N236JB
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.
92 reports on file, 2006-12-14 – 2024-03-04.
Part: CROSSBEAM — CORRODED (FRM 17) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING]: CORROSION ON PREVIOUS REPAIRED CROSS BEAM LOCATED BTW FR17 AND Y=250LH TO Y=1080RH AT FWD FUSELAGE FLOOR STRUCTURE; REF. TOMEX NR-00178/JETBLUE WO1284057 NR00022 SUMMARY: CORROSION ON CROSS BEAM LOCATED BTW FR17 AND Y=250LH TO Y=-1080RH AT FWD FUSELAGE FLOOR STRUCTURE. WAS REMOVED PER EMB-190 SRM 51-10--03 AND SRM 51-12-01 AND IT WAS MEASUREDAND EVALUATED OUT OF. (CONSIDERED A MAJOR REPAIR)
Part: BEAM — CORRODED (FRMS 85-87 S17AL) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION:[CPCP FINDING] CORROSION ON LOWER BEAM BTW FR 85/87 AND STGR 17A (LH) ON AFT PASSENGER DOOR CUTOUT STRUCTURE.; REF TOMEX NR 00214;JETBLUE WO 1284057 NR-00025:SUMMARY:CORROSION ON LOWER BEAM BTW FR 85/87 AND STGR 17A (LH) ON AFT PASSENGER DOOR CUTOUT STRUCTURE WAS REMOVED PER EMB 190 SRM 51-12-01,EMB 190 SRM 51-10-03, WAS MEASURED AND EVALUATED OUT LIMITS PER EM". (CONSIDERED A MAJOR REPAIR)
Part: FLOORBEAM — CORRODED (FRM 14) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR STRUCTURE CROSS BEAM @ FR14 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
Part: CROSSBEAM — CORRODED (FRM 14) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING]: CORROSION ON CROSS BEAM LOCATED BTW FR14 AND Y=310RH TO Y=770RH AT FWD FUSELAGE FLOOR STRUCTURE.; REF. TOMEX NR00182/JETBLUE WO1284057 NR00021. CORROSION ON CROSS BEAM LOCATED BTW FR14 AND Y=310RH TO Y=-770RH AT FWD FUSELAGE FLOOR STRUCTURE WAS REMOVED PER EMB-190 SRM 51-12--01 AND SRM 51-10-03, IT WAS MEASURED ANDEVALUATED OUT OF LIMIT. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — NONE (LT WING) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / TE UPPER REAR SKIN / RIB 14-16 & RIB 17-19 / SRM DEVIATION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
Part: FLOOR SUPPORT — CORRODED (FRMS 13-19) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION (CPCP FINDING): CORROSION ON BEAM LOCATED BTWN FR13-19 AND Y=260LH AT FWD FUSELAGE FLOOR STRUCTURE; REF TOMEX NR00173 / JETBLUE WO1284057 NR-00013: CORROSION ON BEAM LOCATED BTWN FR13-19& Y=260LH AT FWD FUSELAGE FLOOR STRUCTURE WAS REMOVED PER EMB-190 SRM51-10-03;51-12-01, WAS MEASURED AND EVALUATED OUT OF LIMITS PER EMB-190 SRM 53-10-10 AD/51, THEREFO. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 82 S28-29R) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: REF. TOMEX NR00223 INITIAL INSPECTION: (CPCP FINDING) CORROSION ON SHEAR CLIP FR 82 BTW STGR 28R/29R AT AFT CARGO COMPARTMENT; REF TOMEX NR-00223/ JETBLUE WO 1284057 NR-00016:SUMMARY: CORROSION ON SHEAR CLIP FR 82 BTW STGR 28R/29R AT AFT CARGO COMPARTMENT. WAS REMOVED PER EMB-190 SRM 51-12-01 AND EMB-190 SRM 51-10-03 AND EVALUATED, IT IS OUT OF WITHIN LIMITS PER EMB 190 SRM.(CONSIDERED A MAJOR REPAIR)
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR CROSS BEAM X=3301.3 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
Part: FLOORBEAM — CORRODED (FRM 17) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / CROSSBEAM / BTWN FR17 & Y=250 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 83 S27-28L) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION(CPCP FINDING): CORROSION ON SHEAR CLIP FR83 BTWN STRG 27L-28L AT AFT CARGO COMPARTMENT; REF TOMEX NR 00225: CORROSION ON SHEAR CLIP FR83BTWN STRG27L/28L @ AFT CARGO COMPARTMENT WAS REMOVED PER EMB-190 SRM51-12-01;51-10-03 & EVALUATED OUT OF LIMITS PER EMB190 SRM 51-75-16. THEREFORE IT WAS REPLACED PER EMB 190 SRM-51-41-01;51-41-02;51-43-03.(CONSIDERED A MAJOR REPAIR)
Part: FLOOR SUPPORT — CORRODED (FRM 84) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION:[CPCP FINDING] CORROSION ON UPPER SHEET BTW FR84 AND Y=300 APPROX (LH) AT CABIN FLOOR STRUCTURE W2.; REF. TOMEX NR-00208/ JETBLUEWO1284057 NR-00026. SUMMARY:CORROSION ON UPPER SHEET BTW FR84 AND Y=300 APPROX (LH) AT CABIN FLOOR STRUCTURE W2 WAS REMOVED PER EMB 190 SRM 51-12-01, EMB 190 SRM 51-10-03, WAS MEASURED AND EVALUATED OUT LIMITS PER EMB190 S"(CONSIDERED A MAJOR REPAIR)
Part: STRINGER — NOT REPORTED (S28R) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: IN REF TO R.C. 526:E22-1020-02: REPLACE STRINGER 28RHS P/N 170-85163--001.; REPLACE PER EMB 190 SRM 51-41-02 AND SRM 51-43-03 ALL WORK ACCOMPLISHED ON TOMX WO 2494 NR 00273.
