FR 87 AND BTW STGR 28R/27R WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00029 ) REF TOMX W/O# 2362, N/R# 00336. CORROSION ABOVE FR 87 AND BTW STGR 28R/27R WAS REPAIRED PER ETI-190-23-706 REV. ORIGINAL AND ETD2023-190-026416 REV.:/. ACCOMPLISHED BY TOMX TECH #10000939, TOMX QC# 10000266.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE /FUSELAGE / FLOOR STRUCTURE / BTW FR14 TO FR20 / Y=-273.0 / CTR SEAT TRACK BEAM / PREVIOUS DOUBLER /CORROSION/ PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER DOUBLER REMOVAL IN REF NRC 00042, CORROSION ON SHEAR CLIP ABOVE FR 88 BTW STGR 28RH/STGR27RH WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00028 ) REF TOMX W/O #2362, N/R # 00283.CORROSION ON SHEAR CLIP ABOVE FR 88 BTW STGR 28RH/STGR27RH WAS REMOVED PER EMB-190 SRM 51-10-03 AND SRM 51-12-01 AND FOUND OUT OF LIMITS PER EMB-190 SRM 51-75-16, THEREFORE IT WAS REPLACED PER EMB 190 SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03. ACCOMPLISHED BY TOMX TECH # 439821, TOMX QC #10000016.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK BEAM AT FWD AVIONICS ACCESS DOOR (123BL); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00013 ) REF TOMX WO 2362 NR 00064: BEAM ON FWD AVIONICS ACCESS DOOR (123BL) WAS REPLACED PER EMB 190 SRM 51-41-01,SRM 51-43-03 AND SRM 51-41-02 WORK ACCOMPLISHED BY TOMX TECH 10000939 RRII ACCOMPLISHED BY TOMX QC 299517.
Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP IN FR81 BTW STGR 28R/27R AT AFT CARGO; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00016 ) REFERENCE TOMX W/O# 2362, N/R# 00190. CORROSION ON SHEAR CLIP IN FR81 BTW STGR 28R/27R WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE WAS REPLACED PER EMB-190 SRM 51-12-01,SRM 51-10-03, SRM 51-75-16,SRM 51-41-01 AND SRM 51-41-02. ACCOMPLISHED BY TOMX TECH # 10001734, TOMX QC #269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR BEAM BTW FR87-88 AND -Y=300 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00018 ) REFERENCE TOMX W/O # 2362, N/R # 00217. CORROSION ON FLOOR BEAM BTW FR87-88 AND -Y=300 AT AFT FLOOR STRUCTURE WAS REMOVED AND EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER EMB-190 SRM 51-12-01, SRM 51-10-03, SRM 51-75-16, SRM 51-41-01, SRM 51-43-03 AND SRM 51-42-01. ACCOMPLISHED BY TOMX TECH #10001734, TOMX QC #269616.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE SKIN / FR 62-66 & STGR 02L-02R / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: IN REF TO RC E12-111-02: CORROSION ON PREVIOUS REPAIR DOUBLER ON CTR SEAT TRACK BEAM, LOCATED BTW FR14 TO FR20 AND Y=280 LH, FLOOR STRUCTURE (W1). EVALUATION; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00015 ) CORROSION ON PREVIOUS REPAIR DOUBLER ON CTR SEAT TRACK BEAM, LOCATED BTW FR14 TO FR20 AND Y=280 LH, FLOOR STRUCTURE (W1) WAS ATTENDED WITH ETI-190-23-698 REV.:ORIGINAL AND ETD2012-190-001959 REV.:A. ALL WORK ACCOMPLISHED ON TOMX W/O# 2362, N/R # 00237. ACCOMPLISHED BY TOMX# 10001762, TOMX QC # 299517.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK ON RIB 22 AT LH WING; ALL WORK ACCOMPLISHED REF TOMX W/O2362 NR 00187 RIB # 22 AT LH WING WAS REPLACED PER EMB 190 SRM 51-43-04 AND SRM 51-43-03.