N717FD
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.
155 reports on file, 2006-05-03 – 2018-10-16.
Part: RIB — CRACKED (TE FLAP) · airframe 45,977 hrs · 40,645 cycles
X-RAY INSPECTED, LT WING CENTER FLAP RIB 27 POSN FOUND CRACKED. PER SRM 57-50-00-201 PARA 4A FIG 201 REPAIRED THE CRACKED RIB. AND PER SRM 57-50-00-201 PARA 4E FIG 205 MAKE THE SKIN REPAIR DOUBLER & WET INSTALL THE REPAIR DOUBLER. THIS REPAIR IS CAT A MAJOR REPAIR IAW GMM 6-2-100.
Part: STRINGER — CRACKED (RT WING) · airframe 45,977 hrs · 40,645 cycles
NDT INSPECTED, RT WING LOWER SKIN RIB18, STRINGER 11 WEB POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.
Part: STRINGER — CRACKED (RT WING) · airframe 45,977 hrs · 40,645 cycles
NDT INSPECTED, RT WING UPPER SKIN RIB18, STRINGER 11 POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.
Part: STRINGER — CRACKED (LT WING) · airframe 45,977 hrs · 40,645 cycles
LT WING FUEL TANK RIB18 STRINGER WEB NDT INSPECT FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5720-T0343001. MINOR REPAIR IAW GMM 6-2-100.
Part: DOUBLER — CHAFED (TE FLAP) · airframe 45,977 hrs · 40,645 cycles
EXISTING REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 WAS EVALUATED AND FOUND CHAFING DAMAGE ON REPAIR DOUBLER PER EA: 6-5750-124214. REWORK THE REPAIR PER EA: 6-5750-124214A. TITLE: WINGS - RT INBD FLAP - PREVIOUS REPAIR DOUBLER GOUGED. EO: 6-5100-7-5000 D 07 PT.1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.151.
Part: CROSSBEAM — UNKNOWN (N/A) · airframe 45,977 hrs · 40,645 cycles
EXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR27 Y-140 - Y-805 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707.THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.151.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,977 hrs · 40,645 cycles
TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y-1456 AND Y-953 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
Part: FITTING — CRACKED (FUSELAGE) · airframe 45,977 hrs · 40,645 cycles
FUSELAGE CENTER WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE "M" FOUND CRACK SIGNAL. PER EA 6-5710-167809 B PT2 REPAIR THE CRACKED "M" HOLE. THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100.
Part: CROSSBEAM — UNKNOWN (N/A) · airframe 45,977 hrs · 40,645 cycles
EXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR35 Y-140 - Y-1470 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707.THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.151.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,977 hrs · 40,645 cycles
TOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. TOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. REPAIR THE CRACKED WEB PER SRM 53-15-15-201 PARA.5.A FIG201. THIS IS B CATEGORY REPAIR. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT:24000 FC, SUBSEQUENT INSPECTION AT INTERVAL:3000FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,977 hrs · 40,645 cycles
TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,977 hrs · 40,645 cycles
TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y-450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
Part: CROSSBEAM — UNKNOWN (ZONE 100) · airframe 45,977 hrs · 40,645 cycles
EXISTING REPAIR ON AFT CARGO FLOOR CROSSBEAM AT FR56 LHS REQUIRES EVALUATION FOR CONFORMITY THE REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53-10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATALOG- A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707.THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.151.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 45,977 hrs · 40,645 cycles
EXISTING REPAIR ON FUSELAGE STRINGER BTW FR60 AND FR62 STGR51 LH REQUIRES EVALUATION FOR CONFORMITY THE REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53-10-14 FIG201 SHT1,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707.THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100 REV.151.THE INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT,THE INSPECT INTERVAL WAS TBD,INSPECT METHOD WAS TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: LIMITER — MALFUNCTIONED (SLAT SYSTEM) · airframe 45,779 hrs · 40,537 cycles
SLATS STUCK LESS THAN 15 DEGREES ON RETRACTION. SLATS SYS 1 AND 2 FAULT LIGHTS ILLUMINATED. FOLLOWED ECAM AND QRH. SFP1 SLAT POSITION REMAINED STUCK. ARRIVED AT THE GATE THE FLAPS AND SLATS WERE FULLY RETRACTED, CREW DEBRIEF STATED THAT THE SLATS RESET AFTER TOUCHDOWN. PERFORMED A BYTE CHECK OF SFCC 1 AND 2 REF TSM 27-80-00 PG 102, FOUND BOTH SFCC'S INDICATING A SLAT JAM. IN THE A/C PACK BAY, FOUND THE LT WING TORQUE LIMITER POPPED. RESET THE TORQUE LIMITER. REF TSM 27-80-02, FOUND 2L SCREWJACK TORQUE LIMITER TRIPPED. BACKLASH CHECK IS GOOD AND THE SLAT TRACKS WERE ALSO GOOD, OPERATED THE FLAPS/SLATS THROUGH FIVE FULL CYCLES WITH BOTH ENGINES RUNNING AND ALL CHECKS WERE GOOD, OK FOR SERVICE.
Part: COMPUTER — FAILED (NR 2) · airframe 45,759 hrs · 40,526 cycles
SLATS SYS 1/2 FAULTS AND SLATS STUCK BETWEEN 0 AND 15 DURING RETRACTION AFTER TAKEOFF. CYCLED SLAT/FLAP HANDLE PER QRH. SLATS WENT BACK TO 15 BUT STUCK AGAIN DURING RETRACTION. RETURNED TO AIRPORT AND SLATS AND FLAPS EXTENDED NORMALLY FOR APPROACH. SLATS RETRACTED FULLY DURING AFTER LANDING CHECKLIST. PERFORMED BITE TEST OF SFCC 1 AND 2 REF TSM 27-80-00. NO FAULTS NOTED AT THIS TIME. BOTH SFCC'S PASSED. FURTHER TROUBLESHOOTING REQUIRED. DURING TROUBLESHOOTING FOUND NR 2 SFCC FAILING BITE SELF CHECK FOR FLAP SYSTEM. R&R SFCC NR 2 AND PERFORMED BITE CHECK WITH ALL SELF CHECKS PASSING AND NO FAULT BALLS PRESENT REF AMM27-51-18-04.
