N651AE

Part: CONTROL PANEL — MALFUNCTIONED (ZONE 200) · airframe 53,747 hrs · 51,264 cycles

UNABLE TO SET BARO FOR ADC 1 REGARDLESS OF REVERSIONARY PANEL SETTING. FACT 30DEC25 18:49 PHL R/R PFD 100 IAW AMM 34-22-01 OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,607 hrs · 51,107 cycles

RIGHT INBD SEAT TRACK CORRODED AT BTW FR 36-47. R & R SEAT TRACK IAW AMM 53-01-06.

Part: SKIN — DENTED (ZONE 100) · airframe 53,607 hrs · 51,107 cycles

DENT ON LWR SKIN AT FR80-81 BTW STR17-19R. REPAIRED DENT IAW ETD2025-145-931822 AND EO1-53-25-0421

Part: BEAM — CRACKED (ZONE 100) · airframe 53,607 hrs · 51,107 cycles

TWO BEAMS FOR SPC SUPPORT CRACKED BTW FRAMES 7-8 NEAR STRINGERS 20L AND 20R. REPLACED THE BEAMS IAW SRM 51-40-02.

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

WINDSHIELD CTR POST CRACKED ON BOTTOM END. R & R CTR POST IAW SRM 53-12-01

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

STRINGER 6R CRACKED ABOVE FLT DECK WINDOW BETWEEN FRAMES 12-13. R & R STRINGER 6R IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR 8 BTW STRINGERS 4-9R. R & R SHEAR IAW IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR 59 BTW STRINGERS 15-16L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

53-2140 SHEAR TIE CRACKED AT FRAME 61 BTW STRINGERS 6-7L. R & R SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,507 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR 80 BTW STRINGERS 5-6R. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR 73 BTW STRINGERS 8-10L. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR CLIP CRACKED AT FRAME 61 BETWEEN STRINGERS 6 & 7R. R & R SHEAR CLIP IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

BRACKET SUPPORT CRACKED AT FRAME 68 BETWEEN STRINGERS 15-16L . R & R SUPPORT BRACKET IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

DOOR SUPPORT MECHANISM CRACKED BTW FR 61-62. R & R SUPPORT MECHANISM IAW SRM 51-40-02

Part: FRAME — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

FRAME 59 CRACKED AT BETWEEN S15 & 16L. REPAIRED IAW ETD 2025-145-931141.

Part: ANGLE — DAMAGED (ZONE 100) · airframe 53,607 hrs · 51,107 cycles

AFT CARGO ENTRY, FRAME 66 POST AND LWR ANGLE DAMAGED. R & R POST & ANGLE IAW SRM 51-40-02 AND DWG 145-25681-007-10-31-2025.

Part: BEAM — CRACKED (ZONE 100) · airframe 53,607 hrs · 51,107 cycles

CARGO ENTRY LWR BEAEM CRACKED . R & R LOWER BEAM IAW SRM 51-40-02.

Part: POST — DAMAGED (ZONE 100) · airframe 53,607 hrs · 51,107 cycles

AFT CARGO ENTRY, FR 67 POST AND LWR ANGLE DAMAGED. R & R POST AND ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR24 BTW STRINGERS 15-16R. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT SHEAR TIE CRACKED AT FR48 BTW STRINGERS 13-14L. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (WNG-BDY FAIRING) · airframe 53,607 hrs · 51,107 cycles

LEFT WING TO BODY FAIRING, FUSELAGE ATTACHMENT FOUND CRACKED AT FR48. REPAIRED IAW SRM 53-23-12

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,607 hrs · 51,107 cycles

LEFT SUPPORT CORRODED AT BTW FRAMES 19-23. R & R SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

CTR OMEGA BEAM CRACKED AT FR33. REPAIRED IAW ETD2025-145-931166

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

53-2063 LH OMEGA BEAM CRACKED AT FR36 IB SIDE. REPAIRED IAW ETD2025-145-931162

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,607 hrs · 51,107 cycles

LOWER BEAM AT SERVICE DOOR ENTRY CORRODED. R & R LOWER BEAM IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR31. REPAIRED IAW ETD2025-145-931170

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR22. REPAIRED OMEGA BEAM IAW ETD2025-145-931090

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

53-2088 SHEAR CLIP CRACKED AT FR27 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FRAME 25 BTW STRINGERS 15-16L. R & R SHEAR TIE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FRAME 24 BTW STRINGERS 16-17R. R & R THE SHEAR CLIP IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR23. REPAIRED BEAM IAW ETD2025-145-931070.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

SHEAR TIE CRACKED AT FR27 BTW STRINGERS 15-16R. R & R THE SHEAR TIE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

RIGHT SHEAR CLIP CRACKED AT FR 48 BTW S13 & 14R. R & R SHEAR CLIP IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR33. REPAIRED IAW ETD2025-145-931170. PIEDMONT EO1-53-25-0392 PERFORMED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,607 hrs · 51,107 cycles

RT SILL CORRODED BTW FRAMES 23-29. R & R SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 53,607 hrs · 51,107 cycles

FWD DIGITAL BTW FR16-18 CORRODED. REPAIRED IAW PIEDMONT ESR1-53-24-004

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR24. REPAIRED IAW ETD 2025-145-931172 AND BULLETIN 51-05.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

CTR OMEGA BEAM SUPPORT ANGLE CRACKED AT FR1-20. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LEFT OMEGA BEAM CRACKED AT FR 34. REPAIRED IAW ETD2025-145-931170

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 53,607 hrs · 51,107 cycles

LH OMEGA BEAM CRACKED AT FR21. REPAIRED IAW ETD2025-145-931090

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,607 hrs · 51,107 cycles

CORROSION ON POTABLE WATER WASTE VALVE EXTERNAL DOUBLER. R & R DOUBLER IAW SRM 51-40-02.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 536,073 hrs · 51,107 cycles

COROSSION BTW SKIN AND STR20L AT BTW FR13-14. REPAIRED IAW ETD 2025-145-931807

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 100)

ON TAXI OUT, BAG BAY SMOKE INDICATION. FOLLOWED QRC/QRH AND BLEW BAG BAY FIRE BOTTLES AND RTG. R & R CARGO SMOKE DETECTOR #100 + #200 IAW AMM 26-15-01, OPS CHECK GOOD.. R & R CARGO FIRE EXT BOTTLES HIGH RATE AND METERING IRT AMM 26-23-01 OPS CHECK GOOD AT THIS TIME

Part: WINDOW — UNDERTORQUED (ZONE 200) · airframe 53,263 hrs · 50,713 cycles

LOUD SQUEAL NOTED FROM AROUND F/OS WINDSHIELD MEL 10AUG25 PRESS CONTROL AUTO AND MANUAL RETORQUED FO AND CAPTAIN WINDSHIELDS IRT AMM 56-10-01-700-802-A. OPS CHECK GOOD IRT AMM 21-31-00-860-801-A. LEAK CHECK GOOD. NO FURTHER DISCREPENCIES NOTED AT THIS TIME. OK FOR SERVICE.

Part: SEAL — LEAKING (ZONE 800) · airframe 53,149 hrs · 50,573 cycles

ON CLIMBING THROUGH FL 280 HIGH PITCH SQUEAL STARTED ON FLT DECK DIVERTED TO PHL AND SQUEAL PERSISTED UNTIL BELOW FL 180 FACT 18JUL25 19:37 PHL PRESSURIZED AC IAW AMM 21-31-00 FOUND MAIN PAX DOOR TO BE LEAKING. CLEANED AND LUBED DOOR SEALS. OPS CHECK GOOD AC OK FOR SERVICE

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 51,578 hrs · 48,803 cycles

LH AFT EXTERNAL EMEGENCY LIGHT INOP. RAR LAMP ASSY IAW AMM 33-50-10

Part: VALVE — FAULTED (HIGH STAGE) · airframe 51,238 hrs · 48,421 cycles

ON T/O AFTER THRUST LEVERS ADVANCED, BLD 2 VLV FAIL MSG APPEARED. REJECTED T/O. MSG DISAPPEARED WHEN THRUST LEVERS RETARDED. R & R HIGH STAGE VALVE PRESS SWITCH IAW AMM 36-11-07. OPS CHECKS GOOD.