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSSBEAM BTW FR84 AND -Y=300-1200 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00022 ) REF TOMX WO# 2362, N/R # 00223. CORROSION ON CROSSBEAM BTW FR84 AND -Y=300-1200 AT AFT FLOOR STRUCTURE (W2) WAS REMOVED PER EMB-190 SRM 51-12-01 AND SRM 51-10-03 EVALUATED AND REPLACED PER EMB-190 SRM 51-10-02, SRM 51-43-03 AND SRM 51-43-04. ACCOMPLISHED BY TOMX TECH # 10000939, TOMX QC#10000016.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,896 hrs · 30,151 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON FRAME 80 BTW STRG 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00012 ) CORROSION ON FRAME 80 BTW STRG 26R/27R WAS EVALUATED OUT OF LIMITS, THEREFORE WAS REPAIRED PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND ETI-190-23-685 REV 1. ALL WORK ACCOMPLISHED ON TOMX WO # 2362 N/R # 00188. ACCOMPLISHED BY TOMX TECH # 10001734, TOMX QC # 299517.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,252 hrs · 29,636 cycles
FLT#2933, DCA-MCO. (AIRCRAFT DIVERTED TO JAX) 'BLEED 1 FAIL; INTERROGATED CMC AND NO CORRELATED MESSAGES WITH BLEED 1 FAIL. PERFORMED OPS CHECK OF #1 BLEED PER AMM 36-11-. AL CHECKS NORMAL. AT THIS TIME IN MANY CONFIGURATIONS WITH PACKS AND OTHER BLEED / CLOSS BLEED AND ALL CHECKS ARE GOOD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,188 hrs · 29,591 cycles
FLT#2534, PBI-DCA. 'ELPU 2 BATTERY CAPACITY TEST FAILED; REMOVED AND REPLACED ELPU 2 IN REF TO AMM 33-50-01. THE OPS CHECK IS GOOD. OK FOR FURTHER SERVICE. PARTS TRANSACTION COMPLETED UNDER W/O # 1257900 TASK CARD. E190-33-50-01-720-801-FWD.'
2021
Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,905 hrs · 26,589 cycles
FLT 1539, MVY-JFK. DURING FLIGHT COCKPIT SMELLED OF EXHAUST FUMES AT VARIOUS STAGES OF THE FLIGHT, ESPECIALLY ON THE DESCENT. FA'S DIDNT NOTICE IT BUT BOTH PILOTS NOTED IT ON BOTH LEGS. THOUGHT IT WAS AN ANOMOLLY OR TRANSIENT ODOR FIRST LEG THEN SAW ITS A REPEAT WRITE UP; FOLLOWING FIM 21-20-00-810-803-A NO SMOKE/ABNORMAL SMELL FOUND. RUN ENGINES 1 + 2 AND APU USING BLEED MULTIPLE TIMES AND EVERYTHING CHECKS GOOD. AS PRECAUTIONARY REMOVED AND REPLACED RECIRCULATING FILTERS IAW AMM 21-24-02.
2020
Part: FLOOR SUPPORT — DAMAGED (FRAMES 48-49) · airframe 39,710 hrs · 25,823 cycles
DURING HEAVY MAINTENANCE. RESOLVED ON W/O: 1068962 TASKCARD: NR-00013, REF AEROMAN NR 2020-274932. ACCOMPLISHED REPAIR COMMON TO THE CENTER FUSELAGE II MIDDLE FLOOR STRUCTURE COMMON TO LT LONGITUDINAL BEAM BETWEEN FR 48 TO FR 49, IAW EC E20-660-01 EA 53-0648-20 REV 0 COVER PART 1 AND ETD 2020-190-027393 REV B.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 39,710 hrs · 25,823 cycles
DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT POWER UNIT NR 3 AT MID CABIN RT SIDE IN PASSENGER CABIN. RESOLVED ON W/O: 1068962 TASKCARD: NR-00014. REMOVED AND REPLACED EMERGENCY LIGHT AT MID CABIN RT SIDE IN PASSENGER CABIN, IAW E190 AMM 35-50-01-000-801-A AND AMM 33-50-01-400-801-A ITEM 3 STEP G AND H. PERFORMED BONDING TEST. TEST IS OK, IAW E190 AMM 20-13-21-720-801-A. TOOL USED BONDING METER P/N M1-G-KIT S/N DC005009 DUE DATE OCT-03-2020.
