N939AE

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 42,951 hrs · 38,874 cycles

DURING APPROACH #1 ENGINE FLAMED OUT AFTER BIRD STRIKE. CREW SAID SHORTLY AFTER PASSING 2200 FT.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 42,951 hrs · 38,874 cycles

DURING APPROACH #1 ENGINE FLAMED OUT AFTER BIRD STRIKE. #1 ENGINE R+R IAW W/C 71-00-00. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: CONNECTOR — LOOSE (TE FLAPS SYS) · airframe 42,775 hrs · 38,662 cycles

FLAP FAILED ON TAKEOFF. FLAPS STUCK AT 9 DEGREES AND WOULD NOT MOVE. CMC MSG FLAP LH TRANSMISSION FAIL. CMC SHOWED NO NEW MESSAGES, PERFORMED OPS CHECK I.A.W AMM 27-51-00-700-801-A. OPS CHECK GOOD. INSPECTED APPLICABLE CANNON PLUGS FOR LOOSENESS FOUND P1247 FOR L/H FLAP XMSN BK TRAILING EDGE SLIGHTLY LOOSE, TIGHTENED AS REQUIRED. PERFORMED GVI OF THE MECHANICAL LINE REF 27-51-00-200-801-A/600 NO DEFECTS NOTED. PERFORMED FLAPS OPS CHECK IAW AMM 27-51-00-700-801-A OPS CHECK GOOD. A//C GOOD FOR SERVICE.

Part: SENSOR — UNSECURE (TE FLAPS) · airframe 42,564 hrs · 38,420 cycles

FLAPS STUCK AT 9. WITH FLAPS FAIL ON EICAS. MESSAGE FLAP LT TRANS FAIL IAW FIM 27-51-00-810-816-A. FOUND LT FLAP VELOCITY SENSOR C/P 3 REVOLUTIONS LOOSE, TIGHTENED PLUG AND CHECKED ALL PLUGS IN FLAP DRIVE SYSTEM OPS CK PER MM 27-51-00-700-801-A. OPS CHECK GOOD NO MESSAGES ON EICAS OR CMC, OK FOR SERVICE.

Part: SHROUD — UNSECURE (LT TE FLAP) · airframe 42,482 hrs · 38,333 cycles

FLAP FAIL WITH FLAPS STUCK AT 8 DEGREES. INSPECTED FLAPS AND FOUND LH IB FLAP SHROUD JAMMED INTO LH IB FLAP LEADING EDGE. REMOVED LH IB FLAP IAW AMM27-50-00-000-801-A. REPLACED AND INSTALLED LH IB FLAP IAW AMM27-50-00-400-801-A

Part: PROFILE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E028391 SERVICE DOOR LOWER FWD PROFILE IS CORRODED AT NUTPLATE HOLES. RAR SERVICE DOOR LOWER FWD PROFILE IAW EMB 145 SRM 51-40-02.

Part: TRUNNION — CORRODED (NLG) · airframe 42,124 hrs · 37,934 cycles

E028366 NLG RH TRUNNION IS PITTED AT LEG FITTING. BLENDED AS REQUIRED TO REMOVE DAMAGE FROM NLG RH TRUNNION AT LEG FITTING IAW EMB-145 SRM 53-11-08 AD AND 51-10-03 FOUND TO ACCEPTED FOR 5000 FC'S THEN REQUIRES REPLACEMENT PER ETD2024-145-007867 AND PIEDMONT EO1-32-24-0207.

Part: TRUNNION — CORRODED (NLG) · airframe 42,124 hrs · 37,934 cycles

E028372 NLG LH TRUNNION IS PITTED AT LEG FITTING. BLENDED AS REQUIRED TO REMOVE DAMAGE FROM NLG LH TRUNNION AT LEG FITTING IAW EMB-145 SRM 53-11-08 AD AND 51-10-03 FOUND TO BE ACCEPTED FOR 5000 FC'S THEN REQUIRES REPLACEMENTPER ETD2024-145-007867 AND PIEDMONT EO1-32-24-0207

Part: ATTACH BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E028093 PAX DOOR LINER ATTACHMENT BRACKET AT FWD LOCK BOX IS CORRODED. FABRICATED AND INSTALLED ATTACHMENT ANGLE BRACKET FOR THE PAX DOOR LINER AT FWD LOCK BOX IAW ERJ 145 SRM 51-20-03, 51-30-01, 51-40-02 AND ERJ 145 CPM 51-21-06 AND EO1-05-24-0225.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E028189 CENTER OMEGA BEAM GUSSET #2 HAS CORROSSION. RAR CENTER OMEGA BEAM GUSSET#2 IAW EMB 145 SRM 51-40-02. SEE WIPS AND TASK FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FRMS 60-65) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027327 CARGO L/H FLOOR SUPPORT BETWEEN FR 60 AND 65 IS CORRODED AROUND NUTPLATE HOLES. RAR CARGO L/H FLOOR SUPPORT BETWEEN FR 60 AND 65 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRM 22) · airframe 42,124 hrs · 37,934 cycles

E027309 GALLEY, LH OMEGA BEAM RH SIDE AT FRAME 22 IS CRACKED. PERFORMED CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER ON L/H OMEGA BEAM RH SIDE AT FRAME 22 IAW ETD-2024-145-008186 AND EO1-53-24-0219

Part: CROSSBEAM — CORRODED (FRM 23) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027302 RH CROSSBEAM AT FRAME 23 IS CORRODED. REMOVED AND REPLACED WITH SERVICEABLE RH CROSSBEAM AT FRAME 23 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027319 GALLEY, PAX DOOR FWD FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED THE CORRODED GALLEY, PAX DOOR FWD FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (FRM 53) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027255 DIAMOND GUSSET AT FRAME 53 IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE DIAMOND GUSSET AT FRAME 53 IAW EMB145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRM 39) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027252 RH INBD CROSSBEAM AT FRAME 39 IS CORRODED. RAR RH INBD CROSSBEAM AT FRAME 39 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 43-44) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027244 CENTER OMEGA BEAM LH SIDE IS CORRODED BETWEEN FRAMES 43 AND 44. PERFORMED CUTOUT AS REQUIRED TO REMOVED DAMAGE FROM CENTER OMEGA BEAM LH SIDE BETWEEN FR 43 AND 44 AND FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIMS IAW EO1-53-24-0224.

Part: CROSSBEAM — CORRODED (FRM 53) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027254 RH INBD CROSSBEAM AT FRAME 53 IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE R/H INBOARD CROSSBEAM AT FRAME 53 IAW EMB 145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRM 49) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027250 RH OTBD CROSSBEAM AT FRAME 49 IS CORRODED. RAR RH OTBD CORRODED CROSSBEAM AT FRAME 49 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027216 RH OTBD FLOOR SILL #6 HAS CORROSSION. REMOVED AND REPLACED R/H OTBD FLOOR SILL #6 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027158 CARGO DOOR LWR CENTER SILL IS CORRODED. REMOVED AND INSTALLED SERVICEABLE CARGO DOOR LOWER CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

A027161 CARGO R/H FLOOR SUPPORT BETWEEN FR-68NAND FR-71 IS CORRODED AROUND NUT-PLATES HOLES. RAR CARGO R/H FLOOR SUPPORT BETWEEN FR 68 AND 71 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027221 CENTER OMEGA BEAM GUSSET #3 HAS CORROSSION. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #3 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027224 CENTER OMEGA BEAM GUSSET #6 HAS CORROSSION. RAR CENTER OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02,

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027223 CENTER OMEGA BEAM GUSSET #5 HAS CORROSSION. RAR CENTER OMEGA BEAM GUSSET #5 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027220 LH OTBD FLOOR SILL #7 HAS CORROSSION. RAR THE LH OTBD FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027213 RH OTBD FLOOR SILL #3 HAS CORROSSION. RAR CORRODED RH OUTBD FLOOR SILL #3 IAW EMB 145 SRM 51-40-02. PREPPED, PRIMED, AND PAINTED RH OUTBD FLOOR SILL #3 IAW EMB 145 CPM 51-21-06 ELLCOMETER #8533

