N645AE

Part: DISPLAY — ODOR (ZONE 200) · airframe 54,949 hrs · 52,602 cycles

UPON ENTERING FLT DECK ELECTRICAL BURNING SMELL WITH CA MFD FLICKERING ON AND OFF. R & R IAW AMM 34-22-01. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,856 hrs · 52,508 cycles

EMERGENCY EXIT OVHD LIGHT AT ROW 11 INOPERATIVE. R & R EMERGENCY EXIT LIGHT ASSY ON SIDEWALL AT ROW 12 IAW AMM 33-50-14. OPS CK GOOD

Part: WIRE — BROKEN (ZONE 200) · airframe 54,856 hrs · 52,508 cycles

EMERGENCY LIGHT STRIP A ROW 1A WIRES ARE BROKEN ON AIRCRAFT SIDE FACT 13OCT25 07:28 ROA INSTALLED NEW CONNECTOR MALE AND SUCKET PER SWPM 20-21-00 PN ON 48-7190 PN ON M39029-32-248

Part: LIGHT — BROKEN (ZONE 200) · airframe 54,856 hrs · 52,508 cycles

EMERGENCY LIGHT STRIP AT ROW 2A IS BROKEN. R & R FLOOR PROXIMITY LIGHT STRIP IAW AMM 35-50-12 PN ON 1013196 PN OFF 1013196

Part: SKIN — DENTED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2435 DENTS ON REAR FUSE SKIN AFT OF FR65 BTW STR19-21L. REPAIRED IAW EO1-53-24-0509

Part: CHANNEL — CRACKED (ZONE 300) · airframe 52,661 hrs · 50,064 cycles

55-2392 BOTTOM OF VERT STAB LH TE CHANNEL PROFILE CRACKED ON AFT SIDE OF SPAR 3. RAR CHANNEL PROFILE IAW SRM 51-40-02

Part: PROFILE — CRACKED (APU BAY) · airframe 52,661 hrs · 50,064 cycles

53-2399 APU COWLING HAS A CRACKED INTERNAL LWR RH REINFORCMENT PROFILE. RAR PROFILE IAW SRM 51-40-02

Part: SPAR — CHAFED (ZONE 300) · airframe 52,661 hrs · 50,064 cycles

55-2388 BOTTOM OF VETRICAL STAB BOTH LIPS CHAFED ON FWD OF FRONT SPAR 1. REPAIRED IAW EO1-05-24-0458

Part: SUPPORT BRACKET — BROKEN (ZONE 200) · airframe 52,561 hrs · 50,064 cycles

53-2319 RH WING TO FUSE LATERERAL FAIRING SUPPORT BRACKET BROKEN. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: BONDING STRAP — CORRODED (RT TE FLAP) · corrosion level 2 · airframe 52,661 hrs · 50,064 cycles

57-2271 RH IB FLAP HAS CORROSION ON BONDING STRIP AT FLAP ROOT. RAR BONDING STRIP IAW SRM 51-40-02

Part: SEAL — CRACKED (TR DOOR) · airframe 52,661 hrs · 50,064 cycles

78-2258 CACK ON LH LWR TR DOOR OB PROFILE SEAL. RAR SEAL IAW SRM 51-40-02

Part: TRUNNION — CRACKED (RT MLG) · airframe 52,661 hrs · 50,064 cycles

32-2227 RH MLG AFT UPPER TRUNNION CRACKED. REPAIRED IAW EO1-05-24-0458

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2212 RF1 UF BLEED DUCT SUPPORT ANGLE CRACKED AT SFT OF FR68 LH SIDE. RAR ANGLE IAW SRM 51-40-02

Part: FITTING — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2143 FR1, BOX FITTING CRACKED AT FR61-62 STR4-5R. RAR FITTING IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2144: 2 ANGLES CRACKED AT BTW FR67-68 AND BTW STR4-5R. RAR ANGLES IAW SRM 51-40-02

Part: FITTING — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2143 RF1, BOX FITTING CRACKED BTW FR61-62 STR4-5R. RAR FITTING IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2150 RF1, SHEAR CLIP CRACKED AT FR65 BTW STR7-9L. RAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2151 RF1, SHEAR CLIP CRACKED AT FR73 BTW STR8-10R. RAR CLIP IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2147 RF1, SHEAR CLIP CRACKED AT FR73 BTW STR8-10L. RAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2149 RF1, SHEAR CLIP CRACKED AT FR72 BTW STR16-17L. RAR CLIP IAW SRM 51-40-02

Part: GUSSET — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2111 RF1, TIOLET GUSSET CRACKED AT FR61 RH SIDE. RAR GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2148 RF1, SHEAR CLIP CRACKED AT FR73 BTW STR15-16L. RAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 800) · airframe 52,661 hrs · 50,064 cycles

53-2145 CARGO DOOR ROD HLODER LWR ANGLE CRACKED AT FR68. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2102 CTR FUSE III, LH OMGA BEAM IB ANGLE CRACKED AT FR46-50. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2099 CTR FUSE III, CTR OMEGA BEAM ANGLE CRACKED AT FR46-50. REPAIRED IAW EO1-53-24-0462

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2108 CF2, LH SHEAR CLIP CRACKED AT FR25 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2098 CTR FUSE III, ANGLE CRACKED AT FR46 FLOOR LEVEL. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2109 CF2, RH SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2032 FF2, UPPER ANGLE CRACKED IN NOSE HYDRAULIC COMPARTMENT BTW FR6-7. REPAIRED IAW EO 1-53-24-0484

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,661 hrs · 50,064 cycles

53-2036 CTR FUSE IV, RH OMEGA BEAM CORRODED UNDER 2 NUTPLATES BTWFR59-61. REPAIRED IAW EO 1-53-24-0457

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,661 hrs · 50,064 cycles

53-2037 CTR FUSE IV, RH GUSSET CORRODED BTW FR59-61. R & R GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 52,661 hrs · 50,064 cycles

53-2034 CTR FUSE IV, SHEAR CLIP CRACKED AT FR58 BTW STR15-16L. RAR CLIP IAW SRM 51-40-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,661 hrs · 50,064 cycles

53-2022 CORROSION ON EXTERNAL POTABLE WATER DOUBLER. RAR DOUBLER IAW SRM 51-40-02

Part: BRACKET — BROKEN (POTABLE WTR BAY) · airframe 52,661 hrs · 50,064 cycles

BROKEN BRACKET ON POTABLE WATER EXTERNAL DOUBLER. RAR BRACKET AND DOUBLER IAW SRM 51-40-02

Part: SKIN — GOUGED (ZONE 200) · airframe 52,661 hrs · 50,064 cycles

53-2012 FR2, GOUGE FOUND 7" FWD OF FR7 2" ABOVE STR15L. REPAIRED IAW EO 1-53-24-0459

Part: PITOT HEAD — FAILED (NR 3) · airframe 52,422 hrs · 49,808 cycles

DURING TAXI IN, BURNING SMELL FOLLOWED BY PITOT 3 INOP MESSAGE. R+R PITOT STATIC TUBE #3 IAW AMM 34-13-02. PERF OPS CHECK IAW AMM 30-31-00. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: NONE — NONE · airframe 49,975 hrs · 47,025 cycles

NDIS 645 05-52 0034380 13JAN23 MDT CLOSE FOUND POSSIBLE CORROSION ON FWD FUSELAGE UNDERSIDE R/H SIDE JUST FWD OF R/H RVSM ZONE DURING LIGHTNING STRIKE INSPECTION. FACT 13JAN23 09:22 MDT REMOVED PAINT FROM AFFECTED AREA. BEGAN CUT-OUT OF DAMAGE AND PATCH LAYOUT FOR DAMAGE IN BAY OF FR12-F13 ,STGR 1912-20R IRT AMM 51-75-00. UPON FURTHER INSPECTION FOUND ADDITIONAL PITTING CORROSION ON INTERIOR SURFACE OF SKIN AROUND CUT-OUT. REQUIRES FURTHER EVALUATION. EXTENDED CUT-OUT OF DAMAGE IRT SRM 51-75-00. FURTHER CORROSION IS PRESENT IN FWD PORTION OF BAY, REQUIRES EVAL. TWO CORRODED FASTENERS ON INTERIOR ANGLE OF STGR 20R FWD OF FR13 REQUIRE REPLACEMENT. PERFORMED H.F.E.C. INSPECTION TO DAMAGE CUT-OUT AREA. NO FLAWS DETECTED. CORRODED FASTENERS WERE REPLACED. REF HA-300 SEQ 41 DATED 01/26/23 FOR REPAIR DOCUMENTATION 01/28/23 MDT. REPAIRED PER EO1-53-23-0023.

