N15790

Part: STRINGER — CORRODED (BS 720/740)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH AREA CORROSION WAS FOUND ON STRINGER 27L BETWEEN BS 720F PLUS 6 AND BS 740. THE CORRODED PART OF STRINGER WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-03 FIG 1. (M)

Part: SKIN — CORRODED (BS 448/480)

TNN - DURING D-CHECK INSPECTION ON AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 448 AND BS 480, STRINGER 26R. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)

Part: CHANNEL — CRACKED (BS 1273)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1. 5 INCH LONG CRACK WAS FOUND ON U-CHANNEL ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 CHAPTER 51-40-03 AND 51-30-02. (M)

Part: SPLICE — CORRODED (BS 1010)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH IG CORROSION WAS FOUND ON STRINGER 30 SPLICE ON CARGO COMPARTMENT AT BS 1010. THE DAMAGED PART WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAPTER 53-10-03 FIG 1. (M)

Part: STRINGER — CRACKED (WS 686.5)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 12 AND WS 686.5 WEB ATTACHMENT. THE CRACKED STRINGER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)

Part: STRINGER — CRACKED (WS 629)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 11 AND WS 629 WEB ATTACHMENT. THE CRACKED STIFFENER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)

Part: WEB — CRACKED (BS 1213)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.625 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)

Part: STRINGER — CORRODED (BS 720/740)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BETWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M)

Part: FRAME — CORRODED (BS 219)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 30 SQUARE INCH AREA IG CORROSION WAS FOUND ON FUSELAGE FRAME AT BS 219 AND RT WL 233. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-03. (M)

Part: SEAT TRACK — CORRODED (BS 395)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 4 INCH AREA IG CORROSION WAS FOUND ON PASSENGER FLOOR SEAT TRACK AT BS 395 AND RBL 40. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)

Part: SEAT TRACK — CORRODED (BS 360/380)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360/380 ALONG RBL 18. THE DAMGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)

Part: SEAT TRACK — CORRODED (BS 360/380)

TNN - DURING D-CHECK INSPECTON ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 20 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360 AND 380 ALONG RBL 22 AND RBL 24. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)

Part: FLOORBEAM — CORRODED (BS 328)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 6 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 328 FROM LBL 01 TO RBL 05. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 2. (M)

Part: STIFFENER — CORRODED (RT FRONT SPAR)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)

Part: SPAR CHORD — CORROSION (VERT STAB)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON VERTICAL STABILIZER FRONT SPAR LEFT CHORD AT FS 54. THE CORRODED AREA IS TRIMMED OUT AND REPAIRED PER ECRA 5530-01250. ISSUE A NEW DIP NR CM 556 TO READ AS FOLLOWS WITHIN 11 MONTHS OF INSTALLATION OF THIS REPAIR, CAL WILL DETERMINE IF ADDITIONAL ARE REQUIRED FOR THIS REPAIR FOR SSID ITEM E-4A. (M)

Part: FLOORBEAM — CORRODED (BS 1148)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 1148 FLOORBEAM UPPER CHORD AT LBL 10. THE CORROED PART OF UPPER WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAP 53-10-08 FIG 3. (M)

Part: FRAME — CORRODED (BS 1148)

DURNIG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 1148 FRAME FORWARD FLANGE ON CARGO COMPARTMENT. THE CORRODED PART OF FRAME WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-04 FIG 1. (M)

Part: FRAME — CRACKED (CARGO DOORWAY)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG CRACK WAS FOUND ON C3 DOOR FORWARD FLANGE AT STRINGER 27R ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 1. (M)

Part: SKIN — CORRODED (BS 740)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 720F PLUS 4 AND STRINGER 28L - STRINGER 26R. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5330-02842. (M)

Part: SKIN — CORRODED (BS 720-733)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 27R AND BS 720D PLUS 13. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)

Part: SHEAR TIE — CORRODED (BS 950)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 950E SHEAR TIE ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 14. (M)

Part: SKIN — CRACKED (BS 720-724)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .75 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 28R AND BS 720A PLUS 4. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)

Part: BEAM — CORRODED (HORIZ STAB)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON RIGHT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 190. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)