Part: ADC — FAILED (NR 2) · airframe 45,731 hrs · 40,502 cycles
DURING T/O ROLL, NO AIRSPEED WAS INDICATED ON THE F/O'S PFD. REJECTED T/O AT 70 KTS. PERFORMED LEAK TEST, HELD 350 KTS FOR OVER 20 MINUTES. REMOVED AND REPLACED NR 2 ADC, OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE.
Part: PITOT TUBE — FAILED (PITOT/STATIC SYS) · airframe 45,731 hrs · 40,502 cycles
DURING T/O ROLL, FO'S PFD DID NOT DISPLAY ANY AIRSPEED. REJECTED T/O AT 65 KIAS. REMOVED AND REPLACED F/O'S PITOT TUBE REF 34-11-15-04, OPS CHECK GOOD. INSPECTED OLD PITOT TUBE ASSY AND FOUND INSECT IN TUBE. A/C OK FOR CONTINUED SERVICE.
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 45,444 hrs · 40,331 cycles
ON APPROACH, SLATS EXTENDED AND INDICATED NORMALLY. AT FLAPS 15 AND FLAPS 20 COULD FEEL A PITCH CHANGE, BUT STILL NO INDICATOR MOVEMENT. CYCLED THE FLAP HANDLE AND COULD FEEL PITCH CHANGE BUT STILL NO INDICATION. PERFORMED A GO AROUND AND INDICATOR BEGAN TO MOVE DURING GA. LEFT FLAPS AT 15/20 FOR SUBSEQUENT LANDING WITH GOOD INDICATIONS. NO CAUTIONS OR ECAMS DURING EVOLUTION. HOOK ALSO ADJUSTED WITH FLAP EXTENSION. DURING DEBRIEF AND AS INDICATED IN PDIS THERE WERE NO ASSOCIATED FAULTS WITH THE FLAP EXTENSION INDICATION THE CAPTAIN OBSERVED. COMPLIED WITH A BITE CHECK OF THE NR 1 AND 2 SFCC, WITH NO FAULTS ON FLAPS. PERFORMED A FLAP/SLAT OPS CHECK, WITH ENGINES RUNNING, NO FAULTS INDICATED ON GAUGE OR FLAPS MOVEMENT. CHECKED LT AND RT TORQUE LIMITERS AND THEY WERE NOT TRIPPED. NO HISTORY FOR FLAPS FAULTS OR INDICATION. AMM 27-54-00-05 PARA 1. JRH.
Earlier reports · 2006–2017 · 136 reports
2017
Part: RUDDER — DELAMINATED (ZONE 300) · airframe 44,784 hrs · 39,974 cycles
RUDDER THERMOGRAPH FAILS STEP 10 EA 6-5540-A0319362 A PT2 PREVIOUS REPAIR. REPAIRED RIGHT HAND PREVOUS REPAIR AREA BETWEEN NR 3 AND NR 4 SCREW ON TRAILING EDGE FROM BOTTOM IAW SRM 55-41-12-201 PARA 31 FIG 222, EA 6-5540-T0335547, AND TD/7037 1608/807/2017A. MAJOR REPAIR
Part: SKIN — DENTED (RUDDER) · airframe 44,784 hrs · 39,974 cycles
RUDDER OUTER LEFT SKIN APPROX 4.5FT FROM BOTTOM OF RUDDER AND APPROX 3 FT FROM THE LEADING EDGE SPAR THERE IS A DENT " BY 0.025". REPAIRED SKIN IAW SRM 55-41-12 PARA 30 FIG 219-220, AND COMPLIED WITH EA 6-5540-T0335649 CLASSIFIED AS A CAT "B" MAJOR REPAIR.
Part: TRANSMITTER — CRACKED (HYD SYSTEM) · airframe 44,109 hrs · 39,542 cycles
DURING CRUISE, FL350, ECAM WARNING WITH GREEN HYD SYSTEM LOW QUANTITY LEVEL WHICH WAS ALSO SHOWING ON HYD PAGE OF ECAM. ACCOMPLISHED QRH PROCEDURE TO INCLUDE MANUAL GEAR EXTENSION, QTY INCREASED UPON ENGINE SHUTDOWN. REMOVED AND REPLACED THE GREEN PRESSURE TRANSMITTER 17WV IAW MM 29-32-13-04, LEAK CHECKED GOOD, CHECKED PRESSURE ON ECAM GREEN PUMP READS 3600 PSI SYSTEM SHOULD READ 3000 PSI PLUS OR MINUS 200 PSI.
2016
Part: CONTROL UNIT — MALFUNCTIONED (AUTOPILOT) · airframe 43,708 hrs · 39,316 cycles
DURING CLIMBOUT AND TWICE DURING CRUISE, AIRCRAFT YAWED ABRUBTLY AND UNCOMMANDED. ALL FLT CONTROL PARAMETERS CHECKED NORMAL. SET FAULTS FCC NR 1 WITH TRANS FLAG.AND FMC 1 & 2 WITH NCD. R & R NR 1 FAC AS A PRECAUTION IAW MM 22-18-34-04 AND PERFORMED AFS/LAND TEST WITH NO FAULTS. PERFORMED AUTOPILOT OPS TEST IAW MM 22-10-00-5 PARA 1D. CHECK OF PITCH TRIM AUTOTRIM CIRCUITS WITH NO FAULTS ON PITCH TRIM NR 2 PITCH TRIM, NR 1 REMAINS DEF. IAW TSM: 27-21-00 FOR UNCOMMANDED MOVEMENT AND PERFORMED CHECKS FOR CORRECT BEHAVIOR OF AUTOPILOT YAW ACTUATOR SERVO MOTORS IAW MM 22-13-27-04.AND ASM:22-13-00 CHECKED GOOD. ACFT OK FOR SERVICE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,322 hrs · 39,089 cycles
DURING CLIMBOUT, PASSING 8000 FT LT AMBER ECAM FOR AVIONICS DOOR OPEN. RELEASED FOR SERVICE IAW MEL. VERIFIED FORWARD AVIONICS DOOR CLOSED AND LOCKED. ITEM WAS VERIFIED CLOSED, MEL ADDED, AIRCRAT DEPARTED. MEL ITEM FACT'S PER AMM 52-41-14-05-02 ADJ/TEST, NO DEFECTS NOTED.
