N660CL

Part: WIRE HARNESS — DAMAGED (ZONE 400) · airframe 46,522 hrs · 43,654 cycles

DURING TAKE OFF CLIMB ENG 2 OIL TEMP TEMP REACHED 133 DEG C. FOLLOWED QRH AND ENG WAS SHUT DOWN. FACT 18JUN25 16:21 CLT R+R'D #2 ENG INDICATING HARNESS IAW RRMM 76-13-15-400-802 + 76-13-15-000-802. PERFORMED ENGINE RUN IAW RRMM 72-00-00-700-801 SUBTASK 72-00-00-710-001. OPS CHECK GOOD AC OK FOR SERVICE

Part: RECEPTACLE — BURNED (WATER WARMER) · airframe 46,223 hrs · 43,305 cycles

AT APPROX 10,000 FT, FA NOTICED STRONG BURNING SMELL FROM FRONT OF CABIN FOLLOWED BY FLT DECK CREW NOTICING ON FLT DECK. REMOVED #100 LIQUID WARMER. RECEPTICAL FOR LIQUID WARMER SHOWS SIGNS OF ARCING, "P8001". INSTALLED NEW LIQUID WARMER CONNECTION RECEPTACLE IAW ZODIAC CMM 25-31-98. REINSTALLED ORIGINAL "P8001" LIQUID WARMER.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,968 hrs · 39,712 cycles

F036819 LH FLOOR BEAM WEB AND LOWER FLANGE CORRODED AT FR38. ACCOMPLISHED REPAIR ON L/H FLOOR BEAM AT FR38 IAW EMB 145 SRM 53-00-10RE, FIGIRE 202, SHEET 2 AND EO1-53-25-0155

Part: VALVE — FAULTED (ZONE 400) · airframe 45,763 hrs · 42,816 cycles

HS VLV 2 FAIL MSG ON EICAS FACT 05FEB25 15:22 CLT R&R'D #2 HSV PER AMM 36-11-02-400-801A PERFORMED OPS CHECKS PER AMM 36-00-00-700-803A ALL CHECKS GOOD. OK FOR SERVICE.

Part: EICAS — FALSE INDICATION (ZONE 200) · airframe 47,079 hrs · 42,588 cycles

LOST EICAS DISPLAY DURING EVALUATION FLIGHT. EMERGENCY DECLARED. FACT 26NOV24 05:11 CLT DURING GROUND RUN EICAS REMAINED NORMAL ACFT OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 45,225 hrs · 42,249 cycles

AIRCRAFT HAS A STRONG ODOR THROUGHOUT POSSIBLE BLEEDS. FACT 01NOV24 12:31 PHL DUMPED AND SERVICED LAV SEVERAL TIMES. RAN BOTH PACKS WITH APU. NO SMELL NOTED. RAN PACKS ON ENGINE BLEEDS NO SMELL NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: O-RING — FAILED (BLEED COUPLING) · airframe 45,223 hrs · 42,247 cycles

ON TAKEOFF ROLL BLD 2 LEAK MSG DISPLAYED ON EICAS. MEL 30OCT24 13:17 AVL C30409 36-1-4 BOTH ENG BLEEDS FACT 31OCT24 01:50 AVL R+R'S BLEED 2 COUPLING O-RINGS UNDER PANEL 272AF IAW AMM 36-11-10. OPS AND LEAK CHECK GOOD. REACTIVATED E1+E2 BLEED VLVS IAW AMM 36-11-05. A/C OK FOR SERVICE CLEAR MEL.

Part: THRUST REVERSER — WARNING MESSAGE (NR 1) · airframe 45,000 hrs · 41,976 cycles

784 - TEMP REPAIR IAW EO1-53-21-0254 & ETD2021-145-030320 PERFORMED AT TAT:47747 AND TAC 44977 REQUIRES REPLACE OF PART 145-21873-007 AT FRAME 73 SUPPORT BRACKETS AT STR 16R AT OR BEFORE 5000 FC. REPLACED SUPPORT BRACKET IAW SRM 51-40-02.

