N562FE

Part: INDICATION SYS — INOPERATIVE (R1 DOOR SLIDE) · airframe 97,703 hrs · 34,487 cycles

R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM INOP ON PRE FLIGHT FACT 22FEB19 20:53 MEM U REMOVED AND REPLACED REMOTE SLIDE PACK PRESS INDICATOR. TEST GOOD. A/C OK FOR SERVICE. REF AMM 25-61-03-5/25-61-01-2.

Part: LIGHT — FALSE ACTIVATION (L1 DOOR) · airframe 97,625 hrs · 34,433 cycles

L1 CABIN DOOR PRESS LIGHT ON CONTINUOUSLY CANNOT TEST. PERFORMED OPS CHECK OF L1 DOOR REMOTE PRESSURE LIGHT IAW AMM 25-61-03-5, OPS NORMAL.

Part: INDICATOR — INOPERATIVE (EVAC SLIDE) · airframe 97,311 hrs · 34,254 cycles

DURING PREFLT CK FOUND L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR LIGHT ON. L-1 DOOR EVACUATION SLIDE PUSHBUTTON INDICATOR PLASTIC COVER FOUND BROKEN. REMOVED AND REPLACED L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST PUSHBUTTON INDICATOR IAW MM 25-61-03-2. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: INDICATOR — DAMAGED (L1 DOOR) · airframe 97,311 hrs · 34,254 cycles

DURING PREFLT CK FOUND L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO- TEST INDICATOR LIGHT ON. L-1 DOOR EVACUATION SLIDE PUSHBUTTON INDICATOR PLASTIC COVER FOUND BROKEN. REMOVED AND REPLACED L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PERSS-TO- TEST PUSHBUTTON INDICATOR. OPS CHECK IS GOOD

Part: SWITCH — BROKEN (L1 DOOR) · airframe 97,280 hrs · 34,234 cycles

PUSH TO TEST SWITCH FOR ESCAPE SLIDE ON L1 DOOR BROKEN. SECURED TEST SWITCH FOR L1 ESCAPE SLIDE. OPS VERIFED NORMAL

Part: SKIN — CORRODED (ZONE 600) · airframe 97,138 hrs · 34,135 cycles

RH WING UPPER SURFACE CORROSION AROUND ONE FASTENER APPROX XORS 247 STRG 10. REMOVED CORROSION AROUND ONE FASTENER ON RH WING UPPER SURFACE AT APPROX 247 STRG 10 PER EA 8-5710-T0342473 P1.

Part: SKIN — CRACKED (TE FLAP) · airframe 97,138 hrs · 34,135 cycles

RT WING INBD FLAP UPPER SURFACE APPROX XIFH 207, TWO CRACKS AROUND FASTENERS. CONFIRMED USING NDT HFEC. DOUBLER REPAIRED PER SRM 57-10-00 FIG 85 SHEET 3 VOL 1. REF EA 8-5700-T0342609.

Part: SKIN — CORRODED (LT WING) · airframe 97,138 hrs · 34,135 cycles

RH WING UPPER SURFACE CORROSION AROUND THREE FASTENER APPX XORS 333 STRG 8. REMOVED CORROSION AROUND THREE FASTENERS XORS 333 STRG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 97,138 hrs · 34,135 cycles

AFT CARGO, CTR OF FLOOR SUPPORT (AGA3874-9) AT APPROX STA 1841 CORRODED ON L-ANGLE. REPAIRED CORRODED FLOOR SUPPORT, REF SRM 53-00-01 VOL I FIG 8, SHEET 2 AND DRAWING AGA3874 MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 97,138 hrs · 34,135 cycles

AFT CARGO COMPT, APPROX STA 1885, LONG 43L. LONG SHEAR TIE END, IS CORRORED/CRACKED. INSTALLED AS REQ NEW LONG SHEAR TIE END AT STA 1885 L43 REF DWG NFA6074.

Part: SPAR CAP — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 97,138 hrs · 34,135 cycles

LT HORIZONTAL STABILIZER XFS = 90 FRONT SPAR IB UPPER TEE CAP HAS 2" OF MINOR SURFACE CORROSION. MARKED REPAIRED UPPER FORWARD SPAR CAP ALC7082 REF SRM 55-20-00 FIG 9 SH 1 VOL I, MAJOR REPAIR.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 97,138 hrs · 34,135 cycles

MAIN CARGO DECK APPROX STA 755 LBL 27.5 SEAT TRACK HAS BROKEN LOBE. REPLACED DAMAGED SEAT TRACK FROM STATION 715 TO STATION 772 LBL 27.5 REF SRM 53-70-00 FIG 1 VOL 1.

Part: LIGHT — MALFUNCTIONED (R1 DOOR SLIDE) · airframe 95,382 hrs · 33,162 cycles

R1 ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM DOES NOT ILLUMINATE. WHILE PERFORMING DAILY CHECK FOR R1 SLIDE BOTTLE PRESSURE, FOUND BOTTLE INDICATOR LIGHT WORKING NORMALLY. CHECKED CONDITION OF WIRING AND CONNECTIONS. NO DISCREPENCIES FOUND. OK FOR SERVICE IAW AMM 25-61-03-5.

Part: STOWAGE BOX — BROKEN (COCKPIT) · airframe 94,722 hrs · 32,792 cycles

FO OXYGEN MASK STORAGE DOOR BROKE OFF. REPLACED FO'S OXYGEN MASK STOWAGE BOX PN MXP403 SN SE03777 REF MM 35-13-04-4. OPS CHECK AND LEAK CHECK GOOD.

Part: SKIN — WORN (LT WING LE) · airframe 94,139 hrs · 32,500 cycles

LEFT DROOPED LEADING EDGE ASSY HAS A DOUBLER WORN BEYOND LIMITS ON THE OUTBOARD LEADING EDGE. REMOVED AND REPLACED FILLER ON PREVIOUS REPAIR AT L/E. IAW SRM 51-31-01 VOL 2 & SRM 51-00-01 VOL 1. REPAIRED IAW SRM 57-00-01 FIG 4 VOL 1

Part: CARGO TRACK — CORRODED (BS 1830) · airframe 94,139 hrs · 32,500 cycles

AFT CARGO BAY BS 1830, RBL 28 CARGO TRACK CORRODED AT NUTPLATE. REPLACED THE CARGO TRACK IAW SRM 51-21-01 VOL II.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 94,139 hrs · 32,500 cycles

LEFT UPPER HORIZONTAL STAB FAIRING AJC7690-1 HAS CRACK IN FORMER RIB AT FWD PANEL. REMOVED AND REPAIRED THE FAIRING IAW SRM 53-00-01, VOL 1, FIG. 8 AND INSTALLED IAW DRAWING AJC7405.

Part: SKIN — CRACKED (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING UPPER SURFACE PANEL 516ET LAND IS CRACKED. REPAIRED IAW EA T 8-5730-T0328017

Part: SKIN — CORRODED (RT WING) · airframe 94,139 hrs · 32,500 cycles

RIGHT WING TOP SURFACE CORRODED. REPAIRED IAW EA T 8-5730-T0328132 PT 1.

