N750FD
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
260 reports on file, 2009-01-19 – 2019-10-07.
Part: RIB — CRACKED (RT WING) · airframe 56,549 hrs · 23,333 cycles
RIGHT OUTBOARD SIDE OF RIB 5, EVIDENCE OF A CRACK.
Part: RIB — CRACKED (N/A) · airframe 56,549 hrs · 23,333 cycles
MDIS 750 57-10 0606 08OCT19 MEM OPEN U RH OUTBOARD SIDE OF RIB 5, EVIDENCE OF CRACK. COMPLIED WITH E.A. 6-5710-T0350686 PART 1 REV A, PART 2 AND PART 3 TEMPORARY REPAIR OF R/H WING RIB 5 FOR 2 CYCLE FERRY FLIGHT
Part: TRANSMITTER — CRACKED (HYDRAULIC SYS) · airframe 56,262 hrs · 23,142 cycles
BLUE RSVR LOW ON ECAM AT TOP OF DESCENT. FOUND CRACK IN BLUE SYSTEM PRESSURE TRANSMITTER HOUSING CAUSING HYDRAULIC LEAK. R&R BLUE SYSTEM PRESSURE TRANSMITTER IAW 29-12-12-04-0. LEAK AND OPS CK GOOD.
Part: O-RING — FAILED (HYD SYSTEM) · airframe 56,231 hrs · 23,122 cycles
CLIMBING APPROX FL180 GREEN SYS QTY WENT TO 0 RETURNED TO DEPARTURE FOR EMERGENCY LANDING, AFTER GEAR EXTENDED VIA GRAVITY EXTENSION AND AT 2000 GREEN QTY RETURNED TO NORMAL. TAXIED CLEAR OF RWY. VERIFIED GREEN SYSTEM HYDRAULIC QTY. WAS NOT DEPLETED COMPLETLY IT WAS STILL WELL ABOVE RED DOT. FOUND HYDRAULIC FLUID LEAKING OUT OF THE NR 2 ENGINE COWLING. FOUND OUTLET LINE OF GREEN SYSTEM HYDRAULIC PUMP LEAKING,REMOVED AND REPLACED O-RING AND BACK-UP O-RING ON LINE REF. A300-600 AMM 29-11- 32-04-01, BLED SYSTEM AND OPERATED FLIGHT CONTROLS THROUGH SEVERAL TIMES. NO LEAKS WERE NOTED.FREE FALL SYSTEM RETURNED TO NORMAL CONFIGURATION REF. AMM 32-33-00-02. RAN NR 2 ENGINE VERIFIED GREEN SYSTEM HYDRAULIC QTY NORMAL WITH NO DISCREPANCIES NOTED,A/C IS OK FOR CONTINUE SERVICE.
Earlier reports · 2009–2018 · 256 reports
2018
Part: FLAP — OBSTRUCTED (RT WING) · airframe 55,320 hrs · 22,596 cycles
RIGHT WING INBOARD FLAP HAD A PANEL JAMMED IN THE FLAP. THE RT WING INNER OUTER FLAP DEFLECTOR WAS REMOVED AND REPAIRED ON WRI 57-50/8979. INSTALLED SERVICEABLE FLAP DEFLECTOR IAW AMM 27-54-41-04. OPS CHECKED GOOD IAW AMM 27-50-00-03. ACFTOK FOR SERVICE.
Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 55,087 hrs · 22,462 cycles
F/O SLIDING WINDOW EXTREMELY HARD TO OPEN. FOUND F/O'S SLIDING WINDOW OUT OF ADJUSTMENT. RE-RIGGED F/O'S SLIDING WINDOW PER MM 56-12-00-04. OK FOR SERVICE.
Part: ACTUATOR — UNKNOWN (RT MLG) · airframe 54,715 hrs · 22,230 cycles
REMOVE AND REPLACE RT MLG BRACE STRUT ACTUATING CYLINDER DUE TO REPEAT LDG EXTENSION PROBLEMS. COMPLETED INSTALLATION AND TEST OF RT BRACE STRUT ACTUATING CYLINDER FROM PREVIOUSLY NOTED STEP E TO COMPLETION REF AMM 32-31-55-04 AND ALL CHECKS OK.
Part: UPLOCK ACTUATOR — FAULTY (RT MLG) · airframe 54,691 hrs · 22,215 cycles
UPON GEAR EXTENSION RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED, RED RIGHT GEAR UNLOCK LIGHT ILLUMINATED, FOLLOWED ECAM/QRH MANUAL GEAR EXTENSION 3 GREEN LIGHTS. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR AND RT MLG DRAG BRACE ACTUATING CYLINDER. COMPLETED NUMEROUS EXTENSIONS AND RETRACTIONS AND FREE FALL TESTS AND ALL TESTS OK PER AMM 32-33-00-05 AND 32-31-00-05.
Part: UPLOCK — FAILED (MLG) · airframe 54,582 hrs · 22,155 cycles
ON FINAL, WHEN GEAR SELECTED DOWN, THE RT MAIN GEAR DID NOT COME DOWN AND LOCK. WENT AROUND DID ECAM PROCEDURE FOR MANUAL GEAR EXTENTION. VERIFIED DOWN BY ALL 3 IND. STOPPED ON RWY DUE TO LACK OF NOSEWHEEL STEERING. AFTER FREE FALL EXTENSION.. PERFORMED LANDING GEAR NORMAL EXTENSION AND RETRACTION OPERATIONAL TEST WITH AIRCRAFT ON JACKS IAW 32-31-00-05, 07-11-00-00, CYCLED LANDING GEAR UP/DOWN THREE TIMES, OPS CHECKED AND COCKPIT INDICATIONS ALL NORMAL.
2017
Part: SEQUENCE VALVE — FAILED (MLG) · airframe 54,331 hrs · 22,005 cycles
DURING NORMAL GEAR EXTENSION, THE RIGHT MAIN GEAR ON SYS 1 AND 2, INDICATOR SHOWED RED UNLOCKED WITH THE AMBER DOOR LIGHT ILLUMINATED. SYSTEM 3 SHOWED NO LIGHT FOR RIGHT MAIN DOWN INDICATOR. THE GEAR WAS LOWERED WITH THE MANUAL GEAR EXTENSION AND ALL 3 GEAR SHOWED DOWN AND LOCKED. USING TSM 32-30-00, FIGURE 115, REMOVED AND INSTALLED THE RT MAIN GEAR SEQUENCE VALVE.
Part: NOT REPORTED — MALFUNCTIONED (LANDING GEAR) · airframe 54,208 hrs · 21,944 cycles
DURING GEAR EXTENSION RIGHT MAIN DID NOT EXTEND. GEAR DOOR DID OPEN, CONFIGURATION VERIFIED BY LAX TOWER. GRAVITY EXTENSION ACCOMPLISHED. PERFORMED NORMAL GEAR EXTENSION AND RETRACTION SEVERAL TIMES REF AMM AMM 32-31-00-05-09. OPS CHECKED GOOD, LEAK CHECK GOOD, ALL INDICATIONS NORMAL, NO FAULTS, NO DEFECTS NOTED. PERFORMED GEAR FREE FALL EXTENSION REF AMM 32-33-00-05, OPS CHECKED GOOD, NO FAULTS, NO DEFECTS NOTED, ALL INDICATIONS NORMAL. PERFORMED NORMAL GEAR EXTENSION AND RETRACTION AGAIN 4 MORE TIMES REF AMM 32-31-00-05-09, OPS CHECKED GOOD, ALL INDICATIONS NORMAL, NO FAULTS, NO DEFECTS NOTED, A/C OK FOR SERVICE.
Part: WINDOW — BINDING (COCKPIT) · airframe 54,057 hrs · 21,854 cycles
FIRST OFFICER'S WINDOW EXTREMELY HARD TO OPEN WITH ZERO PRESSURE. LUBRICATED THE WINDOW IAW MM 12-22-56-00. WINDOW OPERATES NORMAL, NO BINDING IAW MM 56-12-00-04, AND M/M 25-13-21-4.