Part: THRUST REVERSER — WARNING MESSAGE (ZONE 600) · airframe 44,969 hrs · 41,937 cycles

APPROXIMATELY 60 KNOTS ON TAKE OFF ROLL. E1 REVERSE DISAGREE DISPLAYED ON EICAS, AND NO TAKE OFF CONFIG. C/W MEL PROCEDURE DEACT AND STOW E1 T/R IAW AMM TASK 78-31-01-980-801-A. MEL 07SEP24 16:55 SBY C25113 78-2 ENG 1 OR 2 REV DISAGREE MESSAGES FACT 14SEP24 06:07 MDT C/W FIM TASK 78-30-00-810-814-A. R/R'D DAU #2 IRT AMM 31-41-01 OPS CHECK GOOD. CYCLED T/R'S MULITPLE TIMES MESSAGE DID NOT REAPPEAR, OK FOR SERVICE AT THIS TIME. (REACTIATED E1 T/R IRT AMM TASK 78-31-01-980-801-A)

Part: YOKE — DAMAGED (ZONE 400) · airframe 44,951 hrs · 41,917 cycles

RH PYLON YOKE FWD AND AFT FASTENER HOLES REQUIRE REAMING. REPAIRED IAW EO1-54-24-0497

Part: SKIN — GOUGED (ZONE 100) · airframe 44,951 hrs · 41,917 cycles

00104 FUSE SKIN IS GOUGED AT FR73 STR20L. REPAIRED IAW EO1-53-24-0478

Part: SLEEVE — LEAKING (ANTI-ICE DUCT)

THE WING ANTI ICE FAILED IN ICING CONDITIONS. FACT 17APR24 00:09 CLT UPON INSPECTION FOUND SLEEVES LEAKING BLEED AIR ON Y-PIPE @DTCV REMOVED AND REPLACED SLEEVES IRT AMM 21-60-01. LEAK CHECK GOOD, PERFORMED A/I VALVES OPS CHECK IAW AMM 30-00-00-700-803-A. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: RELAY — FAULTED (TAT SENSOR) · airframe 44,352 hrs · 41,247 cycles

TAT 1 INOP. CLEARED ON ITS OWN. FOUND TAT 1 C/B POPPED OUT. PUSHED IT BACK IN. A/C OK FOR SERVICE AT THIS TIME. R/R RELAY K0064 IAW AMM 20-13-02. TAT SENSORS OPS CHECK GOOD IAW AMM 30-33-00. OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,853 hrs · 40,702 cycles

NEW CREW FOR A/C NOTICED STRONG FUEL SMELL IN THE GALLEY AREA, FLIGHT DECK, AND THROUGHOUT THE CABIN. SMELL WAS NOTICED WITH APU RUNNING WITH PACK 2 ON. TURNED OFF APU/PACK AND APPLIED PC AIR AND SMELL DISAPATED. FACT: RAN APU AND BOTH #1 AND #2 PAXES. NO FUEL SMELL NOTEDIN CABIN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,993 hrs · 39,696 cycles

ON CLIMBOUT #2 ENGINE OIL TEMP REACHED 140C. R&R ENGINE #2 OIL TEMP/PRESSURE SENSOR IAW ROLLS-ROYCE MM 79-31-10. OPS CHECK GOOD. OK FOR SERVICE. DOWNLOADED CMC WITH NO EXCEEDANCE MESSAGES FOUND.

Part: RELAY — FAILED (AIR/GROUND) · airframe 41,696 hrs · 38,262 cycles

YOKE UNLOCK WITH GUST LOCK ENGAUGED INTERMITENLY. FOUND AIR/GRND POSN RELAY K0831 FAILING INTERMITTANTLY CAUSING GUST LOCK INTERLOCK RELAY TO CYCLE. R/R'D RELAY K0831 IAW AMM 20-13-02-04. OPS CHECKS GOOD PER AMM TASK 27-71-00-700-801-A. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UPLOCK — FAULTED (MLG) · airframe 41,168 hrs · 37,656 cycles

LANDING GEAR LEVER DISAGREE MSG FOR RIGHT MAIN. FOLLOWED QRH, ISSUE REMAINED. R/R RT MAIN UPLOCK BOX REF 32-33-10 AND R/R UPLOCK POSITION SWITCHES REF 32-61-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E911537 - LH ELEVATOR LWR INBD SKIN HAS AN OIL CANNED DENT BTW RIB 73.0% AND TRAILING EDGE, BTW RIB YH=-1595.0 AND RIB YH=-1880.0 .... REPAIRED LH ELEVATOR LWR INBD SKIN AN OIL CANNED DENT BTW RIB 73.0% AND TRAILING EDGE, BTW RIB YH=-1595.0 AND RIB YH=-1880.0 IAW PIEDMONT EO1-55-22-0068

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E909508 - LH ELEVATOR LOWER INBD AFT SKIN IS CRACKED .... REMOVED AND REPLACED LH ELEVATOR LOWER INBOARD AFT SKIN IAW PIEDMONT EO1-55-22-0067.