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027217 LH OTBD FLOOR SILL #4 HAS CORROSSION. RAR LH OUTBD FLOOR SILL #4 IAW EMB145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRM 44) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027258 LH CROSSBEAM AT FRAME 44 IS CORRODED. REMOVED AND REPLACED LH CROSSBEAM AT FRAME 44 IAW EMB 145 SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027267 LAV POTABLE WATER CABLE SUPPORT IS CORRODED TOP AND BOTTOM. REMOVED AND INSTALLED NEW SERVICABLE LAV POTABLE WATER CABLE SUPPORT IAW EMB 145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (FRM 49) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027257 LH CROSSBEAM AT FRAME 49 IS CORRODED. REMOVED AND REPLACED CORRODED LH CROSSBEAM AT FRAME 49 IAW ERJ145 SRM 51-40-02

Part: CROSSBEAM — CORRODED (FRM 53) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027251 RH OTBD CROSSBEAM AT FRAME 53 IS CORRODED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE R/H OUTBOARD CROSSBEAM AT FRAME 53 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027218 LH OTBD FLOOR SILL #5 HAS CORROSSION. RAR LH OUTBD FLOOR SILL #5 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027222 CENTER OMEGA BEAM GUSSET #4 HAS CORROSSION. RAR THE CENTER OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027225 LH OMEGA BEAM GUSSET #4 HAS CORROSSION. REMOVED AND REPLACED CORRODED L/H OMEGA BEAM GUSSET #4 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027160 CARGO R/H FLOOR SUPPORT BETWEEN FR-71 AND FR-73 IS CORRODED AROUND NUT-PLATES HOLES. RAR CARGO R/H FLOOR SUPPORT BETWEEN FR 71 AND 73 IAW EMB 145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRM 53) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027259 LH CROSSBEAM AT FRAME 53 IS CORRODED. RAR LH CROSSBEAM AT FR 53 IAW EMB-145 SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRM 39) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027249 RH OTBD CROSSBEAM AT FRME 39 IS CORRODED. RAR RH OUTBD CROSSBEAM AT FR 39 IAW EMB-145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027159 CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP BETWEEN STGRS 16L-17L IS CORRODED. ACCOMPLISHED REPAIR ON CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP BETWEEN STGRS 16L-17L IAW EMB 145 SRM 53-31-04RE ,ITEM 4.FIGURE 212 AND EO1-53-24-0227

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E027136 CABIN L/H FLOOR SILL #2 HAS CORROSION. REMOVED & REPLACED L/H FLOOR SILL #2 AND DRILLED NEW ONE IAW EMB 145 SRM 51-20-03 AND 51-40-02.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 42,124 hrs · 37,934 cycles

E027141 CARGO DOOR INNER SKIN IS CHAFED AT VB2 AND HB3. FABRICATED AND INSTALLED REPAIR DOUBLER TO CARGO DOOR INNER SKIN AT VB2 AND HB3 IAW ETD2024-145-008192 REV.:/ AND EMB 145 SRM 52-30-01 RE, EMB 145 SRM 51-40-02 AND EO1-52-24-0223

Part: SHEAR TIE — CRACKED (FRM 81 S12R) · airframe 42,124 hrs · 37,934 cycles

E026958 INSIDE OF 312AR ACCESS PANEL AT FR 81 AND STRGR 12R A SHEAR CLIP IS CRACKED. REMOVED AND REPLACED SHEAR CLIP INSIDE OF 312AR ACCESS PANEL AT FR 81 AND STRGR 12R IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (FRM 81 S2-3R) · airframe 42,124 hrs · 37,934 cycles

E026969 INSIDE OF 312AR ACCESS PANEL SHEAR CLIP HAS A POSSIBLE CRACK AT FR- 81 BETWEEN STGRS 2R-3R. REMOVED AND REPLACED SHEAR CLIP INSIDE OF 312AR ACCESS PANEL AT FR- 81 BETWEEN STGRS 2R-3R IAW EMB 145 SRM 51-40-02

Part: GUIDE — CORRODED (EMERGENCY EXIT) · airframe 42,124 hrs · 37,934 cycles

E026713 RH EMERGENCY EXIT GUIDE PINS HAVE CORROSION. REMOVED MINOR SURFACE CORROSION. FROM RH AFT EMERGENCY EXIT GUIDE PIN IAW EMB 145 CPM 51-14-04.REAPPLIED CIC TO AFT GUIDE PIN IAW EMB 145 CPM 51-61-00. REMOVED AND REPLACED R/H EMERGENCY EXIT FWD GUIDE PIN IAW EMB 145 AMM 20-10-01, 52-21-00, 12-22-00. S/N 1099402153.

Part: DOOR FRAME — CORRODED (CARGO) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E026684 CARGO DOOR LOWER FRAME INBOARD PROFILE HAS CORROSION AROUND NUT PLATE HOLES. INSTALLED SERVICEABLE CARGO DOOR LOWER FRAME INBOARD PROFILE IAW EMB 145 SRM 51-20-01 AND 51-40-02 AND PIEDMONT EO1-05-24-0225.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 42,124 hrs · 37,934 cycles

E026716 RH EMERGENCY EXIT HAS CORROSION ON LOWER FRAME AT RUBBER STOP. RAR #4 CORRODED BEAM ON RH EMERGENCY EXIT ON LOWER FRAME AT RUBBER STOP IAW EMB 145 SRM 51-40-02.

Part: LAMP — INOPERATIVE (AFT) · airframe 40,946 hrs · 36,654 cycles

AFT AISLE EMERGENCY LIGHT INOP-C/A-RAR AFT AISLE EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: NONE — NONE ([0000] [UPR]) · airframe 40,239 hrs · 35,894 cycles

CARGO SMOKE INDICATION ON FINAL DESCENT DECLARED EMERGENCY NO INJURIES REPORTED.-C/A-RAR BAG COMPARTMENT HIGH RATE EXTINGUISHER BOTTLE AMM 26-23-01 SEE LGPG 4791650/2 FOR RAR OF METERING BOTTLE

Part: DOOR — DIRTY (MAIN PAX DOOR) · airframe 39,883 hrs · 35,458 cycles

MAIN DOOR DIFFICULT TO CLOSE/ GET A GREEN INDICATON ON-C/A-CLEANED MAIN PAX DOOR AND LUBED IAW AMM 52-10-01-05. OPC GOOD. NO DEFECTS NOTED.

Part: NOT REPORTED — NOT REPORTED · airframe 39,195 hrs · 34,679 cycles

PRESSURIZATION FAIL WHILE IN FLIGHT AT FL 240 IN BOTH THE AUTO AND MANUAL MODE DECLARED EMERGENCY. MEL 21-30 AUTH# 020319D-C ORIG AML PG 4847349. PACK 2 LOUD NOISE, BLOWN DUCT SLEEVE.-C/A-RAR #2 ACM DUCT SLEEVE, INSP CHECK GOOD IAW AMM 21-51-14, NO LEAKS, RH COOLING SYSTEM TEST GOOD IAW AMM 21-51-00 MEL 21-30 RESTORED.SEE ITEM #1 AND ITEM # 3 THIS AML PAGE. PRESSURIZATION CHECK GOOD IAW AMM 21-31-00.

Part: NONE — NONE · airframe 38,889 hrs · 34,319 cycles

AT APPROX. 100 KNOTS SPS 1 INOP WARNING & AT LEAST ONE OTHER CAUTION MESSAGE. REJECT TAKEOFF, RTG.-C/A-FOUND STALL PROTECTION COMPUTER NOT PROPERLY SECURED INTO RACK. BUMPED BACK COMPUTER AND TIGHTENED KNOBS OVER 2 FULL TURNS EACH, IAW AMM 27-36-02. OPC GOOD IAW 27-36-00-700-801.