Part: VANE — PUNCTURED (TE FLAP) · airframe 94,139 hrs · 32,500 cycles

RIGHT INBD FLAP VANE HAS PUNCTURE DAMAGE ON BOTTOM SIDE. REPAIRED IAW SRM 51-71-00, VOL II.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 94,139 hrs · 32,500 cycles

FOUND VERTICAL STABILIZER PANEL 374CR DELAMINATED ON BOTTOM SIDE. REPAIRED VERTICAL STABILIZER PANEL 374CR REF SRM 51-71-00, VOL 2 AND DWG AMC7196.

Part: SKIN — DELAMINATED (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING, OUTBD. T/E PANEL #551DB IS DELAMINATED. ) REPAIRED IAW SRM 51-71-00 VOL 2 AND DRAWING ARC0623.

Part: SKIN — CHAFED (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING FWD OF INBD FLAP HINGE FITTING, LWR WING SKIN SURFACE HAS EVIDENCE OF HEAVY CHAFING. REPAIRED PER EA 8-5730-T0328126. REPAIR CLASSIFIED AS MINOR.

Part: SKIN — CORRODED (RT WING) · airframe 94,139 hrs · 32,500 cycles

RIGHT WING TOP SURFACE CORRODED. CORROSION REMOVED AND EXCEEDED MAX LIMITS IAW SRM . REPAIRED IAW EA. 8-5710-T0328199

Part: DOUBLER — WORN (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT DROOPED LEADING EDGE ASSY HAS A DOUBLER WORN BEYOND LIMITS ON THE OTBD LEADING EDGE. REMOVED AND REPLACED FILLER ON PREVIOUS REPAIR AT LEADING EDGE REF SRM 51-31-01 VOL II.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

LOWER FUSELAGE RT SIDE AT APPROXIMATELY STA 987, LONGERON 40R TO 41R, HAS AN INTERNAL DOUBLER REPAIR. REPAIR IAW SRM 53-20-00, FIG 13, SHEET 14.

Part: SKIN — CHAFED (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING, JUST FWD. OF INBD FLAP HINGE FITTING, LOWER WING SKIN SURFACE HAS EVIDENCE OF HEAVY CHAFING. DEPTH MEASURED 128 DEEP BEFORE REWORK USING DIAL DEPTH GAUGE MA1548. WORK COMPLETED IAW EA T-8-5730-T0328126 PT.1

Part: SKIN — DAMAGED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

LOWER AFT FUSELAGE LT SIDE, AT APPROXIMATELY STA 2040, LONGERON 41, HAS AN EXTERNAL REPAIR DOUBLER. REPAIR IAW SRM 53-00-01, FIG 4, SHEET 2.

Part: CAP — CRACKED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

FWD CARGO, STA 595 RT SIDE CRACKED AT LONGERON 39. REPAIRED TEE CAP IAW EA 8-5310-T0327811, P1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

AFT CARGO COMPARTMENT LT SIDE, OTBD FLOOBOARD SUPPORT ANGLE HAS CORROSION, APPROXIMATE STA 1841 TO STA 1967. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-31-01, VOL 2.

Part: RIB — GOUGED (RT WING) · airframe 94,139 hrs · 32,500 cycles

RIGHT WING L/E RIB CASTING GOUGED INBD OF NR 6 L/E SLAT TRACK STA XORS -317 BLENDED AND TREAT AREA IAW EA 8-5740-T0327942.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

STA 595, 3 CRACKS IN THE WEB RT LONGERON 39. PERFORMED BULKHEAD CRACK REPAIR AT STA 595 JAW SRM 53-40-00, VOL II, FIG 25, SHEET 2 & 3.

Part: SKIN — DENTED (RUDDER) · airframe 94,139 hrs · 32,500 cycles

LEFT UPPER AFT RUDDER HAS A SMALL DENT, AT RS ZAR459. REPAIRED PER SRM 55-00-01 FIG. 3, SHT.2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

MAIN CARGO, FLOOR SEAT-TRACK DAMAGED, GOUGED LBL 47, STA 755. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1.

Part: DOUBLER — CORRODED (BS 1155) · airframe 94,139 hrs · 32,500 cycles

FOUND A DOUBLER IS CORRODED AT BS 1155, BETWEEN LONGERON 48 - 49R. REMOVED AND REAPLCED THE DOUBLER IAW SRM 51-21-01 AND DWG NAA6064.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,139 hrs · 32,500 cycles

AFT CARGO COMPARTMENT STA 1830, RBL 28 SEAT TRACK CORRODED AT NUTPLATE. MARKED, REPLACED RT AFT CARGO COMPARTMENT SEAT TRACK FROM STA 1787 THRU STA 1964 IAW DAC 3855 REF, SRM 51-31-01, VOL II.

Part: SKIN PANEL — CRACKED (LT HORIZ STAB) · airframe 94,139 hrs · 32,500 cycles

LEFT HORIZONTAL STABILIZER UPPER OUTER AFT SKIN PANEL ALC7439 HAS 1 EA. CRACK PROPAGATING PAST PREVOIUS STOP DRILL. TOTAL LENGTH IS 3.25" FROM AFT EDGE OF PANEL TO END OF CRACK. EXCEEDS CRACK LIMITS OF WORKCARD 55X1203, ALI-P3 FIG 2 TABLE 1, REPAIR IAW EA 8-5510-T0327675.

Part: RIB — CRACKED (STAB FAIRING) · airframe 94,139 hrs · 32,500 cycles

LEFT UPPER HORIZONTAL STABILIZER FAIRING AJC7690-1 HAS CRACK IN FORMER RIB AT AFT END. R & R FAIRING IAW SRM 53-00-01, VOL-1, FIG 8 AND INSTALLED IAW DWG AJC7405.

Part: SKIN — CORRODED (BS 2000) · airframe 94,139 hrs · 32,500 cycles

AFT FUSELAGE WASTE TANK AREA BS 2000 SKIN CORRODED INBD OF LONGERON 43L. IAW SRM 53-20-00 FIG 4 SHEET II VOL I. REMOVED CORROSION FROM SKIN IAW SRM 53-20-00 FIG.4

Part: TEE FITTING — WORN (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING ANTI-ICE TELESCOPING DUCT PANEL OUTBD, AFT LANDING IS WORN. REPLACED DAMAGED TEE CAP IAW DRAWING ARB 1284.

Part: SKIN — WORN (LT WING) · airframe 94,139 hrs · 32,500 cycles

LEFT WING ANTI-ICE TELESCOPING DUCT PANEL INBD, FWD LANDING IS WORN. REPLACED IAW DRAWING ARB 1284.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 93,349 hrs · 32,124 cycles

AT 2354Z NOTED HYD 3 ELEV OFF, COMPLIED WITH QRH, DECREASING HYD 3. DECLARED EMER & DIVERTED. HAD ACFT TOWED FROM RAMP ENTRY BLOCK IN WITH 1.6 GAL HYD 3. NORMAL APPROACH, CONFIGURATION & LANDING. AT LT MLG, FOUND LOOSE B-NUT AT MLG HYD ACTUATOR BALANCE TUBE, AT TOP OF TUBE, WHERE TUBE FITS INTO UNION, NUT WAS FINGER TIGHT, NUT IS PAINTED WHITE, TIGHTEN NUT. TOPPED OFF NR 3 HYD SYS. OPERATED SYS, NO LEAKS PINNED GEAR. OPERATED GEAR HANDLE TO UP POSITION, NO LEAKS. REPEATED LEAK CHECK 3 TIMES, NO LEAKS. ACFT OK FOR SERVICE.