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E907210 - EVIDENCE OF CRACK AT TWO FASTENERS ON THE LH SIDE AT FRAME 78 .... INSTALLED SKIN BUSHING (1 LOCATION) ON THE LH SKIN AT FRAME 78 AT LOWER FASTENER LOCATED 1" BELOW STR 6L IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0053.

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E907209 - EVIDENCE OF CRACK AT TWO FASTENERS ON THE LH SIDE AT FRAME 77 .... INSTALLED 2 SKIN BUSHINGS ON LH SKIN AT FRAME 77 AT 2 FASTENER HOLE LOCATIONS IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0053.

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E908787 - LH FWD ENGINE PYLON SPAR II YOKE UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE .... REAMED LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE TO 1ST OVERSIZE TO REMOVE DAMAGE AND INSTALLED REPAIR BUSHINGS IAW EMBRAER SB145-54-0008 FIGURE 2 STEPS 1-9 AND EO1-54-22-0057. INCORRECT ATA CODE GIVEN. PLEASE CORRECT ATA CODE TO 5420 FROM 5340

Part: NONE — NONE · corrosion level 2 · airframe 40,661 hrs · 37,113 cycles

E907791 - SSI 53-20-13 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATES HOLES .... RAR SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 40,661 hrs · 37,113 cycles

E907197 - SSI 53-20-29 EVIDENCE OF CORROSION ON THE LAV BUCKET AT THE WASTE DRAIN HANDLE .... RAR LAV BUCKET STIFFENERS AND LAV BUCKET IAW EMB 145 SRM 51-20-03, 51-40-02, , 51-40-06, AND 51-40-09.

Part: NONE — NONE · airframe 40,661 hrs · 37,113 cycles

E907711 - POSSIBLE CRACK ON FRAME 66 AT STRINGER 16R .... REMOVED AND REPLACED FR66 (LOWER FRAME SECTION) IAW EMB145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 40,661 hrs · 37,113 cycles

E907832 - LEFT HAND LOWER SEAT TRACK CORRODED BETWEEN FRAME 18 TO 23 .... REMOVED AND REPLACED LEFT HAND LOWER #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: NONE — NONE · corrosion level 2 · airframe 40,661 hrs · 37,113 cycles

E907833 - LEFT-HAND UPPER SEAT TRACK CORRODED BETWEEN FRAME 20 AND 21 .... REMOVED AND REPLACED LEFT-HAND #1 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · corrosion level 2 · airframe 40,661 hrs · 37,113 cycles

E908064 - RIGHT HAND LAVATORY GUSSET CORRODED AT FORWARD AND AFT NUTPLATES AND AT POTABLE WATER OVERFLOW NIPPLE ..... REMOVED AND REPLACED RIGHT HAND LAVATORY GUSSET IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 40,624 hrs · 37,074 cycles

NDIS 660 33-50 0039670 20FEB22 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS INOP. FACT 20FEB22 09:45 SBY R&R'D LAMP. NO FIX. LIGHT LEASE COVER IS REMOVED. REPAIRED BROKEN WIRE TO SERVICE DOOR EMERGENCY LIGHT AT SERVICE DOOR HINGE ATTACH POINT WITH AN ENVIRON-MENTAL SPLICE I.A.W. S.W.P.M. 20-21-00. OPS CHECK GOOD AND REINSTALLED ORIGINAL LIGHT LENSE COVER.