Part: UNKNOWN — FUMES (CABIN) · airframe 49,589 hrs · 46,579 cycles

UPON TAXI OUT ELECTRONIC FUMES SMELLED FROM ROW 7 O/H BIN AREA BY_FA AND PAX. RAN A/C PACKS NO SMELL NOTED. SUSPECT PAX WAS USING VAPE

Part: BATTERY — ODOR (MASTER) · airframe 48,430 hrs · 45,193 cycles

ELECTRICAL BURNING SMELL IN FLIGHT DECK AFT OF CREW SEATS. R & R LT AND RT RELAY SUPPORT PANELS AND LT & RT CONTACTOR PANELS. PERFORMED GVI OF RELAYS & CONTACTORS. NO DEFECTS OR SMELLS NOTED. REINSTALLED PANELS. FOUND SMELL TO BE MAIN BATTERIES. BATTERIES R & R. RAN ACFT FOR 15 MINS. NO SMELLS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887286 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-78 MARKED .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-78 APPROXIMATELY 1" BELOW STR 8L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0325

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887287 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-79 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-79 APPROXIMATELY 1" BELOW STR 6L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0325

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887289 - R/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-77 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON R/H EXTERNAL FUSELAGE SKIN AT FR-77 APPROXIMATELY 1" BELOW STR 8R AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0324

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887285 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-77 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-77 APPROXIMATELY 1" ABOVE STR 9L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0325

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E889024 - REINFORCEMENT ON FR 69 DAMAGED FROM CHAFING BETWEEN STRGS 18L-19L .... REMOVED AND INSTALLED SERVICEABLE LOWER LH FR 69 FRAME REINFORCEMENT ANGLE IAW PIEDMONT EO1-53-21-0319 AND EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887717 - RH EMERGENCY HATCH INTERNAL WEBBING UPPER HAS 2EA SMALL NICKS .... INSTALLED R/H EMERGENCY HATCH INTERNAL WEBBING IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888033 - DIAMOND GUSSET AT FR 20 CORRODED .... BLENDED AREA FOUND TO BE NOT ALLOWABLE. RAR RH OMEGA BEAM DIAMOND GUSSET AT FR 20. IAW EMB 145 SRM 53-21-10, SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888039 - LH LOWER #1 SEAT TRACK EMERGENCY STOWAGE ATTACHMENT FEET CORRODED .... REMOVED AND REPLACED L/H LOWER #1 SEAT TRACK EMERGENCY STOWAGE ATTACHMENT FEET IAW EMB 145 AMM 25-26-03.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888045 - SERVICE DOOR FORWARD SILL CORRODED AROUND GALLEY NUT PLATE HOLE .... PERFORMED BLEND OUT OF DAMAGE ON THE SERVICE DOOR FWD SILL AROUND GALLEY NUT-PLATE HOLE. BLENDED AREAS FOUND TO BE BEYOND ALLOWABLE LIMITS. RAR SERVICE DOOR FWD SILL AROUND GALLEY NUT-PLATE HOLE. IAW EMB 145 SRM 51-10-03, SRM 53-21-10, SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888031 - OUTBD BRACKET AT FR 23 FLOORBOARD STEP DOWN CORRODED .... PERFORMED BLEND OUT OF DAMAGE ON THE OUTBD BRACKET AT FR23 FLOOR BOARD STEP DOWN. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE OUT OF LIMITS, RAR OUTBD BRACKET AT FR 23 FLOORBOARD STEP DOWN IAW EMB 145 SRM 51-10-03, SRM 53-22-10-AD, SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888036 - LH UPPER #1 SEAT TRACK CORRODED .... REMOVED AND REPLACED LH #1 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888042 - SERVICE DOOR CENTER SILL CORRODED AROUND FWD NUT PLATE HOLE .... PREPPED, FABRICATED AND INSTALLED FABRICATED INTERNAL DOUBLER FOR SERVICE DOOR CENTER SILL REPAIR AROUND FWD NUT-PLATE HOLE AND APPLIED HYSOL TO AREA IAW EMB 145 SRM 53-21-02RE, ITEM 2, FIGURE 201 AND EO1-53-21-0320

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888043 - SERVICE DOOR CENTER SILL CORRODED AROUND AFT NUT PLATE HOLE ... PREPPED, FABICATED AND INSTALLED FABRICATED INTERNAL DOUBLER FOR SERVICE DOOR CENTER SILL REPAIR AROUND AFT NUT-PLATE HOLE AND APPLIED HYSOL TO AREA IAW EMB 145 SRM 53-21-02RE, ITEM 2, FIGURE 201 AND EO1-53-21-0320

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888030 - AFT SERVICE DOOR SILL CORRODED AROUND AT UPPER JOGGLE .... RAR SERVICE DOOR AFT SILL IAW EMB-145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E888037 - LH LOWER #1 SEAT TRACK CORRODED .... INSTALLED LH #1 LOWER SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

CORRECTION TO DUPLICATE UNIQUE CONTROL NUMBER - E887876 - CARGO DOOR CUT-OUT FR 65 SHEAR CLIP CORRODED .... REPAIRED CARGO DOOR CUT OUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04-RE FIGURE 212 AND EO1-53-21-0317

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887759 - CARGO DOOR INTERNAL WEBBING HAS NUMEROUS NICKS ... ACCOMPLISHED REPAIR OF 3 DAMAGED AREAS ON CARGO DOOR INNER SKIN AT FWD FRAME /HB4, VB3/HB4, AND VB2/HB3 IAW EMB 145 SRM 52-30-01 ITEM 12 AND FIGURE 213 AND EO1-52-21-0316

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887314 - LAV BUCKET EXTERNAL SURFACE CORRODED AROUND WASTE DRAIN VALVE MARKED ... REMOVED, PREPPED AND INSTALLED SERVICEABLE LAV ( BUCKET) CUP IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887742 - CARGO DOOR UPPER FRAME PROFILE CORRODED AT NUTPLATE HOLE ... REMOVED AND INSTALLED NEW CARGO DOOR UPPER FRAME PROFILE IAW EMB 145 SRM 51-40-02, 51-40-09

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887860 - RH #1 CARGO FLOOR SILL CORRODED ... REMOVED AND INSTALLED NEW RH #1 CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · airframe 48,307 hrs · 45,064 cycles

E887858 - LH #2 CARGO FLOOR SILL CORRODED .... UPON FURTHER INVESTIGATION FOUND DAMAGE ON THE LH #2 CARGO FLOOR SILL TO BE OUT OF LIMITS IAW EMB 145 SRM 51-31-10-AD. REMOVED AND REPLACED LH #2 CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887876 - CARGO DOOR CUT-OUT FR 65 SHEAR CLIP CORRODED .... REPAIRED CARGO DOOR CUT OUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04-RE FIGURE 212 AND EO1-53-21-0317

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887864 - CARGO DOOR LWR CUT-OUT FLOOR SILL CORRODED ... REMOVED AND REPLACED CARGO DOOR CUT- OUT LOWER FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887863 - RH #4 CARGO FLOOR SILL CORRODED .... RAR RH #4 CARGO FLOOR SILL IAW EMB145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887870 - SHEAR CLIP AT FR 65 BETWEEN STRGS 21R-20R CORRODED ... REMOVED AND REPLACED SHEAR CLIP AT FR 65 BETWEEN STRGS 21R-20R IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887865 - FR 66 CRACKED AT STRG 16R .... REMOVED, FABRICATED AND INSTALLED FABRICATED FR-66 SPLICE "U" SHAPE DOUBLER REPAIR AT STRG 16R IAW EMB 145 SRM 53-00-04-RE FIGURE 201 AND EO1-53-21-0318