Part: SKIN — CRACKED (VERT STAB)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RIGHT VERTICAL STABILIZER SKIN WAS FOUND CRACKED JUST AFT TO THE BS 1183 BULKHEAD AT APPROX WL 302. NO ADDITIONAL REWORK OF THE CRACK IS NECESSARY DUE TO WITHIN LIMIT. ISSUE A DIP NR CM558 TO INSPECT THE FIN SKIN CRACK LOCATED AFT OF BS 1183 AT RT WL 302 PER ECRA 5310-03881 AND REPEAT THE INSPECTION EVERY 3000 FLT CYCLES UNTIL PERMANENTLY REPAIRED. (M)

Part: BEAM — CORROSION (HORIZ STAB)

TNN - DURING D-CHECK INSPECTION AT AIR ASIA, A 3 INCH LONG CORROSION WAS FOUND ON LEFT STAB UPPER T/E BEAM AT ELEV STATION 119. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-06 FIG 1. (M)

Part: BEAM — CORROSION (HORIZ STAB)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 155. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)

Part: SEAT TRACK — CORRODED (BS 1130)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON BS 1130 AND LBL 46 SEAT TRACK. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)

Part: WEB — CRACKED (BS 1229)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1229. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)

Part: WEB — CRACK (BS 1275)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1275. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02 FIG 1. (M)

Part: WEB — CRACKED (BS 1238)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES 1. 5 INCH AND .625 INCH LONG CRACKS WERE FOUND ON L-ANGLES WHICH ARE ATTACHED TO RGHT LOWER TORQUE BOX VERTICAL WEB AT BS 1263. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAPTER 51-40-02 AND 51-30-02 FIG 1. (M)

Part: CHANNEL — CRACKED (BS 1273)

TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.25 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAP 51-40-03. (M)

Part: FUSE — FAILED (ROW 20)

INSPECTION FOUND AFT SECTION OF AISLE EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND PINS PULLED OUT OF CONNECTOR AT ROW 20 SEAT LIGHT PIGTAIL. THE CONNECTOR WAS REPINNED. ALSO, FOUND AFT POWER SUPPLY BASE F-2 FUSE BLOWN. THE FUSE WAS REMOVED AND REPLACED. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED.

Part: SKIN — DELAMINATED (RT TE FLAP)

INSPECTION FOUND RT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD AND INBOARD TRAILING EDGE CORNER. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.

Part: SKIN — CORRODED (RT TE MIDFLAP)

INSPECTION FOUND THE RT WING INBOARD MIDFLAP CORRODED AROUND TWO RIVETS ON UPPER SURFACE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.

Part: SKIN — DELAMINATED (NR 7 SPOILER)

INSPECTION FOUND NR 7 SPOILER DELAMINATED AT LOWER OUTBOARD AFT TRAILING EDGE. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.

Part: WIRE — BROKEN (CABIN)

INSPECTION FOUND R-1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT LIGHT ASSEMBLY.

Part: SKIN — DELAMINATED (NR 2 SPOILER)

INSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.

Part: SKIN — CORRODED (NR 5 SPOILER)

INSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.

Part: SKIN — CORRODED (NR 1 SPOILER)

INSPECTION FOUND NR 1 SPOILER CORRODED ALONG OUTBOARD EDGE AND DELAMINATED ON TOP. THE NR 1 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.

Part: SKIN — DELAMINATED (LT TE FLAP)

INSPECTION FOUND LT OUTBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-61-12.

Part: STIFFENER — CORRODED (WS 224)

INSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4.

Part: STIFFENER — CRACKED (BS 234)

INSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.

Part: CHORD — CRACKED (LT WING)

INSPECTION FOUND A .5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2.

Part: SKIN — DELAMINATED (LT AILERON TAB)

INSPECTION FOUND LT INBOARD AILERON TAB TRAILING EDGE SEPARATED IN TWO AREAS. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11.

Part: BRACKET — CORRODED (NR 7 SPOILER)

INSPECTION FOUND NR 7 SPOILER ATTACH SUPPORT BRACKET CORRODED. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (NR 7 SPOILER)

INSPECTION FOUND A 1 INCH CRACK IN NR 7 SPOILER SUPPORT BRACKET SIDE BRACE ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: BEAM — CRACKED (LT WING)

INSPECTION FOUND A .375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6.

Part: BRACKET — CRACKED (RT WING)

INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD ANGLE BRACKET UNDER J-BEAM AT RT WING NR 8 SPOILER. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1090-1130)

INSPECTION FOUND SEAT TRACK CORRODED AT FS 1090 TO 1130, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.

