N231JB

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,168 hrs · 29,542 cycles

FLT#582, RSW-DCA. 'WHILE PERFORMING TASK CARD E190-33-50-01-720-801-M. FOUND RH OVERWING EXIT IDENTIFIER SIGN INOP; REMOVED AND REPLACED RH OVERWING EXIT IDENTIFIER SIGN IAW AMM 33-50-15 OPS CHECK GOOD. PART INSTALLED ROBBED FROM A/C 216JB REF TO LOG PAGE 3625598, ITEM 1 (REPLACED RH OVERWING EXIT LOWER IDENTIFIER SIGN IAW AMM 33-50-15. OPS CHECKS GOOD.). THIS ACTION C/W WITH T/C E190-33-50-01-720-801-M OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR73 STGR 28RH/29RH AT AFT CARGO COMPARTMENT; REPLACED SHEAR CLIP IAW EMB SRM 51-41-01 AND 51-41-02. WORK ACCOMPLISHED ON TOMX NR 00162. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR 87 STGR 28RH.27RH AT AFT CARGO COMPARTMENT; FOUND OUT OF LIMITS. REPLACED SHEAR CLIP IAW EMB SRM 51-41-01, 51-41-02, AND 51-41-03. WORK ACCOMPLISHED ON TOMX NR 00182. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / CROSS BEAM 84 / CORROSION - PERMANENT REPAIR. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION CENTRAL BEAM LH FR 12-20 AT PASSENGER CABIN FLOOR STRUCTURE; FOUND OUT OF LIMITS. REPLACED BEAM IAW EMB 190 SRM 53-10-10/AD 51, 51-41-01, AND 51-43-03. WORK ACCOMPLISHED ON TOMX NE 00148. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION IN LONGITUDINAL BEAM LOCATED BETWEEN FR 85 +12 INCHES AND FRAME 89 AND Y270 CF III FLOOR STRUCTURE; FOUND OUT OF LIMITS. REPLACED BEAM IAW EMB 190 SRM 53-23-10/AD52, 51-41-01, 51-42-01 AND 51-43-03. WORK ACCOMPLISHED ON TOMX NR 00098. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION CENTRAL BEAM RH FR12-18 AT PASSENGER CABIN FLOOR; FOUND OUT OF LIMITS. REPAIRED BEAM IAW EMB190 SRM 53-10-10/REPAIR 51 AND ETI-190-23-548 REV 3. WORK ACCOMPLISHED ON TOMX NR 00147. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION IN SEAT TRACK LOCATED FR 60 AND 73, Y260; FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW EMB190 SRM 53-22-10/AD52, 51-41-01, 51-43-01 AND 51-43-02. WORK ACCOMPLISHED ON TOMX NR 00105. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: R/H WING LEADING EDGE SKIN AT RIB 17 HAS WEAR AND A CRACK; THIS HAS BEEN ACCOMPLISHED BY EC E-23-368-01. A/C IS OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR75 STGR 28RH/29RH AT AFT CARGO COMPARTMENT; REPLACED SHEAR CLIP IAW EMB 190 SRM 51-41-01 AND 51-41-02. WORK ACCOMPLISHED ON TOMX NR 00165. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER SKIN PANEL BTWN FR2 TO FR8 & STRG28R TO STRG28L / LIGHTNING STRIKE BURN MARKS - PERMANENT REPAIR. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION IN THE DOUBLER LOCATED IN LONGITUDINAL BEAM AT Y=-310.0 AND FR 84/85 IN CF III FLOOR STRUCTURE; REF TOMX NT 00096. DOUBLER WAS REPLACED PER EMB SRM 51-43-01, 51-43-03, 51-41-02 AND 53-23-10/REP 54.( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION IN CROSS BEAM LOCATED IN FR84 BETWEEN Y500 AND Y930 AT CF III FLOOR STRUCTURE; FOUND OUT OF LIMITS, REPAIRED PER EMB 190 SRM 53-23-10 REPAIR 55 AND ETI-190-23-551 REV 3. WORK ACCOMPLISHED ON TOMX NR 00092.( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOORS / RH FLOOR TRACK / BTWN Y = 273.0 AND FR 12-13 & EXISTING DOUBLER REPAIR BTWN Y=273.0 AND FR13-14 / CORROSION - PERMANENT REPAIR. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR88 STGR 28RH/27RH AT AFT CARGO COMPARTMENT; FOUND OUT OF LIMITS. REPLACED SHEAR CLIP IAW EMB 190 SRM 51-10-02, 51-41-02 AND 51-43-03. WORK ACCOMPLISHED ON TOMX NR 00180. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: WINGS / RH WING / LEADING EDGE SKIN AT RIB 17 / WEAR AND CRACK - PERMANENT REPAIR. ( CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 43,619 hrs · 28,359 cycles

DURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP OVER FR86 STGR 22LH/23LH AT AFT CARGO COMPARTMENT; FOUND OUT OF LIMITS. REPLACED SHEAR CLIP IAW EMB 190 SRM 51-10-03, 51-41-01 AND 51-41-02. WORK ACCOMPLISHED ON TOMX NR 00230. ( CONSIDERED AS A MAJOR REPAIR)

Part: ROD — LOOSE (MLG ACTUATOR) · airframe 43,020 hrs · 27,924 cycles

FLT#1288, PBI-PVD. 'RIGHT MAIN GEAR DOOR FORWARD ACTUATOR ROD LOSSE AT THE TOP ( MAIN LANDING GEAR DOOR); SWING GEAR & ADJ R/H MLG LOWER DOOR PER AMM 32-12-00. MDDR CLEARED. MX-4 UPDATED.

Part: PRESSURE VALVE — FALSE INDICATION · airframe 41,020 hrs · 26,487 cycles

FLT # 2030, RSW-JFK(DIVERTED TO MCO). BLEED 2 LEAK; T/S PER FIM 36-11-00-810-837A ODS SYSTEM NORMAL - NO FAULTS. FOUND LEAKS AT #2 ENG PRSOV AND CROSS BLEED DUCTING GOING TO RT BLEED. SECURED CLAMPS- AFTER OPS CKS NORMAL. RAN APU/ ENG 2 BLEED FOR 1 HOUR- NO FAULTS. AIRCRAFT OK FOR SVC.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 39,925 hrs · 25,696 cycles

FLT 519, JFK-ATL. ON SHORT FINAL "" HYD 2 LO QTY"" MESSAGE APPEARED. ON CLEARING RUNWAY LOST ALL SYSTEM 2 HYD PRESSURE FOLLOWED BY LOSS OF STEERING; FOUND R/H LANDING HGEAR SIDE STAY EXTEND HOSE RUPTURED. R & R SIDESTAY HOSE HOSE IAW AMM 32-11-05-400. NO LEAKS NOTED

Part: ACM — FAILED (LEFT) · airframe 39,851 hrs · 25,650 cycles

FLT 1351, ACK-BOS. PACK 1 FAIL (SMELL OF SMOKE BEFOR IT FAILED) ( AIR CONDITIONING PACKS - SINGLE ) ; R&R #1 ACM IAW AMM 21-51-05. OPS CHECK GOOD AT THIS TIME. MX-4 UPDATED AND PLACARD REMOVED.

Part: FLOORBEAM — CORRODED (FRM 84) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: FLOOR STRUCTURE FR84 @ Y=230RH ; REF TOMX NR 00391: ORIGINAL DOUBLE REPAIR WAS REMOVED & REPLACED IAW EMBRAER SRM 51-43-03 ITEM 6 FIG 2, 51-43-04 ITEM 5 FIG 2 AND 53-23-10 REPAIR 54 ITEM 6 STEP J-M.

Part: SKIN — CRACKED (LT WING LE) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CRACK: LH WING LEADING EDGE SLAT TRACK #5 CUTOUT ; REF TOMX NR 00013: R & R LEADING EDGE SKIN LH WING RIB 17 TO RIB 22 IAW 51-43-04 PAR. 5 FIG 2, 51-42-02 PAR. 6 FIG 2, AND 5-42-02 PAR.5 FIG 2.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: AFT SEAL REST AT AFTCARGO DOOR CUTOUT ; CORROSION @ AFT SEAL REST OF AFT CUTOUT REMOVED PER EMB E-190 SRM 51-12-01 PAR.6B & FOUND OUT OF LIMITS PER EMB E-190 SRM 53-23-11 PAR. 5 TABLE101.SEAL REST WAS REPLACED PER EMB E-190 SRM 51-40-08 PAR.6 & SRM 51-41-01 PAR. 4 FIG. 2.ALL WORK PERFORMED ON TOMEX NR 00306.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: MIDDLE SEAL REST AT AFT CARGO DOOR CUTOUT ; CORROSION ON MIDDLE SEAL REST AT AFT CARGO DOOR CUTOUT WAS REMOVED PER EMB E-190 SRM 51-12-01 PAR. 6B & FOUND OUT OF LIMITSPER EMB E-190 SRM53-23-11 PAR. 5 TABLE 101. SEAL REST REPLACED PER EMB E-190 SRM 51-40-08 PAR.6 & SRM 51-41-01 PAR.4 FIG. 2. ALL WORK ACCOMPLISHED ON TOMEX NR 00306.

Part: SEAT TRACK — CORRODED (FRMS 45-46) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: RH SEAT TRACK FR45-46RH ; REF TOMX NR 00477: BLEND-OUT ACCOMPLISHED & OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-41-01 STEP 6 FIG 2 AND SRM 51-43-03 STEP 6 FIG 2.

