N675FE

Part: SPAR — CRACKED (FRM 47 L33-34R) · airframe 34,164 hrs · 18,928 cycles

CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER Ï¿½CÏ¿½ HOLE PER SB: A300-57-6113(REV.01) AND DWG: R57110371(ISSUE.L) AND EA: 6-5710-T0370822 P1, TITLE: WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR HOLE C CRACK REPAIR - SB A300-57-6113. THIS IS CATEGORY C REPAIR. LIFE LIMITED SOLUTION: 6 MONTHS. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: SEAT TRACK — CORRODED (FRM 54) · corrosion level 2 · airframe 34,164 hrs · 18,928 cycles

MAIN DECK FR54-FR54.2 Y450 SEAT TRACK FOUND HEAVY CORROSION REPLACED THE MAIN DECK FR54-FR54.2 Y450 CORRODED SEAT TRACK WITH A FABRICATED PART PER DWG: A53813127(ISSUE.C00) AND A300-600F SRM51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 34,164 hrs · 18,928 cycles

CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER HOLE 165 FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER HOLE 165 PER EA: 6-5710-T0370822 P1, TITLE: WINGS Ï¿½ BASIC WING STRUCTURE Ï¿½ RH WING REAR SPAR HOLE C CRACK REPAIR Ï¿½ SB A300- 57-6113. THIS IS CATEGORY C REPAIR. LIFE LIMITED SOLUTION: 6 MONTHS. MAJOR REPAIR IAW FEDEX GMM6-2-100. ORIG SUBMISSION DATE: 10/24/2022

Part: ANGLE — DAMAGED (ZONE 800) · airframe 34,164 hrs · 18,928 cycles

COMPLY WITH EA 6-5230-T0369311 B P4, MAIN CARGO DOOR LOWER FWD CORNER CONNECTOR CLIP DAMAGE - REWORK, BY REPLACING THE CONNECTION CLIP REPLACED THE MAIN DECK CARGO DOOR LOWER FWD CORNER CONNECTION CLIP WITH A FABRICATED PART PER DWG: A52371130(ISSUE. F), DWG: A52371207(ISSUE. G) AND A300-600F SRM51-40-21 AND EA: 6-5230-T0369311 B P4. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: DOOR FRAME — CRACKED (FRM 14C S22-23R) · airframe 34,164 hrs · 18,928 cycles

RH FWD CREW DOOR - FRAME SEGMENT CRACKED AT FR14C ITEM 40 REPLACED RH FWD CREW DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299 (ISSUE.G). TRACKING EA 6-5210-T0370794 P1 RAISED AND ACCOMPLISHED. EA TITLE: DOORS - PASSENGER/CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR - RSC TRACKING. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: ENGINE — SMOKE (NR 1) · airframe 34,090 hrs · 18,892 cycles

AT CRUISE WE NOTICED SOME SORT OF SMOKE IN THE COCKPIT. DECLARED EMERGENCY AND DIVERTED TO PIT. NO SMOKE INDICATOR LIGHTS. EMERGENCY DECLARED. NR 1 ENGINE REMOVED AND REPLACE. COALESCER SOCKS REMOVED AND REPLACED & O2 SERVICED. PERFORMED ENGINE RUNS PER JRH, NO SMOKE OR SMELLS. ORIG SUB DATE: 8/19/2022

Part: DIAPHRAGM — DAMAGED (DOOR ASSIST) · airframe 33,612 hrs · 18,607 cycles

R1 DOOR EMERGENCY CYLINDER-DAMPNER FOUND AT 0 PSI. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-10-14-03-02. NOTICED PRESSURE SLOWLY DEACREASING. AFTER TEN MIN BOTTLE ONLY INDICATING 500PSI. FOUND DIAPHRAM WITH HOLE IN IT , REPLACED DIAPHRAM & O-RINGS LEAK CKS OK IAW MM 52-10-14-03-02.

Part: NONE — NONE (N/A) · airframe 33,563 hrs · 18,580 cycles

DURING DESCENT RECEIVED ENGINE 2 LOOP B FAULT ECAM MESSAGE ACCOMPANIED BY OVERHEAD INDICATION. COMPLIED WITH APPROPRIATE QRH PROCEDURE. RELEASED FOR SERVICE PER MEL : 26-12-XX CATEGORY : C EXP : 26MAR22 "MEL 26-12-XX: ENG 2__LOOP B__ - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST OF ENG FIRE WARNING SYSTEM PRIOR TO EACH DEPARTURE." LOOP TEST PER AMM 26-12-00-05-02 , NO FAULTS AT THIS TIME NO HISTORY LAST THIRTY DAYS , OK FOR SERVICE.

Part: SLIDE — FAILED (N/A) · airframe 33,459 hrs · 18,522 cycles

PDIS 675 25-60 1477 18FEB22 BOS OPEN U WHILE CLOSING THE DOOR, THE DOOR SLIDE DEPLOYED. IT SHOULD BE NOTED THAT THE FO, RAMP, AND MX FOLLOWED PROCEDURES EXACTLY. FURTHERMORE, THE DOOR WAS NOT FULLY CLOSED, NOR WAS THE SLIDE ARMED (IN FACT THE DOOR WAS STILL PINNED); HENCE, THE DOOR RANDOMLY DEPLOYED. R/I 28FEB22 23:29 IND REASON CODE : INST ON A/C ''ONLY'' **NO REMOVAL** ON MPN: A25673040038009 CPN: 2514585 POS: L1 SRL: 792 TAG NBR: 9G5372 ENT BY: 353958 RPT BY:353958 FACT 28FEB22 23:29 IND INSTALLED L1 DOOR SLIDE COVER REF MM 25-61-21-04. REVERSED MEL PROCEDURES. A/C OK FOR FLT. RII: 5180016

Part: LIMITER — MALFUNCTIONED (TE FLAP) · airframe 31,204 hrs · 17,125 cycles

AFTER TAKEOFF FROM PDX FLAPS SYS 1 AND 2 FAULT. FLAPS STUCK. CONFIGURATION SLATS 15 FLAPS 20 DIVERTED TO KOAK PER GOC REQUEST. RECORDED FAULT (01111) FLAPS JAM. SFCC2 RECORDED FAULT (01110) HIGH SPEED V (01110). SFCC1 AND SFCC 2 BITE TEST PASSED. FOUND LT FLAP TORQUE LIMITER INDICATOR ACTIVATED. RAN FLAPS THROUGH 2 FULLS CYCLES WHILE MOTORING ENGINE WITH NO FAULT FOUND. IAW TSM 27-50-02 STEP 3 BEGAN DRAIN AND FILL OF ACTUATORS AND SCREWJACKS. DRAINED TORQUE LIMITER OF 4.0, SERVICED TO FULL IAW AMM 12-13-27-00. DRAINED LT NR 6 SCREWJACK OF 11.0 OZ. SERVICED TO FULL IAW AMM 12-13-27-00. COMPLETED DRAIN AND REFILLED JACK SCREWS 1,2,3,4,5 AND DOWN DRIVE GEAR BOX 1,2,3,4,5 IN REF TO AMM 12-13-27. FOLLOWED FIM 27-50-02. NO FAULTS AND DEFECTS NOTED AT THIS TIME. OPERATED FLAPS WITH BOTH ENGINES RUNNING SEVERAL TIMES WITH NO FAULTS AND NOTHING FOUIND ON THE SFCCS. A/C OK FOR SERVICE.

Part: SKIN PANEL — DELAMINATED (RUDDER) · airframe 31,160 hrs · 17,098 cycles

LOWER LT SIDE RUDDER LEADING EDGE PANEL HAS DELAM. REPAIRED RUDDER PANEL IAW EA 6-5540-T0354180 AND SRM 55-41-12 AND 51-77-10.

Part: SKIN — GOUGED (LE SLAT) · airframe 31,160 hrs · 17,098 cycles

LEFT WING NR 1 SLAT LEADING EDGE UPPER SURFACE HAS GOUGE AND MULTIPLE SCRATCHES ALONG ENTIRE SLAT, FROM END TO END. REPAIRED LEADING EDGE OF LT NR 1 SLAT IAW EA 6-5750-T0354063-P1, SRM 51- 73-10, SRM 51-73-11, SRM 51-21-10, SRM 51-23-10, SRM 51-75-10, AND DWG A57863006, ISSUE C. TITLED: WINGS - FLIGHT SURFACES - LT WING NR 1 SLAT NOSE SKIN SCRATCHES. EA 6-5750-T0354063-P1.

Part: TRIM PANEL — CRACKED (NR 2 NACELLE) · airframe 31,160 hrs · 17,098 cycles

NR 2 ENGINE PYLON INBOARD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.

