N682AE

Part: VALVE — ABNORMAL (ZONE 200) · airframe 46,468 hrs · 43,892 cycles

STRONG SMELL/ODOR WITH APU & BOTH PACKS ON IN COCKPIT. FACT 07NOV25 19:12 PHL REMOVED LH DUAL VALVE IAW AMM 21-60-01 AND ASSOCIATED CLAMPS+ DUCTS. INSTALLED LH DUAL VALVE IAW AMM 21-60-01, OPS CHECK GOOD. RAN PACKS FOR AN HOUR WITH BOTH APU & ENGINES. NO SMELL IN COCKPIT. AC OK FOR SERVICE AT THIS TIME.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,116 cycles

53-2428 UNDER BAGGAGE DOOR POST SUPPORT IS CRACKED AT FR68. REPAIRED IAW ETD2025-145-902791

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2229 SHEAR CLIP CRACKED AT FR80 BTW STR 5-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2177 SHEAR CLIP CRACKED AT FR61 BTW 6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2179 SHEAR CLIP CRACKED AT FR61 BTW STR 6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 800) · airframe 45,116 hrs · 42,277 cycles

53-2122 ALL 3 CARGO DOOR MECH SUPPORT BRACKETS CRACKED AT BTW FR67-68, BTW STR 4-5R. RAR BRACKETS IAW SRM 51-40-02

Part: FRAME ANGLE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2109 ANGLE CRACKED AT LH TOP OF FR10. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2102 LH OMEGA BEAM CRACKED AT FR22. REPAIRED IAW ETD2025-145-901886 AND EO 1-53-25-0074

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,116 hrs · 42,277 cycles

53-2098 RH SILL #6 CORRODED BTW FR53-59. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2101 LH OMEGA BEAM FOUND CRACKED AT FR21. REPAIRED IAW ETD 2025-145-901886 AND EO 1-53-25-0094

Part: SUPPORT — CRACKED (ZONE 800) · airframe 45,116 hrs · 42,277 cycles

53-2121 CARGO DOOR MECH, FWD SUPPORT CRACKED AT BTW FR61-62. BTW STR4-5R. RAR SUPPORT IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2135 SHEAR CLIP CRACKED AT FR66 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2139 SHEAR CLIP CRACKED AT FR73 BTW STR8-10R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2110 RH TOP FUSELAGE ANGLE CRACKED AT FR10. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2127 SHEAR CLIP CRACKED AT FR62 BTW STR6-8L. RAR SHEAR CLIP IAW SRM 51-40-02 AND EO 1-53-25-0080

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,116 hrs · 42,277 cycles

53-2114 BAG DOOR SURROUND LWR BEAM CORRODED. RAR BEAM IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2126 LH WING TO BODY FAIRING, ANGLE SUPPORT #5 CRACKED. REPAIRED ANGLE IAW SRM 57-20-01

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2137 SHEAR CLIP CRACKED AT FR65 BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — DAMAGED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2118 AT CARGO ENTRY, T-PROFILE AND LWR ANGLE DAMAGED AT FR67. REPAIRED IAW ETD2025-145-902286 REV. A AND EO 1-53-25-0078

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2125 CRACKED LH WING TO BODY FAIRING SUPPORT ANGLE. REPAIRED SUPPORT ANGLE IAW SRM 57-20-01

Part: STRIP — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2129 RH WING TO BODY FAIRING, STRIP BTW FR48-49 CRACKED. REPAIRED STRIP IAW SRM 53-23-12

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2051 SHEAR CLIP CRACKED AT FR25 BTW STR 15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: STIFFENER — CRACKED (ZONE 400) · airframe 45,116 hrs · 42,277 cycles

78-2071 RH TR UPPER IB AISLE STIFFENER CRACKED. REPAIRED IAW ESR1-78-25-001

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2061 LH OMEGA BEAM CRACKED AT FR33. REPAIRED IAW ETD2025-145-901900 AND EO 1-53-25-0077

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,116 hrs · 42,277 cycles

53-2055 RH SILL #1 CORRODED BTW FR23-29. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2050 SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2054 SHEAR CLIP CRACKED AT FR28 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2056 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: RIVET — LOOSE (ZONE 400) · airframe 45,116 hrs · 42,277 cycles

78-2072 LOOSE RIVETS ON RH TR FIXED EXTERNAL SKIN. REPAIRED IAW ESR 1-78-22-002A

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2083 LH IB OMEGA BEAM ANGLE TO WING BOX CRACKED AT BTW FR47-50. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 45,116 hrs · 42,277 cycles

53-2075 RH SILL #2 CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2052 SHEAR CLIP CRACKED AT FR25 BTW STR 16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2053 SHEAR CLIP CRACKED AT FR27 BTW STR15-16R

Part: RIVET — MISSING (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2060 RIVET MISSING ON LH OMEGA BEAM AT FR31 IB SIDE. REPAIRED IAW ETD 2025-145-0901900 AND EO1-53-25-0077

