N669MB

Part: UNKNOWN — ODOR (CABIN) · airframe 46,771 hrs · 43,895 cycles

STRONG FUME SMELL AT GATE, PACKS ON & APU BLEED. INSPECTED BOTH PACKS. NO DEFECTS NOTED. RAN GROUND AIR AND BOTH PACK OFF APU. NO SMELL DETECTED. A/C OK FOR SERVICE.

Part: UNKNOWN — FUMES (CABIN) · airframe 46,737 hrs · 43,856 cycles

WHILE ON APU BLEED, EXHAUST FUMES NOTED ON AIRCRAFT. CLEARED ON ENGINE BLEED. OPERATED PACKS ON APU BLEED IRT TO AMM TASK 21-20-00-700-801-A. NO EXHAUST SMELL NOTED. CLEAR MEL.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,660 hrs · 43,758 cycles

CREW REPORTED FUEL SMELL IN CABIN DURING DEPLANING WITH ENGINES OFF AND APU RUNNING BOTH PACKS. CREW SHUT OFF PACKS AND REPORTED NO GSE EQUIPMENT AROUND A/C WITH NO DEFECTS NOTED ON POST FLIGHT WALKAROUND. CREW SELECTED PACK 1 FOLLOWED BY PACK 2 WITH NO FUEL SMELL NOTED. CREW SHUTDOWN APU AND REPORTED SLIGHT HINT OF FUEL SMELL. RESTARTED APU AND RAN BOTH PACKS WITH NO FUEL SMELL IN A/C.

Part: ENGINE — SMOKE (NR 2) · airframe 46,509 hrs · 43,591 cycles

AFTER E-2 SHUTDOWN THERE WAS SMOKE OUT THE EXHAUST WITH A SMOKEY SMELL IN THE CABIN. COULD NOT DUPLICATE E2 SMOKE, SEE SEQ #2 FOR DMT. FOUND APU LEAKING OIL, SEE SEQ #3 FOR APU MEL. RAN PACKS AS REQ NO MORE OIL SMELL. A/C OK FOR SERVICE

Part: A/C PACK — ODOR (NR 1) · airframe 46,476 hrs · 43,547 cycles

MELTING PLASTIC SMELL IN FLIGHT DECK. AIR CONDITIONING PACKS NOTE: FOUND TO BE PACK 1 ACM. INSPECTED #100 ACM AND PACK SYSTEMS, RAN PACK 1 FOR 30 MINUTES COULD NOT DUPLICATE. THIS CLEARS MEL 21-15-2.

Part: SWITCH — FAILED (ZONE 700) · airframe 46,325 hrs · 43,369 cycles

ON TAKEOFF, A/C HAD LG AIR/GND FAIL MSG ON EICAS. LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FACT 03JUN25 06:49 MDT FOUND WOW PROX SWITCH CMC MESSAGES FOR NLG AND RH AND LH MLG.R&R'D NLG WOW PROX SWITCH IRT AMM 32-63-02. R&R'D RH AND LH WOW #2 PROX SWITCHES IRT AMM 32-63-01. ADJUSTED MLG PROX SWITCHES IRT AMM 32-63-05. OPS CHECK GOOD IRT AMM 32-30-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,204 hrs · 43,222 cycles

CREW REPORTS FUMES IN FLIGHT DECK AT GATE. UPON ARRIVAL NO FUME SMELLED IN COCKPIT WITH NO CHANGE OTHER THAN APU ON/OFF. RAN APU WITH PACKS 1/2 IN VARIOUS CONFIGURATIONS. WPU ON AND PACKS ON/OFF TRIED TO LOCATE ANY CUPRIT OF FUMES NONE LOCATED. FLIGHT DECK CLEAR OF ANY UNNORMAL ODERS. OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 46,093 hrs · 43,113 cycles

SLIGHT BURNING ODOR AFTER POSSIBLE LIGHTNING STRIKE PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM 05-30-01. NO ENTRY OR EXIT POINT FOUND. RAN BOTH PACKS OFF APU. NO DEFECTS NOTED OR SMELL NOTED AT THIS TIME. A/C OK FOR SERVICE AT THIS TIME.

Part: NONE — NONE (NONE) · airframe 45,550 hrs · 42,535 cycles

EXHAUST SMELL IN CABIN WITH PACK 2 RUNNING. FACT 17DEC24 10:46 ROA REF LOG PAGE 305438-1 APU CAUSING EXHAUST SMELL OPS CHECK GOOD WITH ENGINES

Part: CABIN AIR SYS — ODOR (ZONE 100) · airframe 45,550 hrs · 42,535 cycles

STRONG EXHAUST FUMES FROM PACKS DURING OPERATION ( P/C C/B C30 AND E6) MEL 17DEC24 09:40 ROA C35206 49-1 APU AUXILIARY POWER UNIT

Part: UNKNOWN — ODOR (CABIN) · airframe 45,503 hrs · 42,475 cycles

BURNING OIL SMELL THROUGHOUT FLIGHT DECK AND CABIN WHEN APU IS ON. FACT 07DEC24 21:58 PHL RAN BOTH PACKS ON APU BLD AND ENGINE BLDS 1 AND 2 INDEPENDENTLY NO ABNORMAL SMELLS NOTED DURING TEST PACKS FUNCTION AS INTENDED OK FOR SERVICE AT THIS TIME

Part: BUSHING — DAMAGED (ZONE 800) · airframe 45,500 hrs · 42,472 cycles

52-2455 BUSHING ELONGATED ON SIDE-HINGED MAIN DOOR ROTATING ARM LWR BUSHING HOUSING, AT UPPER LUG LWR SURFACE. REPAIRED IAW EO1-52-24-0701

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2452 RH FLT DECK LATERAL SIDE ANGLE CRACKED AT FR10. RAR ANGLE IAW SRM 51-40-02

Part: HINGE FITTING — CRACKED (ZONE 600) · airframe 45,500 hrs · 42,472 cycles

57-2441 RH OB FLAP SHROUD, IB HINGE AFT SECTION LUG CRACKED. RAR HINGE IAW SRM 51-40-02 AND AMM20-10-01

Part: LUG — OUT OF LIMITS (RUDDER) · airframe 45,500 hrs · 42,472 cycles

55-2428 RUD II, TOP CTR BRACKET LUG IS OUT OF LIMITS. RAR BRACKET IAW SRM 51-40-02 AND EO1-55-24-0699

Part: FRAME — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2397 LH COCKPIT, LATERAL SIDE FRAME CRACKED AT FR10. RAR SIDE FRAME IAW SRM 51-40-02