Part: VALVE — FAULTED (HIGH STAGE) · airframe 51,238 hrs · 48,421 cycles

ON T/O AFTER THRUST LEVERS ADVANCED, BLD 2 VLV FAI MSG APPEARED. REJECTED T/O. MSG DISAPPEARED WHEN THRUST LEVERS RETARTED. R & R HIGH STAGE VALVE PRESS SWITCH IAW AMM 36-11-07. OPS CHECKS GOOD.

Part: CONNECTOR — FAULTED (ANTI-ICE VALVE) · airframe 51,106 hrs · 48,267 cycles

ENG 2 ANTI ICE VALVE FAILED. R&R PLUG P0973 ON E2 ANTI-ICE VALVE IRT SWPM 20-50-00, ALSO R&R RELAY KO536 IRT AMM 20-13-02. OPS TEST GOOD AT THIS TIME

Part: TRANSDUCER — FAULTED (NR 2 ENG A/I) · airframe 51,093 hrs · 48,257 cycles

E2 ANTI ICE FAIL CAUTION LIGHT DISPLAYED. T/S IAW FIM 30-21-00-810-806-A FROM BLOCK 1 TO 5. R & R RT PRESSURE TRANSDUCER IAW AMM 30-21-06. OPS CHECKED GOOD IAW AMM 30-21-00.

Part: WARNING MESSAGE — ILLUMINATED (A/C PACK OVRHEAT) · airframe 50,646 hrs · 47,756 cycles

PACK 1 O/H ON T/O ROLL. RESET PACK NO FURTHER ISSUES. NO 30 DAY HISTORY. FACT 06APR24 06:38 SCE IRREGULARITY CLEARED USEING NORMAL CREW PROCEDURES

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,634 hrs · 46,620 cycles

RH OVERWING EMERGENCY LIGHT INOP. R&R'D OVERWING EMERGENCY LIGHT ASSY IAW AMM33-50-10

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E980072 RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE HAS RELEVANT INDICATION DURING HFEC ROTOSCOPE INSPECTION. PERFORMED BUSHING REPAIR TO RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0160.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E980072 RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE HAS RELEVANT INDICATION DURING HFEC ROTOSCOPE INSPECTION. PERFORMED BUSHING REPAIR TO RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0160.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E980070 LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE ELONGATED. PERFORMED BUSHING REPAIR TO LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0159.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E980070 LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE ELONGATED. PERFORMED BUSHING REPAIR TO LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0159.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979232 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 32-33 STRINGERS 5L-7L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 32-33 STRINGERS 5L-7L IAW ETD2023-145-014613 AND EO1-53-23-0158..

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979234 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 35-36 STRINGERS 4L-6L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 35-36 STRINGERS 4L-6L IAW ETD2023-145-014595 AND EO1-53-23-0157.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979232 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 32-33 STRINGERS 5L-7L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 32-33 STRINGERS 5L-7L IAW ETD2023-145-014613 AND EO1-53-23-0158.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979234 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 35-36 STRINGERS 4L-6L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 35-36 STRINGERS 4L-6L IAW ETD2023-145-014595 AND EO1-53-23-0157.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979228 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 31-32 STRINGERS 5L-7L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 31-32 STRINGERS 5L-7L IAW ETD2023-145-014575 AND EO1-53-23-0156.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,237 hrs · 46,166 cycles

E979228 NO REPAIR INFO FOUND ON EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 31-32 STRINGERS 5L-7L. RE-ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BETWEEN FRAMES 31-32 STRINGERS 5L-7L IAW ETD2023-145-014575 AND EO1-53-23-0156.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,237 hrs · 46,166 cycles

E978540 GALLEY FWD DIAMOND GUSSET HAS CORROSION INSIDE SERVICE DOOR. RAR GALLEY FWD DIAMOND GUSSET (INSIDE SERVICE DOOR) IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,237 hrs · 46,166 cycles

E978317 R/H #2 FLOORBOARD SUPPORT HAS CORROSION. RAR CABIN RH #2 OUTBD FLOOR SUPPORT IAW SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,237 hrs · 46,166 cycles

E978318 R/H #3 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICABLE R/H #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,237 hrs · 46,166 cycles

E978319 L/H #3 FLOORBOARD SUPPORT HAS CORROSION : REMOVED AND REPLACED LH #3 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,237 hrs · 46,166 cycles

E978210 SSI 53-30-28 LAV CENTER FLOOR BEAM GUSSET HAS CORROSION AT FWD AND AFT ENDS. REMOVED AND REPLACED WITH NEW SERVICEABLE LAV CENTER FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,151 hrs · 46,071 cycles

INTERPHONE CALL CHIME SOUNDS CONSTANTLY. CHIME SILENTS ON BACKUP INTERPHONE. FACT 04MAY23 09:56 PHL R/R'D PA AMP IAW AMM 23-31-01. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: PIPE — LEAKING (BLEED SYSTEM) · airframe 47,411 hrs · 44,052 cycles

BLEED ENGINE LEAK 2 IN CLIMBING THROUGH 10000 FT RAN QRH AND EXTINGUISHED. FOUND BLEED PIPE FWD OF #2 ENGINE PRSOV DAMAGED/LEAKING. R+R BLEED PIPE REF 36-11-09. OK FOR SERVICE LEAK CHECK GOOD

Part: NONE — NONE · airframe 46,687 hrs · 43,244 cycles

PDIS 651 30-21 2575711 28DEC21 PHL ASSGN E2 A/ICE FAIL EICAS ON CLIMB IN ICING CONDITIONS C/W QRH. DEACTIVATED PER AMM 30-21-01-040-801-A CURRENTLY ON THE MEL MEL 28DEC21 11:49 PHL C36208 30-8-1 ENGINE ANTI-ICING VALVES

Part: NONE — NONE · airframe 46,637 hrs · 43,187 cycles

PDIS 651 56-10 2575592 18DEC21 CLT CLOSE SUSPECTED CRACK IN CAPTAINS WINDSHIELD 32539 00 SMS FACT 18DEC21 14:56 CLT INSPECTED IAW PPG CMM 56-10-01 FOUND TO BE SCRATCH WITHIN LIMITS NO ACTION REQUIRED. OK FOR SERVICE

Part: NONE — NONE

PDIS 651 27-62 2489442 22OCT21 ALB CLOSE SPOILER FAIL EICAS MESSAGE DURING DESCENT WITH ROLL MOVEMENT TOWARD THE LEFT. C/W QRH, LANDED NORMALLY 29929 00 EK FACT 22OCT21 12:52 ALB TOUBLESHOOTED SPOILER FAIL IRW EMB 145 FIM 27-63-00-810-807-A. COMPLETED FIM FROM BLOCK 1 TO BLOCK 21. NO DEFECTS NOTED. DURING OPERATION OF SPOILERS FOUND LH SPEED BRAKE TO BE RETRACTING SLOWLY. R&R'D LH SPEED BRAKE ACTUATOR IRW EMB 145 AMM 27-62-02. OPS CHECK GOOD P/N 360540-1011 S/N ON 0353 S/N OFF 0394

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 45,941 hrs · 42,404 cycles

EMERGENCY LIGHT BULBS AT MAIN DOOR WILL NOT ILLUMINATE. WHILE REMOVING PANEL 811XW NOTICED WIRE BROKEN ON EMERGENCY LIGHT ASSY AT MAIN DOOR. CRIMPED NEW CONTACT AND CONNECTED AT SP7425 REF SWPM 20-50-01. REINSTALLED PANEL 811XW AS REQ. OPS CHECK ON MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-00-700-801-A/500 OP CHECK GOOD. NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 45,829 hrs · 42,296 cycles

BLEED 1 OVER-TEMP IN ICING CONDITIONS DURING CLIMB. R&R FAN AIR VALVE IAW AMM 36-11-03 PERFORMED OPS CHECK IAW AMM 36-11-11-700-801-A/500 ALSO AMM 36-00-00-700-806-A/500 OPS CHECK GOOD PERFORMED R&R AS PRECAUTIONARY MAINTENANCE. OK FOR SERVICE.