Part: NONE — NONE · corrosion level 2 · airframe 48,307 hrs · 45,064 cycles

E887868 - FR 69 DAMAGED FROM CHAFING BETWEEN STRGS 18L-19L .... PREPPRED, FABRICATED AND INSTALLED SERVICEABLE REPAIR INTERNAL DOUBLER AND FILLER FOR FR 69 BETWEEN STRGS 18L-19L IAW ETD2021-145-037110 AND EO1-53-21-0319

Part: UNKNOWN — ODOR (CABIN) · airframe 47,002 hrs · 43,662 cycles

PACK 2 OVERHEAT WITH STRONG BURNING SMELL WHEN THRUST LEVERS AT HIGH SETTING. C/W FIM TASK 21-51-00-810-804-A BLOCK 2 RESULT IN NO PACK 2 OVERHEAT EICAS MESSAGE. NO RESULT BLOCK II TRANSITORY CONDITION OF AIR CONDITIONING SYSTEM. END TROUBLE-SHOOTING. FOUND WON AND LEAKING SLEEVE AT NR 2 PACK VALVE Y DUCT REPLACED SLEEVE. SYSTEM OPERATIONS CHECK GOOD, OK FOR SERVICE. STRONG FUEL SMELL IN FLIGHT DECK AND CABIN, REF SEQ 1. RAN PACKS NR 1 AND NR 2 FOR 15 MINUTES. NO ABNORMAL ODORS OBSERVED. OK FOR SERVICE AT THIS TIME. NO SMELLS DURING NR 2 ENGINE RUNS.

Part: COMPUTER — MALFUNCTIONED (AURAL WARNING) · airframe 46,053 hrs · 42,575 cycles

PDIS 645 31-50 2130021 14FEB20 CLT CLOSE AFTER TAKEOFF, TAKEOFF CONFIG TRIM AURAL WARNING, WA RNING STOPPED BY ITSELF. NO EICAS MESSAGES. TRIM IND ICATIONS WITHIN RANGE. FACT 14FEB20 16:39 CLT R&R AURAL WARNING COMPUTER IAW EMB AMM 31-51-01 AND 31-51-00 OPS CHECK GOOD OK FOR SERVICE.

Part: KNOB — DETACHED (STNDBY ALTIMETER) · airframe 45,639 hrs · 42,116 cycles

STAND-BY ALTIMETER KNOB FELL OFF....FIX: RESECURED KNOB.OK FOR SERVICE.OPS CHECK GOOD

Part: ACM — SEIZED (AC BAY) · airframe 45,111 hrs · 41,507 cycles

PDIS 645 21-01 2075172 08SEP19 MDT CLOSE SMOKE IN COCKPIT AT FL 210 CREW RAN QRH. NO EICAS MESSAGES PRESENT. FACT 08SEP19 11:33 MDT FOUND #1 ACM SEIZED R&R'D #1 ACM REF AMM 21-51-03 OPS CK GOOD AT THIS TIME.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 45,103 hrs · 41,498 cycles

PAX DOOR EMERGENCY LIGHT INOP. FIX: REMOVED #1 EMERGENCY LIGHTING SYS BATTERY. FOUND BAD FUSE ON BATTERY PACK BASE. R&RD FUSE. REINSTALLED BATTERY.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 44,564 hrs · 41,387 cycles

BLEED 1 LEAK WARNING AFTER TAKE-OFF C/W QRH MESSAGE EXTENDED RETURNED TO PHL. FIX: MAINT INSPECTED AND FOUND DAMAGED ORING IN BAG BAY BLEED VALVE AT JOINT 19 IN REF TO AMM 36-11-10. R&RD BLEED ORING IN REF TO AMM 36-11-10. OPS CHECK GOOD AND LEAK CHECK OK FOR SERVICE AT THIS TIME.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 44,877 hrs · 41,248 cycles

BLEED 1 LEAK EICAS MESSAGE ON APPROACH. FIX: FOUND LEAKING 0-RING ON BAG BAY BLEED DUCT AND AFT CABIN BLEED DUCT. R&RD O-RINGS IAW AMM 36-11-10-000-801-A/400-801-A. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: ACM — INOPERATIVE (NR 1) · airframe 44,757 hrs · 41,112 cycles

NR 1 PACK HAD LOSS OF AIRFLOW. R & R ACM IAW AMM 21-51-03, OPS CHECK GOOD. FOUND DURING RUNS AT TRI.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,757 hrs · 41,112 cycles

AT 24,000 FT SMOKE ENTERED COCKPIT WITH BURNT PLASTIC SMELL AND HAZE IN CABIN. THERE WAS ALSO LOSS OF AIRFLOW IN PACK #1... FIX: INSPECTED PACK 1 FOR DAMAGE, NONE FOUNDNO #1 PACK HAD LOSS OF AIR FLOW). R & R THE LT ACM.

Part: SWITCH — FAULTY (AC BAY) · airframe 44,588 hrs · 40,928 cycles

645 05-50 1881141 25MAY19 CLT CLOSE ELECTRICAL SMELL IN FLT DECK DURING TAXI OUT. 29593 00 VAG FACT 25MAY19 15:50 CLT R\R #2 PACK OVERTEMP SWITCH RAN A/C WITH BOTH PACK OPS CHECK GOOD OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 44,188 hrs · 40,462 cycles

PDIS 645 21-30 1907392 14MAR19 ROA CLOSE AT FLT LEVEL 250 CABIN GOT WARM IN BACK, CAPT LOWERED TEMP AND WENT INTO MANUAL MODE AT WHICH POINT PACK 1 CLOSED. CABIN ALTITUDE SHOT FROM 4000 TO 7000 FT IN SECONDS. STARTED DECENDING PACK 1 CAME ON AND DIVERTED TO ROA. FACT 14MAR19 04:14 ROA OPS CHECKED NR 1 PACK PER AMM 21-20-00 RAN CABIN TEMPAT FULL COLD AND FULL HOT IN AUTO AND IN MANUAL. OPS CHECK GOOD. PACK 1 DID NOT SHUT DOWN. NO DEFECTS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,000 hrs · 40,244 cycles

CABIN LT OMEGA BEAM AT FR.38 IS CORRODED. REPAIRED CABIN LT OMEGA BEAM AT FR 38 IAW SRM 53-00-10RE ITEM 3 FIGURE 202 SHEET 2.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 44,000 hrs · 40,244 cycles

CARGO DOOR EXTERIOR SKIN IS CRACKED AT HANDLE CUTOUT. COMPLIED WITH ERS EM-53MR-946 CARGO DOOR SKIN - PERMANENT REPAIR.

Part: WIRE — BROKEN (CABIN) · airframe 44,000 hrs · 40,244 cycles

LT FORWARD EMERGENCY PROXIMITY LIGHT STRIP NR 3 HAS A BROKEN WIRE. R&R NR 3 LT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,000 hrs · 40,244 cycles

CABIN CENTER OMEGA BEAM AT FR38 IS CORRODED.

Part: FITTING — CRACKED (LT PYLON) · airframe 44,000 hrs · 40,244 cycles

LT PYLON INTERIOR FUSELAGE TO RIB "5" SHEAR CLIP IS CRACKED. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP INSIDE PYLON IAW SRM 51-40-02.

Part: WIRE — BROKEN (CABIN) · airframe 44,000 hrs · 40,244 cycles

LT EMERGENCY PROXIMITY LIGHT STRIP NR 4 HAS A BROKEN WIRES. R&R NR 4 LT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12-04.

Part: RIB — CRACKED (RT WING) · airframe 44,000 hrs · 40,244 cycles

RT WING RIB 21 IS CRACKED INSIDE PANEL 651CB. PERFORMED REPAIR ON RT RIB 21 AS REQUIRED IAW SRM 57-20-07 STEP 4.

Part: BEAM — GOUGED (ESCAPE HATCH) · airframe 44,000 hrs · 40,244 cycles

RT PASSENGER CABIN ESCAPE HATCH BEAM 2 IS GOUGED 2 EACH. RT PASSENGER CABIN ESCAPE HATCH BEAM (INTERNAL SKIN) GOUGES REPAIRED IAW ERS-EM-52MR-947.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,000 hrs · 40,244 cycles

PROTRUSION AND CORROSION IN SKIN AND RIVETS PULLED THROUGH AT FRAME 67 BETWEEN STGRS 20L AND 21R. PROTRUSION AND CORROSION IN SKIN AND RIVETS PULLED THROUGH AT FRAME 67 BETWEEN STGRS 20L AND 21R REPAIRED IAW ERS-EM-53MR-3603.