Part: WIRE — DAMAGED (CABIN) · airframe 43,182 hrs · 39,007 cycles
AFTER BLOCK IN, SPARKS COMING FROM THE CEILING PANEL NEXT TO THE GND SERVICE PANEL. AFTER REMOVING THE FWD CEILING PANEL FWD OF THE GND SERVICE PANEL FOUND WIRES BURNT. ALSO FOUND CB`S TR2 SUPPLY & 205XP BUS BAR & 214XP & 215XP GND SERVICE BUS BAR, TERMINAL BLOCK WHERE WIRES ARE BURNT IS 5706VT. REPAIRED WIRING IAW 20-43-10, IAW 20-43-11 TO 20-43-13, PERFORMED LIGHTING TEST IAW 33-12-00-05, MCD & COURIER LIGHTING OPERATE NORMALLY.
Part: ROLLER TRAY — CORRODED (CARGO BAY) · airframe 43,056 hrs · 38,927 cycles
UPON REMOVAL OF ROLLER TRAY AT FRAME 32, FOUND HEAVY CORROSION ON TOP OF FLANGE. CHECKED DIMENSIONS L 5.0", W 1.5" NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REPAIRED UPPER FLANGE BY CUTTING & SPLICING IAW SRM 53-10-15 FIG 207. FABRICATED FLANGE ON T16 1198513 & SPLICE ON T16 1198512. CLASSIFIED AS MAJOR CAT A REPAIR.
Part: SKIN — CORRODED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
FORWARD CARGO PIT, BETWEEN FRAME 36 - 37 & STRINGERS 50 - 51 LT SIDE HAS LIGHT SURFACE CORROSION ON THE INTERNAL SKIN. ACCOMPLISHED SKIN REPAIR ON EA 6-5330-T03244564. CLASSIFIED AS A MAJOR CAT C REPAIR.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 131ZF IS DELAMINATED & BROKEN. FABRICATED FLOOR PANEL 131ZF ON T16 1196409 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 43,041 hrs · 38,914 cycles
BULK PIT FLOOR PANEL 161GF HAS DELAMINATION ON UPPER SKIN. FABRICATED FLOOR PANEL 161GF ON T16 1196098 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 132QF, HAS CORROSION AROUND FASTENER HOLES. FABRICATED FLOOR PANEL 132QF ON T16 1196402 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
AFT PIT FLOOR PANEL 151AF IS CRACKED. FABRICATED FLOOR PANEL 151AF ON T16 1196099 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,041 hrs · 38,914 cycles
MAIN CABIN FLOOR PANEL 241KF DELAMINATED. FABRICATED FLOOR PANEL 241KF ON T16 1197922 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 132JG IS DELAMINATED AROUND THE EDGES & HAS BROKEN INSERTS. FABRICATED FLOOR PANEL 132JG ON T16 1196111 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
BULK CARGO COMPARTMENT HAS CRACK ON FLOORBEAM SUPPORT LT CTR AT FRAME 66. BLENDED CORRODED AREA IAW SRM 51-10-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED CROSSBEAM IAW SRM 51-40-22, FABRICATED NEW INTERCOSTAL IAW SRM 51-40-44, INSTALLED NEW CROSSBEAM IAW SRM 51-40-22. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
MAIN CABIN RT SIDE FRAME 43 IS CRACKED, BETWEEN STRINGER 24 - 28. REMOVED FRAME 43, BETWEEN STRINGERS 24 - 28 RT IAW SRM 51-40-21. LOCATED & DRILLED NEW FRAME IAW SRM 51-40-44. INSTALLED NEW FRAME IAW SRM 51-40-21. PAINTED AREA IAW SRM 51-75-10. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
AFT PIT FLOOR PANEL 151FF IS DAMAGED. FABRICATED FLOOR PANEL 151FF ON T16 1196113 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FITTING — CORRODED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
AFT CARGO BILGE HAS CORROSION ON SHEAR CLIP A FRAME 59, STRINGER L 54. R & R SHEAR CLIP IAW SRM 51-40-21. FABRICATED SHEAR CLIP ON T16 1196435. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
AFT PIT FLOOR PANEL 152CF IS DAMAGED. FABRICATED FLOOR PANEL 152CF ON T16 1196410 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 132HG HAS PUNCTURES ON BOTTOM SIDE. FABRICATED FLOOR PANEL 132HG ON T16 1196118 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 132ZF HAS DELAMINATED EDGES, MISSING & TORN INSERTS. FABRICATED FLOOR PANEL 132ZF ON T16 1196407 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
AFT PIT FLOOR PANEL 151CF IS CRACKED. FABRICATED FLOOR PANEL 151CF ON T16 1196112 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 43,041 hrs · 38,914 cycles
BULK PIT FLOOR PANEL 161BF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 161BF ON T16 1196408 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 131RF HAS BROKEN OUT INSERT. FABRICATED FLOOR PANEL 131RF ON T16 1196100 IAW RZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 43,041 hrs · 38,914 cycles
FORWARD PIT FLOOR PANEL 131QF HAS DELAMINATION AT EDGES & PUNCTURES ON BOTTOM SIDE. FABRICATED FLOOR PANEL 131QF ON T16 1196097 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