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

CTR OMEGA BEAM CRACKED AT FR27. REPAIRED IAW ETD2025-145-901908

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,116 hrs · 42,277 cycles

53-2086 LH WING STUB FWD ANGLE CRACKED ON INNER FUSE AT FR46. RAR ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2059 LH OMEGA BEAM CRACKED AT FR28. REPAIRED OMEGA BEAM IAW ETD2025-145-901890 AND EO1-53-25-0096

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2049 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PLATE — CRACKED (ZONE 400) · airframe 45,116 hrs · 42,277 cycles

78-2066 OB KICKER PLATE CRACKED ON RH TR UPPER DOOR ASSY. REPAIRED IAW ESR1-78-24-007A

Part: SKIN — DENTED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2038 DENT ON LH LWR SKIN BTW FR80-81, BTW STR14-15L. REPAIRED IAW ETD 2025-145-901511 AND EO 1-53-25-0073.

Part: SKIN — DAMAGED (ZONE 200) · airframe 45,116 hrs · 42,277 cycles

53-2033 CRACK AROUND RIVET AT FR78 BTW STR5-6R. REPAIRED IAW SRM 52-32-01 AND EO 1-53-25-0071

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,221 hrs · 39,027 cycles

ON CLIMB OUT AT FL80 NO AIRFLOW FROM PACK 1 OR 2 WITH NO PRESSURIZATION. BURSTING DUCT NOISE FROM UNDER FLT DECK FLOOR. UPON INSPECTION OF AIRCRAFT FOUND DUCT FROM HEAT EXCHANGER ON PACK 1 COMPLETELY DETACHED AND SLEEVES DAMAGED. R/R SLEEVES AND CLAMPS IN REF TO AMM 21-20-04. PERFORMED COOLING SYSTEM OPS CHECK. OPS CHECK GOOD. PERFORMED PRESSURIZATION CONTROL SYSTEM ADJUSTMENT TEST IAW AMM 21-31-00. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,873 hrs · 38,638 cycles

BLD 2 LEAK ON EICAS IN FLIGHT. FACT 14JUN23 23:05 CLT R/R CLAMP ABOVE CROSSBLEED VALVE ON PIPE LEADING FROM APU REF AMM 20-10-10-910-801-A NO FIX. BLEED 2 LEAK STILL APPEARS ON EICAS.FOUND Y DUCT ON RH PACK AT Y DUCT. R/R SLEEVE IRT 21-60-01 OPS CHECK GOOD LEAK CHECK GOOD.A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,717 hrs · 38,466 cycles

LG AIR GRUND SYSTEM FAILURE AND VOICE FLAPS AND TRIM NOTE: LG AND FLAPS WAY UP CAUTION MSG ERASE AT 6000 AND VOICE TOO FACT 07MAY23 15:50 PHL RR LEGU IAW AMM 32-32-01 AND R&R LH LG AIR GROUND PROX SWITCHES IAW AMM 32-63-01. PERFORMED GEAR SWING MULTIPLE TIMES. NO DEFECTS NOTED. NO MSG FOUND ON EICAS. OK FOR SERVICE AT THIS TIME

Part: SKIN — CRACKED (FRM 79) · airframe 40,886 hrs · 37,553 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 79 LH SIDE BELOW VERTICAL STAB .... REPAIRED FUSELAGE EXTERNAL SKIN AROUND 2 FASTENERS ON FR 79 LH SIDE BELOW VERTICAL STAB IAW EO1-53-22-0229

Part: SKIN — CRACKED (FRM 77) · airframe 40,886 hrs · 37,553 cycles

E943764 - FUSELAGE EXTERNAL SKIN CRACKED AROUND FASTENER ON FR 77 BTW STR 4R-5R. .... REPAIRED FUSELAGE EXTERNAL SKIN AROUND FASTENER ON FR 77 BTW STR 4R-5R IAE EO1-53-22-0230.

Part: SKIN — CRACKED (FRM 77) · airframe 40,886 hrs · 37,553 cycles

E943631 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 77 LH SIDE BELOW VERTICAL STAB .... UPON FURTHER INVESTIGATION ONLY 1 AREA ON FUSELAGE SKIN FOUND TO BE CRACKED. REPAIRED FUSELAGE EXTERNAL SKIN AROUND FASTENER ON FR 77 LH SIDE BELOW VERTICAL STAB (BETWEEN STR 3L-4L) IAW EO1-53-22-0229.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 40,886 hrs · 37,553 cycles

E944174 - GALLEY R/H FLOOR BEAM FWD DIAMOND GUSSET HAS CORROSION .... REMOVED AND REPLACED GALLEY R/H FLOOR BEAM FWD DIAMOND GUSSET IAW EMB145 SRM 51-40-02

Part: A/C PACK — ODOR (NR 1) · airframe 38,442 hrs · 34,758 cycles

BURNING SMELL FROM PACK 1 WHEN DOORS CLOSED. SMELL DISAPPATED WHEN PACK 1 TURNED OFF.- THIS DISCREPANCY IS ON LP 240083 SEQ 1 BUT MERLIN SAYS IT IS ALREADY USED. VERIFIED IT AND THAT IS WHY THIS IS LISTED AS SEQ 4. MX RAN PACK 1 WITH CREW. NO DEFECTS OBSERVED. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 38,303 hrs · 34,597 cycles

PAX DOOR WILL NOT OPEN FROM INTERIOR HANDLE. FOUND DOOR HANDLE LOOSE, RESECURED HANDLE IAW WITH 52-11-01 OPS CHECK GOOD NO DEFECTS NOTED HANDLE WAS NOT REMOVED.