Part: FITTING — DAMAGED (CABIN) · airframe 44,000 hrs · 40,244 cycles

ALL LT EMERGENCY LIGHT FLOOR EXTRUSIONS DAMAGED (EXCLUDING RAMP). R&R ALL LT EMERGENCY LIGHT FLOOR EXTRUSIONS (EXCLUDING RAMP) IAW AMM 33-50-12-04.

Part: WIRE — BROKEN (CABIN) · airframe 44,000 hrs · 40,244 cycles

EMERGENCY LIGHT STRIP AT 251BF HAS BROKEN WIRE ON THE AIRCRAFT SIDE. REPAIRED LIGHT STRIP WIRE AT 251BF IAW SWPM 20-50-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,968 hrs · 40,215 cycles

PACK 1 & 2 OVERLOAD CONTINUOUS MSG-C/A-OPERATED BOTH PACKS ON GROUND IN VARIOUS TEMP SETTINGS FOR 20 MINS. COULD NOT DUPLICATE MSG. OPS CHECK IAW AMM TASK 21-20-00 SUCCESSFUL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,927 hrs · 40,168 cycles

ROW 12 CEILING EMERGENCY LIGHT INOP-C/A-RAR ROW 12 CEILING EMERGENCY LAMP IAW EMB AMM TASK# 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,112 hrs · 39,290 cycles

DURING A PS-2 CHECK, FOUND THE COCKPIT EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-50-05-000-801-A AMM 33-50-05-400-801-A. OPS CHECKED GOOD. NO FURTHUR DEFECTS NOTED.

Part: SENSOR — FAILED (NR 2 ENGINE) · airframe 43,000 hrs · 39,170 cycles

ABORTED TAKEOFF AT 60 KTS E2 NO DISP. C/W FIM 75-41-00-810-804-A01 & FIM 75-41-00-810-801-A01. REMOVED AND REPLACED ENGINE T2.5 SENSOR IAW MM 75-41-10.

Part: UNKNOWN — ODOR · airframe 42,983 hrs · 39,149 cycles

POSSIBLE LIGHTING STRIKE WHILE IN CLOUDS FLIGHT LEVEL 220 ELECTRICAL BURNING SMELL LIKE FOR ABOUT 5-10 MIN EXIT OUT OF CLOUDS SMELL DISSIPATED. PERFORMED GVI OF AIRCRAFT IAW SRM 51-10-02. NO EVIDENCE OF LIGHTING STRIKE FOUND. CREW PERFORMED ENGINE RUN. NO SMELL NOTED AIRCRAFT OK FOR SERVICE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,192 hrs · 38,389 cycles

GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. NO FURTHER DISCREPANCIES FOUND.

Part: WIRE — BROKEN (CABIN) · airframe 41,927 hrs · 38,170 cycles

SERVICE DOOR EMERGENCY LT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. PERFORMED GVI AND FOUND BROKEN WIRE. RESPLICED WIRE IN REFERENCE WITH SWPM-2430-20-21-00. OPC GOOD. NO FURTHER DISCREPANCIES WERE FOUND. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,460 hrs · 36,861 cycles

RIGHT EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10. OPS TESTED GOOD IAW AMM 33-50-00.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 40,456 hrs · 36,851 cycles

CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. LUBED MAIN CABIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 40,361 hrs · 36,763 cycles

CONNECTOR ON LIGHT STRIP 8 BROKEN. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-00-03. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 40,124 hrs · 36,572 cycles

EMERGENCY LIGHT ON AFT GALLEY WALL INOP. REMOVED AND REPLACED 3 EMERGENCY LIGHT INVERTER, OPC GOOD IAW AMM 33-50-11.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 40,122 hrs · 36,570 cycles

LIGHTNING STRIKE ENROUTE W/ AN ELECTRICAL SMOKE SMELL NOTED IN COCKPIT AND THE CABIN. LIGHTNING STRIKE INSPECTION ACCOMPLISHED IAW MTX W/C 05-200-00. REFERENCE NRWC 645-ORD-03378 FOR ELECTRICAL SMOKE SMELL NOTED IN COCKPIT AND CABIN. C/W ODOR EVENT T/S PER ETN-EM-72-034, NO ABNORMAL SMELLS NOTED.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 40,112 hrs · 36,561 cycles

NR 1 BLEED OVERTEMP. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW AMM 36-11-03. OPS CK GOOD IAW AMM 36-00-00 LEAK CK GOOD

Part: THERMOSTAT — FAILED (FAN CONTROL) · airframe 39,780 hrs · 36,293 cycles

DURINB CLIMB BELOW 10,000 IN ICICNG CONDITIONS, RECEIVED BLEED 1 OVTEMP WOULD STAY ON A FEW SECONDS THEN GO OFF AND THEN REPEAT. STAYED OFF AFTER AOM 1 CHECKLIST. REMOVED AND REPLACED THE NR 1 FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. PERFORMED AIR BLEED OPERATIONAL TEST IAW AMM 36-00-00. OPERATIONAL CHECKED GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 39,736 hrs · 36,257 cycles

RIGHT AFTER ROTATION LG AIR/GND FAIL MSG ON EICAS "TRANSFERRED TO NRWC 645-DFW-03291"-C/A-REFFERENCE NRWC 645-DFW-03291, FOUND LEFT AND RIGHT WOW PROX SWITCH OUT OF ADJUSTMENT. ADJUSTED IAW 32-63-05 AND OPS CHECK GOOD IAW 32-30-00 WITH NO DEFECTS AT THIS TIME.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,724 hrs · 36,249 cycles

SERVICE-DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPAIRED A WIRE IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LANDING GEAR — MALFUNCTIONED · airframe 39,703 hrs · 36,235 cycles

AFTER TAKE OFF, WENT TO SELECT GEAR UP. HANDLE WOULD NOT MOVE. WAS ABLE TO BRING HANDLE UP, BUT LOUD CRACKLING NOISE AND LANDING GEAR AIR / LAND FAIL MESSAGE. SELECTED GEAR DOWN, RECEIVED 3 GREEN, LOCKED & LANDED. FOUND THREE LOOSE FASTNERS ON TOP AFT SIDE OF PANEL 114AZ, SECURED FASTNERS IAW AMM 53-11-04. PERFORMED THREE LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL TEST IAW AMM 32-30-00 OPS CHECKED GOOD , COULD NOT DUPLICATE FAULT. FOUND SYSTEM TO BE WORKING PROPERLY, ACFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 39,654 hrs · 36,190 cycles

THE BRACKET THAT HOLDS THE FLASHLIGHT BEHIND SEAT 18 B IS BROKEN. THE FLASHLIGHT KEEPS FALLING OUT. R&R F/A REAR FLASHLIGHT AND CRADLE ASSEMBLY IAW AMM 33-50-16. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: DOOR — BINDING (MAIN PAX) · airframe 39,222 hrs · 35,786 cycles

UNABLE TO OPEN MAIN CABIN DOOR. HAD TO OPEN FROM OUTSIDE. PERFORMED MULTIPLE OPENING AND CLOSINGS OF MAIN CABIN DOOR. OPS CHECKS GOOD AND WITHIN LIMITS AT THIS TIME. REFERENCE AMM 52-18-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,769 hrs · 35,393 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 38,291 hrs · 34,942 cycles

MAIN DOOR EMER LAMP INOPERATIVE. R & R MAIN DOOR EMER LAMP IAW AMM 33-50-06. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,281 hrs · 34,932 cycles

AFT GALLEY WALL EMER EXT LIGHT INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY & NR 2 BATTERY PACK IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A & SN 109601.

Part: FCU — FAILED (FUEL SYSTEM) · airframe 37,818 hrs · 34,536 cycles

FUEL 1 LO LEVEL EICAS TANK 1 FUEL QTY ZERO, ABORT TAKEOFF. INSPECTED MAIN GEAR FOR A.B.T.O, NO DEFECTS NOTED. INSPECTED LT WING FOR FUEL LEAK, NO DEFECTS NOTED. TROUBLE SHOT IAW FIM 28-41-00-810-840. R & R FCU IAW AMM 28-41-01. OPERATIONS CHECKED GOOD.

