N801FD

Part: GIRT BAR — DETACHED (R1 DOOR SLIDE) · airframe 41,631 hrs · 14,685 cycles

R1 DOOR WILL NOT ARM. FOUND GIRT BAR DETACHED NOT ALLOWING PROPER OPERATION REINSTALLED GIRT BAR IAW MM 25-61-22-04-01.

Part: POWER SUPPLY — MALFUNCTIONED (DOOR SLIDE) · airframe 41,373 hrs · 14,549 cycles

COULD NOT GET RT SLIDE TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BOTH BATTERIES ON ASPSU IAW AMM 52-73-18-04, BITE TEST OK. R1 DOOR SLIDE ECAM INDICATION OPS NORM. REMOVED PLACARD.

Part: WARNING MESSAGE — INTERMITTENT (DOOR SLIDE) · airframe 41,351 hrs · 14,537 cycles

BOTH ECAM SLIDE INDICATIONS ARE INTERMITTENT. RESET EMERGENCY SLIDE SYSTEM AND PERFORMED OPS CHECK SEVERAL TIMES IAW AMM 52-73-13-04. OPS CHECKED GOOD.

Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 41,194 hrs · 14,453 cycles

INFORMATION ONLY, REJECTED T/O 9L, PARKING BRAKE SET INDICATION, WE NEVER SET PARKING BRAKE. ONCE WE STARTED TAXI TO RUNWAY, CHECKED HANDLE DOWN POSITION, WE HAD NORMAL CONFIGURATION ON BELOW THE LINE CHECK LIST, PERFORMED RTO, SPEED BELOW 60 KTS, CLEARED RUNWAY COMPLETED RTO AND AFTER LANDING CHECK LIST, NO BRAKE COOLING REQUIRED TALKED TO MAINTENANCE, NO FURTHER PROBLEMS. INFO NOTED, CYCLED PARKING BRAKE SEVERAL TIMES, PARKING BRAKE INDICATIONS OPERATED NORMALLY, REF AMM 32-45-00, ACFT OK FOR SERVICE.

Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 40,726 hrs · 14,164 cycles

DUAL SLATS FAULT 1 & 2 ON APPROACH, 3000' MSL 170 KTS, FLAPS STUCK AT 15'. R & R SLAT COMMAND SENSOR UNIT 51CV IAW AMM 27-51-17-04. R & R BOTH SFCC'S IAW AMM 27-51-18-04. FLAP & SLATS OPERATION TESTED GOOD IAW AMM 27-81-00-05. ALSO REF TSM 27-80-07.

Part: STRINGER — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 39,023 hrs · 13,058 cycles

STRINGER 44L AT FRAMES 41 - 42 IN A/C BAY CORRODED. BLENED IAW SRM 51-74-10, PERFORMED DVI TO VERIFY NO CORROSION FOUND IAW NTM 51-70-00, PERFORMED ROTO TEST TO OPEN HOLES TO VERIFY NO CRACKS FOUND IAW NTM 51-10-01. FABRICATED THE REPAIR PARTS IAW SRM 53-10-14-201 PARA 4.C FIG 203 SHEET2. INSTALLED THE REPAIR IAW SRM 53-10-14-201 PARA 4. C FIG 203 SHEET 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRINGER — CORRODED (FRAMES 41-42) · airframe 39,023 hrs · 13,058 cycles

STRINGER 44L AT FRAMES 41 - 42 CORRODED.

Part: STRINGER — CORRODED (FRAMES 41-42) · airframe 39,023 hrs · 13,058 cycles

STRINGER 45L AT FRAMES 41 - 42 CORRODED. REPAIRED IAW SRM 51-74-10 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: COMPUTER — FAILED (FLAP SYSTEM) · airframe 38,848 hrs · 12,960 cycles

DURING FLAP EXTENSION, EXPERIENCED FLAP SYS 1 & 2 FAULT ILLUMINATION, FLAPS FAILED TO EXTEND. PERFORMED QRH PROCEDURE. WHEN FLAP HANDLE MOVED TO 40 DEGREES, FLAPS EXTENDED TO 40. BITE CHECKED BOTH SFCC'S & BOTH PASSED. RESET & TESTED EACH SEGMENT OF BOTH SFCC'S. NR 1 SFCC FAULTS BOTH THE LT & RT WTB'S. NR 2 SFCC FAULTS BOTH THE LT & RT WTB'S. NORMAL CONFIGURATION FOR LANDING. ACFT LANDED NORMAL WITH SLAT & FLAP DEPLOYMENT. R & R NR 2 SFCC & NR 1 SFCC IAW MM 27-51-18-04. OPERATED FLAPS & SLATS WITH NO FAULTS. OK FOR SERVICE.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 37,339 hrs · 12,011 cycles

INADVERTENT OPENING OF R1 CABIN DOOR STARTED INITIATION OF SLIDE DEPLOYMENT. INSTALLED R1 ESCAPE SLIDE IAW MM 25-61-20-02, AND ADJUSTMENT AND TEST IAW MM 25-61-20-05-01. OP'S CHECKED NORMAL, INSTALLED R1 PNEUMATIC EMERGENCY DOOR ASSIST BOTTLE ARMING LEVER, IAW MM 52-10-00-03. ACFT OK FOR SERVICE.