Part: BUSS BAR — FAILED (WINDOW HEAT) · airframe 37,450 hrs · 33,657 cycles

PDIS 682 30-42 2191311 24SEP20. CLT CLOSE WINDSHIELD HEAT 1 FAILED ON TAXI. P/C C/B G-13 AND COLLARED C/B (ORIGINALLY PLACED ON MEL 9/24). DURING TROUBLESHOOTING, REPLACED BUS BAR AND WINDSHIELD HEAT FUSE, WHICH WAS FOUND MELTED TO THE BUS BAR.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG) · airframe 36,940 hrs · 33,065 cycles

LANDING GEAR LEVER DISAGREE MESSAGE AFTER GEAR RETRACTION. LANDING GEAR AMBER INDICATION. CYCLED LANDING GEAR PER QRH MESSAGE CLEARED. FOLLOWED FIM 32-32-00-810-803-A/ 32-63-00-810-804-A. NO DEFECTS. INSP HARNESSES AND WIRING. NO DEFECTS. CW LG PROX SWITCH TEST. NO DEFECTS. R+R NLG UPLOCK BOX IAW AMM 32-33-07. R+R BOTH UPLOCK PROX SW AND NLG SEQ PROX SW IAW AMM 32-33-07. ALL 3 OPS TEST GOOD. OK FOR SERVICE SUBJECT TO SUCCESSFUL EVAL FLIGHT. T/S LP 212784-1. FOUND LH NLG WHEEL SPIN BRAKE WORN TO LIMITS. R+R NLG WHEEL SPIN BRAK IN REF TO AMM 32-49-06. A/C RELEASED FOR EVALUATION FLIGHT DUE TO LG/LEVER DISAGREE MESSAGE ON EICAS. AFTER GEAR RETRACTION. MAINTENANCE ACTION COMPLETED SUBJECT TO SATISFACTORY EVALUATION FLIGHT. REF LP 212784 SEQ 1. EVAL FLIGHT SATISFACTORY.

Part: SOLENOID VALVE — MALFUNCTIONED (NLG DOORS) · airframe 36,936 hrs · 33,059 cycles

DURING GEAR RETRACTION NLG CAME UP WITH AN IMPACT NOISE,PAUSED THEN REPEATED. DOORS NEVER DID SHUT....FIX:R&RD NLG DOOR SOLENOID VALVE IAW EMB AMM 32-33-02 OPS/LEAK TEST SATISFACORY. OK FOR SERVICE

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG) · airframe 36,939 hrs · 33,063 cycles

DURING GEAR RETRACTION, NLG CAME UP WITH A LOUD IMPACT NOISE,PAUSED THEN REPEATED,DRS NEVER DID SHUT....FIX:R&RD LG ELECTRONIC UNIT IAW AMM 32-32-01. OPS TEST/GEAR SWING SATISFACORY IN HANGER.REQ EVALUATION FLT...EVALUATION FLT SATISFACORY

Part: B-NUT — LOOSE (HYD LINE) · airframe 36,385 hrs · 32,426 cycles

PDIS 682 29-13 2001241 18OCT19 PHL CLOSE HYD 1 SYS QTY INDICATION SHOWED ZERO DURING FLIGHT A LONG WITH ASSOCIATED FAILURE MESSAGES FACT 18OCT19 17:20 PHL INSPECTED A/C NOTED LH NLG DOOR LH ACTUATOR HYD HOSE TO BE LOOSE AT B-NUT. RE TORQUE HYD HOSE SERVICE HY D #1 AND CYCLED LANDING GEAR SEVERAL TIME WITH NO DE FECT OR LEAK NOTED. REF AMM 29-10-03-06, 32-33-03-04. OK FOR SERVICE.

