N249JB
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.
147 reports on file, 2006-10-19 – 2024-04-11.
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SEAT TRACK END LH Y= -300 AT CF III FLOOR STRUCTURE. REMOVED CORROSION IAW SRM 51-12-01 AND 51-10-03. DEEMED OUT OF LIMITS IAW SRM 53-23-10 AD51. ACCOMPLISHED REPAIR ON SEAT TRACK END LH Y= -300 AT CF III FLOOR STRUCTURE IAW SRM 53-23-10 REPAIR 54P.(CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (LT WING LE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / FIXED WING LEADING EDGE / RIB 22 / CRACK - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - IAE V2533-A5 - ESN V18656 - PROJECT SHOP VISIT - HPT HUB INSPECTION PER SB 72-0713 - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: UNKNOWN — CORRODED (FRMS 90-91) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / REAR PRESSURE BULKHEAD / LOWER BULKHEAD RING / BTWN FR90-91 & STR 26L-28L / CORROSION - TIME LIMITED REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CORRODED (FRM 74 S29R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II / LOWER SKIN / AT STR 29R BETWEEN FR73 â FR74 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: CROSSBEAM — CORRODED (FRM 17) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / CROSSBEAM / BTWN FR17 & Y=250 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS-RH/ OB FLAP/ LOWER SURFACE RIB 10/ DEBONDING- PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: STOP FITTING — CRACKED (FRM 68 S22R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: FLOOR SUPPORT — CORRODED (FRMS 13-14) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / RH FLOOR TRACK / BTWN FR13-14 & Y=273 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (NONE) · airframe 44,469 hrs · 29,251 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: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: DURING OPERATION TEST ON EMERGENCY WON'T TURN ON EXTERIOR LIGHT ON LH OVERWING LH; EMERGENCY LIGHT POWER UNIT 5 WAS REPLACED PER EMB 190 FIM 33-50-00-810-811-A,AMM 33-50-01-00-801-A,AMM 33-50-01-400-801-A, SATISFACTORY TEST.
Part: FLOOR SUPPORT — CORRODED (FRMS 12-17) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: CENTER RH LONGITUDINAL BEAM FR12-17 FWD FUSELAGE PAX CABIN FLOOR STRUCTURE (W1); REF TOMX W/O N249JB/2525/E190/BRIDGE NR00068: DEEMED OUT OF LIMITS IAW SRM 53-10-10/AD52. R & R RH FLOOR TRACK FWD FUSELAGE PAX CABIN IAW SRM 51-41-01, 51-41-02, 51-43-03, AND 51-43-04. (CONSIDERED A MAJOR REPAIR)
Part: FRAME — CRACKED (FRM 16) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / DOUBLE JOGGLE AREA AT FR16RH / CRACKS - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — GOUGED (FRMS 20-21) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER SKIN / BTWN FR20-21 & STR 27LH-28LH / GOUGES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: BLADE — UNKNOWN (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P771638 - LOW EGTM / HPT BLADE FINDINGS - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: BEARING — LEAKING (NR 4) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - IAE V2527-A5 ESN V12220 - UER - NO. 4 BRG COMPARTMENT OIL LEAK MINIMUM REPAIR AND HUB INSPECTION PER SB72-0713 - PROJECT VISIT. (CONSIDERED A MAJOR REPAIR)
Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P771797 - CABIN ODOR / EVIDENCE OF OIL IN HPC1 AND HPC2 WEEP HOLE - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: HINGE ARM — UNKNOWN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 77 S28-29L) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR77 STR28-29L AFT CARGO; REF TOMX W/O N249JB/2525/E190/BRIDGE NR00100: DEEMED OUT OF LIMITS IAW SRM 51-10-03, 51-12-01, AND 51-75-16. R & R SHEAR CLIP @ FR77 STR28-29L IAW SRM 51-41-01, 51-41-02, AND 51-43-03. (CONSIDERED A MAJOR REPAIR)
Part: OIL SYSTEM — LOW PRESSURE (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P772428 - LOW OIL PRESSURE / IFSD - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — MECHANIC ERROR (FUSELAGE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / UPPER SKIN ABOVE WINDSHIELD FRAME BTWN STGR 4R-5R / MISDRILLED HOLES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CORRODED (FRMS 89-90 S29R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / LOWER SKIN / STGR 29R / FR 89-90 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
Part: SEAL — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1524G - ESN P736406 - NO. 4 COMPARTMENT SEAL OIL LEAK - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: PRESSURE BLKHD — CRACKED (FRM 35 S30L) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — UNKNOWN (VERTICAL STAB LE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322CL / OUTER SKIN / RE-SKIN â STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: STRINGER — CORRODED (FRMS 86-87 S27R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: STR27R FR86/87 CF III; REF TOMX W/O N249JB/2525/E190/BRIDGE NR00110: DEEMED OUT OF LIMITS IAW SRM 53-23-03/AD51. R & R STR27R +CTLIII IAW SRM 51-41-01, 51-41-02, 51-43-03, AND 51-43-04.(CONSIDERED A MAJOR REPAIR)
Part: DOUBLER — CORRODED (FRMS 88-89) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING, CORROSION ON DOUBLER LOCATED BTW FR88/FR89 AND STGR 28R/25R AT AFT CARGO COMPARTMENT; REF.TOMX WO N249JB/2525/E190/BRIDGE N/R 00102-DOUBLER WAS REPAIRED PER EMB190 SRM 53-23-60/REP 51P.REPAIR INSPECTION METHOD EXTERNAL LFEC-INTERVAL 4009FC. (CONSIDERED A MAJOR REPAIR)
Part: STRUCTURE — PILOT ERROR (TAIL STRIKE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE/ AFT FUSELAGE (SECTIONS 17-19) / TAIL STRIKE DAMAGE â ADDITIONAL INSPECTIONS & TEMPORARY REPAIR FOR MX FERRY. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — DENTED (FRMS 82-84) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / SKIN BETWEEN FR82-84 & STGR 21L023L / DENT - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SEAL — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1524G - ESN P736576 - HOC / SUSPECTED NO. 4 COMPARTMENT REAR SEAL LEAK - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SEAL — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P800674 - WORN #3 CARBON SEAL - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (INSPECTION) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - IAE V2533-A5 - ESN V18630 - PROJECT SHOP VISIT - HPT HUB INSPECTION PER SB 72-0713 - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1524G - ESN P736406 - NO. 4 COMPARTMENT SEAL OIL LEAK - REPAIR WORKSCOPE.(CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 88 S27-28R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR88 STR27-28R AFT FUSELAGE; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00150: DEEMED OUT OF LIMITS IAW SRM 51-10-03, 51-12-01, AND 51-75-16. R & R SHEAR CLIP @ FR88 STR27-28R IAW SRM 51-41-01 AND 51-41-02.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT/ CRACKS- PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: ENGINE — UNKNOWN (UNKNOWN) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - IAE V2533-A5 - ESN V18658 - PROJECT SHOP VISIT - HPT HUB INSPECTION PER SB 72-0713 - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (RT WING) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / RH WING / TRAILING EDGE LOWER SKIN REAR SPAR / RIB 10-12 / CRACK - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 56 S27-28R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR86 STR27-28R AFT CARGO; REF TOMX W/O N249JB/2525/E190/BRIDGE NR00107: DEEMED OUT OF LIMITS IAW SRM 51-10-03, 51-12-01, AND 51-75-16. R & R SHEAR CLIP @ FR86 STR27-28R IAW SRM 51-41-01- AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — DAMAGED (FRMS 1-7) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FWD LOWER SKIN BETWEEN FR1-7 & STGR 24R-25R AND 24L-25L / HAIL DAMAGE - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (INSPECTION) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - IAE V2533-A5 - ESN V18656 - PROJECT SHOP VISIT - HPT HUB INSPECTION PER SB 72-0713 - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CORRODED (LT WING) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / UPPER SURFACE / FRONT SPAR AT RIBS 19-20 / BONDING SPIGOT / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 87 S27-28R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR87 STR27-28R AFT DRAIN DOUBLER; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00133: DEEMED OUT OF LIMITS IAW SRM 51-10-03, 51-12-01, AND 51-75-16. R & R SHEAR CLIP @ FR87 STR27-28R IAW SRM 51-41-01 AND 51-41-02.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR CROSS BEAM X=3301.3 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: STRINGER — CORRODED (FRMS 88-89 S29R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: STR29R FR88-89 AFT CARGO; REF TOMX W/O N249JB/2525/E190/BRIDGE NR00101: DEEMED OUTOF LIMITS IAW SRM 51-75-16. REPAIRED STR29R @ FR88-89 IAW SRM 53-23-03/REPAIR510, EMBRAER ETD2024-190-008437 REV :/, ETI-190-24-085 REV1, AND JETBLUE E/C E24-357-01. (CONSIDERED A MAJOR REPAIR)
Part: POWER SUPPLY — NO TEST · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: EICAS ADVISORY MESSAGE - EMER LT BATT FAULT-; (RESOLVED ON W/O: 1300462 TASKCARD: NR-00032 ) PERFORM TROUBLESHOOTING PER EMB-190 FIM 33-50-00-810-802-A AND REPLACE EMERGENCY LIGHT POWER UNIT ELPU#2 PER AMM 33-50-01-000-801-A, AMM 33-50-01-401-801-A.MDDR CLEARED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - V2533A5 - ESN V18038- PERFORMANCE RESTORATION - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: PANEL — UNKNOWN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322AL / OUTER SKIN / RE-SKIN â STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: ARM — UNKNOWN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: TAIL CONE — DENTED (FRMS 78-80) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR / TAILCONE/DENT BTWN FRAME 78-80 BETWEEN LH STR 1 AND 2 SPLICE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 83 S27-28R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR83 STR27-28R AFT CARGO COMPARTMENT; REF TOMX W/O N249JB/2525/E190/BRIDGE NR-00103: EVALUATED CORROSION AND DEEMED OUT OF LIMITS IAW E190 SRM 51-75-16. R & R SHEAR CLIP FR83 STR27-28R IAW E190 SRM 51-41-01 AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / CARGO DOOR / CARGO DOOR SILL / CORROSION - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — DENTED (FRMS 23-24) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN / BTW FR 23-24 & STGR 15L-16L / PREVIOUS DOUBLER / DENT - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - V2533A5 - ESN V18338- PERFORMANCE RESTORATION - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: FLOORBEAM — CORRODED (FRM 17) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM, FILLER, LOCATED ON FR17, STGR 17R, HAS CORROSION THAT IS BEYOND LIMITS. NOTE: THERE IS NO SPECIFIC SRM LIMIT FOR THIS SPECIFIC PART, THEREFORE IT WAS DETERMINED TO REPLACE IT; REMOVED AND REPLACED FLOOR-BEAM FILLER, LOCATED AT FR 17, STGR 17R, IAW EA 53-0217. REF. AEROMAN NR # 2018-245821. P/N: 170-21769-403. (CONSIDERED A MAJOR REPAIR)
Part: SEAL — LEAKING (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P771470 - #3 BEARING SEAL NESTED - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 87 S27-28R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION ON SHEAR-CLIP, LOCATED AT FR 87, BTW. STGR 27R AND 28R, LWR. FUSELAGE, THAT IS BEYOND ALLOWABLE SRM LIMITS, REMOVED AND REPLACED SHEAR-CLIP (P/N: 170-66041-002) LOCATED AT FR 87 AND BTW. STGR 27R AND STGR 28R (LOWER FUSELAGE) PER E190 SRM: 51-40-08. CROSS-REF. AEROMAN NR# 2018-245826. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / INBD FLAP / LOWER SKIN / DENTS / PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — UNKNOWN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322AL / OUTER SKIN / RE-SKIN â STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (LT WING LE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: AFTER WING LEADING EDGE SKIN REMOVAL, FOUND CRACK ON RIB 22 AT LH WING; REF. TOMX W/O N249JB/2525/E190/BRIDGE N/R 00143 - RIB 22 AT LH WING WAS REPAIRED PER EMB190 ETI-190-24-078 REV.1, ETD 2024-190-008271 AND EC E24-403-01.
Part: SKIN — UNKNOWN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322BL / OUTER SKIN / RE-SKIN â STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: NONE — NONE (NONE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CABIN SYSTEMS - SIFI CABLE P/N N31201-101, RETERMINATIONDEVIATION FROM APPROVED DATA - N526JB. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (LT WING LE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / FIXED LEADING EDGE / RIB 22 / CRACK - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CORRODED (RT WING) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / REAR SPAR - TE OVERHANG / WX3494-WX4490 AND RIBS 9-18 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 75 S28-29R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR75 STR28-29R AFT CARGO COMPARTMENT; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00095: DEEMED OUT OF LIMITS IAW SRM 51-75-16. R& R SHEAR CLIP @ FR75 STR28-29R IAW SRM 51-41-01 AND 51-41-02.