Part: FLOORBEAM — CORRODED (FRM 16) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING]: CORROSION ON CROSS BEAM LOCATED BTW FR16 AND Y=1000LH TO Y=1170LH AT FWD FUSELAGE FLOOR STRUCTURE; REF. TOMEX NR00169/ JETBLUE WO 1284057 NR-00017 SUMMARY: CORROSION ON CROSS BEAM LOCATED BTW FR16 AND Y=1000LH TO Y=-1170LH AT FWD FUSELAGE FLOOR STRUCTURE WAS REMOVED PER EMB 190 SRM 51-12--01,SRM 51-10-03, WAS MEASURED AND EVALUATED OUT OF LIMITS PER EMB-190 SRM 51--75-16 AND NE 03-071, THEREFORE WAS REPAIRED PER ETI-190-24-035 REV ORIG AND ETD2024-190-004120 REV:/. WORK PERFORMED BY TECH. J. LUNA#10000210; INSPECTED BY J. GUTIEREZ # 10001841.
Part: SHEAR TIE — CORRODED (FRM 76 S28-29R) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: REF TOMEX NR00222:INITIAL INSPECTION: (CPCP FINDING) CORROSION ON SHEAR CLIP FR 76 BTW STGR 28R/29R AT AFT CARGO COMPARTMENT; REF. TOMEX NR 00222 / JETBLUE WO 1284057:CORROSION ON SHEAR CLIP FR 76 BTW STGR 28R/29R AT AFT CARGO COMPARTMENT WAS REMOVED PER EMB190 SRM 51-12-01, SRM 51-10-03, WAS MEASURED AND EVALUATED PER OUT OF LIMITS PER EMB190 SRM 51-75-16, THEREFORE WAS REPLACED.(CONSIDERED A MAJOR REPAIR)
Part: STRINGER — CORRODED (FRMS 76-77 S29R) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: (CPCP FINDING) CORROSION ON STGR 29R BTW FR 76/77 AT AFT CARGO COMPARTMENT.; REF. TOMEX NR-00227/ JETBLUE W01284057 NR-00019. CORROSION ON STGR 29R BTW FR 76/77 AT AFT CARGO COMPARTMENT WAS REMOVED PER EMB-190 SRM 51-10--03, SRM 51-12-01, WAS MESURED AND EVALUATED OUT LIMITS PER EMB 190 SRM 53-23-- 03AD\51, THEREFORE W. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 83 S27-28L) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: (CPCP FINDING) CORROSION ON SHEAR CLIP FR 83 BTW STGR 27L/28L AT AFT CARGO COMPARTMENT; REF. TOMEX NR 00-00224/ JETBLUE NR 0018. SUMMARY: CORROSION ON SHEAR CLIP FR 83 BTW STGR 27L/28L AT AFT CARGO COMPARTMENT WAS REMOVED PER EMB--190 SRM 51-12-01 AND EMB-190 SRM 51-10-03 AND EVALUATED OUT OF LIMITS PER EMB 190 SRM 51-75-16. THEREFORE. (CONSIDERED A MAJOR REPAIR)
Part: FLOOR SUPPORT — CORRODED (FRMS 12-17) · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING]: CORROSION ON BEAM LOCATED BTW FR12/17 AND Y=260RH AT FWD FUSELAGE FLOOR STRUCTURE; (RESOLVED ON W/O: 1284057 TASKCARD: NR-00024) REF. TOMEX NR-00186 JETBLUE WO1284057 NR-00024.SUMMARY CORROSION ON BEAM LOCATED BTW FR12/17 AND Y=260RH AT FWD FUSELAGE FLOOR STRUCTURE. WAS REMOVED PER EMB-190 SRM 51-12-01 AND SRM 51-10-03 AND EVALUATED, IT IS OUT OF LIMITS PER EMB 190 SRM 53-10-10 AD\51 AND REPLACED PER EMB--190 SRM 51-41-01, SRM 51-41-02 , SRM 51-43--01 AND SRM 51-43-02. WORK PERFORMED BY TECH #E.BERMEJO#337318; INSPECTED BYJ.GUTERIERREZ # 10001841.
