N83428

AERONCA 7AC Serious injury Part 91 — operator not named in the NTSB record

ATA 5320

Part: WEB — CANNING (BS 1323 & 1333)

TNN - HNRC: 837853 (SEQ NR 01063) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX HORIZONTAL WEB BETWEEN BS 1323 AND BS 1333. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED TO THE DAMAGED WEB PER B727 SRM 51-40-2. (X)

ATA 5320

Part: WEB — CANNING (TORQUE BOX)

TNN - HNRC: 837851, 837852 (SEQ NR 01061, 01062) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX VERTICAL WEB AT THE FOLLOWING AREAS: BETWEEN BS 1313 AND BS 1323 AND BETWEEN BS 1223 AND BS 1233. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED ON THE AIRSTAIR LT TORQUE BOX WEB OIL CANNING AREAS PER B727 SRM 51-40-2. (X)

ATA 5320

Part: WEB — CANNING (TORQUE BOX)

TNN - HNRC: 837848, 837849, 837850 (SEQ NR 01058, 01059, 01060) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT TORQUE BOX VERTICAL WEB AT THE FOLLOWING AREAS: BETWEEN BS 1243 AND BS 1253. BETWEEN BS 1283 AND BS 1303. BETWEEN BS 1313 AND BS 1323. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED AT THE AFT AIRSTAIR RT TORQUE BOX WEB OIL CANNING AREAS PER B727 SRM 51-40-2. (X)

ATA 5330

Part: SKIN — CANNING (BS 675)

TNN - HNRC: 817317 (SEQ NR 01040) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING AND DENT WERE FOUND ON FUSELAGE SKIN AT BS 675, BETWEEN S21R AND S22R. THE DAMAGED SKIN 2.5 INCH BY 5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3, FIGURE 3A. (X)

ATA 5313

Part: STRINGER — CORRODED (BS 490)

TNN - HNRC: 817313 (SEQ NR 01036) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STR 28R AT BS 490. THE CORRODED STR S28R FROM BS 480 TO BS 510 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (X)

ATA 5330

Part: SKIN — CORRODED (BS 481/500)

TNN - HNRC: 817298 (SEQ NR 01041) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FUSELAGE SKIN INNER SURFACE AT S28R BETWEEN BS 481 AND BS 500. THE CORRODED SKIN 3 INCHES BY 18 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3 FIG 3A. (X)

ATA 2752

Part: ACTUATOR — LEAKING (LT TE FLAP)

GUM - FLT 921 - AFTER DEPARTURE DEPARTURE SPN CREW DECLARED AN EMERGENCY INTO GUM BASE DUE TO LOSS OF 'A' SYSTEM HYDRAULICS. MAINTENANCE FOUND INBOARD FLAP HYDRAULIC ACTUATOR MOTOR LEAKING (LT W/W) ON REMOVAL FOUND 3 SCREWS ON MOTOR ACCESS PANEL MISSING AND O-RING BLOWN OUT. REMOVED AND REPLACED HYDRAULIC MOTOR PER MM 27-51-52. RESERVICE A, B AND STANDBY SYSTEM TO FULL. RAN FLAPS, NO PRESSURE OR FLUID LOSS NOTED. AIRCRAFT RELEASED FOR SERVICE. (M)

ATA 2917

Part: PRESSURE REG — INOPERATIVE (A HYD SYSTEM)

GUM - FLT 0862 - L/P 7957135 - A-SYSTEM HYDRAULIC PRESSURE IS ZERO. CREW COMPLETED A-SYSTEM CHECK LIST/PROCEDURES. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND AIR PRESSURE REGULATOR AT FAULT. REMOVED AND REPLACED A-SYSTEM AIR REGULATOR PER MM 29-11-12. OPS CHECK NORMAL AND RELEASED AIRCRAFT FOR SERVICE. (X)

ATA 2917

Part: REGULATOR — INOPERATIVE ('A' HYD SYSTEM)

GUM - FL 862 - DURING FLIGHT 'A' HYDRAULIC SYSTEM INDICATION DROPPED TO ZERO ENGINE DRIVEN HYDRAULIC PUMPS SHUT OFF. MAINTENANCE TROUBLESHOOT SYSTEM AND FOUND AIR PRESSURE REGULATOR INOP. REMOVED AND REPLACED AIR PRESSURE REGULATOR AND RESERVICED SYSTEM. PERFORMED OPERATIONAL CHECKS NORMAL. (M)

ATA 2612

Part: FIRE LOOP — CHAFING (NR 2 ENGINE)

TPE - FLT 5922 - DURING TAKEOFF ROLL, NR 1 ENGINE FIRE BELL ACTIVATED INTERMITTENTLY AT 80 KNOTS. ABORTED TAKEOFF BELOW 100 KNOTS. FOUND COWLING CHAFING AGAINST B-LOOP, GROUNDING LOOP AND CAUSING ALARM. REMOVED AND REPLACED DETECTION LOOP. OPS CHECK GOOD PER MM 26-11-01. (X)

ATA 2750

Part: FLAP TRANSMITTER — FAILED (RT TE FLAP)

TPE - FLT 922 - OUTBOARD FLAPS FAILED TO RETRACT BEYOND 15 DEGREES AFTER TAKEOFF. FOUND OUTBOARD RT FLAP POSITION TRANSMITTER AT FAULT. REMOVED AND REPLACED RT OUTBOARD POSITION TRANSMITTER PER MM 27-52-01, ADJUSTED PER MM 27-52-11. OPERATED FLAPS TO 40 DEGREES AND TO STOWED POSITION NUMEROUS TIMES. SYSTEM OPS CHECK GOOD. (X)