Part: FLOORBEAM — CORRODED (FRM 17) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FLOOR-BEAM, UPPER SURFACE, LOCATED ON FR 17, + .617, STGR 17R, IS BEYOND ALLOWABLE E190 SRM LIMITS; REMOVED AND REPLACED FLOOR-BEAM (P/N: 170-03263-001, TRACK, RIGHT-FLOOR, FWD.) LOCATED BTW FR 12 AND FR 20, PER E190 SRM: 51-40-08. CROSS-REF. AEROMAN NR# 2018-245816. (CONSIDERED A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - V2533A5 - ESN V18011- PERFORMANCE RESTORATION - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 76 S28-29R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR76 STR28-29R AFT CARGO COMPARTMENT; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00097: SHEAR CLIP FOUND OUT OF LIMITS. R & R SHEAR CLIP FR76 STR27-28L IAW E190 SRM 51-10-03, 51-12-01, 51-41-01, AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: CARBON SEAL — WORN (ENGINE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - PW1133GA-JM - ESN P770722 - WORN #3 CARBON SEAL - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: CABLE — DAMAGED (GPS) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CABIN SYSTEMS - GPS ANTENNA CABLE P/N N31201-103, RETERMINATION- DEVIATION FROM APPROVED DATA - N592JB. (CONSIDERED A MAJOR REPAIR)
Part: FRAME — DAMAGED (FRM 16) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / RHS FR16 DOUBLE JOGGLE AREA HOLE #6, #7, #A, AND #C / CRACKS - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CORRODED (FRMS 81-82) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: CORROSION: FUSELAGE SKIN FR81-82 STR27-28R; (RESOLVED ON W/O: 1300462 TASKCARD: NR-00020) DEEMED OUT OF LIMITS IAW SRM 51-12-01, 51-10-03, AND 53-23-01/AD51. ACCOMPLISHED REPAIR FUSELAGE SKIN FR81-82 STR27/28R IAW SRM 53-23-01/REPAIR 62P. REQ'S REINSPECT @ 20,000FC/26,600FH (WHICHEVER OCCURS FIRST) WITH SUBSEQUENT INSPECTIONS EVERY 9,000FC/11,970FH (WHICHEVER OCCURS FIRST). FUR-E190-53-01238 CREATED.
Part: DOUBLER — CORRODED (FRMS 75-76) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR BARREL / FR 75-76 AND STGR 32-36LH / WASTE ACCESS PANEL CUTOUT DOUBLER / CORROSION - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: FLOORBEAM — CORRODED (FRM 14) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR STRUCTURE CROSS BEAM @ FR14 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (LT WING LE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CRACK ON WING LEADING EDGE SKIN LOCATED BTW RIB 23 AND RIB 22 AT LH WING; LEADING EDGE SKIN PANEL LOCATED BTW RIB 22 AND RIB 27 ON LH WING WAS REPLACED PER EMB190 SRM 51-42-02.SRM51-41-02 AND SRM 51-43-02.
Part: SHEAR TIE — CORRODED (FRM 88 S27-28R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP LOCATED AT FR 88, BTW STGR 27R TO STGR 28R, ON LOWER FUSELAGE IS BEYOND ALLOWABLE LIMITS; REMOVED AND REPLACED SHEAR CLIP LOCATED AT FR 88, BTW STGR 27R AND 28R, ON LOWER FUSELAGE IAW SRM 51-40-08 AND DWG. 170-65180-445 & 170-66041-002. REF. AEROMAN NR # 2018-245827. REF. P/N: 170-66531-001, SHEAR - CLIP. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 76 S27-28L) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR76 STR27-28L AFT CARGO COMPARTMENT; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00098: SHEAR CLIP FOUND OUT OF LIMITS. R & R SHEAR CLIP FR76 STR27-28L IAW E190 SRM 51-10-03, 51-12-01, 51-41-01, AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: FITTING — BROKEN (VERTICAL STAB) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: STABILIZER/VERTICAL STAB/ BROKEN FITTING HOIST POINT ON AREA OF ACCESS PANEL # 325EL ON VERTICAL STABILIZER. (CONSIDERED A MAJOR REPAIR)
Part: STRUCTURE — CORRODED (FRMS 15-16) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FLOOR PLATE STRUCTURE, LOCATION IS BTW FR 15 TO FR 16 AND STGR 17L, CORROSION IS BEYOND LIMITS OF E190 SRM: 53-10-10; INSTALLED NEW FLOOR PLATE DOUBLER AND FASTENERS, LOCATED BETWEEN FR 13 TO FR 16, INSIDE PASSENGER CABIN, AS PER EMBRAER E190 SRM 51-40-08. REF. P/N: 170-12118-001. REF. AEROMAN NR # 2018-245823.(CONSIDERED A MAJOR REPAIR)
Part: SKIN — UNKNOWN (FRM 22 S24-25L) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE- FWD/ EXTERNAL SKIN FR22 STGR 24L-25L/ DENTTEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SEAT TRACK — CORRODED (FRM 84) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FLOOR STRUCTURE / RH SEAT TRACK / FR84 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SKIN — CRACKED (RT WING TE) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: WINGS / RH WING / TRAILING EDGE LOWER SKIN REAR SPAR / RIBS 10-11, 11-12 / CRACK DAMAGE 1-3 /MATERIAL SUBSTITUTION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: FRAME — CORRODED (FRM 80 S27-28R) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTWN STR 27R-28R / CORROSION - TIME-LIMITED REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 82 S28-29R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR82 STR28-29R AFT CARGO COMPARTMENT; REF TOMX W/O N249JB/2525/E190/BRIDGE NR 00105: DEEMED OUT OF LIMITS IAW SRM 51-75-16. R& R SHEAR CLIP @ FR82 STR28-29R IAW SRM 51-41-01 AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: STOP FITTING — DAMAGED (FRM 68 S22L) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: STOP FITTING — CRACKED (FRM 68 S22) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED (FRM 85 S27-28R) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: SHEAR CLIP FR85 STR27-28R AFT CARGO; REF TOMX W/O N249JB/2525/E190/BRIDGE NR00106: DEEMED OUT OF LIMITS IAW SRM 51-10-03, 51-12-01, AND 51-75-16. R & R SHEAR CLIP @ FR85 STR27-28R IAW SRM 51-41-01- AND 51-41-02. (CONSIDERED A MAJOR REPAIR)
Part: SEAT TRACK — CORRODED (FRMS 12-20) · corrosion level 2 · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: CORROSION: CTR LH LONGITUDINAL BEA, FR12-14, 17, AND 19-20 SEAT TRACK @ FWD FUSE PAX CABIN FLOOR STRUCTURE (W1); REF TOMX W/O N249JB/2525/E190/BRIDGE NR-00112: EVALUATED CORROSION AND DEEMED OUT OF LIMITS IAW E190 SRM 53-10-10 AD52. R & R LH LONGITUDINAL SECTION BEAM FR12-20 IAW SRM 51-41-01, 51-41-02, 51-43-03, AND SRM 51-43-04.(CONSIDERED A MAJOR REPAIR)
Part: ENGINE — UNKNOWN (UNKNOWN) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: ENGINE - V2533A5 - ESN V18011- PERFORMANCE RESTORATION - REPAIR WORKSCOPE. (CONSIDERED A MAJOR REPAIR)
Part: PRESSURE BLKHD — CRACKED (FRM 35 S30L) · airframe 44,469 hrs · 29,251 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - PERMANENT REPAIR (TBD). (CONSIDERED A MAJOR REPAIR)
Earlier reports · 2006–2023 · 58 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,432 hrs · 29,222 cycles
FLT#731, BOS-LGA. (AIRCRAFT DIVERTED TO JFK) 'REF DEF LOG 3822231-1 BLEED 1 FAIL. ANTI-ICE WING FAIL; REMOVED AND REPLACED BLEED PRESSURE REGULATING SHUT IAW AMM 36-11-01. PERFORMED OPS CHECK NO MSG BUT PRESSURE STILL AT 9 PSI NO FIX. FURTHER T/S REQUIRED.