Part: PLATE — CRACKED (NR 1 PYLON) · airframe 31,160 hrs · 17,098 cycles

NUMBER 1 PYLON INBD FISH PLATE CRACKED. REMOVED FISH PLATE ON NR 1 PYLON INBD SIDE IAW SRM 51-40-21. LOCATED AND DRILLED NEW FISH PLATE PO 962545.4 AND SHIM PO 972481.1 IAW SRM 51-40-44 AND DWG A54612371 ISSUE B, ASSEMBLED FISH PLATE AND SHIM IAW SRM 51-40-21 AND DWG A54612121 ISSUE N. INSTALLED FISH PLATE ON NR 1 PYLON INBD SIDE IAW SRM 51-40-21 AND DWG A54612121 ISSUE N.

Part: COVER — CRACKED (ZONE 400) · airframe 31,160 hrs · 17,098 cycles

#2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.

Part: TRIM PANEL — CRACKED (NR 2 PYLON) · airframe 31,160 hrs · 17,098 cycles

NUMBER 2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW SRM 51-40-21 AND DWG A54515187, ISSUE E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

MAIN CABIN SEAT TRACK AT -Y953, BETWEEN FR 56 AND FR 57, HAS CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-16 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE, UPPER SURFACE IS CORRODED AT FRAME 30, LOCATION AT APPROXIMATELY -Y 2425.7. REMOVED DAMAGE IAW SRM 51-73-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, WITH A MAX MATERIAL REMOVED OF .024". REPAIRED SEAT TRACK IAW SRM 53-10-16, REPAIR 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

WHILE ACCOMPLISHING TASK CARD 53309364 RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 29 AND 30 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIG 208. ALODINED AND PRIMED PARTS AND REPAIRED AREA IAW SRM 51-21-10. TOPCOATED REPAIR AREA IAW SRM 51-75-10.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 31,160 hrs · 17,098 cycles

MAIN GEAR WELL FLOOR PANEL 147BF IS DELAMINATED. REPAIRED FLOOR PANEL 147BF BY FABRICATION IAW SRZ-25-005 REV: R.

Part: RIB — CRACKED (TE FLAP) · airframe 31,160 hrs · 17,098 cycles

LEFT HAND WING CENTER FLAP SHOWING INDICATION AT RIB 27 AFT CRACKED. REPAIRED LEFT CENTER FLAP RIB 27 IAW SRM 57-50-00 PG 203 AND PG 220 AND EA 6-5750-T0354210-P1.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 231GG HAS PUNCTURES. FABRICATED NEW FLOOR PANEL 231GG PER SRZ-25-005 REV R.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

ATTACHING ANGLE FOR CUSP WEB JUST AFT OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED ANGLE PER AIRBUS DWG A53981418 ISSUE K

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 232SG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 231FF HAS PUNCTURES REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

CUSP WEB ON AFT SIDE OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED WEB PER AIRBUS DWG A53981360 ISSUE K

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 232WG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005

Part: CROSSBEAM — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

CENTER CABIN BELOW FLOOR OVER WING L/H SIDE C44 TRACK SUPPORT GOUGED (STREAMER) REMOVED AND REPLACED CROSSBEAM PER AIRBUS DWG A53812846 ISS. A.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 231YG IS MISSING EDGE FILL FABRICATED NEW FLOOR PANEL PER FEDEX SRZ-25-005 REV R AND PART MARKED NEW PANEL PER FEDEX GMM 07-0-1001

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 31,160 hrs · 17,098 cycles

(PARTS RACK) FLOORBOARD 261PF IS BROKEN ON THE EDGE FABRICATED NEW FLOOR PANEL 261PF IAW FEDEX SRZ 25-005 REV - R, PART MARKED PER FEDEX GMM 07-0-1001

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 33 AND 34 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIG 208. ALODINED AND PRIMED PARTS AND REPAIR AREA IAW ARM 51-21-10. TOP COATED REPAIR AREA IAW SRM 51-75-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 30 AND 31 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12 FIG 208. ALODINED AND PRIMED PARTS AND REPAIR AREA IAW SRM 51-21-10. TOP COATED REPAIR AREA IAW SRM 51-75-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS APPROX 7" FWD OF FRAME 35 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIG 208. ALODINED AND PRIMED PARTS AND REPAIR AREA IAW SRM 51-21-10. TOP COATED REPAIRED AREA IAW SRM 51-75-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

WHILE ACCOMPLISHING TASK CARD 53309364, RE- INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 32 AND 33 AND STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIG 208. ALODINED AND PRIMED PARTS AND REPAIRED AREA IAW SRM 51-21-10. TOP COATED REPAIRED AREA IAW SRM 51-75-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,160 hrs · 17,098 cycles

FORWARD CARGO PIT, INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW RT OUTBOARD ROLLER TRACK IS CRACKED ON AFT UPPER CORNER. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW OUTBOARD ROLLER TRACK IAW SRM 51-40-21 AND DWG 14A53778347.

Part: POWER SUPPLY — INOPERATIVE (ESCAPE SLIDE) · airframe 28,302 hrs · 15,460 cycles

PRIOR TO PUSHBACK, RIGHT SLIDE INDICATION WILL NOT SHOW ARMED. TROUBLESHOT IAW ASM 52-73-00. REMOVED AND REPLACED THE AUTONOMOUS POWER SUPPLY IAW MM 52-73-18-04, AND 52-73-00-05-02. OPS CHECKED GOOD.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 241GF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GF ON T17/1291767 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR P/N FX-B5327048001600.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 252NH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 252NH P/N FX-B5327027500300 ON T17/1291764 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 241GJ FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GJ P/N FX-B5327062002000 ON T17/1291773 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 251TH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 251TH P/N FX-B5327027700200 ON T17/1291751 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 252GF FLOOR PANEL BROKEN. FABRICATED 252GF FLOOR PANEL P/N FX-B5327027300000 ON T17/1291843 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 241TH FLOOR PANEL BROKEN. FABRICATED 241TH FLOOR PANEL P/N FX-B5327060000200 ON T17/1291847 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 241RJ FLOOR PANEL BROKEN. FABRICATED 241RJ FLOOR PANEL P/N FX-B5327062400000 ON T17/1291849 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 241FJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX- -B5327062003200 ON T17/1291757 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (241FJ).

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 251BH FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX-B5327028700200 ON T17/1291842 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (251BH).

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 27,673 hrs · 15,110 cycles

MDCC 242KK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242KK P/N FX-B5327063600000 ON T17/1291838 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 27,673 hrs · 15,110 cycles

CROSSBEAM CRACKED IN 2EA PLACES FR41 -Y450 TO -Y953 RT. REMOVED AND REPLACED CROSSBEAM AT FR41 BETWEEN SEAT TRACKS -Y450 TO -Y953 IAW SRM 51-40-21. MAJOR REPAIR.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,673 hrs · 15,110 cycles

DUMMY SEAT TRACK LT NR 4 AT FR 38.2 TO FR40 FAILED GAP CHECK. REMOVED DUMMY SEAT TRACK CRACKED AT LT NR 4 FR38.2 TO FR40. LOCATED AND DRILLED NEW DUMMY SEAT TRACK AND INSTALLED IAW SRM 51-40-44 AND SRM 51-40-21. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAME 55) · corrosion level 3 · airframe 27,673 hrs · 15,110 cycles

MAIN DECK CARGO SEAT TRACK Y450 FR 55 HAS A BUILDUP OF CORROSIVE MATERIAL. REPLACED SEAT TRACK FROM FR54.2 TO FR57.5 IAW SRM 51-40-21. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16. MAJOR REPAIR.

Part: DUMMY RAIL — CRACKED (FUSELAGE) · airframe 27,673 hrs · 15,110 cycles

DUMMY SEAT TRACK LT NR 5 AT FR 54 TO FR54.2 FAILED GAP CHECK. UPON REMOVAL OF LT NR 5 DUMMY SEAT TRACK AND 3EA FLOOR SUPPORTS FOUND DUMMY SEAT TRACK CRACKED. REMOVED AND REPLACED LT NR 5 DUMMY SEAT TRACK FR 54 TO FR54.2 AND REINSTALLED 3EA FLOOR SUPPORTS IAW SRM 51-40-21. MAJOR REPAIR.

Part: DUMMY RAIL — CRACKED (FUSELAGE) · airframe 27,673 hrs · 15,110 cycles

DUMMY SEAT TRACK RT NR 5 AT FR38.2 TO FR40 FAILED GAP CHECK. UPON REMOVAL OF RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 FOUND CRACKED. NO ESTABLISHED LIMITS PER SRM. REMOVED AND REPLACED RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 IAW SRM 51-40-21. MAJOR REPAIR

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 27,673 hrs · 15,110 cycles

MAIN DECK BETWEEN FRAME 57 TO FRAME 57.1 Y 1959. SEAT TRACK HAS GOUGE ON CROWN. CLS ATTACHED AT DAMAGE LOCATION FR57 - FR57.1 Y1959 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 204. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201 USING A53274005-SFS-. MAJOR REPAIR

Part: DOOR — UNKNOWN (R1) · airframe 27,165 hrs · 14,792 cycles

R1 DOOR SLIDE WILL NOT ARM. RAN A R1 DOOR SLIDE ARMING TEST AND TEST OF THE ASPSU IAW MM 25-61-20-06-01 AND 52-73-00-05-02. ALL CHECKS WERE NORMAL.