Part: BUSHING — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

55-2395 HORIZONTAL STAB, LH HINGE FITTING HAS ALL BUSHINGS CORRODED. REPAIRED IAW EO1-55-24-0678

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2404 FLT DECK LATERAL SIDE ANGLE AT FR 10 IS CRACKED. RAR ANGLE IAW SRM 51-40-02

Part: WINDOW POST — NOT REPORTED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2370 LH WINDSHIELD TOP PILLAR REINFORCEMENT HAS 7 HOLES NOT COLD WORKED. REPAIRED IAW EO1-53-24-0677

Part: SUPPORT — MECHANIC ERROR (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2337 FR27 MISDRILLED AT FAIRLEAD SUPPORT BTW STR20-21R. REPAIRED IAW EO1-53-24-0675

Part: TORQUE BOX — CRACKED (ZONE 500) · airframe 45,500 hrs · 42,472 cycles

57-2355 NDT CRACK INDICATION ON IB FWD HOLE OF LH WING TQ BOX. REPAIRED IAW EO 1-57-24-0673

Part: BUSHING — MIGRATED (ZONE 300) · airframe 45,500 hrs · 42,472 cycles

55-2336 HORIZONTAL STAB, RH HINGE BUSHING MIGRATED. REPAIRED IAW EO1-55-24-0678

Part: SKIN — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2211 CRACK ON BLEND OF FUSE SKIN BTW FR23-24 BTW STR20-21L. REPAIRED IAW EO1-53-24-0271

Part: SKIN — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2212 FUSELAGE SKIN BLEND IS CRACKED AT BTW FR26-27 AT STR21L. REPAIRED IAW EO1-53-24-0700

Part: SUPPORT ANGLE — CHAFED (NOT REPORTED) · airframe 45,500 hrs · 42,472 cycles

53-2163 CTR FUSE 3, BLEED SYSTEM SUPPORT AFT ANGLE CHAFFED. RAR SUPPORT ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,472 cycles

53-2167 CTR OMEGA BEAM CORRODED AT BTW FR18-20. REPAIRED IAW EO 1-53-24-0681

Part: PROFILE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2165 CF1, FLOOR LEVEL T PROFILE CRACKED. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2127 SHEAR CLIP CRACKED AT FR56 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FRAME — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2120 FR 59 CRACKED BTW STR15-16L. REPAIRED IAW EO1-53-24-0661

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2129 SHEAR CLIP CRACKED AT FR59 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2128 SHEAR CLIP CRACKED AT FR58 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: GUSSET — CORRODED · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2126 LH GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,500 hrs · 43,472 cycles

53-2124 CTR GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2096 RH SILL CORRODED BTW FR19-20. RAR SILL IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 800) · airframe 45,500 hrs · 42,472 cycles

53-2077 CARGO DOOR MECHANISM SUPPORT BRACKET CRACKET AT STR5R BTW FR67-68. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2084 CARGO ENTRY, FR67 LWR POST UPPER SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2094 LH OMEGA BEAM CRACKED AT FR21,22,23. REPAIRED IAW EO1-53-24-0662

Part: POST — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2082 CARGO ENTRY, FR67 LWR POST CRACKED. RAR LWR POST IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2098 CTR GUSSET CORRODED BTW FR20-23. RAR GUSSET IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2078 CARGO DOOR MECHANICAL VERTICAL SUPPORT BRACKED CRACKED BTW FR67-68 BTW STR4-5R. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2095 FWD UDERFLOOR DIGITAL CORRODED. REPAIRED IAW ESR1-53-24-004. TRACKED REPAIR ON EO1-05-24-0650

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2079 SHEAR CLIP CRACKED AT FR67 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ATTACH BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 45,500 hrs · 42,472 cycles

53-2089 RH WING, WING TO BODY FAIRING ATTACH BRACKET #2 CRACKED JUST AFT OF SPAR 2. RAR ATTACH BRACKET IAW SRM 51-40-02

Part: POST — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2080 CARGO ENTRY, FR66 LWR POST CRACKED. RAR POST IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2075 SHEAR CLIP CRACKED AT FR61 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2083 CARGO ENTRY, FR67 LWR POST SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2081 CARGO ENTRY, FR66 LWR POST SUPPORT BRACKET CRACKED. RAR SUPPORT BRACKET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2072 SHEAR CLIP CRACKED AT FR71 BTW STR5-6L. RAR SHEAR CLIP IAW SRM 51-40-02 AND EO1-53-24-0679

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2049 SHEAR CLIP CRACKED AT FR26 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: DOUBLER — DENTED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2045 DENT AT FWD OF REPAIR DOUBLER AT BTW FR24-25 AT STR21L.. REPAIRED IAW EO1-53-24-0666

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2060 LH OMEGA BEAM IB FLANGE CRACKED AT FR36. REPAIRED IAW EO1-53-24-0670

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2048 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2052 SHEAR CLIP CRACKED AT FR28 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2056 CTR OMEGA BEAM CRACKED AT FR29. REPAIRED IAW EO1-53-24-0688

Part: FRAME — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2047 FR25 CRACKED UNDER SILL BTW STR15-16R. REPAIRED IAW EO1-53-24-0663

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2071 RH SHEAR CLIP CRACKED AT FR73 BTW STR8-10R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2055 CTR OMEGA BEAM CRACKED AT FR28. REPAIRED IAW EO1-53-24-0668

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2063 RH SILL CORRODED AT BTW FR41-48. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2063 CORROSION ON RH SILL BTW FR41-48. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2054 LH OMEGA BEAM CRACKED AT FR29. REPAIRED IAW EO1-53-24-0691

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2053 LH OMEGA BEAM CRACKED AT FR28. REPAIRED IAW EO1-53-24-0667

Part: FRAME — CRACKED (ZONE 100) · airframe 45,500 hrs · 42,472 cycles

53-2009 CRACK ON FR4 IN BATTERY COMPARTMENT BTW STR19-20L. REPAIRED IAW ETD 2024-145-030671 AND EO1-53-24-0680

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2015 FUSELAGE SKIN CORRODED AROUND HEATED WATER DRAIN AT BTW FR60-61. REPAIRED IAW ETD2024-145-029497 AND TRACKED WITH EO1-05-24-0650

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 45,500 hrs · 42,472 cycles

53-2012 TOILET WASTE VALVE SUPPORT CORRODED. RAR SUPPORT IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 45,500 hrs · 42,472 cycles

53-2013 EXTERNAL SKIN CRACKED AROUND FASTENER AT FR77 BELOW STR8R. REPAIRED IAW EO 1-53-24-0683

Part: DUCT — MELTED (ZONE 100)

ODD ODOR IN AIRCRAFT WITH APU RUNNING WHILE ON THE GROUND. (NOTE: FOUND PACK 1 BLACK DUCTS MELTED.)