Part: FIRE BOTTLE — FAULTED (CARGO BAY) · airframe 93,177 hrs · 32,030 cycles

CARGO FIRE EXTINGUISHER AGENT LOW LIGHTS ON FOR BOTTLE 1. REASON CODE, REMOVAL FROM ACFT ONLY, NO INSTALLATION. REMOVED LOWER CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER IAW AMM 26-22-01-4, ALL HARDWARE IS ATTACHED TO THE RACK. REASON CODE, INSTALLATION ON ACFT ONLY, NO REMOVAL. REPLACED LOWER CARGO FIRE BOTTLE AS NEEDED IAW MM 26-22-01-4. OPERATIONS CHECK IAW AMM 26-22-02-5. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 93,165 hrs · 32,024 cycles

FUMES IN COCKPIT, EMER DECLARED UPON DESCENT. NOT PACK NR 1 OR 2, NOT HUD. THREE PEOPLE CONFIRMED SHOE POLISH SMELL. O2 MASKS USED. AFTER LANDING INSPECTION OK BY AIRPORT AUTHORITY. PERFORMED ENG OF INDIVIDUAL ENGS & CORRESPONDING PACK IN AN ATTEMPT TO ISOLATE SOURCE OF SMELL IAW-JRH. WITH CAPTAIN IN THE COCKPIT VERIFIED THAT NO SMELL OR FUMES WERE PRESENT IN THE COCKPIT DURING THE ENG & PACK RUN. INSPECTED CARGO COMPARTMENTS & SMELL & FUMES REPORTED BY FLIGHT CREW WERE NOT FOUND. HOWEVER, A SMALL SOAP SPILL WAS DISCOVERED IN AFT MAIN CARGO, THIS WILL BE REPORTED IN A SEPARATE WRI.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 926 hrs · 31,709 cycles

ON DESCENT WITH ENG & WG ANTI-ICE ON, GOT NUMEROUS LVL 1 & 2 ALERTS FOR AIR SYS PROBLEMS. WITH CABIN ALT RISING, DID A HIGH SPEED DIVE TO 10,000 FT. CABIN ALT GOT TO 7800 FT & STARTED BACK DOWN TO NORMAL. VALUES OF CABIN ALT, THEREAFTER ALERTS INCLUDED LVL 2 FOR CABIN IN FLO, LVL 1 ALERTS FOR AIR SYS 1 OFF & AIR SYS 2 OFF. RAN ALL APPROP QRH PROCEDURES. FOUND 1-2 ISOL VLV HAD CLOSED ITSELF, NR 1 PACK TURNED ITSELF OFF & LOST NR 2 PACK WITH NO AIR SUPPLY. OPENED 1-3 ISOL & TURNED NR 1 PACK BACK ON. NR 3 AIR CONDITIONING PACK & NR 2 PNEUMATIC SYS WERE DEFERRED AT TIME OF EVENT, FOUND FAN AIR VLV FAULTY. R & R NR 1 FAN AIR VLV. R & R NR 1 PNEUMATIC SYS CONTROLLER. CONTROLLER OPERATIONS CHECKED GOOD. NR 1 FAN AIR VLV OPERATIONS CHECKED OK.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 926 hrs · 31,709 cycles

ON DESCENT, WITH ENG & WG ANTI-ICE ON, GOT NUMEROUS LVL 1 & 2 ALERTS FOR AIR SYS PROBLEMS. WITH CABIN ALT RISING DID A HIGH SPEED DIVE TO 10,000 T. CABIN ALT GOT TO 7800 FT & STARTED BACK DOWN TO NORMAL. VALUES OF CABIN ALT, THEREAFTER ALERTS INCLUDED LVL 2 FOR CABIN IN FLO, LVL 1 ALERTS FOR AIR SYS 1 OFF & AIR SYS 2 OFF. RAN ALL APPROP QRH PROCEDURES. FOUND 1-2 ISOL VLV HAD CLOSED ITSELF, NR 1 PACK TURNED ITSELF OFF & LOST NR 2 PACK WITH NO AIR SUPPLY. OPENED 1-3 ISOL & TURNED NR 1 PACK BACK ON. FOUND FAN AIR VLV FAULTY. R & R NR 1 FAN AIR VLV. R & R NR 1 PNEUMATIC SYS CONTROLLER. CONTROLLER OPERATIONS CHECKED GOOD. NR 1 FAN AIR VLV OPERATIONS CHECKED OK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 923 hrs · 31,563 cycles

L1 DOOR PNEUMATIC BOTTLE HAS LOW PRESSURE. SERVICED L1 DOOR IAW AMM 52-11-07-6-0. BOTTLE RETAINED PRESSURE AND DOOR OPERATED PROPERLY. ACFT OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 923 hrs · 31,559 cycles

L1 DOOR PNEUMATIC BOTTLE IS LOW. SERVICED L1 DOOR BOTTLE IAW AMM 52-11-07-6-0. BOTTLE RETAINED PRESSURE AND DOOR OPERATED PROPERLY. ACFT OK FOR SVC.

Part: FIRE BOTTLE — UNKNOWN (NR 3 ENGINE) · airframe 921 hrs · 31,436 cycles

NUMBER 3 ENG AGENT 2 LOW LIGHT ON. R & R THE NR 3 ENG NR 2 FIRE BOTTLE.

Part: DOUBLER — CRACKED (RT WING) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 545 CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 91,335 hrs · 30,999 cycles

LEFT WING LE BEADED DOUBLER AT XOS 545 CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 700) · airframe 91,335 hrs · 30,999 cycles

CENTER LANDING GEAR BAY LT SIDEWALL SPOILER CONTROL ROD ACCESS CUT OUT SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED IAW SRM 51-31- 01 VOLUME II. DOUBLER FABRICATED IAW DRAWING AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING NR 5 SLAT LOWER SURFACE AT XOS 717.5 FOUND DENTED. REPAIRED IAW EA 8-5750-T0311623 REVISION B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 668 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING LE SUPPORT RIB AT REFUELING ACCESS DOOR OTBD CUT OUT RWS 643.5 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. RIB FABRICATED IAW DRAWING ARB1187 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING FIXED LE STRINGER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0311421 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 665 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING RIB) · airframe 91,335 hrs · 30,999 cycles

RIGHT WING FIXED LE EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACKED. RIB DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. RIB DOUBLER FABRICATED IAW DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 91,335 hrs · 30,999 cycles

LEFT WING LE COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STIFFENER — CRACKED (LT WING) · airframe 91,335 hrs · 30,999 cycles

LEFT WING FIXED LE STIFFENER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0311419 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 91,335 hrs · 30,999 cycles

LEFT WING LE COMPARTMENT BEADED DOUBLER AT XOS 669 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT WING) · airframe 91,335 hrs · 30,999 cycles

LEFT WING FIXED LE RIB DOUBLER AT STATION XOS 789 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. DOUBLER FABRICATED IAW DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: AUTOLAND SYS — MALFUNCTIONED (COCKPIT) · airframe 90,494 hrs · 30,541 cycles

AFTER BLOCK OUT, ACFT WENT TO SINGLE LAND 1, NO AUTO LAND. RELEASED FOR SERVICE IAW MEL 22-10-03 CATEGORY C. AUTO LAND SYS INOPERATIVE.