MDC SEAT TRACK GOUGED, 5" FWD OF FRAME 57.1 & Y450. REMOVED DAMAGED AREA, AFTER REWORK L=0.26" & W=0.20, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. FABRICATED NEW SEAT TRACK SECTION FROM PN A53274005- SFS-DAP, FROM FRAME 57.1 - 58, Y450, IAW SRM 53-10-16 FIG 208. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-16 FIG 208 CLASSIFIED AS A CAT A MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 242ZJ IS CRACKED. FABRICATED FLOOR PANEL 242ZJ ON T16 1195835 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 242WH IS PUNCTURED. FABRICATED FLOOR PANEL 242WH ON T16 1196091 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 241JF IS CRACKED. FABRICATED FLOOR PANEL 241JF ON T16 1195908 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 232WG IS CRACKED. FABRICATED FLOOR PANEL 232WG ON T16 1195903 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK COMPARTMENT FLOOR PANEL 241BF CRACKED. FABRICATED FLOOR PANEL 241BF ON T16 1195955 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 232CF IS CRACKED. FABRICATED FLOOR PANEL 232CF ON T16 1195816 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 241QJ IS CRACKED. FABRICATED FLOOR PANEL 241QJ ON T16 1195906 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 242EF IS CRACKED. FABRICATED FLOOR PANEL 242EF ON T16 1195824 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251SH HAS BROKEN CORNER PIECE. FABRICATED FLOOR PANEL 251SH ON T16 1195959 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251RG IS DAMAGED. FABRICATED FLOOR PANEL 251RG ON T16 1196095 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251ZG HAS BROKEN CORNER PIECE. FABRICATED FLOOR PANEL 251ZG ON T16 1196092 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 241QF IS CRACKED. FABRICATED FLOOR PANEL 241QF ON T16 1195834 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 252HH, HAS A DAMAGED CORNER. FABRICATED FLOOR PANEL 252HH ON T16 1195960 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 242ZH IS CRACKED. FABRICATED FLOOR PANEL 242ZH ON T16 1195902 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251WH IS DAMAGED. FABRICATED FLOOR PANEL 251WH ON T16 1196096 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 241FK IS CRACKED. FABRICATED FLOOR PANEL 241FK ON T16 1195838 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 232RG IS PUNCTURED & ELONGATED HOLES. FABRICATED FLOOR PANEL 232RG ON T16 1195821 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 242GK IS CRACKED. FABRICATED FLOOR PANEL 242GK ON T16 1195904 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK PANEL 251BF IS DAMAGED. FABRICATED FLOOR PANEL 251BF ON T16 1196094 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251NG HAS BROKEN CORNER. FABRICATED FLOOR PANEL 251NG ON T16 1196093 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 43,041 hrs · 38,914 cycles
MAIN DECK FLOOR PANEL 251JF, MIDDLE PANEL HAS BROKEN CORNER. FABRICATED FLOOR PANEL 251JF ON T16 1195858 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 43,041 hrs · 38,914 cycles
MDC SEAT TRACK GOUGED, FRAME 57, -Y1959. REMOVED DAMAGE IAW SRM 51-73-10. CHECKED LIMITS= L=0.140", W= 0.406", D= 0.118", FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, TR 86778 & TR 85721. REMOVED DAMAGED SECTION IAW SRM 53-10-16 FIG 208. REMOVED 6 EACH SPLICES FOR ACCESS IAW SRM 51-40-21. LOCATED & DRILLED NEW SEAT TRACK SECTION IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK SECTION & 6 EACH SPLICES IAW SRM 51-40-21. LOCATED & DRILLED 2 EACH SPLICES IAW SRM 51-40-44, PN R5327049020000 & INSTALLED 2 EACH IAW SRM 51-40-21. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (FDEA201603170944) · corrosion level 2 · airframe 43,041 hrs · 38,914 cycles
COURIER AREA AT FRAME 18 & 19, & -Y450 SEAT TRACK HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. TREATED ALODINED, PRIMED & PAINTED IAW SRM 53-10-16 FIG 102. REMOVED CORROSION AT SEAT TRACK FLANGE FRAME 18, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS, TREATED, ALODINED & TOP COATED, INSTALLED IAW SRM 53-10-16 PAGE 236 FIG 206. REPAIR IS A CAT A MAJOR REPAIR.
Part: SENSOR — FAILED (FUEL SYSTEM) · airframe 42,862 hrs · 38,798 cycles
DURING DESCENT AT 180FL, THE ECAM SHOWED FUEL LOW LEVEL WITH THE LOW LEVEL LIGHT ON THE OVERHEAD FOR THE LT OUTER TANK. FOUND PLUG LOOSE TO THE LOW LEVEL SENSOR UPON TANK ENTRY. R & R THE LT OUTER LOW LEVEL SENSOR 605QJ.
2014
Part: WARNING SYSTEM — MALFUNCTIONED (L1 DOOR) · airframe 41,347 hrs · 37,983 cycles
L1 DOOR ESCAPE SLIDE BUZZER WILL NOT TEST. RELEASED FOR SERVICE IAW MEL 52- XX. L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYS BUZZERS INOPERATIVE. PERFORMED OPERATIONAL CHECK OF L1 DOOR EMER DOOR WARNING SYS. NO DEFECT NOTED, OPERATED NORMAL SEVERAL TIMES IAW ASM 52-73-00. ITEM CLEARED.
Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 41,273 hrs · 37,940 cycles
RIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.
Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 41,273 hrs · 37,940 cycles
LEFT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P1 WING BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,490 hrs · 37,533 cycles
AT EMPENNAGE AREA BETWEEN FRAME 86 & FRAME 87, STRINGER 34L UPPER ANGLE CRACKED. REMOVED WEB & UPPER ANGLE IAW SRM 51-40-21, NO DAMAGE ON WEB NOTED. FABRICATED NEW ANGLE IAW DRAWING 53986751, MAT 2024-T3, 032C BATCH 0002526114. LOCATED & DRILLED, TREATED & PRIMED, APPLIED TOPCOAT TO NEW ANGLE IAW SRM 51-40-44, 51-21-10, 51-75-10. PART MARKED ANGLE IAW 7-0-1001. INSTALLED NEW ANGLE TO WEB & INSTALLED WEB IAW SRM 51-40-21. APPLIED TOPCOAT TO FASTENERS IAW SRM 51-75-10.
Part: BULKHEAD — CORRODED (FRAME 39) · corrosion level 2 · airframe 40,490 hrs · 37,533 cycles
COMPARTMENT AFT OF FWD CARGO BAY FRAME 39, FWD CORNER OF PRESSURE BULKHEAD CORRODED. PERFORMED REPAIR IAW DWG R53810795 & R53810796 IAW EA 6-5310-T0304935.
Part: INTERCOSTAL — BENT (FRAMES 84-85) · airframe 40,490 hrs · 37,533 cycles
COMPARTMENT INTERIOR INTERCOSTAL ANGLE BENT AT STRINGER 33L BETWEEN FRAMES 84 - 85. REMOVED DAMAGED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED NEW ANGLE IAW T13 1039785 & SRM 53-19-18. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.
Part: INTERCOSTAL — BENT (FRAMES 85-86) · airframe 40,490 hrs · 37,533 cycles
COMPARTMENT INTERIOR INTERCOSTAL BENT AT STRINGER 33L BETWEEN FRAMES 85 - 86. REMOVED DAMAGED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED NEW ANGLE STRAP IAW T13 1039628 IAW SRM 53-19-18. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.
Part: INTERCOSTAL — BENT (FRAMES 86-87) · airframe 40,490 hrs · 37,533 cycles
COMPARTMENT INTERIOR INTERCOSTAL ANGLE BENT AT STRINGER 34R BETWEEN FRAMES 86 - 87. REMOVED DAMAGE ANGLE IAW SRM 51-40-21. FABRICATED PART IAW T13 1040084. INSTALLED ANGLE IAW SRM 51-40-21.
Part: INTERCOSTAL — CRACKED (FRAMES 86-87) · airframe 40,490 hrs · 37,533 cycles
COMPARTMENT INTERIOR INTERCOSTAL ANGLE CRACKED & BENT AT STRINGER 33R BETWEEN FRAMES 86 - 87. REMOVED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED INTERCOSTAL ANGLE IAW T13 1039629 & T131039784. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.
Part: STRAP — BENT (FUSELAGE) · airframe 40,490 hrs · 37,533 cycles
THIS COMPARTMENT INTERIOR INTERCOSTAL RIB BENT AT STRINGER 33R BETWEEN FRAME 85 - FRAME 86. R & R INTERCOSTAL RIB STRAP, FABRICATED ON T13/1039630 BATCH 0002540969 AT STRINGER 33R BETWEEN FRAME 85 - FRAME 86 IN THIS COMPARTMENT IAW SRM 51-40-21. TOP COATED FASTENERS IAW SRM 51-75-10.
Part: SKIN — DENTED (FRAMES 96-97) · airframe 40,490 hrs · 37,533 cycles
AFT FUSELAGE SKIN BETWEEN FRAMES 96 & 97 FROM STRINGER 3 & 4R DENTED. REPAIRED IAW SRM 53-19-12 FIG 202.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 40,490 hrs · 37,533 cycles
BULK CARGO COMPARTMENT FLOOR PANEL 161AF HAS NUMEROUS DENTS & PUNCTURED IN 1 LOCATION. FABRICATED NEW FLOOR PANEL 161AF ON T13 1040702 IAW DRAWING SRZ=25-005.
2013
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,490 hrs · 37,533 cycles
STRINGER SPLICE HAS CORROSION FRAME C83, STRINGER 36R. REMOVED CORROSION L 500 INCHES, W .500 INCHES & D .045 INCHES, FOUND TO BE OUT OF LIMITS IAW SRM 53-19-14 PAGE 101. REPLACED SPLICE IAW SRM 51-40-21 & 51-40-44.
Part: SKIN — DENTED (FRAMES 6-7) · airframe 40,490 hrs · 37,533 cycles
FORWARD LOWER FUSELAGE RT SIDE DENTED BETWEEN FRAMES 6 - 7 & STRINGER 26 - 27R. REPAIRED IAW SRM 53-11-12 FIG 201. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — DENTED (FRAME 16) · airframe 40,490 hrs · 37,533 cycles
FORWARD LOWER SKIN DENTED AT FRAME 16 BETWEEN STRINGERS 33 - 34R. REPAIRED IAW SRM 53-12-12 FIG 202. REPAIR CLASSIFIED AS MAJOR.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 40,490 hrs · 37,533 cycles
BULK CARGO COMPARTMENT FLOOR PANEL 162HF HAS NUMEROUS DENTS & SEVERAL PUNCTURES. R & R FLOOR PANEL 162HF IAW SRM 51-72-10.
Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,490 hrs · 37,533 cycles
MAIN CABIN DECK FLOORBOARD BETWEEN FR 26 - FR 29 Y O IS PUNCTURED ON TOP SURFACE. R & R FLOOR PANEL IAW AMM 53-10-25-04-02. FABRICATED FLOOR PANEL IAW SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 241HK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — DAMAGED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 242EK PUNCTURED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 40,490 hrs · 37,533 cycles
AFT CARGO BAY FLOOR PANEL 152EF EDGE IS CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 106. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 241RJ CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 241LK CRACKED, FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 241TH CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 242HK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 40,490 hrs · 37,533 cycles
MAIN DECK FLOOR PANEL 241JF CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — CRACKED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 242LK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
Part: FLOOR PANEL — DAMAGED (MID CABIN) · airframe 40,490 hrs · 37,533 cycles
MID CABIN FLOOR PANEL 241AK EDGE BROKEN, FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.
