N179JB

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 43,726 hrs · 28,598 cycles

DURING HEAVY MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE ABOVE ROW 20 & 21. EMERGENCY LIGHT POWER SUPPLY NR 6 WAS REMOVED AND REPLACED IAW AMM 35-50-01. SATISFACTORY TEST.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 43,726 hrs · 28,598 cycles

DURING EMERGENCY LIGHTS CHECK, LT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. THE POWER SUPPLY NR 5 WAS REMOVED AND REPLACED IAW FIM 33-50-00-810-816-A, AND AMM 35-50-01. SATISFACTORY TEST.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 43,726 hrs · 28,598 cycles

DURING HEAVY MAINTENANCE, INOPERATIVE EXTERNAL EMERGENCY LIGHT, RT AFT, AND EMERGGENCY LIGHT IN THE CABIN. POWER SUPPLY NR 6 WAS REPLACED IAW AMM 33-50-01-000-801-A, AND AMM 33-50-01-400-801-A. OPS TESTED GOOD.

Part: LIGHT — INOPERATIVE · airframe 43,111 hrs · 28,144 cycles

FLT#1967, HPN-PBI. ' PHOTO LUMINESCENT ESCAPE ROUTE MARKING AT 6B MISSING AN AISLE WAY ( PHOTOLUMINESCENT ESCAPE PATH LIGHT- 10%); INSTALLED NEW FLOOR LIGHTING STRIP PER AMM 33-50-00. MDDR 482052 AND MEL 33-50-21A CLEARED. MX-4 UPDATED. PLACARD REMOVED.'

Part: WINDOW FRAME — DENTED · airframe 43,058 hrs · 28,105 cycles

FLT#1865, BOS-RSW. 'BIRDSTRIKE AT1500-185KTS HIT BELOW WINDSCREEN AND LEFT A LARGE DENT; ACCOMPLISHED BIRD STRIKE INSP IAW AMM 05-50-02 NO ENGINE INGESTION FOUND. SEE L/P 3453408 ITEM 1 (REPAIRS ACCOMPLISHED UNDER JETBLUE WO#1191170 AND EAMS-MCN WO#H8723.) & 2(REPAIRS ACCOMPLISHED UNDER JETBLUE WO#1191170 AND EAMS-MCN WO#H8723.) FOR DAMAGE FOUND.'

Part: LIGHT — FAILED (EMER-BATT-CTR-RH) · airframe 42,690 hrs · 27,837 cycles

FLT#955, BOS-DCA. 'AFT RH EXTERIOR EMERGENCY LIGHT INOP; REMOVED AND REPLACED #6 ELPU IAW AMM 33-50-01. OPS CHECKS GOOD, A/C OK FOR CONTINUED SERVICE AT THIS TIME.'

Part: TRANSMITTER — FAILED (WX-REC-TRA) · airframe 41,407 hrs · 27,021 cycles

FLT 657, CLE-FLL(DIVERTED TO MCO).FAULTY WX RADAR RETURNS RADAR FAIL; REMOVD + REPLACED WX RADAR /TRASMITTER IAW MM 34-42-01 TEST NORMAL REF MM 34-42-00 OK FOR SVC

Part: SENSOR — FAULTED (MLG WOW) · airframe 40,278 hrs · 26,280 cycles

FLT 917, BOS-JFK. A/C DECLARED AN EMERGENCY FOR A WOW SYSTEM FAULT. OPEN.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, CRACK FLOOR STRUCTURE FR48-49LH PASSENGER CABIN; REF AEROMAN NR 150542: ACCOMPLISHED REPAIR OF CRACK ON LONGITUDINAL FLOOR BEAM FR49 & Y782LH IAW AEROMAN EA 53-0384-20 & ETD 2020-190-015805.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, INOP CEILING PANEL 254CRC ELPU; (REF AEROMAN NR 150674 WO 2020 162/1) R & R CEILING PANEL 254CRC ELPU OPS OK

Part: SKIN PANEL — CRACKED (LT WING) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL WING MAIN BOX AFT EDGE AT LEVEL RIB 10 LH WING; (REF AEROMAN NR 150395) PERFORMED PERMANENT REPAIR IAW SRM 57-10-01 REPAIR 59. INTELLIFORM UPDATED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, EMERGENCY LIGHT 243QLC INOPERATIVE; REF AEROMAN NR 150432: REMOVED AND REPLACED ELPU6 IAW AMM 33-50-01-400-801-A STEP 3.G THROUGH 3.H. OPS CHECKS GOOD.

