N346JB

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 23,795 hrs · 16,090 cycles

FLT 2934, EMERGENCY LIGHTS OVER WING UPPER SIGNS RH+ LH AS WELL AS CEILING SIGN FWD PANEL AND AFT CEILING EMERGENCY LIGHTS WILL NOT EXTINGUISH ON AIRCRAFT SHUT DOWN. R & R BATTERY OPS CK'D NORMAL IAW 33-50-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · airframe 23,301 hrs · 15,762 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE FR87-88 CENTER AFT GALLEY; (REF AEROMAN NR 420734) R & R FLOOR STRUCTURE WEB FR87-88 CENTER AFT GALLEY IAW SRM 51-40-08 & DEG 170-66000-439.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-23) · airframe 23,301 hrs · 15,762 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM FR12-23 RH SIDE; (REF AEROMAN NR 420726) ACCOMPLISHED REPAIR IAW AEROMAN EA 53-0024-20 COVER REV 0, PART 1, PART2 AND EMBRAER ETD 2020-790-001110 REV AND EC E20-019-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-15) · airframe 23,301 hrs · 15,762 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE WEB FR12-15 STR17L; (REF AEROMAN NR 420730) R & R WEB FLOOR STRUCTURE 51-40-08 & DWG 170-06822-507.

Part: WEB — CORRODED (FRAMES 87-88) · airframe 23,301 hrs · 15,762 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE WEB FR87-88 RH AFT GALLEY; (REF AEROMAN NR 420737) R & R FLOOR STRUCTURE WEB FR87-88 RH AFT GALLEY IAW SRM 51-40-08 & DEG 170-66000-439.

Part: WEB — CORRODED (FRAMES 87-88) · airframe 23,301 hrs · 15,762 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE WEB FR87-88 LH AFT GALLEY; (REF AEROMAN NR 420733) R & R FLOOR STRUCTURE WEB FR87-88 LH AFT GALLEY IAW SRM 51-40-08 & DEG 170-66000-439.

Part: LIFE RAFT — FAILED (FWD) · airframe 19,249 hrs · 12,820 cycles

IAW TASK CARD E190-25-60-00-200-901, FOUND THE FWD LIFE RAFT INDICATOR ON THE RED BAND. R & R THE FWD LIFE RAFT IAW AMM 25-66-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,984 hrs · 12,621 cycles

FT 2680, EWR-BOS, 2 EA EMERGENCY LIGHTS IN AFT CABIN INOP. WILL NOT TEST, REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 6 IAW AMM 33-50-01.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 17,058 hrs · 11,246 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO CUTOUT STRUCTURE MID SEAL REST. MID SEAL REST REPLACED IAW SRM 51-41-01 REV 36.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 11,618 hrs · 7,393 cycles

L2 & R2 EXIT LIGHT COVERS MISSING. INSTALLED MISSING LENS COVERS ON LIGHT ASSY IAW AMM 33-50-17. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND S2 LWR DOOR BEAM 13" AFT OF FRAME 86, RBL 44, RIVET CORRODED REPAIRED BY COMPLYING WITH EA E15-772-01 SPOT-FACE, NDT, TOPCOAT.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE FOUND AFT FUSELAGE, FRAME 88, STRINGER 28R, SHEAR TIE IS CORRODED. REPAIRED BY REMOVING AND REPLACING SHEAR TIE IAW SRM 51-41-02.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND AFT CABIN CORROSION ON AFT SERVICE DOOR LOWER BEAM HAS CORROSION 9.5 INCHES AFT OF FRAME 86 AT RBL 43. COMPLIED WITH EA TASK CARD E15-772-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE FOUND P2 LWR DOOR BEAM, 2 RIVETS CORRODED 9 INCHES AFT OF FRAME 86, LBL 43. REPAIRED BY COMPLYING WITH EA E15-774-01. SPOT-FACING, NDT, TOPCOAT.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND L2 DOOR LOWER BEAM HAS CORROSION AROUND RIVET, 9 INCHES AFT OF FRAME 85, LBL 45. REPAIRED BY COMPLYING WITH EA E15-774-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE FOUND P2 LOWER DOOR BEAM, 2 RIVETS CORRODED, 5" AFT OF FRAME 85, LBL 44". REPAIRED BY COMPLYING WITH EA 15-774-01, SPOT-FACING , NDT, TOPCOAT.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND AFT CABIN CORROSION AFT SERVICE DOOR LOWER BEAM HAS CORROSION 13.5 INCHES AFT OF FRAME 86 AT RBL 45. COMPLIED WITH EA TASK CARD E15-772-01.