2019
Part: SKIN — CRACKED (RT WING) · airframe 38,590 hrs · 25,039 cycles
DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL BTW RIB 9 TO RIB 10 TRAILING EDGE AREA ON RH WING; REF. AERO N/R 2019-337111. PERFORMED PERMANENT REPAIR ON LOWER SKIN PANEL BTW RIB 9 TO RIB 10 TRAILING EDGE AREA ON R/H WING IAW E190 SRM 57-10-01.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 38,590 hrs · 25,039 cycles
DURING HEAVY MAINTENANCE, INOP DOOR FRAME EMERGENCY LIGHT RH AT AFT GALLEY AREA; REF AEROMAN N./R 2019-337155. REMOVED AND REPLACED EMERGENCY LIGHT RH (ELPU 6) AT AFT GALLEY AREA IAW E190 AMM 33-50-01-400-801-A OPS CHECK GOOD PER E190-33-50-01-710-801-A, E190 AMM 33-50-00-710-801-A.
Part: SKIN — CRACKED (LT WING) · airframe 38,590 hrs · 25,039 cycles
DURING HEAVY MAINTENANCE, WAS FOUND WITH CRACK DAMAGE COMMON TO THE LEFT HAND WING UPPER SKIN P/N 190-33053-009, AFT EDGE AT RIB 11. THIS DAMAGE IS OUT OF THE SRMâS SCOPE. EMBRAER PROVIDED REPAIR INSTRUCTIONS BY MEANS OF REF. /2/. THE REPAIR CONSISTS OF TRIMMING OUT THE CRACKED SKIN SECTION, PERFORMING NDT INSPECTIONS, FABRICATING/INSTALLING AN ALCLAD 7075-T6 REPAIR DOUBLER AND INSTALLING REPAIR FASTENERS AT MISSING PRODUCTION FASTENERS LOCATIONS. AEROMAN ISSUED REF /1/ EA. EC E19-827-01 INCORPORATES REF /1/ EA WITHOUT DEVIATION. EC E19-827-02 TRACKS PENDING 12 MONTH DTA REQUIRED PER REF /2/; EMBRAER APPROVED THIS REPAIR PER REF /2/ AND IS CLASSIFIED AS MAJOR AND TIME-LIMITED PENDING DTA.
2018
Part: LIFE RAFT — UNSECURE (AFT) · airframe 35,770 hrs · 23,060 cycles
FT # 1354, DCA-BOS. LIFE RAFT LACE UNRAVELED; REPLACED LIFE RAFT IAW AMM 25-66-00.
2017
Part: SLAT SYSTEM — FAILED · airframe 32,623 hrs · 20,700 cycles
SLAT FAIL MESSAGE ON EICAS DURING APPROACH, WHEN FLAPS WERE SELECTED TO 1. SLATS FAILED AND DID NOT MOVE DURING SLAT FAIL QRH PROCEDURE. PERFORMED SIM 27-81-00-810-805-A. TRANSCONDOR CONDITION OF SFACE OPS CHECK OF FLAP/SLAT SYSTEM IAW AMM 27-80-00. OPS CHECKED NORMAL. NO DEFECTS NOTED.
Part: UNKNOWN — ODOR (CABIN) · airframe 32,149 hrs · 20,371 cycles
RETURN TO FIELD DUE TO AN ODOR, MORE PREVALENT AFT THAN FWD. PERFORMED FIM 21-20-00-810-801A. APU WAS NOT IN OPERATION. NO SOURCE EVIDENT IN CABIN. SUSPECT ENGINE RESIDUAL WAS FLUID.
2016
Part: UNKNOWN — ODOR (CABIN) · airframe 27,837 hrs · 17,357 cycles
FLIGHT DIVERTED. ELECTRICAL ODOR ASSOCIATED WITH 4 PREVIOUS WRITE UPS, COMPLIED WITH SMOKE AND/OR ABNORMAL ODOR INSPECTION IAW FIM TASK 21-20-00-820-801A NO ABNORMAL ODORS OR SMOKE NOTED, ACFT OK TO CONTINUE SERVICE.