Part: RIB — CRACKED (RT WING) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, CRACK LE RIB 17 RH WING; REF AEROMAN NR 150421 WO 2020 162/1 R &R LE RIB 17 RH WING IAW E190 SRM 51-40-08 & DRAWING 191-03201-433

Part: BEAM — CRACKED (FUSELAGE) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, TWO CRACKS WERE FOUND ON THE CENTER FUSELAGE II MIDDLE FLOOR STRUCTURE LH LONGITUDINAL BEAM P/N 190-22016-403 AT FR 49 AND AT Y782 (LH). THE E-190 SRM II 53-22-10 DOES NOT PROVIDE ALLOWABLE DAMAGE LIMITS OR REPAIR INSTRUCTIONS FOR THIS DAMAGE. AEROMAN CONTACTED EMBRAER FOR REPAIR DISPOSITION, WHICH PROVIDED THE REF.(2) ETD REPAIR, CONSISTED OF REMOVING THE DAMAGE COMPLETELY BY A TRIMMING OUT, FABRICATING AND INSTALLING A REPAIR DOUBLER TO MATCH THE CONTOUR THE LONGITUDINAL BEAM WITH FILLER AND RESTORING THE ORIGINAL FINISHING ON THE REPAIR AREA. AEROMAN HAS ISSUED THE REF.(1) EA ACCOMPLISHING THE REPAIR, AND THIS EC INCORPORATES THIS EA WITHOUT DEVIATION; THIS REPAIR HAS BEEN APPROVED BY THE REF.(2) EMBRAER ETD AND ANAC APPROVAL. THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY ""A"" PERMANENT REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,399 hrs · 25,543 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE PROFILE WEB BTW FR12 AND FR16 LH SIDE AT FWD GALLEY AREA; (RESOLVED ON W/O: 1032226 TASKCARD: NR-00001 ) ACCOMPLISHED REPAIR TOFWD FUSELAGE LH SILL FLOOR BETWEEN FR12 TO FR16 IAW EC E20-468-01

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 38,114 hrs · 24,696 cycles

FT # 1890, DCA-BOS. AFT SERVICE DOOR EMERGENCY EXIT LIGHT AND COURTESY LIGHT INOP; REPLACED EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECK GOOD.

Part: BEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 32,606 hrs · 20,807 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON A REPAIR ON THE TOP FLANGE OF A BEAM AT FRAME 17. REPAIRED IAW EC E17-1087-01.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 31,792 hrs · 20,181 cycles

EMERGENCY DECLARED. RECEIVED A FLAP FAIL MESSAGE ON SHORT FINAL WHEN WE SELECTED GEAR DOWN, FLAPS 3. THE FLAPS STUCK AT 2. RAN THE QRH FOR FLAP FAIL AND LANDED UNEVENTFULLY. R & R THE LT & RT NR 2 FLAP ACTUATORS IAW AMM 27-51-01. OPS CHECKED NORMAL. ALL FAULTS CLEARED. FIM 27-51-00-810-802-A. ACFT OK TO RETURN TO SERVICE.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 31,792 hrs · 20,181 cycles

EMERGENCY DECLARED. RECEIVED A FLAP FAIL MESSAGE ON SHORT FINAL SELECTED GEAR DOWN, FLAPS 3. THE FLAPS STUCK AT 2. RAN THE QRH FOR FLAP FAIL AND LANDED UNEVENTFULLY. R & R THE LT & RT NR 2 FLAP ACTUATOR IAW AMM 27-51-01. OPS CHECKED NORMAL. ALL FAULTS CLEARED. FIM 27-51-00-810-802-A. ACFT OK TO RETURN TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 27,825 hrs · 17,412 cycles

AT CRUISE INTERMITTENT, HYD 2 HI TEMP, SYNOPTIC PAGE CONFIRMED INTERMITTENT SPIKES INTO THE AMBER TEMP RANGE. SHORTLY THEREAFTER INTERMITTENT, HYD 2 OVERHEAT, EICAS. HYD SYNOPTIC PAGE AGAIN CONFIRMED SPIKES INTO THE RED TEMP RANGE. QRH PROCEDURES FOLLOWED AND BOTH HYD VALVES CLOSED PROPERLY. NO OTHER MALFUNCTIONS NOTED. HYD QUANTITIES AND PRESSURE WERE STEADY AND WITHIN NORMAL RANGES; FOUND NUMEROUS HITS IN AHEAD FOR NR 2 ENGINE PUMP LOW PRESS. R & R NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-01. OPS CHECKS, LEAK CHECKS GOOD. REFER TO ITEM 1816045, ITEM 1 FOR FILTER CHANGE AND MAB 29-01-16-003 COMPLIANCE.