Part: SEAT TRACK — CORRODED (FRAME 18) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION BLISTER ON LT SEAT TRACK AND FRAME 18. REPAIRED BY BLEND-OUT, NDT, CUTTING OUT DAMAGE, FABRICATING AND INSTALLING DOUBLER IAW SRM 53-10-10.

Part: FINGER DOUBLER — CORRODED (FRAME 78) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION AFT CARGO FWD FINGER DOUBLER 3" AFT OF FR 78, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE REF: SRM 51-43-03. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION, BLISTER ON LT SEAT TRACK AND FRAME 19. REPAIRED BY BLEND-OUT, NDT, CUTTING OUT DAMAGE, FABRICATING AND INSTALLING DOUBLER. IAW SRM 53-10-10.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION, AFT CARGO FWD FINGER DOUBLER 10 INCHES AFT OF FRAME 77, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE IAW SRM 51-43-03.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION, AFT CARGO FWD FINGER DOUBLER AT FRAME 77, RBL 15. R & R FINGER DOUBLER IAW SRM 51-43-03, SRM 41-43-04.

Part: FINGER DOUBLER — CORRODED (FRAME 78) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION AFT CARGO FINGER DOUBLER 1 INCH AFT OF FRAME 78, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE IAW SRM 51-43-03.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE FOUND AFT CABIN CORROSION ON AFT SERVICE DOOR LOWER BEAM HAS CORROSION 9.5 INCHES AFT OF FRAME 86 AT RBL 45. COMPLIED WITH EA TASK CARD E15-772-01.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION, AFT CARGO FWD FINGER DOUBLER 8" AFT OF FRAME 77, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE, REF SRM 51-43-03.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND L2 DOOR LOWER BEAM HAS CORROSION AROUND A RIVET 5 INCHES AFT OF FRAME 85, LBL 46. REPAIRED BY COMPLYING WITH EA E15-774-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND S2 LOWER DOOR BEAM, 6 INCHES AFT FRAME 85, RBL 44, RIVET CORRODED. REPAIRED BY COMPLYING WITH EA E15-772-01.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION. AFT CARGO FWD FINGER DOUBLER 2" AFT OF FR 77, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE, REF SRM 51-43-03.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,553 hrs · 6,695 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION. AFT CARGO FWD FINGER DOUBLER 14 1N. AFT OF FRAME 77, RBL 14. REPAIRED BY REMOVING AND REPLACING FINGER PLATE, REF SRM 51-43-03.

Part: I/O MODULE — FAILED (NR 1 MAU) · airframe 3,596 hrs · 2,166 cycles

FLT 978 FLL-BOS, AIR RETURN TO FLL DUE TO AUTO PILOT, AUTO THROTTLE FAILED IN FLIGHT. AUTO THROTTLE AURAL WARNING ON CONTINUOUSLY. TROUBLESHOOTING PER FAULT CODE 22110029PB1 FIM 22-11-00-810-82M. REMOVED AND REPLACED AIOPB1 IN MAU 1 MOD 9/10. GROUND OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 2,321 hrs · 1,447 cycles

FLT 1010 JFK-BOS, CREW DECLARED EMERGENCY DUE TO BLEED LEAK EICAS ON ENGINE 1. TROUBLESHOT PER FIM 36-11-00-810-836A NO LEAK LOCATIONS AVAILABLE IN NVM. COULD NOT REPRODUCE FAILURE THROUGH OPERATIONAL CHECK OF THE BLEED LEAK DETECTORS. CHECK OK.

Part: LOOP — FAULTY (BLEED AIR SYS) · airframe 2,056 hrs · 1,278 cycles

FLT 1677 FLL-KIN RETURNED TO FLL DUE TO BLEED 1 LEAK AT ALTITUDE- COMPLIED WITH QRH MESSAGE EXTINGUISHED. PERFORMED FIM TASK 36-11-00-810-836-A. 36-21-00-810-803-A AND 36-21-00-810-801-A. FOUND LOOPS A&B AT FAULT. REMOVED AND REPLACED LOOPS A&B IAW AMM 36-21-02. ALL CHECKS GOOD.