Part: POTENTIOMETER — OUT OF ADJUST (NLG STEERING) · airframe 38,384 hrs · 34,569 cycles

A/C PULLS HARD LEFT WITH STEERING ON. ADJUSTED NOSE WHEEL STEERING FEEDBACK POT IAW EMB 145 AMM 32-50-00. OPS CHECK SAT. OK FOR SERVICE AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,384 hrs · 34,569 cycles

FOUND DURING RON, CEILING EXIT SIGN ASSY AT ROW 12 FACING AFT INOP. R&R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD.

Part: HANDLE — OUT OF ADJUST (MAIN CABIN DOOR) · airframe 45,400 hrs · 42,289 cycles

MAIN CABIN DOOR WOULD NOT OPEN FROM INSIDE THE CABIN. FIX ADJUSTED PAX DOOR INNER HANDLE IAW EMB 145 AMM 52-18-00 OPTS CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

RTO DUE NO T/O CONFIG BRAKE WARNING AT 60KTS. NO EMERGENCY. CREW/PAX OKAY. MESSAGE CLEARED AND A/C IS GOOD TO GO BY MAINTENANCE.

Part: UNKNOWN — MALFUNCTIONED (AIRSPEED) · airframe 37,127 hrs · 33,128 cycles

PDIS 660 31-40 2006861 07SEP19 PHL CLOSE FO'S PFD SHOWED NO AIRSPEED INDICATION DURING TAKEOFF ROLL FACT 07SEP19 23:57 PHL PERFORMED ADC OPS CHECK IAW AMM 34-15-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 36,978 hrs · 32,976 cycles

FUSELAGE SKIN CRACKED AROUND RIVET AT FRAME 77 BETWEEN STR3R-4R....FIX:ACCOMPLISHED REPAIR OF SKIN CRACK AT FR77 BETWEEN STR 3R-4R IAW SRM 53-22-01 AND E01-53-19-0323.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 36,978 hrs · 32,976 cycles

LEFT INBD AILERON PCA WING ATTACHMENT DAMAGED. BLENDED AREA OF DAMAGE IAW EO1-57-19-0296.

Part: SKIN — CRACKED (FRAME 77) · airframe 36,978 hrs · 32,976 cycles

FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R. ACCOMPLISHED REPAIR OF SKIN CRACK ON FR77 BETWEEN STR 5R AND 6R IAW SRM 53-22-01 ITEM 9. AND EO1-53-19-0323.

Part: SKIN — CRACKED (FRAME 75) · airframe 36,978 hrs · 36,976 cycles

FUSELAGE UPPER AFT SKIN CRACKED ON FRAME 75 AT FIRST FASTENER HOLE BELOW STRINGER 2R. COMPLETED REPAIR OF CRACKS AT RH FR 75 AT SYR 2 IAW SRM 53-31-01 AND EO1-53-19-0321

Part: SKIN — CRACKED (FRAME 75) · airframe 36,978 hrs · 32,976 cycles

FUSELAGE UPPER SKIN CRACKED 2 PLACES,SKIN CRACK 1:ON FRAME 75 AT PREVIOUS REPAIR ON FIRST FASTENER BELOW STR 2L. SKIN CRACK 2: ON STR 2L JUST AFT OF FRAME 75....FIX: COMPLETED REPAIRS ON CRACKS AT LH FR75 AT STR 2L IAW EMB SRM 53-31-01 AND EO1-53-19-0322. NOTE: A/C IN HVY CHECK

Part: BRACKET — CORRODED (FRAME 65) · corrosion level 2 · airframe 36,978 hrs · 32,976 cycles

CARGO DR LWR FWD CUTOUT CORRODED AT FRAME 65L PROFILE BRACKET. R&RD CARGO DR LWR FWD CUTOUT AT FRAME 65L PROFILE BRACKET IAW EMB SRM 53-31-04 AND EO1-53-19-0328

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,789 hrs · 32,775 cycles

R/H FWD EMERGENCY LIGHT WILL NOT TURN ON. REMOVED AND REPLACED LIGHT IAW AMM 33-50-10-04 AND 33-50-00-700-801-A. OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCPIT) · airframe 36,101 hrs · 31,985 cycles

RTO SERVICE DOOR WARNING IN FLIGHT. RTO AT APPROX 45 KNOTS DUE TO MASTER WARNING SERVICE DOOR OPEN AND NO T/O CONFIG WARNING. MESSAGES CLEARED BEFORE STOPPING NDIS 660 05-50 0016450 21JAN19 PHL CLOSE AIRCRAFT REQUIRED RECONFIGURATION HISTORY: FACT 21JAN19 23:37 PHL C/W RECONFIG.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,576 hrs · 31,370 cycles

