N318JB
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
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.
90 reports on file, 2011-03-24 – 2024-07-24.
Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,027 hrs · 24,211 cycles
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 11 AT COCKPIT FLOOR STRUCTURE WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB-190 SRM 51-12-01, SRM 51-10-03 AND SRM 51-75-16. COMPLETED BY.
Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,027 hrs · 24,211 cycles
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 SRM 53-10-10 AD54.
Part: BEAM — CORRODED · airframe 36,027 hrs · 24,211 cycles
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, SRM 51-41-02.
Part: BEAM — CORRODED · airframe 36,027 hrs · 24,211 cycles
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 190 SRM 53-10-10/AD51 AND WAS REPAIRED PER EMB 190 ETI-190-24-200 REV.2, ETD2024-190-017662 REV.: A AND EC E24-861-01.
Part: SKIN — CORRODED (ZONE 100) · airframe 36,027 hrs · 24,211 cycles
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: 10000267 - VEGA ALVAREZ, ERNESTO 17/JUL/24 INSPECTED BY: 253312 - HERNANDEZ CISNEROS, JONATHAN 17/JUL/24.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,027 hrs · 24,211 cycles
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 IN ETD) DESCRIPTION: DURING BASIC 6 CHECK ON N318JB (MSN 364) AT QRO DATED JUL2024, CORROSION WAS FOUND AFFECTING THE RH FLOOR TRACK P/N 170-03263-001 BETWEEN FR 12 - 14 AT Y = 300. REFER TO REF /1/ ETI FOR DETAILS. THE CORROSION HAS BEEN BLENDED AND FOUND TO BE NOT APPLICABLE PER SRM 53-10-10/REPAIR 52 SINCE AN REINFORCEMENT AND ADJACENT TRACK SECTIONS COULD INTERFERE WITH THE REPAIR INSTALLATION. EMBRAER WAS CONTACTED FOR ASSESSMENT AND PROVIDED APPROVAL TO PERFORMING A REPAIR PER SRM 53-10-10 / REPAIR 52 WITH DEVIATIONS. THESE INSTRUCTIONS ARE APPROVED BY REF /2/ ETD AS A PERMANENT REPAIR WITH NO POST REPAIR INSPECTION REQUIRED. THIS EC E24-861-01 ACCOMPLISHES PERMANENT REPAIR INSTRUCTION PER THE REF /1/ ETI AND COMPLIES WITH REF /2/ ETD & REF /3/ ANAC WITHOUT DEVIATIONS. SUBSTANTIATION: THIS REPAIR IS APPROVED AS PERMANENT REPAIR PER REF /2/ ETD & REF /3/ ANAC AND IS CLASSIFIED AS MAJOR. (E/C: E24-861-01)
Part: SKIN — CORRODED (ZONE 100) · airframe 36,027 hrs · 24,211 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II & III / FR 73-74 / STGR 28 RH TO 29 LH / LOWER SKIN / CORROSION â PERMANENT REPAIR; REFERENCES: /1/ TOMX ETI-190-24-211 REV 01 /2/ EMBRAER ETD2024-190-018554. DESCRIPTION: AT CURRENT (7/2024) BASIC 6 CHECK FOR N318JB MSN 364 AT QRO, TOMX REPORTED CORROSION AFFECTING THE CENTER FUSELAGE II LOWER REAR SKIN P/N: 190-25004-001 AND CENTER FUSELAGE III LOWER SKIN P/N: 170-91883-005 BETWEEN FR 73 TO FR 74 BETWEEN STGR 28R TO 29L. THE DAMAGES ARE SHOWN IN FIGURE 1 AND 2 OF THE REF /1/ ETI. AS PER THE REF /1/ ETI, TOMX BLENDED OUT THE AREAS IAW SRM 51-10-03 AND FOUND OUT OF THE LIMITS AS PER SRM 52-23-01 AD 51 DUE TO REMAINING THICKNESS LESS THAN 10%. TOMX CONTACTED EMBRAER FOR REPAIR DISPOSITION, EMBRAER PROVIDED THE REF /2/ ETD WHICH CONSISTS OF A DOUBLER AND TRIPLER REINFORCEMENT AS THE PERMANENT REPAIR WITH POST REPAIR INSPECTION REQUIREMENTS. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ ETI AND COMPLIES WITH REF /2/ ETD WITHOUT DEVIATION. EC E24-895-01 IS ISSUED TO ACCOMPLISH THE PERMANENT REPAIR PER THE REF /2/ RDAF. EC E24-895-02 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION REQUIREMENTS (LFEC THRESHOLD= INTERVAL = 7500FC) PER THE REF /2/ ETD AND ANAC FORM. SUBSTANTIATION: THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /2/ETD AND IS CLASSIFIED AS MAJOR. (E/C: E24-895-01)
Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,027 hrs · 24,211 cycles
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 WITHIN LIMITS PER EMB-190 SRM 53-10-10 AD54. COMPLETED BY 10000267 - VEGA ALVAREZ, ERNESTO 10/JU"
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,027 hrs · 24,211 cycles
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 51-10-03 AND SRM 51-75-16.
