N296JB

Part: ACOUSTIC LINER — MISREPAIRED (ENGINE 1) · airframe 36,663 hrs · 23,950 cycles

ENGINE #1, UPPER AND LOWER INNER BARREL SKIN (ACUSTIC PANELS) WITH EXISTING DENTS REPAIR AND REPAIR DOUBLER WITH MISSING RECORDS. NOTE: THE O.E.M. (COLLINS AEROSPACE) INSTRUCTIONS AS FOLLOW: "DUE TO THE SIZE OF THE CUTOUT, THE EXISTING FASTENER HOLES, AND THE HONEYCOMB BEING POTTED, COLLINS AEROSPACE CANNOT PROVIDE A REPAIR FOR THIS DAMAGE, AND THE DAMAGED COMPONENT REQUIRES REPLACEMENT OR REBUILD/OVERHAUL TO SATISFY DURABILITY / STRENGTH / REPARABILITY REQUIREMENTS SET FORTH BY EASA/FAA ". ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 NON RUTINE ITEM: 21-103 ).

Part: SKIN PANEL — BURNED (ZONE 200) · airframe 36,663 hrs · 23,950 cycles

FORWARD FUSELAGE, FR06, STRINGER 24RH+40MM, EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030843 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER COO-EO-2023-18932-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM: 21-85 ).

Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

FORWARD FUSELAGE, FROM FR04+165MM TO FR05+170MM, BETWEEN STRINGER 23RH+45MM AND STRINGER 25RH+95MM, EXTERNAL SKIN WITH EXISTING REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-029872 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023- 18861-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEMS : 21-84 ).

Part: SKIN PANEL — BURNED (ZONE 200) · airframe 36,663 hrs · 23,950 cycles

FORWARD FUSELAGE, AT X=2743.5 STRINGER 15RH+120MM, AT FR10 STRINGER 17RH, AND AT FR11+260MM STRINGER 17RH EXTERNAL SKIN WITH LIGHTNING STRIKES. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030848 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023- 18934-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEMS : 21-81, 21-82 AND 21-83 ).

Part: FITTING — NICKED (ZONE 500) · airframe 36,663 hrs · 23,950 cycles

LH WING, EXTERNAL SIDE AT MAIN LANDING GEAR, RIB 5 AND BACKUP FITTING TO SPAR 2 ATTACHMENT, LOWER ATTACHMENT HOLE "C" WITH NICKS, SCRATCHES AND GOUGES IN INTERNAL BORE. NOTE: FITTING HOLE WAS REPAIRED AS PER EMBRAER ETD2023-190-030541 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-19010-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 NON RUTINE ITEM: 5-8 ).

Part: SKIN PANEL — MISREPAIRED (ZONE 200) · airframe 36,663 hrs · 23,950 cycles

PER CUSTOMER REQUEST REPLACE THE FASTENER INSTALLED ON CENTER FUSELAGE I, FR26+94MM, STRINGER 11RH+105MM, EXTERNAL SKIN WITH THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2018-190-086940 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18985-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-74 ).

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 36,663 hrs · 23,950 cycles

RH WING, MAIN BOX T/E LOWER SKIN, AT RIB 10 WITH EXISTING REPAIR WITHOUT RECORDS. NOTE: THE RH WING, LOWER SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-031227 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18978-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM: 21-112 ).

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 36,663 hrs · 23,950 cycles

LH WING, MAIN BOX T/E LOWER SKIN, AT RIB 10 AND RIB 11 WITH EXISTING REPAIR WITHOUT RECORDS. NOTE: THE LH WING, LOWER SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-031226 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18979-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM: 21-113 ).

Part: SKIN PANEL — BURNED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

LOWER FUSELAGE, AT FR76+365MM, STRINGER 26LH+142MM EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030547 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18904-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM: 21-12 ).

Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

PER CUSTOMER REQUEST REPLACE THE FASTENER INSTALLED ON CENTER FUSELAGE III, AT FR90+140MM, STRINGER 27RH+17MM, EXTERNAL SKIN WITH EXISTING THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2011-190-06011 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18970-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-53 ).

Part: SKIN PANEL — BURNED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

CENTER FUSELAGE I, FROM FR33+40MM TO X=11035.0, BETWEEN STRINGER 24LH AND STRINGER 25LH, LOWER EXTERNAL SKIN WITH LIGHTNING STRIKES. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030701 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18927-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-40 ).

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

CENTER FUSELAGE I, AT FR25+235MM, STRINGER 26LH+17MM, EXTERNAL LOWER SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030721 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18924-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-5 ).

Part: SKIN PANEL — BURNED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

LOWER FUSELAGE, AT FR01+150MM, STRINGER 24RH+130MM, EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030945 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18945-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-13 ).

Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

FORWARD FUSELAGE, BETWEEN FR16+250MM AND FR18+80MM, AND BETWEEN STRINGER 20RH AND STRINGER 21RH, EXISTING SKIN REPAIR EVALUATION. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030699 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18944-R01 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-22 ).

Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 36,663 hrs · 23,950 cycles

CENTER FUSELAGE III, FROM FR81+95MM TO FR82+85MM, BETWEEN STRINGER 23LH+35MM AND STRINGER 26LH+105MM, EXTERNAL SKIN WITH EXISTING REPAIR WITHOUT TRACEABILITY OF MATERIALS. FURTHERMORE, FROM FR80+70MM TO FR81+70MM, BETWEEN STRINGER 23LH AND STRINGER 24LH EXTERNAL SKIN WITH EXISTING BLENDOUT. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030676 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18905-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-51 AND 21-50 ).

Part: SPOILER — FAULT MESSAGE · airframe 36,262 hrs · 23,679 cycles

FLT#2151, BOS-MCO. (AIRCRAFT DIVERTED TO FLL) 'ON DESCENT INTO MCO WITH SPEED BRAKES TO FULL WE GOT SPOILER FAULT MSG; T/S FAULT PER TSM 27-03-00 PERFORMED R.T.S PER AMM 29-10-00-863-802-A/200 FAULT CLEARED. OK TO CONTINUE. '

Part: NONE — NONE · airframe 35,765 hrs · 23,309 cycles

FLT#1051, HPN-PBI. ' DURING IDLE DESCENT 15000' EXPERIENCED ODOR APU OFF EVENT LASTED ABOUT 2 MINS; PERFORMED FAULT ISOLATION. ENG'S 1 AND 2 RUN UP NO ODOR OR FUMES NOTED, ALL NORMAL. AIRCRAFT OK FOR SERVICE REF MM TASK 21-20-00-810-803.'

Part: NONE — NONE · airframe 35,231 hrs · 22,977 cycles

FLT # 6399, FLL-HAV (AIR TURN BACK TO FLL). BLD LEAK #2 EICAS MSG ON CLIMB OUT. PERFORMED QRH & EICAS MSG WENT OUT; PERFORMED REPAIR OF PRE COOLER EXHAUST SEAL PER MAB 36-00-14-012 & SRM 51-21-06 OPS & LEAK CK NORMAL A/C OK FOR SVC

Part: STRINGER — CRACKED · airframe 35,219 hrs · 22,971 cycles

DURING HEAVY MAINTENANCE, CRACK ON END AREA OF STRINGER 9LH AT FUSELAGE STRUCTURE FRAME 91; REF TOMX WO 1834 NR -00468, STRINGER 9LH AT FUSELAGE STRUCTURE FRAME 91 WAS REPLACED FOR A NEW STRINGER PER EMB-190 SRM 51-41-02 AND SRM 51-43-03

Part: RIB — CRACKED · airframe 35,219 hrs · 22,971 cycles

DURING HEAVY MAINTENANCE, CRACK ON FIXED LEADING EDGE RIB # 22 AT LH WING; REF TOMX WO 1834 NR -00593, RIB # 22 ON FIXED LEADING EDGE AT LH WING WAS REPLACED PER EMB190 SRM 51-43-02