PDIS 660 36-10 1722792 16OCT18 PHL CLOSE DURING INFLIGHT DEICE CHECK BLD 2 VLV FAIL AND BLD 2 VLV CLOSED EICAS MESSAGE ILLUMINATED. 28769 00 PCS HISTORY: NONE FACT 16OCT18 12:00 PHL RAN ENGINE NR 2 AND OPERATED BLEED VALVE. NO ISSUES NOTED. NO RELATED MESSAGES ON EICAS OR CMC. ALSO PERFORMED NR 2 ENGINE BLEED VLV OPS TEST IAW AMM TASK 36-11-05-700-02A. BLEED VLV OPS NORMAL. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,549 hrs · 31,335 cycles

DISCREPANCY: CEILING LINING LIGHT AT ROW 3 INOP. CORRECTIVE ACTION: R&R LIGHT BULB AT ROW 3 AND INSTALLED COVER.

Part: DUCT — NOT REPORTED (BLEED AIR SYS) · airframe 35,125 hrs · 30,873 cycles

PACK 2 NOT COOLING CABIN ADEQUATELY. R&R BLEED DUCT FOR NR 2 PACK THAT CONNECT UNDER FUSELAGE DUCTS TO INTERNAL FUSELAGE DUCTS.

Part: RELAY — ODOR · airframe 34,833 hrs · 30,553 cycles

ELECTRICAL ODOR NEAR FLIGHT DECK. WHEN APU AND PACKS WERE ON FOR APPROXIMATELY THIRTY MINUTES. FOUND THE RELAY K0095 EXCESSIVELY HOT, R & R RELAYS K0095 AND K0285 AND K1145 IAW SWPM 20-13-03, OPS CHECKED GOOD, NO FURTHER ELECTRICAL BURNING NOTED AND INSPECTED RELAY SOCKET, AND SURROUNDING AREAS NO DEFECTS NOTED, OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 34,808 hrs · 30,526 cycles

MAIN DOOR EMERGENCY LIGHT COVER BROKEN. INSTALLED A NEW COVER IAW AMM 25-23-04-000-801-A. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 34,228 hrs · 29,899 cycles

COCKPIT EMERGENCY LIGHT OVERHEAD NOT ILLUMINATING. R & R OVERHEAD COCKPIT EMERGENCY LIGHT IAW AMM 33-50-08-000-400-802-A. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (FLAPS) · airframe 33,986 hrs · 29,651 cycles

SPS ADVANCE AND FLAP LOW SPEED EICAS MESSAGES DISPLAYED WITH FLAP 1, CIRCUIT BREAKER TRIPPED. RESET FLAP 1 CB AND PERFORMED FLAP RESET. OPERATED FLAPS THROUGH ENTIRE RANGE AND THE CIRCUIT BREAKER REMAINED SET. NO RELEVANT EICAS MESSAGES ARE DISPLAYED OK FOR SERVICE

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 33,950 hrs · 29,018 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN GROUND WIRE. SPLICED THE WIRE IAW 20-21-00.

Part: ANTI-ICE SYSTEM — NO TEST (WING) · airframe 33,560 hrs · 29,225 cycles

WING ANTI-ICE TEST FAIL, CMC MESSAGE ANTI-ICE VALVE FAILED. OPEN

Part: MASTER SWITCH — DIRTY (NR 1 & 2) · airframe 32,988 hrs · 28,615 cycles

CHECK PFD 2 EICAS MESSAGE ON CLIMB OUT BEFORE 18000FEET. NR 1 CAPTAIN MFD AND NO. 2 F/O PFD WHEN BLANK, NR 2 FMS WHEN BLANK AND COMM NAV WHEN TO DASHES.WHEN PARKED AT GATE. FOUND NR 2 AVIONIC MASTER SWITCH OUT. CLEANED AND LUBED THE NR 1 AND 2 AVIONIC MASTER SWITCHES. POWERED AIRCRAFT AND AVIONIC SYSTEMS. NO DEFECTS. OK FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 32,776 hrs · 28,395 cycles

LEFT FUSELAGE SKIN GOUGED FROM CAP HOLD CABLE. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 12, AND 51-40-02.