Part: COMPUTER — FAILED (COCKPIT) · airframe 90,494 hrs · 30,541 cycles

DURING TAKEOFF, SPEED TAPE INDICATIONS ERRATIC, SR WAS ABSENT, AFTER SLATS RETRACT AIRSPEED LIMITED TO 260. AT 2000 FEET AP 1 SELECTED, INDICATIONS ERRATIC, SELECTED AP 2 INDICATIONS OK, THEN FD 1 FAILED. SELECTED FLT DIR CAPTAIN'S ON 2. ALSO STBY INDICATOR FALLING OFF. DURING APPROACH STBY PFD NORMAL. AIR TURN BACK AFTER CONSULTATION WITH GOC. PER CREW DEBRIEF SLAT RETRACT SPEED & FLAP RETRACT SPEED BECAME ERRATIC ON CAPTAIN`S PFD, SPEEDS WERE STEADY & CORRECT ON FIRST OFFICER`S SIDE & IN FMC. R & R NR1 FCC IAW AMM 22-01-03-4. RTS TEST FAILED, COULD NOT COMPLETE RTS DUE TO ROB FLAP POSITION ON MEL27-50 7734. CAPTAIN’S FLT DIR OPERATIONS CHECKED NORMAL IAW FIM 34-24-01. R & R SAI IAW AMM 34-28-01-2, OPERATIONS CHECKED NORMAL. CANNOT COMPLETE SIGN OFF UNTIL ROB FLAP POSITION XMTR IS REPLACED.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 89,346 hrs · 29,936 cycles

L1 SLIDE PUSH TO TEST LIGHT INOPERATIVE. REPLACED BOTH BATTERIES LIGHT TESTED OK REF AMM 25-61-03-2. REPLACED BOTH BATTERIES LIGHT TESTED. OK REF AMM 25-61-03-2.

Part: TRANSMITTER — FAULTED (OIL PRESSURE) · airframe 89,057 hrs · 29,785 cycles

IN CLIMB FL 330, NR 2 OIL PRESSURE GUAGE SHOWED NO INDICATION AND AMBER X. ALL OTHER ENGINE INDICATIONS NORMAL. NO ALERTS INDICATED. AIU NR 1 SHOWS NR 2 ENG OIL PRESSURE TRANSMITTER FAULTING. R & R NR 2 OIL PRESSURE TRANSMITTER REF MM 79-33-01-2. RAN ENG REF JRH. NO LEAKS, CHECKED NORMAL. OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 89,001 hrs · 29,749 cycles

DURING CLIMB PASSING 10,000 FT, RED FIRE LIGHT IN FUEL LEVER NR 2 FLICKERED, & WENT OUT, FLICKERED AGAIN. NO OTHER INDICATIONS ON GLARE SHIELD OR DISPLAYS OR ANY SECONDARY INDICATION. TOUCHING THE FUEL LEVER CAUSED LIGHT TO COME ON STEADY AND ACCOMPANIED BY ALL OTHER FIRE INDICATIONS. ALL INDICATIONS WENT AWAY WHEN LETTING GO OF THE FUEL LEVER. DECLARED EMERGENCY, RETURNED TO DEPARTURE, ENGINE SHUTDOWN, NO INDICATIONS OF FIRE. PERFORMED FIRE LOOP TEST, ALL INDICATIONS NORMAL. ALL WARNINGS THAT WERE RECEIVED COULD ONLY HAVE COME FROM FDCU, R & R FDCU. PERFORMED ADJUSTMENT TEST OF FDCU IAW ALL TESTS NORMAL, RAN ENGINE IAW JRH, NO FAULTS OR WARNINGS NOTED DURING ENGINE RUN. SYS OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,945 hrs · 29,710 cycles

EXIT LIGHTS DO NOT ILLUMINATE WITH EMERGENCY LIGHT SWITCH OR TEST. R & R LT EMERGENCY LIGHT IAW EA 8-3320-102877A AND MM 33-50-00. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,918 hrs · 29,690 cycles

DURING PREFLIGHT FOUND L1 & R1 DOOR EMERGENCY "EXIT" LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY U1-1756, NO JOY, REINSTALLED ORIGINAL UNIT, REF MM 33-51-01-4. CHECKED S3-692 TERMINAL 4 & 5 FOR CONDITION AND SECURITY, CHECKED OK, NO VOLTAGE. CHECKED CONNECTOR P1-1756 PIN 3 FOR SECURITY, CHECKED OK. REF WDM 33-52-01 PG3. RELAMPED EXIT SIGN AND OPS CHECKED THE EMERGENCY LIGHTS PER M/M 33-51-00-5, OPS CHECKED GOOD.

Part: SKIN — CRACKED (ZONE 100) · airframe 88,834 hrs · 29,637 cycles

LOWER EXTERNAL FUSELAGE SKIN CORRODED AND CRACKED BS 1079 BETWEEN L47-48R. REPAIRED EXTERNAL FUSELAGE SKIN IAW EA 8-5330-163344. MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 88,834 hrs · 29,637 cycles

INSIDE CENTER CARGO BAY RT SIDE FITTING, TOP BOLT, APPEARS TO HAVE SMALL DARKENED CRACK COMING FROM FASTNER HOLE. REPAIRED FRAME FITTING IAW SRM 53-30-00, FIG 7, VOL I. MAJOR REPAIR.

Part: SKIN — CHAFED (ZONE 100) · airframe 88,834 hrs · 29,637 cycles

EXTERNAL POWER PANEL CUT OUT INNER SURFACE EDGES CHAFED AT TWO PLACES. REPAIRED IAW EA 8-5330-163352. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · airframe 88,834 hrs · 29,637 cycles

BELLY SKIN AT FS 1401 HAS CORROSION. BLENDED AREA IAW SRM 53-00-01, VOL I ORIG MAT 0.050, MAT LOSS 0.011, REMAINING MAT 0.039, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, VOL I. INSTALLED DOUBLER IAW SRM 51-31-01, VOL II. FABRICATED DOUBLER IAW SRM 51-31-01 VOL II, SRM 53-00-01, VOL I AND EA 8-5330-84850 STA 1401. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · airframe 88,834 hrs · 29,637 cycles

BELLY SKIN AT FS 1381 HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FABRICATED DOUBLER IAW EA 8-5330-84850, INSTALLED DOUBLER IAW SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: SPAR CAP — DAMAGED (ZONE 500) · airframe 88,834 hrs · 29,637 cycles

LEFT WING REAR SPAR, LOWER CAP AT XORS 345.75 FOUND TWO AFT FASTENER HOLES OVERSIZED WHILE ACCOMPLISHING EO 8-5710-7-5007. PT 1 COMPLIED WITH EA 8-5710-163343 BY REAMING HOLE A & D TO .371 AND INSTALLING BUSHINGS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,689 hrs · 29,553 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51-01-4. OPS CHECKED NORMAL.