Part: FLOORBEAM — CORRODED (BS 1065)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1065, STRINGER 28R. THE CORROSION WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-40-3 AND 51-10-6.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION FOUND MAIN CABIN EMERGENCY LIGHT AT ROW 8 HAD A WEAK BATTERY. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-50-00.

Part: SKIN — CORRODED (RT ELEVATOR)

INSPECTION FOUND RT ELEVATOR LOWER SKIN CORRODED JUST AFT OF OUTBOARD LEADING EDGE TIP WEIGHT. THE CORRODED SKIN WAS REMOVED. NEW SKIN WAS INSTALLED IAW SRM 51-30-2 AND 51-40-5.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER OUTBOARD CORNER OF CAPTAIN'S WINDSHIELD CUTOUT AND A .125 INCH CRACK WAS FOUND IN SKIN AT LOWER FORWARD CORNER JUST FORWARD OF CAPTAIN'S SLIDING WINDOW. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-30-3.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION FOUND A 3.5 INCH CRACK AT FORWARD LOWER SIDE OF NR 3 CARGO DOOR FRAME BETWEEN STRINGER 25R AND 26R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-4.

Part: TAB — DEBONDED (LT ELEVATOR)

INSPECTION FOUND LT ELEVATOR TAB INBOARD MOST TRAILING EDGE AREA DEBONDED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.

Part: SKIN — CRACKED (NR 8 LE SLAT)

INSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT INNER SKIN AT OUTBOARD STRIKER PLATE AREA. THE OUTBOARD STRIKER SKIN PLATE WAS REPLACED IAW SRM 51-10-1 AND 51-30-2.

Part: FLOOR — CORRODED (LAVATORY)

INSPECTION FOUND LT AFT SINK DRAIN FLOOR AREA CORRODED. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, PAGE 6 AND 51-10-2.

Part: BEAM — CRACKED (RT WING)

INSPECTION FOUND A .375 INCH CRACK IN RT WING J BEAM FORWARD OF SPOILER NR 8 ACTUATOR MOUNT FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-07914.

Part: SKIN — CRACKED (R-1 DOORWAY)

INSPECTION FOUND A 1.9 CRACK IN R-1 DOOR LOWER AFT CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 51-30-21, 51-10-2, 51-40-5, AND ECRA 5307-01141, FIGURE 4.

Part: SKIN — CRACKED (NR 8 LE SLAT)

INSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: HOSE — LEAKING (NR 2 ENGINE)

ON CLIMBOUT, A-SYSTEM WENT TO 0 QUANTITY. FOUND .125 INCH HOLE IN ENGINE DRIVEN PUMP OUTLET HOSE. REPLACED HOSE AND INSPECTED LINE FILTERS AND MAIN SCAVANGE, LEAK CHECK OK.

Part: SPAR CHORD — CORRODED (WS 672-685)

INSPECTION FOUND RT WING FORWARD SPAR LOWER CHORD PLATE CORRODED ON INNER SURFACE BETWEEN FS 672 AND 685. THE CORRODED AREA WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW ECRA 5710-01836.

Part: ACTUATOR — LEAKING (NR 4 LE SLAT)

FLT 959 - GUM - LOST SYSTEM 'A' HYDRAULIC PRESSURE WHILE LOWERING FLAPS, NR 4 LE SLAT DID NOT DEPLOY. COMPLIED WITH EMERGENCY PROCEDURES AS PER FLIGHT MANUAL. REMOVED AND REPLACED NR 4 LE SLAT ACTUATOR. CHECKED BOTH ENGINE CASE DRAIN FILTER MAGNETIC PLUGS, FOUND METAL PARTICLES. REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS DUE TO SUSPECTED FAILURE. PERFORMED LEAK AND OPERATIONAL CHECK ON ENGINE RUN AND ALL INDICATIONS NORMAL. (M)

Part: TRANSMITTER — FAILED (NR 2 ENGINE)