Part: SKIN — DENTED (RT AILERON) · airframe 53,772 hrs · 21,683 cycles
RT AILERON OTBD TRAILING EDGE, LOWER SURFACE HAS A DENT. REPAIRED IAW SRM 57-61-11, SRM 51-77-12, PARA 4B, FIG 218, AND EA 6-5750-T0333816. MAJOR REPAIR
Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 53,772 hrs · 21,683 cycles
MAIN CARGO FLOOR PANEL 242LK CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CLASSIFIED AS A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,772 hrs · 21,683 cycles
MAIN CABIN FLOOR PANEL 241HK IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CLASSIFIED AS A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,772 hrs · 21,683 cycles
MAIN CABIN FLOOR PANEL 251ZG HAS A BROKEN EDGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 CLASSIFIED AS A MAJOR REPAIR.
Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 53,328 hrs · 21,421 cycles
LEFT INBD FLAP HAS A PUNCTURE IN THE UPPER SURFACE APPROXIMATELY IN THE MIDDLE OF FLAP CAUSED BY LOOSE FASTENER FROM DROP DOWN PANEL IN FRONT OF PUNCTURE. REMOVED DAMAGE AND ACCOMPLISHED HFEC OF DAMAGE CUTOUT AREA. NO INDICATIONS NOTED IAW NTM PT6 51-10-08. A DOUBLER WAS FABERICATED AND INSTALLED DOUBLER IAW SRM 57-50-00. SEALED, PAINTED, AND COMPLETED INSTALLATION IAW SRM 57-50-00, FIGURE 205. OPERATED FLAPS IAW AMM ADJ/TEST IAW 27-50-00-05. OK FOR SERVICE.
2016
Part: NACELLE — CONTAMINATED (NR 1) · airframe 52,953 hrs · 21,209 cycles
DURING TAKE OFF, TOWER REPORTED SMOKE FROM THE NR 1 ENGINE. NO OTHER INDICATIONS OF FIRE. INSPECTED THE NR 1 ENGINE INTAKE AND EXHAUST. NO DAMAGE NOTED. OPENED COWLING AND INSPECTED FAN/CORE/EXHAUST SECTIONS. NO EVIDENCE OF FIRE FOUND. NO FLUID LEAKS FOUND. ON ARRIVAL NOTED WATER DRIPPING FROM #1 ENGINE COWL. WHEN COWLING OPENED FOUND RESIDUAL WATER IN BOTTOM OF ENGINE COWL.
Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM) · airframe 52,736 hrs · 21,074 cycles
GREEN HYDRAULIC LOW LEVEL ECAM WARNING DURING FLT. DROPPED TO BELOW RED DOT. IMMEDIATELY ON ALERT WITH SOME FLUID INDICATION, TURNED OFF BOTH GREEN HYD PUMPS. EVENTUALLY FLUID DROPPED TO ALMOST ZERO. REMOVAL, INSTALLATION OF NR 2 ENGINE CASE DRAIN HYD TUBE AND RIB 12 CLAMP BLOCK IN RT PYLON CARRIED OUT IAW AMM 29-11-69-04-01. LEAK CHECKS CARRIED OUT OK. PARTS: TUBE MPN A2911503000400, MFG CLAMP BLOCK MPN A2901501900000, MFG BUSHING, MPN NSA 935812-11.
Part: PUMP — WORN (NR 2 ENGINE) · airframe 52,426 hrs · 20,903 cycles
ON TAKEOFF ROLL, GOT YELLOW SYS, TURNED OFF PUMP, LOW PRESS. REJECTED TAKEOFF. INFO ONLY, YELLOW SYS LOW PRESS WARNING COMES BACK WHILE CYCLING FLIGHT CONTROLS. R & R YELLOW SYS ENG DRIVEN PUMP & OPERATIONS CHECKED GOOD IAW MM 29-11-32-04-01. DRY MOTOR NR 2 ENG IAW THE JRH. ALL CONDITIONS NORMAL.
2015
Part: CONNECTOR — DIRTY (HYDRAULIC SYS) · airframe 517 hrs · 20,542 cycles
ON TAKEOFF ROLL, 80 KNOTS, YELLOW HYD SYS LO LEVEL ECAM ANNUNCIATED. SPOILER FAULTS ON SPOILER 3 & 2, 5. RTO, SERVICED YELLOW SYS HYD IAW AMM 12-12-29-00. VERIFIED HEAD PRESS, RAN NR 2 ENG IAW JRH. ALL PARAMETERS NORMAL. RECHECKED HYD SERVICING AFTER RUN, NO LEAKS. RESET EFCU'S ACCOMPLISHED BITE CHECKS & OPERATION OF SYS IAW TSM 27-61-00. SUSPECT SPOILER FAULTS RESULTED FROM HYD LO QTY WARNING. SHOOK DOWN WIRING FROM YELLOW TRANSMITTER, CLEANED & RESEATED YELLOW HYD TRANSMITTER ELEC CONNECTOR. NO DEFECTS NOTED. OK FOR SERVICE.
Part: ENGINE — LEAKING (NR 1) · airframe 510 hrs · 20,099 cycles
GOT MIN EQUIPMENT BAY SMOKE WARNING IN FLIGHT, APPROX 16000 FEET COMPLIED WITH ECAM. ORH SAW HAZY LIGHT SMOKE AT ENG INSTRUMENT PANEL. RAN AVIONICS SMOKE CHECKLIST LANDED UNEVENTFULLY. PREFORMED CRUISE POWER ENG RUN IAW JRH, CONFIRMED OIL SMELL COMING FROM ENG 1 BY SWITCHING BLEED SOURCES FROM ENG 1 TO ENG 2 TO POWER PACK 1. AFTER 10 MIN RUN AT 1.33 EPR & TAXI TO & FROM RUN PAD. ENG 1 USED 2 QTS OF OIL INDICATED. 5MIN AFTER SHUTDOWN OBSERVED 1 QT OF OIL POUR OUT FROM HP COMPRESSOR SECTION. OIL APPEARS TO BE COMING FROM HP COMP SECTION APROX STAGE 2 OR FURTHER BACK. ENG 1 R & R WILL FIX THIS SMOKE & ODOR PROBLEM. THE NR 1 ENG IS APPROVED FOR REMOVAL, DUE TO INTERNAL OIL LEAKAGE AMM 21-51-00-03, 21-51-16-03. AFTER ENG 1 R & R WRI 72- 10 5497. REFORMED PACK ODOR & OIL BURN OUT FOR BOTH PACKS. AFTER REPLACED COALESCER SOCKS FOR BOTH SOCKS.
Part: WEB — GOUGED (FUSELAGE) · airframe 509 hrs · 20,032 cycles
THIS COMPARTMENT LT DOOR, 313AL, CUT OUT BUCKLED WITH GOUGE. LOCATED OTBD IN FROM FWD CORNER. REMOVED DAMAGED WEB, INSTALLED NEW WEB & 2 EA INTERCOSTAL AFT THS COMPARTMENT LT DOOR CUT OUT IAW SRM 51-40-21. FABRICATED ON T15 1115998. MAJOR REPAIR.
Part: STRINGER — CORRODED (ZONE 300) · corrosion level 2 · airframe 509 hrs · 20,032 cycles
FUSELAGE EXTERNAL STRINGER BELOW VERT STAB AT LT MIDDLE FIN TO FUSELAGE FITTING IS CORRODED. R & R ON FUSELAGE EXTERNAL STRINGER 3L BELOW VERT STAB IAW 51-40-21. REMOVED CORROSION AT STRINGER 3L, ORIGINAL THICKNESS .155 AFT REWORK MATERIAL LOSS IS .040. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. MAJOR REPAIR.
Part: FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 50,958 hrs · 20,032 cycles
RIGHT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES. REPAIRED IAW DWG R57240425 REV D & EA 6-5710-T0314932. MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER AREA FLOOR PANEL 222NF IS CRACKED. FABRICATED COURIER AREA FLOOR PANEL 222NF IAW SRZ-25-005 REV K ON T14 1113353 CAT A MAJOR REPAIR.
Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER AREA, CENTERLINE FLOOR SUPPORT IS GOUGED ON UPPER SURFACE BETWEEN FRAME 11 & 12. R & R FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
SEAT TRACK YD 37.52 HAS CORROSION FROM FRAME 11 - 17 IN SEVERAL AREAS. R & R SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER AREA, FLOORBEAM YC HAS CORROSION IN 3 PLACES BETWEEN FRAME 11 & 12 ON TOP SURFACE T CAP CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15 L=1.0" W=1.0" D= 100%. R & R T CAP IAW SRM 51-40-21 CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
BULK CARGO COMPARTMENT FLOOR PANEL 171CF IS DAMAGED & BROKEN ON EDGE OF PANEL. FLOOR PANEL 171CF FABRICATED ON T15 1114494, REPAIR CLASSIFIED CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 161BF DAMAGED. FLOOR PANEL 161BF FABRICATED ON T14 111859 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT CARGO FLOOR PANEL 151UF IS CRACKED AT CORNER FLOOR PANEL 151UF. FABRICATED ON T14 1114496 IAW DWG SRZ25-005. CLASSIFIED AS CAT A MAJOR.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
MAIN DECK BETWEEN FRAME 57 & 57.2 SEAT TRACK -Y450 HAS GOUGE. R & R SEAT TRACK SECTION -Y450 BETWEEN FRAME 57 TO 57.2, PN A53274005SF BATCH 0002120270 IAW SRM 53-10-16. MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 161AF DAMAGED. FLOOR PANEL 161AF FABRICATED ON T14 111858 IAW DWG SRZ 25-0. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 231BH IS CRACKED. FLOOR PANEL 231BH FABRICATED ON T14 1111397 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER AREA FLOOR PANEL 221PF HAS 5 INCH LONG CRACK AT THE RT CUT OUT. FABRICATED NEW FLOOR ON T14 1113599 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 241AK IS CRACKED. FLOOR PANEL 241AK FABRICATED ON T14 1111592 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
PANEL 152HF IN AFT PIT PUNCTURED. FLOOR PANEL 152HF FABRICATED ON T14 1111933 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
PANEL 152QF IN AFT PIT PUNCTURED. FLOOR PANEL 152GF FABRICATED ON T14 1111934 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 242XK IS DELAMINATED ON THE LOWER SURFACE. FLOOR PANEL 242XK FABRICATED ON T14 1111593 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER COMPARTMENT FLOOR PANEL 221MF HAS EDGE DAMAGE & IS MISSING ONE INSERT. FLOOR PANEL 221MF FABRICATED ON T14 143354 IAW DWG SRZ 25-005. CAT A CLASSIFIED MAJOR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD PIT FLOOR PANEL 131 HG IS CRACKED. FABRICATED NEW FLOOR PANEL 131HG ON T14 1111506 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251VF DAMAGED. FLOOR PANEL 251VF FABRICATED ON T14 1111616 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
MAIN CARGO DECK FLOOR PANEL 241RJ IS CRACKED AT RT END OF THE CUT OUT. FABRICATED NEW FLOOR PANEL 241RJ ON T14 1113601 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251WH DAMAGED. FLOOR PANEL 251WH FABRICATED ON T14 1111615 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS A CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD CARGO COMPARTMENT FLOOR PANEL 131QF, HONEYCOMB MATERIAL IS DAMAGED AT SEVERAL LOCATIONS AROUND THE PANEL EDGES. FABRICATED NEW FLOOR PANEL 131QF ON T 141113602 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 231EF HAS TWO EACH PUNCTURES. FLOOR PANEL 231EF FABRICATED T14 1111400 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232DF HAS A PUNCTURE. FLOOR PANEL 232 DF FABRICATED T14 1111597 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232HG HAS A PUNCTURE & DELAMINATION. FLOOR PANEL 232HG FABRICATED T14 1111599 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 231FF IS CRACKED. FLOOR PANEL 231FF FABRICATED T14 111598 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR.
2014
Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 50,958 hrs · 20,032 cycles
LEFT WING AILERON OTBD HINGE PIN HAS CORROSION. NO DAMAGE ALLOWED ON PIN IAW WC 65X5093CP & AMM 57-51-34-06. R & R PIN PN A5764001300000 ON WC 65X5093CP. REPAIR CLASSIFIED AS MINOR CAT A.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
MCD FLOOR PANEL 241CK HAS DAMAGE AT FWD RT CORNER. FABRICATED NEW FLOOR PANEL 241CK ON T14 1113600 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 151LF HAS DAMAGE AT FWD LT CORNER & AFT LT CORNER. FLOOR PANEL 151LF FABRICATED ON T14 1113598 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: ATTACH FITTING — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 50,958 hrs · 20,032 cycles
NUMBER 2 PYLON ATTACH FITTING RIB 18 HAS CORROSION ON BORE. R & R NR 2 PYLON ATTACH FITTING RIB 18 IAW AMM 54-51-75-04-01. CORROSION FOUND DURING INSPECTION ON EA 6-5450-120174 P2.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
COURIER AREA, FLOOR SUPPORT BETWEEN FRAME 12 & 13 IS SCRATCHED ON TOP SURFACE, JUST INBD OF FLOORBEAM YC T CAP GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15 L=2.0" W=.010" D=.050". R & R T CAP IAW SRM 51-40-21 & 51-72-00. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
SEAT TRACK YE 17.69 HAS CORROSION FRAME 11 - 17 IN SEVERAL AREAS. R & R SEAT TRACK IAW SRM 51-40-21. CLASSIFIED AS MAJOR CAT A REPAIR. DAMAGE DIMENSIONS L=6.0" W=0.400" D=0.040" FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101.
Part: ADAPTER — DEFORMED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
MAIN DECK AT FRAME 58 BETWEEN SEAT TRACK Y1456 & Y1959 SEAT TRACK ADAPTER CROWN IS DEFORMED. R & R SEAT TRACK ADAPTER IAW SRM 51-40-21.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 151AF DAMAGED. FABRICATED NEW FLOOR PANEL 151AF ON T14 1111857 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD PIT FLOOR PANEL 132AF IS CRACKED. FLOOR PANEL 132AF FABRICATED ON T14 1111508 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 231KG IS CRACKED. FLOOR PANEL 231KG FABRICATED ON T14 1111398 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 151FF DAMAGED. FABRICATED NEW FLOOR PANEL 151FF ON T14 1111855 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232UG IS CRACKED ON THE UPPER SURFACE. FLOOR PANEL 232UG FABRICATED ON T14 1111600 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 151JF DAMAGED. FABRICATED NEW FLOOR PANEL 151JF ON T14 1111856 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232KG HAS A PUNCTURE. FLOOR PANEL 232KG FABRICATED ON T14 111611 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 261RF IS CRACKED. FABRICATED NEW FLOOR PANEL ON T14 1111613 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT CARGO FLOOR PANEL 151DF IS CRACKED. FABRICATED NEW FLOOR PANEL 151DF ON T14 1111412 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS A CAT A REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT PIT FLOOR PANEL 152LF IS CRACKED & DELAMINATED. FLOOR PANEL 152LF FABRICATED ON T14 1111396 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 231GG DAMAGED. FABRICATED NEW FLOOR PANEL ON T14 1111854 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 231AH DAMAGED. FLOOR PANEL 231AH FABRICATED ON T14 1111860 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 262KF DAMAGED. FLOOR PANEL 262KF FABRICATED ON T14 1111853 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 231CF DAMAGED. FLOOR PANEL 231CF FABRICATED T14 1111413 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: ATTACH FITTING — GOUGED (RT PYLON) · airframe 509 hrs · 20,032 cycles