Part: CONTROL HANDLE — OBSTRUCTED (MLG) · airframe 88,330 hrs · 29,366 cycles

AFTER LOWERING LANDING GEAR, HAD 3 RED GEAR LIGHTS IN BOTH MAIN GEAR INDICATIONS AND CONFIG PAGE, ALSO GEAR WARNING HORN AND CAWS, SITUATION STAYED SAME UNTIL 1500' AGL WHEN GO-AROUND EXECUTED, RAISED GEAR HANDLE ON GO-AROUND AND GEAR RETRACTED NORMAL WITH ALL WARNINGS GONE/NO GEAR LIGHTS. EXTENDED GEAR IN PATTERN THEN GEAR DOWN INDICATIONS NORMAL. LANDED NORMAL, NO EMERGENCY DECLARED. TROUBLESHOTING IAW FIM 32-30-03, ALL STEPS CHECKED GOOD. FOUND GEAR HANDLE STICKING, ABLE TO DUPLICATE ON GROUND. CLEANED GEAR CONTROL MECHANISM IAW AMM 32-31-02-7. OPS CHECKED NORMAL ON GROUND.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 87,855 hrs · 29,118 cycles

EMERGENCY EXIT SIGN INOPERATIVE. OUND LOOSE BULB IN EXIT SIGN. RESEATED BULB AND SIGN OPERATES NORMAL IAW MM 33-50-00-5.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 87,662 hrs · 29,013 cycles

EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY PER AMM 33-51-01-4. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: LAMP — WRONG PART (DOOR SLIDE) · airframe 87,592 hrs · 28,976 cycles

DOOR SLIDE PRESS TO TEST LIGHT INOPERATIVE. WRONG LAMPS INSTALLED IN PUSH TO TEST CAP. INSTALLED CORRECT LAMPS IAW SMP, LIGHT TESTS NORMAL.

Part: SKIN — DENTED (BS 1008) · airframe 87,368 hrs · 28,848 cycles

DENT AT STA. 1008, IMMEDIATELY ABOVE L35R AND 3" CIRCUMFERENTIAL X 2" LONGITUDINAL X 0.125" DEEP. DENT EXCEEDS SRM 53-20-00, FIG 13. COMPLIED WITH EA 8-5330-153029 AND REPAIRED IAW SRM 53-20-00, FIG 6 AS REF.

Part: FUEL CONTROL — FAILED (NR 2 ENGINE) · airframe 87,194 hrs · 28,748 cycles

AT FL360, ENCOUNTERED TURB ACFT WAS SLOWING TO .80M FROM .83 NR 2 ENG FLAMED OUT W/ AUTO RESTART FROM IGNITION OVERIDE ON , EAI ON OAT -58C. MIGHT POSSIBLY HAVE HAPPENED ON PREVIOUS FLIGHT AT TOP OF DECENT. CHECKED ACFT FUEL TANK SUMPS FOR WATER IAW AMM CH 72-00-00-1-1, FIG 137, NO WATER FOUND. INSTALLED PREVIOUSLY REMOVED NR 2 ENG FUEL PUMP AND MEC IAW MM REF 73-12-01-2 AND 73-20-01-2 UP TO STEP 32. SPECIFIC GRAVITY SET. PERFORMED NR 2 ENGINE FLIGHT IDLE OPS CHECK AND MAX POWER ADJUSTMENT TEST PER JRH 7-7 AND AMM 71-00-00-5. OPS CHECKED GOOD.

Part: RIB — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RIGHT HAND WING LOWER SURFACE LEADING EDGE CAVITY INBOARD OF SLAT TRACK NR 8 SUPPORT RIB FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RIGHT HAND WING LOWER SURFACE LEADING EDGE CAVITY INBOARD OF SLAT TRACK NR 8, SUPPORT RIB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN- ACCORDANCE-WITH ANY APPROVED DATA. SUPPORT RIB FABRICATED PER DRAWING ARB1162, REVISION S AND REPLACED AS PER SRM 51-33-01, VOLUME II, REVISION 96. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: LONGERON — CORRODED (BS 765-854) · corrosion level 2 · airframe 86,292 hrs · 28,290 cycles

CORROSION ON LONGERON 51L BETWEEN STA 765 TO 824. FOUND AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111. REPAIR CLASSIFIED AS CATEGORY "B" INITIAL INSPECTION TO BE CARRIED OUT AT 15,000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 10,000 FLIGHT CYCLES.

Part: LONGERON — CORRODED (BS 765-824) · corrosion level 2 · airframe 86,292 hrs · 28,290 cycles

CORROSION ON LONGERON 51R BETWEEN STA765 TO 824 FOUND AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111. REPAIR CLASSIFIED AS CATEGORY "B" INITIAL INSPECTION TO BE CARRIED OUT AT 15,000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 10,000 FLIGHT CYCLES.

Part: LONGERON — CORRODED (BS 765-824) · corrosion level 2 · airframe 86,292 hrs · 28,290 cycles

AFTER REMOVAL OF SKIN TO FACILITATE REPAIR (REF SNRM N00362) FOUND CORROSION ON LONGERON 50L BETWEEN STA 765 TO STA 824. CORRODED LONGERON 50L BETWEEN STA 765 TO STA 824 PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111. REPAIR CLASSIFIED AS CATEGORY "B" INITIAL INSPECTION TO BE CARRIED OUT AT 15,000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 10,000 FLIGHT CYCLES.

Part: LONGERON — MISINSTALLED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

LONGERON 52 BETWEEN STA 765 TO STA 791.75 FOUND NOT IAW BLUEPRINT DWG NDA6214, AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. DISCREPANT LONGERON 52 BETWEEN STA 765 TO STA 859 PERFORMED SPLICE REPAIR IAW SRM 53-10-00 FIG 1 AND FIG 2, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111. REPAIR CLASSIFIED AS CATEGORY "B" INITIAL INSP TO BE CARRIED OUT AT 15,000 FLIGHT CYCLES AND REPETITIVE INSP TO BE CARRIED OUT AT EVERY 10,000 FLIGHT CYCLES. REFER TO SNRM N00255 FOR WORK DETAILS.

Part: RIB — MISREPAIRED (RT WING SLAT) · airframe 86,292 hrs · 28,290 cycles

EXISTING REPAIR - RT WING LOWER SURFACE L/E CAVITY OTBD OF SLAT TRACK NR 8 SUPPORT RIB. EVALUATED AND FOUND ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW RIB FABRICATED PER DRAWING NR ARB1286 REVISION K. RIB REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II, REVISION 96. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: BULKHEAD — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

CENTER ACCESSORY COMPARTMENT - EXISTING REPAIR DOUBLER FOUND ON AFT BULKHEAD STA 1156, L44 TO 46 LEFT. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. EXISTING REPAIR DOUBLER, REPAIRED AS PER EA 8-5310-143723, REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100, REVISION 111.