Part: STRINGER — CORRODED (ZONE 100) · airframe 36,027 hrs · 24,211 cycles
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, SRM 51-10-03, SRM 53-23-03 AD/51, SRM 51-43--04 AND SRM 51-41-02.
Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 36,027 hrs · 24,211 cycles
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.
Part: RIB — CRACKED (ZONE 500) · airframe 36,027 hrs · 24,211 cycles
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.
Earlier reports · 2011–2022 · 78 reports
2022
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,857 hrs · 21,855 cycles
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.
Part: NONE — NONE · airframe 32,150 hrs · 21,351 cycles
FLT#1751, HPN-RSW. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO SAV) 'DURING CRUISE FLIGHT AT 280 FEET AIRCRAFT ANNUNCIATED A BLEED 1 FAIL MESSAGE. AS BLEED 2 WAS DEFERRED AIRCRAFT BEGAN TO DEPRESSURIZE. CREW DONNED 02 MASKS. DECLARED EMERGENCY AND DESCENDED TO 10.000 FEET. GOT BELOW ALTITUD BEFORE 02 MASK DEPLOYED IN CABIN. PRIOR TO BLEED 1 FAIL, THE AIRCRAFT ENTERED ICING CONDITIONS, AND WINGS & ENG ANTIICE WAS ACTIVATED. CREW REQUESTED IMMEDIATE DESCENT TO GET BELOW ICE LEVEL OCCURRED APPROX 1 MIN PRIOR TO BLEED 1 FAIL. PER SYSTEM LOGIC PACK 2 OFF OCCURRED UPON ICE ACTIVATION W/A BLEED DEFERRED; ACCOMPLISHED HIGH POWER ASSURANCE RUNS ON ENG #1 & #2 IAW LMM 72-00-00, BOTH ENG BLEED SYSTEM CHECKS NORMAL. THIS CLEARS MDDR C/N 482994, MX-4 UPDATED, PLACARD REMOVED, MCC NOTIFIED REF LP 3424142 ITEM #1 AND L/P .'
Part: EICAS — FAULT MESSAGE · airframe 32,067 hrs · 21,289 cycles
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.'
Part: EICAS — FAULT MESSAGE · airframe 32,061 hrs · 21,282 cycles
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)
Part: A/C PACK — DIRTY · airframe 31,829 hrs · 21,102 cycles
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 OK. CAN NOT DUPLICATE THE FAULT AT THIS TIME.NO EICAS MSG.THIS CLEARRD MDDR 478035.MX 4 UPDATED.'
Part: NONE — NONE · airframe 31,425 hrs · 20,821 cycles
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 SERV SHADER VALVE. ACCOMPLISHED FULL STRUT SERVICE IAW AMM 12-12-09. VERIFIED NLG TARGETS BY JACKING A/C, TARGETS MADE IA WAMM 32-20-00 & 07-10-01.' (SUPPLEMENTAL TO DESCRIPTION)
2021
Part: DOOR — DIRTY (R2) · airframe 30,446 hrs · 20,170 cycles
FLT 1294, MCO-HPN. R2 DOOR WILL NOT DISARM; CLEANED GIRT ON HOLDS AND REMOVED DEBRIS R2 DOOR CHECKED SERVAL TIMES AND CHECKS GOOD
Part: GIRT BAR — OUT OF ALIGNMENT (R2) · airframe 30,449 hrs · 20,171 cycles
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.
Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 30,451 hrs · 20,172 cycles
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.