Part: BEAM — CORRODED (FRMS 87-88) · corrosion level 2 · airframe 45,112 hrs · 29,303 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION:[CPCP FINDING] CORROSION ON BEAM BTW FR87/88 AND Y=300 APPROX (RH) AT CABIN FLOOR STRUCTURE W2.; REF. TOMEX NR-00196/JETBLUE WO 1284057 NR-00027.SUMMARY:CORROSION ON BEAM BTW FR87/88 AND Y=300 APPROX (RH) AT CABIN FLOOR STRUCTURE W2 WAS REMOVED PER EMB 190 SRM 51-12-01, EMB 190 SRM 51-10-03, WAS MEASURED AND EVALUATED OUT LIMITS PER EMB 190 SRM.(CONSIDERED A MAJOR REPAIR)
Earlier reports · 2006–2023 · 74 reports
2023
Part: SLIDE — FAILED (L2-SLIDE) · airframe 44,765 hrs · 29,072 cycles
FLT#146, CLT-BOS. 'FOUND L2 DOOR SLIDE LACI9NG PIN HANGING FROM DOOR & LACING PARTIALLY UNRAVELED; REPLACED L2 DOOR SLIDE PER AMM 25-65-01.'
Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 44,464 hrs · 28,838 cycles
FLT#1105, JFK-ORD. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' AT FL 220 W/ICINGS WE HAD A BLEED 2 FAIL EICAS. THIS LED TO THE CABIN LOSING PRESSURE. IT ENDED UP COMING BACK ON ONCE WE TURNED APU ON; TROUBLESHOT PER FIM TASK 36-10-00-810-810A. REMOVED AND REPLACED #2 NAPROSOV. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME. OK FOR CONT SVC. MULTIPLE BLEED CHECKS PERFORMED UNABLE TO DUPLICATE FAULT. REF AMM 36-11-03.'
2022
Part: STRINGER — CORRODED (FRMS 88-89 S28R) · airframe 42,289 hrs · 27,239 cycles
DURING HEAVY MAINTENANCE, STRINGER 28R BETWEEN FR 88-89 CORRODED. TEMP REPAIRED. MAJOR REPAIR.
Part: DOUBLER — CORRODED (WASTE PANEL) · airframe 42,289 hrs · 27,239 cycles
DURING HEAVY MAINTENANCE, CORROSION IN THE INTERNAL DOUBLER OF WASTE PANEL. CORRODED DOUBLER WAS REMOVED IAW SRM 51-12-03, 51-10-03. EVALUATED OUT OF LIMITS. REPAIRED IAW SRM 53-23-60- R51.
Part: STRINGER — CORRODED (FRMS 88-89 S28R) · airframe 42,289 hrs · 27,239 cycles
DURING HEAVY MAINTENANCE, STRINGER 28R BETWEEN FR 88-89 CORRODED. REPAIRED. MAJOR REPAIR.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 42,190 hrs · 27,172 cycles
FLT#1602, JFK-BUF. 'EMER LIGHT BATT FAULT; REMOVED AND REPLACED FWD R/H ELPU PER AMM 33-50-01. PERFORMED OPS CHECK. NO FAULTS NOTED. PERFORMED ELPU CHARGE PER AMM 33-50-01-800-801A. A/C OK FOR CONTINUED SERVICE.'
Part: NONE — NONE · airframe 42,086 hrs · 27,105 cycles
FLT#2286, PIT-BOS. 'EMER LIGHT FAULT MESSAGE; PERFORMED RESET IAW AMM 33-50-00. NO-FAULT NOTED. ADVISED MCC BOB.'
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 40,260 hrs · 27,084 cycles
FLT#732, LGA-BOS. ' EMER LY BATT FAULT INTERMITTENT EICAS; REMOVED AND REPLACED ER LIGHT POWER UNIT IAW AMM 33-50-01-000-801-A. OPS CHECK OK.'
Part: NONE — FAILED (ATT PANEL FWD) · airframe 41,983 hrs · 27,014 cycles
FLT#532, LGA-BOS. 'EMRG LT BATT FAULT EICAS MSG ON EICAS MULTIPLE TIMES OFF AND ON, STARTED AT BRAKE RELEASE FOR PUSHBACK. STAYED ON FOR 5-10 MINUTES AT A TIME THEN OFF FOR A FEW SECONDS AND BACK ON AGAIN; PERFORMED TEST OF MAU2 GIO2A AND GIO1A MODULE TEST PASSED. PERFORMED WIRE CHECK AND FOUND OK. REMOVED AND REPLACED FWD ATTENDANT PANEL. OPS CHECK GOOD, NO FAULT PRESENT IAW AMM 25-25-01 AND FIM 33-50-00-810-801-A.'
Part: NONE — NONE · airframe 41,961 hrs · 27,001 cycles
FLT#515, BOS-RSW. 'EMER LT BATT FAULT EICAS MESSAGE; T/S TO FWD R/H EMERG LIGHT BATTERY, GAINED ACCESS AND FOUND CANNON PLUG HALFWAY OUT. RESECURED CANNON PLUG AND OPS CHECK GOOD REF AMM 33-50-00 & 01.'