Part: SWITCH — STICKING (EMERGENCY LIGHTS) · airframe 26,753 hrs · 14,562 cycles

L1 DOOR EMERGENCY TEST SWITCH (25WL) STICKS IN THE TEST POSITION. REMOVED AND REPLACED THE SWITCH IAW SMP. SYSTEM OPS CHECKED GOOD IAW MM 33-51-00-05. ACFT OK FOR SERVICE.

Part: NOT REPORTED — MALFUNCTIONED (RUDDER SYS) · airframe 26,004 hrs · 14,095 cycles

AS WE LOST A/S THE RUDDER STARTED PULSING LT & RT. NO RUDDER LIMIT LIGHTS ILLUMINATED. IT DAMPED AS WE SLOWED & DESCENDED. NR 2 YAW DAMPER WAS ENGAGED. WE HAD KICKED AUTOPILOT OFF AT THIS POINT, SIGNIFICANT YAWING LT & RT. PRECAUTIONARY R & R NR 2 FAC IAW MM 22-26-34-04 & NR 2 FLC IAW MM 27-23-26-04. AFS LAND TEST OPERATIONAL CHECKS NORMAL.

Part: GCU — MALFUNCTIONED (APU) · airframe 25,806 hrs · 13,977 cycles

DUE TO NR 2 GEN FAULT, STARTED APU & THEN APU GEN FAULTED. INFO ONLY, MASSIVE AMOUNT OF RAIN & LIGHTNING STRIKE TWO LEGS PRIOR. APU HAD FAULTED FIRE TRIP ON GND POWER CONTROL UNIT. R & R THE APU GEN CONTROL UNIT IAW A & B AMM CHPT 24-22-12-04. RAN APU GEN UNDER LOADS FOR 30 MINS NO FAULTS. ACFT OK FOR SERVICE.

Part: GCU — FAILED (NR 2) · airframe 25,806 hrs · 13,977 cycles

AT FL300 NR 2 GEN FAULTED, RESET FAULTED AGAIN. COMPLIED IN ECAM & QRH & PAW. FOUND NR 2 GEN GCU FAILED ON THE GPCU. R & R THE NR 2 ENG GEN GCU IAW A & B AMM CHPT 24-22-12-04. RAN THE NR 2 ENG IAW A & B JRH, NR 2 GEN. OPERATIONS CHECKED SATISFACTORY. ACFT OK FOR SERVICE.

Part: STATOR — FAILED (MLG BRAKE) · airframe 248 hrs · 13,460 cycles

AFTER TAKEOFF NR 1 BRAKE INDICATOR ROSE TO 300. DROPPED GEAR TO COOL THE BRAKES. AFTER BRAKES WHERE COOL, CONTINUED FLIGHT TO DESTINATION. REMOVED TIRE & FOUND THAT STATOR DISK HAS COME APART & WEDGED BETWEEN THE TWO ROTOR DISK. R & R BRAKE IAW 32-42-27-04. NO LEAKS NOTED. ALSO FOUND SOME DAMAGE TO THE INSIDE OF THE NR 1 TIRE RIM. REPLACED NR 1 TIRE IAW 32-41-11-04.

Part: SPAR — DAMAGED (LT WING) · airframe 246 hrs · 13,353 cycles

LEFT WING ROOT REAR SPAR SPOT FACE DAMAGED. REPAIRED IAW SRM 51-71-80. COMPLIED WITH EA 6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SPAR — DAMAGED (LT WING) · airframe 246 hrs · 13,353 cycles

LEFT WING ROOT REAR SPAR 47, RIB 1 HOLE U SPOT FACE DAMAGED. SPOTPACED THE HOLE U AT LT WING ROOT SPAR IAW SRM 51-71-80. COMPLIED WITH EA :6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 26-38) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 26 - 38.2, Y0. REMOVED THE CORROSION IAW SRM 51-74-10 EXCEEDED THE ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-16-101 FIG 102. CUT OUT THE DAMAGED SEAT TRACK SECTION AT FRAME 26 - 28 IAW SRM 53-10-16-201 PARA 4. WET INSTALLED THE REPAIR PARTS IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (FRAMES 36-37) · airframe 246 hrs · 13,353 cycles

LOWER FUSELAGE, FRAME 36 - 37, STRINGER 43R - 44R,SEVERAL LIGHTING STRIKE BURN MARKS ON SKIN. REPAIRED THE SKIN IAW SRM 53-10-12 FIG 208. INSTALLED THE DOUBLER & FASTENERS ON REPAIRED PART IAW SRM 53-10-12 FIG 208. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 54.3 - 58, Y-450. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.

Part: RIVET — CORRODED (FUSELAGE) · airframe 24,648 hrs · 13,353 cycles

AGEING INSPECTION, EXISTING REPAIR ON MDCC SEAT TRACK BETWEEN FRAME 65 - 69, Y0 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND THE REPAIR CONFORMED TO SRM 53-10-16 FIG 201 EXCEPT MINOR DEVIATION. NO CHAMFER EDGES, MOREOVER, SOME RIVETS CORRODED. REPORTED TO ENGINEER. REPLACED THE CORRODED RIVETS, CHAMFERED THE EDGES & RESTORED FINISH IAW SRM 53-10-16 FIG 201 VIEW B. EO 6-5100-7-5000 D EOCN D1 PART 1 WAS COMPLETED. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 126.

Part: FITTING — LOOSE (PYLON TO WING) · airframe 24,648 hrs · 13,353 cycles

RIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND INBD LUG BUSHING LOOSE. REPAIRED IAW AMM 54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FRAMES 26-38) · airframe 24,648 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED FRAME 26 - 38.2, Y-1959. REMOVED THE CORROSION IAW SRM 51-74-10. CRACK WAS FOUND AND WAS OUT OF ALLOWABLE IAW SRM 53-10-16-101. CUT OUT SEAT TRACK. REPAIRED IAW SRM 53-10-16 FIG 201. THIS REPAIR WAS CATEGORY "A". MAJOR REPAIR IAW GMM 6-2-100.

Part: FITTING — LOOSE (PYLON TO WING) · airframe 24,648 hrs · 13,353 cycles

LEFT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REMOVED THE BUSHING IN REPAIR AREA IAW SRM 51-72-20. RE-BORED THE RIB 12 FITTING WITHOUT EXCEED 62.23MM IAW AMM 54-51-72-08-02. INSTALLED THE BUSH IAW AMM 54-51-72-08-02. REBORED THE BUSH IAW AMM 54-51-72-08-02. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.

Part: FITTING — LOOSE (PYLON TO WING) · airframe 24,648 hrs · 13,353 cycles

RIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REPAIRED IAW SRM 51-72-20, AND AMM54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (TE FLAP) · airframe 24,648 hrs · 13,353 cycles

AGEING INSPECTION, EXISTING REPAIR ON LT WING MID FLAP UPPER SKIN RIB 13 - 15 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 205. MOREOVER WORN MARKS WERE ALSO ON EXISTING REPAIR DOUBLER, REPORTED TO ENGINEER. REMOVED THE EXISTING REPAIR DOUBLER & REPAIRED AGAIN SRM 57-50-00 FIG 205 & COMPLETED. EO 6-5100-7-5000 D EOCN D1 PART 1 WAS COMPLETED. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 126.

Part: ADAPTER — WORN (FRM 32 FLOORBEAM) · airframe 246 hrs · 13,353 cycles

MDCC FLOORBEAM ADAPTOR WORN, FRAME 32 BETWEEN Y1456 & Y1959. REMOVED THE DAMAGED ADAPTER IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (TE FLAP) · airframe 24,648 hrs · 13,353 cycles

AGEING INSPECTION, EXISTING REPAIR ON RT WING INBD FLAP UPPER SKIN RIB 11 - RIB 13 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 206. WORN MARKS WERE ALSO FOUND ON EXISTING REPAIR DOUBLER, REPORTED TO ENGINEER. REMOVED THE EXISTING REPAIR DOUBLER & REPAIRED AGAIN IAW SRM 57-50-00 FIG 206 & COMPLETED. EO 6-5100-7-5000 D EOCN D1 PART 1 WAS COMPLETED. REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 126. THE FIRST INSPECTION THRESHOLD WAS 49100 FLIGHT CYCLES AFTER REPAIR EMBODIMENTS. THE REPETITIVE INSPECTION INTERVAL & METHOD WERE TBD. TRACKING EA 6-5750-T0316689 ISSUED & COMPLETED.

Part: SEAT TRACK — CORRODED (FRAMES 76-77) · airframe 246 hrs · 13,353 cycles

MDCC FRAMES 76 - 77, Y79.0 SEAT TRACK CORRODED. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FRAME 73 - 77 IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100. .