Part: RIB — CRACKED · airframe 35,219 hrs · 22,971 cycles

DURING HEAVY MAINTENANCE, CRACK IN RIB 17 OF FIXED L.E. LH WING ; REF TOMX WO 1834 NR -00193, RIB 17 OF FIXED L.E. LH WING WAS REPLACED PER EMB190 SRM 51-43-04

Part: RIB — CRACKED · airframe 35,219 hrs · 22,971 cycles

DURING HEAVY MAINTENANCE, CRACK: RIB 11 AND SPAR II LOWER SKIN LH WING; REF TOMX NR 00100: LOWER SKIN BTW RIB 11 AND SPAR II OF LEFT WING WAS REPAIRED PER EMB190 SRM 57-10-01/REPAIR 54P PAR 11. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY.

Part: VALVE — FAILED (FAN AIR) · airframe 31,378 hrs · 20,452 cycles

FLT 1279, DIVERTED. THE NR 2 BLEED IS CURRENTLY ON MEL, THE NR 1 BLEED FAILED IN ROUTE. BLEED 1 FAIL EICAS MESSAGE IN FLIGHT . RESET SUCCESSFUL. BLEED 1 FAIL MESSAGE HAPPENED AGAIN, RESET SUCCESSFUL. ENGINE BLEED SYS-BOTH-BELOW FL150-APU OK. R & R FAN AIR VALVE IAW AMM 36-11-09. OPS CHECKED GOOD, NO DEFECT NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,549 hrs · 18,363 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM INBD POSITION RT LOCATED BTWN FR 12-20 AT FWD GALLEY AREA. CORROSION IS BEYOND LIMITS AS PER SRM 53-10-10; REPLACED FLOORBEAM LOCATED AT FR 12-20 RT SIDE PASSENGER CABIN IAW SRM 51-40-08 AND DRAWING 170-00822-503 & NR 927011-2018-246841.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,549 hrs · 18,363 cycles

DURING HEAVY MAINTENANCE (B5 CHECK) AT (SAL), CORROSION WAS FOUND ON FR 17 CROSSBEAM FLOOR PN 170-21769-403 UPPER FLANGE BETWEEN Y 273.0 TO THE OUTBOARD END AND 2 EXISTING REPAIRS WERE FOUND ON FR 17 CROSSBEAM. SEE REF /1/ EA FOR MORE DETAILS. SRM 53-00-10 REPAIR 53 FIGURE 203 SPLICE REPAIR FOR THE FLANGE. THE FLANGE IS TO ENCOMPASS THE 2 EXISTING REPAIR, HOWEVER THE UPPER FLANGE IS EQUAL TO 4MM, PER SRM THE REPAIR IS OUT OF LIMITS, CONTACTED AND PROVIDED REF/2/. THIS EC E18-665-01 ACCOMPLISHES THE 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 PER REF /4/ MX-244 GUIDELINES.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,549 hrs · 18,363 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR STRUCTURE (CROSS BEAM) AT LEVEL OF FR 17 RT SIDE AT FWD GALLEY AREA. NO FOUND ALLOWABLE DAMAGE IN SRM; PERFORMED PERMANENT REPAIR ON CROSSBEAM LOCATED AT FR 17 RT SIDE IN PASSENGER CABIN IAW EA 53-0218-18 COVER AND PART 1. REF. NR 246842.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,446 hrs · 18,279 cycles

FT 824, MCO-DCA. EMERGENCY LIGHTING ABOVE ROW 13 AND AFT MAIN DOOR LINER (RED) LIGHTS INOP. R&R BATTERY & EMERGENCY PWR SUPPLY 5 IAW AMM 33-50-01. OPS CKS GOOD. A/C OK FOR SVC.