Part: NONE — NONE · airframe 38,842 hrs · 34,266 cycles

AFT EMERGENCY FLASHLIGHT NOT CHARGING-C/A-RAR AFT EMERGENCY FLASHLIGHT IAW ETN-EM-33-059. OPS CHECK GOOD

Part: NONE — NONE · airframe 38,801 hrs · 34,218 cycles

MEL 2532 - AUTH# 11-166M-C FWD FLIGHT ATTNDENT EMERGENCY FLASHLIGHT MISSING SWAPPED WITH AFT-C/A-RAR AFT EMERGENCY FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MEL ITEM CLOSED

Part: NONE — NONE · airframe 38,758 hrs · 34,168 cycles

AFT FA EMERGENCYFLASHLIGHT INOP"MEL 25-32 AUTH# 100398M-CREF LOGPAGE 4801873-1-C/A-REMOVED AND REPLACED AFT FA EMERGENCY FLASHLIGHT IAW EMB 145 AMM 33-50-15. OPC GOOD. MEL ITEM RESTORED.

Part: NONE — NONE · airframe 38,741 hrs · 34,143 cycles

AFT FA EMERGENCY FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA EMERGENCYFLASHLIGHT M PROCEDURES C/W REF MEL 25-32 AUTH 100398M-C

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,106 hrs · 33,398 cycles

#4 EMERGENCY CEILING LIGHT INOP-C/A-RAR #4 EMERGENCY CEILING LIGHT IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD.

Part: FRAME — DENTED (FRM 72 S14-17L) · airframe 37,717 hrs · 32,963 cycles

FR 72 HAS 3 DENTS BETWEEN STGR 14L-17L -C/A-PERFORMED PERMANENT REPAIR TO FR 72 BETWEEN STGR 14L AND 17L IAW ERS-EM-53MR-4311 REVISION: ORIGINAL.

Part: STRINGER — CRACKED (FRAME 13) · airframe 37,717 hrs · 32,963 cycles

STRINGER 6R AT FRAME 13 IS CRACKED 1 CRACK, LENGTH .2"-C/A-RAR STRINGER 6R SPLICE AT FRAME 13 IAW EMB 145 SRM 51-40-02

Part: FITTING — DAMAGED (LT AILERON) · airframe 37,717 hrs · 32,963 cycles

DAMPER FITTING ON LH AILERON OUTBD HAT BUSHING HOLE DAMAGED-C/A-RAR THE DAMAGED LH AILERON DAMPER FITTING IAW EMB 145 SRM 51-40-02,51-20-03, AND EO-EM-27MR-112

Part: BULKHEAD — GOUGED (FRM 7) · airframe 37,717 hrs · 32,963 cycles

FWD PRESSURE BULKHEAD HAS MULTIPLE GOUGES BEHIND LH WINDSHIELD WIPER MOTOR. -C/A-PERFORMED PERMANENT REPAIR TO FWD PRESSURE BULKHEAD IAW ERS-EM-53MR-4310

Part: FITTING — DAMAGED (RT AILERON) · airframe 37,717 hrs · 32,963 cycles

DAMPER FITTING ON RH AILERON HAT BUSHING HOLE DAMAGED-C/A-RAR THE DAMAGED RH AILERON DAMPER FITTING IAW EMB 145 SRM 51-40-02,51-20-03, AND EO-EM-27MR-112

Part: HINGE FITTING — DAMAGED (LT AILERON) · airframe 37,717 hrs · 32,963 cycles

LH AILERON INBD INBD HINGE FITTING OUTBD HAT BUSHING HOLE DAMAGED-C/A-RAR THE DAMAGED LH AILERON INBD HINGE FITTING IAW EO-EM-27MR-112

Part: FLOOR SUPPORT — CORRODED (FRMS 30-36) · corrosion level 2 · airframe 37,717 hrs · 32,963 cycles

CENTER OMEGA BEAM #2 GUSSET IS CORRODED (LEVEL2 CORRROSION)-C/A-ACCOMPLISHED PERMANENT REPAIR FOR CENTER OMEGA BEAM #2 GUSSET IAW ERS-EM-53MR-4313

Part: SEAT TRACK — CORRODED (FRM 50) · corrosion level 2 · airframe 37,717 hrs · 32,963 cycles

LH UPPER SEAT TRACK SUPPORT AT FR 50 IS CORRODED.CORROSION LEVEL 2-C/A-REMOVED AND REPLACED LH UPPER SEAT TRACK SUPPORT FOR FR 50 IAW EMB 145 SRM 51-40-02

Part: STRINGER — GOUGED (FRAMES 20-21 S2L) · airframe 37,717 hrs · 32,963 cycles

STGR 2L GOUGED BETWEEN FR 20-21-C/A-REMOVED AND REPLACED GOUGED STGR 2L BETWEEN FRAMES 19-24 IAW EMB 145 SRM 51-40-02

Part: BULKHEAD — DAMAGED (COCKPIT) · airframe 37,717 hrs · 32,963 cycles

PILOTS BULKHEAD UPPER AND LOWER GUIDE PIN HOLES ELONGATED-C/A-FABRICATED AND INSTALLED REPAIR DOUBLERS FOR PILOTS BULKHEAD UPPER AND LOWER GUIDE PIN HOLES IAW EMB 145 SRM 53-21-02 AND ETN-EM-53-153R1

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 37,717 hrs · 32,963 cycles

SSI 53-30-48 AIRCRAFT STRUCTURE CARGO DOOR CUTOUT FR 65 SHEAR CLIP LOWER CORNER CORRODED. CORROSION LEVEL 2-C/A-REMOVED AND REPLACED DAMAGED SECTION OF CARGO DOOR CUTOUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04.

Part: SHEAR TIE — CORRODED (FRM 68) · corrosion level 2 · airframe 37,717 hrs · 32,963 cycles

SSI 53-30-48 AIRCRAFT STRUCTURE CARGO DOOR CUTOUT FR 68 SHEAR CLIP LOWER CORNER CORRODED. CORROSION LEVEL 2-C/A-REMOVED AND REPLACED DAMAGED SECTION OF CARGO DOOR CUTOUT FR 68 SHEAR CLIP IAW EMB 145 SRM 53-31-04.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-68) · airframe 37,717 hrs · 32,963 cycles

SSI 53-30-48 AIRCRAFT STRUCTURE CARGO DOOR LOWER FLOOR SILL CORRODED.CORROSION LEVEL 2 -C/A-REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02

Part: ACCESS PANEL — GOUGED (RT PYLON) · airframe 37,717 hrs · 32,963 cycles

RH PYLON PREVIOUS REPAIR DOUBLER INSIDE ACCESS PANEL 424DB IS GOUGED. -C/A-REMOVED DAMAGED DOUBLER AND FABRICATED NEW DOUBLER IAW EMB 145 SRM 51-40-02 AND ETD# ETD2014-145-072880. INSTALLED SERVICEABLE DOUBLER FOR PREVIOUS REPAIR INSIDE RH PYLON ACCESS PANEL 424DB IAW ERS-EM-53MR-4307.

Part: RIB — CRACKED (RT WING) · airframe 37,717 hrs · 32,963 cycles

RH WING RIB 21 IS CRACKED INSIDE PANEL 651CB. CRACK LENGTH 0.25 NUMBER OF CRACKS 1-C/A-REPAIRED RH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4.