Part: SHIMMY DAMPENER — FAILED (LMLG) · airframe 40,725 hrs · 26,124 cycles
FLT # 1955. BOS-DCA. L MAIN LANDING GEAR SCISSORS LINKS HAVE SEPARATED; REMOVED AND REPLACED LH LANDING GEAR SHIMMY DAMPNER. ALL WORK AMM 32-11-03.
2020
Part: SLIDE — MALFUNCTIONED (R2 DOOR) · airframe 38,366 hrs · 24,665 cycles
FLT 6206, ORD-JFK. R2 DOOR ARMING LEVER FROZEN IN ARMED POSITION (REPEAT) FOUND TRASH IN LOWER GIRT BAR FITTINGS PREVENTING UNLOCKING OF DOOR OPENED DOOR AND REMOVED TRASH DOOR ARMS AND DISARMS NORMAL, PER AMM 52-42-00. REF TS ENTERED ON 12-01-20. FOUND R2 DOOR SLIDE DISARMED JAMMED. REMOVED R2 DOOR SLIDE. INSTALLED GIRT-BAR WITHOUT SLIDE AND OPERATIONS CHECK DOOR. R2 DOOR ARMED AND DISARMED WITHOUT ANY PROBLEMS. DETERMINED PROBLEM OCCURRED AFTER R2 DOOR SLIDE INSTALLATION ON 11-6-20. FOUND RT NUTPLATE DAMAGED ON SLIDE, REF AMM 25-65-01. ITEM REMAINS OPEN. SLIDE NIS IN JFK. AFTER REPLACING R2 DOOR SLIDE ASSEMBLY, REF 2954260 ITEM 2 ARMING LEVER NOW WORKING PROPERLY, IAW AMM 52-42-20.
Part: BELLCRANK — LACK OF LUBE (R2 GIRT BAR) · airframe 38,341 hrs · 24,652 cycles
FLT 518, JFK-BOS. R2 DOOR IS NOT DISARMING. CLEANED AND LUBRICATED R2 GIRT BAR BELLCRANK ASSEMBLY, PER AMM 52-12-41. OPERATIONS CHECK OK. A/C OK FOR CONTINUED SERVICE.
2019
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 37,043 hrs · 23,761 cycles
LEFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R THE NR 4 ELPU IAW AMM 33-50-01. OK FOR SERVICE.
Part: LIFE RAFT — DAMAGED (FWD) · airframe 35,665 hrs · 22,814 cycles
FT # 1615, LIFE RAFT IN FWD OF AIRPLANE NEEDS RE-LACING; R & R LIFE RAFT IN FWD GALLEY IAW AMM 25-66-01-400-801-A.
2018
Part: SKIN PANEL — CRACKED (RT WING) · airframe 33,467 hrs · 21,245 cycles
DURING HEAVY MAINTENANCE AT SAL, FOUND WITH A CRACK IN THE RT WING LOWER FWD SKIN PANEL P/N 190-33061-010 AT RIB 9 AND STR 19/STR 20 AREA. THE CRACK MEASURES 2.158 INCH. THIS CRACK RESULTED IN FUEL LEAK IN THIS AREA. SEE REF/2/ ETD FOR MORE DETAILS. CONTACTED FOR DISPOSITION AND PROVIDED THE REF/2/ ETD REPAIR CONSISTING OF A SKIN CUTOUT, INSTALLATION OF 3 REPAIR DOUBLERS, FABRICATION OF NEW PYLON ATTACH FITTINGS AND RE-ACCOMPLISHMENT OF THE STRINGER 19 RUNOUT PROCEDURE ARE PER THE REF/7/ SB. SINCE THE REF/6/ SB WAS PREVIOUSLY ACCOMPLISHED AND THE ADDITIONAL STRINGER RUNOUT AND CRACK CUT OUT IMPACT THE FAA AD AREA AN GLOBAL AMOC WAS REQUESTED. THE FAA PROVIDED THE REF/8/ AMOC LETTER AS GLOBAL AMOC APPROVAL. THE REF/1/ EA ACCOMPLISHES THIS PROPOSED REPAIR AS PER REF /2/ ETD WITHOUT DEVIATION. THIS REPAIR AFFECTS THE AIRCRAFT WEIGHT AND BALANCE AS STATED IN REF /2/ ETD GREATER THAN 10 LBS THEREFORE MX-79 IS REQUIRED FOR OPS ENGINEERING. EC E18-458-01 ACCOMPLISHES THE REPAIR PER THE REF/1/ THRU REF/5/ DOCUMENTS, WITHOUT DEVIATION. EC E18-458-02 TRACKS THE 12 MONTH DTA LIMITATION PER THE REF/2/ ETD; THIS EC HAS BEEN APPROVED PER THE REF/6/ ANAC FORM AND THE REF/7/ SB-AD DEVIATIONS HAVE BEEN APPROVED VIA THE REF/8/ AMOC LETTER. THIS IS CLASSIFIED AS A MAJOR PERMANENT REPAIR.