Part: DUCT — MELTED (ZONE 100) · airframe 45,295 hrs · 42,226 cycles

ODD ODOR IN AIRCRAFT WHILE APU RUNNING ON THE GROUND. FOUND 3 DUCTS MELTED ON DUAL TEMP CONTROL VALVE #100. R&R 3 DUCTS IRW AMM 21-60-01 LEAK CHECK OPS CHECK GOOD, NO ODOR NOTICED IN CABIN OR COCKPIT.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,015 hrs · 41,896 cycles

CREW ARRIVED AT THE A/C, POWERED ON AND OBSERVRED PLASTIC/ACRID SMELL WITH EITHER PACKS RUNNING. SMELL DISSIPATES WITH PACKS OFF. FACT 12JUN24 22:54 CLT RAN PACKS HOT AND COLD FOR 30 MINS, NO SMELLS NOTED. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,963 hrs · 41,837 cycles

FUEL SMELL IN CABIN AND FLT DECK WITH BOTH PACKS RUNNING ON APU BLEED ONLY. NO SMELL WHEN PACKS ON WITH ENGINE BLEEDS. FACT 03JUN24 17:04 PHL MX RAN APU & BOTH PACKS FOR 10-15MINS. NO OBVIOUS FUEL SMELLS DETECTED. INSPECTED APU UNIT FOR LEAKS DURING RUN, NONE NOTE. A/C OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,472 hrs · 40,181 cycles

DURING GROUND STOP IN PHF WITH CREW ON A/C, WITH NO PAX ONBOARD. AIRCRAFT WAS BEING POWERED BY GPU WITH APU CURRENTLY ON MEL. AIRCRAFT REACTED AS IF GPU POWER WAS DISCONNECTED WITH NO INPUT FROM CREW OR GROUND PERSONNEL. THEN RAMP PERSONNEL NOTIFIED CREW OF A FIRE FROM GPU RECEPTACLE. CREW EVACUATED A/C AND GOT GPU DISCONNECTED FROM A/C. ONCE DISCONNECTED FIRE DISSIPATED. WHEN FIRE CREW ARRIVED AT THE A/C THEY NOTICED SMOKE COMING FROM THE BATTERY COMPARTMENT. AS A PRECAUTION A/C MAIN BATTERIES WERE DISCONNECTED. PERFORMED DVI, FOUND OVERHEAT DAMAGE TO GPU RECEPTACLE INSERT PANEL AND A/C SKIN DIRECTLY ABOVE GPU RECEPTACLE. SEE LP 284136-2 AND -3 FOR DISCREPANCY.

Part: NONE — NONE · airframe 40,448 hrs · 36,916 cycles

SMOKE AND SMELL IN FLIGHT DECK IN ICING. WINDSCREENS SEEM DISCOLORED AT BOTTOM OF CENTER POST NO RELEVANT EICAS MESSAGES APPEARED DURING EVENT.

Part: WARNING MESSAGE — ILLUMINATED (AC BUSS) · airframe 41,753 hrs · 38,284 cycles

115V AC OFF BUSS MESSAGE DURING T/O ROLL AT ABOUT 75 KTS. T/O ABORTED AND MESSAGE CLEARED WITH NO ACTION TAKEN. CREW FOLLOWED QRH AND RESET BUSS AS PRECAUTION. IRREGULARITY CLEARED USING NORMAL CREW PROCEDURE.

Part: NONE — NONE · airframe 41,720 hrs · 38,249 cycles

BAG BAY SMOKE INDICATION ON EICAS, FA INSP NO FIRE OR SMOKE NOTED. BAG BAY FIRE BOTTLES DEPLOYED. NO EVIDENCE OF FIRE OR SMOKE AFTER LANDING .... R&R FWD/AFT CARGO AREA SMOKE DETECTORS IAW AMM 26-15-01. OPS CHECK GOOD. R&R HIGH RATE & METERED BAGGAGE COMPARTMENT FIRE BOTTLES IAW AMM 26-23-01. OPS CHECK GOOD.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E909326 - RH ELEVATOR SERVO TAB TRAILING EDGE DOES NO ALIGN WITH THE ELEVATOR TRAILING EDGE....COMPLETE: RAR RH ELEVATOR UPPER AND LOWER AFT CENTER SKIN PANELS IAW PIEDMONT EO1-27-22-0064. RH ELEVATOR TRAILING EDGE NOW PROPERLY ALIGNS WITH THE SERVO TAB TRAILING EDGE.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E908716 - RUDDER 1 CENTER LOWER HINGE UPPER FITTING HAT BUSHING GOUGED....COMPLETE: FABRICATED REPAIR BUSHINGS AND INSTALLED ON RUDDER ONE CENTER LOWER HINGE UPPER FITTING IAW EMB 145 SRM 55-00-02 STEP 3,D AND EMB 145 AMM 20-10-08 AND PIEDMONT EO1-27-22-0054