Part: SEAT TRACK — CORRODED (FRAMES 40-42) · airframe 246 hrs · 13,353 cycles

MDCC SEAT TRACK CORRODED ,FRAMES 40 - 42, Y-1456. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 RT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOORBEAM — CRACKED (FRAME 32) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 32, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 212. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM6-2-100.

Part: FLOORBEAM — CRACKED (FRAME 64) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 64 Y-112 FLOORBEAM CRACKED. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211, NO CRACK FOUND. REPAIRED THE FLOORBEAM IAW SRM 53-10-15 FIG 211. WET INSTALLED THE REPAIR PARTS IAW SRM 53-10-15 FIG 211. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: REPAIR — DAMAGED (TE FLAP) · airframe 24,648 hrs · 13,353 cycles

AGEING INSPECTION, EXISTING REPAIR ON RT INBD FLAP LE SKIN RIB 12A - 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 57-50-00 FIG 208. HOWEVER, DENTS & NICKS WERE FOUND ON EXISTING REPAIR INSERT. REPORTED TO ENGINEER. REMOVED THE DAMAGED REPAIR INSERT & REPAIRED AGAIN IAW SRM 57-50-00 FIG 208 & COMPLETED. EO 6-5100-7-5000 D EOCN D1 PART 1 WAS COMPLETED. THE REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 126. THE FIRST INSPECTION THRESHOLD WAS 51000 FLIGHT CYCLES AFTER REPAIR. THE REPETITIVE INSPECTION INTERVAL & METHOD WERE TBD.

Part: ADAPTER — CRACKED (FRAME 59) · airframe 246 hrs · 13,353 cycles

MDCC FLOORBEAM ADAPTOR CRACKED, FRAME 59 BETWEEN Y-953 & Y-1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: ADAPTER — WORN (FRM 30 FLOORBEAM) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE CROSSBEAM ADAPTOR WORN, FRAME 30 BETWEEN Y1456 & Y1959. REPLACED THE DAMAGE ADAPTOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: ADAPTER — CRACKED (FRAME 62) · airframe 246 hrs · 13,353 cycles

MDCC FLOORBEAM ADAPTOR CRACKED, FRAME 62 BETWEEN Y953 & Y1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. FABRICATED THE NEW ADAPTER IAW DWG A53278288. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM6-2-100.

Part: ADAPTER — CRACKED (FRAME 67) · airframe 246 hrs · 13,353 cycles

MDCC FLOORBEAM CRACKED, FRAME 67 BETWEEN Y1456 & Y1959. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211. PERFORMED HFEC INSPECTION TO THE CUT OUT IAW NTM 51-10-08. NO CRACK FOUND. FABRICATED THE REPAIR ANGLE & FILLER SRM 53-10-15 FIG 211. WET INSTALLED THE REPAIR ANGLE, FILLER & ADAPTER IAW SRM 53-10-15 FIG 211. THE REPAIR WAS CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 71-72) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 71 - 72, Y124.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 ,CRACK FOUND .CUT AND REMOVED THE CORROSION ON SEAT TRACK SECTION FOR FR68-FR69 .PER SRM 53-10-16 FIG 201. MADE THE REPAIR SPLICE AND SEAT .TRACK PER SRM 53-10-16 FIG 201. DRILLED THE FASTENER HOLES PER SRM 53-10-16 FIG 201. WET INSTALLED THE REPAIR SPLICE SEAT TRACK AND FASTENERS IN REPAIR AERA PER SRM 53-10-16 FIG201. THIS REPAIR CATEGORY IS "A". MAJOR REPAIR IAW GMM6-2-100.

Part: FLOORBEAM — CRACKED (FRAME 31) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 31, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 212. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 70-71) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 70 - 71, Y0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 74-75) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 74 - 75, Y-45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 40-45) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 40 - 45, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED THE SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 LT SIDE UPPER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0316343 PT1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 71-72) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 71 - 72, Y88.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FR 69-72 Y852.4. PER SRM 51-40-21.THIS REPAIR CATEGORY IS "A" .MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 LT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 38-40) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 38.2 - 40, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 65-66) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 65 - 66, -Y95.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 70-71) · airframe 246 hrs · 13,353 cycles

MDCC FRAME 70 - 71, -Y45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21, FRAME 68 - 73, -450. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FRAMES 44-48) · airframe 246 hrs · 13,353 cycles

MDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 44 - 48, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10. THE REMOVAL WAS WITHIN ALLOWABLE IAW SRM 53-10-16 101. MINOR REPAIR IAW GMM6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 RT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 RT SIDE LOWER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 24,648 hrs · 13,353 cycles

AGEING INSPECTION, EXISTING REPAIR ON MDCC FLOORBEAM BETWEEN FRAME 28, Y-450 TO Y-953 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH EA 6-5310-101017. MOREOVER, THE EXISTING REPAIR FITTING FOUND CRACKED. REPORTED TO ENGINEER. NEW EA 6-5310-T0316542 A ISSUED & COMPLETED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12A-17) · airframe 246 hrs · 13,353 cycles

MAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y-1959 FLOOR SUPPORT CORRODED. REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW SUPPORT IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12A-17) · airframe 246 hrs · 13,353 cycles

MAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y1959 FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND DELAMINATION & REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 246 hrs · 13,353 cycles

CENTER WING JOINT AT FRAME 40 LT SIDE LOWER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.

Part: APU — SHUTDOWN (APU BAY) · airframe 22,940 hrs · 12,425 cycles

NUMBER 1 GEN INOPERATIVE DUE TO MEL. APU AUTO SHUT DOWN 30 MIN INTO FLT AT 290 RESULTING IN SINGLE GEN OPERATIONS. AFTER DESCENDING TO FL210, APU RESTARTED RAN OK RTB MEMPHIS. CLEARED FAULTS IN ECB, RAN APU IAW AMM 49-61-11-04 COULD NOT DUPLICATE FAULT. REPLACED ECB AS PRECAUTIONARY IAW AMM 49-61-11-04, OPERATIONS CHECKED GOOD.

Part: PIN — CORRODED (MLG TRUNNION) · airframe 21,477 hrs · 11,592 cycles

RT MLG AFT TRUNNION PIN HAS PITTING CORROSION UNDER PIN HEAD AROUND THE CIRCUMFERANCE. REPLACED RT MLG AFT TRUNION PIN IAW AMM 32-11-11-04, STEPS B-12-D AND D-8-(A- F).

Part: ADAPTER — CORRODED · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO FLOOR 1 EA CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACK 2R -3R CORRODED INSIDE THE SCALLOP AREA APPROX 1" SQ AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND FLOOR CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACK 2R-3R TO BE OUT OF LIMITS IAW FSRM 53-10-15, PG 104. R & R CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACKS 2R-3R IAW FSRM 51-72-10 AND 51-40-21, PARA 7.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO SEAT TRACK 2L BETWEEN FR78 AND FR79 HAS 2IN. AREA OF SURFACE OXIDATION AND 2 AREAS OF BARE METAL BETWEEN FR75 AND FR77 APPROX 8IN. AFTER REMOVAL OF SURFACE OXIDATION AREA WAS FOUND TO HAVE LEVEL 1 CORROSION AND OUT OF LIMITS IAW FSRM 53-10-16, FIG 102, PG 105. R & R SEAT TRACK SECTION IAW FSRM 53-10-16, FIG 201. REPROTECTED IAW FSRM 51-75-10. .

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO FLOOR PANEL 231EF HAS TWO CRUSHED AREAS, THE DAMAGE WAS FOUND ON REPAIR OF SEAT TRACK 4L, FR 20. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO AFT FLOORBOARD 251BH HAS TWO CRACKS AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 231NG TOP SKIN PUNCTURE APPROX .5" X .2500" AND PANEL 231TG TOP SKIN PUNCTURE APPROX .5" X .5". REPAIRED FLOOR PANEL IAW SRM 53-10-20, PARA 9(A) PG 205 AND FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 232YG CENTER TOP SKIN CRACKED APPROX 8 INCHES FWD OF THE CLEVIS ADAPTER. AFT CLEVIS AREA CRACK APPROX 4". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

AFT LEFT FLOORBOARD 251QH HAS AN 8 INCH CRACK AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242UJ TOP SKIN HAS IMPACT DAMAGE AT 5 CLEVIS LOCATIONS AND TOP SKIN CRACKING AROUND THE CLEVIS POINTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 21,477 hrs · 11,592 cycles

NR 1 ENG PYLON BOTTOM LWR SURFACE 16" FWD OF AFT END, ATTACH WEB CRACKED 3EA PLACES AT PNEUMATIC PRESSURIZATION LINE MEASURED .4", .7", AND 1.0" IN LENGTHS. FOUND CRACKS ON WEB AT NR 1 PYLON BOTTOM LWR SURFACE 16" FWD OF AFT ENDTO BE OUT OF LIMITS IAW FSRM 54-54-11 AND SRM 51-72-10, PARA 1. R & R WEB ASSY IAW FSRM 51-72-10, PGS 1-3.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO TRACK 3L AT FR 21 HAS 2 SCALLOPS DAMAGE. REPAIRED SEAT TRACK IAW EA6-5313-T0300020.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO AFT RIGHT FLOORBOARD 252UH HAS ONE 3 INCH & ONE 6 INCH CRACK AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 21,477 hrs · 11,592 cycles

AVIONICS COMPARTMENT CEILING AREA AT FR 10, -33" RT OF CENTERLINE INTERCOSTAL HAS A 1" CRACK. FOUND DAMAGE ON INTERCOSTAL TO BE BEYOND ECONOMICAL REPAIR IAW FSRM 51-72-10, PG 1. R & R INTERCOSTAL WEB ON AVIONICS COMPARTMENT CEILING AREA AT FR 10 -33" RT SIDE IAW A FSRM 51-40-21, PAR 7. REPROTECTED FASTENERS AND AREA IAW FSRM FSRM 51-75-10, PG 201.