Part: SKIN — CRACKED (RT WING) · airframe 33,473 hrs · 21,247 cycles
DURING HEAVY MAINTENANCE, CRACK FOUND RT WING MAIN BOX LOWER SKIN RIB 9 &10. PERFORMED REPAIR IAW EC E18-458-01 & EA 57-0086-18 REV 0. CLASSIFIED AS MAJOR PERMANENT REPAIR.
2016
Part: BEAM — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND FWD CARGO CUTOUT LOWER BEAM AT FR 24" AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLEND OUT, NDT AND TOPCOAT.
Part: BEAM — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD SERVICE DOOR LOWER BEAM, PN 170-03599-005, CORRODED AT FRAME 16 +8.0 AT RBL 45.0, REF BP NON-ROUTINE H4859-0095. REPAIRED IAW EC E16-096-01, REF EAMS NRS H4859-0095.
Part: BEAM — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD CARGO DOOR CUTOUT LOWER BEAM CORRODED FRAME 24 +4.5" AT RBL 16.0". BLENDED AREAS IAW ETD 2016-190-012093, ATTACHED AND EC E16-100-01, REF EAMS H4859-00609.
Part: FRAME — CORRODED (FRAME 88) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
SHEAR TIE CORRODED AT FRAME 88, STR 27 TO 28R. REPLACED THE SHEAR TIE IAW EAMS H4859-00573.
Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA SUPPORT AT FR16, LBL45" CORRODED. REPLACED BRACKET IAW SRM REF 51-43-03 REF EAMS NR H4859-00103.
Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD WET AREA LAV FLOOR DOUBLER AT FRAME 16, LBL 36", REF NR 00104: R & R FWD WET AREA LAV FLOOR DOUBLER FRAME 16, LBL 36 IAW SRM 51-41-02.
Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD WET AREA PANEL SUPPORT FRAME 16, RBL 28, REF NR 00113: R & R PANEL SUP FRAME 16, RBL 28, SRM 51-41-01.
Part: BEAM — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FOUND CORROSION FWD CARGO CUT OUT LOWER BEAM FR 24 + 5.5" AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLENDOUT, NDT, TOP COAT.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD CARGO FINGER DOUBLER, CORRODED AT 7 DIFFERENT LOCATIONS. BLENDED AREAS IAW ETD 2016-190-012135 AND EC E16-101-01.
Part: FLOOR SUPPORT — CORRODED (FRAME 80) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
AFT CARGO FLOOR SUPPORT CORRODED 2" AFT OF FR 80, RBL 21. REPLACED FLOOR SUPPORT IAW EAMS H4859-00584.
Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
AFT PASSENGER DOOR LOWER BEAM 2" AFT OF FRAME 85, LBL47, CORRODED ETD 2016-190-010746 ATTACHED. REPAIRED IAW EC E16-094-01, REF EAMS NR H4859-00093.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD CARGO FWD FINGER DOUBLER FRAME 24 + 12" AT RBL 13.0". REPAIRED BY COMPLYING WITH EA E16-101-01.
Part: PLATE — CORRODED (FRAME 79) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
AFT CARGO AFT FINGER PLATE CORRODED 10" AFT OF FRAME 79, RBL12, ETD 2016-190-012031-A ATTACHED. REPAIRED AS EC E16-103-01, REF EAM SNR H4859- 00583.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT FWD CARGO FWD FINGER DOUBLER FR 24 +10 AT RBL 14.0". REPAIRED BY COMPLYING WITH EA E16-101-01, BLEND OUT, NDT TOP COAT.
Part: PLATE — CORRODED (FRAME 78) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT AFT CARGO FINGER PLATE ON FRAME 78 AT RBL 13.0". REPAIRED BY COMPLYING WITH EA E16-099-01, BLEND OUT NDT AND TOP COAT.
Part: FLOOR SUPPORT — CORRODED (FRAME 15) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD WET AREA PANEL SUPPORT FR 15, RBL 28, REF NR 00112: R & R PANEL SUPPORT FRAME 15, RBL 28, SRM 51-41-01.
Part: FINGER DOUBLER — CORRODED (FRAME 25) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD CARGO FWD FINGER DOUBLER ON FRAME 25 AT RBL 13.0 HAS CORROSION. REPAIRED BY COMPLYING WITH EA E16-101-01, BLEND OUT, NDT AND TOPCOAT.
Part: BEAM — CORRODED (FRAME 26) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION AT FWD CARGO CUTOUT LOWER BEAM FRAME 26 +10.0" AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLENDOUT, NDT AND TOPCOAT.
Part: FLOORBEAM — CORRODED (FRAME 13) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD WET AREA RT FWD SILL 4 IN AFT OF FRAME 13, RBL 38. R & R FWD WET AREA RT FWD SILL IAW SRM 51-41-02, 51-43-04.
Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA RT SILL. 11" AFT OF FRAME 18, CORRODED. BLENDED AREA IAW E16091-01. REF TO EAMS NR H4859-00119.
Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA RT FLOOR SPLICE CORRODED, 1" IN AFT OF FRAME 18, RBL 28. BLENDED AREA IAW EC E16-091-01. REF TO EAMS NR H4859-00115.
Part: BEAM — CORRODED (FRAMES 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD SERVICE DOOR LOWER BEAM FRAME 16 +10.0" AT RBL 45.0". REPAIRED BY COMPLYING WITH EA E16-096-01, BLEND OUT NDT TOPCOAT.
Part: PLATE — CORRODED (FRAME 78) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT AFT CARGO FINGER PLATE AT FRAME 78 +3.0 AT RBL 14.0". REPAIRED BY COMPLYING WITH EA E16-099-01, BLEND OUT, NDT AND TOP COAT.
Part: STRAP — CORRODED (FRAME 85) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
AFT PASS DOORBEAM STRAP 2" AFT OF FRAME 85, LBL47" CORRODED. REPAIRED IAW EC E16-090-01 REF EAMS NR H4859-00092.
Part: FLOORBEAM — CORRODED (FRAME 12) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FORWARD WET AREA RT FLOORBEAM 8" AFT OF FRAME 12, RBL 12". REPLACED TRACK IAW SRM REF 51-41-01, REF EAMS NR H4859-00128.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD CARGO FORWARD FINGER DOUBLER FRAME 24 +1.0 " AT RBL 14.0. REPAIRED BY COMPLYING WITH EA E16-101-01, BLEND OUT, NDT AND TOPCOAT.
Part: PLATE — CORRODED (FRAME 77) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AFT CARGO FWD FINGER PLATE AT 6.0" AFT OF FRAME 77 AT RBL 13.0. REPAIRED IAW EC E16-099-01, BLEND OUT, NDT TOPCOAT.
Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD WET AREA PANEL SUPPORT FRAME 17, RBL 28, REF NR 00114: R & R PANEL SUPPORT FR 17, RBL 28, SRM 51-41-01.
Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
AFT PASS DOOR LOWER BEAM 6" AFT OF FRAME 85, LBL47" CORRODED. REPAIRED IAW EC E16-094-01.
Part: FLOOR SUPPORT — CORRODED (FRAME 12) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD GALLEY WET AREA FLOOR SUPPORT CORRODED 2" AFT OF FRAME 12, RBL 15. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.
Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD CARGO SHEAR CLIP AT FRAME 16, STR 26L-27L. REPAIRED BY REMOVING AND REPLACING SHEAR CLIP, REF SRM 51-41-01.
Part: FLOOR SUPPORT — CORRODED (FRAME 12) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA FLOOR SUPPORT AT FRAME 12, RBL 37 CORRODED. REPLACED THE FLOOR IAW SRM REF 51-41-01, IAW EAMS NR H4859-00145.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT FWD CARGO FWD FINGER DOUBLER FRAME 24 +6.0", RBL 13.0". REPAIRED BY COMPLYING WITH EA E16-101-01, BLEND OUT, NDT AND TOPCOAT.
Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA LT SEAT TRACK AT FR 16, LBL 10 CORRODED. INSTALLED DOUBLER IAW SRM IAW 53-10-10, REF EAMS NR H4859-00110.
Part: BEAM — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD CARGO CUTOUT LOWER BEAM HAS CORROSION AT FRAME 24 +7.0 AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLENDOUT, NDT, AND TOPCOAT.
Part: BEAM — CORRODED (FRAME 25) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND ON FWD CARGO CUTOUT LOWER BEAM AT FRAME 25 AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLEND OUT, NDT AND TOPCOAT.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
SHEAR TIE AT FRAME 17, STR 25-26L, CORRODED. REPLACED SHEAR TIE IAW EC E16-137-01.
Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
FWD WET AREA LT SILL AT FRAME 16 CORRODED. BLENDED AREA IAW EC E16-091-01 REF EAMS NR H4859-00102.
Part: BEAM — CORRODED (FRAME 26) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT FWD CARGO CUTOUT LOWER BEAM FRAME 26 +8.0 " AT RBL 16.0". REPAIRED BY COMPLYING WITH EA E16-100-01, BLENDOUT, NDT AND TOP COAT.
Part: PLATE — CORRODED (FRAME 77) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
CORROSION FOUND AT AFT CARGO FWD FINGER PLATE ON FRAME 77 AT RBL 13.0". REPAIRED BY COMPLYING WITH EA E16-099-01, BLEND OUT, NDT TOP COAT.
Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 27,378 hrs · 16,996 cycles
SHEAR TIE AT FRAME 87, STR 27 TO 28R CORRODED. REPLACED SHEAR TIE IAW EAMS H4859-00444.
2015
Part: A/C PACK — FAILED (NR 2) · airframe 27,047 hrs · 16,794 cycles
AIR TURNBACK AT APPROXIMATELY FL 220, SMOKE IN AFT CABIN ALONG WITH BURNING ODOR THROUGHOUT CABIN. SLIGHT ODOR IN COCKPIT 10 MIN LATER. PACK 2 FAIL FOLLOWED BY BLEED 2 FAIL APPEARED. PERFORMED SMOKE/ABNORMAL ODOR IN CABIN/COCKPIT CHECK IAW TSM 21-20-00-810-801A. FOUND NR 2 ACM TO BE AT FAULT MEL APPLIED.
