N354JB

Part: STEERING SYS — WARNING MESSAGE · airframe 24,134 hrs · 16,676 cycles

FLT#195, HPN-MCO. 'STEER FAIL ON APPROACH; NOTED ACTIVE FC 45452175CMC. ACCOMPLISH FIM TASK 45-45-00-810-973-A. TRANSITORY CONDITION OF THE STEERING CONTROL MODULE. AS A PRECAUTION, OPS CHECK OF NWS OK AND ALL STEERING PARAMETERS NORMAL ON CMC REF AMM 32-52-00.'

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: SEVERAL CORROSIONS ON FLOOR WEB (UPPER AND LOWER SURFACE) BTW FR 12-14 AND Y=920 TO Y=1240 RH SIDE; REF TOMX WORK ORDER 2047 NR 00251, REMOVED AND REPLACED WEB (UPPER AND LOWER SURFACE) BTW FR 12-14 AND Y=920 AND Y=1240 REF SRM 51-43-02 AND 51-41-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP BTW FR 81 STGR 27R AND STGR 28R OF AFT CARGO COMPARTMENT WAS FOUND; REF TOMX WO 2047 NR 0222. REMOVED AND REPLACED SHEAR CLIP BTW FR 81 STGR 27R AND 28R REF SRM 51-41-01 AND 51-41-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CRACK ON UPPER SKIN OF FIXED LEADING EDGE ON OUTBD SLAT TRACK OF SLAT #2 (BTW RIB 19 AND RIB 20) AT LH WING; REPAIRED CRON ON UPPER SKIN OF FIXED LEADING EDGE ON O/B SLAT TRACK OF SLAT #2 (BTW RIB 19 AND RIB 20). REF EC E22-793-01-N354J-B AND ETI 190-22-661.REF TOMX WO 2047 NR 00091.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON TRANSVERSAL BEAM BTW FR 84 AND Y=+300/1200; REF TOMX WO 2047 NR 00233. REMOVED AND REPLACED TRANSVERSAL BEAM REF SRM 51-41-01, 51-42-01, AND 51-43-01.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CRACK AND MIGRATED BUSHINGS IN HINGE FITTING #3 LOCATED IN FWD FRONT SPAR OF RUDDER SURFACE. TC NDT-55-40-00-211-801; REF TOMX WO 2047 NR-00305 RUDDER WAS REPLACED PER AIPC 27-21-05 ITEM 10, AMM 51-60-02-820-801-A ANDF JOB CARD 669 TASKCARD E190-27-21-05-400-801.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON FLOOR SUPPORT UPPER SURFACE BTW FR 15-16 AND Y=-1110 TO Y=-1170 (LH SIDE); REF. TOMX WO: N354JB/2047 NR-00260-: CORROSION ON FLOOR SUPPORT BTW FR 15-16 AND Y=-1110 TO Y=-1170 (LH SIDE) WAS REMOVED AND EVALUATED OUT OF LIMITS DUE TO EXCESSIVE CORROSION, PER EMB 190 SRM 51-12-00. THEREFORE WAS REPLACED PER EMB190 SRM 51-43-03.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP BTW FR 81 STGR 29 AND 28R OF AFT CARGO COMPARTMENT WAS FOUND; REF TOMX WO2047 NR00221, REMOVED AND REPLACED SHEAR CLIP BTW FR 81 STGR 29R AND 28R OF AFT CARGO COMPARTMENT REF SRM 51-41-01 AND 51-41-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON TRANSVERSAL BEAM BTW FR 84 AND Y=+300/1200; REF TOMX WO 2047 NR 00233. REMOVED AND REPLACED TRANSVERSAL BEAM REF SRM 51-41-01, 51-42-01, AND 51-43-01.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON WEB BTW FR 87 AND Y= +300 / Y=-1200; REF TOMX WO: N354JB/2047 NR-00229 - CORROSION ON SHEAR PANEL CENTRAL AND LH SIDE BTW FR87 AND Y= +300 / Y=-1200 WAS REMOVED AND EVALUATED OUT LIMITS PER EMB 190 SRM 51-12-01, SRM 51-10-03 AND SRM 53-23-- 10/AD53. THEREFORE WERE REPLACED BY NEW SHEAR PANELS PER EMB 190 SRM 51-42-01, SRM 51-42-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON FLOOR STRUCTURE WEB (UPPER AND LOWER SURFACE) BTW FR 12-16 AND Y=-1090 TO Y=-1270 (LH SIDE); REF. TOMX WO: N354JB/2047 NR-00259 - CORROSION ON FLOOR STRUCTURE WEB (UPPER AND LOWER SURFACE) BTW FR 12-16 AND Y=-1090 TO Y=-1270 (LH SIDE) WAS REMOVED AND EVALUATED OUT OF LIMITS PER EMB-190 SRM 51-12-- 01, SRM 51-10-03 AND SRM 53-10-10/AD56. THEREFORE WAS REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-43-04.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CRACK ON UPPER SKIN OF FIXED LEADING EDGE ON OUTB SLAT TRACK OF SLAT #2 (BTW RIB 19 AND RIB 20) AT RH WING; REF. TOMX WO: N354JB/2047 NR-00083 -: CRACK ON UPPER SKIN OF FIXED LEADING EDGE ON OUTB SLAT TRACK OF SLAT #2 (BTW RIB 19 AND RIB 20) AT RH WING WAS REPAIRED PER EMB 190 SRM 57-49-01 R/51;