Part: FLOORBOARD — CRACKED (MAIN CARGO) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO FLOORBOARD 242PH HAS A 4 INCH CRACK AT CLEVIS CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO FLOORBOARD 251BH HAS 2 CRACKS 4 & 6 INCHES AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 231AH HAS TWO AREAS OF CRUSHED CORE DAMAGE AT THE CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO AFT RT FLOORBOARD 252VF HAS TWO CRACKS 8 INCHES LONG AT CLEVIS CUTOUTS. FABRICATED, AND INSTALLED NEW FLOORBOARD IAW AMM 53-10-25-04-02 AND IAW DWG SRZ-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO FLOOR PANEL BETWEEN FR 30 AND FR32 AND SEAT TRACKS 4L & 5L IMPACT DAMAGE APPROX 30 SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242EK CRUSH AT 2 CLEVIS ADAPTER FABBED FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242QJ HAS CRUSH CORE DAMAGE AT ALL CLEVIS ADAPTER AREAS AND TOP SKIN CRACKED APPROX 90 PERCENT OF THE PANEL. PANEL FWD TEFLON MISSING. FABRICATED REPLACEMENT PANEL WITH TEFLON STRIPS IAW DWG SRZ-25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242RG HAS CRUSH DAMAGE AT CLEVIS AND METAL STRIP ON PANEL CHAFED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242SF TOP SKIN HAS CRUSH DAMAGE AT THE CLEVIS AND TOP PLY CRACK APPROX 12". PANEL FWD TEFLON MISSING AND AFT TEFLON MISSING. FABRICATED REPLACEMENT PANEL WITH TEFLON STRIPS IAW DWG SRZ-25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

FLOOR PANEL 242ZJ IMPACT DAMAGE AT 3 CLEVIS ADAPTER. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 21,477 hrs · 11,592 cycles

MDCC SEAT TRACK 4L AT FRAME 20 HAS 3 SCALLOP DAMAGE. REPAIRED SEAT TRACK IAW EA6-5313-T0300020.

Part: WEB — CRACKED (ZONE 300) · airframe 21,477 hrs · 11,592 cycles

INSIDE TAIL SECTION BETWEEN FR 86 & FR 87 ON STR 33R, WEB HAS 1" CRACK. R & R WEB AND STRAP ON INSIDE TAIL SECTION BETWEEN FR 86 AND FR 87, STR 33R IAW SRM 51-72-10, PG 1 -3.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 21,477 hrs · 11,592 cycles

SEAT TRACK 3R, BETWEEN FR 57.1 AND 57.2, HAS A 4 INCH AREA OF SURFACE OXIDATION. REMOVED CORROSION IAW SRM 51-74-10 PG 209 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102, PG 105. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED NEW SEAT TRACK SECTION WITH TWO REPAIR SPLICES AND INSTALLED IAW SRM 53-10-16 FIG 201. REPROTECTED AREA IAW SRM 51-21-10 AND 51-75-10.

Part: CARGO TRACK — CORRODED (MAIN DECK) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO TRACK BETWEEN FR 64- 72 HAS TEN AREAS OF CORROSION ON LOWER SURFACE OF SCALLOPS AND EXTEND UNDER THE SCALLOPS 20 SQUARE INCHES. REMOVED LIGHT CORROSION. FOUND NINE AREAS TO BE WITHIN LIMITS IAW SRM 53-10-16, FIG 102, PG 105. FOUND ONE AREA TO BE OUT OF LIMITS IAW FSRM 53-10-16, FIG 102, PG 105, BETWEEN FR 66 AND 67. REMOVED SEAT TRACK SECTION FROM FR 65.5 TO 68.5 IAW SRM 53-10-16, FIG 201. FABRICATED NEW SEAT TRACK SECTION AND REPAIR ANGLES AND INSTALLED SECTION AND REPAIR ANGLES IAW SRM 53-10-16, FIG 201, PG 207 AND SRM 51-40-21. REPROTECTED AREAS IAW SRM 51-23-10.

Part: ADAPTER — DAMAGED (ZONE 300) · airframe 21,477 hrs · 11,592 cycles

MAIN DECK CARGO CLEVIS ADAPTOR AT FR31 BETWEEN SEAT TRACKS 4L AND 5L HAS BROKEN OUT BETWEEN SCALLOPS, REF AMM 53-10-16-6, R & R DAMAGE CLEVIS ADAPTER FR31 BETWEEN SEAT TRACK 4L AND 5L IAW AMM 53-10-23-4. REPROTECTED AREA IAW SRM 51-75-10.

Part: GEARBOX — DIRTY (TE FLAPS) · airframe 19,495 hrs · 10,496 cycles

LOWERED FLAPS TO 20*, 5 SEC LATER RECEIVED ECAM FLAPS SYS 1 & 2 FAULT. RECYCLED, WHICH FIXED PROBLEM. THEN TRIED TO CONFIGURE FLAPS 40*, RECEIVED SAME ECAM FLAPS SYS 1 & 2 FAULT. FLAPS STUCK AT 15*/20*. REPLACED LEFT TEE GEARBOX PER AMM 27-54-14. REPLACED LEFT DUPLEX BEVEL GEARBOX PER AMM 27-54-35. CHECKED BOTH FOR SERVICING AND BOTH WERE FULL FROM SHOP. THE BEVEL GEARBOX MOUNT BOLTS WERE TORQUED AND WITNESSED PER STEP "3.C CAUTION". CYCLED FLAPS SEVERAL TIMES WITH NO DEFECTS OR LEAKS. WORK IN PROGRESS. PER MOCC REQUEST, CHECKED ALL FLAP SCREWJACKS FOR FLUID LEAKING, LOW FLUID LEVEL AND DISCOLOR OF THE FLUID. ALL FLAP GEAR JACK SCREWS ARE PROPERLY.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 19,094 hrs · 10,289 cycles

ENG 1 RT THRUST REVERSER COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE, ABOUT 1.5 INCH. REPAIR THE DAMAGE AREA WITH DOUBLER AND FASTENERS IAW DWG NR: SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ADAPTER — CRACKED (FLOORBEAM) · airframe 19,094 hrs · 10,289 cycles

TPE CLOSED RT MAIN DECK COMP'T FLOORBEAM FITTED WITH ADAPTER WAS CRACK AT FR64 AND -Y 1456 POSITION. REPLACED WITH NEW ADAPTER AND CHECK CONDITION NORMAL.REF AB6F SRM 51-40-21. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING SPOILER) · airframe 19,094 hrs · 10,289 cycles

CLOSE R LT WING SPOILER SHROUD SUPPORT SKIN CRACK ABOUT 0.75 IN BELOW NR3 SPOILER INBD EDGE. FABRICATE A NEW SUPPORT SKIN IAW DWG NR A57240194 AND INSTALL WITH FASTENERS. REF AB6F SRM 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARRIAGE — MISALIGNED (RT FLAP TRACK) · airframe 19,094 hrs · 10,289 cycles

RT WING NR5 FLAP TRACK FWD CARRIAGE UPPER BRIDGE INBD SIDE SHIM MIGRATION. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100, REPAIR CLASSIFIED AS MINOR.

