N720FD

Part: FRAME — DAMAGED (ZONE 200) · airframe 45,140 hrs · 26,290 cycles

MAIN DEC CARGO FR 28 S8-20 LT FRAME DAMAGED, BLEND OUT THE DAMAGE IAW SRM 51-73-10, COMPLIED WITH EA 6-5310-163149.

Part: SKIN — DELAMINATED (RT WING) · airframe 45,140 hrs · 26,290 cycles

RIGHT WING OTBD FIXED L/E OTBD TRAILING SECTION DELAMINATED. REMOVED THE ORIGINAL T/E DOUBLER IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201 FIG 215. INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215.

Part: SKIN — DAMAGED (ZONE 100) · airframe 45,140 hrs · 26,290 cycles

LOWER FUSELAGE SKIN FR38, S35-36R FOUND ONE LIGHTNING STRIKE. REMOVED DAMAGE IAW SRM 51-73-10. EXCEED LIMITS IAW SRM 53-10-12/101, DIAGRAM 112, REPAIRED IAW SRM 53-10-12/201 FIG 225.

Part: SKIN — DELAMINATED (RT WING) · airframe 45,140 hrs · 26,290 cycles

RT WING OTBD FIXED T/E UPPER SURFACE DELAMINATED. REMOVED THE DAMAGE T/E SKIN IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201, FIG215 WET INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215 SEALED THE EDGE WITH SEALANT IAW SRM 57-51-12/201, FIG 215. RESTORED THE FINISH IAW SRM 51-75-10.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 45,140 hrs · 26,290 cycles

SKIN DOUBLER AT RT WING TIP UPPER SKIN UNDERNEATH STATIC DISCHARGE DELAMINATION FOUND AROUND THE ORIGINAL DOUBLER AT RT WING TIP UPPER SKIN. UNDERNEATH STATIC DISCHARGE, REPAIRED IAW SRM 57-51-12/201, FIG 215 AND CLASSFIED AS MAJOR IAW GMM6-2-100.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 45,140 hrs · 26,290 cycles

FLOOR SUPPORT CORRODED AND DELAMINATED BETWEEN FR11 TO FR13A. REPLACED FLOOR SUPPORT PER SRM51-40-21.

Part: SPAR — CRACKED (CENTER WING) · airframe 45,140 hrs · 26,290 cycles

ONE CRACK WAS FOUND AT FASTENER HOLE "F" OF LT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.

Part: SPAR — CRACKED (CENTER WING) · airframe 45,140 hrs · 26,290 cycles

ONE CRACK WAS FOUND AT FASTENER HOLE "C" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.

Part: SPAR — CRACKED (CENTER WING) · airframe 45,140 hrs · 26,290 cycles

ONE CRACK WAS FOUND AT FASTENER HOLE "F" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.

Part: FRAME — CRACKED (LT WING) · airframe 45,140 hrs · 26,290 cycles

FOUND A CRACK 8MM IN LENGTH AT LT SIDE FRAME 40 LOWER OTBD RADIUS AREA. REPAIRED PER EA 6-5710-163147

Part: RIB — CRACKED (RT WING) · airframe 45,140 hrs · 26,290 cycles

ONE CRACK ABOUT 10MM IN LENGTH WAS FOUND IN THE AREA OF HOLE 47 OF MLG RIB 5, RT SIDE. COMPLIED WITH EA 6-5710-163-146

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,140 hrs · 26,290 cycles

FOUND A CRACK 6MM IN LENGTH AT RT SIDE FRAME 40 LOWER OTBD RADIUS AREA. COMPLIED WITH EA 6-5710-163147.

Part: LIMITER — FAILED (SLATS) · airframe 45,113 hrs · 26,281 cycles

FAULT ON INITIAL SLAT EXTENSION SLATS STUCK AT 00 FOLLOWED QRH ECAM. TRIED FLAP/SLAT LEVER EXTEND TWO TIMES SAME AS SLAT ONLY STUCK 0. PERFORMED SFCC BITE, CHECKED NR 1 SFCC FAULT CODE 00110 & NR 2 SFCC SLAT JAM LATCHED. PERFORMED FLAP/SLAT OPS CHECKED NORMAL AT THIS TIME. DURING TROUBLESHOOTING FOUND RT SYSTEM SLAT TORQUE LIMITER ACTIVATED AND CURRENTLY INSPECTING ALL RT SLATS SCREWJACK FOR ANY LOCKOUT. ALL RT SCREWJACKS ARE FOUND GOOD AND NOT LOCKED OUT. REPLACED RT SYSTEM TORQUE LIMITER.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 44,908 hrs · 26,197 cycles