Part: YOKE — CRACKED (RT ENGINE) · airframe 32,776 hrs · 28,395 cycles

RIGHT ENGINE FWD LOWER YOKE IS CRACKED ON FWD SIDE. REMOVED AND REPLACED THE ENGINE FWD LOWER YOKE IAW SRM 51-40-02 AND EM-54MR-386.

Part: ACM — FAILED (AC BAY) · airframe 31,450 hrs · 27,129 cycles

WHEN PACK 1 TURNED ON BURNING ODOR AND SMOKE IN COCKPIT. NO SMOKE PRESENT AT MAINTENANCE ARRIVAL. TROUBLESHOT ODOR EVENT IAW FIM 21-20-00-810-801-A, FOUND PACK 1 ACM INTERMITTENT SEIZING DEFERRED IAW MEL 21-30. REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM 21-51-03. OPC GOOD AT THIS TIME. NO LEAKS FOUND. MEL RESTORED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,354 hrs · 26,129 cycles

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

Part: PUMP — FAILED (LT ENGINE) · airframe 30,142 hrs · 25,924 cycles

E1 HYD PUMP FAIL AT 32000 FT, WENT AWAY AT 3000 FT & GEAR EXTENSION. R & R NR 1 HYD PUMP IAW MM 29-10-03. OPERATIONS CHECK LEAK, CHECKED OK.

Part: FLAP — MALFUNCTIONED (WING) · airframe 30,028 hrs · 25,797 cycles

FLAP FAIL ON EICAS & NO FLAP INDICATION SHOWS A DASH. TROUBLE SHOT FLAP DRIVE TX FAIL CMC MSG IAW FIM 27-51-00. FVS, FDMU & FPTU READINGS CHECK WITHIN LIMITS. RESET FLAP SYS. OPERATIONS TEST FLAP SYS PASSED IAW AMM 27-51-00-700-801-A.

Part: MECHANISM — DIRTY (CABIN DOOR) · airframe 29,615 hrs · 25,423 cycles

CABIN ENTRY DOOR HARD TO OPEN & WILL NOT CLOSE. CLEANED & LUBED MAIN CABIN DOOR ACTUATING & LOCKING MECHANISM IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,112 hrs · 24,950 cycles

LEFT AFT EXTERNAL EMER LIGHT FAILS TO ILLUMINATE. R & R LT AFT EXTERNAL EMER LIGHT IAW AMM 33-50-00.

Part: BRAKE ASSY — FAILED (MLG) · airframe 28,911 hrs · 24,762 cycles

BRAKE DEGRADE MASTER CAUTION UPON LOWERING GEAR. R & R RT OTBD & RT INBD BRAKES IAW AMM CARD 32-600-14. PERFORMED FUNCTION CHECK IAW WC 32-700-05. FUNCTION CHECKED GOOD, OK FOR SERVICE. LR MAIN BRAKE ASSEMBLY PN 2-1707-2 SN 1928.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,461 hrs · 24,410 cycles

FLASHLIGHT BEHIND CAPTAINS SEAT CRADLE BROKEN. R & R FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,122 hrs · 24,075 cycles

FRAME 65 CORRODED AROUND STRIKER PLATE. FABRICATED & INSTALLED INTERNAL DOUBLER FOR FRAME 65 AT STRIKER PLATE IAW SRM 53-31-04.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,122 hrs · 24,075 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK FAILED. R & R NR 2 & 3 BATTERY POWER SUPPLY, BATTERY & CHARGER, FOR EMER LIGHTS SYS IAW AMM 33-50-04. OPERATIONAL CHECKED GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,122 hrs · 24,075 cycles

RIGHT FLOORBEAM OTBD SUPPORT CRACKED. R & R SUPPORT FOR RT FLOORBEAM OTBD SIDE OVER WING BOX IAW SRM 53-23-02 & SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,122 hrs · 24,075 cycles

LEFT FLOORBEAM OTBD SUPPORT CRACKED. R & R LT OMEGA BEAM OTBD SIDE OVER WING BOX IAW SRM 53-23-02 & SRM 51-40-02. SEE WIP ENTRIES FOR DETAILS.