2015
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP AT FRAME 17 BETWEEN STR 25R & 26R. R & R SHEAR CLIP AT FRAME 17 BETWEEN STR 25R & 26R REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND SHEAR CLIP IS CORRODED AT FRAME 83 BETWEEN STR 27R & 28R. R & R SHEAR CLIP, REF SRM 51-41-02 & 51-41-01. TOP COATED RIVETS, REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 79) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND SHEAR CLIP CORRODED AT FRAME 79 BETWEEN STR 29L & STR 29R. R & R SHEAR CLIP AT FRAME 79 BETWEEN STR 29L & STR 29R, REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: STRINGER — CORRODED (FRAMES 81-82) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND STR 28L IS CORRODED FROM FRAME 81 TO FRAME 82. CUTOUT DAMAGED SECTION, PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED FILLER, SPLICE AND SHIMS CLEANED, ALODINED, TOPCOATED AND SEALED IAW E15-588-01.
Part: SHEAR TIE — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND LT SUPPORT CORRODED AT FRAME 77 BETWEEN STR 29L & STR 29R, SHEAR TIE LOCATED AT FRAME 77 BETWEEN 29L AND CENTERLINE. R & R WITH NEW, REF SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03. TOP COATED AS REQUIRED, SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP AT FRAME V16 BETWEEN STR 27L & 28L. REMOVED, FABRICATED AND INSTALLED SHEAR CLIP AT FRAME 16 BETWEEN STR 27L & 28L REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 78) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND SHEAR CLIP CORRODED ON FRAME 78 FROM CENTERLINE TO STR 29R. R & R SHEAR CLIP AT FRAME 78 BETWEEN CENTERLINE & STR 29R WITH NEW SHEAR CLIP ON WO H4633, TASK 375, PN 170-6635-002. CORROSION- L=1" X 1.0" X .030" NOMINAL .063" REMAINING .033", 45 PERCENT MATERIAL LOSS FCBS 53-23-00-002. NO PREVIOUS REPAIRS NOTED. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND SHEAR CLIP IS CORRODED AT FRAME 88 BETWEEN STR 27R & 28R. R & R SHEAR CLIP, REF SRM 51-40-01 & 51-41-02. TOP COATED RIVETS REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP AT FRAME 17 BETWEEN STR 26R & 27R. REMOVED AND INSTALLED SHEAR CLIP AT FR 17 BETWEEN STS 26R & 27R REF SRM 51-41-01 & 51-41-02. PAINTED TOPCOAT REF SRM 51-23-06, THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP AT FRAME 17 BETWEEN STR 27R & 28R. REMOVED FABRICATED AND INSTALLED SHEAR CLIP AT FRAME 17 BETWEEN 27R & 28R, REF SRM 51-41-01 & 51-41-02. ALODINED, PRIMED AND TOP COATED, REF SRM 51-23-04, 51-23-05 & 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND RT SUPPORT CORRODED AT FRAME 77 BETWEEN STR 29L & STR 29R. R & R SHEAR TIE AT FRAME 77 BETWEEN STR 29R TO CENTERLINE, REF SRM 51-41-01, SRM 51-41-02, SRM 51-43-03. TOPCOATED AS REQUIRED, SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND AFT CARGO BAY FLOOR SHEAR CLIP CORRODED AT FRAME 82 BETWEEN STR 28L & 27L. REMOVED SHEAR CLIP FRAME 82 BETWEEN STR 28L & 27L. FABRICATED NEW SHEAR CLIP, COMPLIED WITH FPI INSPECTION, DRILLED, ALODINED, PRIMED AND TOP COATED AND INSTALLED FABRICATED SHEAR CLIP, SRM 51-43-03, SRM 51-41-01, SRM 51-41-02 NTM 51-00-00-9185-801A, SRM 51-41-01, SRM 51-41-02, SRM 51-43-03, SRM 51-23-04, SRM 51-23-05 AND SRM 51-23-06.
Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP AT FRAME 16 BETWEEN STR 27R & 28R INSTALLED NEW SHEAR CLIP AT FRAME 16 BETWEEN STR 27R & 28R. REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06, THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND CORRODED SHEAR CLIP, FRAME 17 BETWEEN STR 27L & 28L. R & R SHEAR CLIP, FRAME 17 BETWEEN STR 17L & 18L, REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06 THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: FINGER DOUBLER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE FOUND CORROSION, FWD CARGO DOOR, FWD FINGER DOUBLER. R & R FWD CARGO, FWD FINGER DOUBLER AFTER RTS STATED IT WAS BEYOND REPAIR. REF SRM 51-10-03, SRM 51-41-02, SRM 51-43-04. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND SHEAR CLIP CORRODED AT FRAME 76 BETWEEN STR 29R & 28R. R & R SHEAR CLIP CORRODED AT FRAME 76 BETWEEN STR 29R & STR 28R, REF SRM 51-41-01 & 51-41-02. PAINTED TOP COAT REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: SHEAR TIE — CORRODED (FRAME 78) · corrosion level 2 · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE FOUND SHEAR CLIP CORRODED ON FRAME 78 FROM CENTERLINE TO STR 29L. R & R SHEAR CLIP AT FRAME 78 BETWEEN CENTERLINE & STR 29L WITH NEW SHEAR CLIP ON WO H4633, TASK 00375 FOR WORK PERFORMED, PN 170-66351-001, CORROSION L=1.0" X 1.0" X .030 NOMINAL .063" REMAINING .033", 45 PERCENT MATERIAL LOSS. FCBS 53-23-00-002 NO PREVIOUS REPAIRS NOTED. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,312 hrs · 16,258 cycles
DURING HEAVY MAINTENANCE, FOUND LOWER INTERIOR EMERGENCY EXIT SIGN IS INOPERATIVE ON PANEL 242LRW. REMOVED AND INSTALLED EMERGENCY POWER SUPPLY IN CABIN IAW -MM 33-50-01. PERFORMED OPS CHECK IAW MM 33-50-01. OPS CHECKED NORMAL.
Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 26,232 hrs · 16,192 cycles
RETURNED TO DEPARTURE, DURING CRUISE SPDA FAIL ADVISORY MESSAGE FL360 ACCOMPANIED BY FUEL FEED 1 FAULT ADVISORY MESSAGE. PERFORMED QRH PROCEDURE. RESET NOT SUCCESSFUL. MESSAGE REMAIN DISPLAYED AC PUMP 1 PROVIDING FUEL FLOW TO ENG #1. EJECTOR PUMP 1 IS OFF. DURING ABOVE MALFUNCTION DC FUEL PUMP WAS ON PROVIDING FUEL TO ENG 2. APPROXIMATELY EVERY 1 MINUTE EJECTOR PUMP 2 TURNED ON FOR 5 -10 SECONDS WITH DC PUMP OFF. THEN DC PUMP TURNED ON FOR A MINUTE WITH EJECTOR PUMP 2 BACK OFF. THEN ALTERNATED THROUGHOUT THE REST OF THE FLIGHT. R & R MICRO COMMS MODULE SPDA2 SLAT 8 IAW AMM 24-61-07. PERFORMED BOTH ENGS RUN IAW AMM 71-00-00. OPS CHECK GOOD, NO DEFECTS NOTED.
2014
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 22,688 hrs · 13,944 cycles
ON MAINTENANCE CHECK, FOUND FWD AISLE EMERGENCY LIGHTS WILL NOT TEST. R & R 2 EMERGENCY POWER SUPPLY IAW AMM 33-50-01. OPS CHECK GOOD.
Part: SLAT SYSTEM — FAILED · airframe 22,173 hrs · 13,630 cycles
CREW DECLARED AN EMERGENCY DUE TO SLAT FAIL INFLIGHT, LANDED, 0 SLAT, FLAP 2. CLEARED SLAT FAIL MESSAGE IAW 45-45-00-970-805-A. R & R LT OTBD SKEW SENSOR AS PRECAUTION IAW 27-83-01 & OPS CHECKED IAW 27-80-00.