Part: SEAL REST — CORRODED (AFT CARGO DOOR) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION ON FOWARD SEAL REST AT AFTER CARGOO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306. CORROSION ON FOWARD SEAL REST AT AFTER CARGOO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306"

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION ON MIDDLE SEAL REST AT AFT CARGO DOOR CUTOUT WAS REMOVED PER EMB E-190 SRM 51-12-01 PAR. 6B & FOUND OUT OF LIMITSPER EMB E-190 SRM53-23-11 PAR. 5 TABLE 101. SEAL REST REPLACED PER EMB E-190 SRM 51-40-08 PAR.6 & SRM 51-41-01 PAR.4 FIG. 2. ALL WORK ACCOMPLISHED ON TOMEX NR 00306. REF. TOMEX NR 00015."

Part: SEAL REST — CORRODED (AFT CARGO) · corrosion level 2 · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION ON MIDDLE SEAL REST AT AFTER CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306. CORROSION ON MIDDLE SEAL REST AT AFTER CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306"

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, FWD LH OVERWING EMERGENCY EXIT LIGHT INOP ; REF TOMX NR 00060: R & R FWD LH EXTERNAL EMERGENCY EXIT LIGHT ASSY IAW AMM 33-50-25-000-802-A & 33-50-25-400-802-A. OPS CHECKS SATIS.

Part: SKIN — WORN (RT WING LE) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, WEAR ON RH WING FIXED LEADING EDGE SKIN FROM RIB22-RIB24 ; REF TOMX NR 00605: REPLACED FIXED LEADING EDGE SKIN RIB17-23 RH WING IAW SRM 51-42-02 PAR. 6 FIG 2, SRM 51-43-04 PAR.5 FIG 2, AND 51-42-02 PAR 5 FIG 2.

Part: RIB — CRACKED (WNG-BDY FAIRING) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, E/C E21-651-01 FUSELAGE/ CENTER FUSELAGE II WING TO FUSELAGE FAIRING FRAME 52 RH RIB/CRACK-PERMANENT REPAIR

Part: FLOORBEAM — CORRODED (FRM 84) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: FLOOR STRUCTURE FR84 & Y1200LH ; REF TOMX NR 00394: R & R PANEL IAW EMB 190 SRM 51-41-02 PAR 6 AND 51-41-01 PAR. 06.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: FWD. SEAL REST AT AFT CARGO DOOR CUTOUT ; CORROSION ON FWD. SEAL REST AT AFT CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR. 6B AND FOUND OUT OF LIMITS PER EMB SRM 53-23-11. SEAL REST WAS REPLACED PER EMB SRM E190-51-40-08 PAR. 6 & SRM 51-41-01 PAR. 4 FIG.2. ALL WORK PERFORMED ON TOMX NR 00306.

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION ON FWD SEAL REST AT AFT CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR. 6B AND FOUND OUT OF LIMITS PER EMB SRM 53-23-11. SEAL REST WAS REPLACED PER EMB SRM E190-51-40-08 PAR.6 & SRM 51-41-01 PAR. 4 FIG. 2. ALL WORK PERFORMED ON TOMX NR 00306. THIS ITEM ENTERED IN ERROR AS A DUPLICATE. ITEM ENTERED UNDER NR 00006 THIS WORK ORDER. COMPLETED AND CLOSED"

Part: SEAL REST — CORRODED (AFT CARGO) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION @ AFT SEAL REST OF AFT CUTOUT REMOVED PER EMB E-190 SRM 51-12-01 PAR.6B & FOUND OUT OF LIMITS PER EMB E-190 SRM 53-23-11 PAR. 5 TABLE101.SEAL REST WAS REPLACED PER EMB E-190 SRM 51-40-08 PAR.6 & SRM 51-41-01 PAR. 4 FIG. 2.ALL WORK PERFORMED ON TOMEX NR 00306. CORROSION @ AFT SEAL REST OF AFT CUTOUT REMOVED PER EMB E-190 SRM 51-12-01 PAR.6B & FOUND OUT OF LIMITS PER EMB E-190 SRM 53-23-11 PAR. 5 TABLE101.SEAL REST WAS REPLACED PER EMB E-190 SRM 51-40-08 PAR.6 & SRM 51-41-01 PAR. 4 FIG. 2.ALL WORK PERFORMED ON TOMEX NR 00306. "

Part: SEAL REST — CORRODED (FRM 80) · corrosion level 2 · airframe 39,538 hrs · 25,457 cycles

DURING HMV, "CORROSION ON AFT SEAL REST AT AFTER CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306. CORROSION ON AFT SEAL REST AT AFTER CARGO DOOR CUTOUT WAS REMOVED PER EMB SRM 51-12-01 PAR 6.B AND WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-11 SEAL REST WAS REPLACED PER EMB E190 SRM 51-40-08 PAR 6 AND SRM 51-41-01 PAR 4 FIG 2. ALL WORK ACCOMPLISHED ON TOMX NR # 00306"

Part: SEAL REST — CORRODED (FWD CARGO DOOR) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: CENTER SEAL REST ON FWD CARGO DOOR ; REF TOMX NR 00569: R & R SEAL REST CENTER FWD CARGO DOOR IAW SRM 51-41-01 PAR. 6 FIG 2.