Part: DOUBLER — CORRODED (FWD LAV) · airframe 30,441 hrs · 20,168 cycles
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; GMM 8.19.4.1 PAR. 13. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: STRINGER — CORRODED (FRMS 86-87 S28R) · airframe 30,441 hrs · 20,168 cycles
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.
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SKIN — DENTED · airframe 30,441 hrs · 20,168 cycles
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 WITH THE FOLLOWING DIMENSIONS: L=2.000" W=0.940" H=0.040" AND W/H=23.5 THEREFORE OUT OF LIMITS PER EMB 190 53-10-01/AD52 PAR 4 TAB 101 FIG 101 SHEET 1. DAMAGED AREA WAS REMOVED PER EMB-190 SRM 53-10-01 REPAIR 62 PAR. 4 C. (HFEC) INSPECTION WAS ACCOMPLISHED ON WD FUSELAGE SKIN BETWEEN FR--10 / FR-11 AND STGR-14LH / STGR-15LH, NO CRACKS WERE FOUND AFTER REMOVED DAMAGE PER EMB190 NDT MANUAL PART 1, 51-00--00 TASK 51-00-00-916-803-A . REPAIR PARTS WERE MANUFACTURED PER EMB190 SRM 53-10-01 REP.62 STEP 4 D FIG.203. REPAIR PARTS WERE INSTALLED PER EMB190 SRM 51-41-01 PAR.6 AND SRM 51-41-02 PAR.6. REPAIR REQUIRES: FWD FUSELAGE SKIN REPAIR INSPECTION REQUIREMENTS: PERFORM A LOW-FREQUENCY EDDY CURRENT (SDI) NDT PART 6 TASK 51-06-00-250-805-A ON FWD FUSELAGE SKIN BETWEEN FR-10/FR-11 AND STGR-14LH/STGR-15LH TO 20,000 FC OR 26,600 FH OR WHICHEVER OCCURS FIST INSPECTION THRESHOLD AND 20,000 FC OR 26,600 FH OR WHICHEVER OCCURS FIRST INSPECTION INTERVAL PER EMB190 SRM 53-10-01/REPAIR 62P PAR 5.A TABLE 202. INTELLI UPDATED WORK ACCOMPLISHED BY TOMX FUERTE, JESUS ALEJANDRO. CHECKED BY SORO VILLALOBOS, GUSTAVO.
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED (FRM 86 S27-28L) · airframe 30,441 hrs · 20,168 cycles
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 REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-43-01 TOMX MX# 201000259 RII QC# 201532129 LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SKIN — DENTED · airframe 30,441 hrs · 20,168 cycles
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.
Part: FLOORBEAM — CORRODED (PASS CABIN) · airframe 30,441 hrs · 20,168 cycles
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 STRUCTURE LOCATED IN FR 84 FROM Y=400.0 TO Y= 1100.0 PN 190-65282-001 WAS REPLACED PER EMB-190 SRM 51-41-01 PAR 4; SRM 51-41-02 PAR. 4 & PAR. 6; SRM 51-42-02 PAR. 4 & PAR. 5 ; SRM 51-43-04 PAR.4 & PAR.5. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 REPLACED PER EMB 190 SRM 51-41-01 AND SRM 51-41-02 TOMX MX# 201000259 QC RII # 201532129 LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: FLOOR SUPPORT — CORRODED (FWD LAV) · airframe 30,441 hrs · 20,168 cycles
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. 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.
Part: SHEAR TIE — CORRODED (FRM 90 S21-23L) · airframe 30,441 hrs · 20,168 cycles
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.
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 STRINGERS: 27-28L;28-29L;28-29R PER EMB 190 SRM 51-43-05;51-41-01;51-41-02. REFERENCE TOMEX NR'S 451;453;454;454 & JETBLUE NR 0020 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: STRINGER — CORRODED (FRM 90 S23L) · airframe 30,441 hrs · 20,168 cycles
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.