RIGHT PYLON TO ENG FWD ATTACH FITTING, INBD LOWER ARM, LOWER CORNER HAS GOUGE, JUST BELOW FEEDER LINES. ACCOMPLISHED FINAL EA 6-5440-T0315003 REV NR PS P1 CLASSIFIED AS MAJOR REPAIR. REPAIR LIFE LIMITATION 6 MONTHS IAW RDAS 80018687 003 2015 ISSUE A.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT PIT FLOOR PANEL 152KF IS CRACKED. FLOOR PANEL 152KF FABRICATED ON T14 1111393 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 251DK IS CRACKED. FLOOR PANEL 251DK FABRICATED ON T14 1111595 IAW DWG SRZ-25-005, REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232LG IS DELAMINATED & HAS A PUNCTURE. FLOOR PANEL 232LG FABRICATED ON T14 1111852 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 232CF HAS TWO PUNCTURES. FABRICATED NEW FLOOR PANEL ON T14 1111851 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 152DF DAMAGED. FLOOR PANEL 152DF FABRICATED ON T14 1111617 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT CARGO PIT FLOOR PANEL 151HF IS CRACKED. FLOOR PANEL 151HF FABRICATED ON T14 /1111510 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 262ZF IS CRACKED & DELAMINATED. FLOOR PANEL 262ZF FABRICATED ON T14 1111411 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD PIT FLOOR PANEL 131ZF IS CRACKED. FLOOR PANEL 131ZF FABRICATED ON T14 1111505 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 242SJ IS CRACKED. FLOOR PANEL 242SJ FABRICATED ON T14 111591 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 261ZF IS CRACKED. FLOOR PANEL 261ZF FABRICATED ON T14 1111399 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FORWARD PIT FLOOR PANEL 132QF IS CRACKED. FABRICATED NEW FLOOR PANEL 132QF ON T14 1111931 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 252XL DAMAGED. FLOOR PANEL 252XL FABRICATED ON T14 1111614 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 231HG IS DELAMINATED. FABRICATED NEW FLOOR PANEL 231HG ON T14 111612 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,958 hrs · 20,032 cycles
MAIN CABIN FLOOR PANEL 242JG IS CRACKED. FLOOR PANEL 242JG FABRICATED ON T14 1111596 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT CARGO PIT FLOOR PANEL 151KF IS MISSING EDGE FILLER. FLOOR PANEL 151KF FABRICATED ON T14 1111393 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 152FF DAMAGED. FABRICATED NEW FLOOR PANEL 152FF ON T14 1111932 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD PIT FLOOR PANEL 132HG IS CRACKED. FABRICATED NEW FLOOR PANEL 132HG ON T14 1111392 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FORWARD CARGO BAY FLOOR PANEL 131JG CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
FWD PIT FLOOR PANEL 132JG IS CRACKED. FABRICATED NEW FLOOR PANEL 132JG ON T14 1111509 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 241VG DAMAGED FRAME 54.2 - 55 MAIN DECK CRACK. FLOOR PANEL 241VG FABRICATED ON T14 1110365 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
AFT PIT FLOOR PANEL 151CF IS CRACKED AT A CORNER. FLOOR PANEL 151CF FABRICATED ON T14 1111394 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251DL DAMAGED CRACK. FLOOR PANEL 251DL FABRICATED ON T14 1110374 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251BH HAS EDGE & CORE DAMAGE FRAME 65 & 69 MAIN DECK. FLOOR PANEL 251BH FABRICATED ON T14 1110360 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 252BF DAMAGED FRAME 55 - 57.1 MAIN DECK. FLOOR PANEL 252BF FABRICATED ON T14 1110368 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251YG DAMAGED FRAME 60 - 65 MAIN DECK. FLOOR PANEL 251YG FABRICATED ON T14 1110370 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 232BH IS CRACKED. FLOOR PANEL 232BH FABRICATED ON T14 1110375 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 241EJ DAMAGE, CRACK, FRAME 54 MAIN DECK. FLOOR PANEL 241EJ FABRICATED ON T14 1110361 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251BF DAMAGED FRAME 55 - 57.1 MAIN DECK. FLOOR PANEL 251BF FABRICATED ON T14 1110363 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251RG DAMAGED FRAME 57.1 TO 58 MAIN DECK. FLOOR PANEL 251RG FABRICATED ON T14 1110372 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251PH DAMAGED FRAME 58 TO 60 MAIN DECK. FLOOR PANEL 251PH FABRICATED ON T14 1110369 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 251NG DAMAGED FRAME 55 - 57.1 MAIN DECK. FLOOR PANEL 251NG FABRICATED ON T14 1110364 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 50,958 hrs · 20,032 cycles
FLOOR PANEL 242TG DAMAGED FRAME 54 - 54.2 MAIN DECK. FLOOR PANEL 242TG FABRICATED ON T14 1110362 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
BULK CARGO FLOOR PANEL 161JF HAS .5 INCH DEEP PUNCTURES ON UPPER SURFACE, FRAME 66 - 70. FLOOR PANEL 161JF FABRICATED ON T14 1109908 IAW DWG SRZ-25-011. REPAIR CLASSIFIED AS CAT A MAJOR.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
BULK CARGO FLOOR PANEL 161GF HAS SEVERAL PUNCTURES ON UPPER SURFACE APPROX .5 INCH DEEP, FRAME 66 - 70, FLOOR PANEL 161GF. FABRICATED ON T14 1109906 IAW DWG SRZ-25-011. REPAIR CLASSIFIED CAT A MAJOR.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 50,958 hrs · 20,032 cycles
BULK CARGO FLOOR PANEL 162HF HAS .5 INCH DEEP PUNCTURES ON UPPER SURFACE, FRAME 66 - 70. FLOOR PANEL 162HF FABRICATED ON T14 1109907 IAW DWG SRZ-25-011. REPAIR CLASSIFIED AS CAT A MAJOR.
2012
Part: UPLOCK — FAILED (MLG) · airframe 48,936 hrs · 18,823 cycles
ON FINAL APPROACH, THE RT MAIN GEAR DID NOT EXTEND. ALL INDICATIONS WERE THE RT GEAR NOT DOWN AND LOCK, WHICH WAS CONFIRMED BY TOWER. COMPLIED WITH QRH, DECLARED EMERGENCY. R & R RT DOOR UPLOCK IAW MM 32-31-33-04. INSPECTION/CHECK OF MAIN GEAR DOOR UPLOCK AND FREE FALL EXTENSION ADJUSTMENT TEST PERFORMED IAW MM 32-31-33-06 AND 32-33-00-05. NO LEAKS NOTED ALL CHECKED NORMAL. OK FOR SERVICE.
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 48,914 hrs · 18,811 cycles
ON DEPARTURE HAD A SLATS FLAPS FAULT ON RETRACTING SLATS/ FLAPS. RECYCLED AND WOULD NOT CLEAR. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FLAPS WERE RETRACTED WHEN ACFT ARRIVED AT GATE IAW TSM 27-50-00. CLEARED FAULTS ON SFCC 1 AND 2 CYCLED FLAPS NORMALLY. NO FAULTS FOUND. INSPECTED FLAP TORQUE LIMITERS NOT TRIPPED IAW MM 27-54-12-04. OK TO CONTINUE.
Part: UPLOCK — FAILED (MLG) · airframe 48,895 hrs · 18,799 cycles
ON FINAL, AT GEAR EXTENSION, RT MAIN GEAR FAILED TO EXTEND - WENT AROUND AND RAN MANUAL GEAR EXT CHECKLIST GEAR CAME DOWN, LANDED. REMOVED AND REPLACED RIGHT MAIN GEAR UPLOCK ASSY
2011
Part: SKIN — DENTED (ZONE 100) · airframe 47,982 hrs · 18,282 cycles
LWR FUSELAGE SKIN FR57.3-58 S44-45R FOUND A DENT 6" IN LENGTH. PERFORMED A DVI AND ENSURED THE DENT IS IN SMOOTH CONTOUR WITHOUT SHARP EDGE. THE SCRATCH HAD BEEN REWORKED TO SMOOTH CONTOUR IAW SRM 51-73-10. PERFORMED A ROTO TEST INSPECTION OF OPENED FASTENER HOLES TO CONFIRM NO DAMAGE. PERFORMED DV AND HFEC INSP FROM INSIDE TO CONFORM NO DAMAGE ON INNER STRUCTURE PARTS. PERFORMED FLAP PEENING ON REWORKED AREA WITH I=0.15MM IAW SRM 51-29-11. PERFORMED SURFACE PROTECTION IAW SRM 51-75-10. INSTALLED 1ST OVERSIZED FASTENERS IAW SRM 51-40-21 COMPLIED WITH EA 6-5330-153460.