Part: AOA — MALFUNCTIONED (NR 1) · airframe 45,188 hrs · 41,608 cycles

SPS1 INOP AND SPS ADVANCE EICAS MSG ON TAKE OFF ROLL. MAINTENANCE: FOLLOWED FIM TASK 27-36-00-810-807-A - NO DEFECTS. NOTED REINSTALLED CTOR,SPC,AND RACK./// TRANSCRIBED TO HA300 SEQ #4 ON WORK PACKAGE DATED 02/04/21. AIRCRAFT IS STILL IN WORK R/R #1 AOA VANE. OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (SPS) · airframe 45,050 hrs · 41,451 cycles

ON TAKE OFF ROLL GOT SPS INOPERABLE FOLLOWED SPS ADVANCE. SUSPECTED ONE OF THE 2 AOA VANES TO HAVE STUCK DURING TAKEOFF DUE TO ICE VERIFIED BOTH AOA VANES FREEDOM TO MOVE AND PEFORMED STALL PROTECTION SYSTEM OPERATIONAL TEST, IAW EMB 145 AMM 27-36-00-700-801-A. OPERATIONAL CHECK NORMAL, NO FUTHER DEFECTS NOTED AT THIS TIME.

Part: SKIN — CRACKED (FRAME 79) · airframe 44,893 hrs · 41,265 cycles

FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AT 1 RIVET ON FR 79 BETWEEN STR 8L/9L. EVALUATION COMPLETE: FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AT 1 RIVET ON FR 79 BETWEEN STR 8L/9L. FABRICATED AND INSTALLED BUSHING ON FUSELAGE EXTERNAL SKIN AT FRAME 79 BETWEEN STRINGERS 8L-9L, IAW EMB SRM 53-32-01 AND PIEDMONT EO1-53-20-0384.

Part: STRINGER — CHAFED (FRAMES 52-53) · airframe 44,893 hrs · 41,265 cycles

RIGHT STRINGER 19 CHAFED BETWEEN FR 52 AND FR 53. FABRICATED AND INSTALLED SERVICEABLE REPAIR DOUBLER ON STRG 19R AT FR 52 AND FR 53, IAW EMB 145 SRM 53-24-02 AND EO1-53-20--0382. SEE TRUNOVER FOR DETAILS.

Part: FITTING — CRACKED (RT ENG YOKE) · airframe 44,893 hrs · 41,265 cycles

RIGHT ENGINE FORWARD LOWER PYLON YOKE FORWARD FITTING IS CRACKED. R & R RT ENGINE FWD LOWER PYLON YOKE FWD FITTING, IAW PIEDMONT AIRLINES ETD2020-145--028742 AND EO1-54-20-0369. SEE TURNOVER FOR DETAILS.

Part: SPRING — CRACKED (NLG BRAKE) · airframe 44,893 hrs · 41,265 cycles

RT NLG WHEEL BRAKE SPRING HAS CRACK AT MOUNTING HARDWARE. INSTALLED FABRICATED DOUBLER AND FILLER FOR REPAIR OF THE RT NLG WHEEL BRAKE SPRING, IAW EMB 145 SRM 53-11-10 AND EO1-53-20-0385. SEE TURNOVER FOR DETAILS.

Part: STRINGER — CHAFED (FRAMES 52-53) · airframe 44,893 hrs · 41,265 cycles

LEFT STRINGER 19 CHAFED BETWEEN FR 52 AND FR 53. FABRICATED AND INSTALLED SERVICEABLE REPAIR DOUBLER ON STRG 19L AT FR 52 AND FR 53, IAW EMB 145 SRM 53-24-02 AND EO1-53-20--0383 SEE TURNOVER FOR DETAILS.

Part: TRUNNION — DAMAGED (RT WING) · airframe 44,893 hrs · 41,265 cycles

RT MLG AFT UPPER TRUNNION CRACKED OUTBD OF BEARING ABOVE 1ST FASTENER TO TRUNNION EDGE. EASI 6581 USED. 100-500KHZ PROBE, FREQ=400KHZ,V-GAIN=78.0, H-GAIN=65.0, LPF =100. REPAIR IS REMOVED AND INSTALLED SERVICEABLE RT MLG AFT TRUNNION, IAW TI TI-145-- 14-018 RH REV. G, ETD2020-145-029103 AND EO1-57-20-0379.

Part: SPRING — CRACKED (NLG BRAKE) · airframe 44,893 hrs · 41,265 cycles

LT NLG WHEEL BRAKE SPRING HAS CRACK AT MOUNTING HARDWARE. INSTALLED FABRICATED DOUBLER AND FILLER FOR REPAIR OF THE RT NLG WHEEL BRAKE SPRING, IAW EMB 145 SRM 53-11-10 AND EO1-53-20-0385. SEE TURNOVER FOR DETAILS.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 44,893 hrs · 41,265 cycles

FR 72 BETWEEN 16L-17L IS CRACKED. REMOVED SHEAR CLIP AT FR 72 AND STR 16L-17L, CUT AND REMOVED DAMAGED SECTION OF FR 72. FABRICATED REPAIR SECTION OF FRAME AND L-DOUBLERS AND U-SHAPE DOUBLER. INSTALLED ALL REPAIR ITEMS, IAW EMB 145 SRM'S 51-40-02, SRM 53-00-04 ITEM 3, SRM 53-00-04 ITEM 2, ETD2020-145-029908 REV A AND PIEDMONT EO1-53-20-0389.

Part: SKIN — CHAFED (FRAMES 42-43) · airframe 44,893 hrs · 41,265 cycles

SMALL CHAFE BEHIND LT UPPER OVERWING FAIRING SUPPORT BETWEEN FR 42-43 AND STR 13L-14L. SMALL CHAFE BEHIND LT UPPER OVERWING FAIRING SUPPORT BETWEEN FR 42-43 AND STR 13L-14L, DRILLED OUT SMALL CHAFE AND INSTALLED SOLID RIVET AND WASHER AT LT UPPER OVERWING FAIRING SUPPORT BETWEEN FR 42--43 STR 13L-14LM. RESTORED TO ORIGINAL FINISH, IAW EMB 145 SRM 53-23-01, ITEM 4, CPM 51-21-06, PIEDMONT BULLETIN 51-02 AND PIEDMONT EO1-05-20-0386.

Part: TRUNNION — CRACKED (LT MLG) · airframe 44,893 hrs · 41,265 cycles

LT MLG AFT UPPER TRUNNION CRACKED OUTBD OF BEARING ABOVE 1ST FASTENER TO TRUNNION EDGE. EASI 6581 USED. 100-500KHZ PROBE, FREQ=400KHZ, -V-GAIN=78.0, H-GAIN=65.0, LPF =100. REMOVED AND INSTALLED SERVICEABLE LT MLG AFT TRUNNION, IAW AERNNOVA TI TI-145--14-018 LH REV. F, ETD2020-145-029122 REV A AND EO1-57-20-0378. SEE TURNOVER FOR DETAILS.

Part: YOKE — CRACKED (LT ENGINE) · airframe 44,893 hrs · 41,265 cycles

LEFT ENGINE FORWARD LOWER PYLON YOKE FORWARD FITTING IS CRACKED. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE LT ENGINE FWD LOWER PYLON YOKE FWD FITTING, IAW PIEDMONT AIRLINES ETD2020-145-028740 AND EO1-54-20-0368. SEE TURNOVERS FOR DETAILS.