2022
Part: IRU — FAILED (342601-01-50-1) · airframe 41,014 hrs · 26,601 cycles
FLT#253, FLL-SJU (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL). ' AUTOPILOT DISCONNECTED IN CLIMB ABOUT 20,000 FT. MULTIPLE EICAS MESSAGES APPEARED, AMBER STICK SHAKER ANTICIPATED #2, BELOW AT FAILURE. LATER ABOUT 15 MINUTES IRS FAIL APPEARED (#2) ALSO. RAN QRH'S & RETURNED TO DEPARTURE AIRPORT; ALL FAULTS CORRELATED TO "IRS DATA INVALID OR MISCOMPARED". AT ARRIVAL "IRS 2 FAIL" DISPLAYED ON EICAS WITH PFD2 FAULTED.PER FIM 34-26-00-810-808-A WITH FC#34265515IR2. REMOVED AND REPLACED IRU2 PER AMM34-26-01. OPS CHECKS ARE NORMAL. A/C OK FOR SERVICE.'
Part: NONE — FAILED (PCU-LWR-SYS3) · airframe 40,477 hrs · 26,206 cycles
FLT # 2184, RDU-BOS. AT FL 290 IN CRUISE A/C UNEXPECTEDLY YAWED TO THE LEFT REQUIRED HALF-SCALE RUDDER TRIM TO CORRECT. DURING DECENT A/C YAWED RIGHT REQUIRING REMOVAL OF TRIM . RUDDER OSCILLATED INFREQUENTLY BUT NOTICEABLY THROUGH DECENT. APPROACH WAS NORMAL; TROUBLESHOT SYSTEM WITH TECHNICAL SUPPORT, UPON REVIEWING DVDR FOR AC, FOUND LOWER PCU TO APPEAR INTERMITTENTLY OFFLINE. R&R LOWER RUDDER PCU IAW AMM 27-22-01. PERFORMED QUICK RIGGIN PROCEDURE IAW AMM 27-22-01. OPS/LEAK CHECK GOOD.
2020
Part: WEB — CRACKED (FAIRING) · airframe 38,023 hrs · 24,674 cycles
DURING HEAVY MAINTENANCE, CRACK BELLY FAIRING ON WEB AT LEVEL FR 45 LT SIDE ON LOWER FUSELAGE. RESOLVED ON W/O: 1061524 TASKCARD: NR-00015. ACCOMPLISHED REPAIR OF TWO CRACKS FOUND ON THE WING TO FUSELAGE FAIRING AT FR 45 LEVEL LT RIB AT CENTER FUSELAGE LL IN ACCORDANCE WITH AEROMAN EA 53-0578-20 COVER AND PART 1, AND EMBRAER ETD2020-190-02516.
Part: SKIN — CRACKED (LT WING) · airframe 38,023 hrs · 24,674 cycles
DURING HEAVY MAINTENANCE, CRACK LEADING EDGE EXTERNAL SKIN SLAT TRACK 6 AREA ON LT WING, REF: ARM W/O 2020-277/1 N/R 2020-245049. ACCOMPLISHED REPAIR BETWEEN RID 24-25, IAW AEROMAN EA 57-0597-20 RIB 1 (COVER AND PART 1) EMBRAER ETD 2020-190-0249472 REV B AND EC E20-608-01.
Part: RIB — CRACKED (WNG-BDY FAIRING) · airframe 38,023 hrs · 24,674 cycles
DURING HEAVY MAINTENANCE, TWO CRACKS FOUND ON THE WING TO FUSELAGE FAIRING AT FR 45 LEVEL LT RIB AT CENTER FUSELAGE II. SEE REF 1 EA FOR DETAILS. THE CRACKS WERE EVALUATED AGAINST SRM AND NO REPAIRS WERE FOUND APPLICABLE. EMBRAER WAS CONTACTED AND PROVIDED REPAIR INSTRUCTIONS VIA REF 2, ETD CONSISTS OF TRIMMING THE AREA OF DAMAGE. PERFORM DVI & HFEC INSPECTION. FABRICATE & INSTALL REPAIR DOUBLERS AND RESTORE SURFACE PROTECTION PER SRM. THIS EC E20-594-01 ACCOMPLISHES PERMANENT REPAIR PER THE REF 1 EA AND COMPLIES WITH REF 2 ETD WITHOUT DEVIATION. THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF 2 ETD AND IS CLASSIFIED AS MAJOR.
Part: RIB — CRACKED (RT WING) · airframe 38,023 hrs · 24,674 cycles
DURING HEAVY MAINTENANCE, CRACK RIB 10 MAIN BOX LOWER SKIN SPAR 2 TRAILING EDGE ON RT WING. RESOLVED ON W/O: 1061524 TASKCARD: NR-00007, REF: ARM W/O 2020-277/1 N/R 2020-245029. PERFORMED PERMANENT REPAIR LOCATED RIB 10 MAIN BOX LOWER SKIN SPAR 2 TRAILING EDGE ON RT WING, IAW E190 SRM 57-10-01 REPAIR 54.
Part: SKIN — CRACKED (LT SLAT TRACK) · airframe 38,023 hrs · 24,674 cycles
DURING HEAVY MAINTENANCE, CRACK LEADING EDGE EXTERNAL SKIN SLAT TRACK 5 AREA ON LT WING, REF: ARM W/O 2020-277/1 N/R 2020-245048 TECH 8622918 INSP 8612311. ACCOMPLISHED REPAIR BETWEEN RIB 19-20, IAW AEROMAN EA 57-0594-20 REV 1 (COVER AND PART 1) EMBREAR ETD 2020-190-024845-A AND EC E20-607-01.
Part: SENSOR — FAILED (TE FLAPS) · airframe 37,479 hrs · 24,296 cycles
FT # 412, ORD-BOS. EMERGENCY DECLARED. FLAP FAIL EICAS; R & R R/H FLAP INBD/OUTBD FLAP SKEW SENSORS. REF AMM 27-53-06 REF TO LP 2777104 ITEM #2 ( R+R FLAP ACT ) PLEASE REFER TO L/P 2777106 ITEM # 1 FOR RIGGING & OP'S CKS.