Part: SKIN — CHAFED (FUSELAGE) · airframe 47,982 hrs · 18,282 cycles
FUSELAGE SKIN CHAFED AT C32-C33 S43R. STRIPPED THE PAINT PER SRM 51-75-20. REMAINING THICKNESS IS 0.044" PER NTM 51-10-04 NO CRACK FOUND PER NTM 51-10-08. ORIGINAL THICKNESS IS 0.063", OUT OF LIMITS PER SRM 53-10-12/101 PARA 7. REPAIRED SKIN PER SRM 53-10-12/201 FIG 216.
Part: SKIN — CHAFED (FUSELAGE) · airframe 47,982 hrs · 18,282 cycles
FUSELAGE SKIN CHAFED AT C31-C32, STR 43R. STRIPPED PAINT PER SRM 51-75-20 2. REMAINING THICKNESS IS 0.036" PER NTM 51-10-04 3. NO CRACK FOUND PER NTM 51-10-08 4. ORIGINAL THICKNESS IS 0.063" , OUT OF LIMITS PER SRM 53-10-12/101 PARA 7 5. REPAIRED SKIN PER SRM 53-10-12/201 FIG 216
Part: SKIN — CHAFED (FUSELAGE) · airframe 47,982 hrs · 18,282 cycles
FUSELAGE SKIN CHAFED AT C34 S43R. STRIPPED THE PAINT PER SRM 51-75-20. REMAINING THICKNESS IS 0.051" PER NTM 51-10-04. NO CRACK FOUND PER NTM 51-10-08. ORIGINAL THICKNESS IS 0.063", OUT OF LIMITS PER SRM 53-10-12/101 PARA 7. REPAIRED SKIN PER SRM 53-10-12/201 FIG 216.
2010
Part: LANDING GEAR — MALFUNCTIONED · airframe 46,760 hrs · 17,611 cycles
LG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. COMPLIED WITH TEST OF PROXIMITY DETECTOR PROCESSING UNIT (54GB) IAW TSM 32-61-00. NO FAULTS NOTED AT THIS TIME. GEAR PINS INSTALLED. PERFORMED TEST OF LANDING GEAR ELECTROVALVE (3GA) 6 TIMES FAILED STEP 2 (B) 3 TIMES. DOORS DID NOT OPEN WITH HYD POWER ON CONTROL LEVER SWITCHED FROM NEUTRAL TO UP 3 TIMES. SUSPECT BAD ELECTROVALVE (3GA). REMOVED AND STOWED ALL 3 GEAR PINS. RELEASED FOR SERVICE IAW MEL: 32-30-01-A "MEL 32-30-01-A.
Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 46,760 hrs · 17,611 cycles
LG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. JACKED A/C VERIFIED VALVE 3GA FAULTY REMOVED AND REPLACED VALVE IAW MM 32-31-12-04. ALSO REMOVED AND REPLACED MODULE LANDING GEAR CONTROL HANDLE (2GA) IAW MM 32-32-11-04-0. PERFORMED LANDING GEAR SWING IAW MM 32-31-00 CHECKS NORMAL.
Part: IDG — MALFUNCTIONED (NR 1) · airframe 46,420 hrs · 17,415 cycles
ABORTED TAKEOFF AT 100 KNOTS, DUE CHIME AND LOW OIL ON NR 1 IDG OR LOW OIL ON NR 1 ENG. RELEASED FOR SERVICE IAW MEL: 24-11-01-A CATEGORY: B EXPIRATION: "MEL 24-11-01-A: GEN NR 1 - INOP. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN AML/EAML THAT OIL QT Y OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, AND APU ARE CHECKED ONCE EACH FLIGHT DAY." REPLACED THE NR 1 ENGINE IDG REF MM 24-11-11-04, CKS. OK ON ENGINE RUNS.
2009
Part: ELECTRONIC UNIT — FAULTED · airframe 44,894 hrs · 16,563 cycles
ON FINAL FULL CONFIGURATION (GEAR AND FLAPS 40), THERE WAS NO INDICATION OF BRAKE RELEASE (RELEASE BARS NOT IN VIEW). EXECUTED A GO AROUND TO TROUBLESHOOT. RELEASE BARS CAME BACK FOR NO APPARENT REASON, WENT OFF AGAIN, BUT ALL INDICATIONS NORMAL AT 500 FT, LANDING UNEVENTFUL. REPLACED PROX DETECTOR PROCESSING UNIT IAW MM 32-31-71-4. OPS CHECK GOOD, PERFORMED NORMAL BRAKING TEST AND IN FLIGHT BRAKING TEST IAW MM32-42-00-5 NO FAULTS NOTED. ACFT OK FOR SERVICE. ACFT OK FOR SERVICE.
Part: SKIN — CRACKED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
OLD EXTERNAL DOUBLER PATCH REPAIR WITH CRACKED HOLES. REPAIR PERFORMED IAW EA 6-5730-129153.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS BETWEEN RIB 14 AND 29 TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.
Part: RIB — CRACKED (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
RT WING CRACK IN RIB 7 UPPER FWD FLANGE INBOARD SIDE FLANGE BLENDED TO A SMOOTH PROFILE IAW EA 6-5710-129160.
Part: SKIN — MISINSTALLED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
IRREGULARLY BOLT HOLE AT LT WING TOP SKIN RIB 8 STRINGER 14 SKIN REINFORCING REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.
Part: SHROUD — DELAMINATED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
DAMAGE ON OUTER SHROUD BOX LT WING REPAIR PERFORMED IAW EA 6-5750-120235 AND RAS/BAE/1009297/2009.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
MULTIPLE CORROSION, TOP SKIN, TE OVERHANG, RIB 25-29, LEFT WING CORROSION REMOVED BY BLENDING AND NEW FASTENERS INSTALLED IAW EA 6-5720-129141. FABRICATION NEW PANEL IAW EA 6-5750-129151.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS BETWEEN RIB 9 IN LEVEL OF CENTER SPAR TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS LT WING TOP SKIN PANEL BETWEEN RIB 1 AND 14 UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS /BAE/1009557/2009.
Part: SHROUD — CORRODED (ZONE 600) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
CORROSION ON OUTER SHROUD BOX RT REPAIR PERFORMED IAW EA 6-5720-120231 AND RAS/BAE/1009111/2008.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENERS ON THE RT WING UPPER SURFACE BETWEEN RIB 1 AND 14. REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/1009447/2009 ISSUE "A".
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
CORROSION SPOT BETWEEN RIB 14 AND 15 / BETWEEN FRONT SPAR AND STRINGER 9 AT RT WING TOP SKIN, ARROUND FASTENER EXTERNAL SURFACE REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENER RT WING TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 14 AND 29 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"
Part: PLATE — CHAFED (WING) · airframe 44,816 hrs · 16,508 cycles
CHAFING MARKS IN THE LOWER WING PYLON REINFORCING PLATE. REPAIR PERFORMED IAW EA 6-5710-129142, TD/J1/S1/09291/2009 ISSUE "C" AND RAS /BAE/1009291/2009 ISSUE "A".
Part: RIB — DENTED (LT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
DENT IN LEADING EDGE RIB 26-27 NOSE RIB REPLACED BY NEW ONE IAW SRM 57-50-00/201/FIG 208.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
CORROSION SPOTS AROUND FASTENERS ON THE RT WING TOP SKIN RIB 8 REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/1009447/2009 ISSUE "A"
Part: RIB — CRACKED (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
CRACK AT LEADING EDGE SLAT JACK RIB 4A REPAIR PERFORMED IAW EA 6-5740-129105 AND RAS/BAE/1009425/2009 ISSUE "A".
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS AROUND SOME FASTENERS AT TOP SKIN JOINT EXTERNAL SURFACE IN THE AREA OF RIB 9 FRONT AND REAR SPAR REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
CORROSION AND CHAFING, BOTTOM SKIN PANEL 1 AND 2, PYLON AND FLAP TRACK 2 REINFORCEMENT PLATE. REPAIR PERFORMED IAW EA 6-5720-129136, TD/J1/S1/09343/2009 ISSUE "A", TD/J1/S1/09620/2009 ISSUE "A" AND RAS/BAE/1009343/2009 ISSUE "A".