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E908133 -RH WING RIB 21 IS CRACKED....COMPLETE: FABRICATED AND INSTALLED REPAIR ON RH WING RIB 21 IAW EMB 145 SRM 57-20-07-RE ITEM # 4 AND EO1-57-22-0041.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E908132 - LH WING RIB 21 IS CRACKED....COMPLETE: FABRICATED AND INSTALLED REPAIR ON LH WING RIB 21 IAW EMB 145 SRM 57-20-07-RE ITEM #4 AND E01-57-22-0040.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E908004 - FR 81 CRACKED AT AFT INBD FASTENER HOLE OF LH VERTICAL STABILIZER LOWER DRAG ANGLE....COMPLETE: MAPPED FOR PIEDMONT TECH SERVICES EVALUATION IAW PIEDMONT MPPM 13.2. REMOVED LH AFT DRAG ANGLE SECTION AND FASTENERS FROM LH AFT FUSELAGE SKIN BTW FR79-81 STGR 5L TO TOP EDGE TO FOM IAW EMB 145 SRM 51-40-02. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM FR 81 AT AFT INBD FASTENER OF LH VERTICAL STABILIZER LOWER DRAG ANGLE IAW ETD2022-145-008201. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM FR 81 AT AFT INBD FASTENER OF LH VERTICAL STABILIZER LOWER DRAG ANGLE AND FABRICATED AND INSTALLED DOUBLER AND FILLER IAW ETD2022-145-008201 AND EO1-53-22-0037. FABRICATED DOUBLER AND FILLER FOR REPAIR OF FR 81 AT AFT INBD FASTENER OF LH VERTICAL STABILIZER LOWER DRAG ANGLE IAW ETD2022-145-008201. INSTALLED FASTENERS IN LH AFT FUSELAGE SKIN BTW FR79-81 & STGR 5L TO TOP EDGE IAW EMB145 SRM 51-40-02. REINSTALLED L/H VERTICAL STABILIZER LOWER DRAG ANGLE FROM AFT PRESSURE BULKHEAD TO FR 78 IAW EMB-145 SRM 51-40-02. APPLIED EDGE SEALANT TO LH AFT FUSELAGE VERTICAL DRAG ANGLE IAW EMB 145 SRM 51-20-01. PREPPED, PRIMED AND PAINTED FR 81 AT AFT INBOARD SIDE OF L/H VERTICAL STABILIZER LOWER DRAG ANGLE IAW EMB 145 CPM 51-21-06, PIEDMONT BULLETIN CPM 51-02 AND PIEDMONT DRAWING AE-ERJ145-IR. SEE WIPS AND TASKS FOR ADDITIONAL INFORMATION.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E907563 - LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE....COMPLETE: REAMED LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE TO 1ST OVERSIZE TO REMOVE DAMAGE AND INSTALLED REPAIR BUSHINGS IAW EMBRAER SB-145-54-0008 FIGURE 2 AND PIEDMONT EO1-54-22-0055.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E907564 - RH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE....COMPLETE: REAMED RH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE TO 1ST OVERSIZE TO REMOVE DAMAGE AND INSTALLED REPAIR BUSHINGS IAW EMBRAER SB-145-54-0008 FIGURE 2 AND PIEDMONT EO1-54--22-0056.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E906373 - FRAME 66 IS CRACKED AT STRINGER 18L....COMPLETE: FABRICATED AND PREPPED FILLER AND INSTALLED REPAIR PARTS TO FR 66 AT STR 18L IAW ETD-2022-145-007541 AND EO1-53-22-0039

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905811 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6L-7L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6L-7L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0051.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905816 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 6L-7L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 6L-7L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0052.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905819 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 4R-5R....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 4R-5R IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0052.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905814 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 5L-6L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 5L-6L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0051.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905822 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGERS 6R-7R....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0052.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905825 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 5R-6R....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 5R-6R IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0052.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905813 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 4L-5L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 4L-5L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0051.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905817 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3R-4R....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3R-4R IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0052.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905809 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 5L-6L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 5L-6L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0051.

Part: NONE — NONE · airframe 41,010 hrs · 37,472 cycles

E905822 - POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3L-4L....COMPLETE: ACCOMPLISHED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3L-4L IAW EMB-145 SRM 53-32-01 ITEM 9 AND PIEDMONT EO1-53-22-0051.

Part: NOT REPORTED — NOT REPORTED · airframe 40,961 hrs · 37,410 cycles

PDIS 669 30-42 2473251 12FEB22 CLT CLOSE W/S HEAT 1 FAILED 2 TIMES IN FLIGHT FACT 12FEB22 12:28 CLT INSPECTED FOUND NO OVBIOUS DEFECTS. OPS CHECKED SYSTEM AND T/S IAW FIM 30-42-00-810-A BLOCK 1&8 AND AMM 30-42-00 SUB TASK 30-42-00-700-801-A. OPS CHECKED GOOD AT THIS TIME. TRANSITORY CONDITION OF W/S HEAT SENSORS

Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,486 hrs · 36,875 cycles

BURING SMELL NOTED ON FLIGHT DECK DURING TAXI. OPERATED BOTH ENGINES BOTH PACKS TO MAX HOT AND MAX COLD WITH NO DISCREPANCIES NOTED. RAN PACKS WITH APU BLEED WITH NO DISCREPANCIES NOTED. RAN A/C TO HIGHER POWER OPERATED BOTH PACKS. NO DISCREPANCIES NOTED

Part: LOCALIZER — MALFUNCTIONED · airframe 39,134 hrs · 35,373 cycles

PDIS 669 34-32 2433662 22FEB21 ORF CLOSE LOC WAS ERRONEOUS ON BOTH SIDES FACT 22FEB21 23:45 ROA. PERFORMED VOR/ILS/LOC OPS CHECK IN REF TO AMM TASK 34-32-00-700-801-A. NO FAULTS NOTED. CREW REPORTED OBSERVING ILS WAS WORKING PROPERLY AFTER RESET. STATION REPORTED RESETTING ILS SYSTEM. OKAY FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (STALL) · airframe 39,101 hrs · 35,340 cycles

PDIS 669 27-36 2433571 13FEB21 SYR CLOSE AFTER T/O GOT SPS2 INOP WITH SPS ADVANCED AND THE AOA FLAGGED ON F/O'S PFD. FACT 13FEB21 14:01 SYR R/R STALL PROTECTION COMPUTER IAW EMB AMM 27-36-02. OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (PNEUMATIC SYSTEM)

BLEED 1 LEAK DURING CLIMB OUT, CREW C/W QRH, MSG EXTINGUISHED. MAINTENANCE: MELED 02SEP20 17:58 MKE C24601 36-1-1 ENGINE BLEED SYSTEMS.