Part: ALTIMETER — FROZEN (STANDBY) · airframe 36,335 hrs · 32,371 cycles

STBY ALTIMETER IS FROZEN. R & R INTG STBY INST(ISIS)IAW EMB AMM 34-01-01 OPERATIONAL/LEAK CHECK GOOD.OK FOR SERVICE

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,796 hrs · 31,722 cycles

AFTER PAX DOOR CLOSED, BURNING SMELL NOTED AROUND FLT DECK AREA. FIX: RAN PACK #1 & #2 NO SMELL NOTED. TAXIED PLANE WITH PACKS ON. NO SMELL NOTED. OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (FAN AIR) · airframe 34,750 hrs · 30,521 cycles

PDIS 682 36-20 1665443 29NOV18 ROA CLOSE BLEED 2 LOW TEMP EICAS MESSAGE WHILE IN ICEING CONDITIONS. INCREASED THRUST DID NOT CORRECT HISTORY: NO FACT 29NOV18 17:37 ROA R&R FAN AIR VALVE IAW AMM 36-11-03. GROUND RAN BOTH ENGINES WITH PACKS ON , A/ICE SYS ON NO DEFECTS NOTE D OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 34,342 hrs · 30,044 cycles

RT WING EMERGENCY LIGHT IS INOP. R&R BULB AT SAID LOCATION, RESECURED LIGHT LENS USING RETAINED HARDWARE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 33,102 hrs · 28,653 cycles

DURING CARGO BAY SMOKE DETECTION TEST, SWITCH LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED THE SMOKE DETECTOR IAW 26-15-01-00/400-801-A, OPS CHECKED GOOD, NO DEFECTS NOTED. OK FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 32,804 hrs · 28,339 cycles

RIGHT WINDSHIELD HEAT SWITCH WILL NOT ENGAGE. R & R THE WINDSHIELD HEAT SWITCH COVER. OPS CHECKED GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 32,764 hrs · 28,303 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-10-000-400-801-A, OPS CHECKED GOOD. OK FOR SERVICE.

Part: SKIN — PUNCTURED (FRAME 78) · airframe 32,643 hrs · 28,186 cycles

FUSELAGE SKIN PUNCTURED JUST AFT OF FRAME 78, BETWEEN STRINGERS 5R AND 6R. COMPLIED WITH ERS-EM-53MR-2943.

Part: MOUNT — CRACKED (PAX DOOR HANDLE) · airframe 32,643 hrs · 28,186 cycles

PAX DOOR INNER HANDLE TORQUE BOX SUPPORT HAS A ONE INCH CRACK. THE MOUNTING BRACKET WAS REPAIRED IAW EM-52-MR-162.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 32,643 hrs · 28,186 cycles

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

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 32,643 hrs · 28,186 cycles

AFT WALL OF RIGHT MLG WHEEL WELL HAS A 1 INCH CRACK THAT IS VISIBLE FROM THE AFT SIDE OF WALL. REPAIRED RT MLG WW BULKHEAD IAW SRM 53-23-12.

Part: ATTACH ANGLE — CRACKED (WG-BDY FAIRING) · airframe 32,643 hrs · 28,186 cycles

LEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE ON WING HAS 1/8 INCH CRACK JUST AFT OF SPAR 2. R & R THE ATTACH ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (WG-BDY FAIRING) · airframe 32,643 hrs · 28,186 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE HAS A 1/2 INCH CRACK JUST FWD OF SPAR 2. REPAIRED THE ATTACH ANGLE IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (WG-BDY FAIRING) · airframe 32,643 hrs · 28,186 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE ON FUSELAGE HAS 1/8 INCH CRACK BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,643 hrs · 28,186 cycles

NR 5 EMERGENCY LIGHT IS DAMAGED. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,643 hrs · 28,186 cycles

SIGN ON AFT SIDE OF G2 GALLEY INOPERATIVE. INSTALLED A NEW POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,643 hrs · 28,186 cycles

NR 4 EMERGENCY LIGHT IS DAMAGED ON THE END. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,643 hrs · 28,186 cycles

R1 AND R7 EMERGENCY LIGHT PROFILES ARE CRACKED AND DAMAGED. REPLACED THE R1 AND R7 EMERGENCY LIGHT PROFILES IAW AMM 33-50-12.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,643 hrs · 28,186 cycles

NR 2 AND 3 EMERGENCY LIGHTS FOUND INOPERATIVE. INSTALLED A NEW POWER SUPPLY AND BATTERY IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,382 hrs · 27,958 cycles

LT EXTERNAL WING EMERG LIGHT FOUND BURNT ON INSPECTION. REMOVED AND REPLACED BULB ON LT WING EMERGENCY LIGHT REF AMM 33-50-10. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,268 hrs · 27,836 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,198 hrs · 27,756 cycles

AFT CABIN FLOOR MOUNTED EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,112 hrs · 27,670 cycles

CABIN CEILING AISLE EMERGENCY EXIT LIGHT AT ROW 12 INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT IAW AMM 33-50-08, OPS CHECKED GOOD.