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
SEVERAL CORROSION SPOTS RT WING TOP SKIN PANEL SURFACE FRONT SPAR ATTACHMENT BETWEEN RIB 1 AND 14 AND REAR SPAR ATTACHMENT BETWEEN RIB 1 AND 9 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"
Part: STRINGER — UNKNOWN (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
STRINGERS RIB 14 WITH RUN-OUTS REPROFILED INCORRECTLY. REPAIR PERFORMED IAW EA 6-5710-129150 AND RAS/BAE/1009505/2009 ISSUE "A".
Part: RIB — CRACKED (RT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
DEVIATION RT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED IAW EA 6-5750-120193 , TD FOK/001/2009 ISSUE "C" AND RAS/FOK/001/2009 ISSUE "A" .
Part: SKIN — CORRODED (LT WING LE FLAP) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND HEAVY CORROSION UNDER OUTER STATIC DISCHARGER OUTER FLAP LT REPAIR PERFORMED IAW EA 6-5750-129109, RAS/FOK/043/2009 ISSUE "B" AND RAS/FOK/043/2009 ISSUE "A"
Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
DEVIATION LT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND MODIFICATION IAW OF RIB AS PER SB A300-57-6098. INSTALLED IAW SRM 51-72-10 AND TD FOK/359/2008 ISSUE "C" .
Part: SKIN — DELAMINATED (RUDDER) · airframe 44,816 hrs · 16,508 cycles
FOUND DELAMINATION ON RUDDER DURING NTM INSPECTION. REPAIR PERFORMED BY RUDDER REPLACEMENT IAW AMM 272121PB 400.
Part: BEAM — CRACKED (FUSELAGE) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACK INDICATION ON BEAM 4 RT, C 49 OUTBOARD. REPAIR PERFORMED IAW DRAWING R538-10581, INSTALLATION OF REINFORCING ANGLE, SHIMS AND REPAIR STRAP.
Part: SKIN — WORN (LT WING) · airframe 44,816 hrs · 16,508 cycles
FOUND ELONGATED HOLES ON LT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.
Part: RIB — CHAFED (RT WING) · airframe 44,816 hrs · 16,508 cycles
FOUND OLD DRILLING MARKS IN RT WING REAR SPAR RIBS IN THE TRAILING EDGE AREA. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009148/2009 ISS A, APPROVED BY EA 6-5710-129140.
Part: SKIN — WORN (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
FOUND ELONGATED HOLES ON RT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.
Part: STIFFENER — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED STIFFENERS ON FIRE WALL C 95. REPAIR PERFORMED BY REPLACEMENT OF PART IAW RAS/EFW/9000159/2009 ISS A, APPROVED BY EA 6-5310-120205.
Part: RIB — DAMAGED (ZONE 600 TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND SEVERAL HOLES DAMAGED ON RT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW, RAS/FOK/352/2009 ISS B, APPROVED BY EA 6-5750-120182.
Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON FWD PAX DOOR LT UNDER DOOR STOP FITTINGS REPAIR PERFORMED BY REPLACEMENT OF DAMAGED PART IAW RAS 705178676/027/2009 ISS A, APPROVED BY 6-5210-129128.
Part: RIB — DAMAGED (ZONE 500 TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND SEVERAL HOLES DAMAGED ON LT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW RAS/FOK/351/2008 ISS A, APPROVED BY EA 6-5750-120184.
Part: SKIN — CHAFED (NR 2 SLAT) · airframe 44,816 hrs · 16,508 cycles
FOUND 2 OLD CHAFING MARKS ON SLAT NR 2 BETWEEN CLOSING RIB AND RIB 3. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IN AREA 1 AND DOUBLER REPAIR IN AREA 2 IAW RAS/FOK/004/2009 ISS A, APPROVED BY EA 6-5740-120228.
Part: SKIN — CHAFED (NR 1 SLAT) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS ON SLAT NR 1 NEAR TRACK NR 3, LOWER SURFACE. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/003/2009 ISS A, APPROVED BY EA 6-5740-120194.
Part: HINGE FITTING — CORRODED (LT AILERON) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION AND SCRATCHES ON LT AILERON HINGE FITTING. REPAIR PERFORMED BY REAM UP THE HOLE UNTIL DAMAGE REMOVAL AND INSTALLING A BUSHING IAW RAS/FOK/032/2009 ISS A , APPROVED BY EA 6-5750-120232.
Part: FITTING — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED HOLE ON FITTING AT FRAME 91 NEAR P 37 RT REPAIR PERFORMED BY BUSHING REPAIR IAW RAS/EFW/9000157/2009 ISS B, APPROVED BY EA 6-5310-120201.
Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 44,816 hrs · 16,508 cycles
FOUND DELAMINATION ON SPOILER NR 3 RT OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-51 PB 400.
Part: SKIN — DELAMINATED (NR 4 SPOILER) · airframe 44,816 hrs · 16,508 cycles
FOUND DELAMINATION ON SPOILER NR 4 LT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-51 PB 400.
Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS ON RT INNER FLAP LEADING EDGE RIB 10-20. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/027/2009 ISS A, APPROVED BY EA 6-5750-120230.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION AROUND FASTENERS ON TOP SKIN OF FALSE SPAR, RIB 4-5A. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION AND REPLACEMENT OF FASTENERS IAW RAS/BAE/1009315/2009 ISS A, APPROVED BY EA 6-5720-129104.
Part: SPAR — CHAFED (NR 2 SPOILER) · airframe 44,816 hrs · 16,508 cycles
FOUND WEAR MARKS ON LT SPOILER NR 2 ON FRONT SPAR. REPAIR PERFORMED BY PATCH REPAIR IAW RAS 70518127/019/2009 ISS A, APPROVED BY EA, 5750-129127.
Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 44,816 hrs · 16,508 cycles
FOUND DELAMINATION ON SPOILER NR 5 RT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-53 PB 400.
Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 44,816 hrs · 16,508 cycles
FOUND DELAMINATION ON SPOILER NR 5 LT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-53 PB 400.
Part: FRAME — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND SEVERAL DAMAGED AREAS ON RT FRAME C 47 IN SEVERAL HOLES. REPAIR PERFORMED BY REAM UP THE HOLES IAW 041976/041/2005 ISS A, APPROVED BY EA 6-5310-129126.
Part: SKIN — CHAFED (RT WING) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS ON OUTER SURFACE A D-NOSE RT WING BETWEEN JACK PAD 2 AND WOFX-48.90. REPAIR PERFORMED BY BLEND OUT AND NDT FOR CRACK FREE CONDITION AND INSTALLING AN INFILL PLATE IN AREA 1 IAW RAS/BAE/1009278/2009 ISS A, APPROVED BY EA 6-5710-120234.
Part: FITTING — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND OLD REPAIR ON C 47 IN HOLE N, BUSHING INSTALLATION IAW RAS/AS/0001/2006 ISS C, AFTER REMOVAL FOUND NEW DAMAGES, AND DAMAGES IN HOLE 3, 7, 12. REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALL A BUSHING IAW 041976/041/2005 ISS A, APPROVED BY EA 6-5310-129126.
Part: SKIN — CRACKED (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACKED HOLES ON AN OLD REPAIR IN RT SHROUD BOX AREA ON TOP SKIN REPAIR PERFORMED BY OVERSIZING THE HOLES. INSTALLING EXTERNAL STRIP DOUBLER AND INTERNAL BACK STRIPS IAW RAS/BAE/0107/96 ISS D, APPROVED BY EA 6-5750-129135.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON SKIN AND STRINGER P 56 LT, C 77 AND P45 LT-45 RT IN THIS AREA WAS INSTALLED AN EXTERNAL DOUBLER. REPAIR PERFORMED BY REMOVAL OF EXTERNAL DOUBLER, REWORK OF CORROSION, CHECK FOR CRACK FREE CONDITION, INSTALLING A REINFORCING PLATE IAW RAS/EFW/9000166/2009 ISS B AND BY INSTALLING A NEW EXTERNAL DOUBLER AND PERFORMING A STRINGER REPAIR IAW RAS 942.3485/90 ISS B, APPROVED BY EA 6-5310-129138.