Part: SHUTOFF VALVE — FAILED (ENGINE) · airframe 27,195 hrs · 17,438 cycles

DIVERTED DUE TO A OF LOSS OF CABIN PRESSURIZATION AND CABIN OXYGEN MASKS DEPLOYED. BLEED 1 LEAK INFLIGHT, AFTER 2 MINUTES MESSAGE REAPPEARED. COMPLIED WITH QRH. R & R THE HP & PRSOV , FOUND BOTH LEAKING DURING TROUBLESHOOTING. ACCOMPLISHED AN ENG RUN, ACFT OK FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE) · airframe 27,195 hrs · 17,438 cycles

DIVERTED DUE TO A LOSS OF CABIN PRESSURE AND CABIN OXYGEN MASKS DEPLOYMENT. BLEED 1 LEAK INFLIGHT, AFTER 2 MINUTES MESSAGE REAPPEARED. COMPLIED WITH QRH. R & R THE HP & NAPRSOV. FOUND BOTH LEAKING DURING TROUBLESHOOTING. RAN ENGINES, OK FOR SERVICE. NR 1 ENG NAPRSOV REMOVED DUE STATIC LEAK WITH APU BLEED AIR SOURCE. REMOVED & REPLACED NAPRSOV IAW AMM 36-11-03 ENG 1. HIGH POWER RUN ACCOMPLISHED, OPS CHECKED OK, NO FAULTS NOTED. NR 1 ENGINE HP VALVE REMOVED DUE STATIC LEAK WITH APU BLEED AIR SOURCE. REMOVED & REPLACED THE NR 1 ENGINE BLEED PRESSURE REGULATING SHUT OFF VALVE IAW AMM 36-11-01 HIGH POWER RUN ACCOMPLISHED. OPS CHECKED OK. NO FAULTS NOTED.

Part: DEFLECTOR — DAMAGED (AIRFRAME) · airframe 24,845 hrs · 15,743 cycles

AT LEVEL FL220, 270KTS INDICATED INCREASED SPEED TO 290KTS THEN HEARD LOUD SHUTTERING SOUND, BOTH FA'S CALLED SAYING THEY ARE HEARING A LOUD SHUTTERING SOUND AS WELL, AT THAT POINT THE CABIN STARTED CLIMBING AT 1300FPM TO 2200 FPM, WE DECREASED SPEED TO 250KTS TO LOWER THE SHUTTERING SOUND ONCE THE POWER WAS REDUCED THE CABIN STOPPED CLIMBING AND THE SHUTTERING WAS REDUCED. WE CONTINUED SLOWING TO 210KTS AND THE NOISE WENT AWAY, THE POWER LEVERS WERE AT IDLE DURING DESCENT. WHEN THE SHUTTERING ACCOURED IT ALSO HAD A VIBRATION ASSOCIATED IN THE AIRFRAME DOOR DEFLECTOR. PERFORMED PRESSURIZATION CHECK IAW AMM 21-31-00-720-802A, ALL CHECKS NORMAL. REMOVED L1 DOOR DEFLECTOR AND REPLACED PAX DOOR DEFLECTOR IAW AMM 52-11-28.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,138 hrs · 15,300 cycles

CENTER AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY. ACCOMPLISHED SATISFACTORY CHECK OUT IAW AMM 33-50-01.

Part: A/C PACK — FAULTED (NR 1) · airframe 23,786 hrs · 15,058 cycles

SMOKE AND FUMES IN CABIN AND FUMES IN COCKPIT. AFTER TURNING OFF POWER TO IFE/CSS AND IFFC CONNECTIVITY INFLIGHT REPORTED SMOKE DISSIPATED AND FUMES LESSENED. PASSENGER IN ROW 9 REPORTED GRINDING MOTTOR SOUND ONCE FLAPS WENT DOWN; ACCOMPLISHED FIM TASK 21-20-00-810-801A AND 21-51-00-810-802A. FOUND NR 1 PACK FAULTED. PERFORMED FLAP OPS CHECK AS REQUIRED, NO FAULTS NOTED. ENGINES 1 AND 2 GROUND RUN SATISFACTORY.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 23,662 hrs · 14,987 cycles

FLIGHT CREW REPORTED A COMPLETE LOSS OF NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE. ACCOMPLISHED QRH 10-11 PROCEDURE. R & R THE NR 2 PUMP IAW AMM 29-11-01. PERFORMED OPS & LEAK CHECK. OPS & LEAK CHECKED PASSED.