Part: UNKNOWN — SMOKE (CABIN-COCKPIT) · airframe 38,407 hrs · 34,574 cycles

SMOKE ODOR OBSERVED IN COCKPIT AND CABIN AFTER LANDING. MAINTENANCE: GROUND RAN ENG IAW AMM 71-00-01 MX A/C RAN PACK 1 AND PACK 2 FOR 15 MINS. NO SMOKE SMELL PRESENT ALSO GROUND RAN #1 AND #2 MAIN ENGINES FOR 15 MINS NAD NO SMOKE SMELL WAS PRESENT A/C IS OK FOR SERVICE. RAN WITH BOTH ENGINES RUNNING.

Part: COUPLING — DISCONNECTED (BLEED AIR SYS) · airframe 38,341 hrs · 34,495 cycles

BLEED 1 LEAK MESSAGE ON EICAS. RAN QRH AND MESSAGE WENT AWAY. FOUND BLEED COUPLING NOT CONNECTED UNDER LT WING LATERAL PANEL, AFT. RECONNECTED AND I-RINGED COUPLING IAW AMM 36-11-09. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 38,172 hrs · 34,298 cycles

BURNING RUBBER SMELL OUT OF PACK 1 WHILE IN FLIGHT. MAINTENANCE: GROUND RAN AC NO BURNT SMELL NOTED, ALSO PERFORMED OPS CHECK OF PACK SYSTEMS IAW 21-51-00, OPS CHECK GOOD OK FOR SERVICE.

Part: RELAY — MALFUNCTIONED (PITOT SYSTEM) · airframe 38,003 hrs · 34,124 cycles

PDIS 669 30-31 2242001 11FEB20 PHF CLOSE PITOT 3 INOP EICAS MSG FACT 12FEB20 05:18 PHF R&R RELAYS K0058,K0060,K0278,K0111,K1237 IAW AMM TASK 20-13-02-000/400-801-A. NO FIX R&R PITOT 3 SENSOR IAW AMM TASK 34-13-02-00\400-801-A. OPS CHECK GOOD REQUIRES LEAK CHECK. PERFORMED ELECTRICAL RESET. OPS CHECKED PITOT HEATING SYSTEM IAW AMM 30-31-00-700-801-A.OPS CHECK FOR PITOT 3 HEAT FAILED. LEAK CHECKS GOOD IAW EMB MM 34-13-00.

Part: ENGINE — SMOKE (NR 1) · airframe 37,235 hrs · 33,250 cycles

SMOKE REPORTED FROM THE NR 1 ENGINE AFTER SHUTDOWN. GROUND RAN THE NR 1 ENGINE, NO SMOKE NOTED ON SHUTDOWN, REPLACED THE LPT SHAFT O-RING IAW SUBTASK 05-50-00-020-001,

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,978 hrs · 31,800 cycles

PDIS 669 78-33 1691761 03JAN19 MHT ASSGN E2 REV DISAGREE MESSAGE ON TAKE OFF ROLL. CMC SHOWS E2 ICU VALVE FAIL. HISTORY: MEL 03JAN19 14:31 MHT C00314 78-2 ENG 1(2) REV DISAGREE MESS.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 34,322 hrs · 29,915 cycles

BLEED 1 VLV CLOSED EICAS ADVISORY DISPLAYED ON CLIMB OUT. WOULD NOT EXTINGUISH. CND. FOUND TO BE TRANSITORY CONDITION OF ENGINE BLEED VALVE TROUBBLESHOT IAW FIM 36-11-00-816-001-A. OK FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 33,165 hrs · 28,707 cycles

AFTER SELECTING FLAPS TO 9 DEGREES, FLAP LOW SPEED ADVISORY MESSAGE ILLUMINATED. TROUBLESHOT THE FLAP LOW SPEED ADVISORY MESSAGE IAW FIM 27-51-00-810-801-A. FOUND FLAP RT SENSOR FAIL MESSAGE ON MFD. TROUBLESHOT IAW FIM 27-51-00-810-815-A. FOUND TO BE ASSOCIATED WITH FLAP CHANNEL 2.

Part: WARNING MESSAGE — NO INDICATION (NR 2 ENGINE) · airframe 32,870 hrs · 38,386 cycles

ON TAXI OUT E2 NO DISPATCH MESSAGE WITHOUT NR 2 ENGINE RUNNING. PERFORMED DOWNLOAD OF CMC TROULESHOOTING IAW FIM 75-41-00-810-803-B01.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 32,658 hrs · 28,151 cycles

STRONG FUEL ODOR IN COCKPIT AND CABIN WHEN APU IS STARTED. INSPECTED THE APU FUEL LINES AND SURROUNDING AREAS WHILE APU RUNNING. NO DEFECTS OR LEAKS NOTED. NO ODOR IN CABIN AT THIS TIME. OK FOR SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,619 hrs · 28,113 cycles

STRINGER 6R CRACKED AT FR 13. REMOVED AND REPLACED STRINGER 6R AT FR 13 IAW SRM 51-40-02, 51-20-03.

Part: ENGINE — FAILED (LEFT) · airframe 32,485 hrs · 27,983 cycles

ABORTED TAKEOFF AT AROUND 95 OR 100 KNOTS DUE TO SMOKE IN THE COCKPIT, HIGH SPEED ABORT CONTINUED BELOW. REMOVED AND REPLACED LT ENGINE IAW MTX WC 71-000-00, OPS TEST GOOD, ALSO REF NRWC 669-ORD-02694, FOR ODOR/ SMOKE EVENT C/W ETN-EM-72-034. OPS TEST GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,358 hrs · 27,863 cycles

FOUND RT SIDE EXTERNAL EMERGENCY LIGHT INOP UPON PS-2 INSPECTION. R&R RT EXTERNAL CENTER FAIRING EMERGENCY LAMP IAW AMM 33-50-10. OPS CHECK GOOD .