Part: SENSOR — FAILED (TE FLAPS) · airframe 37,479 hrs · 24,296 cycles
FT # 412, ORD-BOS. EMERGENCY DECLARED. FLAP FAIL EICAS; R & R R/H FLAP INBD/OUTBD FLAP SKEW SENSORS. REF AMM 27-53-06 REF TO LP 2777104 ITEM #2 ( R+R FLAP ACT ) PLEASE REFER TO L/P 2777106 ITEM # 1 FOR RIGGING & OP'S CKS.
2019
Part: PROCESSOR — FAILED (NR 1 MAU) · airframe 36,901 hrs · 23,907 cycles
FT # 1042, SAV-JFK. EMERGENCY DECLARED INTO JFK. AVNX MAU 1A FAIL WITH ASSOCIATED MESSAGES. DUE TO THE LOSS OF THE MAU 1A, NWS WAS LOST AND THE AIRCRAFT WAS TOWED TO THE GATE WITHOUT INCIDENT; T/S PER FIM 45-45-00-810-939-A. R & R MAU1 NIC+PROC MOD 1 PER AMM 31-41-04. ALL FAULTS CLEARED. AC OK FOR SVC.
2018
Part: SKIN — DENTED (FUSELAGE) · airframe 33,713 hrs · 21,617 cycles
FLT 1089, BOS-DCA. REFER TO EC E18-787-01. FUSELAGE / FWD FUSELAGE / LOWER SKIN BTWN FR15-20 STGR 21R-22R / DENTS - TEMPORARY REPAIR; THIS REPAIR HAS BEEN APPROVED VIA REF /1/ ETD AND IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, FILLER AT FR 17, STR 17R. NO SPECIFIC ALLOWABLE DAMAGE REFERENCE IN THE SRM, THEREFORE THE DAMAGED PART WILL REQUIRE REPLACEMENT; REMOVED AND REPLACED THE FLOOR BEAM FILLER LOCATED AT FR17, STR 17R, IAW EA 53-0217 COVER PART 1. REF NR 2018-245821. REF. P/N: 170-21769-403.
Part: FILLER — CORRODED (FUSELAGE) · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE (BASIC 6 CHECK AT SAL), DURING THE ACCOMPLISHMENT OF THE POST REPAIR INSPECTIONS REQUIRED BY EC E16-274-02, REPORTED CORROSION ON THE FILLERS OF THE PREVIOUSLY ACCOMPLISHED REPAIR (EC E16-274-01 & REF /3/) AT THE FLOORBEAM FR 17 BETWEEN RBL 13 â RBL 35. REFER TO EC E16-274-03; THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /2/ ETD AND IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, UPPER SURFACE, LOCATED ON FR 17, + .617", STGR 17R, IS BEYOND ALLOWABLE SRM LIMITS; REMOVED AND REPLACED FLOORBEAM (P/N: 170-03263-001, TRACK, RIGHT-FLOOR, FWD.) LOCATED BTW FR 12 AND FR 20, PER SRM: 51-40-08. CROSS-REF. NR 2018-245816.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR-CLIP, LOCATED AT FR 87, BTW. STR 27R AND 28R, LWR. FUSELAGE, THAT IS BEYOND ALLOWABLE SRM LIMITS; REMOVED AND REPLACED SHEAR-CLIP (P/N: 170-66041-002) LOCATED AT FR 87 AND BTW. STR 27R AND STR 28R (LOWER FUSELAGE) PER SRM: 51-40-08. CROSS-REF. NR 2018-245826.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, FILLER, LOCTATED ON FR17, STR 17R, HAS CORROSION THAT IS BEYOND LIMITS. NOTE: THERE IS NO SPECIFIC SRM LIMIT FOR THIS SPECIFIC PART, THEREFORE IT WAS DETERMINED TO REPLACE IT; REMOVED AND REPLACED FLOORBEAM FILLER, LOCATED AT FR 17, STR 17R, IAW EA 53-0217. REF. NR 2018-245821. P/N: 170-21769-403.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR CLIP LOCATED AT FR 88, BTW STR 27R TO STR 28R, ON LOWER FUSELAGE IS BEYOND ALLOWABLE LIMITS; REMOVED AND REPLACED SHEAR CLIP LOCATED AT FR 88, BTW STR 27R AND 28R, ON LOWER FUSELAGE IAW SRM 51-40-08 AND DWG. 170-65180-445 & 170-66041-002. REF. NR 2018-245827. REF. P/N: 170-66531-001; SHEAR - CLIP
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 33,424 hrs · 21,413 cycles
DURING HEAVY MAINTENANCE, FR97-98 STGR21L-23L DENT DAMAGE. COMPLIED WITH EC E17-052-03. THIS PERMANENT REINFORCEMENT REPAIR IS CLASSIFIED AS MAJOR.
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,419 hrs · 21,412 cycles
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR PLATE STRUCTURE, LOCATION IS BTW FR 15 TO FR 16 AND STR 17L. CORROSION IS BEYOND LIMITS OF SRM: 53-10-10; INSTALLED NEW FLOOR PLATE DOUBLER AND FASTENERS, LOCATED BETWEEN FR 13 TO FR 16, INSIDE PASSENGER CABIN, AS PER SRM 51-40-08. REF. P/N: 170-12118-001. REF. NR 2018-245823.
2017
Part: PUMP — FAILED (HYD SYSTEM) · airframe 30,163 hrs · 18,963 cycles
CREW REPORTED A LOSS OF NR 2 HYDRAULIC SYSTEM DURING CRUISE. DECLARED AN EMERGENCY. HYD 2 EDP FAILED, HYD 2 LOW QTY, HYD 2 LOW PRESSURE, SYS 2 QTY & PRESSURE ZERO. R & R THE NR 2 ENG EDP IAW AMM 29-11-00.
Part: BEARING — DIRTY (AILERONS) · airframe 29,589 hrs · 18,542 cycles
AFTER TAKEOFF, IT WAS NOTICED THAT THE FLIGHT CONTROLS IN THE ROLL MODE WERE STICKING. THE AIRCRAFT WAS HAND FLOWN. THE STICKING OF THE CONTROLS GOT WORSE THE HIGHER THE AIRCRAFT WENT. AUTO PILOT WORKED WELL. NO NOTICE OF ONLY ISSUES OF FL280 OF 290 - 310 KTS. DECENT REMAINED THE SAME WAY ON APPROACH. ONCE SLOWED, THE ROLL RESPONSE WAS SLOW AND THE FLIGHT CONTROLS STILL WAS STICKING. FOUND LT AND RT QUADRANT TORQUE TUBE ASSYS BEARINGS WERE DIRTY AND STIFF. THE AILERON FUSELAGE SECTOR BEARING WAS CLEANED WITHOUT REMOVING THE BEARING ASSEMBLY. ALSO ACCOMPLISHED AILERON CONTROL SYSTEM OPERATIONAL TEST. TESTED OK.