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: SEVERAL CORROSIONS ON FLOOR STRUCTURE WEB UPPER BTW FR 15-16 AND Y=.-320 TO Y=-930 LH SIDE; REF TOMX WO 2047 NR 00262. REMOVED AND REPLACED DOUBLE UPPER SURFACE BTW FR 15-16 Y=-320 TO Y=-930 LH SIDE REF SRM 51-41-02 AND 51-42-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: REF TOMX WO 2047 NR 00253. CORROSIONS ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR 12-19 AND Y=240 TO Y=300 RH SIDE; REMOVED AND REPLACED LONGITUDINAL BEAM REF SRM 51-41-01,51-41-02,51-43-01 AND 51-43-04.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON LONGITUDINAL BEAM BTW FR 87/85 AND Y=-300; REF TOMX WO 2047-NR 00230; REMOVED AND REPLACED LONGITUDINAL BEAM BTW FR 85/86 PER SRM 51-41-01 AND SRM 51-43-03.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP BTW FR 84 STGR 25L AND STGR 24L OF AFT CARGO COMPARTMENT; REMOVED AND REPLACE SHEAR CLIP BTW FR84 STGR 25L AND STGR 24L REF SRM 51-41-01 AND 51-41-02. REF TOMX WO 2047 NR 00225.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP BTW FR 82 STGR 28R AND STGR 27R OF AFT CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR CLIP BTW FR 82 STGR 28R AND 27R OF AFT CARGO PER SRM 51-41-01 AND 51-41-02. REF TOMX WO 2047 NR 00224.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / SKIN / KA LTV RADOME / HOLES / CORROSION. PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: SEVERAL CORROSIONS ON TRANSVERSAL BEAM OF FLOOR STRUCTURE ON FR 17 BTW Y=-290 TO Y=290; REPAIRED TRANSVERSAL BEAM FLOOR STRUCTURE REF EMB 190 SRM 53-00-10 REPAIR 53. REF TOMX WO 2047 NR00264.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: REF TOMX WO 2047 NR 00343. LH PYLON CRACKED ON IB SPAR FITTING; REF TOMX WO 2047 NR 00343. REMOVED AND REPLACED LH PYLON IB SPAR FITTING PER SRM 51-41-02 PAR.4/PAR.6 SRM 51-43-03 PAR.4/PAR..5 AND SRM 51-43-04 PAR.4/PAR.5.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP BTW FR 88/ STGR 28R OF AFT CARGO COMPARTMENT; REF TOMX WO 2047 NR 00226. REMOVED AND REPLACED SHEAR CLIP BTW FR 88 STGR 28R REF SRM 51-41-01 AND 51-41-02.

Part: NONE — NONE · airframe 23,987 hrs · 16,584 cycles

DURING HEAVY MAINTENANCE: CORROSION ON FLOOR SUPPORT (UPPER SURFACE) BTW FR 12-13 AND Y=350 TO Y=410 RH SIDE; REF TOXM WO 2047 NR 00252. REMOVED AND REPLACE FLOOR SUPPORT IAW EMB 190 SRM 51-41-01 AND 51-43-01. BTW FR 12-13 AND Y=350 TO Y=410 RH SIDE.