Part: MANIFOLD — FAILED (NLG STEERING) · airframe 22,043 hrs · 13,825 cycles

AFTER LANDING, RECEIVED STEERING FAULT EICAS MESSAGE. IAW MAINTENANCE INSTRUCTIONS ATTEMPTED RESET, SEEMED SUCCESSFUL, BUT STEERING FAIL APPEARED AGAIN AFTER ABOUT 100 FT OF TAXI. EXPERIENCED ACTUAL LOSS OF NOSE WHEEL STEERING; T/S IAW TSM FIM TASK 32-52-00-810-801A, FOUND STEERING MANIFOLD AT FAULT. R & R STEERING MANIFOLD IAW AMM 32-52-01 LEAK AND OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,934 hrs · 13,747 cycles

DURING MAINTENANCE, AFT SERVICE EMERGENCY DOOR EXIT LIGHTS WERE FOUND TO BE INOPERATIVE; REPLACED NR 5 EMERGENCY LIGHTS BATTERY IAW AMM 33-50-01. OPS CHECK GOOD.

Part: ENGINE — MAKING METAL (NR 1) · airframe 21,861 hrs · 13,694 cycles

DIVERTED, CREW REPORTED ENGINE NR 1 WAS EXPERIENCING HIGH VIBRATIONS AFTER TAKEOFF. CREW ALSO REPORTED EGT WAS 60 DEGREES HOTTER AND FUEL FLOW WAS 400 LBS INCREASED COMPARED TO ENGINE NR 2. INITIAL INSPECTION AND ENGINE WALK AROUND WAS PERFORMED. FOUND METALLIC DEBRIS IN TAILPIPE/EXHAUST AREA. ALSO NOTED, NO ROTATION OF ENGINE. R & R ENGINE NR 1. LEAK AND OPS CHECKS NORMAL. OK FOR SERVICE.

Part: DOUBLER — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT DRAIN MAST DOUBLER 15" AFT OF FR86, RBL12". R & R DOUBLER IAW SRM 51-41-02, 51-41-01, 51-40-02.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

RE FEAMS NR 00592 AFT PASSENGER DOOR CUTOUT LWR BEAM HAS CORROSION FR 85 + 14.0" LBL 49.5" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON LT SHEAR PLATE NEAR MOUNTING HOLE 5" AFT OF FR 87 AT LBL37. R & R PLATE IAW SRM 51-42-01, 51-42-02.

Part: BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, FWD SERVICE DOOR LOWER BEAM, STR 17R, 8" AFT OF FRAME 16 HAS CORROSION. R & R BEAM IAW SRM 51-43-02, 51-43-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT SERVICE DOOR LOWER BEAM 12" AFT OF FR 86, RBL 45. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-127-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON LT SHEAR PLATE ALONG FWD EDGE AROUND RIVETS AT FR 87 LBL 31. R & R EAMS NR 00236 FOR WORK ACCOMPLISHED.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION FR 86 + 5.5", LBL 49.5" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: SKIN — CORRODED (FRAME 75) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, FUSELAGE SKIN 8" AFT OF FR 75, STR 29L-29R. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION FR 86 + 2.0" LBL, 49.5. ACCOMPLISHED BLEND REPAIR IAW EC E16-130-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON LT SHEAR PLATE AROUND RIVETS ALONG FWD EDGE AT FR 87 LBL38-40. R & R EAMS NR 00236, FOR WORK ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

REF EAMS NR 00223, RT SILL CORRODED FROM 7" TO 8.75" AFT OF FRAME 17 AND RBL 47.5" TO 48.5". ACCOMPLISHED BLEND REPAIR IAW JB EC E16-107-01.