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,003 hrs · 26,610 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED FLASHLIGHT IAW MEL 25-53, M PROCEDURES COMPLIED WITH. INSTALLED FLASHLIGHT ASSY ON AFT CABIN OPS CHECK GOOD IAW EMB 145 MM 33-50-16. MEL RESTORED

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 30,092 hrs · 25,755 cycles

ELECTRIC BURN SMELL IN COCKPIT & CABIN NO ABNORMAL INDICATIONS IN COCKPIT SYSTEMS. PERFORMED OPERATIONS CHECK WITH PACK RUNNING IAW 21-00-00. WITH ENG RUNNING IAW RR MM 72-00-00, LIGHTING SYS & NO ELECTRICAL SMELL NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,033 hrs · 24,761 cycles

LEFT UPPER EXTERIOR EMER LIGHT INOPERATIVE. R & R LAMP IN LT UPPER EXTERIOR EMER LIGHT. OPERATIONS TESTED OK IAW AMM 33-50-10.

Part: PITOT TUBE — DAMAGED (PITOT/STATIC SYS) · airframe 28,772 hrs · 24,530 cycles

ON DESCENT RECEIVED AIRSPEED INTEG FLAG, FLAG WENT AWAY. APPROX 25500 AIRSPEED DIFFERENCE BETWEEN PRIMARY STBY WAS LOOKING DIFFERENT BETWEEN BOTH THE PRIMARY WAS 30 KNTS ALSO HAD ALTITUDE DIFFERENCE OF 300 FT BETWEEN PRIMARY ALTITUDE. FOUND PITOT 2 DAMAGE. R & R PITOT NR 2 IAW AMM 34-13-01. PERFORMED ADC SYS IAW AMM 34-15-00 IS GOOD. PERFORMED LEAKAGE TEST, PITOT & STATIC SYS NR 1 & 2, IS GOOD IAW AMM 34-13-00. REFERENCE ETN-EM-34-002. REINSTALLED SHIMS ON ORIGINAL POSITION WERE FOUND. HEATING TEST IS GOOD IAW AMM 30-31-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,672 hrs · 24,433 cycles

SMELL OF ELEC SMOKE ROWS 1, 2 & 3. NO ELEC SMOKE SMELL NOTED AT THIS TIME. ACFT READY FOR SERVICE.

Part: FLASHLIGHT — ODOR (CABIN) · airframe 28,490 hrs · 24,273 cycles

FLIGHT ATTENDANT REPORTED BURNING SMELL FROM FRONT OF AC ROW ONE FOR SHORT TIME THEN WENT AWAY. TROUBLE SHOT IAW FIM TASK 21-20-00-810-801-A. SUSPECT FAULTY FLASHLIGHT ASSEMBLY ABOVE FLIGHT ATTENDANTS SEAT. R & R FLASHLIGHT ASSEMBLY ABOVE FLIGHT ATTENDANTS SEAT IAW AMM 33-50-16. ALL CHECKED GOOD.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 28,487 hrs · 24,270 cycles

HAIL DAMAGE EVENT. CFI LT UPPER BUTT SPLICE AT FRAME 16, STRINGER 1L-1R GOUGED. PERFORMED REPAIR IAW ERS-EM-53MR-1174.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. TOOLING MARK ON RFI TOP SKIN AFT OF FRAME 64 BETWEEN STRINGER 3R - 4R. REPAIRED IAW ERS-EM-53MR-1135.

Part: DOUBLER — GOUGED (LT HORIZ STAB) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. LEFT STAB DOUBLER GOUGED FWD OF SPAR II NEAR ROOT. REPAIRED DAMAGE IAW ERS-EM-55MR-250.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTB UPPER SKIN TIP IAW SRM 55-20-01, 51-20-01, 51-40-06, 51-20-03, 51-40-02, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 28,476 hrs · 24,260 cycles

DURING TAXI IN AIL SYS 1 INOPERATIVE, RUDDER SYS 1 INOPERATIVE, STEERING INOPERATIVE 1. ELEC HYD PUMP TURNED OFF IN AUTO MODE, TOWED. INSP ACFT FOR LEAKS, NONE NOTED CHECKED FLUID LEVELS FOR HYD SYS ALL GOOD. PERFORMED OPERATIONS CHECK OF EMDP NR 1 & 2. OPERATIONS CHECKED GOOD IAW 29-10-04, NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01, ETN-EM-55-073R2 & ETN-EM--55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN PN 145-27270-005 IAW SRM 51-20--01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

REPLACE CTR FUSELAGE I RT SKIN. R & R RT CTR FUSELAGE I SKIN IAW SRM 53-24-01-SI, 51-20-03, 51-20-01, 51-40--02, 51-40-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

REPLACE FWD FUSELAGE I RT SKIN PANEL. R & R RT FWD FUSELAGE I SKIN PN 54051-003 IAW SRM 51-40-02, 51-20-01, 51-40-03,51-40-06, 53-11-01-SI, ETN-EM-51-118 & ETN-EM-53-235.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR INBD LE IAW SRM 51-40-06, 51-40-02, 51-20-01, 51-20-03, 55-20-01SI, ETN-EM-55-073R2, ETN-EM-55-076 & ERS-EM-5500-248.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

REPLACE FWD FUSELAGE II SKIN. R & R FWD FUSELAGE II WIPER PANEL IAW SRM 53-12-01SI, 51-40-02, 51-40-03, 51-20-01, 51-20-03, 51-40-06, ETN-EM-53-206 & ETN-EM-51-118.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. R & R LT FWD FUSELAGE I IAW SRM 51-40-02, 51-20-01, 51-40-03, 51-40-06, 53-11-01-SI, ETN-EM-51-118 & ETN-EM-53-235.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II SKIN PANEL. R & R CTR FUSELAGE II TOP SKIN IAW SRM 53-22-01-SI, 51-20-03, 51-20-01, 51-40--02, 51-40-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-263R1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN IAW SRM 51-20-01SI, 51-40-02, 51-20-03, 51-40-06, 55-20-01 & ETN-EM-55-073R2.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE RT STAB UPPER SKIN. R & R RT HORIZONTAL STAB TOP SKIN IAW SRM 55-10-01SI, 51-40-02, 51-20-01, 51-20-03, 51-40-06 & ETN-EM--55-074.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I UPPER SKIN IAW SRM 53-31-01 SI , 51-40-02, 51-40-06, 51-20-03, 51-20-01, CPM 51-21-04, ETN-EM-53-266 R3 & ETN -EM-51-118.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OTBD LE. R & R RT ELEVATOR OTBD LE IAW SRM 51-20-01, 51-40-02, 51-20-03, 51-40-06, 55-20-01 & ETN-EM-55-073R2 & ERS-EM-5500-246.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 53-24-01-SI, 51-20-03, 51-20-01, 51-40--02, 51-40-03, 51-40-06, ETN-EM-51-118 & ETN-EM-53-265.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM'S 51-20-01 SI, 51-40-02, 51-20-03, 51-40-06, -55-20-01, ETN-EM-55-073R2 & ERS-EM-5500-251.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN PN 145-27270-005 IAW SRM 51-20--01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 28,481 hrs · 24,264 cycles

HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R REPLACED LT STAB UPPER SKIN IAW SRM55-10-01SI, 51-20-01, 51-20-03, 51-40-02, 51-40-06, ETN-EM-55-074 & ETN-EM-51-118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,487 hrs · 24,270 cycles

HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE I. R & R LT CTR FUSELAGE I IAW SRM 51-20-0, 51-20-03, 51-40-02, 51-40-06, 53-21-01SI, ETN-EM-51-118 & ETN-EM-53-262.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,284 hrs · 24,081 cycles

AFT FUSELAGE SKIN CRACKED ABOVE STRINGER 2L AT FRAME 75. ACCOMPLISHED REPAIR ON AFT FUSE SKIN ABOVE STRINGER 2L AT FRAME 75 IAW ERS-EM-53MR-1028.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,284 hrs · 24,081 cycles

AFT FUSELAGE SKIN CRACKED ABOVE STRINGER 2R AT FRAME 75. ACCOMPLISHED REPAIR ON AFT FUSE SKIN ABOVE STRINGER 2R AT FRAME 75 IAW ERS-EM-53MR-1028.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,483 hrs · 23,428 cycles

EMERGENCY LIGHTING FLOOR STRIPS 2 & 3 WILL NOT ILLUMINATE. R & R NR 3 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,458 hrs · 23,405 cycles

ROW 3 AISLE EMER LAMP INOPERATIVE. R & R ROW 3 AISLE EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 27,107 hrs · 23,115 cycles

CAPTAINS FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: ADC — FAILED (NR 1) · airframe 26,713 hrs · 22,777 cycles

ADC1 FAIL IN FLIGHT RED X OVER AIRSPEED ALTITUDE & RED VS REVERSIONARY WORKED FINE. R & R NR 1 COMPUTER MICRO AIR DATA, OPERATIONS CHECKED GOOD IAW AMM 34-15-01.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 26,537 hrs · 22,570 cycles

NR 1 ENG OIL LEAK IN FLIGHT. IN CRUSE FLIGHT OIL LEVEL WAS 6 QT, LANDED WITH 3QT. REPLACED AGB BREATHER CARBON SEAL & O RING IAW MM 72-63-10. LEAK CHECKED GOOD IAW NRWC 669-ORD-01585 RII LAW 173773.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,648 hrs · 21,820 cycles

FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT HOLDER BROKEN. R & R FLIGHT ATTENDANT`S FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: TUBE — FAULTY (LANDING GEAR) · airframe 23,874 hrs · 20,361 cycles

ON FLIGHT 9808 THE CREW REPORTED THAT DURING LANDING GEAR EXTENSION THEY HEARD A BANG NOSE AND THE GEAR FAILED TO EXTEND FOLLOWED BY AN EICAS LG/LEVER DISAGREE MESSAGE. THE CREW COMPLIED WITH AOM PROCEDURES AND DECLARED AN EMERGENCY. THE GEAR EXTENSION ON THE SECOND ATTEMPT WAS GOOD. THE AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE SYSTEM 1 LOWER RETRACTION FLEXIBLE AND SOLID LINE IAW EMB 145 AMM 20-10-03. PERFORMED EXTENSION AND RETRACTION ADJUSTMENT TEST AND LANDING GEAR ADJUSTMENT TEST IAW EMB 145 AMM 32-30-00 AND 32-34-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 23,846 hrs · 20,333 cycles

DURING MAINTENANCE INSPECTION FOUND NR 6 LEFT EMERGENCY LIGHT STRIP EXTRUSION CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 LEFT EMERGENCY LIGHT STRIP EXTRUSION IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,846 hrs · 20,333 cycles

DURING B INSPECTION FOUND THE PASSENGER CABIN EMERGENCY LIGHT IN CEILING PANEL AT 7A NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY AISLE LIGHT LAMP AT CEILING PANEL AT 7A IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 23,846 hrs · 20,333 cycles

DURING MAINTENANCE INSPECTION FOUND AFT AISLE EMERGENCY LIGHT STRIP CONNECTOR BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE AFT AISLE EMERGENCY LIGHT STRIP CONNECTOR IAW EMB 145 SWMP 20-50-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 22,162 hrs · 19,020 cycles

FLIGHT 2880, RED CHARGE LIGHT DOES NOT COME ON FOR FLASHLIGHT IN AFT CABIN. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECKED WAS GOOD.

Part: COVER — MISSING (CABIN PRESSURE) · airframe 21,090 hrs · 18,174 cycles

FOR FLIGHT 3355 MAINTENANCE REPORTED THE AC WAS RETURNING WITH A PRESSURIZATION PROBLEM PIREP-CLIMBING THROUGH 10,000 FT CABIN ALT TURNED RED AND THE CREW DESCENDED BELOW 10,000. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND GROUND AIR CONNECTION COVER MISSING, RETRIEVED OLD COVER AND REPLACED WITH NEW IAW EMB MM 21-22-04 LESS STEP I1. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MISINSTALLED (EMERGENCY EXIT) · airframe 21,046 hrs · 18,143 cycles

ON FLIGHT 2892 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY EXIT DOOR UPPER HANDLE WAS INSTALLED UPSIDE DOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-INSTALLED RIGHT OVERWING EMERGENCY HANDLE TO CORRECT POSITION IAW AMM 25-23-03. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,052 hrs · 18,148 cycles

DURING B-INSPECTION FOUND THE LAST ROW OF FLOOR STRIP EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY BATTERY AND CHARGER IAW W/C # 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C # 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,834 hrs · 17,248 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP FORWARD OF EMERGENCY ROW WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP BETWEEN ROWS 10-12 IAW AMM 33-50-12. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,783 hrs · 16,494 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT ON THE MAIN ENTRANCE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IN THE EMERGENCY LIGHT ON THE MAIN DOOR IAW EMB 145 AMM 33-50-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 18,415 hrs · 16,212 cycles