Part: CARRIAGE — MISALIGNED (TE FLAP) · airframe 19,094 hrs · 10,289 cycles

LT WING T/E FLAP NR6 FRONT CARRIAGE UPPER BRIDGE OTBD SHIM EXTRUDED. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 18,559 hrs · 9,966 cycles

LOST GREEN SYS HYD PRESSURE DURING CLIMBOUT. RESERVOIR INDICATED EMPTY. FOUND NR 1 ENGINE GREEN HYD PUMP (TOP PUMP) INLET TO PYLON MANIFOLD HOSE CRACKED AND LEAKING. CREW DEBRIEF WHEN HYD PRESS WAS LOST, GREEN PUMPS TURNED OFF. LANDING GEAR MANUALLY EXTENDED HYD FLUID INDICATED POSITIVE HYD FLUID. (FLUID LEVEL POINTER IN MIDDLE BETWEEN 0 AND BOTTOM OF TOP HAT). REMOVED NR 1 ENG GREEN HYD PUMP PRESSURE LINE AND CLAMPS. INSTALLED NEW HYD PRESSURE LINE AND CLAMPS. REMOVED AND INSP'D CASE DRAIN FILTER, NO CONTAMINATION NOTED. INSTALLED NEW FILTER ELEMENT SERVICED GREEN HYD SYS & LEAK CKD WITH ELEC PUMPS, NO LEAKS NOTED. HYD LINE AND FILTER STILL REQUIRE LEAK CHECK DURING DRY MOTOR/ENG RUN.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 16,894 hrs · 9,050 cycles

IN CRUISE FLT, RECEIVED ECAM ALERT "BLUE SYSTEM LO QUANTITY." COMPLIED W/ALL ECAM PROCEDURES AND APPLICABLE QRH PROCEDURES. BLUE SYSTEM QTY INDICATOR AT RED DOT ON OVERHEAD PANEL GAUGE. FOUND BLUE SYS PRIORITY VALVE 2064 LEAKING. PART NIS IN MEM. DURING FURTHER TROUBLESHOOTING, FOUND BLUE SYSTEM HYDRAULIC PRESSURE TRANSMITTER LEAKING FROM TOP OF TRANSMITTER AROUND TOP CAP ASSY. LEAKS BOTH STATIC AND UNDERPRESSURE. PRIORITY VALVE NOT LEAKING AT THIS TIME. REMOVED AND REPLACED "BLUE" PRESSURE TRANSMITTER. REF MM 29-32-13-4. SERVICED BLUE SYSTEM HYDRAULIC PER MM. LEAK CHECK GOOD. TRANSMITTER CHECKS OK. OK FOR CONTINUED SERVICE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CORRODED. REMOVED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A5378198422200, PO 624015.1 AND A5378198423400, PO 623903.1. PART MARKED THRUST BRACKETS IAW FEDEX GMM 7-0-1001. LOCATED AND DRILLED HOLES IAW A300-600 SRM 51-40- 44. ALODINED; PRIMED AND PAINTED THE THRUST BRACKETS IAW A300-600 AMM 51-23-10-0. INSTALLED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. APPLIED CIC TO THRUST BRACKETS IAW A300-600 AMM 51-22-00-0.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CRACKED. REMOVED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A5378198422200, PO 624015.1 AND A5378198423400, PO 623903.1. PART MARKED THRUST BRACKETS IAW FEDEX GMM 7-0-1001. LOCATED AND DRILLED HOLES IAW A300-600 SRM 51-40-44. ALODINED; PRIMED AND PAINTED THE THRUST BRACKETS IAW A300-600 AMM 51-23-10-0. INSTALLED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. APPLIED CIC TO THRUST BRACKETS IAW A300-600 AMM 51-22-00-0.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 15,830 hrs · 8,473 cycles

ATTACH ANGLE ALONG FRAME 12A RIGHT IS CRACKED ON FWD SIDE APPROX 6 INCHES BELOW THE FLOOR. REMOVED ANGLE IN REF TO A300-600F SRM 51-40-21; PARA 6. RECEIVED A NEW ANGLE, PO 624972.1. LOCATED AND DRILLED IN REF TO A300-600F SRM 51-40-21; PARA 6. INSTALLED IN REF TO AIRBUS DWG A5361037801.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 TG; TOP SURFACE IS CRUSHED AFT OF FRAME 21. MATERIAL ID A 402 H 35039-003, PO 613022.1 IAW FEDEX DWG SRZ 25-005, REV F. PART MARKED NEW FLOOR PANEL IAW FEDEX GMM 7-0-1000.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD NR 251 XF IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW SRZ 25-005; REV F. PART MARKED IAW GMM 7-0-1000.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR BOARD NR 251 RT IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD 262 WF IS BROKEN. MATERIAL ID N 407 35039-003, PO 613022.1 AND FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-- 5; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD 261 UF IS BROKEN. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD NR 251 QH IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003, PO 622013.1 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7- 0-1000.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL FROM FRAME 22 TO FRAME 26, RBL 37 TO RBL 57 HAS NUMEROUS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 PF HAS BALL BEARINGS STUCK IN THE TOP SURFACE AND PUNCTURES FROM FRAME 19 TO 22; RBL 57 TO RBL 77. REPAIRED DAMAGED AREAS PER A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 GG HAS NUMEROUS PUNCTURES AND BEARINGS STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD 262 HF IS BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005, REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005, REV F. PART MARKED IAW FEDEX GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 BH AT FRAME 28; RBL 97 HAS A BROKEN CORNER. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005, REV F. MATERIAL ID A 402 H 35039-003IAW FEDEX DWG SRZ 25-005, REV F.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL NR 231 CF IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED PER A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 XG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 GG IS PUNCTURED ON THE UPPER SURFACE IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL NR 231 GH IS PUNCTURED ON THE UPPER SURFACE AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD 252 DH EDGE IS BROKEN. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 PG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 FG UPPER SURFACE IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 MSRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 CF HAS NUMEROUS PUNCTURES AND BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 YG UPPER SURFACE HAS NUMEROUS PUNCTURES AND THE AFT END IS CRUSHED AND BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 WG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED IAW A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 SG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

BALL BEARINGS ARE EMBEDDED ON THE TOP SURFACE OF PANEL NR 232 GG, MAIN CARGO DECK. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 JH UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 RG HAS PUNCTURES AND BALL BEARINGS STUCK IN THE UPPER SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 CF IS CRACKED. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H35039-003 IAW FEDEX DWG SRZ 25-005; REV F.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 HG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 GG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS AND THE EDGING COMPOUND IS MISSING FROM THE INBD CORNER. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOORBOARD NR 251 XG EDGE IS DETERIORATED. REPAIRED EDGE IAW FEDEX DWG SRZ 25-005, REV F.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 FG HAS NUMEROUS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 XG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED AREA PER A300-600 SRM 53-10-20, FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 ZG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 UG HAS BALL BEARINGS (4 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL NR 232 VH HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

FLOORBOARD PANEL NR 231 EP MAIN CABIN IS SCORED; GOUGED AND PUNCTURED. REPAIRED AREA PER A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 SG HAS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 AH HAS BELL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 DH IS WORN THROUGH THE TOP AND IS PUNCTURED. REPAIRED DAMAGED AREA IAW A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR BOARD NR 251 XH IS CRACKED. REPAIRED DAMAGED AREA IAW A300-600 SRM 51-77-11.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 FG HAS NUMEROUS PUNCTURES IN THE UPPER SURFACE FROM BALL BEARINGS. REPAIRED DAMAGED AREAS IAW A300-600 SRM 53-10-20; FIG 201.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 JG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 UG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN FLOOR PANEL 231 TG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 NG HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CARGO DECK FLOOR PANEL 232 TG HAS PUNCTURES AND BALL BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN UNDER FLOOR PANEL 231 AH AT FRAME 28; THE SUB-FLOOR PANEL IS CORRODED. FOUND TO BE OUT OF LIMITS REF A300-600 SRM 53-14-15. REMOVED PANEL NR 131 DC TO FOM. REF A300-600 SRM 51-40-21. LOCATED AND DRILLED BRACKET REF A300-600 SRM 51-40-44. BRACKET WAS INSTALLED REF A300-600 SRM 51-40-21; PARA 4-7. APPLIED CIC REF A300-600 AMM 51-22-00-0. INSTALLED PANEL 131 DC PER AIRBUS PMS 01-05-17.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN, UNDER FLOOR PANEL 231 BH; THE SUB-FLOOR PANEL IS CORRODED BETWEEN FRAME 29 AND FRAME 30. CHECKED THE LIMITS FOR FLOOR PANEL 231 BH SUB-FLOOR PANEL AND FOUND IT TO BE OUT OF LIMITS REF A300-600 SRM 51-74-10 AND SRM 53-14-15. REMOVED PANEL 131 NW REF A300-600 SRM 51-40-21; PARA 5. REMOVED THE SUB-FLOOR PANEL BETWEEN FRAMES 29-30 REF A300-600 SRM 51-40-21; PARA 6. LOCATED AND DRILLED BRACKET REF A300-600 SRM 51-40-44. INSTALLED BRACKET REF A300-600 SRM 51-40-44. APPLIED CIC REF A300-600 AMM 51-20-00- 0. INSTALLED PANEL 131 NW PER AIRBUS PMS 01-05-12.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

MAIN CABIN ARTICULATING SEAT TRACK RIGHT NR 6 BETWEEN FRAME 38.2 AND FRAME 40 HAS AN ATTACH HOLE THAT IS WORN OUT OF LIMITS. RECEIVED A NEW SEAT TRACK, PO 624240.1. LOCATED AND DRILLED THE NEW SEAT TRACK IAW A300-600 SRM 51-40-40. TRANSFERRED THE ATTACH CLIPS FROM THE OLD TRACK IAW A300- 600M SRM 51-40-21; PARA 7. INSTALLED THE NEW ARTICULATING SEAT TRACK IAW FEDEX A300-600 EO E6-5310-7-3322 PT1.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 15,830 hrs · 8,473 cycles