Part: SKIN — CORRODED (FRAME 80) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN 4 INCHES AFT OF FRAME 80 STRINGERS 29R-29L. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT SERVICE DOOR LOWER BEAM 5" AFT OF FR85, RBL47". ACCOMPLISHED BLEND REPAIR JB, EC E16-127-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION, FR 85 + 5.5" LBL 47.0" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: FLOORBEAM — CORRODED (FRAME 12) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

LT BEAM OTBD OF LT SEAT TRACK CORRODED 1.75" TO 2.5" AFT OF FRAME 12 AND LBL 10.25" TO 11.5". ACCOMPLISHED BLEND REPAIR IAW JB EC E16-107-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT SERVICE DOOR LOWER BEAM 4 INCHES AFT OF FRAME 85, RBL 46. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-127-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON AFT CARGO FLOOR SUPPORT AT FR 75 STR 29R. R & R SUPPORT IAW SRM 51-41-01, 51-41-02.

Part: SKIN — CORRODED (FRAME 80) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, FUSELAGE SKIN 15" AFT OF FR 80, STR 29R - 29L. ACCOMPLISHED PERMANENT BLEND REPAIR IAW JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION FR 85 + 14.0" LBL 49.5" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: SKIN — CORRODED (FRAME 80) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN FOUR INCHES AFT OF FRAME 80, STRINGERS 29R-29L. ACCOMPLISHED BLEND REPAIR JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION FR85 + 1", LBL 47.0", AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB ECD E16-130-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION FRAME 86 + 13.0", LBL 49.0" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON RT SHEAR PLATE AROUND RIVETS AND FWD EDGE OF PLATE AT FR 87 FROM RBL 29-37. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-116-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION FR 86 + 13.0", LBL 47.O" AS MARKED. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-130-01.

Part: SPLICE — CORRODED (FRAME 18) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

RT SPLICE CORRODED FROM .5" TO 1.75" AFT OF FR 18 AND RBL 23.0" TO 25.0". ACCOMPLISHED BLEND REPAIR IAW JB EC E16-107-01.

Part: SKIN — CORRODED (FRAME 80) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN 15" AFT OF FRAME 80, STRINGERS 29R-29L. BLEND REPAIR IAW JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT SERVICE DOOR LOWER BEAM 9" AFT OF FR86, RBL 46. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-127-01.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, AFT CARGO DOOR FWD FINGER DOUBLER 1" AFT OF FR 77, RBL 12". R & R DOUBLER IAW SRM 51-43-01, 53-43-02, 51-23-06.

Part: BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION, FWD SERVICE DOOR LOWER BEAM, STR 17R 11" AFT OF FRAME 16 HAS CORROSION ON EDGE OF THE GIRT BAR FITTING CUTOUT. R & R BEAM IAW SRM 51-43-02, 51-43-01.

Part: SHEAR TIE — CORRODED (FRAME 85) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON SHEAR CLIP FR 85, STR 27R - 28R. R & R CLIP IAW SRM 51-41-01, 51-41-02.

Part: SKIN — CORRODED (FRAME 75) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN 2" AFT OF FRAME 75, STRINGERS 29L-29R. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-146-01.

Part: BEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

REF EAMS, NR 00559 CORROSION, FWD SERVICE DOOR LOWER BEAM, STR 17R 6" AFT OF FR14 HAS CORROSION. R & R BEAM IAW SRM 51-43-02, 51-43-01.

Part: STRINGER — CORRODED (FRAME 76) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

REF EAMS NR 00608, CORROSION, STR 29R 8" AFT OF FR76. ACCOMPLISHED PERMANENT ANGLE REPAIR IAW JB EC E16-131-01.