2012
Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 39,162 hrs · 36,800 cycles
NR 2 ENG PYLON FWD ENGINE MOUNT FITTING INBD AFT TENSILE BOLT HOLE HAS OXIDATION AND PITTING IN ITS BORE. REAMED NR 2 ENG FWD ENG MOUNT FITTING TO CLEAN OXIDATION AND PITTING TO 0.997 IAW SRM 54-51-81. INSP HOLE FOR CRACKS IAW NTM 51-60-00. REPROTECTED BORE IAW SRM 54-51-81 STEP 2(E) PG 205. INSTALLED REPAIR BUSHING IAW SRM 54-51-81, CONFIG 2, FIG 202.
2011
Part: FRAME — CRACKED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
CABIN LT SIDE FRAME 40 TOP MOST TENSION BOLT HOLE 'A'. FOUND DAMAGED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.
Part: HINGE — CRACKED (E/E BAY) · airframe 37,996 hrs · 36,158 cycles
AVIONICS COMPARTMENT DOOR, FOUND RT HINGE CRACKED. PERFORMED REPAIR PER A300-600 SRM 52- 41-14 FIG 201 REV 75. AVIONICS COMPARTMENT DOOR REMOVED AND RE-INSTALLED AFTER REPAIR COMPLETED PER AMM 52-41-14-04 REV 52.0 AVIONICS COMPARTMENT DOOR ADJUSTMENT TEST CARRIED OUT PER AMM 52-41-14-05 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: FRAME — CRACKED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
CRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON CABIN LT SIDE FRAME 40 CENTER TENSION BOLT HOLE 'B'. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.
Part: FRAME — CRACKED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
CRACKED INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT. OPEN HOLE INSP ON CABIN LT SIDE FRAME 40 LOWEST TENSION BOLT HOLE 'C'. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: SPAR — DAMAGED (CENTER WING BOX) · airframe 37,996 hrs · 36,158 cycles
DURING ACCOMPLISHMENT OF EO6-5710-7-3305, D2, PT3 WORK STEP 6, FOUND HOLE 'A' EXISTING FASTENER HOLE DIAMETER 0.625" IS BIGGER THAN NEW FASTENER SIZE 0.562" AT CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE LT SIDE. INSTALLED NEW FASTENER PER EA 6-5710-143621. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100 REV 112.
Part: FRAME — DENTED (BS 1741 L12L) · airframe 37,996 hrs · 36,158 cycles
MAIN DECK FUSELAGE FRAME DENTED AT STA 1741, LT L12. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV112.
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
BULK CARGO FLOOR PANEL 162DF FOUND CORRODED. FLOOR PANEL REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ 25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
BULK CARGO FLOOR PANEL 162CF FOUND CORRODED. FLOOR PANEL REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ-25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 37,996 hrs · 36,158 cycles
BULK CARGO FLOOR PANEL 161CF FOUND UNDER CORRODED. REMOVED PER AMM 53-10-35 REV 52.0. NEW FLOOR PANEL FABRICATED PER DRAWING SRZ 25-011 REV D. NEW FLOOR PANEL INSTALLED PER AMM 53-10-35 REV 52.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.
Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 37,996 hrs · 36,158 cycles
AFT CARGO DOOR HANDLE FWD FRAME FOUND CORROSION. REMOVED AND NEW FRAME INSTALLED PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: FRAME — DAMAGED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING ACCOMPLISHMENT OF EO 6-5310-7-5017 A5 PART 3, HOLES A-N AT FRAME 47 LT ARE FOUND TO BE IN OVERSIZED CONDITION. REPAIRED PER EA 6-5310-143612, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: FRAME — DAMAGED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING ACCOMPLISHMENT OF EO 6-5310-7-5017 A5 PART 4, HOLES A-N AT FRAME 47 RT FOUND TO BE IN OVERSIZED CONDITION. ACCOMPLISHED REPAIR PER EA 6-5310-143612, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
AFT CARGO ROLLER TRAY AT ABOUT 140 MILLIMETER TO THE LT AND RT FROM THE MIDDLE AT FRAME 60 FOUND CORROSION AROUND FASTENER AREA. REMOVED ASSY AMM 25-52-24-04, REV 52.0. NEW TRAY REWORKED (FABRICATED) IAW DWG NR A25772926 ISSUE F. FABRICATED NEW PART, INSTALLED IAW AMM 25-52-24-04, REV 52.0 REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.
Part: FITTING — CORRODED (NR 2 PYLON) · airframe 37,996 hrs · 36,158 cycles
ENGINE NR 2 PYLON FORWARD MOUNT FORWARD LT BOLT BORE HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 6-5450-152689.
Part: FITTING — NICKED (NR 2 PYLON) · airframe 37,996 hrs · 36,158 cycles
ENGINE NR 2 PYLON ENGINE FORWARD MOUNT FORWARD RT BOLT BORE HOLE FOUND NICKED. REPAIRED AS PER EA 6-5450-152689.
Part: FITTING — CORRODED (NR 1 PYLON) · airframe 37,996 hrs · 36,158 cycles
ENG NR 1 PYLON FORWARD MOUNT FITTING LT AFT BOLT BORE HOLES FOUND WITH CORROSION. REPAIRED AS PER EA 6-5450-152690.