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 86,292 hrs · 28,290 cycles

EXISTING REPAIR FOUND ON RIGHT HAND HORIZONTAL STABILIZER UPPER SURFACE, ADJACENT TO REAR SPAR AT STA XE 84. EXISTING REPAIR AT RIGHT HAND HORIZONTAL STABILIZER UPPER SURFACE, ADJACENT TO REAR SPAR AT STA XE 84 EVALUATED, FOUND WITH SHORT EDGE MARGIN. RIGHT HORIZONTAL STABILIZER UPPER SURFACE AT STA XE 84, REPAIR CARRIED OUT PER EA 8-5510-143732, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (LT NR 2 SLAT) · airframe 86,292 hrs · 28,290 cycles

LEFT HAND WING SLAT NR 2 INBOARD INNER SURFACE FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW REPAIR CARRIED OUT PER SRM 57-10-00, FIGURE 29, VOLUME 1, REVISION 96. E.O. 8- 5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 86,292 hrs · 28,290 cycles

RIGHT HORIZONTAL STAB DRY BAY, STA XE 87, UPPER STRINGER NR 7 FOUND EXISTING REPAIR. EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR ACCOMPLISHED PER EA 8-5510-143416, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 86,292 hrs · 28,290 cycles

LT WING SLAT NR 7 INNER SURFACE FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN-ACCORDANCE-WITH ANY APPROVED DATA. EXISTING REPAIR REMOVED AS PER SRM 51-35-02, VOLUME II, REVISION 96. NEW REPAIR ACCOMPLISHED AS PER SRM 57-10-00, FIGURE 31, VOLUME I, REVISION 96. FEDEX EO 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: ATTACH FITTING — UNKNOWN (LT MLG) · airframe 86,292 hrs · 28,290 cycles

EXISTING REPAIR AT MLG LT WING TRUNNION FITTING AFT UPPER ATTACHMENT HOLE. REPAIRED AS PER EA 8-5740-143417. (MAJOR REPAIR)

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 86,292 hrs · 28,290 cycles

EXISTING REPAIR ON LT WING INBD FLAP ASSY, UPPER SURFACE, LOWER INBD SEGMENT. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AND FOUND NOT IN ACCORDANCE WITH APPROVED DATA. EXISTING REPAIR REMOVED AS PER SRM 51-35-01 VOL. II REVISION 96 AND NEW REPAIR ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 96. E.O. 8-5100-7-5001A7 PT.2 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING DURING INSTALLATION OF FUEL TANK ACCESS PANEL NR 638AB, FOUND ONE EXTRA FASTENER. RIGHT HAND WING FUEL TANK ACCESS PANEL 638AB CUTOUT 01 EACH EXTRA FASTENER CARRIED OUT REPAIR AS PER EA 8-5710-143726, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — DAMAGED (NR 2 SLAT) · airframe 86,292 hrs · 28,290 cycles

AFTER REMOVAL OF EXISTING REPAIR DOUBLER AT LEFT HAND WING SLAT NR 2, FOUND FASTENER HOLES ELONGATED ON INNER SURFACE SKIN OUTBOARD CORNER. ACCOMPLISHED REPAIR AS PER SRM 51-10-00 FIGURE 29 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 86,292 hrs · 28,290 cycles

LT WING TELESCOPIC DUCT CUTOUT FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED AS PER EA 8-5710-143715, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 86,292 hrs · 28,290 cycles

RIGHT HORIZONTAL STABILIZER DRY BAY, STA XE 228, UPPER STRINGER NR 9 FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR CARRIED PER EA 8-5510-143413, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (LT WING) · airframe 86,292 hrs · 28,290 cycles

LT LOWER SURFACE FUELING STATION DOOR CUTOUT FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 68, VOLUME I, REVISION 96. EO 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 86,292 hrs · 28,290 cycles

EXISTING FLUSH REPAIR FOUND AT LT WING INBOARD FLAP LOWER SURFACE, LOWER INBOARD SEGMENT AT STA XIFH 159.3. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. REPAIR CARRIED OUT AS PER SRM 57-10-00, FIGURE 3 VOLUME I, REVISION 96. EO 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: PANEL — MISREPAIRED (ZONE 200) · airframe 86,292 hrs · 28,290 cycles

MAIN DECK CARGO COMPARTMENT EXISTING REPAIR FOUND ON LT MLG OVER PRESSURE PANEL TOP SURFACE AT STA 1441 TO STA 1461. EXISTING REPAIR ON LT MLG OVER PRESSURE PANEL TOP SURFACE BETWEEN STA 1441 TO STA 1461. FOUND PREVIOUSLY ACCOMPLISHED AND NOT IAW APPROVED DATA. EXISTING REPAIR REMOVED IAW SRM 51-33-01 VOL II, REV 96. NEW REPAIR ACCOMPLISHED IAW DWG 3G10530000, REV 0. EO 8-5100-7-5001A7 PT.1. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: PANEL — MISREPAIRED (ZONE 200) · airframe 86,292 hrs · 28,290 cycles

MAIN DECK CARGO COMPARTMENT - EXISTING REPAIR FOUND ON LT MLG OVERPRESSURE PANEL TOP SURFACE AT STA 1381 TO STA 1401. EXISTING REPAIR ON LT MLG OVERPRESSURE PANEL TOP SURFACE BETWEEN STA 1381 TO STA 1401 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. EXISTING REPAIR REMOVED IAW SRM 51-33-01, VOL II, REV 96. NEW REPAIR ACCOMPLISHED IAW DWG SG10530000 REV 0. EO 8-5100-7-5001A7 PT.1. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.

Part: FLOORBEAM — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

CTR CARGO - EXISTING REPAIR AT STA 1701 FLOORBEAM WEB AFT SURFACE ABOVE LONGERON 44 RT TO LONGERON, 48 RT. EXISTING REPAIR AT CTR CARGO, STA 1701 FLOORBEAM WEB AFT SURFACE ABOVE LONGERON 44 RT TO LONGERON 48 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. NEW REPAIR CARRIED OUT IAW EA 8-5310-143710, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CHAFED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING DROOP L/E FWD SURFACE FOUND CHAFED. RT WING DROOP L/E FWD CHAFED SURFACE REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 4, VOL I, REV 96. REPAIR CLASSIFIED IAW GMM 6-2-100, REV 111.

Part: SKIN — DAMAGED (NR 4 SLAT) · airframe 86,292 hrs · 28,290 cycles

RIGHT HAND WING SLAT NR 4 TOP EDGE FOUND TRIMMED OFF. RIGHT HAND WING SLAT NR 4 TOP EDGE TRIMMED OFF EVALUATED AND FOUND ACCEPTABLE IAW SRM 57-00-01 FIGURE 1A VOLUME I REVISION 96.

Part: SKIN — DAMAGED (NR 4 SLAT) · airframe 86,292 hrs · 28,290 cycles

LEFT HAND WING SLAT NR 4 TOOP EDGE FOUND TRIMMED OFF. LEFT HAND WING SLAT NR 4 TOOP EDGE TRIMMED OFF EVALUATED AND FOUND ACCEPTABLE IAW SRM 57-00-01 FIGURE 1A VOLUME I REVISION 96.