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 LOCATIONS: 27-28L;28-29L REPLACED DUE TO CORROSION PER EMB 190 SRM 51-43-05;51-41-01;51-41-02. REF. TOMEX NR"S 291;447;448;449;450 AND JETBLUE NR 0019 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: STIFFENER — CORRODED (FR 86-87 S27-28L) · airframe 30,441 hrs · 20,168 cycles
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 BETWEEN STRG 27R-28R WAS REPLACED PER EMB-190 SRM 51-41-01 AND SRM 51-41-02 TOMX MX 200802742 RII QC 201532129 LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 REPLACED PER EMB 190 SRM 51-41-01 AND SRM 51-43-03. TOMX MX# 200002656 QC RII# 201532129
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 RII# 201532129 LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 LOCATIONS: 27-28L;28-29L REPLACED DUE TO CORROSION PER EMB 190 SRM 51-43-05;51-41-01;51-41-02. REF. TOMEX NR"S 291;447;448;449;450 AND JETBLUE NR 0019 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 DUE TO CORROSION BETWEEN FR 80-83 @ FOLLOWING STRINGER LOCATIONS: 24-25L;27-28L;28-29L;25-26R;27-28R;28-29R PER EMB 190 SRM 51-43-03;51-41-01-51-41-02. REF TOMEX NRC'S 434;435;436;437;439;440;442;445;593 & JETBLUE NR 0018 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SEAT TRACK — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 AND BTWN FR 84-85 WAS REPAIRED PER EMB 190 SRM 53-23-10/REPAIR 54P. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. REF. TOMEX WO 1708 NRC 00414 AND JETBLUE NR 00023 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: STRINGER — CORRODED (FRMS 85-86 S23L) · airframe 30,441 hrs · 20,168 cycles
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.
Part: ANGLE — CORRODED (FRM 85 S19L) · airframe 30,441 hrs · 20,168 cycles
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 51-43-01 AND SRM 51-43-03.
Part: FLOOR SUPPORT — CORRODED (FWD LAV) · airframe 30,441 hrs · 20,168 cycles
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 PER EMB-190 SRM 51-12-01;SRM51-10-03; 51-75-16. FLOOR SUPPORT WAS REPLACED PER EMB 190 SRM 51-43-03. REF. TOMEX WO 1708 NRC 00373 & JETBLUE NR 0021 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAIR STATION 4TOY762C RII INSP 236812
Part: FLOORBEAM — CORRODED (FRM 84) · airframe 30,441 hrs · 20,168 cycles
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 STRUCTURE LOCATED IN FR 84 FROM Y=400.0 TO Y= 1100.0 PN 190-65282-001 WAS REPLACED PER EMB-190 SRM 51-41-01 PAR 4; SRM 51-41-02 PAR. 4 & PAR. 6; SRM 51-42-02 PAR. 4 & PAR. 5 ; SRM 51-43-04 PAR.4 & PAR.5. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 STRINGERS: 27-28L;28-29L;28-29R PER EMB 190 SRM 51-43-05;51-41-01;51-41-02. REFERENCE TOMEX NR'S 451;453;454;454 & JETBLUE NR 0020 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
Part: SHEAR TIE — CORRODED · airframe 30,441 hrs · 20,168 cycles
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 STRINGERS: 27-28L;28-29L;28-29R PER EMB 190 SRM 51-43-05;51-41-01;51-41-02. REFERENCE TOMEX NR'S 451;453;454;454 & JETBLUE NR 0020 FOR PERTINENT DETAILS. LOG SIGN TOMAX REPAR STATION 4TOY762C RII INSP 236812
2018
Part: SKIN — CRACKED (HORIZ STAB) · airframe 23,310 hrs · 15,330 cycles
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/ ETD. THIS EC IS CATEGORIZED AS TEMPORARY REPAIR AND IS CLASSIFIED AS MAJOR WITH NO POST REPAIR INSPECTIONS.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRAKET SUPPORT BAG LOC AT LEVEL FR76 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED SUPPORT BAG LOCATED AT LEVEL FR76 BTW STR 29R TO STR 29L ON AFT CARGO IAW E190 51-40-08 AND DRAWING 170-65110-453,170-65180-445.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR76 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED SUPPORT BAG LOCATED AT LEVEL FR76 BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW 51-40-08 AND DRAWING 170-65110-453, 170-65180-445.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REPAIR ANGLE OF STR 29R, LOCATED BTW FR 76 AND FR 77, ON AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR (REPLACEMENT) ON STR 29R, LOCATED BTW FR 76 TO FR 78, ON AFT CARGO COMPARTMENT IAW SRM 53-23-03, REPAIR 51, FIG 212. P/N REPLACED 170-65188-003.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REPAIR ANGLE OF STR 29R LOCATED BTW FR76 TO FR77 IN AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STR 29R LOCATED BETWEEN FR76 TO FR78 IN AFT CARGO COMPARTMENT IAW SRM 53-23-03 REPAIR 51 FIG 212.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FRAME 87 LOCATED BTW STR 28R TO STR 29R ON AFT CARGO COMPARTMENT. REPLACED FRAME 87 BETWEEN STR 26R TO STR 26R ON AFT CARGO COMPARTMENT IAW SRM 51-40-08 AND DRAWING 170-65180-445, 170-65110-453.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR75 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED BRACKET SUPPORT BAG LOCATED ON FR75 BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW SRM 51-40-08 AND DWG 470-65180-445.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR74 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED SUPPORT BAG LOCATED AT LEVEL FR74 BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW E190 51-40-08 AND DRAWING 170-65110-453, 170-65180-445.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR78 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED BRACKET SUPPORT BAG LOCATED AT LEVEL FR78 AND BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW SRM 51-40-08 AND DRAWING 170-65180-445.