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 37,717 hrs · 32,963 cycles

SSI 53-200-29 TOILET WASTE VALVE SUPPORT IS CORRODED ON EXTERNAL SKIN. CORROSION LEVEL 2-C/A-REMOVED AND REPLACED WASTE VALVE SUPPORT IAW EMB 145 SRM 51-40-02

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,516 hrs · 32,751 cycles

EMERGENCY LIGHT ON ROW 12A PSU PANEL INOPERABLE. C/A: R & R OVERWING EMERGENCY LIGHT BULB ON ROW 12A PSU PANEL, IN REF WITH EMB 145 AMM 33-50-07. OPERATIONS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,430 hrs · 32,654 cycles

FWD OVERWING OVERHEAD EMERGENCY EXIT LOCATOR SIGN INOPERABLE. C/A: R & R NR 6 INVERTER, IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: CONTROL PANEL — DAMAGED (EMERGENCY LIGHTS) · airframe 37,298 hrs · 32,518 cycles

EMERGENCY LIGHT PANEL ON MAIN DOOR DAMAGED. C/A: R & R EMERGENCY LIGHT PANEL ON MAIN DOOR. OPERATIONS CHECK GOOD, IAW AMM 25-23-04.

Part: UNKNOWN — NOISE (COCKPIT/CABIN) · airframe 37,019 hrs · 32,223 cycles

HEARD INTERMITTENT WHISTLING NOISE IN CABIN AND COCKPIT, MOSTLY DURING CLIMB AND DESCENT. C/A: CLEANED MAIN CABIN DOOR SEAL, IAW EMB-145 AMM 52-00-04. PRESSURIZED A/C, IAW EMB-145 AMM 21-31-00. NO AIR LEAK NOTED AT THIS TIME.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 36,663 hrs · 31,825 cycles

FOUND FLASHLIGHT ABOVE FLIGHT ATTENDENT SEAT BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: BRACKET — DAMAGED (FLASHLIGHT) · airframe 36,561 hrs · 31,712 cycles

AFT CABIN FLASHLIGHT BRACKET DAMAGED-C/A-AFT CABIN FLASHLIGHT ASSY REMOVED AND REPLACED IAW EMB145 AMM 33-50-16 AND ETN-EM-33-059. OPC GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,266 hrs · 31,437 cycles

WHILE REMOVING FLOOR PANEL FOR RECIRC FAN MEL DAMAGED EMERGANCY LIGHT STRIP #4-C/A-DERFERED PER MEL 33-30 NO "M' PROCEDURES APPLICABLE. REMOVED AND REPLACED #4 EMERGENCY FLOOR STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MEL RESTORED

Part: PRINTER — FAILED (COCKPIT) · airframe 36,236 hrs · 31,417 cycles

SUPPLEMENTAL AT 37000FT CRUISE THE 115 VAC BUS OFF, CAME ON THE EICAS - STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN-C/A-FOUND PRINTER TO BE THE CAUSE OF BURNING SMELL PLACED PRINTER ON MEL. DEFERRED PRINTER 23-06 MAINTENANCE ACTION COMPLIED WITH COLLARED CB J7. REMOVED AND REPLACED ACARS PRINTER IAW AMM 23-22-02 OPC GOOD MEL RESTORED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,083 hrs · 31,284 cycles

CALLEY CEILING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED GALLEY CEILING EMERGENCY LIGHT LAMP IAW EMB 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: CRADLE — DAMAGED (AFT FLASHLIGHT) · airframe 35,599 hrs · 30,825 cycles

AFT CABIN FLASHLIGHT CRADEL DAMAGED-C/A-PEFORMED VISUAL INSPECTION OF THE FLASHLIGHT ASSEMBLY IN AFT AND FOUND BRACKET TO BE DAMAGED. REMOVED AND REPLACED BRACKET REF CMM 25-60-14. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,372 hrs · 30,655 cycles

LH #1 EMERGENCY LIGHT STRIP NOT WORKING.-C/A-REMOVED AND REPLACED LH #1 EMERGENCY LIGHT STRIP IAW EMB AMM 33-50-12. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (BRAKE SYSTEM) · airframe 34,188 hrs · 29,651 cycles

EMER BRK LO PRES RETURNED AFTER HYD 1ST FLIGHT OF DAY TEST AND NO BRAKE ACCUATION. C/A-ITEM DEFERRED PER MEL 32-5 (MEL REOPENED) TDMI 939T3288 OPENED TO CHECK ACCUM PRECHARGE EACH FLT DAY. "M PROCEDURES C/W AUTH# 040981M-C. TROUBLESHOT IAW EMB FIM 32-44-00-810-801-A REMOVED AND REPLACED LOW PRESSURE SWITCH IAW AMM 32-44-05-000-801-A AND 32-44-05-400-801-A REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 32-44-07-000-801-A AND 32-44-07-400-801-A NO FIX REMOVED AND REPLACED NR 1 AND NR 2 BRAKE REF NRWC 939-CMI-03939 NO FIX NO FURTHER TIME TO TROUBLESHOOT MEL REMAINS OPEN RESTABLISHED M PROCEDURES. REMOVED AND REPLACED ACCUMALATOR NR 2 LOW PRESSURE SWITCH IAW AMM 32-44-05 OPERATIONAL AND LEAK CHECK GOOD MEL#32-5 AUTH$ 040981M-C RESTORED. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLY IAW W/C 32-600-14 OPC GOOD LEAK CHECK GOOD NO OTHER DEFECTS NOTED. SWITCH P/N 15851 S/N 2209. LR MAIN BRAKE ASSY P/N 2-1707-2 S/N 0706 (1) AND S/N 1927 (2)

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG WOW) · airframe 33,786 hrs · 29,224 cycles

LG AIR/GND FAIL IN FLIGHT AFTER GEAR EXTENSION "TRANSFERRED TO NRWC 939-ORD-03774"-C/A-FOUND LH MLG FRONT WOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED LH MLG FRONT WOW PROXIMITY SWITCH IAW EMB 32-63-05. ALL OTHER WOW PROX SWITCHES WITHIN LIMITS. AIR GROUND SYSTEM OPS CHECK GOOD IAW EMB AMM 32-63-00. ALSO SWUNG GEAR IAW EMB AMM 32-30-00 TO MONITOR NLG TIRES POSSIBLY RUBBING ON DOORS WITH NO FAULTS FOUND.

Part: COUPLING — NOT REPORTED (AC BAY) · airframe 33,478 hrs · 28,930 cycles

UPON CLIMBOUT OUT ENTERING ICING CONDITIONS WE RECIVED BLEED 2 VALV CLOSED FOLLOWED BY WING ANTICE FAIL CAUTION AFT THAT WE GOT BLEED LEAK 2 WARRING AND ICE CONDITION AI INOP WARRING RAN CHECK LIST DID NOT GO AWAY UNTIL EXITING ICING CONDITION. C/A-INSTALLED NEW RUBBER COUPLING NR 2 ACM LOCATION NR 10 OPS CEHCK LEAK CHECK FROUND IAW AMM 21-51-00 OPS CEHCK GOOD OF ANT ICE SYSTEM IAW CH 30-00-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,294 hrs · 28,761 cycles

EMERGENCY AREA LIGHT AT EXIT ROW INOP-C/A-REMOVED AND REPLACED EMERGENCY AREA LIGHT AT EXIT ROW LIGHT BULB IAW EMB 145 AMM 33-50-08 OPS CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · airframe 33,293 hrs · 28,760 cycles

RH OMEGA BEAM CORRODED AROUND NUTPLATE HOLE AT FR 19-C/A-REPAIRED RH OMEGA BEAM AT FR 19 IAW ERS-EM-53MR-3498.