FLAPS WOULD NOT RETRACT AFTER TAKE OFF. FLAPS STUCK AT 20 DEGREES. RECYCLE, NO HELP. RETRACTED NORMAL AFTER LANDING. AFTER BLOCK IN, NOTED FLAPS WERE FULLY RETRACTED. INTERROGATED MTP, NO FAULTS. INSPECTED BOTH NR 1 & NR 2 SFCC'S. BOTH SFCC'S REGISTERED A "FLAP JAM" FAULT. RESET BOTH SFCC'S & PERFORMED BITE TEST IAW TSM 27-50-00. ALL TESTS PASSED NO FAULTS NOTED WITH BOTH SYSTEM TORQUE LIMITER INDICATORS. VISUALLY INSPECTED ALL SCREWJACKS ON BOTH LT & RT FLAP ASSY. ALL INSPECTIONS SATISFACTORY. RAN BOTH ENGINES IAW JRH. OPERATED FLAPS IAW AMM 27-50-00-03 AT ALL FLAP SETTINGS SEVERAL TIMES. NO ABNORMALITIES NOTED. NO FURTHER ABNORMALITIES NOTED ON MTP & OVERHEAD FLAP SYSTEM FAULT INDICATORS. ACFT OK FOR SERVICE.

Part: COMPUTER — FAULTED (TE FLAPS) · airframe 44,909 hrs · 26,198 cycles

FLAPS STUCK AT 20 DEG ON TAKEOFF. WOULD NOT MOVE AND RECYCLE WAS NO HELP. LEFT FLAPS DOWN AFTER LANDING AT 20 DEG. NR 1 SFCC FAULTED HIGH SPEED P SWITCH AND NR 2 SFCC FAULTED FLAP JAM. R & R SCREWJACK IAW AMM 27-54-21-04, 27-54-22-04, & 27-54-24-04. CARRIED OUT EXTENSION AND RETRACTION OF FLAP WITH ACFT SYS IAW AMM 27-50-00-3, PG 1 TO 3 MORE THAN TEN TIMES FOUND SATIS SFCC ALL NO FAULT. ATB CONFERENCE WITH MOCC/ DUTY MGR AND CALL UP ACFT FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 44,188 hrs · 25,918 cycles

AFTER TAKE OFF, FLAPS WOULD NOT RETRACT FROM 20 DEG COMPLIED QRH. RETURNED TO LAND IAW INSTRUCTION CARRIED OUT LUBRICATION ON LT FLAP TRACK AND JACKSCREW DRIVE UNITS. SERVICED LT FLAP TRACK TORQUE LIMITER, TEE GEAR BOX, DOWN DRIVE GEAR BOX, BEVEL GEAR AND JACKSCREWS IAW AMM. FWD BEVEL GEAR BOX SERVICED 20 CCM. DOWN GEAR BOX NR 3 AND NR4 SERVICED 30 EA. SCREWJACK 1, 2, 3 & 4 FLUID OVER FLOW WHEN LEVEL PLUG REMOVED, FLUSHED TILL NEW FLUID FLOW OUT. SCREWJACK 5 & 6 DRAINED CCM EA AND SERVICED TILL FULL. WORK IAW AMM 12-13-27-00 AND 12-22-27-00. R & R NR 1 SFCC IAW AMM27-51-18-04. PERFORMED MECHANICAL AND ELECTRICAL CTRL (FLAPS) ADJ/TEST IAW AMM 27-51-00 FOUND ALL TEST PASSED. OPERATED FLAP SEVERAL TIMES WITH BOTH ENG RUNNING, NIL ABNORMALITIES NOTED. VISUAL INSPECTION ON FLAP TORQUE LIMITER FOUND SATISFACTORY. NO FAULT ON BOTH SFCC.

Part: RIB — CRACKED (MLG) · airframe 43,933 hrs · 25,822 cycles

A CRACK WAS FOUND IN THE AREA OF HOLE 47 OF LT SIDE MLG RIB NR 5 AT THE SPOT FACE, THE CRACK LENGTH WAS 33 MM. REPAIRED THE HOLE 47 OF LH MLG RIB 5 IAW EA 6-5750-149032 PART1.