Part: WIRE — DAMAGED (CABIN) · airframe 28,122 hrs · 24,075 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. REPAIRED WIRE NR W716-0008-20 IN THE SERVICE DOOR WIRE HARNESS BETWEEN SPLICE SP7377 & ELEC CONNECTOR P7198 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,122 hrs · 24,075 cycles

RIGHT FLOORBEAM INBD SUPPORT CRACKED. R & R SUPPORT FOR RT FLOORBEAM INBD SIDE OVER WING BOX IAW SRM 53-23-02 & SRM 51-40-02. INSTALLED STANTION SUPPORT FOR RT OMEGA BEAM AT FRAME 50 IAW SRM 51-40-02.

Part: LIGHT — BURNED (CABIN) · airframe 28,122 hrs · 24,075 cycles

NUMBER 3 LIGHT STRIP IS BURNT & REQUIRES REPLACEMENT. R & R NR 3 EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRTC E425536 FOR OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,061 hrs · 24,020 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,688 hrs · 23,695 cycles

COCKPIT FLASHLIGHT CAPTAINS SIDE INOPERATIVE. R & R CAPTAIN`S SIDE FLASHLIGHT IAW EMB 145 AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (TE FLAP) · airframe 27,280 hrs · 23,373 cycles

FLAP FAILURE ALERTED FROM 0 TO 9. OPERATIONS CHECKED FLAPS IAW 27-53-00, OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 26,647 hrs · 22,757 cycles

BAGG SMOKE WARNING CAME ON JUST PRIOR TO LANDING, BAGG EXTINGUISHER WAS PRESSED WARNING REMAINED ON CFR CALLED. TRANSFERRED TO NRWC 660-MIA-01582. R & R BAGG COMPARTMENT HIGH RATE & METERING EXTINGUISHER BOTTLE IAW AMM 26-23-01. R & R BAGG SMOKE TEST RELAY K0629 IAW AMM 20-13-02.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,633 hrs · 22,749 cycles

FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT BRACKET IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,610 hrs · 22,725 cycles

EMERGENCY LIGHTS ON AT ARRIVAL TO ACFT. HALF THE FWD EMERGENCY FLOOR LIGHTS WERE OFF. PREVIOUS FLIGHT 1 HR PRIOR. R & R COCKPIT BULB & ENTRY DOOR BULB IAW MM 33-50-05 & 33-50-06. OPERATIONS CHECKED GOOD IAW MM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,118 hrs · 22,285 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 3165 FOUND AFT EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFT EMERGENCY LIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD. THE ACFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 25,750 hrs · 21,983 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT LAMP ON MAIN DOOR IAW EMB 145 AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 24,986 hrs · 21,361 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. SERVICED AND LUBRICATION OF MAIN CABIN DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,877 hrs · 21,271 cycles

DURING B INSPECTION, FOUND THE PASSENGER DOOR EMERGECNY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW AMM 32-50-10. OPS CHECKED GOOD IAW 33-50-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 24,594 hrs · 21,035 cycles

FLIGHT ATTENDANT REPORTED EMERGENCY LIGHT STRIP SHOULD BE SOLID GREEN WITHOUT ORANGE ARROWS AT ROWS 8 AND 9. R & R FWD EMERGENCY LIGHT STRIP AT ROW 8 & 9 IAW AMM 33-50-12. OPS CK GOOD. INSTALLED CORRECT LIGHT STRIP.

Part: BEAM — CORRODED (DOOR SILL) · corrosion level 2 · airframe 24,364 hrs · 20,848 cycles

DURING MX INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R CARGO DOOR SILL IAW SRM 51-40-02, LEVEL 2 CORROSION. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,322 hrs · 20,816 cycles

DURING B INSPECTION, FOUND THE NR 2 AND 7 EMERGENCY LIGHTS ON FLOOR FAILED OPS CHECK. ACFT REMOVED FROM SERVICE. R & R LIGHTS IAW AMM 33-50-12. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,322 hrs · 20,816 cycles

DURING MX INSPECTION FOUND THE NR 3 EMERGENCY LIGHT STRIP TO HAVE A BROKEN WIRE. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 3 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 23,747 hrs · 20,368 cycles