Part: MAU — FAILED (NR 2) · airframe 24,920 hrs · 15,313 cycles
NOSEWHEEL STEERING FAILED ON EICAS UPON LANDING GEAR SELECTED DOWN. CREW DECLARED AN EMERGENCY. R & R NIC PROCESSOR MODULE 3 IAW AMM 31-41-04. NO FURTHER FAULTS.
2014
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,352 hrs · 14,326 cycles
DURING MAINTENANCE CHECK, FOUND LT LOWER AFT EXTERNAL EMERGENCY LIGHT HAS SEVERAL INOPERATIVE LEDS. R & R LIGHT ASSEMBLY IAW AMM 33-50-25. OPS CHECK GOOD.
2013
Part: CONNECTOR — DAMAGED (BLEED SYS) · airframe 21,105 hrs · 12,923 cycles
AIR RETURN DUE TO BLEED 2 LEAK MESSAGE AFTER TAKEOFF. QRH COMPLIED WITH, MESSAGE WENT AWAY AFTER 3 MINUTES. THEN BLEED 2 LEAK MESSAGE RETURNED WITH BLEED 2 OFF. BLEED 1 TURNED OFF IAW QRH. BLEED 2 MESSAGE WAS INTERMITTENT THOUGH ALL BLEEDS WERE OFF. QRH ISOLATION STEPS LED TO ACFT BEING UNPRESSURIZED. DURING TROUBLESHOOTING FOUND CONNECTOR P2146 WITH A BROKEN PIN. R & R CONNECTOR P2146 (CH1) IAW CMM 26-14-53. OP'S CHECK GOOD. PERFORMED LEAK CHK AT RT BLEED LINES. NO LEAKS NOTED OR FAULTS NOTED DURING HIGH POWER RUN.
2012
Part: SIGN — INOPERATIVE (CABIN) · airframe 18,191 hrs · 11,056 cycles
FLT 1019 BOS-JFK, DURING WEEKLY CHECK FOUND L1 DOOR EMERGENCY EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED L1 DOOR EXIT IDENTIFIER SIGN IAW AMM REFERENCE 33-50-15. OPS CHECK GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,200 hrs · 10,584 cycles
FLT 6405 MCO-BNA, ON HEAVY MAINTENANCE CHECK FOUND AFT CABIN LEFT SEAT TRACK AT FR 84 LBL 11.0 (W=82X1 .30" NOMINAL .080 REMAINING .045") AND LBL 11.5" DEFECT SIZE W .59X 1.20" NOMINAL .080" REMAIN .045". COMPLIED WITH TASK CARD E12-371-01 PER N/R 1512. MATERIAL REMOVED 16 PERCENT. REPAIRED BY BELNDING CORROSION AND FABRICATING A REPAIR STRAP. HFEC INSPECTED PERFORMED. FILL REWORKED AREA WITH HYSOL EA9396. INSTALL STRAP USING ORIGINAL FASTENER HOLES AND ADDITIONAL ADDED AS REQUESTED. ALODINE, PRIMED AND TOP COAT ACCOMPLISHED NDT-53-23-00-211-806 PER TASK CARD E12-371-01AND N/R 1512.
Part: BEAM — CORRODED (SERVICE DOOR) · airframe 17,200 hrs · 10,584 cycles
FLT 6405 MCO-BNA, ON HEAVY MAINTENANCE CHECK FOUND AFT SERVICE DOOR LOWER BEAM 4 AFT FR 8 STRINGER 17R AT RIVET HOLE SIZE OF DEFECT. W=.580 X .580 NORMINAL .157" REMOVED .055" MATERIAL REMOVED 35 PERCENT REF N/R 8548. ACCOMPLISHED TASK CARD E12-358-01. REMOVED THE CORROSION BY MEANS OF A SPOT FACE REWORK WITH MINIMAL REDUCTION. HFEC INSP, COUNTERSUNK AND WET INSTALLED RIVET ALODINED PRIMED AND COATED PER E12-358-01.
Part: STRAP — CORRODED (FUSELAGE) · airframe 17,200 hrs · 10,584 cycles
FLT 6405 MCO-BNA, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN CROSS BEAM AT FR 17 RBL 13 THRU RBL 37 STRAP HAD CORROSION, NOT THE CROSSBEAM. REMOVED CORROSION BY REMOVING TEMPORARY STRAP. NO CORROSION FOUND IN CROSSBEAM. REPAIRED AS PER EC E10-252-03.
2010
Part: CIRCUIT CARD — FAILED (NR 1 MAU) · airframe 10,741 hrs · 6,533 cycles
FLT JB1306 EMERGENCY WAS DECLARED AVNX MAU 1A FAIL ON APPROACH INTO JFK AT 17000 MSL. REMOVED AND REPLACED MAU 1 NIC 1 PROC CARD REF 31-41-04, AFTER FOLLOWING FIM TASK 45-45-00-710-939-1 AND FIM TAK 31-42-00-810-808A. OPS CHECK OK, REFERENCE LOG 710936.