Part: SKIN — DENTED (FRAME 3) · airframe 44,893 hrs · 41,265 cycles

DENT FOUND ON SKIN, AT FRAME 3, BELOW THE LT LONGITUDINAL SKIN SPLICE. COMPLETE: CUT OUT ON BLEND NR 2, FABRICATED FILLER AND DOUBLER FOR DENT. INSTALALED REPAIR OVER DENT FWD OF FRAME 3 BELOW THE LT LONGITUNINAL SKIN, IAW ETD-2020-145-028955 AND EO1-53-20-0367.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 44,893 hrs · 41,265 cycles

SERVICE DOOR CENTER SILL IS CORRODED. FABRICATED AND INSTALLED DOUBLER FOR REPAIR OF SERVICE DOOR LOWER CENTER SILL CENTER NUTPLATE HOLE, IAW EMB-145 SRM 53-21-02 RE ITEM 2 AND EO1-53-20-0381. SEE TURNOVER FOR DETAILS.

Part: DOOR FRAME — CHAFED (CARGO DOOR) · airframe 44,893 hrs · 41,265 cycles

CARGO DOOR INTERIOR WEB FRAME HAS 8 CHAFES. BLENDED 8 EACH CHAFES ON INTERIOR WEB, IAW EMB 145 SRM 51-10--03. THE BLEND 12" FROM FWD EDGE AND 14"- FROM BOTTOM FOUND TO BE BEYOND LIMITS. PERFORMED CUTOUT OF DAMAGED AREA, FABRICATED DOUBLER. INSTALLED DOUBLER FOR REPAIR, IAW EMB 145 SRM 52-30-01RE AND PIEDMONT EO1-52-20-0371.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,851 hrs · 41,219 cycles

FOUND DURING GOOD NIGHT CHECK LT EMERGENCY DOOR UPPER EMERGENCY LIGHT INOPERATIVE. R & R THE INVERTER IAW AMM 33-50-11-000/400-801-A. OPS TESTED GOOD.

Part: VALVE — BROKEN (AC SYSTEM) · airframe 44,765 hrs · 41,120 cycles

A/C DID NOT PRESSURIZE IN FLT RAN QRH AT 5000 MSL CABIN DIFF PRESSURE WOULD NOT EXCEED 0.3PSI. FOUND GROUND CONNECTION VALVE MISSING. PERFORMED BOROSCOPE AND FOUND THE BROKEN VALVE. R&R'D THE GROUND CONNECTION VALVE IAW AMM 21-22-04-400-801-A. PERFORMED PRESSURIZATION TEST GOOD IAW AMM 21-31-00-700-801-A. OK FOR SERVICE AT THIS TIME.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 44,729 hrs · 41,077 cycles

PDIS 651 49-10 2447541 05APR20 PHL CLOSE APU FAILED TO START CMC MSG AUP EXTERNAL SHORT FADEC BITE DISPLAY WFSERVO SC FACT 14APR20 03:59 RIC PERFORMED REPAIR TO FRAME 80 IN AREA WHERE APU SHUNT MOUNTS IAW EO1-53-20-0170. OPS CHECK OF APU GOOD. R EF HA300 SEQ #5 DATED 4/5/20 FOR T/S AND COMPLETE RE PAIR. OK FOR SERVICE. CLEAR MEL.

Part: GASKET — BROKEN (VALVE DOOR) · airframe 44,420 hrs · 40,705 cycles

GASKET ON GROUND CONNECTION VALVE DOOR IS BROKEN. REMOVED AND REPLACED GROUND CONNECTION DOOR RUBBER SEAL RING IN REFERENCE TO AMM 21-22-04-000/400-802A (P/N ON SEAL 120-15661-001 P/N OFF SEAL 120-15661-001)

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 44,420 hrs · 40,705 cycles

CABIN DEPRESSURIZED DURING DECENT AT FL 230 CABIN ALTITUDE REACH 12,100. UNCOMMANDED. PRESS CONTROL AUTO MANUAL. FOUND LOWER DOOR SEAL OF BAG BAY DOOR MISSING. INSTALLED BAG BAY DOOR SEAL IN REF TO AMM 52-30-02-400-801-A. OPS AND LEAK CHECK GOOD. CLEAR MEL. CHANGE OUTFLOW VALVE FILTER DUE TO PRESSURIZATION HISTORY. REMOVED AND REPLACED AIR FILTER ELEMENT IN REFERENCE TO AMM 21-31-08-960-801-A. OK FOR SERVICE.

Part: FAN — INOPERATIVE (GASPER) · airframe 44,420 hrs · 40,705 cycles

GASPER FAN INOP (CREW PULLED AND COLLARED CB F25) GASPER FAN. RESET GASPER FAN C/B F25 AND OPERATED GASPER FAN FOR AN EXTENDED PERIOD OF TIME OVER NIGHT. NO DEFECTS NOTED AT THIS TIME. OPS CHECK GOOD. OK FOR SERVICE. CLEAR MEL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 44,348 hrs · 40,624 cycles

SMOKE IN CABIN DURING CRUISE WITH PACKS RUNNING WITH HEAT ON.SMELL STARTED TO DISSIPATE....FIX: OPERATED #1 AND #2 ENG AND APU WITH BOTH PACKS ON,PRESSURIZED AND CONTROLLED CABIN TEMP AT 27 DEG C. OPS CHECK GOOD. NO SMOKE OR FUMES DETECTED, OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 44,348 hrs · 40,624 cycles

SMOKE SMELL IN CRUISE WITH BOTH PACKS RUNNING. WITH HEAT ON AND SMELL STARTED TO DISSIPATE WHEN TEMP WAS SET TO COOL. OPERATED #1 AND #2 ENGINE + APU WITH BOTH PACKS ON, PRESSURIZED AND CONTROLLED CABIN TEMP AT 270°C OPS CHECK GOOD NO SMOKE OR FUMES DETECTED OKAY FOR SERVICE AT THIS TIME.

Part: SEAL — PEELING (WINDSHIELD) · airframe 44,148 hrs · 40,390 cycles

WATER COMING FROM BEHIND MAG COMPASS. MAINTENANCE PERFORMED VISUAL INSPECTION OF PILOT AND CO-PILOT WINDSHIELD. ON PILOT WINDSHIELD FOUND HUMP SEAL PEELING ALONG TOP RIGHT CORNER. APPLIED SPEED TAPE OVER AREA IAW AMM 56-10-01-08. INSPECTED FLIGHT DECK NO DAMAGE NOTED. FOLLOW UP NO MOISTURE FOUND AT THIS TIME. CLOSED AND RESECURED ALL PANELS OPENED FOR ACCESS AS REQUIRED. OK FOR SERVICE.