Part: YOKE — CRACKED (RT NACELLE) · airframe 33,293 hrs · 28,760 cycles

RH PYLON FWD LOWER PYLON YOKE HAS CRACK.-C/A-REMOVED AND REPLACED RH PYLON FWD LOWER PYLON YOKE IAW ENVOY ERS-EM-54MR-698.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,293 hrs · 28,760 cycles

LH ELEVATOR HAS A HOLE ON UPPER SKIN LWR EDGE OTBD BTW TWO STATIC WICS-C/A-REMOVED AND REPLACED LH ELEVATOR OTBD UPPER SKIN IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. PREPPED AND APPLIED PROTECTIVE COATING IAW EMB 145 CPM 51-21-06, ETN GN-51-017

Part: SKIN — CRACKED (FRAME 77) · airframe 33,293 hrs · 28,760 cycles

RH FUSELAGE AFT SKIN CRACKS AROUND RIVET HEADS ON FRAME 77-C/A-REPAIRED RH FUSELAGE AFT SKIN CRACKS AROUND RIVET HEADS ON FRAME 77 IAW ENVOY ERS-EM-53MR-3496.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,293 hrs · 28,760 cycles

CEILING PANEL EMERGENCY LIGHTS INOP AT 12ABC AND 16ABC.-C/A-COMPLETE:REMOVED AND REPLACED CEILING PANEL EMERGANCY LIGHT BULB AT 16BC. 12BC FOUND NO DISCREPANCY. IAW EMB 145 AMM 35-50-08.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 33,293 hrs · 28,760 cycles

#1 AND #2 EMERGENCY PROX STRIP LIGHTS HAVE DAMAGED WIRES-C/A-COMPLETE:UPON FURTHER INVESTIGATION, FOUND ONLY #1 EMERGENCY PROX LIGHT STRIP TO BE DAMAGED. REPLACED CONNECTOR IAW EMB 145 SWPM 20-21-00. OPC GOOD. EASI #6277 S/N 7859.

Part: CROSSBEAM — CORRODED (FRAME 20) · airframe 33,293 hrs · 28,760 cycles

CROSSBEAM AT FR 20 HAS MULTIPLE AREAS OF CORROSION.-C/A-COMPLETE:REMOVED CORRODED CROSSBEAM AT FRAME 20 AND INSTALLED SERVICEABLE CROSSBEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 33,293 hrs · 28,760 cycles

#5 AND #6 CENTER ISLE EMERGENCY EXIT LIGHTS HAVE BROKEN/REMOVED CONNECTORS ON AIRCRAFT SIDE-C/A-COMPLETE:REPAIRED #5 AND #6 CENTER ISLE EMERGENCY EXIT LIGHT WIRING IAW EMB 145 SWPM 20-21-00, OPC GOOD.

Part: DOOR SEAL — LACK OF LUBE (CABIN DOOR) · airframe 32,969 hrs · 28,441 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR AND FRAME SEAL IAW AMM 52-18-00 DOOR OPS CHECK GOOD.

Part: CLAMP — UNSECURE (DUCT) · airframe 32,860 hrs · 28,326 cycles

DURING ICE TEST, CABIN DEPRESSURIZED. EMERGENCY DECLARED. PERFORMED A PRESSURIZATION CONTROL SYS TEST WITH CREW, OPERATED NORMALLY. NO DEFECTS NOTED. NR 2 ENGINE ANTI-ICE VALVE WOULD NOT OPEN DURING TEST. NO ASSOCIATED EICAS MESSAGES DISPLAYED. FOUND NO CORRELATED CMC MESSAGE. FOUND V-BAND CLAMPS SECURE, BUT ADJUSTABLE CLAMPS FOR BOTH DUCTS WERE LOOSE AND DUCT WAS NOT SECURED ON EITHER SIDE. SECURED THE ADJUSTABLE CLAMPS IAW IAW AMM 30-21-01-400-801-A. PERFORMED THREE GOOD OPS CHECKS IAW AMM 30-00-00-700-802-A/500.

Part: BRAKE ASSY — DEFECTIVE (MLG) · airframe 32,647 hrs · 28,142 cycles

DURING HIGH SPEED TAXI BOTH INBOARD BRAKES RISE TO AMBER RANGE AND OUTBOARD BRAKES REMAIN IN GREEN, AFTER APPROX 10 MIN COOLING NR 3 BRAKE REMAINS IN AMBER RANGE AND REMAINING BRAKES RETURN TO GREEN RANGE. REMOVED AND REPLACED NR 3 BRAKE ASSY IAW W/C 32-600-1. REMOVED AND REPLACED NR 4 BRAKE ASSY IAW W/C 32-600-14. REMOVED AND REPLACED NR 4 MLG BRAKE HYD FUSE IAW AMM 32-41-07 OPS AND LEAK CHECKS GOOD. PERFORMED HIGH SPEED TAXI. NO NR 3 BRAKE TEMP INDICATION SHOWED NORMAL INDICATION. ALL OTHER BRAKE INDICATIONS NORMAL . OPS CHECK GOOD. LT MAIN BRAKE ASSY NR 4 P/N 2-1707-2 S/N 1757; HYDRAULIC FUSE P/N 38-791500 S/N 3929.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 32,002 hrs · 27,498 cycles

EMERGENCY LIGHTS 4 AND 5 INOPERATIVE. REMOVED AND REPLACED THE NR 5 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,804 hrs · 27,313 cycles

EMERGENCY FLOOR PROXIMITY LIGHTS 2, 3, 4, AND 5 INOPERATIVE. REMOVED AND REPLACED THE NR 2 AND 3 CHARGER AND BATTERIES IAW WC 33-700-19, OPS CHECKED GOOD.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 31,790 hrs · 27,301 cycles

LANDING GEAR AIR GROUND FAILED IN FLIGHT, AFTER LOWERING GEAR. REMOVED AND REPLACED LGEU IAW AMM 32-32-01, NO MESSAGE ON EICAS AND LANDING GEAR POSITION INDICATION SHOWED GREEN AND DOWN.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,544 hrs · 27,110 cycles

NR 4 AND 5 FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 3 BATTERY PACK AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: TARGET — OUT OF ALIGNMENT (WOW SWITCH) · airframe 31,094 hrs · 26,653 cycles

LANDING GEAR AIR-GROUND FAIL AFTER TAKEOFF, FOLLOWED BY A NR 1 & 2 ENGINES REVERSER DISAGREE. FOUND THE NOSE LANDING GEAR AIR/GROUND WOW PROXIMITY SENSOR TARGET OUT OF ALIGNMENT. PERFORMED ADJUSTMENT OF THE TARGET IAW AMM 32-63-05. OPS CHECKED GOOD.

Part: BRAKE — LOCKED (NR 3) · airframe 30,890 hrs · 26,422 cycles

DURING LANDING ROLLOUT, A MODERATE UNCOMMANDED BRAKING WAS NOTED THEN DURING TAXI AIRCRAFT. NR 3 BRAKE TEMP INDICATOR QUICKLY ROSE TO MAX SCALE, WITH EICAS MESSAGE. NR 3 BRAKE APPEARS TO BE LOCKED. COULD FEEL THE BRAKE DRAGGING & LOCK WHILE TRYING TO TAXI. REPLACED THE NR 3 MAIN WHEEL ASSY AND BRAKE IAW W/C 32-700-11 AND 32-600-14. OPS CHECKED GOOD IAW NRWCS 939-ORD-03009, 939-ORD-03010, AND 939-ORD-03010.

Part: WARNING MESSAGE — FALSE INDICATION (LT MLG BRAKES) · airframe 30,846 hrs · 26,378 cycles

BRAKE OVERHEAT DURING CLIMB LOWERED GEAR AND TEMP SLOWLY RETURNED TO GREEN. ( LEFT INBOARD) RETRACTED GEAR. AFTER LANDING, BRAKE OVERHEAT CAUTION RETURED AND 1B TEMP GAUGE WENT TO MAX, CONTINUED FROM ABOVE BRAKE TEMP, RETURNED TO NORMAL GREEN WITHIN 5 MINUTES OF LANDING. DECLARED EMERGENCY. TROUBLESHOT BRAKE SYS WARNING, FOUND TO BE INDICATION PROBLEM.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 30,624 hrs · 26,204 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-50-10.

Part: APU — FAILED · airframe 30,104 hrs · 25,679 cycles

VERY STRONG ODOR OF UNBURNED FUEL IN COCKPIT DURING STARTING APU. HAPPENED MULTIPLE FLIGHTS. FOUND OIL LEAKING FROM AFT APU LUBRICATION LINE. VERIFIED ODOR TO BE OIL FROM APU. REMOVED AND REPLACED APU, OPS AND LEAK CHECKED GOOD IAW WC 49-800-05.