Part: PITOT TUBE — DAMAGED (RIGHT) · airframe 32,086 hrs · 27,638 cycles

DURING CRUSE, AT FL 350 RECEIVED A TAS MESSAGE ON BOTH CA AND FO AIRSPEED INDICATIONS. RAN CHECKLIST, DID NOT DETERMINED BAD AIRSPEED VOIT CAUTION. DESCENDED TO LOWER ALTITUDE TO WARM, DETERMINED CA'S AIRSPEED UNRELIABLE AND APPLIED APPROPRIATE CHECK LIST. REMOVED WATER FROM PITOT WATER TRAPS IAW AMM 34-13-00. REMOVED AND REPLACED PITOT NR 2 IAW AMM 34-13-01. PERFORMED LEAKAGE IAW AMM34-13-00, GOOD. PERFORMED HEATING TEST, GOOD IAW AMM 30-31-00. ADC SYSTEM OPS CHECKED GOOD IAW AMM 34-15-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,780 hrs · 27,322 cycles

NR 3 EMERGENCY LIGHT BATTERY INOP. REMOVED AND INSTALLED 3 EMERGENCY LIGHT BATTERY IAW EMERGENCY LIGHT WORKCARD 33-700-19, OPS. CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 12334.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,336 hrs · 26,949 cycles

FLOOR PROXIMITY LIGHT CONNECTOR IS BROKEN AT FLOOR PANEL 261BF ON AIRCRAFT SIDE-C/A- REPAIRED THE.CONNECTOR IAW SWPM 20-21-00. PERFORMED OPC IAW AMM 33-50-00. OPC GOOD.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 28,963 hrs · 24,827 cycles

CAPTAINS SIDE COCKPIT FLASHLIGHT HOLDER DOES NOT RETAIN THE FLASHLIGHT. R & R FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 28,764 hrs · 24,642 cycles

FLASHLIGHT BRACKET ABOVE FLIGHT ATTENDANT JUMP SEAT BROKEN. R & R FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT IAW AMM 33-5-16. OPERATIONS CHECKED GOOD.

Part: B-NUT — LOOSE (ANTI-ICE SYSTEM) · airframe 28,581 hrs · 24,479 cycles

ENGINE 1 ANTI-ICE FAIL ON CLIMB AT 12 - 14,000 FT. RAN CHECKLIST E1 INLET AIR OPEN. ASSOCIATED MSGS, NO ICE ANTI-ICE ON, ENG ANTI-ICE OVERPRESS. TROUBLE SHOT IAW FIM 30-21-00-810-803-A, FOUND B NUT ON LT ENG ANTI-ICE DUCT TO BE LOOSE. TIGHTENED B NUT IAW AMM 32-21-05-400-801-A. ALSO FOUND ANTI-ICE VLV CONNECTOR TO BE LOOSE, TIGHTENED PLUG IAW 30-21-01-400-801-A. OPERATIONS CHECKED IAW 30-21-00-700-803-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,410 hrs · 24,321 cycles

AFT CEILING EMER LIGHT INOPERATIVE. R & R AFT CEILING EMER LIGHT IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 28,044 hrs · 23,945 cycles

LEFT OVERWING EMER DOOR, EXIT SIGN INOPERATIVE. CONNECTED THE TWO ELEC CONNECTIONS FOR THE LT OVERWING EMER DOOR EXIT SIGN IAW AMM 33-50-14 STEP 3 I 2. OPERATIONS CHECKED GOOD IAW 33-50-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 28,002 hrs · 23,911 cycles

LEFT MLG WW AFT WEB HAS 2 EACH CRACKS. PERFORMED REPAIR ON LT MLG WW AFT WEB IAW SRM 53-23-12.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,002 hrs · 23,911 cycles

CARGO DOOR HOLD OPEN CUP SUPPORT AT FRAME 68 FLOOR LEVEL IS CRACKED APPROX 1/2 INCH ON THE LOWER ATTACHMENT POINT. REPLACED SUPPORT IAW SRM 51-40-02.

Part: PROFILE — CRACKED (E&E DOOR) · airframe 28,002 hrs · 23,911 cycles

REAR ELECTRONICS COMPARTMENT DOOR UPPER PROFILE IS CRACKED UNDER PI SUPPORT BRACKET. COMPLIED WITH PERMANENT REPAIR TO REAR ELECTRONICS COMPARTMENT DOOR IAW ERS-EM-52MR-383.

Part: ANGLE — CRACKED (RT WING) · airframe 28,002 hrs · 23,911 cycles

RIGHT WING ROOT PANEL L ANGLE BRACKET ON RT WING UPPER SURFACE IS CRACKED. REPAIRED RT FWD WING ROOT PANEL L ANGLE IAW ETN EM-53-142.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,002 hrs · 23,911 cycles

RUDDER II UPPER CTR HINGE FITTING BORES ARE WORN. R & R RUDDER II UPPER CTR HINGE FITTING ASSEMBLY IAW SRM 55-40-02 & ETN EM-55-070.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,002 hrs · 23,911 cycles

RUDDER II UPPER HINGE FITTING BORES ARE WORN. R & R RUDDER II UPPER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,002 hrs · 23,911 cycles

RUDDER II LOWER HINGE FITTING BORES ARE WORN. R & R RUDDER II LOWER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: HINGE FITTING — WORN (RUDDER) · airframe 28,002 hrs · 23,911 cycles