Part: SKIN — CHAFED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
FOUND ON LT CENTER FLAP TOP SKIN RIB 13-15 2 AREAS OF CHAFING MARKS. REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION IAW AS/FOK/040/2009 ISS A, APPROVED BY EA 6-5750-129134.
Part: SKIN — CHAFED (ZONE 600) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS AT REINFORCING PLATE RIB 8 WING BOTTOM SKIN RHS REPAIR PERFROMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009347/2009 ISS A, APPROVED BY EA 6-5710-129102.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND ON LT INNER FLAP OLD FILLED REPAIR, AFTER REMOVING OF FILLER, DENT VISIBLE, RIB 16-17 TOP SKIN. REPAIR PERFORMED BY BLEND OUT IAW RAS/FOK/066/2009 ISS A, APPROVED BY EA 6-5750-129131.
Part: SKIN — CRACKED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACKED HOLES ON AN OLD REPAIR IN LT SHROUD BOX AREA ON TOP SKIN. REPAIR PERFORMED BY OVERSIZING THE HOLES, INSTALLING EXTERNAL STRIP DOUBLER AND INTERNAL BACK STRIPS IAW RAS/BAE/0107/96 ISS D, APPROVED BY EA 6-5750-129135.
Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND OLD REPAIR ON LT CENTER FLAP TRAILING EDGE TOP SKIN NOT PERFORMED IAW RAS/FOK/024/2009 ISS A. PATCH REPAIR RENEWED IAW RAS/FOK/024/2009 ISS A, APPROVED BY EA 6-5750-129123.
Part: PANEL — DELAMINATED (BODY FAIRING) · airframe 44,816 hrs · 16,508 cycles
FOUND OLD REPAIR ON RT BODY FAIRING PANEL 677GT, C 54.2-55, IN BAD CONDITION. REPAIR RENEWED IAW RAS 70517631/004/2008 ISS B, APPROVED BY EA 6-5350-120215.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON RT OUTBOARD RUN OUT FITTING , C 16-17, P44. REPAIR PERFORMED IAW SRM 53-12-14 FIG 201.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON LT OUTBOARD RUN OUT FITTING, C 16-17, P44. REPAIR PERFORMED IAW SRM 53-12-14 FIG 201.
Part: BEAM — CRACKED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACK ON TRACK 4 LT AT C49 AND 51 ABOVE CENTER TANK. REPAIR PERFORMED IAW DRAWING R538-10581 AND RAS 70518174/022/2009 ISS A, APPROVED BY EA 6-5310-120236.
Part: HINGE — CHAFED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND ON RT CENTER HINGE FLANGE FOR MLG DOOR CHAFING MARKS OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: SKIN — DAMAGED (LT WING) · airframe 44,816 hrs · 16,508 cycles
FOUND A IMPACT DAMAGE AT CUT OUT FOR OUTBOARD NR 10 TRACK IN LEADING EDGE 'D-NOSE' ON LT WING. REPAIR PERFORMED BY BLEND OUT THE AREA, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009163/2009 ISS A, APPROVED BY EA 6-5710-129132.
Part: PLATE — DAMAGED (ZONE 300) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED CONNECTING PLATE BY TOOLING MARKS ON C 91. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON AFT CARGO DOOR SILL BEAM C 59-C59A. REPAIR PERFORMED BY CUT OUT THE AFFECTED PART AND INSTALLING REINFORCEMENT, FILLER AND NUT PLATES IAW RAS/EFW/9000150/2008 ISS A, APPROVED BY EA 6-5310-120197.
Part: STRUT — DAMAGED (ZONE 300) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED STRUT ON C 91, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: SKIN — DENTED (LT TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND DENTS ON LT CENTER FLAP LEADING EDGE REPAIR PERFORMED BY CUT OUT THE STRAP AND IAW SRM 57-50-00 FIG 208 WITH ONE FASTENER OMIT IAW RAS/FOK/006/2009 ISS A, APPROVED BY EA 6-5750-120226.
Part: SKIN — CHAFED (NR 1 SLAT) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS ON RT SLAT NR 1 LOWER SURFACE, RIB 23B-24 REPAIR PERFORMED BY BLEND OUT OF DAMAGE, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/048/2009 ISS A, APPROVED BY EA 6-5750-129108.
Part: FRAME — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED HOLES IN FRAME C 71, P49 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON FLOOR SUPPORT P 46 RT, C 60-63A, SPLICE REPAIR PERFORMED IAW RAS/EFW/9000152/2008 ISS A, APPROVED BY EA 6-5310-120191.
Part: BUTTSTRAP — DAMAGED (ZONE 200) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED HOLES IN STRUCTURE AT FRAME C 58, P 4-5 RT REPAIR PERFORMED BY CUT THE BUTT STRAP, INSTALL A COUPLING SHEET AND BUSHS IAW RAS/EFW/9000140/2008 ISS A, APPROVED BY EA 6-5310-120212.
Part: FAILSAFE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION IN RT FWD PAX DOOR FAIL SAFE RING. REPAIR PERFORMED BY REPLACEMENT OF FAILSAFE RING IAW RAS 70517390/041/2009 ISS A, APPROVED BY EA 6-5310-120177.
Part: BULKHEAD — DAMAGED (ZONE 200) · airframe 44,816 hrs · 16,508 cycles
FOUND TOOLING MARK AT AFT PRESSURE BULKHEAD RIM BETWEEN ME1-ME2 REPAIR PERFORMED BY BLEND OUT AND FASTENER CHANGE IAW RAS/DAHAM/4026750/2008 ISS B, APPROVED BY EA 6-5310-120178.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 37LT, C 39/40 REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION IAW RAS 70517791/007/2008 ISS A, APPROVED BY EA 6-5310-120190.
Part: PANEL — CHAFED (EMERGENCY DOOR) · airframe 44,816 hrs · 16,508 cycles
FOUND CHAFING MARKS ON EMERGENCY EXIT CROSS SHEET PANEL C 56-56A, P 14-15A REPAIR PERFORMED BY BLEND OUT THE AREA IAW RAS/EFW/9000141/2008 ISS C, APPROVED BY EA 6-5310-120165.
Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON INNER STRUCTURE OF AFT CARGO DOOR REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW RAS/DAHAM/4026773/2008 ISS A, APPROVED BY EA 6-5230-129111.
Part: DOOR FRAME — DENTED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND DENT AND SCRATCH IN FUSELAGE DOOR CUT OUT FRAME, C 59A. REPAIR PERFORMED BY CUT OUT THE DAMAGED FRAME AND INSTALLING FRAME COUPLING IAW DRAWING R539-70138, APPROVED BY RAS /EFW/9000148/2008 AND EA 6-5310-120181.
Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 2RH, C 84 REPAIR PERFORMED BY BLEND OUT IAW, RAS/EFW/9000153/2008 ISS A, APPROVED BY EA 6-5310-120223.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION SPOTS ON STRINGER P 51LT, C 54.3-56 REPAIR PERFORMED BY REPLACEMENT OF STRINGER PROFILE AND SPLICING IAW SRM 53-10-14 FIG 201A, APPROVED BY RAS/EFW/9000144/2008 ISS A AND EA 6-5310-120175.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION SPOTS ON STRINGER P 50LT, C 56-57. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PROFILE AND SPLICING IAW SRM 53-10-14 FIG 201A, APPROVED BY RAS/EFW/9000145/2008 ISS A AND EA 6-5310-120176.
Part: FITTING — DAMAGED (ZONE 300) · airframe 44,816 hrs · 16,508 cycles
FOUND NOTCH AT EDGE OF RUDDER ATTACH FITTING LUG RIB 25 REPAIR PERFORMED BY BLEND OUT THE NOTCH TO SMOOTH CONTOUR IAW RAS /DAHAM/4026780/2008 ISS A, APPROVED BY EA 6-5530-120180.