Part: RIB — CRACKED (FAIRING) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CRACK: RIB SUPPORT CENTER FUSELAGE FAIRING FR52 Y=1305 ; REF TOMX NR 00622: ACCOMPLISHED PERMANENT REPAIR IAW TOMX ETI-190-760 REV 1, EMBRAER ETD2021-190-018033, AND JETBLUE EC E21-630-01. NO FURTHER ACTION REQ'D.

Part: FITTING — CORRODED (CARGO DOOR LATCH) · airframe 39,538 hrs · 25,457 cycles

DURING HMV, CORROSION: FWD CARGO DOOR CUTOUT LATCH FITTINGS SETTLEMENT AREA ; REF TOMX NR 00571: BLEND-OUT OUT OF LIMITS. R & R BEAM IAE SRM 51-43-04 PAR 5 FIG 2.

Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 39,200 hrs · 25,285 cycles

FLT 6140, PBI-FLL. SLAT FAIL EICAS MSG. FOLLOWED QRH. QRH DID NOT MANAGE TO RESET SLATS. LANDED SLAT 0/ FLAP 2; R & R R/H S2/3 SKEW SENSOR PER AMM 27-83-01 OPS CK OK. ACCOMPLISHED SLAT ADJUSTMENT/TEST PER AMM 37-80-00, ALL CKS NORMAL. OK TO CONT SVC.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 39,021 hrs · 25,168 cycles

DURING HEAVY MAINTENANCE, INOPERABLE ELPU 1 RT SIDE AT FWD GALLEY AREA, REF AEROMAN NR 2020-401038 WO 2020 384/1. R & R ELPU 1 RT SIDE AT FWD GALLEY AREA, IAW E190 AMM 33-50-01-000-8010-A, 33-50-01-400-801-A. PERFORMED OPERATIONAL TEST, IAW E190 AMM 33-50-01-710-801-A AND 33-50-00-710-801-A, ALL TESTS OK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 39,021 hrs · 25,168 cycles

DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LT BATTERY (ELPU) MID TH SIDE AT PASSENGER CABIN, REF AEROMAN WO 384/1 WCC 2020-401009. R & R ON SERVICEABLE CONDITION THE EMERGENCY LIGHT POWER SUPPLY (ELPU) MID RT SIDE AT PASSENGER CABIN, IAW E190 AMM 33-50-01-400-801-A. PERFORMED EMERGENCY LIGHTING OPERATIONAL TEST, IAW E190 AMM 33-50-00-710-801-A AND PERFORMED EMERGENCY LIGHT POWER UNIT OPERATIONAL TEST, IAW E190 AMM 33-50-01-710-801-A AND TESTS ARE OK.

Part: MODULE — FAILED (ANTI-ICE) · airframe 38,365 hrs · 24,708 cycles

FT # 111, BOS-ORD. RETURNED TO FIELD. A/I ENG 1&2 FAIL PASSING 8000 ON CLIMBOUT. QRH RAN FAIL REMAINED; R & R ANTI ICE MODULE IAW AMM 30-00-01. OPS CHECK GOOD IAW AMM 30-21-00. A/C OK FOR SVC.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 36,045 hrs · 22,992 cycles

FLT 581, JFK-HOU. EXIT LIGHTS FAILED TO ILLUMINATE ONCE GEARS CAME DOWN; PERFORMED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM, OPS CHECK OK IAW AMM 33-50-00-710-801-A. MCC NOTIFIED.

Part: HOOK AND LOOP — WORN (RT DOOR) · airframe 32,086 hrs · 20,190 cycles

RT DOOR OPEN EICAS MESSAGE AT FL 360 DURING DESCENT. EICAS MESSAGE EXTINGUISHED DESCENDING THROUGH 17000 FT. FOUND DOOR LATCH COVER HOOK AND LOOP TO BE WORN. APPLIED NEW HOOK AND LOOP IAW 52-20-00. NO FURTHER DEFECTS NOTED.