Part: BYPASS VALVE — FAILED (HYD SYSTEM) · airframe 26,836 hrs · 16,768 cycles

FLIGHT DIVERTED, HYD 2 OVERHEAT INFLIGHT. COMPLIED WITH QRH; ACCOMPLISHED FIM TASK 29-11-00-810-808A. R & R NR 2 SYS HEAT EXCHANGER THERMAL BYPASS VALVE AND ACCOMPLISHED SATISFACTORY CHECKOUT FOR CONTINUED SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND SHEAR TIE AT FR 87 BETWEEN STR 27R & 28R CORRODED. REMOVED SHEAR TIE AT FR 87 BETWEEN STS 27R & 28R REF EMB 190, SRM 51-41-01;51-41-02. LOCATED AND DRILLED HOLES IN NEW SHEAR TIE REF SRM 51-41-01;51-41-02. APPLIED ALODINE TO HOLES IN NEW SHEAR TIE REF SRM 51-23-04. INSTALLED SHEAR TIE REF SRM 51-41-01; 51-41-02. PRIMED AND TOPCOATED REF SRM 51-23-05:51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: ANGLE — CORRODED (FRAME 86) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND AFT DRAIN MAST INTERNAL FWD & AFT ANGLE BRACKETS ARE CORRODED. REMOVED CORRODED AFT DRAIN MAST FWD & AFT ANGLE BRACKETS REF SRM 51-41-01;51-41-02. DAMAGE LENGTH 3", WIDTH 0.4" AND DEPTH 0.009". LOCATED AND DRILLED NEW PARTS REF SRM 51-40-02. INSTALLED NEW AFT DRAIN MAST INTERNAL FWD & AFT ANGLE BRACKETS REF SRM 51-41-01: 51-41-02. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: ANGLE — CORRODED (FRAME 87) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND AFT DRAIN MAST FWD & AFT ANGLE BRACKETS ARE CORRODED. REMOVED CORRODED AFT DRAIN MAST FWD & AFT ANGLE BRACKETS REF SRM 51-41-01; 51-41-02. DAMAGE LENGTH 3", WIDTH 0.4" AND DEPTH0.009". LOCATED AND DRILLED NEW PARTS REF SRM 51-40-02. INSTALLED NEW AFT DRAIN MAST INTERNAL FWD &AFT ANGLE BRACKETS REF SRM 51-41-01:51-41-02. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2, CORROSION.

Part: STRUCTURE — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND RT FLOOR SPLICE CORRODED FRAMES 18-19; RBL 12.5-RBL 29.5. REMOVED CORROSION, MAX MATERIAL LOSS IS L=3", W=3.5", H= 0.002". LOCATION IS 1.5" AFT OF FRAME 18, RBL 24" REF SRM 51-10-03;51-12-01. TREATED, PRIMED AND TOP COATED REF SRM 51-23-04; 51-23-05;51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SEAT TRACK — CORRODED (FRAMES 12-21) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND LT SEAT TRACK CORRODED FRAMES 12-21; LBL 9.5-12.5. REMOVED CORROSION, MAX MATERIAL LOSS AREA A IS 1" AFT OF FR 16, LBL 11.5 L=1.047, W= 1.71, H= 0.025, AREA B LOCATION IS 1" AFT OF FR 17, LBL 10.5, L= 2.14, W= 0.927, H= 0.015. REF SRM 51-12-01. TREATED; PRIMED AND TOP COATED REF SRM 51-23-04; 51-23-05;51-23-06.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND AFT CABIN-RT SHEAR CLIP FRAME 87-FRAME 88, RBL 12"-RBL 41.5" CORRODED. REMOVED 21 EA, CHERRY MAX RIVETS TO REMOVE CORROSION REF SRM 51-40-02. REMOVED CORROSION, MAX MATERIAL LOSS L=2.0, W=1.75, H=0.002, LOCATION 4.5" AFT OF FRAME 87, RBL 23, REF SRM 51-10-03, TYPE D BLEND OUT. REF 51-12-01, INSTALLED 2 RIVETS, TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-42-01, 51-23-04, 51-23-05, 51-23-06. NOMINAL THICKNESS IS 0.063. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND FWD OF CARGO BAY SHEAR TIE CORRODED AT FRAME 16 BETWEEN STR 28-29R. R & R SHEAR TIE IAW SRM 51-41-01, 51-41-02.