Part: SKIN SPLICE — CRACKED (RT HORIZ STAB) · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CRACK LOWER SKIN SPLICE LOWER RIB 3 LT TO RIB 3 RT ON HORIZONTAL STABILIZER. PERFORMED TEMPORARY REPAIR ON HORIZONTAL STABILIZER LOWER SKIN SPLICE BETWEEN RIB 3 LT TO RIB 3 RT IAW EA 55-0109-18 REV 0 PART 7 AND PART 2, ETD 1028-190-063342 REV A TI - 170-18-074 AND EC 18-512-01.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR74 BTW STR 29R TO STR 29L ON AFT CARGO. REPLACED SUPPORT BAG LOCATED AT LEVEL FR74 STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW 51-40-08 AND DRAWING 170-65110-453,170-65180-455.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR75 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED SUPPORT BAG LOCATED AT LEVEL FR75 BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW 51-40-08 AND DRAWING 170-65110-453, 170-65182-445.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR CLIP LOCATED AT FR 87, BETWEEN STR 28R AND STR 29R, IN AFT CARGO COMPARTMENT. REPLACED SHEAR CLIP LOC AT FR87 BTW STR 28R TO STR 29R IAW SRM 51-40-08 AND DRAWING 170-65900-445.
Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BRACKET SUPPORT BAG LOC AT LEVEL FR78 BTW STR 29R TO STR 29L ON AFT CARGO COMPARTMENT. REPLACED SUPPORT BAG LOCATED AT LEVEL FR78 BETWEEN STR 29R TO STR 29L ON AFT CARGO COMPARTMENT IAW 51-40-08 AND DRAWING 170-65110-453,170-65180-445.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FRAME 87 LOCATED BTW STR 28R TO STR 29R ON AFT CARGO COMPARTMENT. REPLACED FRAME87 BETWEEN STR 26R TO STR 26L ON AFT CARGO COMPARTMENT IAW SRM 51-40-08 AND DRAWING 170-65180-445, 170-65110-453.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,310 hrs · 15,330 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR CLIP LOC AT FR87 BTW STR 28R TO STR 29R IN AFT CARGO COMPARTMENT. REPLACED SHEAR CLIP LOCATED AT LEVEL FR87 BTW STR 28R TO STR 29R ON AFT CARGO COMPARTMENT.
Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 22,409 hrs · 14,669 cycles
DURING HEAVY MAINTENANCE, INOP ELPU RT SIDE AT AFT GALLEY AREA; REPLACED EMERGENCY LIGHT POWER UNIT AS PER AMM 33-50-01-400-801-A AND PERFORMED OPERATIONAL TEST IS OK AS PER AMM 33-50-01-710-801-A AND OPERATIONAL TEST OF THE EMERGENCY LIGHT IS OK AS PER AMM 33-50-00-710-801-A LOC AFT GALLEY AREA REF NR WO 2018-9/1 WCC 2018-57298. SUPPLEMENTAL INFORMATION TO FOLLOW.
2017
Part: SKIN — CRACKED (RT WING) · airframe 21,564 hrs · 14,065 cycles
DURING HEAVY MAINTENANCE, THE RT WING EXTERNAL LOWER SKIN WAS FOUND CRACKED BETWEEN RIBS 10 AND 11 AT SPAR AREA. ACCOMPLISHED A REPAIR IAW EC E17-972-01.