Part: SENSOR — FAILED (TE FLAPS) · airframe 29,439 hrs · 18,286 cycles

ON FINAL APPROACH, CREW DROPPED THE FLAPS AND RECEIVED A FLAP FAIL MESSAGE FLAP FAIL. EMERGENCY DECLARED. R & R THE FLAP POSITION SENSOR UNIT IAW AMM 27-53-04. PERFORMED OPS CHECK FLAPS SYSTEM IAW AMM 27-50-00-710-801-A500.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 28,149 hrs · 17,361 cycles

LEFT OVERWING BOTTOM EMERGENCY EXIT LIGHT FOUND TO BE INOPERATIVE, R & R MIDDLE CABIN POWER SUPPLY IAW E190 AMM 33-50-01. OPS CHECK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 28,149 hrs · 17,361 cycles

EMERGENCY LIGHT IN COCKPIT WAS FOUND TO BE INOPERATIVE; R & R FORWARD CABIN POWER SUPPLY IAW AMM 33-50-01. OPS CHECK GOOD.

Part: CROSSBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,788 hrs · 16,494 cycles

FWD FUSELAGE RT RBL 20 AT FR 17 CROSSBEAM CORROSION. REPAIRED CROSSBEAM IAW EA E15-1130-01.

Part: SHEAR TIE — CORRODED (FRAME 23) · corrosion level 2 · airframe 26,788 hrs · 16,494 cycles

CORROSION ON FRAME 23 SHEAR TIE BETWEEN STR 20 AND 21R. REPLACED THE SHEAR TIE IAW E190 SRM 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 72) · corrosion level 2 · airframe 26,788 hrs · 16,494 cycles

SHEAR TIE FRAME 72 BETWEEN STR 29R-28R CORRODED PN 190-27254-001. REPLACED SHEAR TIE IAW SRM 51-41-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,997 hrs · 13,376 cycles

DURING WALK-AROUND, FOUND RT MIDDLE EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED RT MIDDLE EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-25. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FRAME 16) · airframe 21,859 hrs · 13,289 cycles

DURING HEAVY MAINTENANCE CHECK, FOUND FWD FUSELAGE FRAME 16 FLOORBEAM CORRODED. DETAILED VISUAL INSPECTION AND NDT ACCOMPLISHED, CUT DAMAGED SECTION AND FABRICATED PART. ALL WORK ACCOMPLISHED IAW EC E14-067-01/EAMS NR H4185/2592.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,621 hrs · 13,146 cycles

CREW DECLARED AN EMERGENCY AND DIVERTED. DURING DESCENT, NOTICED A STRONG BURNING ODOR IN THE AFT GALLEY. ODOR APPEARED TO COME FROM THE COFFEEMAKER. SMELLED LIKE A BURNING MATCH. NO VISIBLE SMOKE. RAN PARTIAL QRH FOR SMOKE & FUMES. ODOR DISIPATED AND ONLY REAPPEARED FOR A SHORT TIME BEFORE POWER WAS SHUTDOWN. PERFORMED FIM TASK 25-30-00-810-801A WITH NO DEFECTS NOTED. NOTED COFFEEMAKERS WARMING TRAYS ON WITH NO COFFEE IN POTS. PERFORMED OPS CHECK OF AFT COFFEMAKERS IAW AMM 25-37-00. OPS CHECKED GOOD.

Part: ACM — FAILED (AC BAY) · airframe 17,537 hrs · 10,629 cycles

FLT 1722 MBJ-MCO, ON TAXI OUT AFTER CRANKING NR 2 ENGINE HAS A SMELL OF SOMETHING BURNING THEN NOTICED RAPID INCREASE IN CABIN/COCKPIT TEMP. THEN REPORT FROM F/A SMOKE IN ROW 18 AND BACK. STOP AIRPLANE REF QRH THEN TURN OFF PACK 1 & 2 ALONG WITH RECIRCULATION FANS AND SMOKE STOPPED AT THAT POINT. PERFORMED FAULT ISOLATION FOR SMOKE IN CABIN IAW FIM 21-20-00-810-801-A FOUND NR 1 ACM AT FAULT. THE NR 1 ACM WAS REMOVED AND REPLACED IAW AMM 21-20-00 AND OPS CHECK GOOD.

Part: FITTING — LEAKING (NLG) · airframe 16,732 hrs · 10,148 cycles

FLT 6407 BNA-BOS, CREW DECLARED EMERGENCY AND AIR RETURN TO BNA DUE TO L/G WOW SYS FAIL AND L/G WOULD NOT RETRACT. TROUBLESHOT WOW SYS, NO DISCREPANCIES FOUND. INSPECTED AND FOUND HIGH PRESSURE FITTING LEAKING. REMOVED AND REPLACED FITTING ASSY. SERVICED NOSE LANDING GEAR IAW 12-12-09. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 32-33-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,731 hrs · 10,147 cycles