Part: SPAR CAP — CRACKED (LT WING) · airframe 37,846 hrs · 34,569 cycles

LEFT WING SPAR I, LOWER SPAR CAP CRACKED AT RIB 9. REPAIRED LT WING SPAR I LOWER CAP IAW ERS-EM-57MR-572R1.

Part: SPAR CAP — CRACKED (LT WING) · airframe 37,833 hrs · 34,553 cycles

LEFT WING SPAR I LOWER SPAR CAP CRACKED AT RIB 9. REPAIRED LT WING SPAR I LOWER CAP IAW ERS-EM-57MR-572R1.

Part: UNKNOWN — LEAKING (FUEL SYSTEM) · airframe 37,668 hrs · 34,405 cycles

SMALL FUEL LEAK IN BELLY AREA. COMPLIED WITH LEAK CHECK BOTH WING TANKS & REFUEL SYS IAW AMM 28-11-00. NO LEAKAGE OR SEEPAGE NOTED AT THIS TIME. COULD NOT DUPLICATE.

Part: BRAKE ASSY — FAILED (NR 4) · airframe 37,622 hrs · 34,376 cycles

BRAKE CARBON INSPECTION DUE ON BRAKE ASSEMBLY NR 4. COMPLIED WITH BRAKE ASSEMBLY NR 4 CARBON INSPECTION & BRAKE FAILED. BRAKE ASSEMBLY NR 4 NEEDS REPLACEMENT. SEE ITEM NR 2 LOG PAGE 3962950 FOR DISCREPANCY. R & R NR 4 MLG BRAKE ASSEMBLY IAW WC 32-600-14.

Part: SIGN — INOPERATIVE (CABIN) · airframe 37,622 hrs · 34,376 cycles

FORWARD RT BULKHEAD PANEL EMER LIGHT FOUND NOT WORKING. R & R FWD RT BULKHEAD EMER EXIT SIGN IAW AMM 33-50-13, DID NOT FIX PROBLEM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,498 hrs · 34,267 cycles

LEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. R & R LT FWD EXTERIOR EMER LIGHT BULB IAW AMM TASK 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECK FAILED IAW NWRC 645-CMI-02753 FOR CORRECTIVE ACTION. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 37,490 hrs · 34,258 cycles

MAIN CABIN DOOR HARD TO CLOSE. CLEANED & LUBED MAIN DOOR CABIN ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,233 hrs · 34,024 cycles

AFT GALLEY EMER EXIT LIGHT INOPERATIVE. R & R NR 3 INVERTER. AFT GALLEY EMER EXIT LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: UNKNOWN — ODOR (HYDRAULIC BAY) · airframe 37,006 hrs · 33,791 cycles

STRONG SMELL OF FUEL BY HYD NR 2 COMPARTMENT ON SECURITY SEARCH. PERFORMED GVI OF NR 2 HYD COMPARTMENT, NO LEAKS & NO DEFECTS NOTED. COMPARTMENT LOOKS DRY & CLEAN, OK FOR SERVICE.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 36,878 hrs · 33,682 cycles

PASSENGER DOOR WILL NOT OPEN FROM THE OUTSIDE. INSPECTED & LUBED DOOR MECHANISM. PERFORMED OPERATIONS CHECK OF THE DOOR IAW AMM 52-10-01. ALL CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SOLENOID VALVE — FAILED (LANDING GEAR) · airframe 36,586 hrs · 33,415 cycles

ON CLIMB OUT, LG DID NOT REACT, AMBER DN INDICATION ON EICAS WHEN LEVER CYCLED DOWN, EICAS SHOWED GREEN DN WITH LG LEVER UP AFTER A FEW SECS, LG LEVER DISAGREE WARNING ON EICAS. R & R LG SOLENOID VLV IAW AMM 32-33-04. OPERATIONAL CHECKED GOOD, NO LEAKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,557 hrs · 33,390 cycles

12A EMER LIGHT ASSEMBLY INOPERATIVE. R & R EMER LIGHT ASSEMBLY IAW 33-50-00 AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,557 hrs · 33,390 cycles

FORWARD EMER EXIT SIGN AT 3B INOPERATIVE. R & R EMER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW 33-50-00 AMM.

Part: LIGHT — INOPERATIVE (SEATS 8-9) · airframe 36,462 hrs · 33,310 cycles

EMERGENCY LIGHT STRIP INOPERATIVE AT SEATS 8 - 9. R & R THE LIGHT STRIP IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: TRANSDUCER — FAILED (RT ENGINE) · airframe 36,432 hrs · 33,287 cycles

NR 2 ENGINE ANTI-ICE FAIL ON EICAS. COMPLIED WITH CHECKLIST. SYS RECOVERED IN ANTI-ICE OVERRIDE. VALVE MAY BE STUCK IN OPEN POSITION. REMOVED AND REPLACED THE RT ANTI-ICE TRANSDUCER IAW AMM 30-21-06.OPS CHECK GOOD.

Part: DAMPER — DIRTY (BLEED AIR SYS) · airframe 36,378 hrs · 33,239 cycles

DURING PNEUMATIC ICE TEST, GOT WING ANTI-ICE FAIL. VLV SHOWED OPEN. CLEANED NR 2 WING BLEED AIR DAMPER IAW AMM TASK 36-11-11-100-801A. OPERATIONS CHECKED GOOD IAW AMM TASK 30-00-00-70802A.

Part: FAN — FAULTY (AVIONICS BAY) · airframe 36,312 hrs · 33,188 cycles

BRIEF MILD BURNING ODOR COCKPIT, FWD ENTRY DOOR AREA. CRUISE FLIGHT & NO EICAS MSG. ODOR GONE AFTER 30 SEC. IN HEAVY RAIN. TRANSFERRED TO NRWC 645-MIA-02490. R & R LT AVIONICS EXHAUST FAN IAW MM 21-26-02.

Part: FLT CONTROLS — VIBRATION · airframe 36,215 hrs · 33,103 cycles

UNUSUAL AMOUNT OF VIBRATION FELT ON THE FLIGHT CONTROLS. DIVERTED DUE HI FREQ VIBE IN FLIGHT CONTROLS. FLIGHT CONTROLS CLIMBING THRU FL280 ALL THE WAY UP TO 360. INTERMITTENT LEVEL OFF & POWER CHANGES DID NOT CHANGE THE CONDITION. VIBRATION PERSISTED TO THE POINT OF SHAKING SEEN ON THE FLIGHT CONTROLS WHICH WAS MORE PRONOUNCED ON FIRST OFFICERS SIDE. FLIGHT ATTENDANT REPORTED VIBRATION FELT, MORE SIGNIFICANTLY BY ROW 9 & 10. ALL ENG & EICAS INDICATIONS WERE NORMAL. R & R LG SOLENOID VLV IAW AMM 32-33-04. OPERATIONAL CHECKED GOOD. SEE EASI WO 50119 FOR WORK SCOPE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 36,195 hrs · 33,091 cycles

CLIMBING FROM FL 360 TO FL 370 AUTO PRESSURE SPINED CABIN ALTITUDE TO 8300, CABIN AP TO 8:0 CABIN RATE -2500 FT THEN + 800 FT THEN CABIN ALT AP RATE WERE FLUCTUATING TALL. MANUAL MODE SELECTED. R & R AUTO PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECKED GOOD IAW AMM 21-31-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,124 hrs · 33,019 cycles

AFT GALLEY EMER EXIT SIGN INOPERATIVE. R & R AFT GALLEY EMER EXIT IAW CMM 25-31-98. OPERATIONS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 36,121 hrs · 33,018 cycles

STARTING AT 30,000 FT A BUZZING NOISE IN THE NOSE AREA UNDERNEATH THE COCKPIT FWD FLOOR, VIBRATION COULD BE FELT ON FLOOR & MODERATE VIBRATION IN CONTROL YOKE, AUTOPILOT WAS ON. BUZZING NOISE CONTINUED EVEN WHEN REDUCING SPEED, SPEED AT 30,000 FT WAS 240 - 250 KIAS. DESCENDING & REDUCING THE AIRSPEED DIDN'T CHANGE THE BUZZING OR VIBRATION. ADDING FLAPS & DEPLOYING SPEED BRAKES DIDN'T CHANGE IT. ITR REMAINED CONSTANT CONFIGURED FOR LANDING WITH GEAR & FLAPS TO 45 DEGREES. THE SOUND WASN'T AS NOTICEABLE ON APPROACH, TE VIBRATION IN THE CONTROL YOKE WASN'T AS NOTICEABLE. ON APPROACH, AUTOPILOT WAS OFF. ACFT CONTROL WAS NORMAL. VIBRATION WAS ONLY FELT IN COCKPIT AREA. FLIGHT ATTENDANT COULD NOT FEEL ANYTHING IN THE CABIN. R & R LG ACCUMULATOR THERMAL RELIEF VALVE IAW AMM 32-33-20. LEAK CHECKED GOOD.