Part: WEB — CORRODED (BS 1701-1781) · airframe 86,292 hrs · 28,290 cycles

CTR CARGO - AFTER REMOVAL OF STA 1701 TO STA 1781 SUMP PANEL SUPPORT ABOVE LONGERON 45R, WEB BELOW SUPPORT FOUND CORRODED. CORRODED WEB AT CTR CARGO STA 1701 TO STA 1781 LONGERON 45 RT REMOVED IAW SRM 51-31-01, VOL II, REV 96. WEB FABRICATED IAW DWG NR AFA3912 REVISION M AND INSTALLED IAW DWG NR AFA3912 REV M AND NFA 6034, REV BE. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 86,292 hrs · 28,290 cycles

CABIN L3 DOOR FWD JAMB LOWER WEB FOUND EXISTING REPAIR. EXISTING REPAIR AT CABIN L3 DOOR FWD JAMB LOWER WEB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. CABIN L3 DOOR FWD JAMB LOWER WEB REPAIR CARRIED OUT IAW SRM 53-50-00, FIG 19, VOL I, REVISION 96. EO8-5100-7-5001 A7 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SEAT TRACK — CORRODED (BS 1841) · airframe 86,292 hrs · 28,290 cycles

AFT CARGO - RT SEAT TRACK STA 1841 LOWER SURFACE CORRODED UNDER ANCHOR NUT. AFT CARGO RT SEAT TRACK STA 1841 LOWER SURFACE CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96 AND FOUND WITHIN LIMIT IAW SRM 53-70-00, VOL I, REV 96. ORIGINAL THICKNESS 0.100 INCH, MATERIAL REMOVED 0.005 INCH AND MATERIAL REMAIN 0.095 INCH. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 111.

Part: RIB — CRACKED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING DROOP L/E BELOW EXTERIOR SKIN TOP EDGE FOUND RIB CRACKED. RT WING DROOP L/E BELOW EXTERIOR SKIN TOP EDGE CRACK RIB REMOVED IAW SRM 51-31-01 VOLUME II, REV 96 AND INSTALLED WITH A FABRICATED RIB SRM 51-35-01, VOL II REV 96. RIB FABRICATED IAW DWG ARB1335, REV T. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 111.

Part: SEAT TRACK — CORRODED (BS 1841) · airframe 86,292 hrs · 28,290 cycles

AFT CARGO - LT SEAT TRACK STA 1841 LOWER SURFACE CORRODED UNDER ANCHOR NUT. CORROSION AT AFT CARGO LT SEAT TRACK, STA 1841 LOWER SURFACE REMOVED IAW SRM 51-21-01, VOL II, REV 96 AND FOUND WITHIN LIMIT IAW SRM 53-70-00 VOL I, REV 96. ORIGINAL THICKNESS 0.100 INCH, MATERIAL REMOVED 0.007 INCH AND MATERIAL REMAIN 0.093 INCH. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: WEB — MISREPAIRED (DOOR FRAME) · airframe 86,292 hrs · 28,290 cycles

CABIN L3 DOOR AFT DOOR JAMB LOWER WEB FOUND EXISTING REPAIR. EXISTING REPAIR AT CABIN L3 DOOR AFT DOOR JAMB LOWER WEB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. CABIN L3 DOOR, AFT DOOR JAMB LOWER WEB REPAIR CARRIED OUT IAW SRM 53-50-00, FIG 19, VOL I, REV 96. EO 8-5100-7-5001 A7 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (LT WING) · airframe 86,292 hrs · 28,290 cycles

LT WING DROOP L/E EXTERIOR SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR ON LT WING DROOP L/E EXTERIOR SURFACE FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-10-00 FIG 55, VOL I, REVISION 96 BUT FOUND WITH SHORT EDGE MARGIN. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-33-01, VOL II REV 96. NEW REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-10-00 FIG 55, VOL I, REV 96. EO 8-5100-7-5001, A7, PART 2, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: STIFFENER — CRACKED (NR 1 SLAT) · airframe 86,292 hrs · 28,290 cycles

LT WING L/E NR1 SLAT LOWER STIFFENER FOUND CRACKED. LT WING L/E NR1 SLAT LOWER CAP PN ARB1588-1, CRACKED AREA TRIMMED AND REPAIRED IAW EA 8-5750-143705. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SLAT — MISREPAIRED (NR 2 SLAT) · airframe 86,292 hrs · 28,290 cycles

RT WING SLAT NR 2 UPPER SURFACE OTBD CORNER FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT NR2 UPPER SURFACE OTBD CORNER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. EXISTING REPAIR REMOVED IAW SRM 51-31-01, VOL II REV 96. NEW REPAIR ACCOMPLISHED IAW EA 8-5750-143411, TITLE - WINGS : FLIGHT CONTROLS - RT WING NR 2 SLAT UPPER SKIN CRACK - PERMANENT REPAIR. EO 8-5100-7-5001 A7 PT.2. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.

Part: ANGLE — MISREPAIRED (NR 2 SLAT) · airframe 86,292 hrs · 28,290 cycles

RT WING SLAT NR 2 OTBD EDGE ANGLE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT NR 2 OTBD EDGE ANGLE EVALUATED AND FOUND ACCOMPLISHED NOT IAW ANY APPROVED DATA. NEW ANGLE FABRICATED IAW DWG NR ARB1647 REV C. ANGLE R & R IAW SRM 51-35-01 VOL II, REV 96. REPAIR IDENTIFICATION, CLASSIFICATION AND TRACKING ON ACFT BEING INDUCTED INTO THE MX SYS 14CFR 121.368, 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING DROOP L/E INBD EXTERIOR SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING DROOP L/E INBD EXTERIOR SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIG 4, VOL I, REV 96. EA8-5750-143409, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

AFT FUSELAGE COMPARTMENT DOOR 311AB CUT-OUT EXTERIOR SKIN DOUBLER FOUND CRACKED. REPAIRED IAW EA 8-5330-143712, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (RT WING) · airframe 86,292 hrs · 28,290 cycles

RT WING DROOP, L/E UPPER SKIN FOUND CRACKED. RT WING DROOP L/E UPPER SKIN CRACKED AREA REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 55, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING SLAT TRACK NR 12 CUTOUT FOUND WITH EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY APPROVED DATA. RT WING SLAT TRACK NR 12 CUTOUT REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, VOL I, REV 96. EO 8-5100-7-5001, A7 PART 2, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FWD CARGO - EXISTING REPAIR AT CARGO SIDE AFT DOOR JAMB. EXISTING REPAIR AT FWD CARGO, CARGO SIDE AFT DOOR JAMB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT IAW EA 8-5310-143729. TITLE: FUSELAGE - MAIN FRAME - FWD CARGO DOOR AFT JAMB FRAME REPAIR AT STA 959.00. EO 8-5100-7-5001 A7 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FUSELAGE - EXTERIOR SURFACE AT APPROX STA 1581 TO STA 1601 BETWEEN LONGERON 50 LT AND LONGERON 52 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 1581 TO STA 1601 BETWEEN LONGERON 50 LT AND LONGERON 52 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA 8-9700-119524, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING SLAT TRACK NR10 CUTOUT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT TRACK NR10 CUTOUT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING SLAT TRACK NR10 CUTOUT, REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, VOL I, REV 96. EO.8-5100-7-5001 A7, PART 2, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FWD CARGO - FOUND EXISTING REPAIR ON LONGERON 52 AT STA 808 TO STA 859. EXISTING REPAIR AT FWD CARGO LONGERON 52 STA 808 TO STA 859 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR PARTS REMOVED IAW SRM 51-31-01, VOLUME II, REV 96. NEW REPAIR ON LONGERON 52, STA 765 TO STA 859 ACCOMPLISHED IAW SRM 53-10-00, FIG 1 AND FIG 2, VOL I, REV 96. EO 8-5100-7-5001A7, PT.2. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111. INITIAL INSP TO BE CARRIED OUT AT 15,000 FLIGHT CYCLES AND REPETITIVE INSP TO BE CARRIED OUT AT EVERY 10,000 FLIGHT CYCLES.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