RUDDER II LOWER CTR HINGE FITTING BORES ARE WORN. R & R RUDDER II LOWER CTR HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: ANGLE — CRACKED (LT WING) · airframe 28,002 hrs · 23,911 cycles

LEFT WING ROOT PANEL SUPPORT ON LT WING UPPER SURFACE IS CRACKED. R & R LT WING ROOT PANEL ANGLE SUPPORT ON LT WING UPPER SURFACE IAW ETN EM-53-142. COMPLIED WITH DAMAGE TOLERANCE CHECKLIST IAW GPM 15-27.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,126 hrs · 23,068 cycles

DURING PS 2 CHECK, FOUND RT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT BULB IAW AMM 33-50-07. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — FAILED (NLG) · airframe 26,887 hrs · 22,818 cycles

AFTER TAKEOFF LOUD WIND NOISE, APPEARS NOSE GEAR DOORS DID NOT CLOSE. BURNED OFF FUEL TO GET TO LANDING WEIGHT. R & R NLG SEQUENCE PROXMITY SWITCH IAW MM 32-33-07. PERFORMED GEAR SWING SEE ITEM NR 3 THIS LOG PAGE. PERFORMED VISUAL WALK AROUND OF ACFT NO DEFECT NOTED. PERFORMED EXTENSION & RETRACTION CHECK IAW AMM 32-30-00. OPERATIONS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME ITEM 1 REMAINS OPEN.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,702 hrs · 22,679 cycles

RIGHT OVERWING EXIT SHROUD LIGHT INOPERATIVE AT SEATS 12BC. R & R NR 5 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD IAW AMM TASK 33-50-00-700-801-A.

Part: ENGINE — SMOKE (NR 1) · airframe 26,455 hrs · 22,471 cycles

THE MOST RECENT SMOKE ON SHUTDOWN EVENT OCCURED 325 FH AFTER THE PREVIOUS EVENT, AND PER BLOCK 8 OF ETN-EM-79-015. E1 SMOKING ON SHUTDOWN. RESTORED TDMI 682T7917.

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 26,425 hrs · 22,449 cycles

ON POST FLIGHT FOUND ENG NR 1 SMOKING, ENG WAS SHUTDOWN NORMALLY. DURING TAXI NOTICED SMOKE ON POST FLIGHT APPROX 10 MIN LATER. NO OIL WETTING FOUND UPON INSPECTION IAW ETN-EM-79-015. R & R LPT SHAFT PLUG O RING & MAGNETIC CARBON BREATHER SEAL WITHIN 50 FLIGHT HOURS TDMI 682T7917 IF SUBSEQUENT SMOKE ON SHUTDOWN EVENT OCCUR WHILE TDMI IS OPEN NO FURTHER INSPECTIONS REQUIRED IAW ETN-EM-79-015.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,236 hrs · 22,237 cycles

EMERGENCY EXIT AFT UPPER WALL EMER LIGHT INOPERATIVE. REMOVED RT EMER EXIT AFT UPPER WALL LIGHT, RECONNECTED WIRES & RE-INSTALLED IAW AMM 33-50-14. OPERATIONAL CHECKED GOOD IAW 145 AMM 33-50-00-700-801.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,232 hrs · 22,233 cycles

NUMBER 4 BATTERY SUPPLY INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,232 hrs · 22,233 cycles

NUMBER 3 BATTERY POWER SUPPLY INOPERATIVE. R & R NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,232 hrs · 22,233 cycles

NUMBER 1 BATTERY POWER SUPPLY INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,232 hrs · 22,233 cycles

NUMBER 2 BATTERY POWER SUPPLY INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,737 hrs · 21,768 cycles

LEFT WING FWD EXTERIOR EMER LIGHT INOPERATIVE. R & R LT WING FWD EXTERIOR EMER LIGHT BULB IAW AMM 33-50-10.

Part: CONTROL UNIT — FAILED (SPOILER) · airframe 25,464 hrs · 21,545 cycles

DURING FLIGHT 3406 AT 36000 SHORTLY ON DECENT INTO DFW THRUST LEVER AT IDLE WE FELT SPOILERS OPEN & GOT, SPOILERS FAIL, MSG. COMPLIED WITH, SPOILER FAIL, CHECKLIST & INADVERTENT SPOILER OPEN IN FLIGHT CHECKLIST UPON MOVING THRUST LEVER ABOVE IDLE MSG WENT AWAY. R & R SPOILER CONTROL UNIT IAW MM 27-63-03. OPERATIONS CHECKED GOOD IAW 27-63-01. R & R SPOILER CONTROL UNIT IAW MM 27-63-03 OPERATIONS CHECKED GOOD IAW 27-63-01.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 24,492 hrs · 20,755 cycles