Part: LAMP — NOT SEATED (EMERGENCY LIGHT) · airframe 43,840 hrs · 40,066 cycles

SERVICE DOOR EMERGENCY LIGHT INOP....FIX: RESEATED SERVICE DOOR EMERGENCY LIGHT LAMP INTO SOCKET IAW AMM 33-50-10-000/400-801-A. OK FOR SERVICE

Part: FRAME — DAMAGED (FUSELAGE) · airframe 43,257 hrs · 39,381 cycles

NDIS 651 53-20 0010740 05JUL19 SBY CLOSE WHILE TROUBLESHOOTING APU BATT 1 OFF BUS MESSAGE. TRANSCRIBED FROM LP 189608 FOUND DAMAGE ON STRUCTURE BEHIND UP SHORT LOCATED AT THE LOWER HALF OF FRAME 80. DAMAGE THAT WAS FOUND WAS ARCING. FACT 05JUL19 11:41 SBY REPAIRED DAMAGED AREA IAW EO1-53-19-0259. SEE LOG BOOK PAGE 189611 SEQ 1 FOR APU CORRECTIVE ACTION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 43,222 hrs · 28,805 cycles

LEFT EXTERIOR OVERWING EMERGENCY LIGHT WONT ILLUMINATE. R & R LIGHT LAMP IAW 33-50-10-000/400-801-A.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,169 hrs · 39,276 cycles

EMERGENCY EXIT LIGHTED SIGN ABOVE SERVICE DOOR THRESHOLD IS INOP...FIX: CLEANED AND RESEATED WIRE CONNECTIONS,OPS CHECK GOOD, CLOSED ACCESS PANEL AT SAID LOCATION

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,135 hrs · 39,230 cycles

LH EMERGENCY EXIT LIGHT ON THE OVERWING LATERAL PANEL IS INOP. R & R THE LT OVERWING EMERGENCY EXIT BULB IAW AMM 30-50-10-02-004A, AND AMM 30-50-10-402-004A.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,488 hrs · 38,492 cycles

NDIS 651 33-51 0007180 19JAN19 SBY CLOSE EMERGENCY LIGHT ON L/H WING TO FUSELAGE LATERAL PANEL IS INOP. FACT 19JAN19 12:51 SBY R&R LIGHT BULB AT SAID LOCATION AND RESECURED THE COVER USING RETAINED HARDWARE. P/N ON: 1317 P/N OFF:1317

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 42,178 hrs · 38,137 cycles

PDIS 651 30-14 1742942 24NOV18 PHL CLOSE DURING TAKEOFF ROLL AROUND 30 KNOTS EICAS ADVISORY I CE COND MSG PRESENT FOLLOWED BY ICE COND A/I INOP WA RNING MESSAGE. FACT 24NOV18 22:49 PHL GROUND RAN E1 AND E2 PERFORMED ANTI ICE SYSTEM OPS T EST IN REFERENCE TO AMM 30-00-00 OPS CHECK GOOD NO R ELATED CMC MESSAGES FOUND OK FOR SERVICE.

Part: ANGLE — CRACKED (FRAME 67) · airframe 40,964 hrs · 36,714 cycles

AFT ANGLE THAT ATTACHES TO AFT FLOOR SUPPORT UNDER FLOORBOARD 271FF WAS FOUND CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 40,964 hrs · 36,714 cycles

CARGO DOOR FRAME FORWARD L SHAPE HAS CORROSION ON THE BOTTOM EDGE. REPAIRED THE DOOR FRAME FWD L SHAPE IAW SRM 53-31-04.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 40,964 hrs · 36,714 cycles

CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (LT OVERWING PANE) · airframe 40,964 hrs · 36,714 cycles

LEFT OVERWING PANEL NR 2 LOWER ATTACH BRACKET IS CRACKED APPROX. 1/4 INCH. REMOVED AND REPLACED THE OVERWING PANEL LOWER ATTACH BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO DOOR) · airframe 40,964 hrs · 36,714 cycles

AFT CARGO DOOR HORIZONTAL SUPPORT BRACKET FOR LIFTING AND LOWERING MECHANISM IS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKETIAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FRAME 48) · airframe 40,964 hrs · 36,714 cycles

RIGHT OUTBOARD OMEGA BEAM SUPPORT BRACKET CRACKED APPROXIMATELY 3/4 INCH AT FRAME 48. REMOVED AND REPLACED THE RT OTBD OMEGA BEAM SUPPORT ANGLE IAW SRM 51-40-02.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 40,964 hrs · 36,714 cycles

CARGO DOOR HOLD OPEN HANDLE BRACKET IS CRACKED. INSTALLED A NEW CARGO DOOR HOLD OPEN HANDLE BRACKET IAW SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (FRAME 48) · airframe 40,964 hrs · 36,714 cycles

LEFT OVERWING PANEL UPPER ATTACH BRACKET AT FRAME 48 IS CRACKED APPROXIMATELY ONE INCH. REPAIRED IAW SRM 53-23-12.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 40,964 hrs · 36,714 cycles

PAX DOOR INNER HANDLE SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED PRE-EXISTING REPAIR DOUBLER ON PAX DOOR INNER HANDLE TORQUE BOX REFERENCING EO-EM-52MR-250 FOR MATERIAL AND FASTENER INSTALLATION SPECS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,964 hrs · 36,714 cycles

UPPER FRAME 10R IS CRACKED JUST BELOW RIGHT DV WINDOW SILL. REMOVED AND REPLACED FR 10R BELOW DV WINDOW IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 40,964 hrs · 36,714 cycles

AFT CARGO DOOR VERTICAL SUPPORT BRACKET FOR LIFTING AND LOWERING MECHANISM IS CRACKED. REPAIRED CARGO DOOR VERTICAL SUPPORT BRACKET FOR LIFTING AND LOWERING MECHANISM IAW ERS EM-5300-3198 AND SRM 51-40-02

Part: HINGE FITTING — DAMAGED (RT AILERON) · airframe 40,964 hrs · 36,714 cycles

RIGHT AILERON NR 2 HINGE FITTING, OTBD LOBE HAS ONE MISSING HAT BUSHING, AND ONE CORRODED. REMOVED AND REPLACED THE RT AILERON NR 2 HINGE FITTING IAW EO EM-27MR-112.

Part: FITTING — DAMAGED (RT AILERON) · airframe 40,964 hrs · 36,714 cycles

AILERON DAMPER FITTING ON THE RT AILERON HAS DAMAGE ON INNER SURFACE OF OTBD LOBE AND OTBD BUSHING BORE. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112.

Part: BUSHING — CORRODED (RT AILERON) · airframe 40,964 hrs · 36,714 cycles

RIGHT AILERON PCA FITTING HAT BUSHINGS ARE WORN AND CORRODED. REMOVED AND REPLACED THE PCA FITTING IAW EO EM-27MR-112.

Part: DOOR FRAME — CORRODED (FRM 22) · airframe 40,964 hrs · 36,714 cycles

AFT SERVICE DOOR FRAME HAS CORROSION AROUND LOWER NUT PLATE HOLE. REPAIRED THE DOOR FRAME IAW ERS-EM-53MR-3191.

Part: ATTACH BRACKET — CRACKED (FRAME 50) · airframe 40,964 hrs · 36,714 cycles

LEFT OVERWING PANEL UPPER ATTACH BRACKET AT FRAME 50 IS CRACKED APPROX. 6 INCHES. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (FRAME 49) · airframe 40,964 hrs · 36,714 cycles

LEFT OVERWING PANEL, UPPER ATTACH BRACKET AT FRAME 49 IS CRACKED, 2.5 INCHES. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,794 hrs · 36,560 cycles

LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD IAW AMM 33-50-10.

Part: CHARGER — FAILED (CABIN) · airframe 40,688 hrs · 36,457 cycles

FIND BOTH OVER WING EMERGENCY LIGHT INOP DOING PS-1 INSP. R&R EPSU NR 4 IAW AMM TASK 33-50-04 OPS CHECK NO GOOD REMOVED AND REPLACED BOTH BULB IAW AMM TASK 33-50-10 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 68503.

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 38,660 hrs · 34,606 cycles

AT GEAR DN SELECTION EICAS ANNUNCIATED CAUTION MESSAGE LG AIR GND FAIL. PERFORMED ABNORMAL CHECKLIST. ALL ASSOCIATED SYSTEMS OPS NORMAL AT LANDING. REMOVED AND REPLACED THE NLG LT DOOR ACTUATOR IAW AMM TASK 32-33-03. OPS & LEAK CHECKED GOOD.

Part: CONTROL UNIT — FAILED (MLG) · airframe 38,537 hrs · 34,489 cycles

LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE WITH A LANDING GEAR AIR - GROUND FAIL MESSAGE ON EICAS. REMOVED AND REPLACED THE LGEU IAW AMM 32-32-01. OPS CHECKED GOOD, NO MESSAGES NOTED.

Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 38,416 hrs · 34,380 cycles

LG AIR/GND FAIL EICAS MESSAGE AFTER LOWING LANDING GEAR. INSPECTED AND CLEANED LANDING GEAR PROX SENSORS. RESET LGEU ALL MESSAGES CLEARED REF AMM 32-32-01

Part: FLASHLIGHT ASSY — BROKEN (AFT CABIN) · airframe 38,330 hrs · 34,291 cycles

AFT EMERGENCY FLASHLIGHT CRADLE AND GRIP BROKEN. R & R THE AFT EMERGENCY FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,045 hrs · 33,986 cycles

MAIN PAX DOOR EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED THE LAMP. OPS CHECKED GOOD IAW AMM 33-50-10.

Part: SWITCH — FAULTY (SERVICE DOOR) · airframe 37,387 hrs · 33,362 cycles

SERVICE DOOR OPEN INDICATION DURING FLIGHT. PRESSURIZATION NORMAL. FLIGHT CREW PLACARDED SERVICE DOOR WARNING, MEL 52-04, AUTH 070330-B, MOC 607040. TROUBLESHOT AND R & R THE NR 2 MICROSWITCH ON THE SERVICE DOOR IAW AMM 52-74-01. OPS CHECK GOOD, MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,918 hrs · 32,910 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,601 hrs · 32,615 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75, BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-1978.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,601 hrs · 32,615 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 2R & 3R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1979.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,577 hrs · 32,597 cycles

CORROSION ON FWD LOWER BAGGAGE DOOR CUT OUT. INSTALLED NEW CARGO DOOR CUT OUT SILL IAW SRM 51-40-02.

Part: LIGHT — BROKEN (CABIN) · airframe 36,577 hrs · 32,597 cycles

EMERGENCY FLOOR STRIP NR 1 ASSEMBLY IS BROKEN. R & R EMER FLOOR STRIP NR 1 ASSEMBLY IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FAILED (COCKPIT) · airframe 36,250 hrs · 32,336 cycles

ON TAKEOFF ROLL, WE RECEIVED A TAKEOFF CONFIG MASTER WARNING ON THE PARKING BRAKE. WE WERE AT 100 KTS & PARKING BRAKE WAS RELEASED & ABORTED TAKEOFF. REPEAT WRITE UP ON 12 25. R & R AURAL WARNING UNIT IAW AMM 31-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,657 hrs · 31,751 cycles

CEILING EMER LIGHT AT EXIT ROW INOPERATIVE. R & R CEILING AISLE EMER LIGHT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: DOOR — OPEN (FUEL SYSTEM) · airframe 34,987 hrs · 31,150 cycles

FUEL DOOR REFUELING PANEL OPENED INFLIGHT, RETURNED TO FIELD. PERFORMED GVI OF REFUELING DOOR IAW SMP, NO DAMAGE NOTED.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 34,742 hrs · 30,906 cycles

CAPTAINS FLASHLIGHT CHARGER WILL NOT HOLD FLASHLIGHT. R & R CAPTAINS FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 34,545 hrs · 30,715 cycles

FLIGHT ATTENDANTS FLASHLIGHT HAS CRACKED OUTER RING & CHARGER LIGHT MISSING. R & R IAW AMM 33-50-16.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,181 hrs · 30,422 cycles

LEFT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 & OVERWING EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 12853.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,104 hrs · 30,352 cycles

FLIGHT ATTENDANT`S FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT`S FWD FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 34,043 hrs · 30,305 cycles

LEFT OVERWING EMER LIGHT UPSIDE DOWN. REPOSITIONED LT WING EMER LT TO CORRECT ORIENTATION. OPERATIONS CHECKED OK IAW AMM 33 50 10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,988 hrs · 30,256 cycles

OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER ASSEMBLY IAW 33-50-04.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 33,807 hrs · 30,061 cycles

OVERWING RT & LT EMER LIGHTS INOPERATIVE. R & R EMER POWER SUPPLY BATTERY & CHARGER ASSEMBLY NR 4 IAW AMM 33-50-04. OPERATIONAL CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1ASMI SN 67814.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,634 hrs · 29,886 cycles

OVERHEAD AISLE EMER LIGHT AT ROW 16 INOPERATIVE. R & R ROW 16 AISLE EMER LIGHT BULB IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: TERMINAL — LOOSE (CABIN) · airframe 33,358 hrs · 29,630 cycles

MAIN DOOR ENTRANCE EMER LAMP INOPERATIVE. R & R THE MAIN CABIN DOOR MOUNTED EMER LIGHT LAMP IAW AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. NO FIX, SECURED LOOSE GND WIRE TERMINAL IAW WM CHAPTER 20-00-03, OPERATIONS CHECKED GOOD, NO DEFECTS NOTED END.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 33,109 hrs · 29,389 cycles

PASSENGER MAIN ENTRY DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED MAIN DOOR ROLLERS. OPERATIONS CHECKED GOOD IAW AMM 52-10-01.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 32,963 hrs · 29,279 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00. OPERATIONS CHECK IS GOOD AT THIS TIME.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 32,893 hrs · 29,219 cycles

FORWARD PAX CABIN FLASHLIGHT DAMAGED. R & R FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DAMAGED (COCKPIT) · airframe 32,893 hrs · 29,219 cycles

FIRST OFFICERS FLASHLIGHT DAMAGED. R & R FIRST OFFICERS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DAMAGED (COCKPIT) · airframe 32,893 hrs · 29,219 cycles

PILOTS FLASHLIGHT DAMAGED. R & R PILOTS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 32,548 hrs · 28,877 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED DOOR ROLLERS & PERFORMED OPERATIONS CHECK OF CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED OK.

Part: PANEL — CRACKED (CARGO BAY) · airframe 32,145 hrs · 28,513 cycles

CARGO PANEL 271ALW IS CRACKED. REPAIRED COMPOSITE DAMAGE FOR CARGO PANEL 271ALW IAW ETN-EM-25-329.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 32,145 hrs · 28,513 cycles

LT MLG WELL PANEL 155QZ HAS A CRACKED SUPPORT BRACKET. R & R CRACKED SUPPORT BRACKET IAW SRM 51-40-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,145 hrs · 28,513 cycles

DURING EMERGENCY LIGHTING OPERATIONS CHECK FOUND EMERGENCY LIGHT STRIP NR 4 & NR 5, RT & LT EMERGENCY EXIT LOWER EXIT SIGNS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY NR 3 IAW AMM 33-50-04-400-802-A. R 7 R EMERGENCY LIGHT POWER SUPPLY NR 3 IAW AMM 33-50-04-400-801-A. R & R EMERGENCY LIGHT DC, AC INVERTER NR 5 IAW AMM 33-50-11-400-801-A. ALL EMERGENCY LIGHTS OPERATIONS CHECKED GOOD.

Part: STRUCTURE — CRACKED (CABIN) · airframe 32,145 hrs · 28,513 cycles

CABIN EMERGENCY LIGHTS RT SIDE WALL EXTRUSION NR 5 CRACKED. R & R CABIN EMERGENCY LIGHT RT SIDE WALL EXTRUSION NR 5 IAW AMM 33-50-12.

Part: BEARING — CORRODED (ELEVATOR) · airframe 32,145 hrs · 28,513 cycles

LT INBD, CTR & OTBD ELEVATOR HINGE FITTINGS ON HORIZONTAL STAB HAVE CORRODED BEARINGS. R 7 R BEARINGS ON LT INBD, CTR & OTBD ELEVATOR HINGE FITTINGS ON HORIZONTAL STAB IAW AMM 20-10-08.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 32,145 hrs · 28,513 cycles

BATTERY INOPERATIVE. R & R BATTERY.