LEFT WING CENTER FLAP, UPPER SURFACE IS CHAFED BY RIVETS ON THE SPOILER SUPPORT ARM BETWEEN SPOILERS NR 3 AND NR 4.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 15,830 hrs · 8,473 cycles

GOUGED FLOOR SUPPORT FITTING AT THE MAIN CARGO DECK FRAME 41; LBL 77.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 15,830 hrs · 8,473 cycles

A GUSSET IS CRACKED AT STRINGER 26L AFT OF FRAME 79.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C77 - C78; LBL 32. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK SECTION FROM EXISTING SPLICE AND FRAME 76 10 INCHES TO FRAME 80/82 IAW FEDEX A300-600 SRM 51-40-21; PARA 7. MATERIAL ID FOR THE FABRICATION OF A NEW SEAT TRACK IS A53274005-T79511 IAW A300-600 SRM 53-18-16. FABRICATED AND INSTALLED THE NEW SEAT TRACK IAW A300-600 SRM 53-10-16; PG 208A. PART MARKED SEAT TRACK IAW FEDEX GMM 7-0-1001.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 17 (IN 3 SPOTS) REMOVED CORROSION AND CHECKED LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND SEAT TRACK TO BE OUT OF LIMITS. REMOVED OLS SEAT TRACK BETWEEN C76 AND C77 AND INSTALLED A NEW SEAT TRACK IAW A300-600 SRM 51-41-21. MATERIAL ID FOR THE NEW SEAT TRACK IS A5327400500053, PO 617932.1 IAW A300-600 SRM 53-18-16. FABRICATED A NEW SEAT TRACK IAW AIRBUS DWG A53279206218. ALODINED; PRIMED AND PAINTED IAW A300-600 AMM 51-75-10-8. PART MARKED NEW SEAT TRACK IAW FEDEX GMM 7-0-1001.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C75-C76; RBL 44. BLENDED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS PER SRM 53-10-16. REMOVED CORRODED SEAT TRACK PER SRM 51-41-21. RECEIVED NEW SEAT TRACK P/N A5327400500053, PER SRM 53-18-16. LOCATED AND DRILLED NEW SEAT TRACK PER SRM 53-10-16 AND DWG A53278295. INSTALLED SEAT TRACK PER SRM 51-41-21 AND DWG A53278295. APPLIED CIC PER AMM 51-22-00-0. PART MARKED PER GMM 7-0-1001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION AT C73-C74; RBL 62.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76 - C77; BL 00 (2 SPOTS). BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. SEAT TRACK REPLACED ON NON-ROUTINE N00576 FROM FRAMES C 73 - C 80.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 32 (IN 2 SPOTS), SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053; PO 617932.1 PER SRM 53-18-16; PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A300-600 SRM 53-10-16. INSTALLED TRACK PER A300-600 SRM 51-41-21. APPLIED CIC PER A300-600 AMM 51-22-00-0.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C78; BL00. BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. REMOVED THE OLD SEAT TRACK FROM FRAME C73 - C80 AND INSTALLED A NEW TRACK IAW A300-600 SRM 51-41-21. MATERIAL ID FOR THE NEW TRACK A5327400500053, PO 617760.1 IAW A300-600 SRM 53-18-16. FABRICATED A NEW SEAT TRACK IAW AIRBUS DWG A53279239200. ALODINED, PRIMED AND PAINTED IAW A300-600 AMM 51-75-10-8.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,830 hrs · 8,473 cycles

MAIN DECK FLOOR SEAT TRACK HAS CORROSION, C76-C77;RBL 32. IN 2 SPOTS SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053, PO 617932.1 PER SRM 53-18-16, PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A300-600 SRM 53-10-16. INSTALLED TRACK PER A300-600 SRM 51-41-21. APPLIED CIC PER A300-600 AMM 51-22-00-0. THIS SDR WAS GENERATED IN ERROR. FOR THE SDR DETAILS FOR N/R N00566 SEE SDR TRACKING NR 08-2476.

Part: SKIN — GOUGED (ZONE 600) · airframe 15,830 hrs · 8,473 cycles

RT INBD FLAP UPPER SURFACE MIDSPAN GOUGED AT 3 PLACES. BLENDED GOUGED AREAS IAW SRM 57-50-00. ALL AREAS ARE BEYOND LIMITS IAW SRM 57-50-00 FIG 101 SHEET 5. TRIMMED OUT DAMAGED AREAS OF THE SKIN & STRINGER IAW SRM 57-50-00; FIGS 205 & 206. REPAIRED AREAS IAW SRM 57-50-00; FIG 206.

Part: SKIN — DENTED (ZONE 500) · airframe 15,830 hrs · 8,473 cycles

L/W INBD FLAP LOWER SURFACE HAS NUMEROUS DENTS BETWEEN INBD END AND OUTBD END. REMOVED THE TOP COAT AT THE DENT AREAS IAW AMM 51-75-2-7. REPAIRED THE OUT OF LIMITS AREA IAW SRM 57-50-00. TOP COATED REPAIR & FILLED AREAS IAW SRM 51-23-10.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 15,830 hrs · 8,473 cycles

RIGHT WING INBD FLAP L/E IS GOUGED AT TWO PLACES. REPAIRED RIGHT WING INBD FLAP L/E SECTION IAW A300-600F SRM 57-50-00; FIG 208.

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 15,830 hrs · 8,473 cycles

BS 1091, RT OUTBD FRAME TO FLOORBEAM AFT ATTACH LINK CRACKED UPPER SURFACE. LINK WAS REPLACED ON E.O. 6-5340-7-5002 PT 5.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 15,830 hrs · 8,473 cycles

AFT CARGO DOOR CUTOUT UPPER CLOSE OUT PANEL FWD END IS DAMAGED. REMOVED DAMAGED ANGLE IAW SRM 51-40-21. REMOVED DAMAGED AREA OF SEAL PLATE IAW SRM 51-71-30. REPAIRED THE SEAL PLATE IAW SRM 51-71-31. INSTALLED THE NAS ANGLE.

Part: SKIN — GOUGED (ZONE 100) · airframe 15,830 hrs · 8,473 cycles

THE AFT CARGO DOOR CUTOUT; EXTERNAL SKIN UPPER AFT CORNER IS GOUGED. REMOVED PANEL 152 YW 7 FASTENERS (5 EACH) TO FOM IAW SRM 51-40-21. BLENDED OUT GOUGE IAW SRM 51-73-10. CHECKED LIMITS IAW SRM 53-17-12 AT INTERVALS A, B, C AND D AND WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-17-12. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-01. INSTALLED FASTENERS (5 EACH) AND PANEL 152 YW IAW SRM 51-40-21.

Part: TRANSMITTER — INACCURATE (NR 2 ENG OIL) · airframe 13,247 hrs · 7,134 cycles

LOST OIL PRESSURE ON NUMBER 2 ENGINE. PRECAUTIONARY ENGINE SHUTDOWN, AS PER QRH. SUSPECT OIL PRESS TRANSMITTER T583 AND OR INDICATOR ADDED MPN 64880-420-1, CPN 7910051 QTY 1. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE TRANSMITTER T583 PER MM 79-33-11-4-05. OIL PRESS VS CORE SPEED GOOD PER JRH. OIL LEAK CHECK GOOD. OK FOR SERVICE.

Part: HINGE — WORN (CARGO DOOR) · airframe 12,394 hrs · 6,675 cycles

MAIN CARGO DOOR PIANO HINGE WORN IN SEVERAL LOCATIONS. REMOVED AND REPLACED HINGES IAW A300-600 AMM 52-36-11-4 AND 51-72-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

FWD CARGO FLOORBEAM FWD SIDE MID SECTION IS CRACKED AT FRAME 28. FABBED & INSTALLED REPAIR DOUBLER & FILLER IAW A300-600 FREIGHTER SRM 53-10-15 & EA 6-5310-101017.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

PRESSURE BULKHEAD FR 54 DENTED 4 FASTENERS ROW UP FROM FLOOR LEVEL ABOVE LT OUTBOARD MOST ROLLER TRACK AFT CARGO PIT. REPAIRED AREA IAW EA 6-5310-100991.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK AT FS 76-79 LT 3 HAS CORROSION REF N00602. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

ZONE 240 CLS ADAPTER AT FS 47 BETWEEN NR 2 AND NR 3 RT TRACKS HAS CORROSION REF N00431. REPLACED CLS ADAPTER IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 RT NR 3 SEAT TRACK HAS CORROSION AT FS'S 40,41, 42 AND 43 REF N00403. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 53-10-16 AND 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 RT NR 3 SEAT TRACK HAS CORROSION AT FR'S 40, 41, 42 AND 43REF N00403. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 53-10-16 AND 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZONE 240 RT NR 3 SEAT TRACK HAS CORROSION AT FR 45.5, 47.5, 48.5, 49.5, 50.5 AND 51.5 REF N00535. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK RT NR 1AT FR 71 TO 73 HAS CORROSION REF N00527. REMOVED AND REPLACED DAMAGED SECTION OF TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