Part: SKIN — DENTED (ZONE 500) · airframe 44,816 hrs · 16,508 cycles
FOUND IMPACT AND 2 DENTS ON LT INNER FLAP UPPER SKIN RIB 12-13. PATCH REPAIR PERFORMED IAW. SRM 57-50-00 FIG.205
Part: FRAME — DENTED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND TOOLING MARKS AT FRAME C 74, NEAR STRINGER P 26 LT. REPAIR PERFORMED BY CUTTING OUT THE DAMAGED AREA, REWORK TO SMOOTH CONTOUR AND NDT FOR CRACKS IAW RAS/EFW/9000138/2008 ISS A, APPROVED BY EA 6-5310-120169.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON CORNER FITTING C 58. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGE ON BULK CARGO DOOR SKIN AROUND THE HANDLE. REPAIR PERFORMED BY BLEND OUT THE DAMAGE AND PERORM HFEC INSPECTION IAW RAS/DAHAM/4026839/2008 ISS A, APPROVED BY EA 6-5230-120200.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON CORNER FITTING C 58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: BEAM — WORN (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND ELONGATED HOLES AT FRAME C 74-75, STRINGER P 26 LT. REPAIR PERFORMED BY REAM UP THE HOLES, NDT FOR CRACKS AND INSTALLING BUSHINGS IAW RAS/EFW/9000143/2008 ISS A, APPROVED BY EA 6-5310-120170.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 55, C 72-73. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: SKIN — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND A FASTENER WITH TO SHORT EDGE DISTANCE IN FUSELAGE SKIN AT C 68, P 32-33 RT. DOUBLER REPAIR PERFORMED IAW RAS/EFW/9000149/2008 ISS A, APPROVED BY EA 6-5310-120183.
Part: SKIN — CORRODED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND SKIN CORROSION AND A MISPLACED HOLE AT C 38-38.1, P 29-30 RT. REPAIR PERFORMED BY CORROSION REMOVAL AND INSTALLING NEW AND OVERSIZED FASTENER IAW RAS/EFW/9000151/2008 ISS A, APPROVED BY EA 6-5310-120214.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON SKIN , C57, P 13 LT BEHIND THE LIMIT. DOUBLER REPAIR PERFORMED IAW RAS/EFW/9000154/2008 ISS A, APPROVED BY EA 6-5330-120222.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 54, C 70-71. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 45, C 71-72. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STIFFENER — CRACKED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACK IN CENTER SPAR CUTOUT IN STIFFENER, C 44, IN HOLE NR 3 REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND PERFORMING NDT IAW RAS 70517477/009/2009 ISS A, APPROVED BY EA 6-5710-120225.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 51, C 70-71. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: FITTING — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND ON MANHOLE INTEGRAL FITTING C 38 OLD TEMPORARY REPAIR (MANHOLE FITTING CHANGE) IAW RAS/DABRE/7006140/2006 ISS C. THE REPAIR WAS UPDATED IN A PERMANENT REPAIR BY SOME FASTENER CHANGES IAW RAS/DAHAM/4026700/2008 ISS B, APPROVED BY A 6-5310-120167.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON SKIN PANEL C 39-40, P 28-29 RT REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT INSPECTION IAW RAS 70517297/005/2008 ISS A.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND TOP CAP BEAM HEAVY CORRODED ON C 60 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT ON SKIN REINFORCEMENT A537-10007-206. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS /EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.
Part: RIB — DENTED (TE FLAP) · airframe 44,816 hrs · 16,508 cycles
FOUND 2 DENTS ON LEADING EDGE RIB 12-13 OF CENTER FLAP LT PATCH REPAIR PERFORMED IAW SRM 57-50-00 FIG 208.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND STRINGER COUPLING ON C 65 , P44 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND STRINGER COUPLING ON C 72 , P45 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT IN BEAM A537-10004-204. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS /EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON CROSS BEAM C 58 RT SLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 A.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORNER FITTING ON C 65 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: ATTACH FITTING — CORRODED (ZONE 400) · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018.
Part: ATTACH FITTING — CORRODED (ZONE 400) · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018, APPROVED BY EA 6-5450-120174.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON SILL BEAM C 24A-26, P 42-43 RT. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND REWORK THE HOLES IAW RAS/EFW/9000155/2008, APPROVED BY EA 6-5310-120217.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORNER FITTING C 63 LT CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P45,C 72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION IN KRUEGER FLAP SUPPORT AREA C38-38.1, P29-30 LT ON SKIN PANEL A537-76533-000. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CORROSION REMOVAL AND INSTALLING BUSHES IAW RAS/EFW/9000147/2008 ISS A, APPROVED BY EA 6-5310-120216.
Part: FAILSAFE — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND TOOLMARK AT FAIL SAFE RING FRAME C 73A - 74, P26 RT REPAIR PERFORMED BY REWORK OF TOOLMARK IAW RAS/EFW/9000156/2008 ISSUE A, APPROVED BY EA 6-5310-120203.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON PROFILE C63-64, LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FITTING — CRACKED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACK AT GANTRY 3 RT, C 49 REPAIR PERFORMED BY DOUBLER INSTALLATION IAW DRAWING R538-10581.
Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND IN KRUEGER FLAP AREA , ON WING LE A SUPPORT CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FITTING — CRACKED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND CRACK AT GANTRY 3 RT, C 49 REPAIR PERFORMED BY DOUBLER INSTALLATION IAW DRAWING R538-10581.
Part: BEAM — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
IN KRUEGER FLAP AREA, WING LE ON BEAM HEAVY CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON STRINGER P 53, C 57.1-57.2 OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW RAS/EFW/9000146/2008 ISS A, APPROVED BY EA 6-5310-120179.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION AT INNER DOUBLER C 72-73, P 42 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CROSSBEAM C 64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND IN AFT CARGO COMPARTMENT LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND IN AFT CARGO COMPARTMENT FITTING FOR ATTACHMENT OF LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND IN AFT CARGO COMPARTMENT LONGITUDINAL PROFILE C 63-64 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION SPOTS ON CROSSBEAM C 62 OUT OF SRM LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED STRINGER COUPLING AT C 19, P 50 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FITTING — CORRODED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CORNER FITTING C 65 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED SHORT CROSSBEAM C 63 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSSBEAM C 67 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLANGE — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND OVERSIZED HOLES AT UPPER FLANGE C 32 LT, C 38.1 AND C 30 RT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED LONGITUDINAL PROFILE C 66 , Y 805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSSBEAM AT C 63, Y 1100MM SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED LONGITUDINAL PROFILE C 67-69 RT AT BCD-CUT OUT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSS BEAM C 66. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED STRINGER P 44 RT, C 33-34 SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSSBEAM C 67. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND ATTACHMENT FITTING FOR CROSSBEAM C 61 RT CRACKED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FITTING — DAMAGED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED LONGITUDINAL PROFILE C 66-67 , Y-805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED STRINGER P44 , C65 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
Part: FRAME — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND ON C 73 NO GAP BETWEEN FRAME AND STRINGER REPAIR PROFILE IN AREA OF FLUSH SKIN REPAIR. REPAIR PERFORMED BY CUT THE FRAME AT C 73 BETWEEN P56LH-56RH AND REPAIR IAW SRM 53-10-13 FIG 203 AND REPLACE THE STRINGER COUPLING IAW DRAWING R539-70631.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSSBEAM C 69 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CORNER FITTING AT C 32 LT IN FORWARD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAT SRM 51-72-10.
Part: PROFILE — DAMAGED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND DAMAGED LONGITUDINAL PROFILE C 67, Y 90. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: FLANGE — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
FOUND OVERSIZES HOLES AT UPPER FLANGE C 34 LT/RT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORRODED CROSSBEAM C 61 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,816 hrs · 16,508 cycles
FOUND CORROSION ON TCAS DOUBLER C20-21 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
Part: CROSSBEAM — DAMAGED (ZONE 100) · airframe 44,816 hrs · 16,508 cycles
TO LESS EDGE DISTANCE IN CROSS BEAM COUPLING AT C 64 RT REPAIR PERFORMED BY REPLACEMENT OF 2 ANGLES IAW SRM 51-72-10.