Part: WIRE HARNESS — FAILED (NLG WOW) · airframe 36,098 hrs · 33,000 cycles

AFTER ROTATION AG AIR & GND FAIL ON EICAS. R & R NLG WOW HARNESS W019.

Part: DUCT — UNKNOWN (SUPPLY) · airframe 36,089 hrs · 32,992 cycles

AT 27,000 DURING CLIMB, FLIGHT CONTROLS SHOOK VIOLENTLY & A BUZZING NOISE. ACFT WAS TAKEN OFF AUTO PILOT, CONDITION CONTINUED. DURING DESCENT GOT WORSE. DECLARED AN EMERGENCY, AND LANDED. R & R RT SUPPLY DUCT FROM RT DTCV TO HEAT EXCHANGER.

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 36,015 hrs · 32,923 cycles

CLIMBING THROUGH FL300 AT APPROX .68M WITH AUTOPILOT ON, A SIGNIFICANT VIBRATION BEGAN IN BOTH CONTROL COLUMNS. AUTOPILOT WAS DISCONNECTED & THE VIBRATION CONTINUED. WE LEVELED OFF & SLOWED & THERE WAS NO CHANGE. WE BEGAN A DESCENT & THE VIBRATION SUBSIDED UNTIL APPROX FL270. IT CONTINUED & WAS FELT IN THE CONTROL COLUMN & RUDDER PEDALS UNTIL APPROX 8000FT & 230 KIAS. FROM THERE TO LANDING ALL CONTROLS FELT NORMAL. THE FLIGHT ATTENDANT FELT THE VIBRATION IN THE FLOOR OF THE FWD CABIN. A PILOT SITTING IN SEAT 12B NOTICED AN AIRFRAME VIBE. ACCOMPLISHED VIBRATION DVI IAW WC 12-200-01. NO DEFECTS NOTED AT THIS TIME. FCF FOUND SATISFACTORY.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 35,483 hrs · 32,479 cycles

RIGHT OVERWING AFT EMER LIGHT INOPERATIVE. R & R RT OVERWING AFT EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECK IS GOOD.

Part: DISPLAY — OVERHEATED (COCKPIT) · airframe 35,374 hrs · 32,404 cycles

AT CRUISE, GOT BAG DOOR OPEN MSG FOLLOWED BY STRONG ELEC BURNING SMELL. COCKPIT WINDOWS FOGGED UP BUT DID NOT DEPRESSURIZE. FLIGHT ATTENDANT & SOME PAX SMELLED THE ODOR. NO SMOKE WAS DETECTED. PERFORMED OPERATIONS CHECK OF BAGGAGE DOOR IAW AMM 52-76-01. OPERATIONS CHECKED GOOD AT THIS TIME. REF LOG PAGE 3664795 ITEM 1. DURING TROUBLESHOOTING FOUND PFD NR 1 OVERHEATING CONTINUOUSLY. SWAPPED CAPTAIN'S PFD NR 1 WITH FIRST OFFICER'S MFD DISPLAY NR 2. PFD NR 1 OPERATIONS CHECKED GOOD IAW AMM 34-22-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,366 hrs · 32,398 cycles

ELECTRICAL BURNING SMELL IN COCKPIT. FOUND ALL AVIONICS HAD BEEN ON AWHILE. PERFORMED GVI OF COCKPIT & FWD AVIONICS BAY, NO BURNING SMELL DETECTED.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 35,358 hrs · 32,391 cycles

MAIN CABIN DOOR HARD TO CLOSE.

Part: CONTROL CABLE — UNKNOWN (CONTROL COLUMN) · airframe 35,356 hrs · 32,390 cycles

VIBRATIONS FELT IN CONTROL COLUMN & FLOOR, HEARD AT FL280 & DOWN TO 7000 FT. NO CHANGE WITHOUT AUTO PILOT OFF. REMOVED AND REPLACED THE RT AFT OUTBD ELEVATOR CONTROL CABLE IAW AMM 27-31-01 AND RT ELEVATOR TENSION REGULATOR IAW AMM 27-31-01.

Part: CONTROL CABLE — DEFECTIVE (ELEVATOR) · airframe 35,356 hrs · 32,390 cycles

VIBRATIONS FELT IN CONTROL COLUMN & FLOOR & HEARD AT FL 280 DOWN TO 7000 FT. NO CHANGE WITH AUTOPILOT OFF. REPEAT GRIPE. R & R RT AFT OTBD ELEVATOR CONTROL CABLE IAW AMM 27-31-01. R & R RT ELEVATOR TENSION REGULATOR IAW AMM 27-31-01. SEE NRWCS 645-ABI-02120 & 645-ABI-02121 FOR ADDITIONAL DETAILS & BILLING.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,112 hrs · 32,162 cycles

GALLEY CABIN PARTITION EMER EXIT SIGN INOPERATIVE. R & R GALLEY CABIN PARTITION EMER EXIT SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (DOOR FRAME) · airframe 34,893 hrs · 31,996 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN & CLOSE. LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: CONTROL COLUMN — VIBRATION (COCKPIT) · airframe 34,894 hrs · 31,998 cycles

FLIGHT CREW HEARD LOUD BANG FOLLOWED BY VIBRATION IN CONTROL COLUMN TRANSFERRED TO NRWC 645-DFW-01999. VIBRATION INSPECTION IAW WC 12-200-01, NO ABNORMAL DEFICIENCIES NOTED. THIS ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY & FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

DURING HMBV INSPECTION, QA FOUND AFT FUSELAGE SKIN CRACKED AT FASTENER AREA FRAME 75 & STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. PERFORMED PERMANENT REPAIR ON AFT FUSELAGE SKIN CRACK AT FASTENER AREA IAW ERS-EM-53MR-674. REPAIR MATERIALS FILLER AL CLAD 2024-T3 0.063 INCHES, DOUBLER AL CLAD 2024-T3 0.080 INCHES, ANGLE AL CLAD 2024-T3 0.063 INCHES & ANGLE FILLER AL CLAD 2024-T3 0.032 INCHES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

DURING HMBV INSPECTION, QA FOUND AFT FUSELAGE SKIN CRACKED AT FASTENER AREA FRAME 75 & STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-666.

Part: GUSSET — GOUGED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 61 CEILING PANEL GUSSET BETWEEN STRINGER 3R & 4R GOUGED. ACFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. PERFORMED PERMANENT REPAIR ON FRAME 61 CEILING PANEL GUSSET BETWEEN STRINGER 3R & 4R IAW ERS-EM-53MR-646. REPAIR MATERIALS DOUBLER, 7475T761 040.

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 34,669 hrs · 31,808 cycles

LEFT EMER EXIT CORRODED UNDER LOWER BONDING TAB MARKED. REPAIRED LT EMER EXIT UNDER LOWER FWD GUIDE IAW ERS-EM-5200-187.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

AFT FUSELAGE LT SKIN CRACKED AT FASTENER FRAME 75 STRINGER 2L. DAMAGED SECTION OF SKIN AT FRAME 75 STRINGER 2L AREA WILL BE CUT OUT, DOUBLER & FILLER WILL BE INSTALLED USING ETD2014-145-062647, SEE NRTC E399825.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

RIGHT HAT BEAM INBD SUPPORT CRACKED BETWEEN FRAME 47 & 48 MARKED. R & R RT HAT BEAM INBD SUPPORT IAW SRM 51-40-02.