Part: SKIN — CORRODED (FRAME 76) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN 12 INCHES AFT OF FRAME 76, STRINGERS 29L - 29R. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-146-01.

Part: SHEAR TIE — CORRODED (FRAME 81) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON SHEAR CLIP FR 81, STR 28R - 29R. R & R CLIP IAW SRM 51-41-01, 51-41-02.

Part: SKIN — CORRODED (FRAME 76) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON FUSELAGE SKIN 14 INCHES AFT OF FRAME 76 STRINGERS 29L-29R. ACCOMPLISHED BLEND REPAIR IAW JB EC E16-146-01.

Part: FLOORBEAM — CORRODED (FRAME 13) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

REF EAMS NR 00221, FWD RT SILL CORRODED FROM 2.5" TO 9.0" AFT OF FR 13 AND RBL 47.0" TO 49.0". ACCOMPLISHED BLEND REPAIR JB EC E16-107-01.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,357 hrs · 13,352 cycles

CORROSION ON MIDDLE SHEAR PLATE 5" AFT OF FR 87, LBL 2. ACCOMPLISHED BLEND REPAIR IAW EC E16-116-01.

Part: HARNESS — FAULTY (ZONE 500) · airframe 19,506 hrs · 12,044 cycles

AIR RETURNED TO DEPARTURE, DUE TO AI WING LEAK 1 EICAS. SECURED WING ANT-ICE VALVE CLOSED IAW AMM TASK 30-11-01-801-A IAW MEL. INSPECTED WING PICCOLO PLUMBING FOR LEAKAGE. REACTIVATED WING ANTI-ICE S/O VALVES IAM 30-11-01-040-801-A. R & R LT WING SLAT NR 4 W513 HARNESS IAW AMM 30-11-02. OPS CHECK GOOD.

Part: ACM — FAILED (RIGHT) · airframe 17,864 hrs · 10,943 cycles

BURNING ODOR IN CABIN AFTER ENG START, WIND BLOWING OFF SIDE NOT TAIL WIND, ODOR DISSIPATED BUT RETURNED AT 10,000 FT FOR APPROXIMATELY 5 MIN. ODOR SIMILAR WITH PROBLEM WITH PACKS. ACCOMPLISHED ABNORMAL ODOR INSPECTION IAW FIM TASK 21-20-00-810-801-A, FOUND NR 2 PACK MAKING NOISE AND CAUSING ODOR. R & R 2 ACM, WORKED IAW 21-51-05. OPS CHK, LEAK CHK GOOD.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 17,283 hrs · 10,547 cycles

CREW DECLARED AN EMERGENCY DUE TO A NR 2 ENGINE LOW FUEL PRESSURE CAS MESSAGE ALONG WITH A FUEL FEED 2 FAULT. AFTER RUNNING BOTH QRH PROCEDURES BOTH MESSAGES EXTINGUISHED AND FUEL SYSTEM RETURNED TO NORMAL. R & R ENG NR 2 FUEL LOW PRESSURE SWITCH IAW AMM 73-31-01 & EMM 71-00-73. OPS AND LEAK CHECKED GOOD.

Part: ENGINE — VIBRATION (NR 1) · airframe 17,147 hrs · 10,447 cycles

NR 1 ENGINE VIBRATION DURING CRUISE, ITT +50-60 HOTTER THAN NR 2, N1 + 1%> NR 2, FF + 150> NR 2 APPROXIMATE SPEED .5 ROLL TO RT SIDE TO HOLD LEVEL TRIM. NR 1 ENG SURGE IND DURING DESCENT. TROUBLESHOT IAW FIM 72-00-00-810-807-A & EMM 72-00-00-810-311/100; NO RECORDED OR ACTIVE MAINT MESSAGES ON CMC. INSPECTED DP3 AIR TUBES FOR DAMAGE; NO DEFECTS NOTED. INSPECTED VARIABLE STATOR VANE SYSTEM NO DEFECTS NOTED. IAW FIM CLEANED N2 SENSOR AND FMU HARNESS CONNECTORS. ACCOMPLISHED HIGH POWER ASSURANCE CHECK IAW EMM 72-00-00760-118, CHECKS GOOD, ALL PARAMETERS OK, ACFT OK FOR SERVICE. NOTE: POWERPLANT ENGINEERING REVIEW OF FHDB DVDR DATA SHOWED NO CORRELATED FAULTS / PARAMETERS.