Part: FRAME — DAMAGED · airframe 23,688 hrs · 16,347 cycles

FLT#6220, SAV-MCN. 'REF LOG PAGE 3438867-1 (HIT BIRD AT 2000FT ON TOP RIGHT OF COCKPIT ) HIT BIRD AT 2000FT ON TOP RIGHT COCKPIT; REF EAMS WO H8723 N/R 00001 REPAIRED BIRD STRIKE TO FRAME10-11 STR 3R-6R IAW EMBRAER ETD 2022-190-023487 REV A THIS REPAIR DOES NOT ADVERSELY AFFECT A FATIGUE CRITICAL STRUCTURE AND DOES NOT REPRESENT AN AIRWORTHINESS LIMITATION. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE REQUIRED AND JB EC E22-580-01 FOR ACCOMPLISHING THE PERMANENT REPAIR.'

Part: SKIN — DAMAGED · airframe 23,691 hrs · 16,348 cycles

DURING HEAVY MAINTENANCE AT MCN-EAMS: FUSELAGE/ FWD FUSELAGE/ UPPER SKIN/ RH DONE/ BIRD STRIKE- PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)

Part: GIRT BAR — OUT OF ADJUST · airframe 23,221 hrs · 16,041 cycles

FLT#676, JFK-ORH. 'L1 CABIN DOOR WILL NOT DISARM SO FA'S CAN'T OPEN IT; PER FIM 52-11-00-810-808-A ADJUSTED GIRT BAR IN REF WITH AMM 52-11-41. MULTIPLE TESTS OK.'

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 21,269 hrs · 14,759 cycles

FLT 1376, KIN-FLL. L/H OVERWING EMERGENCY DOOR EXIT LIGHT (BOTTOM) INOP ; REPLACED LEFT SIDE OVERWING LOWER EMERGENCY EXIT LIGHT ASSY IAW AMM 33-50-15, TEST GOOD

Part: RIB — CRACKED (LT WING) · airframe 20,657 hrs · 14,371 cycles

DURING HEAVY MAINTENANCE, WINGS/LT WING/WING MAIN BOX TRAILING EDGE AT RIB 10, CRACK, PERMANENT REPAIR. CLASSIFIED AS MAJOR REPAIR.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 20,657 hrs · 14,371 cycles

SUPPLEMENTAL INFORMATION (RESUBMISSION DIFFICULTY DATE): DURING HEAVY MAINTENANCE, REF TECHOPS MX W/O 1466 N/R 00073, DURING PASSENGER CABIN FINAL WALK. EMERGENCY LIGHT ON AFT SERVICE DOOR SURROUND DOES NOT TURN ON. R & R EMERGENCY LIGHT ASSEMBLY PACK, PER EMB190 AMM 33-50-15-420-006-A,

Part: WIRE — BROKEN (ELT) · airframe 20,655 hrs · 14,370 cycles

DURING RETURN TO SERVICE, FOUND FIXED ELT INOPERABLE. FOUND WIRE W202-00291-22 BROKEN AT CONNECTOR P1236. REPINNED WIRE, IAW SWPM 20-41-10. FIXED ELT, OPERATIONS CHECKS GOOD, IAW AMM 25-61-00-710-801-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,864 hrs · 13,061 cycles

FLT 2002, JFK-BUF. EXPERIENCED CABIN ODOR FROM ENV SYSTEM PRIMARILY DURING TAXI INITIALLY ATTRIBUTED TO EXT. SOURCE BUT HAD MILD RESIDUAL AIRBORNE; COMPLIED WITH FIM TASK 21-20-00-810-801-A COULD NOT DUPLICATE ODOR.