Part: SPAR — CORRODED (RT WING) · airframe 34,669 hrs · 31,808 cycles

RIGHT WING SPAR 3 HAS CORROSION ON AFT SIDE ON LG HARNESS PASS THROUGH CUT OUT. BLENDED AS REQUIRED TO REMOVE CORROSION FROM RT WING SPAR 3 AFT SIDE ON LG HARNESS PASS THROUGH CUT OUT IAW SRM 51-10-03. UT CHECK INDICATES 0.228 INCHES REMAINING THICKNESS, DAMAGE IS ACCEPTED AS IS IAW ERS-EM-5700-199.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 34,669 hrs · 31,808 cycles

RIGHT OMEGA BEAM GUSSET CORRODED AT FRAME 61, 60 & 59 MARKED. R & R RT OMEGA BEAM GUSSET AT FRAME 61, 60 & 59 IAW SRM 51-40-02.

Part: GRILL — DAMAGED (AC PACK) · airframe 34,137 hrs · 31,315 cycles

AFTER WE LEVELED OFF AT CRUSE AT FL 270 & BEGAN ACCELERATING THROUGH ABOUT 280 KIAS WE HEARD A VIBRATION THAT WAS LOUDER THAN NORMAL, ALSO FOUND A STRONG RAPID VIBRATION IN BOTH CONTROL YOKES. SLOWED ACFT TO ABOUT 240 KIAS WHICH LESSENED THE STRENGTH OF THE VIBRATIONS BUT THEY NEVER WENT AWAY COMPLETELY. LANDED IN HOU WITHOUT ANY FURTHER PROBLEMS. PERFORMED ACFT VISUAL INSPECTION & FOUND RT PACK EXHAUST GRILL BADLY DAMAGED. R & R RT SIDE EXHAUST GRILL IAW AMM 20-10-05.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 34,031 hrs · 31,206 cycles

FLIGHT ATTENDANT`S FLASHLIGHT MISSING. REPLACED FLIGHT ATTENDANT`S FLASHLIGHT IAW STANDARD PRACTICES.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 33,971 hrs · 31,148 cycles

CAPTAIN SIDE COCKPIT FLASHLIGHT INOPERATIVE. REPLACED CAPTAIN FLASHLIGHT IAW 33-50-16.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,718 hrs · 30,925 cycles

EXIT SIGN INOPERATIVE AT ROW 3B ON AFT GALLEY WALL. R & R NR 2 EMERGENCY POWER SUPPLY BATTERY & CHARGER ASSEMBLY IAW WC 33-700-19, OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 33,718 hrs · 30,925 cycles

EXIT SIGN INOPERATIVE AT RT INTERIOR OVERWING DOOR WALL. R & R INVERTER NR 5 IAW AMM 33-50-11, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,512 hrs · 30,749 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FA JUMPSEAT) · airframe 32,993 hrs · 30,363 cycles

F/A FLASHLIGHT ABOVE JUMPSEAT NOT CHARGING. R & R FLASHLIGHT IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: CRADLE — FAILED (AFT FLASHLIGHT) · airframe 32,069 hrs · 29,614 cycles

CREW REPORTED THE REAR FLASHLIGHT HOLDER WAS INOPERATIVE. FLASHLIGHT FALLS OUT. ACFT REMOVED FROM SERVICE. R & R AFT FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 31,712 hrs · 29,307 cycles

THE CREW REPORTED THAT AFTER APPROX 1 HOUR OF CRUISE FLIGHT AT 36000 THEY RECEIVED AN EICAS MESSAGE "HYD 1 LOW LEVEL". THE MESSAGE EXTINGUISHED WITH GEAR EXTENTION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. SERVICED NR1 HYD SYS TO 5 QUARTS. NO LEAKS NOTED IAW AMM 12-13-01. THE ACFT OK FOR SERVICE.

Part: CONNECTOR — DIRTY (EXIT SIGN) · airframe 31,369 hrs · 29,023 cycles

ON FLIGHT 4313 THE CREW REPORTED ONE EMERGENCY EXIT SIGN ON THE EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND RE-RACKED CONNECTOR. PERFORMED TEST IAW EMB145 AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — SHEARED (RT MLG) · airframe 31,149 hrs · 28,843 cycles

ON FLIGHT 2936 THE CREW REPORTED THE RIGHT MAIN INBOARD WHEEL BOLT AND NUT SHEARED OFF AT LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN LANDING GEAR WHEEL ASSEMBLY IN REF TO CARD NO 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,483 hrs · 28,303 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT DOOR LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 30,012 hrs · 27,899 cycles

ON FLIGHT 3373 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED ROLLER IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 29,992 hrs · 27,877 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE LOWER FORWARD ENGINE MOUNT FORWARD YOLK FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LEFT ENGINE LOWER FORWARD ENGINE MOUNT FORWARD YOLK FITTING IAW AEA EO-EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 30,012 hrs · 27,899 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM FRAME BETWEEN 47 AND 48 LOWER FLANGE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OMEGA BEAM FRAME BETWEEN 47 AND 48 LOWER FLANGE IAW EMB SRM 53-23-02 AND 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,012 hrs · 27,899 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,993 hrs · 27,877 cycles

RT GALLEY OMEGA BEAM CORRODED AFT OF FR-18 AT SCREW HOLE. REPAIRED OMEGA BEAM IAW AE EO EM-53MR-2022.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,992 hrs · 27,877 cycles

DURING MAINTENANCE INSPECTION, FOUND RIGHT GALLEY OMEGA BEAM CORRODED AFT OF NR 18 SCREW HOLE. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED EO-EM-53MR-2022. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 29,992 hrs · 27,877 cycles

REAR ELECTRONICS COMPARTMENT ACCESS HATCH 272DR INNER FRAME CRACKED AT HINGE PIN FITTING. REPAIRED REAR ELECTRONICS COMPARTMENT ACCESS HATCH 272DR IAW EO-EM-52MR-325.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 29,993 hrs · 27,877 cycles

SHEAR TIE AT FRAME 65 CORRODED ABOVE STRINGER 18L. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 29,760 hrs · 27,691 cycles

DURING B INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT CRADLE DOES NOT HOLD FLASHLIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,574 hrs · 27,539 cycles

ON FLIGHT 3927 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF FLASHLIGHT. SECURED CAPTAIN’S FLASHLIGHT IN CRADLE AS REQUIRED. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — DEFECTIVE (BLEED AIR SYS) · airframe 29,512 hrs · 27,495 cycles

ON FLIGHT 4095 THE CREW REPORTED THAT DURING CLIMBOUT THROUGH 10500 FEET RECEIVED A BLEED 2 LEAK MESSAGE ON EICAS. THE CREW COMPLIED WITH AOM 1 PROCEEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BLEED TUBE ASSEMBLY IAW AMM 36-11-09. NO LEAKS NOTED, THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,771 hrs · 26,931 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHTS AT COCKPIT STEP AND GALLEY OVERHEAD CEILING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11 IAW W/C 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (COCKPIT STEP) · airframe 28,525 hrs · 26,748 cycles

DURING B-INSPECTION FOUND THE COCKPIT STEP PANEL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT STEP EMRGENCY EXIT SIGN IAW EMB 145 AMM 33-50-13 AND OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 28,469 hrs · 26,695 cycles

DURING B-INSPECTION, FOUND THE EMERGENCY EXIT SIGN BELOW THE COCKPIT DOOR IS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE CONNECTOR, CONNECTED IAW AWM 20-50-00. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (COCKPIT) · airframe 27,978 hrs · 26,334 cycles

DURING MAINTENANCE VISIT FOUND THE COCKPIT EMERGENCY EXIT STEP IDENTIFIER SIGN IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED CONNECTOR FOR BATTERY CHARGER NR 1 IAW EMB 145 AMM 33-50-04. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,978 hrs · 26,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CEILING EMERGENCY EXIT INDENTIFIER SIGN NEXT TO THE GALLERY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED CONNECTOR FOR BATTERY CHARGER NR 2 IAW EMB 145 AMM 33-50-04. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 27,896 hrs · 26,271 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S S FLASHLIGHT HOLDER ASSEMBLY IAW EMB 145 AMM TASKS 33-50-16-000-801-A & 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,288 hrs · 25,838 cycles

ON FLIGHT 4371 THE CREW REPORTED EMERGENCY LIGHTS FROM 8-12 ILLUMINATED WHEN POWER WAS REMOVED FROM AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — DAMAGED (RT WING) · airframe 26,731 hrs · 25,391 cycles