ON APPROACH THE CREW RECEIVED EICAS LAVATORY SMOKE INDICATION & THE FLIGHT ATTENDANT REPORTED THE LAVATORY HORN WAS SOUNDING. THE FLIGHT ATTENDANT INDICATED NO VISIBLE SMOKE OR SMELL. THE CREW DECLARED AN EMERGENCY, COMPLIED WITH AOM VOL 1 PROCEDURES & LANDED WITHOUT INCIDENT. CFR CLEARED THE ACFT. LAVATORY SMOKE INDICATION ON EICAS. PERFORMED GVI OF EXTERIOR FOR POSSIBLE LIGHTNING STRIKE NONE FOUND. PERFORMED HIGH POWER ENG RUN WITH CREW NDN. PERFORMED OPERATIONS CHECK OF LAVATORY SMOKE DETECTOR IAW AMM 26-14-00. OPERATIONS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,208 hrs · 20,534 cycles

CENTER OMEGA BEAM CORRODED AROUND NUTPLATE HOLE AT FR 24. PERFORMED REPAIR IAW AEA ERS-EM-53MR-049.

Part: CRADLE — INOPERATIVE (FLASHLIGHT ASSY) · airframe 23,851 hrs · 20,233 cycles

F/A REAR FLASHLIGHT HOLDER WILL NOT HOLD FLASHLIGHT. REPLACED FLASHLIGHT BASE AT REAR BULKHEAD IAW AMM 25-60-00.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 23,638 hrs · 20,079 cycles

AT FL 260, CABIN ALT INDICATED 8400 FT UNABLE TO CONTROL CABIN ALT IN AUTO/MANUAL MODE. COMPLIED WITH AOM VOL 1 EMER/ABNORMAIL PROCEEDURES. PERFORMED PRESSURIZATION CONTROL SYS OPS AND FUNCTIONAL TEST IAW AMM 21-31-00. OPS CHECKED GOOD. FUNCTIONAL CHECKED GOOD. COULD NOT DUPLICATE AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: CLAMP — FAILED (NR 1 ACM) · airframe 23,140 hrs · 19,681 cycles

NR 1 PACK CYCLED OFF TWICE IN FLIGHT ABOVE FL 300 WITH AN ASSOCIATED HOT ODOR. ACFT REMOVED FROM SERVICE. PERFORMED INSPECTION OF PACK DUCTS IAW AMM 21-51-14. R & R LOWER ACM FLEXIBLE JOINT CLAMPS IAW AMM 21-51-03. LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 23,030 hrs · 19,583 cycles

DURING B-INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. FOUND LIGHT LAMP LOOSE IN SOCKET. RESECURED BULB IAW MM 33-50-09. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CLAMP — LOOSE (NR 1 PACK) · airframe 22,754 hrs · 19,374 cycles

DURING DESCENT AT APPROX 25,000 FEET WITH BOTH ENGINES IDLE A STRONG BURNING SMELL WAS DETECTED IN THE COCKPIT AND FIRST FEW ROWS OF THE CABIN. THE FLIGHT CREW PERFORMED EMERGENCY PROCEDURES AND THE ODOR SUBSIDED AFTER 5-10 MINUTES. CONDITIONS WERE BOTH BLEED AND PACK VALVES OPEN, BOTH THRUST LEVERS AT IDLE. ENVIRONMENTAL CONDITIONS WERE VERY HUMID. THE CREW DECLARED AN EMERGENCY AND FOLLOWED AOM-1 PROCEEDURES. DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. AFTER LANDING CFR EXAMINED THE AIRCRAFT AND DETERMINED THE AIRCRAFT WAS SAFE AND WAS CLEARED TO TAXI TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN -EM- 72-034 AS REQUIRED COULD NOT DUPLICATE SMELL WHILE TROUBLESHOOTING SMELL NOTICED NR 1 PACK MAKING EXTREMELY LOUD NOISE. TIGHTENED TWO LOOSE AND LEAKING CLAMPS AS REQUIRED. PERFORMED OPS TEST IAW EMB AMM 21-51-00 OPS CHECK GOOD LEAK CHECK GOOD. A FUNCTIONAL CHECK FLIGHT WAS REQUIRED FOR BURNT AIR SMELL IN FORWARD CABIN. THE FCF FOUND WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 20,975 hrs · 17,999 cycles

FOR THE MAINTENANCE INSPECTION THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CRADLE WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT CRADLE IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,407 hrs · 17,548 cycles

ON FLIGHT 3397 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY OF THE CAPTAINS FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 20,356 hrs · 17,510 cycles

ON FLIGHT 3209 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED A BLEED LEAK MESSAGE ON EICAS. THE CREW COMPLETED THE EPC AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LEAK AT SECTION 1, 3, 5 AND 11. REMOVED AND REPLACED THE O-RING IAW AMM 36-11-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DAMAGED (NLG) · airframe 20,171 hrs · 17,361 cycles