FLT 951 - GUM - AFTER TAKEOFF, NR 2 OIL PRESSURE WENT TO ZERO. SHORTLY THEREAFTER PRESSURE RETURNED TO NORMAL. GUM MAINTENANCE ADVISED FLIGHT CREW TO RETURN TO GUM DUE TO NO MAINTENANCE IN ROR AND YAP. REMOVED AND REPLACED NR 2 OIL PRESSURE TRANSMITTER PER MM 79-32-1. ALSO, REPLACED NR 2 QIL PRESSURE TRANSMITTER PER MM 79-32-1. ALSO, REPLACED NR 2 QIL PRESSURE GAUGE AS PRECAUTIONARY. LEAK CHECK AND OPERATIONAL CHECK NORMAL ON ENGINE RUN. (M)

Part: FRAME — CORRODED (C2 CARGO DOOR)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON C3 CARGO DOOR LOWER FRAME FORMED, SECTION. THE CORRODED FORMED SECTION WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806982 (SEQ NR 01086). (M)

Part: SKIN — MISDRILLED (BS 530)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO RIVET SPACING WAS FOUND BELOW THE SPECIFIED LIMIT ON BS 530, STRINGER 27L THE DAMAGED SKIN WAS REPAIRED PER B727 SRM 53-30-3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806835. (SEQ NR 01084) (M)

Part: SKIN — CORRODED (BS 950)

DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON C2 CARGO DOOR LOWER CUTOUT SKIN INTERIOR DOUBLER AT BS 950F. THE CORRODED SKIN WAS TREATED AND REPAIRED PER EC/RA NR 5330-02403. REF: HANGAR NON ROUTINE ITEM CARD NR 806983 (SEQ NR 01092) (M)

Part: STRINGER — CORRODED (BS 950-1010)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON STRINGER 27R BETWEEN BS 950E AND 1010. THE CORRODED STRINGER WAS TREATED AND REPAIRED PER EC/RA 5310-03275, A DIP HAS BEEN ISSUED TO REPLACE THE REPAIRED STRINGER S-27R AT NEXT D-CHECK. REF: HANGAR NON ROUTINE REPAIR ITEM CRD NR 806984 (SEQ NR 01093). (M)

Part: BEAM — CORRODED (HORIZ STAB TE)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER TE BEAM AT ELEV STATION 17. THE CORRODED TRAILING EDGE BEAM WAS TREATED AND REPAIRED PE B727 SRM 51-10-6 AND 55-10-6. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 806962, (SEQ NR 03020). (M)

Part: INBOARD WEB — OIL CANNING (BS 1213-1223)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR LEFT TORQUE BOX INBOARD WEB AT THE FOLLOWING AREAS; BETWEEN BS 1213 AND 1223, BETWEEN BS 1223 AND 1233. THE DAMAGED WEB WAS INSTALLED REINFORCEMENT STIFFENER ANGLES PER B727 SRM 51-40-2. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 806374 AND 806375, (SEQ NR 02070 AND 02071). (M)

Part: INBOARD WEB — CRACKED (BS 1218)

TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON RIGHT TORQUE BOX INBOARD WEB LIGHTENING HOLE CUTOUT AT BS 1218. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 806372 (SEQ NR 02068). (M)

Part: AOA SENSOR — FAILED (E/E COMPT)

GUM - FLT 873 - STICK SHAKER CAME ON RIGHT AFTER TAKEOFF, FLAPS 15 FEET, 5 FEET, 2 FEET, STAYED ON CONSTANTLY. IT CAME ON AFTER 2 FOOT FLAPS FOR EXTENSION ON LANDING. MAINTENANCE FOUND WIRE LOSE ON NLG GROUND/AIR SENSE SWITCH. MECHANIC SECURED WIRE AND REPLACED ANGLE OF ATTACK SENSOR AS PRECAUTIONARY IAW 727-200 MM 34-18-51. (X)

Part: ACTUATOR — BROKEN (NR 1 LE SLAT)

FLT NR 917 - GUM - ON CLIMB-OUT, LOST A-SYSTEM HYDRAULICS, CREW SHUT DOWN SYSTEM A-PUMPS PRIOR TO COMPLETE HYDRAULIC FLUID LOSS. AIRCRAFT DIVERTED BACK TO GUAM. MAINTENANCE FOUND NR 1 LED SLAT ACTUATOR LEAKING FLUID AND REPLACED ACTUATOR PER MM 27-81-04. SYSTEM SERVICE BACK TO NORMAL AND OPERATION CHECK GOOD. AIRCRAFT RETURN BACK TO SERVICE. (M)