Part: SENSOR — FAILED (TAT) · airframe 29,378 hrs · 18,397 cycles
FT 1453, FLL-SJU, RETURN TO FIELD. DURING CLIMB OUT AT 10,000 FT, EICAS DISPLAYED LOSS OF AOA LIMIT FAIL, AT FAIL, TAT 1 FAIL, AFCS FAULT. R&R TAT SENSOR NR 1 PER AMM 34-15-02. OPS CHECK PASSED. A/C GOOD FOR SERVICE.
2016
Part: BATTERY — DISCHARGED (CABIN) · airframe 27,935 hrs · 17,356 cycles
EMERGENCY LIGHT POWER UNIT NR 2 FAILED FUNCTIONAL TEST DURING ROUTINE MAINTENANCE, R & R EMERGENCY LIGHT POWER UNIT NR 2, FWD RT. PERFORMED FUNCTIONAL & OPS TEST. FUNCTIONAL AND OPS TEST PASSED.
Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON SEAT TRACK 3" AFT OF FRAME 17, RBL 12. ACCOMPLISHED BLEND REPAIR IAW JB EA E16-272-01, REF NR 00130 AND E16-272-01 FOR WORK ACCOMPLISHED.
Part: FRAME — CORRODED (FRM 17) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION WAS FOUND ON FRAME 17, RBL 16. REPAIRED IAW EC E16-274-01.
Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON FLOOR DOUBLER, FRAME 16, LBL13; R & R DOUBLER IAW SRM 51-41-02, REF NR 00132 FOR WORK ACCOMPLISHED.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON AFT CARGO DOOR LOWER BEAM, REPLACED BEAM IAW SRM REF 51-41-01, REF EAMS NR H4935-00736.
Part: BEAM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION WAS FOUND ON AFT PASSENGER DOOR LOWER BEAM AROUND FASTENERS 2" AFT OF FR 85, STR 17L; ACCOMPLISHED BLEND REPAIR IAW JB EA E16-306-01, REF NR 00251 AND E16-306-01.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON FWD CARGO DOOR LOWER BEAM BEHIND NR 1 LATCH FITTING; REPLACED BEAM IAW SRM REF 51-41-01, REF EAMS NR H4935-00716.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON FWD CARGO DOOR BEAM BEHIND NR 4 LATCH. REPLACED BEAM IAW SRM REF 51-41-01, REF EAMS NR H4935-00717.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION FOUND ON AFT CARGO DOOR LOWER BEAM. REPLACED BEAM IAW SRM REF 51-41-01, REF EAMS NR H4935-00737.
Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,108 hrs · 16,743 cycles
CORROSION WAS FOUND ON AFT CARGO DOOR LOWER BEAM DOUBLER, REPAIRED IAW EC E16-290-01, REF EAMS NR H4935-000418.
Part: COFFEEMAKER — FAILED (GALLEY) · airframe 26,831 hrs · 16,574 cycles
BURNED PLASTIC ODOR COMING FROM THE FRONT GALLEY COFFEEMAKERS. R & R COFFEEMAKER IAW AMM 25-30-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
2015
Part: HEAT EXCHANGER — FAILED (NR 2) · airframe 25,908 hrs · 15,978 cycles
DIVERTED DUE TO SMOKE IN THE CABIN. SMOKE FUMES DISSAPATED ONCE RECIRCULATION AND BLEED BUTTONS WERE PUSHED OUT. IAW FIM TASK 21-20-00-810-801-A COMPLIED WITH INSPECTION OF THE SYSTEM AS DIRECTED. R & R NR 2 DUAL HEAT EXCHANGER IAW 21-51-04. OPS AND LEAK CHECK GOOD.
Part: ACM — FAILED (NR 2) · airframe 25,908 hrs · 15,978 cycles
DIVERTED DUE TO SMOKE IN THE CABIN. SMOKE FUMES DISSAPATED ONCE RECIRCULATION AND BLEED BUTTONS WERE PUSHED OUT. PER FIM TASK 21-20-00-810-801-A COMPLIED WITH INSPECTION OF THE SYSTEM AS DIRECTED. FOUND PACK NR 2 FAILED. R & R NR 2 ACM IAW 21-51-005. OPS AND LEAK CHECK GOOD PERFORMED A HIGH POWER RUN-UP OF ENGINE NR 1 TO VERIFY BLEED SYSTEM INTEGRITY.
2014
Part: LINE — LEAKING (HYD SYSTEM) · airframe 21,550 hrs · 13,085 cycles
DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO NR 2 HYD LOW QTY IN FLIGHT. AT 22 PERCENT DROPPED DOWN TO 6 PERCENT DOWN WITH A 2 PERCENT DROP EACH 6 TO 10 MINUTES. LANDED WITH 6 PERCENT AFTER LANDING PRESSURE WENT TO 8 PERCENT THEN 10 PERCENT AT GATE. ALL FLIGHT HYD SYS WORKED NORMAL FOR HYD SYS 2. AFTER INVESTIGATION FOUND NR 2 ENGINE DRIVEN PUMP PRESSURE LINE & CASE DRAIN PUMP LINE LEAKING AT UPPER FLARE. R & R BOTH LINES, HOSES, IAW AMM 29-11-01 & 20-10-03. LEAK CHECK OK. HYD FLUID CHECK NORMAL.
Part: PROCESSOR — FAILED (MAU 3) · airframe 21,276 hrs · 12,940 cycles
ON CHECK FOUND EMERGENCY LIGHT BATTERY FAULT. R & R NIC 1 PROCESSOR 5 IN MAU 3 IAW AMM 31-41-04. FAULT CLEARED. LOADS ACCOMPLISHED. ACFT OK FOR SERVICE.
Part: SEAL — DAMAGED (SERVICE DOOR) · airframe 21,179 hrs · 12,876 cycles
AIRCRAFT DIVERTED, OBSERVED LOUD AUDIBLE AND VIBRATION CLIMBING THRU 210. INFLIGHT CREW CONFIRMED VIBRATION AND SUSPECT R1 DOOR. CHANGES IN FLIGHT CONTROLS AND AIRSPEED DID NOT STOP THE VIBRATION, ENGINE VIBRATIONS WERE NORMAL. VIBRATION STOPPED UPON DESCENDING BELOW 15,000 FT. PERFORMED FIM TASK 05-50-510-801-A, GOT TO STEP 4 AND FOUND R1 FWD DOOR SEAL DAMAGED. R & R FWD SERVICE DOOR SEAL IAW AMM 52-41-21. PERFORMED INSPECTION OF HOSES OF PACK AREAS AND INSPECTION OF RADOME, NO DEFECTS NOTED. PRESSURIZED ACFT, OK. ACFT OK FOR SERVICE..