Part: ACTUATOR — FAILED (NR 8 SLAT) · airframe 15,214 hrs · 9,248 cycles

AIRCRAFT RETURN TO DEPARTURE, DUE TO SLAT FAIL ON FLAP RETRACT, SPEED 210 KNOTS, ALT 2000'. CREW EXECUTED QRH AND THE SLAT FAIL CAME BACK GOING FROM 1 TO 0. FLAPS/SLATS EXTENDED NORMALLY FOR LANDING AND FLAPS/SLATS RETRACTED NORMALLY AFTER LANDING. FOUND FAULT CODE 27811021ACE IAW FIM 27-81-00-810-802-A. FOUND OTBD RT SLAT ACTUATOR (8 RT) TORQUE LIMITER TRIPPED. R & R RT NR 8 SLAT ACTUATOR IAW AMM 27-81-01. ALL MECHANICAL AND ELECTRICAL RIGS OK. OK FOR SERVICE AT THIS TIME ALL, OPS CHECKS GOOD.

Part: RAMP — OUT OF ADJUST (L1 DOOR) · airframe 11,164 hrs · 6,626 cycles

FLT 1326 BWI-BOS, AO REPORTS L1 DOOR HARD TO OPEN. FOUND FWD PAX DOOR FWD COMMAND RAMP OUT OF ADJUSTMENT. RE-ADJUST FWD COMMAND RAMP REFERENCE EMB 190 AMM 52-11-00. OPS CHECK GOOD.

Part: FIRE BOTTLE — FAILED (CARGO BAY) · airframe 10,877 hrs · 6,445 cycles

FLT 950 MCO-BOS, AIR RETURN TO MCO DUE TO CRG FWD FIRE SYS FAIL MSG CLIMBING THROUGH 18000 (CARGO COMP FIRE EXTING SYS - FWD/AFT). REMOVED AND REPLACED HIGH RATE CARGO FIRE BOTTLE PER AMM 26-23-01. OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,796 hrs · 4,484 cycles

FLT 6401 BOS-BNA, ON GROUND MAINTENANCE CHECK FOUND RT WING UPPER EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW E190 AMM 33-50-01.

Part: ACM — FAILED (NR 2) · airframe 7,634 hrs · 4,385 cycles

FLT 1230 RDU-BOS, CREW REPORTED SULFUR ODOR IN FLIGHT WITH VISIBLE HAZE IN CABIN AT APPROXIMATELY 11,000 FEET. ODOR DISSIPATED AFTER SEVERAL MINUTES. T/S PER FIM 21-20-00-810-801A AND INSPECTION FOUND VIBRATION AND SULFUR ODOR COMING FROM PACK NR 2 FOLLOWED BY PACK 2 FAIL EICAS MSG. REMOVED AND REPLACED NR 2 ACM AS PER AMM 21-51-05. OPS CHECK GOOD.

Part: PROBE — FAULTY (TAT) · airframe 3,040 hrs · 1,775 cycles

FLT 606 - JFK-PWM AIR RETURN TO JFK DURING CLIMB PRIOR TO 10000 RECORDED TAT 2 FAIL EICAS SHORTLY AFTER ELECTRICAL BURNING SMELL WAS NOTICED IN COCKPIT AND CABIN. TURN RECIRC FAN OFF AND SMELL DECREASED SIGNIFICANTLY. FOUND TAT 2 PROBE AT FAULT FOR BURNING SMELL. REMOVED AND REPLACED TAT 2 PER AMM 34-15-02. OPS CHECK GOOD.