Part: WIRE — BROKEN (CABIN) · airframe 32,145 hrs · 28,513 cycles

LT CABIN EMERGENCY LIGHT STRIP NR 9 HAS BROKEN WIRE. R & R LT CABIN EMERGENCY LIGHT STRIP NR 7 IAW AMM 33-50-12. REF BOW151597 FOR OPERATIONAL CHECK.

Part: BRACKET — CRACKED (LT WING) · airframe 32,145 hrs · 28,513 cycles

LEFT WING OVERWING PANEL NUTPLATE ANGLE BRACKETS AT FRAME 48 IS CRACKED. REMOVED & INSTALLED NEW ANGLE BRACKET ON LT WING AT FRAME 48 IAW ETN-EM-53-142.

Part: WIRE — BROKEN (CABIN) · airframe 32,145 hrs · 28,513 cycles

LT CABIN EMERGENCY LIGHT STRIP NR 8 HAS BROKEN WIRE. R & R LT CABIN EMERGENCY LIGHT STRIP NR 8 IAW AMM 33-50-12. REF BOW151597 FOR OPERATIONAL CHECK.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 32,145 hrs · 28,513 cycles

RT WING FUEL VENT LINE SUPPORT BRACKET IS CRACKED AT RT RIB 3. REMOVED & INSTALLED NEW FUEL VENT LINE SUPPORT BRACKET ON RT WING AT RT RIB 3 IAW AMM 20-10-01.

Part: WIRE — BROKEN (CABIN) · airframe 32,145 hrs · 28,513 cycles

EMERGENCY FLOOR LIGHTING NR 5 HAS A BROKEN WIRE. REPLACED MISSING CONNECTOR IAW SWPM 20-50-00. SEE BOW 151597 FOR OPERATIONS CHECK.

Part: BRACKET — CRACKED (RT WING) · airframe 32,145 hrs · 28,513 cycles

RT OVERWING PANEL NUTPLATE ANGLE BRACKETS AT FRAMES 41,42 & 48 ARE CRACKED. R & R RT WING ANGLE BRACKET IAW SRM CH 51-40-02.

Part: WIRE — BROKEN (CABIN) · airframe 32,145 hrs · 28,513 cycles

EMERGENCY FLOOR LIGHTING STRIP NR 1 HAS BROKEN WIRE. REPLACED MISSING CONNECTOR IAW SWPM 20-50-00. SEE BOW 151597 FOR OPERATIONS CHECK.

Part: RIB — CRACKED (RT NACELLE) · airframe 32,145 hrs · 28,513 cycles

RT UPPER ENG COWL OTBD RIB IS CRACKED JUST AFT OF THE AFT MOST ATTACHMENT HINGE POINT. REPAIRED RT UPPER ENG COWL OTBD RIB IAW SRM 54-10-07.

Part: WIRE — BROKEN (CABIN) · airframe 32,145 hrs · 28,513 cycles

LT CABIN EMERGENCY LIGHT STRIP NR 5 HAS BROKEN WIRE. R & R LT CABIN EMERGENCY LIGHT STRIP NR 5 IAW AMM 33-50-12. SEE BOW151597 FOR OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,644 hrs · 28,113 cycles

AFT EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. R 7 R NR 4 EMERGENCY BATTERY & POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPERATIONS CHECKED GOOD IAW EMB 145 AMM 33-50-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,594 hrs · 28,079 cycles

EMERGENCY LIGHTING SYS OVERWING INOPERATIVE. REMOVED & INSTALLED NEW NR 4 EMERGENCY LIGHTING BATTERY POWER SUPPLY PER WORK CARD 33-700-19.

Part: DISPLAY — FAILED (COCKPIT) · airframe 30,836 hrs · 27,445 cycles

VERY STRONG BURNING ODOR IN COCKPIT, FOLLOWED BY NR 1 PFD FAILURE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NR 1 PFD IAW AMM 34-22-01. OPS CHECKED NORMAL IAW 34-22-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,507 hrs · 27,167 cycles

THE CREW REPORTED THE F/O FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW 25-60-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 29,881 hrs · 26,621 cycles

DURING PS-1 CHECK FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — BROKEN (FLASHLIGHT) · airframe 29,710 hrs · 26,482 cycles

ON FLIGHT 4177 THE CREW REPORTED THE FIRST OFFICER’S SIDE FLASHLIGHT HOLDER HAD A BROKEN CLIP, IT DID NOT HOLD THE FLASHLIGHT PROPERLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S SIDE FLASHLIGHT IAW EMB MM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 29,521 hrs · 26,322 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 3 AND 7 INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 28,833 hrs · 25,800 cycles

ON FLIGHT 2862 THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED AN EICAS RUDDER SYSTEM 2 INOP MESSAGE. THE CREW COMPLETED THE AOM VOL 1 CHECK LIST, NOTIFIED SOC AND ATC, DECLARED AN EMERGECNY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE DRIVEN PUMP PRESSURE SWITCH IAW EMB 145 AMM 29-10-19. DID NOT FIX. FURTHER TROUBLESHOOTING FOUND THE SYS 2 EMDP PRESSURE SWITCH HAD NO GROUND ON PINS A TO B. REMOVED AND REPLACED IAW EMB-145 AMM 29-30-04. THE OPERATIONAL CHECK OF THE RUDDER SYSTEM WAS GOOD IAW 27-23-00. FOUND PATH THRU RELAY K0362 OPEN. REMOVED AND REPLACED RELAY K0362 REF EMB 145 AMM 20-13-02. THE OPERATIONAL CHECK WAS GOOD REF EMB 145 WM 27-23-50 AND EMB 145 AMM 71-00-01. INSTALLED RELAY K0384 REF EMB 145 AMM 20-13-02. THE OPERATIONAL CHECK WAS GOOD REF EMB 145 WM 27-23-50 AND EMB 145 AMM 71-00-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 28,091 hrs · 25,216 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE CAPTAIN'S FLASHLIGHT WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 27,996 hrs · 25,146 cycles

FLIGHT 3285, CREW REPORTED FORWARD FLIGHT ATTENDANT FLASHLIGHT WOULD NOT CHARGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT AND BASE ASSEMBLY IAW CMM 25-60-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,878 hrs · 25,050 cycles

CARGO DOOR CUTOUT FWD LOWER CORNER CORRODED. REPAIRED CARGO DOOR CUT OUT FWD LOWER CORNER IAW AEA EO-EM-53MR-1129.

Part: SHEAR TIE — CORRODED (DOOR FRAME) · airframe 27,878 hrs · 25,050 cycles

REPAIR CORROSION ON FRAME 65 AND SHEAR TIE AT CARGO DOOR CUTOUT. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 27,881 hrs · 25,055 cycles

DURING MAINTENANCE INSPECTION, FOUND THE NR 1 FLOOR PROXIMITY LIGHT MISSING WIRE CONNECTORS. AIRCRAFT REMOVED FROM SERVICE. INSTALLED CONNECTOR IAW SWPM 20-21-00 AND 20-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,881 hrs · 25,055 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT MISSING BLACK FILLER STRIPS. AIRCRAFT REMOVED FROM SERVICE. INSTALLED SERVICEABLE LIGHT BLACK FILLERS IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,877 hrs · 25,050 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT EMERGENCY OVERWING LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLAPPER VALVE — FAULTY (RT WING) · airframe 27,707 hrs · 24,921 cycles

ON FLIGHT 4119 AFTER DEPARTURE THE AIRCRAFT BEHIND WAITING FOR TAKEOFF ADVISED ATC THEY NOTICED FLUID COMING FROM THE RT WING AFTER TAKEOFF. THE CREW WAS NOTIFIED AND THE FO CHECKED OUT HIS WINDOW AND SAW FUEL COMING FROM OUTBOARD THE RT OUTER FLAP. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE NUMBER 2 ENGINE WAS SHUT DOWN FOR TAXI IN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OUTBOARD FUEL TANK FLAP VALVE AT RIB 19 IAW EMB-145 AMM 28-11-04. THE LEAK CHECK WAS GOOD. REFERENCE NRWC # 651-ORD-00898 FOR ALL WORK PERFORMED AND PARTS. ACCESS DOOR SEAL PART NUMBER:SD145-69685-009. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 27,118 hrs · 24,416 cycles