Part: UNKNOWN — SMOKE (LT WING) · airframe 43,022 hrs · 25,489 cycles

ON TAKEOFF, TOWER REPORTED "EXCESSIVE SMOKE TRAILING FROM LT WING." DID AN ATB, NO INDICATION OF SMOKE ON ACFT AND NO ECAM WARNINGS. MX NOTED NO LEAKS FROM LT WING OR ENGINE. CREW STATED NO ABNORMAL HYD QTY OR OIL QTY DECREASE DURING TAKEOFF. NO ABNORMAL ALERTS OR ENGINE INDICATIONS DURING TAKEOFF. CHECKED FUEL PANEL FOR OVERFILL INDICATIONS, NONE NOTED. OPENED NR 1 ENGINE NACELLE, INSPECTED ENGINE FOR LEAKS REF 71-00-00-02-0, NONE NOTED. MOTORED WITH NACELLE OPEN FOR LEAK CHECK, NO LEAKS OF ANY KIND.

Part: BUSHING — FAILED (RT MLG ATTACH) · corrosion level 2 · airframe 42,649 hrs · 25,280 cycles

RT MLG FIB 5 AFT PINTLE FWD BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 RT MLG AFT PINTLE FWD LUG.

Part: LUG — CORRODED (LT MLG) · corrosion level 2 · airframe 42,649 hrs · 25,280 cycles

LT MLG RIB 5 AFT PINTLE FWD LUG BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN. REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 LT MLG RIB 5 AFT PINTLE FWD LUG.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 42,102 hrs · 24,982 cycles

LOWER FWD CARGO COMPT SMOKE ALERT. BOTH BOTTLES HAVE BEEN DISCHARGED. R&R'D BOTH FORWARD LOWER CARGO BAY SMOKE DETECTORS. AS PER A300-600 AMM 26-16-11-04, PERFORMED OPS TEST NORMALLY. OK FOR SERVICE. RAN UP ENGINES FOR 15 MINS, PACKS ON , AND COULD NOT FIND EVIDENCE OF SMOKE IN THE FWD CARGO AREA NOR OTHERS. RAN UP ENGINES AND APU FOR JRH. INSPECTED PNEUMATICS DUCTS AS PER AMM 21-64-32-09, 21-64-34-04-0.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 41,839 hrs · 24,826 cycles

AVIONICS COMPARTMENT FUSELAGE STRUCTURE BELOW WASTE WATER CONNECTION BOX AT FRAME 12 STR 44L HAS CORROSION ON INTERNAL DOUBLE REMOVED LEVEL 1 CORROSION. REPLACED INTERNAL DOUBLE/STIFFENER AT WASTE WATER CONNECTION BOX IAW EA NR 6-5310-135232, DATED 7/23/10.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,839 hrs · 24,826 cycles

MAIN CARGO DECK FRAME 48, SEAT TRACK 4 RT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 RT IAW SRM 51-40-21.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,839 hrs · 24,826 cycles

MAIN CARGO DECK FRAME 50, SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FR 50, SEAT TRACK 4 LT IAW SRM 51-40-21.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,839 hrs · 24,826 cycles

MAIN CARGO DECK FRAME 48 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 LT IAW SRM 51-40-21.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,839 hrs · 24,826 cycles

RT FWD FUSELAGE EXTERNAL SKIN AT FRAME 20 COMMON TO FWD EDGE OF DOOR CUT-OUT 2 EA AREAS OF IMPACT DAMAGE. AREA 1=.500" X .250" X .316" AREA 2= 8.500" X .250" X .365" BETWEEN RT STR 36 AND 40 REMOVED DAMAGED FRAME SECTION IAW REPAIR DWG SR 30-53-001. INSTALLED FRAME SEGMENTS, SPLICE, STRAPS AND FILLER IAW DWG SR 30-53-001. INSTALLED REPAIR DOUBLER IAW SRM 53-13-18, FIG 201, SHEET 1 PG 205-206.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,839 hrs · 24,826 cycles

MAIN CARGO DECK FRAME 49 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART AT FR 49, SEAT TRACK 4 LT IAW SRM 51-40-21.