Part: DEFLECTOR — TORN (PAX DOOR) · airframe 21,178 hrs · 12,875 cycles
AIRCRAFT VIBRATION IN FLIGHT. RETURNED TO AIRPORT. BEGAN AT 16,000, AIRSPEED CHANGE DIDN'T AFFECT IT, DECENT THRU 16,000 DID. PERFORMED FIM TASK 05-50-00-810-801-A, FOUND FORWARD PAX DOOR DEFLECTOR TORN AT THE CORNER. R & R FWD PAX DOOR DEFLECTOR IAW AMM 52-11-28.
Part: DOOR — FROZEN (R1) · airframe 21,173 hrs · 12,874 cycles
CREW REPORTED R1 DOOR WOULD NOT DISARM. THAWED DOOR BOTTOM OF R1 DOOR. ARM/DISARM OPS CKS GOOD IAW MM 52-41-00.
Part: DEFLECTOR — DAMAGED (R1 DOOR) · airframe 21,168 hrs · 12,870 cycles
CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE DUE TO SEVERE VIBRATION ORIGINATING FROM R1 DOOR, VERY LOUD. DOOR DEFLECTOR, PAX AND SERVICE RT. R & R R1 DOOR DEFLECTOR IAW AMM 52-41-28.
2013
Part: ACM — FAILED (NR 1) · airframe 19,816 hrs · 11,993 cycles
CREW DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO SMOKE ODOR AT COCKPIT AND CABIN. R & R NR 1 ACM IAW 21-51-05-04. OPS CHECK GOOD.
2012
Part: LINKAGE — OUT OF ADJUST (L2 DOOR) · airframe 17,837 hrs · 10,715 cycles
FLT 1600 BOS-DCA,ON TAKEOFF ROLL AT 80 KNOTS L2 PAX DOOR IND UNSAFE. PRIOR TO PUSH L2 SHOWED AMBER CIRCLE WITH BLACK X UNTIL DOOR WAS CYCLED SEVERAL TIMES WITH GREEN INDICATION. UNEVENTFUL REJECTED TAKEOFF WITH RETURN TO GATE. (DOOR POS IND ON MFD & ASSC EICAS-PAX/SVC) ADJUSTED LINKAGE TO SENSOR FOR VENT FLAP. OPS CHECK GOOD IAW AMM 52-11-25.
Part: POWER SUPPLY — FAILED (CABIN) · airframe 17,323 hrs · 10,416 cycles
FLT 461 BOS-RSW, CEILING EMERGENCY LIGHT AT ROW 1 INOP. REMOVED AND REPLACED FORWARD LEFT EMERGENCY LIGHT POWER SUPPLY PER AMM 33-50-00. SYSTEM TEST NORMAL.
Part: ENGINE — LEAKING (NR 1) · airframe 17,056 hrs · 10,231 cycles
FLT 686 DCA-BOS, AIRCRAFT DIVERTED TO JFK DUE TO NR 1 ENGINE INDICATION OF RAPID OIL LOSS FROM 11.4 TO 7.2. FOUND OIL LEAKING ON NR 5 SUMP DRAIN. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD E190-71-00-01-400-801. OPS AND LEAK CHECK GOOD. ON THE SAME FLIGHT JB 686, THE CREW REPORTED AFT CABIN EXPERIENCED SIGNIFICANT JET FUEL ODOR (BURN EYES). AFTER THE ENGINE CHANGE, FIM 21-20-00-810-803A WAS ACCOMPLISHED WITH NO FINDINGS.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 16,984 hrs · 10,183 cycles
FLT 6411 JFK-BNA, DURING HEAVY SERVICE - FWD CABIN RIGHT SIDE CROSSBEAM AT FR17 HAS CORROSION. BLENDED THE AFFECTED AREA, C/W HFEC. FABRICATED L-SHAPE ANGLE AND SHIMS. DRILL TO FIT TO BEAM, ALODINE, PRIMED AND ATTACHED L-REPAIR SHIMS PER E12-501-01 SRM 53-10-10 FIG 78 ITEM 10.
2011
Part: WIRE HARNESS — FAULTY (LE SLAT) · airframe 13,305 hrs · 7,819 cycles
FLT 69 SYR-JFK, CREW DECLARED EMERGENCY DUE TO, SLAT FAIL EICAS MSG IN FLIGHT. REMOVED AND REPLACED SLAT HARNESS W612 RT AND PERFORMED OPERATIONAL TEST OF THE SLAT CONTROL SYS IAW 27-80-00-710-801 NO FAULTS NOTED AT THIS TIME, A/C OK FOR CONTINUED SERVICE.
2009
Part: SENSOR — FAILED (TAT) · airframe 9,115 hrs · 5,375 cycles
FLT 1404 SFO-AUS DIVERTED TO SJC, ON CLIMBOUT THRU FL290 "TAT 1 FAIL" EICAS MESSAGE FOLLOWED BY AUTO THROTTLE DISCONNECTED THEN AUTOPILOT DISCONNECTED, A STRONG BURNED ELECTRICAL FUME SMELL. A/P AND A/T WOULD NOT RE-ENGAGE AND NO GUIDANCE FROM FLIGHT DIRECTORS EXCEPT FPA. EMERGENCY DECLARED WITH A DIVERSION TO SJC STRONG ELECTRICAL FUME SMELL THRU DESCENT AND LANDING. MX PERFORMED SMOKE & ABNORMAL SMELL CHECK REF FIM 21-20-00-810-801-A AND FOUND LT TAT ELECTRICAL CONNECTOR WAS BURNT, REPLACED REF SWPM 20-31-000. REMOVED AND REPLACED TAT SENSOR IAW AMM 34-15-02, OPS TEST ADS SYSTEM REF AMM TASK 34-15-00-710-801A. TEST PASSED.
Part: PROCESSOR — ODOR (HUD) · airframe 8,701 hrs · 5,144 cycles
FLT 75 SYR-JFK - F1 NOTED A STRONG BURNING BATTERY ODOR SOON AFTER T/O. TURNED OFF THE (PRA) ODOR WENT AWAY. OPERATED (PRA) SYSTEM FOR 1 HOUR COULD NOT DUPLICATE ANY BURNING BATTERY ODOR. REMOVED AND REPLACED UNIT DATA PROCESSING BOX AS A PRECAUTIONARY TROUBLESHOOTING MEASURE IAW AMM 46-41-01. OPS CHECK SYSTEM, SYSTEM CHECK NORMAL VOLUME OK.