FLIGHT 3217, THE CAPTAIN’S EMERGENCY FLASHLIGHT CRADLE CRACKED. FLASHLIGHT WOULD NOT STAY IN PLACE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CRADLE. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: CONTACTOR — DEFECTIVE (TAXI LIGHT) · airframe 26,750 hrs · 24,138 cycles

FOR FLIGHT 2954 THE CAPTAIN, FIRST OFFICIER, FLIGHT ATTENDANT AND GATE AGENT ALL SMELLED AN ELECTRICAL BURNING ODOR AS THE AIRCRAFT WAS PARKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE UPPER TAXI LIGHT CONTACTOR IAW 145 AMM 33-42-03. OPT CHECK WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 26,627 hrs · 24,048 cycles

ON FLIGHT 2855 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED A BAGGAGE SMOKE WARNING MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND FOLLOWED MEMORY ITEMS AND AOM PROCEDURES. THE CREW BLEW THE FIRE BOTTLES. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT SMOKE DETECTOR IN CARGO AREA IAW EMB 145 AMM 26-15-01. REMOVED AND REPLACED HIGH RATE BAGG FIRE BOTTLE IAW EMB 145 AMM 26-23-01. REMOVED AND REPLACED METERING BAGG FIRE BOTTLE IAW EMB 145 AMM 26-23-01. REMOVED AND REPLACED METERING BAGG FIRE BOTTLE IAW EMB 145 AMM 26-23-01. REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR IN CARGO AREA IAW EMB 145 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD FOR ALL OF THE ABOVE. PART NUMBERS: CARTRIDGE M30903870; FIREX BOTTLE-224 CU.IN. 337000271 SERIAL NUMBER 36346D1; CARTRIDGE M30903870; FIREX BOTTLE-630 CU.IN. 346000731SEIRAL NUMBER 16052F1; CARGO AREA SMOKE DETECTOR 473597-13 2451.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,061 hrs · 23,648 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY LIGHT ABOVE MAIN SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ABOVE MAIN SERVICE DOOR IAW EMB 145 AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,061 hrs · 23,648 cycles

EMERGENCY LIGHT ABOVE MAIN SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY LAMP ABOVE MAIN SERVICE DOOR IAW EMB 145 AMM 335006, OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,942 hrs · 23,564 cycles

ON FLIGHT 3305 THE CREW REPORTED THE SIDE LIGHTING IN CABIN, RIGHT SIDE FROM 5TH ROW THRU 12 ROW AND 15 ROW THRU 18, AND LEFT SIDE FROM ROW 9 THRU 11 AND 15 THRU 18 STOPPED WORKING; ACRID SMELL ACCOMPANIED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED SIDE PANEL LIGHTS, INVERTER, BALLAST; NO DAMAGE FOUND. RESET AIRCRAFT ELECTRCAL POWER. ALL LIGHTS OPERATING NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,009 hrs · 21,294 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT STRIP AT FLOOR PANEL 241BF TO HAVE A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP AT FLOOR PANEL 241BF IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,301 hrs · 20,711 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — CRACKED (A/C PACK) · airframe 21,007 hrs · 19,645 cycles

ON FLIGHT 2854 DURING THE CLIMB THE CREW REPORTED, RECEIVED AN EICAS MESSAGE REGARDING SMOKE IN THE LAV AND SMOKE IN THE CABIN. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ENT EM-72-034 R4. NO DEFECTS NOTED. FOUND THE NUMBER 1 PACK AIR DUCT TO BE CRACKED. REMOVED AND REPLACED THE NR 1 PACK AIR DUCT IAW EMB AMM 21-25-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,280 hrs · 18,952 cycles

ON FLIGHT 4265 THE CREW REPORTED THAT THE SECOND AND THIRD FLOOR PROXIMITY STRIPS FOR THE EMERGENCY LIGHTING SYSTEM WERE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. OPERATIONAL CHECK OF THE SECOND AND THIRD FLOOR PROXIMITY LIGHTS GOOD IAW EMB 145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,280 hrs · 18,952 cycles

ON FLIGHT 4265 THE CREW REPORTED THAT THE SECOND AND THIRD FLOOR PROXIMITY STRIPS FOR THE EMERGENCY LIGHTING SYSTEM WERE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. OPERATIONAL CHECK OF THE SECOND AND THIRD FLOOR PROXIMITY LIGHTS GOOD IAW EMB 145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,075 hrs · 171,150 cycles

DURING IMBV INSPECTION FOUND LEFT OMEGA BEAM TO BE CORRODED JUST FORWARD OF FRAME 29. REPAIRED OMEGA BEAM BY CUTTING OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW IMB SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,075 hrs · 171,150 cycles

DURING MBV INSPECTION FOUND AFT SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,075 hrs · 17,150 cycles

DURING MBV INSPECTION FOUND CENTER SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-02 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,075 hrs · 17,150 cycles

DURING MBV INSPECTION FOUND FORWARD SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-10 FIGURE 204. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 14,832 hrs · 14,319 cycles

LEFT OVERWING AND AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED. REMOVED AND REPLACED BATTERY CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: CARBON SEAL — FAILED (ENGINE 2) · airframe 14,241 hrs · 13,848 cycles

NUMBER 2 ENGINE OIL QUANTITY DROPPED TO 4 QUARTS, OIL PRESSURE STARTED TO DROP. CREW SHUTDOWN ENGINE. DIVERTED TO CID. POSTFLIGHT INSPECTION REVEALED OIL ON NUMBER 2 ENGINE COWL. REMOVED AND REPLACED NUMBER 4 GENERATOR AND CARBON SEAL ASSEMBLY PER EMB AMM 72-53-10 AND AMERICAN EAGLE WORK CARD 24-800-00. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: REPAIR — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 13,302 hrs · 13,061 cycles

PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED REPAIR DOUBLERS, CLEANED, TREATED AND INSTALLED REPAIR DOUBLERS AND RESTORED PREVIOUS FINISH IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,302 hrs · 13,061 cycles

FOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED DOUBLER, CLEANED AND TREATED AND INSTALLED REPAIR DOUBLER. RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 8,488 hrs · 8,633 cycles

CREW REPORTED THE EMERGENCY LIGHTS AT SEAT 3BC AND GALLEY SERVICE DOOR ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR PLUG LOOSE ON BATTERY PACK RECONNECTED CONNECTOR PLUG. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501826) (K)

Part: FLOOR SUPPORT — CORRODED (FR 20) · corrosion level 2 · airframe 8,477 hrs · 8,625 cycles

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM.(K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,477 hrs · 8,625 cycles

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (SERVICE DOOR) · airframe 8,477 hrs · 8,625 cycles

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED ATHE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K)

Part: STRINGER — GOUGED (FUSLEAGE) · airframe 8,477 hrs · 8,625 cycles

DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND GOUGED FWD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FAB 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)

Part: STRINGER — GOUGED (FUSELAGE) · airframe 8,477 hrs · 8,625 cycles

DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND GOUGED FORWARD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)

Part: ECU — MALFUNCTIONED (E/E BAY)

LRD - FLT 3453 - DURING APPROACH, CREW REPORTED THE FLAPS WOULD NOT DEPLOY. FOLLOWED AOM PROCEDURES AND LANDED WITHOUT FLAPS WITH NO OTHER PROBLEMS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - FOUND DENT ON FUSELAGE UNDER RIGHT ENGINE FRAME 65, 66, 57, STRINGER 14R. DENT WAS REPAIRED IAW EO NR EM-53MR-391 PART A. (M)