Part: DOOR SILL — CORRODED (FRAMES 87) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND AFT PAX DOOR SILL HAS MULTIPLE AREAS OF CORROSION. R & R AFT PAX DOOR BEAM REF SRM 51-40-02, 51-23-04.

Part: DOUBLER — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND FWD LT FLOOR DOUBLER CORRODED FRAMES 13-16, LBL 14-36. REMOVED CORRODED FWD FUSELAGE NINE HOLE FLOOR DOUBLER REF SRM 51-41-02. LOCATED AND DRILLED HOLES IN NEW FLOOR DOUBLER REF SRM 51-41-02. INSTALLED NEW FLOOR DOUBLER REF SRM 51-41-02. PRIMED AND TOPCOATED REF SRM 51-23-05:51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SEAT TRACK — CORRODED (FRAMES 12-21) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND RT SEAT TRACK CORRODEDFRAME 12 TO FRAME 21; RBL 9.5"-RBL 12.5". REMOVED CORROSION BY BLENDOUT REF SRM 51-10-03; 51-21-01. FOUND TO BE OUT OF LIMITS REF SRM 53-10-10, MATERIAL LOSS 0.062". REMOVED SEAT TRACK REF. SRM 51-41-01;51-41-02. LOCATED; DRILLED AND TREATED NEW BEAM REF SRM 51-23-04; 51-40-01. INSTALLED SEAT TRACK AND TOP COATED REF SRM 51-41-01;51-41-02; 51-43-03;51-43-04. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND FWD OF CARGO BAY SHEAR TIE CORRODED AT FRAME 17 STR BETWEEN 28- 29R. R & R THE SHEAR TIE IAW SRM 51-41-01, 51-41-02.

Part: FINGER DOUBLER — CORRODED (FRAMES 77-78) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND CORROSION-AFT CARGO DOOR-HORIZONTAL BEAM FINGER DOUBLER HAS CORROSION ON TOP CENTER AREA. REMOVED AFT CARGO DOOR HORIZONTAL BEAM FWD FINGER DOUBLER REF SRM 51-43-04, DAMAGE LENGTH 1.5"; WIDTH 0.4"; DEPTH 0.025". LOCATED AND DRILLED NEW FINGER DOUBLER REF SRM 51-40-02. INSTALLED NEW FINGER DOUBLER REF SRM 51-43-03, 51-43-04; APPLIED TOPCOAT TO FASTENERS REF SRM 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION

Part: DOOR SILL — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND AFT SERVICE DOOR SILL CORRODED. REMOVED CORROSION BY BLENDING AND SPOT FACING, PERFORMED HFEC INSPECTION. TREATED, PRIMED AND TOPCOATED REPAIRED AREA.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND SHEAR TIE AT FRAME 76, STRINGER 29R CORRODED, R & R SHEAR TIE AT FRAME 76, STR 29R, REF SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND CENTER SHEAR TIE FRAMES 87-88; LBL 9.5"-RBL 9.5"-CORRODED. REMOVED 3 EA TEMP RIVETS TO REMOVE CORROSION REF SRM 51-42-01. REMOVED CORROSION, MAX MATERIAL LOSS AREA B L=1.5, W=1.5, H=0.002, LOCATION 3" AFT OF FRAME 87, LBL 4.5. NOMINAL THICKNESS IS 0.063. TYPE D, BLEND OUT REF 51-12-01. INSTALLED 3 RIVETS, TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-23-04, 51-23-05, 51-23-06.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND CORROSION BELOW FWD PAX DOOR FWD AND AFT GIRT BAR FLOOR FITTINGS FRAME 16 TO FRAME 19, STR 18L, LBL 49 , REMOVED 12 FASTENERS, REMOVED CORROSION, AT FWD AND AFT SLIDE FITTING MOUNT SURFACES, HFEC BLENDED AREAS INSTALLED FASTENERS, ALODINED, PRIMED AND PAINTED BLENDED AREAS AND FASTENERS. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 82) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND SHEAR TIE FRAME 82 BETWEEN STR 27-28R CORRODED. R & R THE SHEAR TIE IAW SRM 51-41-01, 51-41-02.