Part: FAN — FAILED (CARGO BAY) · airframe 8,595 hrs · 5,091 cycles
FLT 654 JFK-JFK SMOKE IN CABIN AT 500 FEET RECEIVED CALL FROM INFLIGHT. REPORTING SMOKE IN CABIN OVERWING WAS VISIBLE. ALSO HAD ODOR IN COCKPIT. PERFORMED FIM TASK 21-20-00-810-801A. REMOVED AND REPLACED AFT CARGO COMPARTMENT ELECTRONIC EQUIPMENT RACK VENTILATION FAN. OPS CHECK OK.
Part: UNKNOWN — ODOR (CABIN) · airframe 6,958 hrs · 4,147 cycles
STRONG BURNING ODOR NOTICED AFTER TAKEOFF. AIR RETURN TO DEPARTURE. ACCOMPLISHED FIM TASK 21-20-00-810-801-A. NO UNUSUAL ODORS NOTED. ACFT OK FOR SERVICE FOLLOWING DUAL HIGH PWR ENG RUN. NO UNUSUAL ODOR NOTED.
2008
Part: A/C PACK — CONTAMINATED (NR 2) · airframe 5,801 hrs · 3,530 cycles
FLT NR 1191, JFK-ACK, AIR TURN BACK TO JFK, AFTER ROTATION BOTH PILOTS SMELLED ELCE. SMOKE. BOTH NOTED SMOKE HAZE IN COCKPIT. INFLIGHT CALLED ON INTERCOM & STATED THERE WAS SMOKE IN THE CABIN. SMOKE WAS COMING FROM FWD LAV AT ABOUT 1000` AGL. THE RED FWD LAV SMOKE CAS POSTED. OPS CHECKED LAVS SMOKE DET. PER AMM 26-14-00.01. OPS CHECKED THE OPERATION TRU`S PER AMM 24-31-00. ALSO INSPECTED BOTH PACKS FOR DEBRIS, FOUND NR 2 PACK HAD COFFEE GROUNDS & COFFEE STAINS IN INTAKE. CLEANED DEBRIS, RAN BOTH PACKS. THEY OPS CHECKED OK PER AMM 21-51-05. ALSO PERFORMED FIM TASK FOR SMOKE PER 21-20-00-810-A. ALSO RAN BOTH ENGINES AT CLIMB 2 POWER WITH RECIRC. FAN ON/OFF & NO ABNORMAL SMELL PER 71-80-01. ALL TASKS C/W NO SMELL. PER LIVE TV MM 44-20-70. GENERAL CABIN INSPECTION NO DEFECTS NOTED LTV. OPS CHECK OK.
Part: FILTER — CONTAMINATED (A/C PACK) · airframe 5,544 hrs · 3,392 cycles
FLT 907, JFK-ORD, AIR RETURN TO JFK, RECEIVED LAV SMOKE WARNING IN FLIGHT. LANDED ACFT ASAP, FOLLOWED QRH PROCEDURES. SMOKE WAS VISIBLE IN CABIN INITIALLY AND THEN DISSIPATED WITH TIME. LAV SMOKE WARNING WENT OUT AFTER SMOKE DISSIPATED. NO VISIBLE SMOKE IN COCKPIT. PERFORMED LTV SMOKE ODOR INSPECTION PER 44-20-10. INSPECTION WAS GENERAL TO CABIN, NO FAULTS NOTED. PERFORMED VISUAL INSPECTION OF NR1 AND NR2 PACK INLETS. FOUND EVIDENCE OF COFFEE RESIDUE ON NR 2 PACK INLET. SMALL TRACES OF COFFEE STAINS ON NR 2 PACK INLET. CLEANED RESIDUE FROM PACK INLET NR 2 AND REMOVED AND REPLACED RECIRC FAN AIR FILTERS AS PER MM 21-24-02. ACFT OK FOR SERVICE. (S)
Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 3,968 hrs · 2,552 cycles
FLT 430, MCO-BOS, AFTER TAKEOFF DETECTED AN ODOR THROUGHOUT CABIN. INITIAL THOUGHT WAS ELECTRICAL ODOR. AFTER REFERENCE TO QRH & DISCUSSION WITH MX CONTROL. ODOR WAS ISOLATED TO PACK NR 2. AS PACK NR 2 WAS TURNED PACK NR 2 ON/OFF THE ODOR CAME/DISSIPATED. CONTINUED FLT TO BOS WITH PACK NR 2 OFF. PERFORMED FIM TASK 21-20-00-810-801-A FOR ABNORMAL ODOR AND ISOLATED TO RT PACK OPERATION.
Part: TURBINE BLADES — DAMAGED (ACM) · airframe 3,923 hrs · 2,529 cycles
STRONG BURNING SMELL IMMEDIATELY AFTER TAKEOFF. SMELL DISSIPATED AFTER 5 MIN. ODOR BEGAN IN CABIN. DECLARED EMERGENCY AND RETURNED TO BASE. FOUND ACM TURBINE BLADES DISINTEGRATED. REMOVED AND REPLACED RT ACM PER AMM 21-51-05. REF LP 310785 ITEM NR 1. OPS CHECK OF RT ACM REQUIRED TASK 21-51-00-710-801.
2007
Part: SLAT — OUT OF RIG (WING) · airframe 3,602 hrs · 2,344 cycles
FLT 1056 PIT-JFK, "SLAT FAIL" EICAS MSG. APPEARED WHILE CLIMBING THROUGH 10,000 FT. SLATS REMAINED FAILED AT ZERO POSITION. FOLLOWED QRH PROCEDURE. APPROACH & LANDING UNEVENTFUL IN ACCORDANCE WITH/QRH. FOUND SLAT PDU BRAKE ENGAGED. PERFORM RIGGING ADJUSTMENT IAW 27-81-00. COULD NOT DUPLICATE FAULT, OK TO CONTINUE SERVICE.
2006
Part: YOKE — SLIPPED (COCKPIT) · airframe 234 hrs · 165 cycles
INTERMITTENT THUMP HEARD AND FELT BETWEEN 3,000 FT AND 15,000 FT CAN BE FELT THROUGH YOKE AND MOSTLY WITH AUTO PILOT ON. RIG PINS INSTALLED IN LT, RT AILERON QUADRANT 2 PINS TOTAL. RIG PINS INSTALLED IN CONTROL YOKES PILOT AND COPILOT FOR TROUBLESHOOTING. PERFORMED TORQUE CHECK OF BOLTS ON CAPT AND F/O YOKE. BOLTS TORQUE WERE LESS THAN VALUE SPECIFIED IN AMM 27-11-01. RETORQUED LOOSE BOLTS TO PROPER TORQUE AND SAFETY WIRED. CONFIRMED YOKE SLIPPAGE IS NO LONGER PRESENT. REMOVED RIGS PINS. PERFORMED A RETURN TO SERVICE CHECK IAW AMM 27-00-00. NO FAULTS NOTED. PERFORMED FUNCTIONAL TEST OF AUTO-FLIGHT SYSTEM IAW 22-11-00 TEST OKAY. NO THUMP OR BINDING IN TEST MODE.