Part: FAN — FAILED (RECIRCULATION) · airframe 29,911 hrs · 25,559 cycles

A STRONG ELECTRICAL BURNING ODOR FILLED THE COCKPIT. DISIPATED WHILE ON OXYGEN. FLIGHT ATTENDANT NOTED THE ODOR AS WELL. PERFORMED ETN-EM-72-034, REMOVED AND REPLACED THE NR 1 PACK RECIRCULATION FAN IAW AMM 21-24-01. OPS CHECKED AIR CONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-20-00. OPS CHECKED GOOD. NO ODOR NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,666 hrs · 25,349 cycles

SERVICE DOOR SWING ARM, EMERGENCY LIGHT INOPERATIVE. FOUND WIRE W716-0008-20 BROKEN, REMOVED AND REPLACED FULL LENGTH OF WIRE IAW WM 20-21-00. OPS CHECKED GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,284 hrs · 24,980 cycles

EMERGENCY LIGHTS NR 7 AND 8 INOPERATIVE. R & R THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,255 hrs · 24,955 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. R&R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09. OPS GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,198 hrs · 24,905 cycles

AFT CABIN FLASHLIGHT INOP. FLIGHT CREW PLACARDED AFT CABIN FLASHLIGHT. REMOVED AND REPLACED AFT CABIN FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKS GOOD. MEL RESTORED.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 29,115 hrs · 24,849 cycles

EMERGENCY LIGHTS AT ROW 12A TO REAR INOPERATIVE REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER IAW W/C 32-700-19.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 28,857 hrs · 24,626 cycles

AT AROUND 23,000 FEET AUTOPILOT FAIL AND RUDDER 1-2 FAIL. COMPLIED WITH AOM 1 PROCEDURES LEAD US TO TURN SYS 1 AND 2 OFF. NORMAL OPS WITH SYS 2 OFF.. EXCESSIVE YAW WITH BOTH SYS OFF. TURNED SYS 1 BACK ON AND PROCEEDED TO DIVERSION AIRPORT UNDER NORMAL CONDITIONS. REMOVED AND REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPS CHECK AND LEAK CHECK GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 28,813 hrs · 24,597 cycles

FLIGHT ATTENDANT FLASHLIGHT CRADLE CRACKED. R & R THE FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,612 hrs · 24,402 cycles

PILOTS FLASHLIGHT INOPERATIVE. R & R PILOTS FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 28,538 hrs · 24,340 cycles

HYD SYS 1 QTY WENT TO ZERO. HYD SYS 1 FAIL, RAN LIST, EMERGENCY LANDING GEAR EXTENSION. FOUND NR 1 HYDRAULIC PUMP PRESSURE LINE CHAFED. R & R PRESSURE HOSE IAW MM 29-10-03. NO LEAKS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,404 hrs · 24,225 cycles

CABIN DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR SWING ARM SHROUD, CONTAINING EMERGENCY LIGHT IAW AMM 25-23-04. EMERGENCY LIGHTS, OPS CHECK GOOD IAW AMM 33-50-00.

Part: CLAMP — LOOSE (ANTI-ICE SYSTEM) · airframe 28,403 hrs · 24,223 cycles

WING ANTI-ICE FAIL CAUTION MSG IN CLIMB DURING A VERY SHORT ICING DETECTION CYCLE. DEFERRED WING ANTI-ICE IAW MEL 30-1, AUTH 070065D-C. CMC=WING 1 A/I LEAK. INSPECTED ECS1 AREA WITH PACK ON, FOUND LARGE LEAK FROM EXHAUST SHROUD COUPLER SPRAYING ON A/I LEAK DETECTED, TIGHT END CLAMP AND SECURED LEAK. A/I SYSTEM REQ OPS CHECK IAW AMM CH 30-00-00-700-802-A, GROUND PNEUMATIC CHECK, MEL REMAINS OPEN. PERFORMED OPS TEST OF WING ANTI-ICING SYSTEM IAW AMM 30-00-00-700-802-A, OPS CHECK GOOD. THIS RESTORES MEL 30-1.

Part: BULB — UNSECURE (FLASHLIGHT) · airframe 27,910 hrs · 23,802 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT DOES NOT TURN ON. AT THIS TIME SECURED FWD FLIGHT ATTENDANT FLASHLIGHT BULB. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: BATTERY — OVERTEMP (MAIN) · airframe 26,999 hrs · 22,979 cycles

ENROUTE CREW RECEIVED EICAS BATT 1 OVERTEMP WARNING MSG PEAK AT 114C. CREW CONTACTED SOC & MOC & THE DECISION TO DIVERT WAS MADE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R NR 1 MAIN BATTERY, OPERATION CHECKED GOOD IAW WC 24-600-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,717 hrs · 22,708 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT IAW SMP.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,246 hrs · 22,263 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 25-60-11. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,019 hrs · 22,039 cycles

FLIGHT ATTENDANT FWD FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED OK.

Part: UNKNOWN — FUMES (CABIN) · airframe 25,897 hrs · 21,928 cycles

LAVATORY SMOKE INDICATION IN FLIGHT, NO CABIN SMOKE, PERSISTENT ALERT. FLIGHT ATTENDANT REPORTED ABNORMAL FUMES, NOT BURNING SMELL REAR OF ACFT. REPORTED INCREASED TEMPERATURE. DIVERTED & CFR REPORTED NO SMOKE OR FIRE, EXTERIOR OR INTERIOR, WITH THERMAL IMAGING EQUIP, LAVATORY SMOKE INDICATION STILL PRESENT. INSPECTED SMOKE DETECTOR & AREA, NO EVIDENCE OF SMOKE OR FIRE. LAVATORY SMOKE DETECTION SYS COMPLIED WITH OPERATIONS CHECK IAW AMM 26-14-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 25,814 hrs · 21,859 cycles

MAIN ENTRY DOOR DIFFICULT TO OPEN & CLOSE. LUBE MAIN DOOR FRAME ROLLERS IAW MM 53-21-02. OPERATIONS CHECKED GOOD IAW MM 52-18-00.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,571 hrs · 21,647 cycles

CAPTAIN DV WINDOW HAS CRACK ON LOWER EDGE. R & R CAPTAIN EMER EXIT DV WINDOW IAW AMM 56-11-01. LEAK CHECKED GOOD.

Part: PLATE — DAMAGED (LT PYLON) · airframe 25,429 hrs · 21,490 cycles

NUMBER 1 ENG FWD PYLON YOKE HAS RUB DAMAGE, HEAD DAMAGE, TO A JO-BOLT FASTENER LOCATED ON THE LOWER AFT SECTION ABOUT 3RD UP FROM THE BOTTOM. COMPLIED WITH ERS EM-54MR-310 TEMPORARY REPAIR OF LT PYLON FWD YOKE GUSSET PLATE & FASTENER. DEFERRED IAW ERS-EM-54MR-310.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 25,000 hrs · 21,157 cycles

NUMBER 4 POWER SUPPLY REQUIRES REPLACEMENT IAW ITEM 1. R & R E BATTERY POWER SUPPLY NR 4 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,000 hrs · 21,157 cycles

GATE AGENT REPORTS EMER LIGHTS ON BATTERY DEAD. R & R EMER BATTERY POWER SUPPLY 1 IAW AMM 33-50-04. PERFORMED OPERATIONS CHECK IAW AMM 33-50-04. OK FOR SERVICE. REF ITEM 2, 3 & 4 FOR OTHER POWER SUPPLY REMOVAL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 25,000 hrs · 21,157 cycles

NUMBER 2 EMER BATTERY POWER SUPPLY REQUIRES REMOVAL IAW ITEM 1. R & R E BATTERY POWER SUPPLY NR 2 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 25,000 hrs · 21,157 cycles