Part: DOUBLER — CORRODED (LT FLOOR) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND FWD LT FLOOR DOUBLER CORRODED FRAMES 13- 16, INSTALLED NEW FLOOR DOUBLER SRM 51-41-02. PRIMED AND TOPCOAT SRM 51-23-05, 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND FLOORBEAM UPPER CAP CORRODED AS MARKED FRAME 17 RBL 12.5, RBL 41, REMOVED CORROSION, CUTOUT DAMAGE DEEPER THAN 20 PERCENT. PERFORMED DYE PENETRANT INSPECTION, NO DEFECTS NOTED. MANUFACTURED LT REPAIR WITH FILLERS, LOCATED DRILLED AND TREATED REPAIR. APPLIED SEALER AND TOPCOATED REPAIR. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-90) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND LT PANEL SUPPORT FRAME 87- FRAME 90, LBL 42"-LBL 44" CORRODED. REMOVED 1 EA TEMP RIVET TO REMOVE CORROSION REF SRM 51-42-01. REMOVED CORROSION, MAX MATERIAL LOSS L=1.5, W=1, H=0.002, LOCATION 2" AFT OF FRAME 88, LBL 40. MATERIAL LOSS IS WITHIN ALLOWABLE LIMITS REF SRM 51-10-03, TYPE D BLEND OUT, REF 51-12-01. INSTALLED 1 RIVET, TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-23-04, 51-23-05, 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND FWD CARGO BAY SHEAR TIE CORRODED AT FRAME 16 BETWEEN STRINGERS 27-28R. R & R THE SHEAR TIE IAW SRM 51-41-01, 51-41-02.

Part: SHEAR ANGLE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND CENTER SHEAR FRAMES 87-88, LBL 9.5-RBL 9.5. REMOVED 3 EA TEMP RIVETS TO REMOVE CORROSION REF SRM 51-42-01. REMOVED CORROSION, MAX MATERIAL LOSS ARE: AREA A L=1.75, W=2.0, H= 0.002, LOCATION IS 3" AFT OF FRAME 87, LBL 2.5. NOMINAL THICKNESS IS 0.063. REF SRM 51-10-03, TYPE D BLEND OUT REF 51-12-01. INSTALLED 3 RIVETS, TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-23-04, 51-23-05; 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND RT FLOOR SUPPORT IS CORRODED FROM FRAME 12-FRAME 14, RBL 36-49. REMOVED CORROSION, MAX MATERIAL LOSSES ARE: AREA A L=1.75, W=11.5, H= 0.002, LOCATION IS AT FRAME 14, RBL 38-49. REF SRM 51-10-03, TYPE D, BLEND OUT REF 51-12-01, 51-23-02. TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-23-04, 51-23-05, 51-23-06.

Part: SKIN — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND INTERNAL SKIN BET FRAMES 75 - 76, STRINGERS 29L, 29R CORRODED. BLENDED CORROSION IAW SRM 51-10-03 TREAT, PRIME TOPCOAT SRM 51-23-04, 51-23-05, 51-23-06.

Part: DOOR SILL — CORRODED (FRAMES 19-21) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND LT DOOR SIL CORRODED FRAMES 19-21; LBL 44"-LBL 49". REMOVED CORROSION, MAX MATERIAL LOSS IS L=3.5, W= 4, H= 0.002. LOCATION IS 2" AFT OF FRAME 19, LBL 45-49", REF SRM 51-10-03, 51-12-01. TREATED, PRIMED AND TOP COATED REF. SRM 51-23-04; 51-23-05; 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND RT FLOOR SUPPORT CORRODED FR 19-20 RBL 12"-RBL 16". R & R OUT OF LIMITS PART WITH NEW IAW SRM 51-41-02;51-43-03. TOP COATED REF SRM 51-23-06.