Part: FRAME — DAMAGED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSPECTION ON LT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE TOP 2ND HOLE DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 11TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. REPAIRED IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 8TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 49, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 10TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND 13TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 5TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 48, FOUND THE 4TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 17TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSPECTION ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 15TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 52, FOUND THE 16TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 5TH HOLE COUNT FROM THE TOP WITH THE CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REV112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC INSP ON RT REINFORCE BASES JUNCTION AT FRAMES 49, FOUND THE 5TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV112.
Part: FRAME — DAMAGED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON LT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE TOP 3RD HOLE DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HFEC HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 48. FOUND THE 5TH HOLE COUNT FROM THE TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN DURING OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 51, FOUND THE 5TH HOLE COUNT FROM TOP WITH CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 49, FOUND THE 17TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 7TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
CABIN - DURING HFEC OPEN HOLE INSP ON RT REINFORCE BASES JUNCTION AT FRAME 53, FOUND THE 13TH HOLE COUNT FROM THE TOP WITH CRACK. PERFORMED REPAIR IAW EA6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,996 hrs · 36,158 cycles
MAIN DECK - LOWER OF LAVATORY UNIT BETWEEN FRAME 11 TO FRAME 12A AT FLOOR SUPPORT, CORROSION. REMOVED AS PER SRM 51-74-10 REV 75. MATERIAL REMOVED 0.061", MATERIAL REMAINED 0.017", MATERIAL THICKNESS 0.078" AND FOUND OUT OF LIMIT AS PER SRM 53-12-15 FIG 101 REV 75. DAMAGED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: FRAME — CRACKED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT REINFORCE BASE JUNCTION AT FRAME 48 FOUND THE HOLE NR 17 FROM TOP WITH CRACKED INDICATION. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,996 hrs · 36,158 cycles
FLOOR SUPPORT BETWEEN FRAME 12A TO FRAME 13A Y953, CORRODED. REMOVED AS PER SRM 51-74-00 REV 75, MATERIAL REMOVED 0.053", MATERIAL REMAINED 0.025", MATERIAL THICKNESS 0.078" AND FOUND OUT OF LIMIT AS PER SRM 53-12-15 FIG 101 REV 75. DAMAGED FLOOR SUPPORT REMOVED AS PER SRM 51-40-21 REV 75. NEW FLOOR SUPPORT FABRICATED PER DRAWING A53612213-204 AND INSTALLED PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 37,996 hrs · 36,158 cycles
DURING HIGH FREQUENCY EDDY CURRENT INSP ON FORWARD CARGO DOOR ACTUATOR ATTACH FITTING, FOUND CRACKED. REMOVED AND NEW FITTING INSTALLED PER SRM 51-40-21 REV 75. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.
Part: FRAME — DAMAGED (ZONE 200) · airframe 37,996 hrs · 36,158 cycles
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LT REINFORCE BASE JUNCTION AT FRAME 49 FOUND THE FIRST HOLE FROM TOP DAMAGED. PERFORMED REPAIR IAW EA 6-5310-143613, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,996 hrs · 36,158 cycles
FORWARD CARGO AT ABOUT FR 38.2 STRINGER 45L FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-10-14 FIG 201 REV 75. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 37,486 hrs · 35,879 cycles
LOSS YELLOW HYD SYS PRESSURE AND QUANTITY. R & R YELLOW PRESSURE HOSE IAW SPM CHAP 20 AND AMM 12-12-29-00 .
2009
Part: PICKUP — MALFUNCTIONED (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF A300-66 MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.
Part: CONTROL UNIT — MALFUNCTIONED (FLAP/SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG. WOULD NOT RETRACT. FOUND THE FEEDBACK PPU, (FPPU) & LT WING (APPU) READING INCORRECTLY. REMOVED AND REPLACED FPPU REF MM 27-81-19-4. STILL REQUIRES RII FOR INSTALL & OPERATIONAL TEST REF 27-84-00-5. REMOVED & REPLACED LT WING APPU REF MM 27-86-11-4.
Part: PICKUP — MALFUNCTIONED (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.
Part: UNIVERSAL JOINT — FAILED (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. OPENED RT WING LOWER L/E PANELS TO INSPECT FOR FAULTS. FOUND RT WING NR 2 SLAT OTBD J/S, INBD SIDE TRANS SHAFT "U" JOINT SHEARED IN TWO. REMOVED JOINT FROM SHAFT AND PART ON MSN. NR 2 SLAT TO NR 1 SLAT CONNECTING WRAP AROUND SEAL IS TORN AND REMOVED NEEDS REPLACEMENT ON ORDER. DISCONNECTOR TRANS SHAFT AT 1ST STEADY BEARING OTBD OF NR 2 ENG PYLON. ROLLED RT WING NR 2 AND 3 SLAT UP TO 270 DEG BEFORE HITTING UP STOPS. ROLLED LT WING AND RT WING NR 1 SLAT UP TO 270 DEG BEFORE HITTING UP STOPS.
Part: SHAFT — SHEARED (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. FOUND RT WING NR 2 SLAT OTBD J/S, INBD SIDE TRANS SHAFT "U" JOINT SHEARED IN TWO. REMOVED AND REPLACED CHA1237-004A, S/N 0158, R & R FPPU REF MM 27-81-19-4. RII FOR INSTALL & OPS TEST REF 27-84-00-5. R & R LT WING APPU MM 27-86-11-4. LT PPU OFF MFG 9028A0002-01 SRL 1730 AND OFF MFG 9028A0002-01 SRL 1072.
Part: SHAFT — WORN (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. INSTALLED NEW NR 1 RT SLAT JACKSCREW AND INBD SECTION OF TORQUE TUBE WITH NEW U-JOINT REF AMM 27-84-22-4 AND SMP, STILL REQUIRES RII FOR INSTALLATION AND OPS CK.
Part: PICKUP — MALFUNCTIONED (SLATS) · airframe 34,915 hrs · 34,511 cycles
DURING FLAP/SLAT EXTENSION, SLATS STUCK BETWEEN 15 DEG AND 30 DEG WOULD NOT RETRACT. REMOVED AND REPLACED LT WING APPU REF A300-66 MM 27-86-11-4. THIS STILL REQUIRES RII FOR INSTALL AND TEST REF 27-80-00-5.