FOUND SEAT TRACK 3R FROM FS 19 TO FS 15 HAS CORROSION 3 AREAS REF N00531. REPLACED SEAT TRACK IAW A300-600 SRM 51-74-10 AND 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC - SEAT TRACK LT NR 4 AT FS 57.1 TO 57.2 HAS CORROSION REF N00488. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 AND 51-74-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

FOUND FWD CARGO FLOORBEAM FWD SIDE MID SECTION IS CRACKED AT FR 29 REF N00284. REPAIRED FLOORBEAM IAW EA 6-5310-100979.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK NR 1 LT AT FS 57.1 TO 57.2 HAS CORROSION REF N00492. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 53-10-16, 51-74-10 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 CLS ADAPTER AT FR 36 BETWEEN LT NR 2 AND NR 3 SEAT TRACK HAS CORROSION REF N00448. REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK AT FS 75.5 RT NR 3 HAS CORROSION REF N00603. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 53-10-16,53-20-16 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK RT NR 3 AT FR 55 TO FR 57.1 HAS CORROSION ON 3 AREAS AND AT 54.3 AND 55 REF, N00483. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 - RT NR 2 SEAT TRACK AT FS 54.3 HAS CORROSION REF N00406. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK MIDDLE SECTION AT FS 69 TO FS 71 HAS CORROSION REF N00519. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 LT NR 2 SEAT TRACK FS 42 TO FS 44 HAS CORROSION 2 LOCATION REF N00417. REMOVED AND REPLACED LT NR 2 SEAT TRACK IAW AT FS 42 TO 44 IAW A300-600 SRM 51-72-10 AND 53-10-16 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

NR 5 LT SEAT TRACK AT FS 38,36,34 AND 30.5 HAS CORROSION REF N00428. REMOVED CORROSION IAW A300-600 SRM 51-74-10 AND FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-16-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK RT NR 1 AT FS 66 TO FS 69 HAS CORROSION REF N00516. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16 AND 51-74-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

FOUND SEAT TRACK 3L AT FS 17 - FS 18 SCALLOP HAS CORROSION REF N00580. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK RT NR 2 AT FS 64 TO 65 HAS CORROSION REF N00507. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZONE 240 NR 4 LT SEAT TRACK AT FS 44.5, 43 TO 44 AND FS 40 TO 41 HAS CORROSION 4 LOCATION REF N00423. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21 AND 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZONE 240 CLS ADAPTER AT FR 37 BETWEEN LT NR 2 AND NR 3 SEAT TRACK HAS CORROSION REF N00447. REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 NR 3 LT SEAT TRACK HAS CORROSION AT FS 44.5 AND 40.5, 2 LOCATION REF N00420. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 201.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZONE 240 CLS ADAPTER AT FS 38 BETWEEN LT NR 2 AND NR 3 SEAT TRACK HAS CORROSION REF N00446. REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-73-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK MIDDLE SECTION HAS CORROSION AT FR 71-73 REF N00524. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 AND 51-74-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

SEAT TRACK NR 2R FR 19 TO FR 15 HAS 4 AREAS OF CORROSION REF N00530. REPLACED SEAT TRACK IAW A300-600 SRM 51-74-10 AND 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC SEAT TRACK RT NR 2 AT FS 71-72 HAS CORROSION REF N00526. REPAIRED SEAT TRACK IAW A300-600 SRM'S 51-40-21, 51-31-00, 53-18-16 FIG 1, 51-23-10 AND 51-23-10.

Part: BRACKET — CORRODED (CARGO BAY) · airframe 12,394 hrs · 6,675 cycles

FWD CARGO COMP BETWEEN FLOORBEAM 24 AND 25 THRUST FITTING JUST I/B OF SEAT TRACK 4L HAS CORROSION AROUND FLOORBOARD NUT PLATE REF N00154. REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

FORWARD CARGO FLOORBEAM FWD SIDE MID SECTION IS CRACKED AT FRAME 30 REF N00200. REPAIRED FLOORBEAM IAW EA 6-5310-100981.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

NR 5 LT SEAT TRACK AT FS 43 TO 44 AND 41 TO 42 HAS CORROSION 2 LOCATIONS REF N00427. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21 AND 53-10-16.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,394 hrs · 6,675 cycles

MDCC ZN 240 FLOORBEAM AT FS 30 LT SIDE CRACKED REF N00455. REPAIRED FLOORBEAM IAW EA 6-5310-100981.

Part: COMPUTER — MALFUNCTIONED (FLAP/SLATS) · airframe 12,391 hrs · 6,671 cycles

FLAP SYS 2 FAULT LIGHT ILLUMINATED ON OVERHEAD PANEL WITH ASSOCIATED FLAP FAULT ON ECAM. FOLLOWED QRH. F/O HAD NO HOOK INDICATION. COULD NOT RECOVER SYSTEM. EMERGENCY DECLARED. FOUND NR 2 SFCC FLAP FAULT SHOWING 5 FAULT BALLS = BAD SFCC. PART NIS RDU. RESET C/W. CYCLED FLAPS UP DOWN SEVERAL TIMES, CHECKED GOOD. TEST PER MM 27-51-0 0-5 GOOD. PLACED NR 2 SFCC ON MEL. COMPUTER REMOVED AND REPLACED THE NR 2 SFCC PER A300-600 MM 27-51-18-4, OPS CHECKS GOOD PER A300-600 MM 27-51-00-5, SYSTEM OK FOR SERVICE.

Part: STRUT — CRACKED (ZONE 700) · airframe 12,151 hrs · 6,529 cycles

ON FINAL APPROACH TO IND LT MAIN LANDING GEAR FAILED TO EXTEND FULLY DOWN AND LOCK. FWD PANEL GEAR HANDLE SHOWING RED DOWN ARROW, LT GEAR INDICATION SHOWS RED -UNLK-, WD GEAR PANEL INDICATION AND OVERHEAD WERE IN AGREEMENT LT GEAR NOT DOWN AND LOCKED. FLIGHT RECORDER INDICATES LATERAL LOADS NO GREATER THAN -.23 AND .22, BOTH IN ACCEPTABLE LIMITS PER AMM 05-51-44-0 PAGE 1 ITEM 2A, THE VERTICAL G'S INDICATED 1.78 THE AMM 05-51-17-0. REMOVED AND REPLACED LEFT MAIN GEAR BRACE STRUT (DOWNLOCK ACTUATOR). PERFORMED LEAK AND OPS CHECK SYSTEM OPS CHECKS NORMAL AND NO LEAKS NOTED. MM 32-31-55-4. OFF C23118-1-9.

Part: CLAMP — LOOSE (BLEED AIR) · airframe 4,621 hrs · 2,398 cycles

CLIMBING THRU 3000 FT ON NR 2 BLEED LEAK ILLUM WITH ECAM WARN. TIGHTENED LOOSE CLAMP. REMOVED AND REPLACED HOT AIR SUPPLY VALVE PER IAW A300-600 MM 21-62-11. OPS AND LEAK CK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,423 hrs · 2,301 cycles

NR 2 REVERSER PRESSURED ECAM WARNING CAME ON AT 75 KIAS T/O ROLL.

Part: THRUST REVERSER — MALFUNCTIONED (NR 2 ENGINE) · airframe 4,362 hrs · 2,275 cycles

ON T/O ROLL, ECAM WARN NR 2 ENGINE REVERSER PRESSURIZED, REJECT T/O.

Part: PRESSURE SWITCH — CONTAMINATED (NR1 T/R) · airframe 4,082 hrs · 2,102 cycles

REJECT T/O, NR 1 ENGINE REVERSER PRESSURIZED LIGHT ON AT ABOUT 69 KTS. FOUND MOISTURE IN PRESSURE SWITCH. PUT HEAT ON THE SWITCH AND DRIED OUT THE SWITCH. RAN ENGINE PER A300 JRH TO T/O POWER AND NO FAULTS NOTED.

Part: HYDRAULIC SYSTEM — LEAKING (BLUE SYSTEM) · airframe 3,867 hrs · 1,969 cycles

00-369 LOST BLUE HYDRAULIC QUANTITY ON DEPARTURE. INITIALLY HAD LEFT GEAR DOOR LIGHT ON. AFT GEAR RETRACTION FOLLOWED BY BLUE BYD SYS LOW QUANTITY.

Part: CONTROL UNIT — FAILED (BRAKE ASSY) · airframe 5,263 hrs · 2,636 cycles

00-376 NORM BRAKES FAILED ON LAND. REPLACED BRAKE SYSTEM CONTROL UNIT.