Part: SHEAR TIE — CORRODED (FRAME 83) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND SHEAR TIE AT FR 83 BETWEEN STR RIGHT SIDE 27R & 28R IS CORRODED. REMOVED SHEAR TIE AT FR 83 BETWEEN STG 27R & 28R REF SRM 51-41-01; 51-41-02. LOCATED AND DRILLED HOLES IN NEW SHEAR TIE REF EMB 190, SRM 51-41-01;51-41-02. APPLIED ALODINE TO HOLES IN NEW SHEAR TIE REF SRM 51-23-04. INSTALLED SHEAR TIE REF SRM 51-41-01;51-41-02. PRIMED AND TOPCOATED REF SRM 51-23-05:51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE FOUND SHEAR CLIP AT FRAME 76 BETWEEN STR 28R, 29R, CORROSION, R & R SHEAR CLIP AT FRAME 76 BET STR 28R, 29R, REF SRM 51-41-01, 51-41-02. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND RT FLOOR SIL HAS CORROSION AS MARKED FROM FRAME 14, RBL 38". REMOVED CORROSION, MAXIMUM MATERIAL LOSSES ARE: AREA B, L=2.5, W=1.5, H=0.002, LOCATION 6" FWD OF FRAME 14, RBL 38. REF SRM 51-10-03, TYPE D, BLEND OUT REF 51-12-01, 51-23-02. TREATED, PRIMED AND TOP COATED AREAS REF SRM 51-23-04, 51-23-05, 51-23-06. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.

Part: SKIN — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 25,842 hrs · 16,084 cycles

DURING HEAVY MAINTENANCE, FOUND FWD CARGO BAY FUSELAGE SKIN CORRODED BETWEEN FRAME 15R AND 16R STR 29R AND 26R. REMOVED CORROSION, ACCOMPLISHED HFEC WITH NO DEFECTS NOTED, FABRICATED AND INSTALLED DOUBLER AND TRIPLER, TREATED AND TOPCOATED AFFECTED AREA.

Part: PUMP — CRACKED (HYDRAULIC SYS) · airframe 20,451 hrs · 12,564 cycles

FLT 39 ROC-JFK, CREW DECLARED AN EMERGENCY INTO JFK. DURING CLIMBOUT HYD EDP FAIL MESSAGE POSTS FOLLOWED BY HYD 2 LO PRESS. CREW PERFORMED QRH FOR BOTH MESSAGES. ALSO HAD HYD 2 LO QTY WITH 0 INDICATION ON THE HYD PAGE. WITH HYD 2 ELEC PUMP ON WE MAINTAINED 2700 PSI IN SYS 2. NORMAL LANDING WITH NORMAL LG EXTENSION. REMOVED AND REPLACED NR 2 ENG HYD EDP PER AMM 29-11-01. OPS AND LEAK CHECKS GOOD.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 16,208 hrs · 9,954 cycles

FLT 583 HPN-FLL, AIRCRAFT DIVERTED TO JFK DUE TO FUEL FEED FAULT AFTER TAKEOFF. ENG 1 MESSAGE APPEARED. RAN CHECKLIST MSG WENT AWAY FOR ABOUT 1 MIN THEN RE-APPEARED. ENG 1 FUEL LOW PRESSURE MSG APPEARED. ALL ENG PARAMETERS APPEARED NORMAL. REPLACED NR 1 ENG LOW FUEL PRESSURE SWITCH PER ESM 71-00-73 AND ACCOMPLISHED ENGINE FEED EJECTOR PUMP OPS CHECK PER AMM 28-21-13. OPS OK, ACFT OK FOR SVC.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,869 hrs · 8,009 cycles

FLT 1262 IAD-BOS, ON GROUND MAINTENANCE CHECK FOUND INTERIOR OVERWING CEILING EMERGENCY EXIT LOCATOR LIGHT AFT SIDE INOP AT ROW 11. REMOVED AND REPLACED BATTERY PACK ASSY IAW 33-50-01. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (RT WING) · airframe 12,373 hrs · 7,689 cycles

FLT 588 PBI-HPN, A/C DIVERTED TO MCO DUE TO A-I WING FAIL EICAS MESSAGE IN FLIGHT. CREW WAS UNABLE TO CLEAR THE MESSAGE WITH QRH PROCEDURE. PERFORMED FIM 30-11-00-810-809-A AND REMOVED AND REPLACED RT WING ANTI ICE VALVE PER AMM 30-11-01. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,562 hrs · 7,201 cycles