2013
Part: DIAPHRAGM — FAILED (DOOR SLIDE) · airframe 21,370 hrs · 13,128 cycles
DURING HEAVY MX CHECK, FOUND AT OPS CHECK, AFT SERVICE DOOR EMERGENCY SLIDE FAILED TO OPEN. REPACKED PNEUMATIC ASSY. REMOVED & REPLACED DIAPHRAGM.SERVICED AND PERFORMED EMERGENCY EVACUATION SLIDE MECHANISM OPS TEST IN REF TO E190 AMM 52-42-40,52-42-51,52-42-53 SATISFACTORY. NOTE: THE DIAPHRAGM WAS REPLACED AGAIN AFTER SUCCESSFUL TEST.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 21,370 hrs · 13,128 cycles
ON HEAVY MX CHECK, FOUND SEAT TRACK CORRODED FRAMES 13 AND 14. CUT OUT DAMAGED PORTION OF SEAT TRACK. HFEC INSPECTED, FABRICATED FILLER AND DOUBLER, ALODINED, PRIMED AND TOPCOATED. WET INSTALLED REPAIR PARTS, REINSTALLED ITEMS REMOVED FOR FOM IAW E13-602-01.
2012
Part: LINE — DISCONNECTED (BLEED AIR SYS) · airframe 16,579 hrs · 10,131 cycles
FLT 1211 BOS-BUF, AIR RETURN TO BOS DUE TO A BLEED 1 OVERPRESSURE ON EICAS IMMEDIATELY AFTER TAKEOFF. CREW COMPLIED WITH QRH PROCEDURES AND ISOLATED THE BLEED. THE TECHNICIAN ON T/S FOUND NR 1 BLEED OVERPRESSURE SWITCH MUSCLE LINE DISCONNECTED. RE-INSTALLED MUSCLE LINE PER FIM 36-14-00-810-808-A00.
2011
Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 15,337 hrs · 9,360 cycles
FLT 1796 CUN-FLL, FLIGHT CREW REPORTED R1 DOOR VERY DIFFICULT TO ARM/DISARM. DOOR SEAL ALSO WHISTLING AND GIRT BAR WOULD NOT DISENGAGE FROM AIRCRAFT. TECHNICIAN INSPECTED DOOR AND FOUND GIRT BAR DISENGAGED. REMOVED AND REPLACED R1 DOOR EMERGENCY EVACUATION SLIDE ASSY. GROUND OPS CHECK AND AIR LEAK CHECK IAW AMM 25-65-01 AND AMM 05-50-08 FOUND OK.
Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 14,774 hrs · 8,983 cycles
FLT 1264 AUS-BOS, AIR RETURN TO AUS DUE TO DURING CLIMB THE NR 1 BLEED LEAK LIGHT MESSAGE ILLUMINATED FOLLOWED 3 MINS LATER THE NR 2 BLEED LEAK MESSAGE ILLUMINATE. CREW RAN QRH PROCEDURE. TECHNICIAN FOUND BOTH NR 1 AND NR 2 ENGINE PRECOOLER SEAL DAMAGED. PERFORMED REPAIR TO ENGINE 1 AND ENGINE 2 PRECOOLER SEAL PER EC E11-320-01. RAN BOTH ENG REF 71-00-00, NO FAULTS NOTED.
2010
Part: ACM — FAILED (NR 2) · airframe 12,596 hrs · 7,676 cycles
FLT 607 PWM-JFK, CREW DECLARED EMERGENCY DUE TO DURING DESCENT APPROX 10000FT RECEIVED EMERGENCY CALL FROM THE CABIN, SMOKE IN COCKPIT/CABIN PERFORMED MEMORY ITEMS FOR SMOKE AND STARTED SMOKE CHECKLIST/WITH THE BLEEDS OFF AND CABIN DUMPED SMOKE DISSIPATED. LANDED NO PROBLEMS. ACCOMPLISHED FIM TASK 21-20-00-810-801A FOR SMOKE AND ABNORMAL SMELL IN CABIN FOUND NR 2 ACM FAILED. REMOVED AND REPLACED NR 2 ACM. OPS CHECK NORMAL.
Part: SENSOR — FAILED (LT WING) · airframe 11,420 hrs · 6,925 cycles
FLT 1048 JFK-ROC AIR RETURN TO JFK, A/ICE WING LEAK EICAS MESSAGE DURING INITIAL CLIMBOUT. PERFORMED QRH PROCEDURE AND MESSAGE EXTINGUISHED. REMOVED AND REPLACED NR 4 LT WING ANTI ICE TEMP SENSOR IAW MM 30-11-02. TEST OK.