FLT 6401 BOS-BNA, ON HEAVY MAINTENANCE CHECK FOUND AFT CABIN RIGHT SEAT TRACK HAS CORROSION AT FR 84 AS MARKED P/N 170-86082-005. REPAIRED BY BLENDING TO REMOVE CORROSION, HFEC, FILL AND BLEND AREA WITH HYSOL EA9396. INSTALL FABRICATED STRAP WITH EXISTING FASTENERS AND 4 FASTENERS PAST BLEND ON BOTH LEGS OF STRAP, PRIME, TOPCOAT AND FILLET SEALANT APPLIED AS PER EC E12-315-01.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 16,731 hrs · 10,147 cycles

FLT 6401 BOS-BNA, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN RIGHT FLOOR CROSS BEAM 17 HAS CORROSION AS MARKED P/N 170-21769-405. REPAIRED BY INSTALLING "L" ANGLE REPAIR, CUTOUTS AT 2 BLENDED AREAS, RESIN FILL IN, HI-LITES 5 PAST DAMAGED AREA AT VERTICAL FLANGE. ALODINE, PRIME, SEAL AND TOPCOATED AS REQUIRED PER EA E12-316-01.

Part: SPINNER — CRACKED (LT ENGINE) · airframe 15,979 hrs · 9,676 cycles

FLT 1061, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED AT FL350, LEFT ENGINE STARTED VIBRATING, ODOR IN CABIN NOT SMOKE BUT HOT METAL. THE N1 VIBRATION WAS 5.0. SPINNER WAS FOUND WITH 8" BY 2" CRACKED AND DISLODGED WHICH CAUSE DAMAGE TO LT ENGINE. REMOVED AND REPLACED LT ENGINE AS PER AMM 71-00-01-04.

Part: COFFEEMAKER — BURNED (GALLEY) · airframe 13,692 hrs · 8,260 cycles

DURING CRUISE - CREW REPORTED BURNING PLASTIC SMELL IN FWD GALLEY. GALLEY WORK LIGHTS AND COFEE POTS WERE TURNED OFF AND SMELL DISAPPEARED. FOUND SOURCE OF ODOR COMING FROM NR 1 COFFEEMAKER. R & R COFFEEMAKER IAW AMM 25-37-03. OPS CK GOOD.

Part: ACM — CONTAMINATED (NR 2) · airframe 11,759 hrs · 7,141 cycles

FLT 1282 RIC-BOS, FL 250 REPORTED ROW 22-24 SMELL OF POPCORN LIKE SCENT & REPORTED SLIGHT MIST IN AIR. TURNED OFF LTV APPEARED TO HAVE NO EFFECT SINCE CAPT WENT BACK TO ASSESS AREA. SMELL DISAPPEARED AFTER 10-15 SECS. INSPECTED AND FOUND NR 2 ACM TO HAVE RECENT COFFEE CONTAMINATION. REMOVED AND REPLACED NR 2 ACM PER MM 21-51-05. OPS LEAK AND SMELL CHECKS OK.

Part: RVDT — DIRTY (NLG STEERING) · airframe 10,704 hrs · 6,528 cycles

FLT 559 HPN - TPA ON TAKEOFF GOT STEER FAIL AT APPROX 70 KTS CONTINUED UPON EXTENSION STEER FAIL EICAS. FOLLOW QRH NO OTHER ISSUES. ACCOMPLISH FIM TASK 32-53-00-810-819A NO CORRELATED FAULT MESSAGE NOTED. REF LOG PAGE 679869 ITEM 1 STEER FAULT EICAS DURING PRE FLIGHT. POWERED DOWN A/C AND ACCOMPLISHED CLEANING OF RVTD 1 IAW ESP. OK FOR SERVICE.

Part: MODULE — FAILED (VHF COMM) · airframe 10,702 hrs · 6,527 cycles

FLT 596 MCO-HPN - FLT CREW DECLARED EMERGENCY INTERCOM FAILURE, EMER CALL TO CABIN WOULD OCCUR SPORADICALLY DURING FLIGHT CAUSING HOT MIKE/LOST COMMUNICATIONS ON BOTH RADIOS. RESEATING OXYGEN MASKS AND RE/DE SELECTING SPEAKERS AND OTHER TROUBLESHOOTING DID NOT HELP. REMOVED AND REPLACED VHF COM MODULE IAW 23-12-01 AND PACIC IAW 44-11-01. ALL RADIOS AND INTERPHONE COMM OPS NORMAL.