FLT 1068 AUS-JFK ON GROUND DURING MAINTENANCE CHECK FWD O/W EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD OVERWING EMERGENCY LIGHT IAW E190 AMM 33-40-00. OPS CHECK GOOD.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 11,015 hrs · 6,879 cycles

FLT JB992 MCO-JFK DECLARED EMERGENCY AND RETURNED TO MCO DUE TO NR 1 ENGINE LOW OIL QUANTITY. MX INSPECTED NR 1 ENGINE FOUND NO EVIDENCE OF OIL LEAKAGE. SERVICED NR 1 ENGINE WITH 7 QUARTS OF OIL IAW AMM 12-13-01. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — FUMES (COCKPIT & CABIN) · airframe 10,255 hrs · 6,442 cycles

FLT 63 JFK-JFK - FUMES IN THE COCKPIT AND CABIN. PERFORMED SMOKE AND ABNORMAL IAW AMM 21-20-00-810-801-A RAN BOTH ENG AND APU NO DEFECT NOTED.

Part: FADEC — FAILED (NR 2) · airframe 10,015 hrs · 6,308 cycles

FLT 1079 JFK-RIC - WHILE IN LEVEL FLIGHT AT 250 KIAS, AUTOTHROTTLE DISCONNECTED DUE TO NR 2 ENGINE ROLLING BACK TOWARD IDLE, F/O (PF) ADVANCED THRUST LEVERS TO REGAIN AIRSPEED NR 2 INITIALLY CONTINUED TO ROLLBACK THEN ADVANCED AND SEEMED TO OPERATE NORMALLY AIRSPEED INCREASED TO ABOUT 230 KIAS ONCE NR 2 CAME BACK. CMC SHOWED AT SPLIT MSG 22310078TA2. PERFORMED FIM TASK 22-31-00-810-922-A. NO FAULTS FOUND. PERFORMED TASK OF THE TCQ LEVERS PER THE AMM 22-31-00-710-801-A/500, AUTO TEST NORMAL. PER MCC /ENGINEERING TSI ISSUED REPLACED FADEC NR 2. REMOVED AND REPLACED FADEC NR 2 PER TSI 2159 AMM 73-00-00. PERFORMED OPS CHECK PER AMM 72-00-00. ALL CHECKS NORMAL.

Part: POWER UNIT — FAILED (CABIN) · airframe 9,999 hrs · 6,296 cycles

ON PRE FLT TEST OF EMERG LIGHTS, MULTIPLE LIGHTS INOP. EMERG LIGHT BATT FAULT EICAS MSG. T/S PER FIM TASK 33-50-00-810-801-A, VISUALLY INSPECTED FWD ELPU. FOUND LT FWD ELPU NOT CHARGING, RESEATED CONNECTOR, UNIT RESET. REMOVED AND REPLACED LT FWD ELPU AS PER AMM MPP 33-50-01. OPS CHECK OK.

Part: SEAL — LEAKING (ATTENUATOR) · airframe 5,293 hrs · 3,612 cycles

FLT NR 1218, BUF-BOS, LOSS OF HYDRAULIC SYSTEM 2, FOUND NR 2 ENG EDP PRESS ATTENUATOR LEAKING, REMOVED AND REPLACED ATTENUATOR FOR NR 2 EDP PER AMM 29-11-27. PERFORMED ENGINE DRIVEN PUMP INSPECTION/CHECK PER AMM 05-50-23. PERFORMED NR 2 HYD SYS PRESSURE/RETURN/CASE DRAIN FILTER INSP/REPLACEMENT PER AMM 29-11-05, NO CONTAMINATION OR DEBRIS FOUND. LEAK CHECKS OK, PERFORMED EDP OPS TEST PER AMM 29-10-00, LEAK AND PRESS CHECK OK. PERFORMED LANDING GEAR FREE FALL CONDITION INSP/CHECK PER AMM 05-50-14 DUE TO LOSS SYS 2 HYD PRESS, ALTERNATE LANDING GEAR EXTENSION SYSTEM WAS UTILIZED.