2009
Part: SENSOR — FAILED (LE SLAT) · airframe 8,851 hrs · 5,425 cycles
FLT 1422 - LGB-PDX, "SLAT FAIL" UPON SELECTING FLAP 1 ON APPROACH. SLATS FAILED TO MOVE AND DISPLAYED AN AMBER "0" POSITION INDICATION. QRH PROCEDURE APPLIED AND FAILURE PERSISTED. REMOVED AND REPLACED LT OUTBOARD SCREW SENSOR 2 AND 3 PER 27-83-01. OPS CHECK NORMAL. NO FAULT PRESENT.
2007
Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP) · airframe 4,004 hrs · 2,664 cycles
FLT 1052, JFK-PIT, IN CRUISE SLAT FAIL MESSAGE NOT ASSOCIATED WITH MOVEMENT OF THE FLAP HANDLE. FLAP HANDLE WAS IN 0 DETENT AND SLATS FLAPS DID NOT DEPLOY. SLATS DID NOT DEPLOY WHEN COMMANDED, FLAPS DROVE TO SELECTED DETENT. FAULT FOUND AS TRANSITORY CONDITION OF SUFACE OPERATION TEST OF FLAPS AND SLATS NORMAL. SLAT FLAP HANDLE WAS REPLACED AS PRECAUTIONARY.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 2,482 hrs · 1,708 cycles
FLT 908, ORD-JFK FLAP FAIL ON APPROACH. REF FIM 27-51-00-810-802. ACCOMPLISHED ACE NR 1 & 2. RESET CYCLED FLAPS SEVERAL TIMES. NO DEFECTS NOTED ACTIVE FAULT CODE 2-81-00-810-805-A00.
Part: SENSOR — FAILED (LT OB SLAT) · airframe 2,480 hrs · 1,707 cycles
FLT 907, JFK-ORD, SLAT LO RATE MESSAGE ON EICAS, FIRST APPEARED AFTER TAKEOFF ON FLAP RETRACTION. SLAT FAIL MESSAGE DURING FLAP EXTENSION. SLAT FAILED BETWEEN LEVER POSITION TO 0 AND 1. PERFORMED SYSTEM TEST IAW FIM TASK 27-53-00-810-803A & IAW FIM TASK 27-53-00-804A, SYSTEM OPS CHECKS GOOD, NO DEFECTS NOTED. TSI N236TO1018 TROUBLESHOOTING OF SLAT FAIL ASSIGNED. COMPLIED WITH TSI 236TO1018, REMOVED & REPLACED SLAT SKEW SENSOR LEFT REF AMM 27-83-01, OPS CHECK GOOD AT THIS TIME.
Part: SENSOR — FAULTY (SLAT SYSTEM) · airframe 2,448 hrs · 1,687 cycles
FLT 1046, WHILE RETRACTING FLAPS OUT OF BNA, RECEIVED -SLAT LO RATE- MESSAGE. WHEN EXTENDING FLAPS IN JFK, RECEIVED -SLAT FAIL- MESSAGE. TSI PREVIOUSLY ASSIGNED FOR TROUBLESHOOTING OF SLAT FAIL MESSAGE. PERFORMED TROUBLESHOOTING REF TSI N236 101011. REMOVED & REPLACED SLAT 3 & 4 SKEW SENSOR AS PER AMM 27-83-01 AND REMOVED AND REPLACED SLAT HARNESS W511, N512 AS PER AMM 27-83-07. PERFORMED OPS CHECK. OPS CHECK SATISFACTORY.
Part: SLAT SYSTEM — FAILED (LE SLATS) · airframe 2,450 hrs · 1,688 cycles
FLT 1048, BNA TO JFK, SLAT FAIL. FAULT CODE 27511013EACE PRESENT. PERFORMED FIM TASK 27-81-00-810-805-. CLEARED SF-ACE INHIBITS AS PER AMM 45-45-00. PERFORMED OPS CHECK OF SLAT SYS IAW AMM 27-83-00. ALL FUNCTIONS NORMAL. NO FAULTS ON EICAS.
2006
Part: CIRCUIT CARD — FAULTED (MAU1) · airframe 1,200 hrs · 867 cycles
ON APPROACH THE LDG HANDLE WAS PLACED DOWN, RECEIVED A EICAS WARNING MSG -LDG LEVER DISAG- REF QRH AND CYCKED TGE HANDLE WITH THE SAME MESSAGE. AGAIN REF QRH AND USED ELECTRICAL OVERIDE SWITCH AND GEAR CAME DOWN WITH NORMAL INDICATIONS. TROUBLESHOT TO PSEM 1, REPLACED PSEM 1 PER AMM 32-61-01, PERFORMED LANDING GEAR EXTENSION & RETRACTION FUNCTIONAL TEST PER AMM 32-33-00, OPS CHECK GOOD, NO FAULTS NOTED. OK TO RETURN TO SERVICE.