Part: FLOOR PANEL — DENTED (UPPER CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252PH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 21-B53270276015. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.

Part: FLOOR PANEL — DENTED (UPPER CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242EK DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 85-R532B1231003. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,832 hrs · 11,716 cycles

FORWARD CARGO COMPARTMENT BILGE AREA OF S45R, SKIN CORRODED BETWEEN FR 38.2 AND FR 39. CUT OUT THE DAMAGED AREA. REPAIRED WITH DOUBLER AND FASTENERS IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW G.M.M. 6-2-100.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

CARGO COMPARTMENT 161GF FLOOR PANEL BROKEN. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 48 A532799630. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.

Part: SKIN — CORRODED (LT WING) · airframe 36,832 hrs · 11,716 cycles

LEFT WING TOP SKIN CORRODED AT REAR SPAR RIB 4. ACCOMPLISHED REPAIR IAW EA 6-5730-149020. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

CARGO COMPARTMENT 162HF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 47 A532799620. REPAIR CLASSIFIED AS MINOR IAW G.M.M. 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

BULK CARGO COMPARTMENT 162AF FLOOR PANEL UPPER SKIN DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 51 A532799660. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.

Part: FLOOR PANEL — DENTED (UPPER CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252UH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 34-R532B1177004. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.

Part: FLOOR PANEL — DENTED (UPPER CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252GF DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW PANEL IAW SRM 53-10-20, AND DRAWING 09-R532B1175009. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

CARGO COMPARTMENT 161BF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 50 A532799650. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-30-04.

Part: FLOOR PANEL — DENTED (UPPER CARGO BAY) · airframe 36,832 hrs · 11,716 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UJ DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 27-R532B1231001. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 36,473 hrs · 11,516 cycles

DURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY UNIT 29WL IAW MM 33-51-14-04. ALSO, R & R EMERGENCY LIGHT BATTERY 29WL IAW MM 33-51-14-04. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE.

Part: LIMITER — FAILED (FLAP/SLATS) · airframe 35,897 hrs · 11,211 cycles

SLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND R TORQUE LIMITER IAW MM 27-84-12-04. ALSO SERVICED LT WING SLATS, SCREW JACKS AND GEAR BOXES IAW MM 12-13-27-00. PERFORMED OPS CHECK IAW MM 27-84-00. ALL TEST PASSED. (CLOSED)

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,925 hrs · 10,163 cycles

CORROSION WAS FOUND ON MANHOLE FITTING AT FR 23-24. REPAIR EVALUATED AND FOUND WITH CORROSION AT FWD MANHOLE INTEGRAL FITTING. MANHOLE REPLACEMENT PLUS REPAIR WERE ACCOMPLISHED IAW EA 6-5310-131032.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 33,925 hrs · 10,163 cycles

RIGHT WING FLAP OUTBOARD UPPER SKIN SURFACE WITH DEEP DENT AT FRICTION PLATE SEATING AREA BETWEEN RIB 2.5 AND RIB 3. REPAIRED IAW E.A. 6-5710-131025.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 33,925 hrs · 10,163 cycles

AFT CARGO COMPT - TRACK ROLLER NR 4 BTW FR55/58 AND 63 CRACKED AND WITH CORROSION AT DRAIN AREA. THE TRACK WAS REPAIRED IAW SRM 53-10-15 FIG 202.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 33,925 hrs · 10,163 cycles

AFT CARGO COMPT- FR60 CROSSBEAM WITH CORROSION BTW Y1300 AND Y1390. BEAM REPAIRED IAW SRM 53-10-15 FIG 207.

Part: ARM — CORRODED (ZONE 300) · corrosion level 2 · airframe 33,925 hrs · 10,163 cycles

VERTICAL STABILIZER RUDDER HINGE ARM NR 4 FOUND WITH CORROSION AT VERTICAL STABILIZER CONNECTION. RUDDER HINGE ARM REPAIRED AS PER EA 6-5510-131027.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 33,925 hrs · 10,163 cycles

RIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 33,925 hrs · 10,163 cycles

PREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR76-77 AT ATGR 23LH-25LH, NEXT TO AFT DOOR LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED AS PER EA 6-5330-131021.