ON FLIGHT 3571 THE CREW REPORTED THAT DURING CRUISE THEY RECEIVED A HYD SYS 1 FAIL EICAS MESSAGE. THE CREW RAN CHECKLIST AND MONITORED THE SITUATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE DRIVEN PUMP NR 1. THE OPERATIONAL TEST CHECK WAS GOOD IAW EMB 145 AMM 29-10-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 22,495 hrs · 19,382 cycles

ON FLIGHT 2935 THE CREW REPORTED THAT AT APPROXIMATELY 16 MILES OUT FROM LANDING AT DFW THE OVERHEAD BAGGAGE SMOKE LIGHT ILLUMINATED. THE BAGGAGE EXTINGUISHER BUTTON WAS PRESSED RELEASING HALON IN THE C4 CARGO, ASSOCIATED BAGGAGE EXTBTL INOP EICAS LIGHT ILLUMINATED BAGGAGE SMOKE LIGHT EXTINGUISHED APPROX 12 MIN AFTER INVALID ILLUMINATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO HIGH RATE FIREX BOTTLE. THE OPERATIONAL CHECKS WERE GOOD IAW AMM 26-23-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,566 hrs · 18,636 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBY IAW EMB AMM 33-50-10 IAW W/C 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,441 hrs · 18,543 cycles

DURING MAINTENANCE INSPECTION, FOUND CENTER FUSELAGE SKIN HAS ONE LIGHTNING STRIKE BURN SPOT BEYOND ALLOWABLE LIMITS. REPAIRED IAW EO-EM-5300-1965 PART B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,441 hrs · 18,543 cycles

DURING MAINTENANCE INSPECTION, FOUND CENTER FUSELAGE SKIN HAS THREE LIGHTNING STRIKE BURN SPOTS ON RIVET HEADS AND FUSELAGE SKIN BEYOND ALLOWABLE LIMITS. REPAIRED IAW EO EM-5300-1965 PART C.

Part: HOLDER — BROKEN (COCKPIT) · airframe 21,165 hrs · 18,311 cycles

ON FLIGHT 3386 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER APPEARED BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPT'S FLASHLIGHT HOLDER IAW EMB STANDARD PRACTICES 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (FLASHLIGHT) · airframe 20,383 hrs · 17,741 cycles

ON FLIGHT 2751 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED LIGHT BULB IAW ERJ AMM 33-51-01. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 14,608 hrs · 13,425 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE RIGHT SIDE OF THE AIRCRAFT FORWARD EMERGENCY LIGHT WOULD NOT COME ON. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY PACK POWER SUPPLY NR 2 IN ACCORDANCE WITH EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 13,102 hrs · 11,975 cycles

ON FLIGHT 3880 CREW REPORTED AT FL360 AIRCRAFT STARTED TO DEPRESSURIZE. CABIN ALTITUDE WAS HOLDING AT 7700 FEET CABIN ALTITUDE STARTED CLIMBING AT 600 FPM CABIN ALTITUDE WARNING AT 10000 FEET. ACCOMPLISHED MEMORY ITEMS AND BEGAN EMERGENCY DESCENT. DESCENDING THROUGH FL340 CABIN LEVELED OFF AND STARTED DESCENDING. NO INDICATIONS OF DOORS OPEN FLIGHT ATTENDANT REPORTED AND NO UNUSUAL NOISES IN CABIN. CREW DECLARED A EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN PRESSURIZATION CONTROLLER IAW ERJ 145 AMM 21-32-01. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 9,039 hrs · 8,488 cycles

STRONG ELECTRICAL ODOR ON FLIGHT DECK, NO SMOKE NOTED, DISAPATED AFTER 10 MINUTES. REMOVED DEBRIS IN FOWARD AVIONIC AREA. OPERATIONAL CHECK GOOD IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 7,943 hrs · 7,482 cycles

AFTER NUMBER 2 ENGINE START RECEIVED ELECTRICAL ABNORMAL MESSAGE FOLLOWED WITH A STRONG ELECTRICAL SMELL. CLEARED APU FAULTS AND TESTED ALL AIRCRAFT ELECTRICAL SYSTEMS IAW EMB AMM 24-31-00 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND LT OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)