DURING MAINTENANCE BASE PHASE 4 INSPECTION FOUND THE RIGHT WING RIB 5 AT AFT HAD A LIGHTNING STRIKE HOLE CRACKED ABOUT 2.5 INCHES LONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT WING RIB 5 AT AFT LIGHTNING HOLE IAW EO EM- 57MR-551 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: NONE — NONE (NONE) · airframe 25,492 hrs · 24,440 cycles

FLT 3207: ON TAKE OFF, CREW REPORTED A POSSIBLE BIRDSTRIKE. INFLIGHT AT FLIGHT LEVEL 370. HEARD TWO NOTICEABLE BANGS, COULD HEAR AS WELL AS FEEL COMING FROM NOSE AREA 3. CAPTAIN DECLARED AN EMERGENCY & DIVERTED. DURING APPROACH NOTICEABLE VIBRATIONS ON CONTROL COLUMN. ACFT LANDED WITHOUT INCIDENT. ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH VIBRATION INSPECTION DVI- IAW MNTC W/C 1220001. FOUND BIRD STRIKE ON RT OUTER UPPER ELEVATOR, NO DAMAGE NOTED AT THIS TIME. ACFT INSPECTED FOR A FERRY FLT & FOUND TO BE IN SAFE CONDITION. R & R HIGH STAGE PRESSURE SWITCH. R & R PRECOOLER FAN AIR VALVE. R & R SENSOR. R & R VALVE OUTLINE. ACFT RETURNED TO SERVICE. (NO DAMAGE FOR BIRDSTRIKE, NO SDR)

Part: COVER — DEFECTIVE (PAX DOOR) · airframe 24,340 hrs · 23,539 cycles

ON FLIGHT 3948 DURING INSPECTION FOUND THE COVER ON THE PASSENGER DOOR HANDLE PREVENTED THE DOOR FROM OPENING ALL THE WAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. TRIMMED THE TOP PORTION OF COVER ON PASSENGER DOOR SO IT NO LONGER INTERFERES WITH DOOR OPERATION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,767 hrs · 23,080 cycles

DURING FLIGHT 3892 THE CREW REPORTED THAT THE EMERGENCY LIGHTS FLOOR STRIPS IN POSITION’S 6, 7 AND 8 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 1 EMERGENCY BATTERY ASSEMBLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: A/C PACK — SMOKE (NR 2) · airframe 20,409 hrs · 20,140 cycles

ON FLIGHT 3488, CREW REPORTED WITH APU RUNNING AND NR 2 PACK OPERATING SMOKE IN CABIN AND PACK 2 OVERHEAT. MEL ISSUED

Part: CONTROLLER — FAILED (ZONE 200) · airframe 16,582 hrs · 16,538 cycles

LOST PRESSURIZATION INDICATION, UNABLE TO RE-PRESSURIZE IN MANUAL OR AUTO, RETURNED TO ROW. REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB AMM 21-31-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (FLAP CONTROL SYS)

FLAP LOW SPEED MESSAGE DURING DESCENT FOLLOWED BY STALL PROTECTION SYSTEM ADVANCED MESSAGE. REPLACED FECU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHT STRIPS 1-3 WILL NOT REMAIN ON. REPLACED NR 2 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. FABRICATED A DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200505716) (K)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. ALODIZED AND APPLIED EPOXY TO THE REWORKED AREA. FILL THE BLENDED AREA WITH HYSOL EA AND APPLIED PRIMER AFTER CURING. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW212005716) (K)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ORD - FLT 4202 - DURING APPROACH CREW REPORTED AN E1 REV FAIL INDICATION FOLLOWED BY ENGINE ONE STARTING TO SPOOL UP AND DOWN. CREW COMPLIED WITH AOM PROCEDURES AND SHUT DOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY IN ORD WITH NO OTHER INCIDENTS NOTED. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142 REV 21, CHAPTER 51-40-02 AND CPM 51-21-04/06 AND 51-61-00. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR CENTER SILL IAW EMB145 SRM AND EMB REPAIR STATEMENT GST-3309/01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - FOUND GALLEY AFT DIGITAL CORRODED. REPAIRED GALLEY DIGITAL IAW EMB 145 REPAIR STATEMENT GST 3309/01. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. AFT DIAMOND GUSSET CORRODED IN GALLEY AREA. INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING ON CORROSION REPAIR ITEM CARD NR 27528. PAX DOOR AFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICE PAX DOOR AFT SILL IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. FORWARD DIAMOND GUSSET CORRODED IN GALLEY AREA. INSTALLED SERVICEABLE DIAMOND FORWARD GUSSET IAW EMB145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING ON A CORROSION REPAIR ITEM. SERVICE DOOR FORWARD SILL HAS CORROSION. PERFORMED EDDY CURRENT AND THICKNESS CHECK, NO DEFECTS NOTED. INSTALLED REPAIR DOUBLER ON SERVICE DOOR FORWARD SILL IAW EMB GST-3309/01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING ON A CORROSION REPAIR ITEM CARD NR 27521. CORROSION HAS BEEN FOUND ON GALLEY FORWARD DIGITAL. REPAIRED FORWARD DIGITAL IAW EMB GST-3309/01. (M)

Part: FITTING — CORRODED (HORIZ STAB)

ABI - FOUND CORROSION AND GOUGES ON RIGHT HORIZONTAL STABILIZER FITTING BEARING MATING SURFACE. REPAIRED RIGHT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING IAW EMB145 SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA FLOOR BEAM AT FRAME 20. REPAIRED LEFT OMEGA FLOORBEAM IAW EMB 145 SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - FOUND SERVICE DOOR AFT SILL CORRODED. REPAIRED SERVICE DOOR AFT SILL IAW EMB REPAIR STATEMENT GST-3308/01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - FOUND GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: CAP — CORRODED (RT MLG)

ABI - FOUND RIGHT MAIN LANDING GEAR SWIVEL BEARING CAPS CORRODED. REMOVED AND REPLACED RIGHT MLG SWIVEL BEARING CAPS IAW EMB 145 AMM. (M)

Part: CAP — CORRODED (LT MLG)

ABI - FOUND LEFT MLG SWIVEL BEARING CAPS CORRODED. REMOVED AND REPLACED LEFT MLG BEARING CAPS IAW EMB 145 AMM. (M)

Part: CAP — CORRODED (NLG)

ABI - FOUND NOSE LANDING GEAR BEARING CAPS CORRODED. REMOVED AND REPLACED NLG BEARING CAPS IAW EMB 145 AMM. (M)

Part: PROBE — INOPERATIVE (NR 2)

ORD - FLT 4003 - DURING CRUISE FLIGHT, THE RIGHT TAT HEAT FAILED. THE FLT WAS RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACED THE NR 2 TAT PROBE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FAN — BURNED (CABIN)

FWA - FLT 3418 - CREW REPORTED FUEL SMELL IN CABIN WITH ANTI-ICE SELECTED ON. MAINTENANCE COULD NOT DUPLICATE FUEL SMELL. MAINTENANCE FOUND THE GASPER FAN TO BE EMITTING FUMES. GASPER FAN WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DUCT — LOOSE (A/C PACK)

LBB - FLT 3819 - DURING APPROACH CREW REPORTED ELECTRICAL SMOKE SMELL IN CABIN. CREW DESELECTED RECIRCULATION FAN, SMELL DISIPATED. AIRCRAFT ARRIVED AT GATE WITH NO FURTHER INCIDENTS. INSPECTION FOUND PACK DUCT LOOSE. RECONNECTED DUCT, PERFORMED OPS CHECK. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 6)

ORD - FLT 4259 - EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 6. REMOVED AND REPLACED POWER SUPPLY NR 3 AND 4. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 6)

FLT 4259 - ORD - EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 6. REMOVED AND REPLACED POWER SUPPLY NR 3 AND 4. OPS CHECK GOOD. REF SIMA0861. (M)

Part: WIRE — DISCONNECTED (ROW 18)

ORD - FLT 4054 - EMERGENCY LIGHT OUT AT 12 B/C. FOUND WIRES DISCONNECTED FROM LIGHT. REATTACHED SAME, OPS CHECK GOOD. (M)