Part: TRACK — MISREPAIRED (ZONE 100) · airframe 33,925 hrs · 10,163 cycles

PREVIOUS REPAIR FOUND LOCATED AT ROLLER TRACK LT, ON FWD CARGO COMPT BTW FR38- 38.1 AT STA Y140. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IAW SRM 53-10-15 FIG203.

Part: FLOORBEAM — MISREPAIRED (ZONE 100) · airframe 33,925 hrs · 10,163 cycles

PREVIOUS REPAIR FOUND LOCATED ON FLOORBEAM RT BTW FR11A-12A AT STA Y-953. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IAW EA 6-5310-131022.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 33,925 hrs · 10,163 cycles

PREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR25-26/32 AT STGR 41LH. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED AS PER FEDEX EA 6-5310-131031.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,925 hrs · 10,163 cycles

CABIN - FLOOR TRACK WITH CORROSION BTW FRAMES 12A AND 13 AT Y730. TRACK WAS REPLACED AS PER SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,925 hrs · 10,163 cycles

FWD CABIN SEAT TRACK AT Y-450 WITH CORROSION BTW FR14B AND FR19. TRACK WAS REPLACED AS PER SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,925 hrs · 10,163 cycles

FWD CABIN SEAT TRACK Y-953 CORRODED BTW FRAMES 15B AND 19. THE TRACK WAS REPLACED AS PER SRM 51-72-10.

Part: TIRE — FAILED (MLG) · airframe 32,882 hrs · 9,578 cycles

ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER TAKEOFF. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD.

Part: TIRE — FAILED (MLG) · airframe 32,882 hrs · 9,578 cycles

ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER T/O. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD.

Part: PROXIMITY SENSOR — FAILED (ZONE 700) · airframe 31,542 hrs · 8,757 cycles

ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FUTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00 -4. WHILE REPLACING 8GA PROX DETECTOR FOUND 12GA PROX DETECTOR ADJUSTMENT NOT WITHIN MM LIMITS. ADJUSTED SAME AS PER MM 32-00-00-4. SWUNG GEAR ON BOTH SYS 1 AND SYS 2 ALL GEARS AND DOORS WORKED NORMAL ON BOTH SYSTEM.

Part: PROXIMITY SENSOR — FAILED (ZONE 700) · airframe 31,542 hrs · 8,757 cycles

ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FURTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00-4. WHILE REPLACING 8GA PROX DETECTOR FOUND 12GA PROX DETECTOR ADJUSTMENT NOT WITHIN MM LIMITS. ADJUSTED SAME AS PER MM 32-00-00-4. SWUNG GEAR ON BOTH SYS 1 AND SYS 2 ALL GEARS AND DOORS WORKED NORMAL ON BOTH SYSTEM.

Part: ATTACH FITTING — CORRODED · airframe 31,208 hrs · 8,556 cycles

RT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG RT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS REF: RAS/BAC/1004683/2007 ISSUE A.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 31,208 hrs · 8,556 cycles

LT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG LT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS/BAC/1004683/2007 ISSUE A.

Part: SKIN — DENTED (RT WING) · airframe 31,208 hrs · 8,556 cycles

THS-FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — DENTED (ZONE 300) · airframe 31,208 hrs · 8,556 cycles

THS - FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

FWD CARGO COMPARTMENT DOOR AFT FRAME FOUND WORN AT FRAME 25 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

AIR COND STR 44 LT OF FR 39 TO 40 WITH CORROSION P/N A53811373200 STRINGER REPAIRED IAW FEDEX EA 6-5310-106705. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MAJOR.

Part: FAIRING — CRACKED (WING TO FUSE) · airframe 31,208 hrs · 8,556 cycles

FAIRING PANEL TO PYLON COWL OF RT CORE WITH 2 CRACKS REPAIRED THE CRACKS IAW SRM 54-56-10 CONFIG. 2 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

FUSELAGE, FWD CARGO COMP'T DOOR FWD FRAME WORN FR 20 STR 39. REPAIRED PER FEDEX EA NR 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — CORRODED (LT WING) · airframe 31,208 hrs · 8,556 cycles

LT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

FUSELAGE FRAME 20 STRG 37 FWD CARGO COMP´T DOOR FWD FRAME FOUND WORN REPAIRED PER FEDEX EA NR 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — CORRODED (CENTER WING) · airframe 31,208 hrs · 8,556 cycles

CORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10-08, 51-10-01 AND 51-10-04. REPAIRED PER SRM 57-10-12 PG. 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: BOLT — CRACKED (NLG DOOR ACT) · airframe 31,208 hrs · 8,556 cycles

FOUND CRACK AT NLG DOOR ACTUATOR BOLT. REPLACE BOLT PER EO 6-5340-7-5001 A4 PART 5 REPLACED BOLT IAW EO 6-5340-7-5001A4 PART 5. PERFORMED TEST CARRY OUT A DOOR GROUND OPENING AND CLOSING TEST IAW AMM 32-31-00.