Part: PIN — CORRODED (BLEED AIR SYS) · airframe 10,090 hrs · 6,164 cycles

FLT JB111 BUF-JFK DURING TAKEOFF CLIMBOUT FROM BUF "BLEED 1 LEAK" EICAS MESSAGE ILLUMINATED, QRH COMPLETED, BLEED LEAK STILL ILLUMINATED. CREW DECLARED EMERGENCY AND RETURNED TO BUF AND LANDED SAFELY. BUF MX TROUBLESHOOTING PER AMM FIM 36-21-00-81-801-A FOUND CORRODED CERAMIC PIN ON CHANNEL 2 PYLON LOOP AT CONNECTOR J1045, CLEANED CONNECTOR AND REPLACED CERAMIC PIN IAW AMM 36-20-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (LE SLAT) · airframe 9,554 hrs · 5,852 cycles

FLT JB1422 - LGB-PDX CREW DECLARED EMERGENCY INBOUND TO PDX WITH A SLAT FAIL EICAS MESSAGE ON APPROACH. CREW ACCOMPLISHED QRH PROCEDURES WITH SLATS FAILED AT ZERO, AIRCRAFT LANDED WITHOUT INCIDENT. MX ACCOMPLISHED FIM 27-81-00-810-802A FOUND LT WING NR 7 SLAT ACTUATOR TRIPPED. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW AMM 27-81-01, ALSO FOUND SLAT TRACKS NR 4, 6, 7 AND 8 OUT OF RIG. ACCOMPLISHED MECHANICAL RIG IAW AMM 27-80-00-820-801A/200 ALSO ELECTRICAL RIG IAW AMM 27-80-00-820-802-A/200. ALL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (LE SLAT) · airframe 9,540 hrs · 5,842 cycles

FLT JB1403 - AUS-SFO 'SLAT FAIL' MESSAGE WHEN SELECTING FLAPS 1. FLIGHT CREW FOLLOWED QRH ,LANDED SLATS 0 AND FLAPS 2 WITHOUT INCIDENT. MX ACCOMPLISHED AMM FIM TASK 27-11-00-810-802A FAULT CONSIDERED TRANSIENT, CYCLED SLATS & FLAPS 2 TIMES NO FAULTS NOTED. A/C OK FOR SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 9,177 hrs · 5,639 cycles

FLT 1422 LGB-PDX - UPON FLAPS DEPLOYMENT, SLATS FAILED TO EXTEND AND RECEIVED SLAT FAIL EICAS MESSAGE. COMPLETED QRH AND SLATS REMAINED AT ZERO THROUGHOUT FIM 27-81-00-810-802A CLEARED INHIBITS C/W TESTS ALL FAULTS CLEARED. OPS TEST OF FLAP/SLAT AMM 27-80-00, ALL CHECKS GOOD. ALSO ACCOMPLISHED SLAT ACTUATOR INSPECTION CHECK OF RIGHT AND LEFT SIDE PER 27-81-01. ALL SLAT ACTUATORS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,882 hrs · 4,830 cycles

FLT 592, MCO-HPN, AIR RETURN TO MCO, F/A REPORTED SMELL OF ELEC SMOKE IN AFT GALLEY, SHUT OFF CABIN AND IFE POWER. PERFORMED FIM TASK 21-20-00-810-801-A. RAN BOTH ENGINES W/BLEED. RAN APU WITH BLEED. RAN PACK 1&2 ALTERNATELY TO ISOLATE. CHECKED FWD MID AND AFT AVIONICS COMPT, TURNED ON IFE SYS NO ELEC SMOKE SMELL NOTED. OPENED AND INSPECTED LTV EER. MONITORED SYSTEM FOR APPROX 2 HOURS, COULD NOT DUPLICATE DISCREPANCY. LTV COMPONENTS AND SYSTEM OPS CHECK/TEST NORMAL. REF M/M 44-20-10.

Part: BRAKE — MALFUNCTIONED (LE SLAT) · airframe 7,676 hrs · 4,712 cycles

SLAT FAIL ON APPROACH. PERFORMED QRH, LANDED WITH SLAT 0 AND FLAP 2. CREW DECLARED EMERGENCY. PERFORMED TSM TASK 27-81-00-810-807A, RESET THE SLAT BRAKE, SLAT OPS CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (SLAT/FLAP SYS) · airframe 7,560 hrs · 4,655 cycles

CREW RECEIVED SLAT FAIL MSG ON APPROACH AND COMPLETED QRH PROCEDURE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. T/S PER E190 FIM 27-00-00-810-802-A00, REMOVED AND REPLACED SLAT / FLAP CONTROL LEVER PER AMM 27-53-01, OPS CHECK OK. NO FAULTS AT THIS TIME.

Part: SLAT — MALFUNCTIONED (WING) · airframe 6,517 hrs · 4,073 cycles

CREW REPORTED SLATS FAIL ON APPROACH, DECLARED EMERGENCY, LANDED UNVENTFULLY. PERFORMED FIM TASK 27083-00-810-814-A AND FOUND NO FAULTS, NO MESSAGES PRESENT AT THIS MOMENT. OPERATIONAL CHECK IS OK.