Part: SKIN — CRACKED (LT WING) · airframe 21,564 hrs · 14,065 cycles
DURING HEAVY MAINTENANCE,, A 1.190 INCH CRACK WAS FOUND BETWEEN RIBS 10 AND 11, AT SPAR 11 OF THE LT WING EXTERNAL LOWER SKIN. ACCOMPLISHED A REPAIR IAW EC 973-01.
Part: UNKNOWN — ODOR (CABIN) · airframe 19,978 hrs · 12,830 cycles
RETURNED TO DEPARTURE, DUE TO SMOKE & FUMES IN THE CABIN AND COCKPIT. VISIBLE WHITE GRAY HAZE. NO EICAS MESSAGES. BEGAN ON CLIMB OUT, ACCOMPLISHED FIM TASK 21-20-00 FOR SMOKE ABNORMAL ODOR. NO SOLID FINDINGS FOUND DURING ANY INSPECTIONS. NOTICED THE LEFT RECIRCULATION FAN CYCLING ON AND OFF SEVERAL TIMES. R & R THE LT RECIRCULATION FAN AND FILTERS. SUSPECT POSSIBLE PRESERVATION FLUID RESIDUE DUE TO FIRST FLIGHT AFTER NR 1 ENGINE REPLACEMENT . PERFORMED 25 MIN ENGINE RUNUP WITH 2 HIGH POWER RUNS. ALL CHECKED OK.
2016
Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
AFT CARGO COMPARTMENT AT FRAME 82 SHEAR TIE CORRODED BETWEEN STRINGERS 26 AND 27R. REPLACED THE SHEAR TIE IAW EC E15-1268-01.
Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
AFT CARGO AT FRAME 82 SHEAR TIE CORRODED ONE INCH AFT OF FRAME BETWEEN STRINGERS 27 AND 28R. REPLACED THE SHEAR TIE IAW REF 51-41-01 AND 51-41-02.
Part: SHEAR TIE — CORRODED (FRAME 85) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
AFT CARGO COMPARTMENT SHEAR TIE AT FRAME 85 BETWEEN STRINGERS 27 AND 28 R CORRODED. REPLACED THE SHEAR TIE IAW SRM 51-41-02 AND 51-43-03.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
AFT FUSELAGE RT GUSSET PLATE AT FRAME 90 RBL 20 CORRODED. REPLACED GUSSET IAW SRM 51-42-02.
Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
STRINGER 29R HAS AREA OF CORROSION EIGHT AND A HALF INCHES AFT OF FRAME 76. REPAIRED IAW TASK CARD NR E16-007-01.
Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
STRINGER 29R HAS AREA OF CORROSION SIX INCHES AFT OF FRAME 76. COMPLIED WITH TASK CARD NR E16-007-01
Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
STRINGER 29R HAS CORROSION FOUR INCHES AFT OF FRAME 76, REPAIRED IAW TASK CARD E16-007-01
Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
STRINGER 29R HAS AREA OF CORROSION TWELVE INCHES AFT OF FRAME 76. REPAIRED IAW TASK CARD NR E16-007-01.
Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
AFT CARGO COMPARTMENT AT FRAME 86 SHEAR TIE CORRODED ONE INCH AFT OF FRAME BETWEEN STRINGERS 27 - 28R; REPLACED THE SHEAR TIE IAW SRM 51-41-01 & 51-41-02.
Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
STRINGER 29R HAS AREA OF CORROSION TEN INCHES AFT OF FRAME 76. COMPLIED WITH TASK CARD NR E16-007-01.
Part: SUPPORT — CORRODED (FRAME 12) · corrosion level 2 · airframe 16,435 hrs · 10,375 cycles
FORWARD FUSELAGE PANEL SUPPORT CORRODED A FRAME 12, RBL 34"; REPLACED SUPPORT IAW SRM 51-41-01.
2015
Part: BLEED AIR SYS — UNKNOWN (NR 1 ENGINE) · airframe 15,743 hrs · 9,895 cycles
FLIGHT DIVERTED, DUE TO ENGINE NR 1 BLEED WOULD NOT OPEN. ACCOMPLISHED ENGINE RUN AND OPERATED NR 1 ENGINE BLEED SEVERAL TIMES WITH NO DEFECT. OPS CHECKED NORMAL IAW AMM 36-10-00. NO ISSUES AT THIS TIME TO REPORT.