Part: SEAL — LEAKING (ATTENUATOR) · airframe 5,293 hrs · 3,612 cycles

FLT NR 1218, BUF-BOS, LOSS OF HYDRAULIC SYSTEM 2, FOUND NR 2 ENG EDP PRESS ATTENUATOR LEAKING. REMOVED AND REPLACED ATTENUATOR FOR NR 2 EDP PER AMM 29-11-27. PERFORMED ENGINE DRIVEN PUMP INSPECTION/CHECK PER AMM 05-50-23. PERFORMED NR 2 HYD SYS PRESSURE/RETURN/CASE DRAIN FILTER INSP/REPLACEMENT PER AMM 29-11-05, NO CONTAMINATION OR DEBRIS FOUND. LEAK CHECKS OK. PERFORMED EDP OPS TEST PER AMM 29-10-00, LEAK AND PRESS CHECK OK. PERFORMED LANDING GEAR FREE FALL CONDITION INSP/CHECK PER AMM 05-50-14 DUE TO LOSS SYS 2 HYD PRESS, ALTERNATE LANDING GEAR EXTENSION SYSTEM WAS UTILIZED.

Part: PROCESSOR — UNKNOWN (CONTROLLER) · airframe 3,919 hrs · 2,731 cycles

INFLIGHT AT FL380 APU WAS OFF, GOT CAUTION -BLEED APU LEAK-. WOULDN'T CLEAR FOLLOWED QRH. BLEED 1 OFF X BLEED OPEN. CLEARED THE AMBER LINE ON THE ECS PAGE. DECLARED EMERGENCY. T/S PER FIM 36-22-00. REPLACED BOTH AMS CONTROLLER PROCESSOR MODULES, PER MM 21-00-01. OPS CHECK OK, NO FURTHER MESSAGES. OK FOR SERVICE.

Part: ACM — FAILED (NR 2) · airframe 3,848 hrs · 2,698 cycles

FLT 1057, JFK-PIT, APPROX 0230-0300Z BURNING ODOR DURING APPROACH. LIGHT SMOKE REPORTED IN CABIN BY FLIGHT ATTENDANT ON LANDING ROLL METAL SHAVING CAME OUT OF AIR VENTS TOWARD REAR OF AIRCRAFT FOLLOWED BY PACK 2 FAIL EICAS MESSAGE. VERIFIED PACK NR 2 FAILED. REMOVED AND REPLACED NR 2 ACM IAW AMM 21-51-05. ALL CHECKS GOOD AT THIS TIME.

Part: PACKING — CUT (NLG STRUT) · airframe 1,883 hrs · 1,356 cycles

LANDING GEAR WOULD NOT RETRACT. FOUND NLG STRUT BOTTOM CHAMBER SHRADER VALVE PACKING CUT AND NO AIR IN THE STRUT. REPLACED PACKING AND SERVICED NLG STRUT IAW AMM 12-12-09 AND GREASED NLG AND SCISSOR LINKS. CYCLED GEARS SEVERAL TIMES IAW 32-33-00-501. FUNCTION CHECK AND OPERATION CHECK OK.

Part: CONNECTOR — DIRTY (BRAKES) · airframe 367 hrs · 301 cycles

ON TAKEOFF BELOW 40 KTS RECEIVED AURAL NO TAKEOFF BRAKE WARNING. NO EICAS MESSAGES, BRAKE HANDLE WAS OFF, PARKING BRAKE LIGHT WAS OFF. OP CHECKED PRESSURE SWITCHES IAW 32-44-09 CHECKED INTEGRITY OF SWITCHES WITH BRAKE ON AND OFF BY USING OHM METER. SWITCHES CHECKED GOOD IN BOTH POSITIONS. CLEANED CONNECTORS AND CHECKED SWITCHES FOR BENT OR DEFORMED PINS. ALSO NO LEAKAGE FOUND AT SWITCHES. OP CHECKED PARKING BRAKE IAW 32-44-09 OPS NORMAL.

Part: PRESSURE SWITCH — LEAKING (EMERGENCY BRAKE)

REJECTED TAKEOFF AT 60 KTS FW T/O CONFIG WARNING. NO TAKEOFF BRAKES, FOUND NR 1 SYS EMERGENCY BRAKE PRESS BAD. REPLACED PER AMM 32-44-09-000-801-A & 32-44-09-801-A. ADJ & TEST PER AMM 32-44-09-720-801-A, INSP OF FUEL QUANTITY IND HARNESS REQUIRED - A CDCCL ITEM.