Part: FITTING — CRACKED (RUDDER) · airframe 4,492 hrs · 2,947 cycles

FLT 1264, AUS-BOS, AIRCRAFT REQUIRES EXCESSIVE RIGHT YAW TRIM AT HIGH SPEED. NEEDED 1/3 TO 1/2 RIGHT TRIM FOR COORDINATED FLIGHT IN CRUISE. SEEMED TO TRIM BACK TO CENTER AT SLOW SPEED. ACFT IS CURRENTLY OUT OF SERVICE. REMOVED & REPLACED RUDDER PER EA E08-045 REVISION A PART 1, RUDDER RIGGING ACCOMPLISHED PER AMM 27-20-00, RUDDER BACKLASH PER AMM 27-20-00-720-801-A/500 AND OPERATIONAL TEST OF THE RUDDER CONTROL SYSTEM PER AMM 27-20-00-710-801-A/500. ACCOMPLISHED CHECK FLT. ALL OPS CHECK OK.

Part: ACTUATOR — FAILED (SLATS) · airframe 3,922 hrs · 2,620 cycles

SLAT FAIL ON APPROACH, TROUBLESHOOT OF SLAT FAIL/SLAT SYS FOUND SLAT ACTUATOR NR 5 AT SLAT TRACK NR 6, TORQUE LIMITER TRIP INDICATOR PLASTIC HOUSING BROKEN. REMOVED AND REPLACED NR 5 SLAT ACTUATOR AT SLAT TRACK NR 6 PER AMM 27-81-01-420-005-A. PERFORMED SLAT CTL SYSTEM RIGGING PER AMM 27-80-00-710-801. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 3,868 hrs · 2,593 cycles

UPON ARRIVAL/APPROACH INTO BUF SLAT FAILURE ILLUMINATED, QRC PROCEDURES FOLLOWED LANDED SLAT 0 FLAP 2. TROUBLESHOT PER FIM TASK 27-81-00-810-015A, BLOCKS 1-2 AND 9-11. TRIP INDICATORS RESET. OPS CHECK GOOD.

Part: CONTROLLER — UNKNOWN (CABIN PRESSURE) · airframe 1,915 hrs · 1,315 cycles

WHILE DESCENDING FROM FL370 TO FL350 A/T DISCONNECT OCCURRED. THIS WAS FOLLOWED IMMEDIATELY BY A RAPIDLY RISING CABIN ALTITUDE. MAX CABIN ALT REACHED 9400-9500 FT. INITIATED EMERGENCY DESCENT. PRESSURIZATION RETURNED TO NORMAL AT 10,000 FT LEVEL OFF. ACCOMPLISHED VISUAL CHECK OF PACK DUCTS & LEAK CHECK INCLUDING CHECK OF BELLOWS. PRESSURIZED A/C MANUALLY IAW CABIN PRESSURIZATION. FUNCTIONAL TEST AMM 21-31-720-802 STEP F1-G2. NO LEAKS NOTED. PERFORMED ENG 1 & ENG 2 ENGINE BLEED OPERATIONAL TEST IAW AMM 36-11-00-710-801-A ENG 1 & ENG 2 BLEED SYSTEMS OPS CHECK OK. AUTO THROTTLE SYSTEMS HZ, OPS CHECK OK IAW AMM 22-31-00-710. REMOVED AND REPLACED CPCS CONTROLLER PRECAUTIONARY PER AMM 21-31-01. FUNCTIONAL

Part: CONTROLLER — UNKNOWN (CABIN PRESSURE) · airframe 1,915 hrs · 1,315 cycles

WHILE DESCENDING FROM FL370 TO FL350 A/T DISCONNECT OCCURRED. THIS WAS FOLLOWED IMMEDIATELY BY A RAPIDLY RISING CABIN ALTITUDE. MAX CABIN ALT REACHED 9400-9500 FT. INITIATED EMERGENCY DESCENT. PRESSURIZATION RETURNED TO NORMAL AT 10,000 FT LEVEL OFF. ACCOMPLISHED VISUAL CHECK OF PACK DUCTS & LEAK CHECK INCLUDING CHECK OF BELLOWS. PRESSURIZED A/C MANUALLY IAW CABIN PRESSURIZATION. FUNCTIONAL TEST AMM 21-31-720-802 STEP F1-G2. NO LEAKS NOTED. PERFORMED ENG 1 & ENG 2 ENGINE BLEED OPERATIONAL TEST IAW AMM 36-11-00-710-801-A ENG 1 & ENG 2 BLEED SYSTEMS OPS CHECK OK. AUTO THROTTLE SYSTEMS HZ, OPS CHECK OK IAW AMM 22-31-00-710. REMOVED AND REPLACED CPCS CONTROLLER PRECAUTIONARY PER AMM 21-31-01. FUNCTIONAL