Part: SEAL — FAILED (PRECOOLER) · airframe 17,631 hrs · 12,152 cycles

FT # 1106, DISPATCH ADVISED MCC THAT THE A/C WAS RETURNING TO THE FIELD FOR A PRESSURIZATION ISSUE. THE #1 PACK IS CURRENTLY ON MEL, BLEED #2 FAILED. CAPTAIN REPORTED INTERMITTENT FAULT ON PACK 2 WHEN BLEED 2 FAULT OCCURRED. BLEED 2 FAIL ( ENGINE BLEED SYS - SINGLE - ICING OK ); UPON TROUBLESHOOTING ON #2 ENG BLEED 2 FAULT FOUND AN AIR LEAK FROM NACELLE PRSOV VALVE TO THE PRECOOLER DUCT. REMOVED AND REPLACED E SEAL AT THE PRECOOLER AND ENG LINE DUCT. RAN ENG NO FAULTS AND LEAKS. RESTORE A/C TO NORMAL CONFIGURATION MDDR 384244 CLEARED PLACARD REMOVED OPS CHECK OK PER AMM 36-11-03.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 14,085 hrs · 9,687 cycles

FOUND THE EMERGENCY LIGHT FWD POWER SUPPLY MALFUNCTIONED. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: DOOR — NONE (R1) · airframe 14,031 hrs · 9,644 cycles

R1 DOOR STUCK IN ARMED POSITION. REMOVED THE BUSTLE AND PINNED BOTTLE, APPLIED HEAD AND PERFORMED OPS CHECK OF DOOR IAW AMM 52-41-00. OPS NORMAL. REMOVED PIN AND INSTALLED BUSTLE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,310 hrs · 6,948 cycles

RIGHT WING OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-00. OPERATIONAL CHECK NORMAL.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 10,310 hrs · 6,948 cycles

CORROSION AFT CARGO FWD FINGER DOUBLER RBL 16.5 ,1.5 INCHES AFT OF FRAME 77. REMOVED AND REPLACED LEFT HAND SHEAR PANEL IAW SRM 51-42-01;51-43-03;51-43-04. REF.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,310 hrs · 6,948 cycles

RIGHT PANEL SUPPORT CORRODED 10.0" TO 15.0" AFT OF FRAME 89 AND RBL 34.0"-35.0". R & R RT PANEL SUPPORT AFT OF FRAME 89, REF SRM 53-23-10.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,310 hrs · 6,948 cycles

LEFT SHEAR PANEL CORRODED AT FRAME 87 AND LBL 39.75 TO LBL 41.0. R & R LT SHEAR PANEL AT FRAME 87 REF SRM 51-42-01, REF EAMS NR 156 FOR ADDITIONAL INFORMATION.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,310 hrs · 6,948 cycles

CORROSION AFT CARGO DOOR FORWARD FINGER DOUBLER 6" AFT OF FRAME 77, RBL 14". REMOVED CORROSION IN MARKED AREA REF SRM 51-12-01. MATERIAL REMOVED IS 1.0 X 0.5 X 0.010. REMOVED FROM ORIGINAL OF 0.157. PART WILL BE REPLACED ON NR 058, REF.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,407 hrs · 4,258 cycles

DURING MAINTENANCE AFT RT EMERGENCY LIGHT WING FAIRING AND CEILING PANEL EMERGENCY LIGHT ROW 21 INOPERATIVE. R & R EPLU NR 6 IAW AMM 33-50-01. OPS CHECK NORMAL.

Part: PRESSURE SWITCH — MALFUNCTIONED (CABIN PRESSURE) · airframe 4,213 hrs · 2,796 cycles

ACFT RETURN TO DEPARTURE DUE TO CABIN ALT HIGH EICAS MESSAGE WHEN CLIMBING OUT OF 28,000 FT. CABIN ALTITUDE INDICATED 8000 FT AND OXYGEN MASKS DROPPED. CABIN ALTITUDE INDICATOR NEVER WENT ABOVE 8000 FT AND IMMEDIATELY STARTED DOWN DURING DESCENT. R & R ALTITUDE PRESSURE SWITCH IAW AMM 35-21-02. PERFORMED FUNCTIONAL CHECK OF ALTITUDE PRESSURE SWITCH IAW AMM 35-21-02 SYS. OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 461 hrs · 284 cycles

FLT 742 SJU-MCO, CREW REPORTED EMERGENCY LIGHT DECK DOES NOT COME ON WITH EMERGENCY LIGHT SWITCH IN ON POSITION. REPLACED BATTERY EMERGENCY A/C RIGHT FWD IAW AMM 33-50-01. OPS CHECK GOOD.