Part: WEB — CRACKED (CARGO DOOR) · airframe 41,839 hrs · 24,826 cycles

AFT CARGO DOOR INNER SURFACE WEB, FWD OF HINGE FITTING HAS A 2" CRACK. FABRICATED WEB PLATE REPAIR IAW SRM 51-71-30 PG 201-204 INSTALLED WEB PLATE REPAIR IAW SRM 51-71-30, PG 201-204.

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 39,519 hrs · 23,544 cycles

"AVIONICS SMOKE" WARNING ILLUMINATED AT 9000' ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT LIGHTS WOULD NOT CLEAR. FOUND DUCT SMOKE DETECTOR 11WA FAULTY. REMOVED AND REPLACED 11WA DETECTOR .

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 39,519 hrs · 23,544 cycles

"AVIONICS SMOKE" WARNING ILLUMINATED AT 9000 FT ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT LIGHTS WOULD NOT CLEAR. FOUND DUCT SMOKE DETECTOR 11WA FAULTY. REMOVED AND REPLACED 11WA DETECTOR.

Part: SKIN — DAMAGED (K FLAP) · airframe 39,141 hrs · 23,311 cycles

UPON SLAT/ K-FLAP EXTENSION, THE RT/K-FLAP PANEL CONTACTED THE UPPER CLOSE-OUT PANEL RESULTING IN DEFORMATION OF PANEL EDGES AND ATTACH LINK. REPLACED K-FLAP SKIN IAW SRM 51-40-21, REPLACED K-FLAP VANE ASSY IAW AMM 27-87-12-4. REPLACED WING WEB/FORMER IAW SRM 51-40-21. OPS CHECKED GOOD IAW AMM 27-84--00-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,141 hrs · 23,311 cycles

BULK CARGO COMPT FR 69 FLOOR SUPPORT CORRODED LBL20 AND TIE DOWN FITTING MISSING. REMOVED DAMAGED FLOOR CROSS BEAM IAW SRM 51-40-21. RECEIVED NEW FLOOR CROSS BEAM P/N NR A59374322230 BATCH NR 0001436243. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED AND SEALED IAW SRM 51-76-10 AND SRM 51-40-21.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 39,141 hrs · 23,311 cycles

MCD FR79-80 STRING 26L ATTACH WEB CRACKED REMOVED SHEAR PLATE IAW SRM 51-40-21. FABBED SHEAR PLATE IAW MAE TRAVLER T8/731840. LOCATED AND DRILLED IAW SRM 51-40-44, ALODINED IAW SRM 51-20-10. PRIMED IAW SRM 51-20-10. INSTALLED SHEAR PLATE IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,141 hrs · 23,311 cycles

MAIN CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FR 14 AND FR 16 RBL 40 HAS CORROSION IN SEVERAL PLACES ON LOWER SURFACE AROUND FASTENER HOLES REMOVED FLOOR SUPPORT BEAM IAW SRM 51-40-21. FABRICATED NEW FLOOR SUPPORT BEAM IAW SRM 53-12-15 AND SPLICES, LOCATED AND DRILLED IAW SRM 51-12-15. ALODINE AND PRIMED IAW SRM 51-21-10. INSTALLED NEW FLOOR SUPPORT AND SPLICES IAW SRM 53-15-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,141 hrs · 23,311 cycles

AFT CARGO FR 67 FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION LBL 60 TO RBL 60, CROSS BEAM. REMOVED CROSS BEAM IAW SRM 51-73-10 LOCATED AND DRILLED NEW CROSS BEAM IAW SRM 51-40-44. INSTALLED CROSS BEAM IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,141 hrs · 23,311 cycles

MAIN DECK ZONE 221, FORWARD CABIN SEAT TRACK 37.5 LBL HAS STRUCTURAL DAMAGE (HEAVY CORROSION EXFOLIATED) BETWEEN FR 15A THRU FR 19. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,141 hrs · 23,311 cycles

MAIN DECK ZONE 221.FORWARD CABIN SEAT TRACK LBL 18 (Y450) BETWEEN FR 14 THRU FR19 HAS STRUCTURAL DAMAGES (HEAVY CORROSION, EXFOLIATION). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 51-40-21.

Part: RIB — CRACKED (LT IB FLAP) · airframe 39,077 hrs · 23,276 cycles

RIB NR 25 FOUND TO BE CRACKED. REPLACE DAMAGED RIB.