Part: ACTUATOR — TRIPPED (SLATS) · airframe 11,161 hrs · 6,773 cycles
FLT JB1424-- DURING APPROACH TO PDX SLAT FAIL INFLIGHT, PERFORMED QRH PROCEDURE SLATS THEN OPERATED NORMALLY LANDED WITHOUT INCIDENT. CREW ADVISED ON FOLLOWING QRH FAULT CLEARED NO CURRENT ACTIVE FAULTS WERE NOTED ON EICAS. PDX MX T/S IN CMC FOUND FAULT CODE 27811021ACE ACCOMPLISHED FIM 27-81-00-810-802-A FOR SF-ACE1 AND SF-ACE2 AND PERFORMED OPERATIONAL TEST OF SLAT FLAP SYSTEM. NO FAULT MESSAGE WERE NOTED IAW AMM 27-80-00-710-801-A/500 AND AMM 27-50-00. AIRCRAFT RETURNED TO SERVICE AND FLOWN TO LGB, MX CONTROL ISSUED TSI 4379 FOR TROUBLESHOOTING, LGB MX FOUND 4 EA SLAT ACTUATORS TRIPPED AT NR 8 LEFT, NR 3 RIGHT, NR 4 RIGHT AND NR 7 RIGHT WINGS. REMOVED AND REPLACED ALL FOUR SLAT ACTUATORS IAW AMM 27-81-01 PERFORMED MECHANICAL AND ELECTRICAL RIGGING PER AMM 27-80-00, ALL OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: MONITOR — OUT OF ADJUST (NR 2 ENGINE) · airframe 10,834 hrs · 6,596 cycles
FLT JB115 JFK-MSY AFTER 40 MINS IN FLIGHT AIRCRAFT RETURNED TO JFK DUE TO ENGINE 2 LP VIBRATION REACHED 4.0 UNITS ON CLIMB AND DURING CRUISE REACHED 2.7-2.9 AND SPIKED TO 3.1 WITH YELLOW EICAS MESSAGE. JFK MX PERFORMED IEVM FAN TRIM BALANCE IAW EMM 72-00-00-800-811 AND ENGINE VIBRATION CHECK IAW EMM 72-00-00-760-121 CHECK GOOD AND WITHIN LIMITS PER EMM 72-00-00-760-171. AIRCRAFT RETURNED TO SERVICE.
2009
Part: ALTIMETER — FAILED (NR1 RADAR) · airframe 8,970 hrs · 5,465 cycles
FLT NR721, AFTER TAKEOFF HAD DUAL RA FAILURE WITH TAIL STRIKE PROT FAIL MESSAGE ON EICAS. ADDITIONALLY RA FLAGS WERE DISPLAYED ON THE PFD'S. LANDING GEAR AURAL WARNING WENT OFF CONTINUOUSLY AND COULD NOT BE SILENCED BY LANDING GEAR EXTENSION. RETURNED TO DEPARTURE. PERFORMED FIM TASK 27-03-00-810-897-A, NO CORRELATED FAULTS FOUND. PERFORMED OPS TEST OF RADAR ALTIMETER UNIT NR1 IAW AMM 34-31-01. RADAR ALTIMETER NR1 WOULD NOT REAPPEAR ON CAPT PFD. REMOVED AND REPLACED RADAR ALTIMETER NR1 IAW AMM 34-31-01. OPS CHK OK. A/C FOR SVC.
Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 8,590 hrs · 5,255 cycles
ON EMERGENCY EVAC SLIDE ASSY SCHEDULED T/C E190-25-65-01-720-801 AFT LT FUNCTIONAL TEST EVAC SLIDE PASSED INFLATION TEST BUT SLIDE LAMPS DID NOT ILLUMINATE. REMOVED AND REPLACED LEFT PAX DOOR EMERGENCY EVAC SLIDE IAW T/C E190-25-65-01-400-801-ALH. ALL CHECKS GOOD.
