N430AA

Part: LINK — BROKEN (NLG DOOR)

LGA INFLIGHT T707/20APR DURING GEAR RETRACTION FELT HEAVY VIBRATION IN THE NOSE GEAR AREA. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOOR LINK LATCH BROKEN. REPLACED LEFT NOSE GEAR DOOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: COVER — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY EXIT LIGHT LENS COVER IS MISSING ON SEAT 20D. RELAMPED AND REPLACED LENS CAP ON EMERGENCY EXIT LIGHT AT ROW 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MAKING METAL (RIGHT)

DFW INFLIGHT T563/23JUL - ON CLIMB-OUT APPROXIMATELY 1400 FEET RIGHT ENGINE LOW OIL PRESSURE LIGHT ON. RIGHT OIL QUANTITY NORMAL. RIGHT OIL TEMPERATURE DECREASING. REDUCED POWER ON RIGHT ENGINE TO IDLE. APROXIMATELY 5 MINUTES LATER INCREASED POWER ON RIGHT ENGINE AND VIBRATION BEGAN. SHUTDOWN RIGHT ENGINE. FOUND OIL PRESSURE OUT OF LIMITS AND METAL IN OIL. REPLACED RIGHT HAND ENGINE.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

TUL - EMERGENCY ESCAPE LIGHTS IN OVERHEAD SWITCH PANEL INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY ESCAPE LIGHTS IN OVERHEAD SWITCH PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

AUS - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT 21D AND AFT INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND 1 INCH DENT ON FUSELAGE SKIN STATION 68 RIGHT SIDE OF A/C FORWARD OF LONGERON 21. REPAIRED PER SRM 53-01 F2 SHEET 3 AARD 53-30-00-02 INTERNAL 2 ROW DOUBLER. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP MEMBRANE BETWEEN STATIN 1079-1098 HAS CORROSION. REMOVED AND REPLACED CORRODED CUSP MEMBRANE BETWEEN STATION 1079-1098 PER SRM 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP MEMBRANE BETWEEN STATIN 1022-1079 CORRODED BOTTOM SIDE AROUND LIGHTENING HOLE. REMOVED AND REPLACED CORRODED CUSP MEMBRANE BETWEEN STATION 1022-1079 PER SRM 53-00-00-02. (M)

Part: FRAME — DENTED (FUSELAGE)

TUL - FOUND FRAME DENTED STATION 408 ABOVE LONGERON 27L. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-01-17. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 2 CORRODED STATION 1199-1203. CORRODED SECTION OF NR 2 TRACK REMOVED NEW SECTION OF SEAT TRACK INSTALLED STATION 1033-1309 PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 1 SEAT TRACK STATION 1025. CORRODED SECTION OF NR 1 SEAT TRACK REMOVED. NEW SEAT TRACK INSTALLED STATION 936-1033 PER SRM 53-05. (M)

Part: CARGO TRACK — GOUGED (FUSELAGE)

TUL - FOUND MID CARGO TIE DOWN TRACK GOUGED, STATION 598. REMOVED AND REPLACED WITH NEW CARGO TIE DOWN TRACK SRM 51-01 FIG 2-4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP, STATION 522-541. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-10-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP STATION 678. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP, STATION 619-627. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK. REPLACED SEAT TRACK NR 1 FROM STATION 1174 TO 1309 PER SRM 51-10-3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND INTERIM REPAIR ON CUSP CRACK PROPAGATING FROM LIGHTENING HOLE BETWEEN STATION 1193-1212 OUTBOARD OF NR 1 SEAT TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00. (M)

Part: WEB — DENTED (FUSELAGE)

TUL - FOUND METAL FIR BOARD/CUSP SHEET HAS DENT STATION 200-205, JUST INBOARD OF NR 2 SEAT TRACK. INSTALLED DOUBLER AARD 53-00-00-02. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LONGERON 4 LT STATION 160. CUT OUT CRACKED, INSTALLED NEW LONGERON SECTION AND SPLICE PER SRM 53-03 FIG 18, SAT 1, 4, 5, 6. (M)

Part: FRAME — GOUGED (FUSELAGE)

TUL - FOUND LOWER SIDE OF BELT FRAME HAS 2 GOUGES STATION 465 BELOW LONGERON 6 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-14. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - FOUND WORN SPOT ON BELL FRAME LONGERON 6L STATION 693. INSTALLED DOBLER PER AARD 53-10-00-14. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - FOUND WORN AREA ON BOTTOM SIDE OF BELT FRAME STATION 522 BELOW LONGERON 6 RIGHT. INSTALLED J ANGLE PER AARD 53-10-00-14. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 3 SEAT TRACK CORRODED STATION 1169-1210. FOUND CORROSION BLEND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK SRM 51-01. (M)

Part: DOOR — OUT OF ADJ (NLG)

DFW-GRU - FLT 1663 - EN ROUTE SHORTLY AFTER TAKEOFF DETECTED A LOUD VIBRATION AT FORWARD PART OF AIRFRAME. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. READJUSTED NOSE LANDING GEAR DOOR. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — LOOSE (LT TR UNIT)

DFW - FLT 1873 - ON TAXI OUT FROM GATE, SMOKE AND FUMES NOTED IN PASSENGER CABIN WITH HYDRAULIC QTY DECREASING. PASSENGERS AND CREW EVACUATED WITHOUT INCIDENT. RETORQUED B-NUT AT LEFT THRUST REVERSER HYDRAULIC VALVE FITTING. PERFORMED AIR CONDITIONING PACK BURNOUT PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CARBON SEAL — FAILED (LT ENGINE)

SMF - FLT 752 - DURING CLIMB-OUT, RIGHT ENGINE EXPERIENCED OIL QTY LOSS, RISE IN OIL TEMP, AND LOSS OF OIL PRESSURE. ENG WAS SECURED, THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SMF. A/C LANDED SMF WITHOUT FURTHER INCIDENT. RIGHT ENGINE WAS REPLACED DUE TO OIL LOSS AND HIGH OIL TEMPERATURE. REQUIRED LEAK, OPERATIONAL, TRIM CHECKS WERE ACCOMPLISHED WITH NO ABNORMALITIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. THE NR 6 CARBON SEAL WAS BROKEN IN PIECES AND FOUND IN THE BOTTOM OF THE NR 6 BEARING HOUSING. THE PIECES PARTIALLY BLOCKED THE NR 6 SCAVENGE PUMP INLET SCREEN. THE BROKEN NUMBER 6 CARBON SEAL AND SCAVENGE PUMP INLET SCREEN BLOCKAGE CAUSED THE LOSS OF OIL. (M)

Part: BEAM — CORRODED (BS 1155-1212)

TUL - FOUND CORROSION UNDER STAINLESS DOUBLER ON AFT CARGO ENTRYWAY DOOR BEAM. REPLACED ENTIRE AFT CARGO LOWER DOOR BEAM FLOOR STATION 1117 TO 1250 ALONG LONGERON 28 RT. (M)