NR3 AIRCON - AFT OF DOOR CUTOUT AT APPROX STA 524 TO STA 540 BETWEEN LONGERON 31 RT AND LONGERON 32 RT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT NR3 AIRCON - AFT OF DOOR CUTOUT AT APPROX STA 524 TO STA 540 BETWEEN LONGERON 31 RT AND LONGERON 32 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01, VOL II, REV 96. NEW REPAIR ACCOMPLISHED IAW SRM 53-50-00, FIG 3, VOL I, REV 96. EO 8-5100-7-5001 A7 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FUSELAGE - EXTERIOR SURFACE AT APPROX STA 463 TO STA 475 BETWEEN LONGERON 29 LT AND LONGERON 30 LT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 463 TO STA 475 BETWEEN LONGERON 29 LT AND LONGERON 30 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. FUSELAGE EXTERIOR SURFACE AT APPROX STA 463 TO STA 475 BETWEEN LONGERON 29 LT & LONGERON 30 LT, REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6, SHEET 15, VOL I, REV 96. EO8-5100-7-5001 A7 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FUSELAGE - EXTERIOR SURFACE AT APPROX STA 557 TO STA 572 BETWEEN LONGERON 45 LT AND LONGERON 47 LT FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT FUSELAGE EXTERIOR SURFACE AT APPROX STA 557 TO STA 572 BETWEEN LONGERON 45 LT AND LONGERON 47 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01, VOLUME II, REVISION 96. REPAIRED ACCOMPLISHED IAW SRM 53-20-00, FIG 2, VOL I, REV 96. EO8-5100-7-5001 A7 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING UPPER SURFACE FIXED L/E AT XOS 660 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING UPPER SURFACE FIXED L/E XOS 660 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR ACCOMPLISHED IAW EA NR 8-5730-143420, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING FUELING STATION DOOR INBD SIDE FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT RT WING FUELING STATION DOOR INBD SIDE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RT WING FUELING STATION DOOR INBD SIDE CARRIED OUT REPAIR IAW SRM 57-10-00, FIG 68 VOL I, REV 96. EO 8-5100-7-5001, A7 PART 2, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 86,292 hrs · 28,290 cycles

FWD CARGO - EXISTING REPAIR AT LOWER FRAME STA 1099, "X" = -38 TO "X" = -48. EXISTING REPAIR AT FWD CARGO LOWER FRAME STA 1099, "X" = -38 TO "X" = -48 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY APPROVED DATA. EXISTING REPAIR FOUND TO BE ACCEPTABLE IAW EA 8-5310- 143711, TITLE: FUSELAGE - MAIN FRAME - FWD CARGO FLOORBEAM SPLICE REPAIR AT STA 1099 AT X = -43. EO NR 8-5100-7-5001 A7 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 86,292 hrs · 28,290 cycles

LT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED AREA ACCOMPLISHED REPAIR IAW EA NR 8-5710-143715, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED INBD AND OTBD AREA TRIMMED AND REPAIRED IAW EA NR 8-5710-143702, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 86,292 hrs · 28,290 cycles

RT WING SLAT NR4 EXTERIOR SURFACE LWR EDGE FOUND 02 EA EXISTING REPAIRS. 02 EACH EXISTING REPAIRS AT RT WING SLAT NR4 EXTERIOR SURFACE LOWER EDGE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR ACCOMPLISHED IAW EA 8-5750-143716. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: CABLE — BROKEN (MLG) · airframe 82,612 hrs · 26,515 cycles

AFTER TAKEOFF, RIGHT MAIN GEAR INDICATED UNSAFE ON BOTH PRIMARY AND SECONDARY WITH GEAR HANDLE UP. FOLLOWED QRH PROCEDURES AND PUT GEAR HANDLE DOWN AND HAD GOOD DOWN AND LOCKED INDICATIONS. FOUND RIGHT MAIN GEAR FOLLOW UP GEAR UP CABLE RUN BROKEN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR FOLLOW UP CABLE. PERFORMED GEAR SWING FOR OPERATIONAL CHECK OF RIGHT MAIN LANDING GEAR DOOR.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 79,527 hrs · 25,190 cycles

WHEN LANDING GEAR EXTENDED GOT ONLY 3 RED LIGHTS ON BOTH GEAR INDICATORS AND CONFIG PAGE. DID NOT FEEL AS IF GEAR CAME DOWN. RECYCLED AND GEAR CAME DOWN NORMALLY. T/S PER FIM FAULT CODE 32-30-03. NO FAULTS INDICATED. ALL SENSOR INDICATIONS AND READOUTS ARE CORRECT. PER MM 31-71-01-2 PERFORMED FUNCTIONAL TEST OF THE PSEU; TEST PASSED. NO FAULT HISTORY, NO CURRENT FAULTS. SENSOR READOUTS AND DISPLAY ARE CORRECT. A/C OK FOR CONTINUED SERVICE.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,619 hrs · 24,327 cycles

FUSELAGE - FRAME SPLICE CORROSION AT STA 475 BETWEEN LONGERONS 23 & 24, LEFT SIDE. TRIMMED FRAME BETWEEN LONG 23 & 24 AND REMOVED FRAME LOWER SECTION THAT TERMINATES AT HORIZONTAL PRESSURE WEB AROUND Z= -37. INSTALLED NEW FRAME SECTION USING ANGLE DOUBLER IAW FEDEX EA 8-5310-84845.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 77,619 hrs · 24,327 cycles

FUSELAGE - LEFT AND RIGHT TEE CAPS, STA 1156, CRACKED. LEFT AND RIGHT TEE CAPS REPLACED OVERSIZING AND BUSHING HOLES AND INSTALLING REPAIR DOUBLERS IAW FEDEX EA 8-5310-84882.

Part: DOUBLER — CORRODED (ZONE 500) · corrosion level 2 · airframe 77,619 hrs · 24,327 cycles

LEFT WING UPPER GEAR DOUBLER CORRODED. CORROSION WAS BLENDED OUT AND REPAIRED WITH FILLER AND DOUBLER IAW FEDEX EA 8-571-84840.

Part: CAP — CRACKED (ZONE 500) · airframe 77,619 hrs · 24,327 cycles

LEFT WING RIB UPPER CUP CRACK AT XORS 372. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8-571-80005.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 77,619 hrs · 24,327 cycles

DURING MAINTENANCE INSPECTIONS, FOUND CRACKS ON LOWER CONSTANT SECTION SKINS OF THE HORIZONTAL STABILIZER. THE CRACKS WERE WITHIN FLYABLE LIMITS. P/N: ALC7204-1, ALC7205-1, ALC7206-1. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, FED EX EA 8-5510-80003.