ON FLIGHT 3958 DURING TAKEOFF THE CREW REPORTED, RECEVIED A "LAV SMOKE EICAS WARNING". THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND PASSENGERS SEATED AROUND ROW 11-14 REPORTED THE ODOR AS WELL. THE CAPTAIN ELECTED TO RETURN TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE IAW AE WC 71-000-00. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 18,100 hrs · 15,960 cycles

ON FLIGHT 3210 THE CREW REPORTED THAT ON TAKEOFF HAD A HARD DEVIATION TO THE RIGHT - LOST NOSE WHEEL STEERING. RECEIVED A NOSE STEERING INOPERABLE MESSAGE ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED NOSE WHEEL STEERING SYSTEM IAW EMB 145 AMM 32-50-00. THE OPERATIONAL CHECK AND TAXI CHECK WAS GOOD AT THIS TIME. NO PARTS REMOVED OR REPLACED. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RMU — DEFECTIVE (COCKPIT) · airframe 17,248 hrs · 15,342 cycles

ON FLIGHT 3618 DURING DESCENT THE CREW REPORTED THE NR 2 RADIO MANAGEMENT UNIT WENT OUT WITH NO TUNING CAPABILITY AND THEN THE NR 1 RADIO MANAGEMENT UNIT STARTED SWITCHING UNCOMMANDED BACK AND FORTH BETWEEN SELECTED FREQUENCY AND STANDBY ON IT'S OWN. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF NR 2 RADIO MANAGEMENT UNIT IAW EMB 145 MM 23-81-00, SYSTEM CHECKS GOOD. PERFORMED OPERATIONAL CHECK OF THE NR 1 RADIO MANAGEMENT UNIT IAW EMB 145 MM 23-81-00, SYSTEM CHECKS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HEAT EXCHANGER — MALFUNCTIONED (NR 1) · airframe 17,050 hrs · 15,198 cycles

ON FLIGHT 4053 THE FLIGHT ATTENDANT REPORTED AFTER TAKEOFF DETECTED AN ODOR OF BURNING RUBBER WHICH WENT AWAY BUT DURING LANDING THE ODOR CAME BACK. ON THE POST FLIGHT NOTICED ODOR COMING FROM THE NR 1 PACK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DUAL HEAT EXCHANGER NR 1 IAW AMM 25-51-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,746 hrs · 13,448 cycles

ON FLIGHT 3253 THE CREW REPORTED A BURNING OIL SMELL DURING TAKEOFF AND CLIMBOUT. THE SMELL DISSIPATED AFTER THE CLIMBOUT. THE CREW DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN-EM-72-034 R4 COULD NOT DUPLICATE SMELL. COMPLIED WITH 0 CARBON SEAL IAW 72-00-00-00-200-802. NO EVIDENCE OF OIL. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (LAVATORY) · corrosion level 2 · airframe 14,337 hrs · 13,132 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LAVATORY BUCKET HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-31-02. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 14,337 hrs · 13,132 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR CABLE SPOOL FORWARD UPPER BRACKET CRACKED (BACKSIDE). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED CARGO DOOR CABLE SPOOL ON FORWARD UPPER BRACKETS PREPPED AND INSTALLED SERVICEABLE BRACKET IAW EMB SRM 51-40-02, 51-20-03 EMB CPM 21-21-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — ODOR (NR 2)

ON FLIGHT 4125 CREW REPORTED DURING TAKEOFF SMOKE ODOR IN COCKPIT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE IAW AMM 21-51-03. ACFT RETURNED TO SERVICE. (K)

Part: APU — SMOKE · airframe 9,801 hrs · 9,096 cycles

ON FLIGHT 4362 - AFTER SHUTDOWN AT THE GATE AND WITH THE APU AND NUMBER 2 PACK RUNNING, A/C CABIN AND COCKPIT FILLED WITH SMOKE. APU AUTO SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE ISSUED MEL 49-1. REMOVED AND REPLACED APU AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,435 hrs · 8,774 cycles

DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 24-25 CROSSMEMBER. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,435 hrs · 8,774 cycles

DURING IMBV INSPECTION, FOUND FWD SERVICE DOOR SILL BETWEEN FR 18-20. CORRODED REPAIRED FWD SILL IAW SRM 53-21-10. A/C RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,435 hrs · 8,774 cycles

DURING IMBV INSPECTION, FOUND AFT SVC DOOR SILL IS CORRODED BETWEEN FR 21-22. REPAIRED SILL IAW SRM 53-21-10. A/C RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (ZONE 500) · airframe 8,505 hrs · 7,861 cycles

SPEED BRAKE CIRCUIT BREAKER (F-13) FOUND POPPED INFLIGHT, EMERGENCY DECLARED. REMOVED AND REPLACED LEFT HORIZONTAL PROXIMITY SWITCH ON SPEED BRAKE IAW EMB AMM 27-63-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 8,025 hrs · 7,426 cycles

EMERGENCY AFT CABIN LIGHTS AND EXIT SIGN INOPERATIVE, FERRIED AIRCRAFT TO ORD. REMOVED AND REPLACED EMERGENCY BATTERY AT AFT CEILING POSITION IAW EMB AMM 33-50-04 AND EXIT SIGN IAW EMB AMM 33-50-14. BOTH ITEMS OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,140 hrs · 6,672 cycles

HAZE WITH OIL SMELL DETECTED AFTER ROTATION. RAN BOTH ENGINES WITH PACKS ON AND NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

THE EMERGENCY FLOOR LIGHTS IN THE FORWARD PART OF THE CABIN FAIL TO ILLUMINATE DURING TEST. REPLACED EMERGENCY BATTERY POWER SUPPLY NR 2, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE GALLEY LT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (CARGO DOOR)

THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LWR SILL. INSTALLED NEW SILL IAW SRM. (K)

Part: BRAKE — FAILED (LT FLAP XMSN)

IAH - FLT 3837 - FLAP FAIL MESSAGE ON EICAS. FLAPS SELECTED TO 9 DEGREES, NO MOVEMENT. ALSO, FLAPS WILL NOT MOVE ON GROUND. REPLACED LEFT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)