2008
Part: ACM — FAILED (NR 1) · airframe 6,638 hrs · 4,166 cycles
FLT 1082, CLT-JFK, SMOKE IN CABIN. APPROACH TO LANDING AT 2000`, SULPHUR ODOR NOTED IN COCKPIT. FLIGHT ATTENDANT CONFIRMED SMOKE IN CABIN AND ODOR OF SULPHUR. COMPLIED WITH SMOKE/FIRE QRH. UPON INSPECTION FOUND PHYSICAL PACK 1 FAILURE WITH FRAGMENTS IN EXHAUST DUCTING GRILLE. TSD DATA PULLED FOR PACK 1 DATA. (AIR CONDITIONING PACKS-SINGLE). REMOVED AND REPLACED NR 1 PACK ACM IAW AMM 21-51-05 AND HEAT EXCHANGER IAW AMM 21-51-04. OPS CHECK OK. (A)
Part: ACTUATOR — TRIPPED (TE FLAPS) · airframe 6,470 hrs · 4,073 cycles
ON APPROACH, AT 210KIAS FLAPS PLACED TO FLAP 1, FLAP FAIL EICAS MSG, FOLLOWED QRH PROCEDURES FINAL FLAP CONFIGURATION, 0 SLAT 0 FLAP, ORIGINALLY SLATS 3 ONLY AND FLAPS 0. REMOVED AND REPLACED RT IB FLAP OB ACTUATOR IAW MM 27-51-01. OPS CHECK OK.
Part: ACTUATOR — TRIPPED (TE FLAPS)
ON APPROACH, FLAPS PLACED TO FLAP 1, FLAP FAIL EICAS MSG. FOLLOWED QRH PROCEDURES, FINAL FLAP CONFIGURATION, 0 SLAT, 0 FLAP, ORIGINALLY SLATS 3 ONL AND FLAPS 0. REMOVED AND REPLACED RT IB FLAP OB ACTUATOR (NR 2 RT)IAW MM 27-51-01. OPS CHECK OK. (K)
Part: MODULE — MALFUNCTIONED (COMMS)
DECLARED EMERGENCY, THE SPDA FAIL EICAS APPEARED IN FLIGHT ON THE ELEC PG THE AC BUSS TIE, APU ICON, AC BUSS 2, TRU, DC BUSS 2. DC US ICON FLASHED FROM GREEN POWERED TO DASHES. COMPLIED W/QRH PROCEDURE. AFTER LDG ENG 1, 2 NO DISPLAY MSG AND CARGO FIRE PROT FAULT APPEARED AFTER LDG. REPLACED SPOA COMMS MODULE SLOT 8 SPDA, NR 2, MM 24-61-07-400-301-A. (K)
2006
Part: SENSOR — FAULTY (TE FLAPS) · airframe 1,282 hrs · 870 cycles
FLAPS FAIL EICAS DURING DESCENT. PERFORMED LANDING WITH FLAPS AT ZERO AFTER COMPLYING WITH QRH. FOLLOWED FIM 27-51-00-810-804A BOTH THE FIM TASK AND FAULT CODE 27S12009ACE IDENTIFY THE LT OB SKEW SENSOR AT FAULT. REMOVED AND REPLACED LT OB SKEW SENSOR IAW MM 27-53-06.
Part: FLAP — OPEN (R1 DOOR) · airframe 252 hrs · 179 cycles
UPON CLIMBOUT NOTICED LOUD VIBRATION NOISE OF F/O'S RIGHT SIDE. NOTICED A/C HAD NOT PRESSURIZED ONLY SHOWING A CAB ALT OF 100 FEET AT 13000 MSL. EICAS INDICATION SHOWED CABIN ALT -300 CABIN RATE -750, A PRESS OF 2.6 PSI AND A LFE OF 0. A/C NEVER PRESSURIZED, AND INDICATIONS WERE NEVER NORMAL UNTIL LANDING. PERFORMED OPERATIONAL TEST OF CABIN PRESSURE CONTROL SYSTEM PER AMM 21-30-00. ALL CHANNELS CHECK GOOD. MANUALLY PRESSURIZED AIRCRAFT ON THE GROUND AND PRESSURIZATION SYSTEM OPERATED NORMALLY. UNABLE TO DUPLICATE ISSUE. SUSPECT VENT FLAP AT R1 DOOR NOT CLOSED. CMC RECORDED NO FAULTS OR EICAS MESSAGES OF THIS EVENT.