Part: ACM — FAILED (NR 1) · airframe 15,735 hrs · 9,888 cycles
DURING LANDING AND GEAR EXTENSION, OBSERVED SMOKE ODOR IN FLIGHT DECK AND UPON LANDING, PACK 1 FAIL EICAS MESSAGE APPEARED. PERFORMED SMOKE INSPECTION IAW FIM 21-20-00-810-801A SUSPECT ACM 1. R & R NR 1 ACM IAW AMM 21-51-05. OPS AND LEAK CHECK GOOD.
2014
Part: STRINGER — CORRODED (FRAMES 86-89) · airframe 10,612 hrs · 6,497 cycles
DURING HEAVY MAINTENANCE CHECK, FOUND FRAMES 86-89 STRINGER 28R CORRODED. COMPLIED WITH SPLICE IN STRINGER IAW E14-017-01.
Part: STRINGER — CORRODED (FRAME 88) · airframe 10,612 hrs · 6,497 cycles
DURING HEAVY MAINTENANCE CHECK, FOUND FRAME 88 STRINGER 27R CORRODED. REPAIRED STRINGER IAW E14-017-01.
Part: SEAT TRACK — CORRODED (FRAME 18) · airframe 10,612 hrs · 6,497 cycles
DURING HEAVY MAINTENANCE CHECK, FOUND FWD FUSELAGE LEFT SEAT TRACK, FRAME 18 CORRODED. REPAIRED IAW SRM 53-10-10. REPAIR 51.
2012
Part: DOOR — OBSTRUCTED (EMERGENCY EXIT) · airframe 5,487 hrs · 3,321 cycles
FLT 6485 JFK-BNA, ON MAINTENANCE CHECK FOUND RT OVERWING EXIT DOOR STUCK. REMOVED RT OVERWING DOOR IAW 52-20-00. INSPECTED AFTER REMOVAL AND FOUND PAINT RESIDUE BETWEEN DOOR SEAL AND CONTACT SURFACE. ALSO FOUND DUST SEAT GLUE IN CONTACT WITH SIDEWALL AREA. CLEANED AND OPS CHECKED NORMAL IAW AMM 52-20-00.
2011
Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 4,037 hrs · 2,482 cycles
FLT 690 DCA-B0S, CREW REPORTED FAINT BURNING SMELL FROM FRONT GALLEY, POSSIBLE COFFEE HEAT PLATE. UNSURE OF SOURCE POTENTIAL, REPEAT WRITE UP. THE TECHNICIAN REMOVED AND REPLACED FWD GALLEY COFFEEMAKER. OPS CHECK, NO BURNING SMELL.
Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 2,174 hrs · 1,320 cycles
FLT 440 MCO-BOS, CREW DECLARED EMERGENCY AND AIRCRAFT RETURN TO MCO DUE TO LOUD VIBRATION/THUMPING BANGING NOISE UNDER COCKPIT FEET AREA EVERY 10-15 SECONDS. SPOILERS SHOWED ARMED IN FLIGHT, NO OTHER INDICATION SPEED BRAKE INDICATION ON. TROUBLESHOOT AND FOUND WX RADAR RECEIVER / TRANSMITTER MAKING A THUMPING SOUND EVERYTIME IT MOVE TO THE LEFT. REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW 34-42-01. OPS CHECK GOOD, NO DEFECTS NOTED, NO FURTHER THUMPING SOUND HEARD.
Part: ACE — FAILED (NR 2) · airframe 2,153 hrs · 1,308 cycles
FLT 1243 BOS-CLT, FLIGHT CREW DECLARED EMERGENCY DUE TO FLAP FAIL, FLIGHT CONTROL NO DISPATCH, WINDSHEAR FAULT, GRN PROX FAIL. AT FAIL, SHAKER ANTICIPATED, AP FAIL, SPOILER FAULT AUTO CONFIG TRIM FAIL. INFLIGHT AUTO PILOT TURNED OFF AND WE DID A O FLAP WITH UNKNOWN SLAT LANDING. REMOVED AND REPLACED SFACE NR 2 ALL FAULTS CLEARED FLAPS OPS NORMAL.