Part: JACKSCREW — UNKNOWN (TE FLAPS) · airframe 34,689 hrs · 34,389 cycles
AFTER TAKEOFF, FLAP RETRACTION, FLAPS WOULD NOT RETRACT (FROM 15/20) UNTIL AFTER LANDING. THEREBY CAUSING AN UNSCHEDULED RETURN TO CWF. TROUBLESHOT IAW TSM 27-50-02 FIG 101/102/103/104. AT ON SITE REP REQUEST SWAPPED NR`S 3/5/6 FLAP SYSTEM JACKSCREWS FROM LT WING TO RT WING, AND ALSO REMOVED AND REPLACED LT NR 4 FLAP JACKSCREW PER CUSTOMER REQUEST. ALSO REMOVED AND REPLACED LT NR 5 DOWN DRIVE SHAFT AND NR 5 LT JACKSCREW, AND RT NR 2 FLAP JACKSCREW, REMOVED AND REPLACED LT FLAP SYSTEM TORQUE LIMITER, SFCC NR 1 AND SFCC 2 COMPUTERS ALL IAW AMM 27-50-00-4; AMM27-50-21-4; AMM27-51-18-4; AMM 27-54-12/22/23/24/25/26/27/28-4 (SUSPECT BAD FLAP JACKSCREW AT NR 4 LT POSITION FROM OVERHAUL VENDOR).
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 34,686 hrs · 34,379 cycles
MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT INBD TANG CRACKED 2 IN LONG AT FR 48, BELOW SEAT TRACK 4RT. REMOVED AND REPLACED VERTICAL FLOOR SUPPORT AT FR 48 BELOW SEAT TRACK 4RT IAW A300-600 SRM 51-72-10.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 34,686 hrs · 34,379 cycles
MAIN DECK CARGO COMPARTMENT VERTCAL FLOOR SUPPORT INBD TANG CRACKED 2 IN LONG AT FR 49, BELOW SEAT TRACK 4RT. REMOVED AND REPLACED VERTICAL FLOOR SUPPORT AT FR 49 BELOW SEAT TRACK 4RT IAW A300-600 SRM 51-72-10.
2007
Part: SKIN — CORRODED (ZONE 500) · airframe 31,743 hrs · 32,804 cycles
L/T WING BOTTOM SKIN UPPER SURFACE CORROSION ADJACENT TO HYD PRESSURE LINE THROUGH HOLE. AREA WHERE HYD LINE AT WING T/E PASS THROUGH TO NR 1 PYLON. AFTER CORROSION REMOVAL, HYDRAULIC LINE PASS, THROUGH HOLES WERE FOUND TO BE ELONGATED. HYDRAULIC BULKHEAD FITTINGS WORN. REPLACED BULKHEAD 2 FITTINGS P/N A9348226020400. REPAIRED WING SKIN PASS-THROUGH HOLES REF: FED-EX EA 6-5730-102780, SEE FED-EX N/R N00656 OF W/O 00035272.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,743 hrs · 32,804 cycles
AFT PIT FLOOR SUPPORT STRUCTURE AT FR66 RBL 36R IS CORRODED. REMOVED AND REPLACED DAMAGED FLOORBEAM AT FR66 IAW FEDEX GMM 7-0-1001 AND FEDEX A300-6-SRM'S 51-40-21 PG 7 AND 51-40-21 PG24 AND AIRBUS DRAWING AS397432222.
2006
Part: SMOKE DETECTOR — MALFUNCTIONED · airframe 31,742 hrs · 32,803 cycles
ON TAXI OUT, GOT MID 1 MAIN DECK LOOP FAULT. COMPLIED WITH MEL, SELECTED AFFECTED LOOP OFF AND CONTINUED DURING CLIMB GOT MAIN DECK CARGO SMOKE WARNING PASSING FL 200. COMPLIED WITH RED ECAMS AND DURING AMBER ECAMS WARNING CEASED. CONTINUED WITH EMERGENCY RETURN AND LANDING. AFTER LANDING EMERGENCY EQUIPMENT FOUND NO EVIDENCE OF SMOKE OR HOT SPOTS. REPLACED SMOKE DETECTORS AT POSITIONS 4WU AND 22WU PER A300-600 AMM SUPP 26-19-12. POSITIONS 3WU AND 8WU REPLACED ON PREVIOUS ENTRY. ALL SMOKE DETECTORS WERE INSTALLED PER EA NR 6-2612-1 03614.
Part: PUMP — CONTAMINATED (HYD SYSTEM) · airframe 30,995 hrs · 32,402 cycles
AFTER GEAR RETRACTION GOT GREEN PUMP NR 2 LOW PRESSURE WARNING ON ECAM. COMPLIED WITH ECAM ELECTED TO RTN TO MHT AS AIRCRAFT HAD TOTAL GREEN SYSTEM FAILURE PREVIOUS FLIGHT AND GREEN SYSTEM HAD BEEN OPEN AND MAINTENANCE PERFORMED. QUANTITY APPEARED TO BE DECREASING BUT COULD NOT CONFIRM DUE TO FLUCUTIONS DUE TO GEAR RETRACTION AND EXTENSION. T/S GREEN PUMP NR 2 LOW PRESSURE LIGHT. REMOVED AND REPLACED NR 2 ENG GREEN PUMP CASE DRAIN FILTER, NO CONTAMINATION FOUND PER 29-11-36-3-01. AS PER MM 29-11-32-4-01 FOUND AIR WHEN BLEEDING PUMP. RAN BOTH ENGINES, RAN ALL PUMPS, NO LO PRESS LIGHTS OR RVSR LIGHTS ON AT ANYTIME.