Part: MODULE — MALFUNCTIONED (COCKPIT) · airframe 36,969 hrs · 22,202 cycles

F/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. FACT 13OCT06 06:02 ORD R REPLACED F/O ADC AND CHECK PER MM 34-11-34-4 RVSM STATUS REMAINS THE SAME. R/I 13OCT06 06:03 ORD R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 4045053-914 POS 2 SRL 86090484 TAG 24137A ON MFG 4045053-914 SRL 95051897 TAG 22A340.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 36,969 hrs · 22,202 cycles

ON T/O ROLL F/O'S AIRSPEED INDICATION ON THE PFD DID NOT BREAK UNTIL THE THE CAPTAINS AIRSPEED REACHED 70KTS. (30 KT DIFFERENCE) IN WORK.

Part: MODULE — MALFUNCTIONED (COCKPIT) · airframe 36,969 hrs · 22,202 cycles

PDIS 720 34-11 0002739 13OCT06 ORD CLOSE R 1ST RTO OF 2 F/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT. PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. OFF MFG 4045053-914 POS 2 SRL 86090484 TAG 24137A ON MFG 4045053-914 SRL 95051897, TAG 22A340 FACT 13OCT06 06:02 ORD R REPLACED F/O ADC AND CHECK IAW MM 34-11-34-4 RVSM STATUS REMAINS THE SAME. R/I 13OCT06 06:03 ORD R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 4045053-914 POS 2 SRL 86090484 AG 24137A ON MFG 4045053-914 SRL 95051897 TAG 22A340.

Part: TEE FITTING — LEAKING (HYD SYSTEM) · airframe 36,604 hrs · 22,026 cycles

GREEN SYSTEM OIL QUANTITY (LOST AUTOPILOT NR 1 SPOILERS ETC) CHECKED ECAM, HYDRO SYSTEM ALMOST ZERO, PRESSURE GONE, AFTER MANUALLY LOWERING GEAR, QUANITTY CAME UP SOME. FOUND T-FITTING LEAKING ON STAB JUST O/B OFF PITCH ACT, ON LT SIDE. REMOVED T-FITTING AND LINES TO FITTING, ALL 3 HYDRO SYSTEMS DEPRESSURIZED, PARTS ON ORDER. LAX MTC WILL REPLACE WHEN PART ARRIVES. LAX R SERVICED GREEN SYSTEM HYDRO PER M/M 12-12-00-0.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 35,729 hrs · 21,519 cycles

EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS. COMPLIED WITH EA 6-7830-923658 EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS PART 1.

Part: REPAIR — UNKNOWN (THRUST REVERSER) · airframe 35,729 hrs · 21,519 cycles

THRUST REVERSER-UPPER TORQUE BOX CAP GOUGE REPAIR. COMPLIED WITH EA 6-7830-92361 THRUST REVERSER UPPER TORQUE BOX GOUGE REPAIR.

Part: ACCESS DOOR — GOUGED (ZONE 500) · airframe 35,729 hrs · 21,519 cycles

COMPLY WITH EA 6-7830-92360, THRUST REVERSER NR 1 INBD T/R ACCESS DOOR GOUGE REPAIR. COMPLIED WITH EA 6-7830-92360.

Part: FITTING — DAMAGED (ZONE 100) · airframe 35,729 hrs · 21,519 cycles

COMPLY WITH EA 6-5310-92351, FUSELAGE SB 53-6111, DISCREPANT BASE FITTING HOLES AT FS 45 RT. COMPLIED WITH EA 6-5310-92351B.

Part: FRAME — MISDRILLED (ZONE 100) · airframe 35,729 hrs · 21,519 cycles

COMPLY WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT. COMLIED WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT.

Part: PANEL — CRACKED (RT WING) · airframe 35,729 hrs · 21,519 cycles

RT WING BOTTOM PNL 675 DB CUT-OUT HAS CRACK.

Part: CONNECTOR — DIRTY (THRUST REVERSER) · airframe 35,674 hrs · 21,478 cycles

ENGINE 2 REV UNLK LT COMES ON ABOVE APPROX 35 N1. ABORTED TO AND RETURNED TO RAMP. REMOVED ELECTRICAL CONNECTORS ON RT AND LT CENTER ACTR SEC LOCK SW AND LT AND RT CENTER ACTUATOR STOW AND DEPLOY SWITCHES. CLEANED AND REINSTALLED ELECTRICAL CONNECTORS. RAN ENGINE TO 47 N1, SYSTEM OPS CHECKS NORMAL PER MM 78-30-00-2.