N846AA

Part: LIGHT — INOPERATIVE (R1 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT OVERHEAD AFT STAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT OVERHEAD AFT STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIRS)

DFW DURING OVERNIGHT MAINTENANCE AFT AIRSTAIRS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SKIN DENTED STATION 312, STRINGER L4. CUT OUT DAMAGE. INSTALLED REPAIR DOUBLER AS PER SRM 53-30-3 PART 1 FIG 5 AT STATION 312 STRINGER 4 LEFT. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN SKIN AT UPPER HINGE FORWARD ENTRY DOOR, NOT HFEC. CUT AND REMOVED DAMAGED SECTION OF SKIN FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED SB 727-53-0198 FIG 4. (M)

Part: FRAME — DENTED (FUSELAGE)

TUL - FOUND BELLFRAME DENTED STATION 950B STRINGER 26L. REMOVED DAMAGED SECTION OF BELLFRAME. INSTALLED DOUBLER PER SRM 53-10-4 PAGE 1. (M)

Part: WEB — CRACKED (TORQUE BOX)

TUL - FOUND CRACKS IN LOWER TORQUE BOX VERTICAL WEB LEFT STATION 1213 RIGHT STATION 1223 RIGHT STATION 1243. STOP DRILLED CRACKS AND INSTALLED DOUBLERS AARD 51-20-01-3 SRM 51-40-02 FIG 1A. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: GEAR ACCY UNIT — MALFUNCTIONED (LT MLG)

ORD - FLT 1021 - AFTER TAKEOFF UPON GEAR RETRACTION, RED LEFT GEAR WARNING LIGHT REMAINED ILLUMINATED. ALL OTHER INDICATIONS AND FUNCTIONS NORMAL. JACKED AIRCRAFT, OPERATED GEAR SEVERAL TIMES. UNABLE TO DUPLICATE PROBLEM. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: UNKNOWN

TUL - HFEC INDICATES A 1 INCH CRACK ON RT MLG WW PRESS DECK BEAD AT RT OUTBOARD AFT CORNER AT BS 947 ABOVE PULLEY. INSTALLED PRESSURE DECK REPAIR PER ECO 11697. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - ONE CRACK AT ACCESS PANEL CUT OUT RT SIDE OF VERTICLE BELOW FLAG. INSTALLED FLUSH DOUBLER REPAIR PER SRM CH 54-10-3 PAGE 18, FIG 4 SHT 5. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - THREE CRACKS AT ACCESS PANEL CUT OUT LEFT SIDE OF VERTICLE, BELOW FLAG. INSTALLED THREE DOUBLERS PER SRM CHAPTER 54-10-3 PAGE 18, FIG 4, SHEET 5. (M)

Part: SENSOR — FAILED (RT MLG)

IAH - FLT 1798 - AFTER TAKEOFF IAH, WHILE RAISING GEAR HANDLE THE RIGHT MAIN GEAR RED LIGHT ILLUMINATED. RECYCLED GEAR AND STILL HAD GEAR RED LIGHT ILLUMINATED. LOWERED GEAR AND GOT SAFE INDICATION. RETURNED AND LANDED IAH WITHOUT INCIDENT. PERFORMED SPECIAL FERRY FLIGHT TO DFW WITH GEAR DOWN FOR FURTHER EVALUATION. REPLACED RIGHT MAIN LANDING GEAR UPLOCK SENSOR. SWUNG GEAR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — LEAKING (NR 3 ENGINE)

ORD - FLT 0792 - AFTER TAKEOFF ORD DURING CLIMB-OUT, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NR 3 ENGINE 8TH STAGE ANTI-ICE AND AIR CONDITIONING SUPPLY DUCT. ALSO, REPLACED STRUT OVERHEAT LOOP AND HP SOV FLEX LINE. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS NOTED. SYSTEM LEAK AND GROUND CHECKED, NORMAL OPERATION. (X)

Part: ACCESSORY UNIT — DEFECTIVE (E/E COMPT)

DFW - FLT 1187 - AFTER TAKEOFF BWI WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CRACKED (BS 328)

TUL - FOUND CRACK ON FRAME ATTACH ANGLE. DAMAGED AREA REMOVED, INSTALLED NEW ANGLE IAW SRM 53-10-4 PG 58-60. (M)

Part: FRAME — CRACKED (BS 970)

TUL - FOUND BELL FRAME AT STATION 970 CRACKED AT SIDE PANEL ATTACH HOLE BETWEEN STRINGER 26 AND 27 LEFT (HFEC). STOPPED DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3. (M)

Part: ANGLE — CRACKED (BS 318)

TUL - FOUND CRACK ON FRAME ATTACH ANGLE. DAMAGED AREA REMOVED, INSTALLED NEW ANGLE IAW SRM 53-10-4 PG 58-60. (M)

Part: SKIN — CORRODED (BS 486)

TUL - FOUND SKIN CORRODED THROUGH AT STRINGER 27L, STATION 486. REMOVED SECTION OF CORRODED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - FOUND STRINGER CRACKED AT END, FORWARD OF STATION 720C. REPAIRED STRINGER PER SRM 53-10-3 PAGE 413. (M)

Part: FRAME — MIS-DRILLED (BS 1130)

TUL - MIS-DRILLED HOLE IN BELT FRAME. REPAIRED BELT FRAME PER SRM 53-10-4 PAGE 1. (M)