NUMBER 3 POWER SUPPLY REQUIRES REPLACEMENT IAW ITEM 1. R & R BATTERY POWER SUPPLY NR 3 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (LT SPOILER) · airframe 25,007 hrs · 21,160 cycles

DURING DESCENT EICAS MSG, SPOILER FAIL, PRESENTED. SPOILERS DID NOT INDICATE OPEN. AOM 1 PROCEDURES COMPLIED WITH. POST FLIGHT INSPECTION FOUND THE RT INBD SPOILER PANEL FLOATING SLIGHTLY UP. NO OTHER DEFECTS NOTED. R & R LT OTBD PROX SWITCH & CONNECTOR IAW AMM 27-63-04, SWPM 20-50-00 & 20-50-05. OPERATIONS CHECKED GOOD. SPOILER PANELS ALL NORMAL NO DEFECTS NOTED. LT OTBD PROX SWITCH PIN BROKEN FOUND.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,936 hrs · 21,099 cycles

EXIT MARKING SIGN ABOVE FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMER LIGHT DC & AC INVERTER 1, INSTALLED ON THE RT SIDE OF THE FUSELAGE, BETWEEN THE TCAS COMPUTER & THE COCKPIT WALL IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

CARGO DOOR SILL HAS SPOTS OF CORROSION. R & R CARGO DOOR SILL IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06 & ETN-EM-51-091.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 24,107 hrs · 20,323 cycles

RIGHT WING TO FUSELAGE PANEL LOWER ATTACH BRACKET AT FRAME 46 IS CRACKED. CRACK APPROX 1 INCH LONG. REMOVED & INSTALLED NEW RT WING TO FUSELAGE PANEL LOWER ATTACH BRACKET AT FRAME 46 IAW SRM 51-40-02 & ETN-EM-53-142 & APPLIED ANTI-MICROBIAL COATING IAW AMM 28-11-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

RIGHT OTBD OMEGA BEAM SUPPORT CRACKED BETWEEN FRAME 47 - 48. R & R RT OMEGA BEAM & SUPPORT IAW SRM 53-23-02 & 51-40-0. SHEAR CLIP PN 140-04213-609.

Part: PLATE — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

SERVICE DOOR SILL PLATE IS CORRODED. R & R SERVICE DOOR SILL PLATED IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (BLEED AIR SYS) · airframe 24,107 hrs · 20,323 cycles

CROSS BLEED VLV SUPPORT BRACKETS TWO EACH ARE CRACKED. R & R CROSS BLEED VLV SUPPORT BRACKETS IAW AMM 20-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

RIGHT OTBD FLOOR SUPPORT AT FRAME 45 IS CORRODED. REPAIRED IAW EMB SRM 53-23-10.

Part: WIRE — BROKEN (CABIN) · airframe 24,107 hrs · 20,323 cycles

WIRE W102-8660 BROKEN NEAR CONNECTOR P8530 GALLEY CEILING SERVICE DOOR EXIT LIGHT CIRCUIT. REPAIRED WIRE IAW SWPM 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

RIGHT OTBD FLOOR SUPPORT BETWEEN FRAMES 35 - 42 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,107 hrs · 20,323 cycles

AFT SIDE OF THE CTR AISLE OVERHEAD EMER EXIT SIGN HAS A DEAD SPOT OF LIGHTING IN THE CTR OF IT. R & R AFT SIDE OF THE CTR AISLE OVERHEAD, CEILING, EMER EXIT SIGN AT THE EMER EXIT ROW. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

RIGHT FLOOR & WALL SUPPORT BETWEEN FRAMES 65 & 68 HAS A SPOT OF CORROSION AROUND NUTPLATE HOLE. REPAIRED RT FLOOR & WALL SUPPORT BETWEEN FRAMES 65 & 68 IAW SRM 53-31-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

LEFT OTBD FLOOR SUPPORT AT FRAME NR 50 IS CORRODED. REPAIRED IAW SRM 53-23-10.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

LEFT FLOOR & WALL SUPPORT BETWEEN FRAMES 73 & 71 HAS A SPOT OF CORROSION AROUND NUTPLATE HOLE. REPAIRED LT FLOOR & WALL SUPPORT BETWEEN FRAMES 73 & 71 IAW SRM 53-31-10.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,107 hrs · 20,323 cycles

LEFT NR 7 PROXIMITY EMER LIGHT STRIP MOUNTING HOLE CRACKED. INSTALLED NEW NR 7 EMER LIGHT STRIP IAW AMM 33-50-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,107 hrs · 20,323 cycles

RIGHT OTBD FLOOR SUPPORT BETWEEN FRAMES 48 - 53 IS CORRODED. REPAIRED IAW SRM 53-23-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,747 hrs · 19,993 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R EMER LIGHT LAMP IN MAIN DOOR IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,222 hrs · 19,492 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT LAMP IAW TASK 33-50-10-000-801-A & TASK 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,874 hrs · 19,200 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 22,426 hrs · 18,854 cycles

DURING TAKEOFF ON FLIGHT 3777, CREW REPORTED TAKEOFF DATA SET SWITCH INOPERABLE ON INC POSITION WHEN BOTH ENGS ARE RUNNING & THE APU IS SHUT DOWN. R & R THE POWER PLANT CONTROL PANEL IAW 145 AMM 76-12-04. OPERATIONS CHECKED SATISFACTORY AT THIS TIME. .

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,345 hrs · 18,796 cycles

ON FLIGHT 2902 THE CREW REPORTED CAPTAIN`S FLASHLIGHT WAS NOT WORKING. THE ACFT WAS REMOVED FROM SERVICE. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16 & OPERATIONS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,983 hrs · 18,504 cycles

REAR FLASHLIGHT HOLDER BROKEN. R & R REAR FLASHLIGHT HOLDER IAW AMM 33-50-16, OPS WORKING GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,450 hrs · 18,047 cycles

CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 12. R & R LAMP IAW AMM 33-50-08.

Part: FAN — FAILED (E/E BAY) · airframe 21,387 hrs · 17,984 cycles

CREW REPORTED ODOR IN COCKPIT & FORWARD CABIN. ODOR IS SIMILAR TO HOT ANTI-FREEZE FLUID. R & R FWD LT AVIONICS FANS IAW AMM 21-26-02. OPS CHECKED GOOD. NO ODORS NOTED.

Part: LIGHT — UNSERVICEABLE (PAX DOOR) · airframe 21,129 hrs · 17,786 cycles

DURING MX INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD IAW AMM 33-50-00-700-801-A. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,129 hrs · 17,786 cycles

DURING MX INSPECTION, FOUND MAIN DOOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD IAW AMM 33-50-00-700-801-A. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 20,961 hrs · 17,645 cycles

FLASHLIGHT HOLDER IN THE COCKPIT BEHIND THE CAPTAIN INOPERATIVE. R & R CAPTAIN’S FLASHLIGHT ASSY IAW AMM 33-50-16 OPS. OPS CHECKED GOOD IAW AMM 33-51-01. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 20,632 hrs · 17,373 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY REQUIRED CHANGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,503 hrs · 16,474 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 23 OMEGA BEAM CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT HAT BEAM IAW EO-EM-53MR-2036. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (CARGO DOORWAY) · airframe 19,526 hrs · 16,496 cycles

CARGO DOOR CUTOUT SHEAR TIE CORRODED AT FR 65. REPAIRED CARGO DOOR CUTOUT SHEAR TIE AT FR 65 IAW EO EM-53MR-1129, PART A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,526 hrs · 16,496 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL L ANGLES AT FRAME 66 AND 67 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL L ANGLES AT FRAME 66 AND 67 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED · airframe 19,504 hrs · 16,474 cycles

CARGO DOOR CUTOUT SHEAR TIE CORRODED AT FR 68. REPAIRED CARGO DOOR CUTOUT SHEAR CLIP AT FR 68 IAW EO EM-53MR-1129, PART B.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,526 hrs · 16,496 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 19,526 hrs · 16,496 cycles