Part: PANEL — CRACKED (NR 1 PYLON) · airframe 31,208 hrs · 8,556 cycles

(N0535) CRACK FOUND ON NR 1 PYLON AFT FAIRING. REPAIR ON GOING AS SRM. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. FAIRING TO PYLON COWL OF RT CORE W/ TWO CRACKS REPAIRED IAW SRM 54-56-10 CONFIG 2 FIG 201.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

FWD CARGO COMPARTMENT DOOR FWD FRAME WORN ON FRAME 20 STR 42 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR "

Part: FRAME — MISINSTALLED (FUSELAGE) · airframe 31,208 hrs · 8,556 cycles

FUSELAGE RIVETS BADLY INSTALLED AT PNL 40 LT FRAME 3 REPAIRED PER SRM 53-11-12 PG 217 AND 218 FIG 203 (SHT 1 AND 2). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: STRUT — DAMAGED (RT MLG DOOR) · airframe 31,208 hrs · 8,556 cycles

RT MLG DOOR STRUT W/SKIN SURFACE DAMAGED REPAIRED PER FEDEX EA NR 6-5280-106709 AND SRM 51-77-12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 31,208 hrs · 8,556 cycles

FUSELAGE LOWER FWD LOBE, REPAIR AT LT SIDE OF FUSELAGE BETWEEN FRAME 25 & 26/32 BETWEEN STR. 42 & 43 REPAIRED PER SRM 53-10-12 FIG. 229 (SHEET 1) PG. 406 TO 410 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR "

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 31,208 hrs · 8,556 cycles

CRACK FOUND ON NR 1 PYLON LOWER FAIRING. REPAIR ON GOING AS SRM REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: SKIN — CRACKED (NR 2 INLET) · airframe 30,104 hrs · 7,865 cycles

ENGINE NR 2 - INLET COWL LIP SKIN WITH 2 CRACKS (3 INCH) AND (.75 INCH) ZONE 05:00 HOURS. REPAIRED IAW CMM 71-11-05, FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: DOOR — DAMAGED (THRUST REVERSER) · airframe 30,104 hrs · 7,865 cycles

THRUST REVERSER DOOR 2 RIGHT AFTER SHEET METAL ZONE TS1 (SKIN) WITH SCRATCH (0.040 INCH). REPAIRED IAW CMM 78-32-34, FIG 601 (REPAIR NR 9). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 28,659 hrs · 7,053 cycles

AT 1200 FT ON T/O, NR 2 ENGINE SEVERE COMPRESSOR STALLS. TOWER REPORTED FLAME FROM RIGHT ENGINE IN FLIGHT. PERFORMED ENGINE FIRE CHECKLIST NR 2. RETURNED TO LAND, IND WEIGHT 216.0. FIRE HANDLE PULLED, 1ST AGENT DISCHARGED. EPR/EGT EXCEEDENCE MESSAGES ON ECAM. IT WAS DETERMINED THAT THE ENGINE NEEDS TO BE REPLACED DUE TO EPR AT 1.37 WHEN THE SURGE HAPPENNED.

Part: GENERATOR — FAILED (NR 1) · airframe 27,860 hrs · 6,845 cycles

ON TAKEOFF CDG NR 1 GEN FAULTED ECAM ALERT AT 60 KTS. REJECTED T/O NR 1 GEN WOULD NOT RESET. SEE PREVIOUS MEL 13JUL04 09:42 RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 16JUL04 MEL 24-11-01: GEN 1 IDG INOP.

Part: ENGINE — INOPERATIVE · airframe 26,681 hrs · 6,543 cycles

HEARD LOUD BANG, NOSE MOVED TO RT SHARPLY. FOLLOWED REJECTED TAKEOFF PROCEDURE. ALL ENGINE INSTRUMENTS NORMAL AT 105 KTS. IAW TROUBLESHOOTING MANUAL AND POWERPLANT ENGINEERING CONCURRENCE, ENGINE WILL BE CHANGED. SHIPPING INFO TENATIVE FOR REPLACEMENT ENGINE FROM MEMPHIS VIA 9004/1 TO CDG THEN 5081/2 TO DXB. REQUIRES GOCC/CREW SCHEDULING CONCURRENCE.

Part: GENERATOR — INOPERATIVE (NR 1) · airframe 26,563 hrs · 6,520 cycles

REJECTED T/O IN CDG DUE TO NR 1 IDG HIGH OIL TEMP ALERT. DISCONNECTED PER MAINT & DEFERRED PER MEL. GEN NR 1 INOP. APU GEN MUST BE USED TO POWER AFFECTED BUSS THROUGHOUT FLT. VERIFY & RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, & APU GEN ARE CHECKED ONCE EACH FLT DAY. DUE TO IDG