FLIGHT 3466, CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED AN "AIR / LDG" INDICATION ON EICAS AS LANDING GEAR WAS SELECTED UP. THE GEAR LEVER WOULD NOT MOVE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. OVERRIDE FUNCTIONED PROPERLY, GEAR WAS DOWN AND LOCKED FOR LANDING. ON LANDING, MESSAGE WENT AWAY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR SLIDING TUBE SEALS IAW AMM 32-20-08. THE OPS & LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,385 hrs · 16,744 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (RT AILERON) · airframe 19,385 hrs · 16,744 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE DAMPER FITTING ON THE RIGHT AILERON TO HAVE SEVERAL GOUGES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,450 hrs · 16,796 cycles

DURING B-INSPECTION, FOUND THE EMERGENCY LIGHT STRIP AT 6L LOCATION HAS WIRE BROKEN OFF AT CONNECTION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT 6L IAW AMM 33-50-12. OPSL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,733 hrs · 14,703 cycles

FOR FLIGHT 2740 WHILE PERFORMING MAINTENANCE FOUND THE LEFT FORWARD WING TO FUSELAGE LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB ON FORWARD LEFT WING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: METERING UNIT — FAILED (NR 2 ENGINE) · airframe 15,511 hrs · 13,790 cycles

ON FLIGHT 3924 DURING CRUISE THE CREW REPORTED AT FLIGHT LEVEL 240 THE NR 2 ENGINE SURGED CONTINUOUSLY FOR APPROXIMATELY 2 MINUTES WHILE ALL OTHER INDICATIONS WERE NORMAL. LARGE FLUCTUATIONS N1, N2 & ITT, IGNITION AB DISPLAYED AS IF IT WAS TRYING TO RELIGHT AFTER 2 MINUTES EVERYTHING STABILIZED AND MAINTAINED NORMAL VALUES. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ROLLS-ROYCE AE3007A FIM TASK 72-00-00-810-804 "THRUST OSCILLATIONS/FLUCTUATIONS" AND REMOVED AND REPLACED ENGINE 2 FUEL PUMP METER UNIT IAW RR MM 73-21-10. THE OPERATIONAL TESTS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,808 hrs · 13,238 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT EXTERIOR FORWARD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE — GOUGED (AILERON) · airframe 14,584 hrs · 13,049 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON HINGE POINT NR 2 TO BE GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON HINGE NR 2 IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 13,118 hrs · 11,874 cycles

ON FLIGHT 3937 SHORTLY AFTER TAKEOFF THE CREW HEARD A LOUD WHINE AND EXPERIENCED A VIBRATION FOLLOWED BY A HOT SMELL COMING FROM THE NR1 PACK. THE CREW SHUT THE NR 1 PACK OFF AND RETURNED TO ORD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR CYCLE MACHINE IAW EMB 145 AMM 21-51-03. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — FAILED (WINDOW) · airframe 8,360 hrs · 7,844 cycles

IN FLIGHT LT DV WINDOW STARTED TO MAKE A VERY LOUD NOISE. PRESS CONTROL WOULD NOT HOLD DESCENDED TO 10,000 FEET. DIVERTED TO SHV DUE TO LACK OF FUEL AT 10,000 FT FOR FLIGHT TO DFW NO OTHER PROBLEMS NOTED LANDED AT SHV. FOUND SEAL TO BE DEFECTIVE ISSUED MEL 21-18 IAW ETN GN-52-001. REMOVED AND REPLACED RIGHT DV WINDOW SEAL IAW EMB 145 AMM 56-11-02 MEL 21-28. RESTORED MEL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — OVERTEMP (NR 1) · airframe 6,726 hrs · 6,406 cycles

"SUP" ON CLIMB OUT OF 10,000 FT NR 1 INLET TURBINE TEMPERATURE WENT TO 920 DEGREES, RETARDED THRUST LEVER TEMPERATURE DROPPED TO 880 DEGREES. AIRCRAFT RETURNED TO ORD. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: TUBE — CRACKED (ENGINE) · airframe 6,057 hrs · 5,839 cycles

ABORTED TAKEOFF, BOTH ENGINES FLUCTUATING EXCESSIVELY AT THRUST SETTING POSITION, ENGINE 2 ITT 110 DEGREE HIGHER THAN ENGINE 1 AT IDLE THRUST. FOUND ENGINE 2 BLEED MANIFOLD TUBE CRACKED. REMOVED AND REPLACED TUBE ASSEMBLY IAW ROLLS ROYCE MAINTENANCE MANUAL 75-00-00-401-801. PERFORMED POWER RUNS ON BOTH ENGINES WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DAMAGED (LT NACELLE)

OIL ACCESS PANEL NR 1 ENGINE IS MISSING, DEPARTED AIRCRAFT INFLIGHT CAUSING A 6-8 INCH TEAR IN NACELLE AND A DENT WITH SEVERAL SCRATCHES. REPLACED ENGINE 1 LOWER COWL AND BLEED AIR DUCT ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — BURNED (COCKPIT MAP)

CAPTAINS MAP LIGHT SMOKES AFTER A FEW MINUTES OF OPERATION AT FULL INTENSITY. REPLACED MAP LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE. (M)