GALLEY RT HAT CHANNEL CORRODED AT FRAME 23. REPAIRED GALLEY RT HAT CHANNEL AT FR 23 IAW EO-EM-53MR-2036, PART A.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,526 hrs · 16,496 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 19,338 hrs · 16,338 cycles

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

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 19,254 hrs · 16,260 cycles

ON FLIGHT 2773 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED SIDE-HINGED MAIN DOOR RUBBER SEAL AND THE FRAME RUBBER SEAL IAW EMB 145 AMM 52-18-00 STEPS 2. J. (3). PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW EMB 145 AMM 52-18-00 STEPS 2. A. THRU K (1). THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,008 hrs · 16,058 cycles

DURING B INSPECTION FOUND THE MAIN DOOR HINGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-10-000-801-A, AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — ODOR (FLASHLIGHT) · airframe 19,006 hrs · 16,055 cycles

ON FLIGHT 4272 THE CREW REPORTED THE CAPTAINS FLASHLIGHT HAS A FOUL SMELL COMING FROM IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAINS FLASHLIGHT BATTERY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE ODOR WAS NO LONGER PRESENT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LGIHT) · airframe 18,999 hrs · 16,044 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR REFLECTANT EMERGENCY EXIT LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR REFLECTANT EMERGENCY LIGHT IAW AMM TASK 33-30-01-000-801-A AND 33-30-01-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 18,873 hrs · 15,940 cycles

ON FLIGHT 3556, THE CREW REPORTED THAT AFTER BECOMING AIRBORNE AFTER TAKEOFF THEY RECEIVED LG AIR/GND FAIL MESSAGE AND LANDING GEAR LEVER COULD NOT BE MOVED. AFTER 10 SEC LG AIR/FAIL MSG WENT OUT. FOLLOWED AOM PROCEDURES AND THE LANDING GEAR EXTENDED NORMALLY BRAKES AND NWS WERE NORMAL. THE CREW DID NOT USE THRUST REVERSER. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW AMM TASK 32-32-01. THE OPERATIONAL CHECK WAS GOOD. FOUND LOOSE BACKSHELLS ON PROXIMITY SENSORS. RESECURED AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,673 hrs · 15,796 cycles

DURING B INSPECTION, FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LAMP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — FAILED (WOW SENSOR) · airframe 18,659 hrs · 15,784 cycles

FLIGHT 4331, CREW REPORTED ON TAKE OFF, RECEIVED A "LANDING GEAR AIR/GND FAIL MESSAGE ON EICAS. LANDING GEAR WAS IN LOCKED DOWN POSITION. CREW RAN CHECKLIST PER AOM VOL 1, DURING WHICH TIME THE MESSAGE EXTINGUISHED ON ITS OWN AND WERE ABLE TO RETRACT THE GEAR NORMALLY. DECLARED AN EMERGENCY. RETURNED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE WHEEL WEIGHT ON WHEELS SENSOR HARNESS. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,563 hrs · 15,700 cycles

ON FLIGHT 4284 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT IN THE FRONT GOES OUT AFTER ONE SECOND. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BATTERY ON FLASHLIGHT DISCHARGED, RE-INSTALLED ON CRADLE, CHARGE BATTERY FOUND TO BE WORKING. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 18,202 hrs · 15,403 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLASHLIGHT BROKEN CLIP ON FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (CABIN) · airframe 18,056 hrs · 15,294 cycles

DURING B-INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT CHARGER HAS A BROKEN LATCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT CHARGER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (FLASHLIGHT) · airframe 17,852 hrs · 15,140 cycles

DURING B-INSPECTION, FOUND THE AFT FLASHLIGHT BATTERY UNSERVICEABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM TASK 33-50-16. OPSL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PLUG — DEFECTIVE (NR 1 ENGINE) · airframe 17,459 hrs · 14,843 cycles

DURING MAINTENANCE INSPECTION NOTED FRESH OIL ON NR 1 ENGINE TURBINE BLADES AFTER CREW REPORTED SMOKE COMING FROM NR 1 ENGINE EXHAUST AFTER SHUTDOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH NR 1 ENGINE RUN TEST IAW ROLLS-ROYCE AMM 72-00-00. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE NR 1 ENGINE SHAFT PLUG IAW RR MM 72-59-15 UP TO AND INCLUDING SUBTASK 72-59-15-410-001. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. PART NUMBERS: GASKET, METAL MS9373-013; GASKET, METAL MS9376-065; PACKING AS3209-122; PLUG SHAFT 23073072.

Part: THERMOSTAT — DEFECTIVE (BLEED AIR SYS) · airframe 17,381 hrs · 14,786 cycles

ON FLIGHT 4361 THE CREW REPORTED THAT ON CLIMBOUT RECEIVED A NR 1 BLEED OVER TEMPERATURE MESSAGE SHORTLY AFTER AIRCRAFT ENTERED ICING CONDITION VERIFIED THAT TEMPERATURE WAS HIGH ON BLEED TEMP INDICATION. WARNING MESSAGE WENT OUT WHEN AIRCRAFT WAS OUT OF ICING CONDITIONS TEMP WAS NORMAL WHEN NOT IN ICING. ATTEMPED AOM 1 PROCEDURE HOWEVER BLEED OVERTEMP WENT OUT. MONITORED TEMPERATURE ON MFDECS BLEED TEMP INDICATION ON REMAINING FLIGHT. ALL WAS NORMAL UNTIL ICING IS ENCOURTERED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FAN AIR CONTROL THERMOSTAT IAW EMB 145 AMM 36-11-06. THE OPERATIONAL CHECK WAS GOOD. REFERENCE TO NRWC# 939-ORD-00722. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,356 hrs · 14,763 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 16,636 hrs · 14,215 cycles

ON FLIGHT 2749 THE CREW REPORTED THAT DURING THE CLIMBOUT RECEIVED A MAIN PITCH TRIM FAIL MESSAGE ON EICAS. ALL OTHER SYSTEMS WORKED NORMAL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL CONTROL UNIT IAW EMB 145 AMM27-40-01. THE OPERATIONAL CHECK WAS GOOD IAW 27-40-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,614 hrs · 14,201 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 16,527 hrs · 14,142 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED FRAME ROLLERS IN REFERENCE TO EMB-145 AMM 52-18-00. NO PARTS REMOVED OR REPLACED. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,846 hrs · 11,340 cycles

TAXIING FOR FLIGHT 9805 DURING THUNDERSTORM WITH AIRCRAFT POWER OFF THE EMERGENCY LIGHTS CAME ON APPROX 1 1/2 HOURS, THEN LIGHTS WENT OUT. CAME OUT POWERED UP PLANE TESTED EMERGENCY LIGHTS AND ALL EMERGENCY LIGHTS ON PLANE FROM ROW 8 TO BACK DIMMED OUT AFTER A FEW SECONDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ALL EMERGENCY BATTERIES NR 1, 2, 3 & 4 IAW EMB 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 7,039 hrs · 6,090 cycles

ON FLIGHT 3869 - CREW DECLARED EMERGENCY DUE TO MOMENTARY LG AIR GND FAIL MESSAGE WHEN GEAR SELECTED DOWN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR AIR GROUND PROXIMITY SWITCH IAW EMB 145 MM 32-63-02-000-801-A. OPS CHECK GOOD IAW 32-63-00-700-801-A. REMOVED AND REPLACED MAIN LANDING AIR/GROUND PROXIMITY SWITCH IAW 32-63-01-000-801-A. OPERATIONAL CHECK GOOD IAW EMB 145 MM 32-00-02-910-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 5,183 hrs · 4,548 cycles

CREW NOTICED OIL BURNING ODOR. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. LEAK AND OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 4,842 hrs · 4,265 cycles

CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB EMB SRM 51-40-02. RETURNED AIRRAFT TO SERVICE.