N926FD

Part: CONNECTOR — NOT SEATED (TE FLAPS) · airframe 98,602 hrs · 39,421 cycles

PDIS 926 27-50 0370 06AUG22 FAT OPEN U WHEN SELECTING FLAPS 25 FOR LANDING WE RECEIVED THE TE FLAP DISAGREE EICAS MESSAGE. WE INITIATED A GO AROUND, COMPLIED WITH THE CHECKLIST AND COMPLETED A FLAPS 20 LANDING. THE MESSAGE REMAINED UNTIL MAINTENANCE DIRECTED US TO RETRACT THE FLAPS IN THE GATE. FACT 07AUG22 20:35 FAT LOWERED FLAPS TO 30 AND INSPECTED TRAILING EDGE FLAP SYSTEM. FOUND LEFT FLAP POSITION TRANSMITTER ELECTRICAL CONNECTOR NOT FULLY SEATED REMOVED & CLEANED CONTACTS PER SMP. TESTED OPERATION OF LEFT FLAP POSITION TRANSMITTER PER AMM 27-58-01-5. OPS NORMAL. INSPECTED ALL TRANSMISSION GEARBOX FLUID LEVELS, CHECK GOOD. CHECKED ALL OVERLOAD INDICATORS ON TRAILING EDGE FLAP SYSTEM. NONE TRIPPED. PERFORMED LUBRICTION OF TRAILING EDGE FLAP SYSTEM PER AMM 12-21-09-3. CYCLED FLAP SYSTEM 3 TIMES AND AGAIN WITH ENGINES RUNNINIG. NO FAULTS NOTED REF AMM 27-51-00-2 & JRH. NO HISTORY FOUND. OK FOR SERVICE.

Part: COLLAR — DAMAGED (N/A) · airframe 98,308 hrs · 39,228 cycles

ON ARRIVAL FOUND R1 DOOR GUST LOCK BROKEN. COLLAR ASSY MPN: 654N0244-7 CPN: 5214377 QTY: 1 REMOVED AND REPLACED R1 DOOR GUST LOCK DOOR HOLD OPEN COLLAR WITH ANOTHER PART FROM STOCK AND IT FIT ALL OPS CHECKS ARE GOOD. AMM REF 52-11-08-6. NEW COLLAR FROM ALLIANCE AEROSPACE ENGINEERING PN 10-N6008-4 ...SN 22-0028. ....AC OK FOR SERVICE

Part: NONE — UNKNOWN (N/A) · airframe 98,294 hrs · 39,216 cycles

TE FLAP DISAGREE ON FINAL. QRH COMPLIED WITH. PERFORMED BITE OF ALL 3 FSEU'S FOUND NO CURRENT FAULTS. ATTEMPTED TO DUPLICATE FAULT, OPERATED FLAP/SLATS FROM FAIRED TO 40 UNITS SEVERAL TIMES COULD NOT RECREATE FAULT. SUSPECT FLAP LEVER OUT OF DETENT FOR MORE THAN 25 SECONDS. NO HISTORY FOR THIS ITEM FOR 90 DAYS REF 757-200 FIM 27-51 FAULT TREE 808. NO OTHER FAULTS NOTED OK TO CONTINUE.

Part: FRAME — DAMAGED (BS 1640 S9-20R) · airframe 97,705 hrs · 38,856 cycles

REPAIR INSTRUCTIONS REQUIRED FOR THE ACCOMPLISHMENT OF FEDEX E.A. F-5310-147693, PART 10, SPLICE REPAIR AT STA 1640, S9R TO S20R COMPLIED WITH E.A F-5310-147693 BS 1640 FRAME I-9F - S-20R, FRAME SPLICE

Part: SKIN — DENTED (BS 1699-1740) · airframe 97,705 hrs · 38,856 cycles

FUSELAGE SKIN @ STA 1730, BETWEEN STR 29L - STR 29R, HAS 2EA DENTS. REPAIRED SKIN IAW FEDEX EA # F-5330-146539-P3

Part: LINE — LEAKING (HYD SYSTEM) · airframe 97,458 hrs · 38,706 cycles

A SLOW LOSS OF RIGHT HYDRAULIC SYSTEM FLUID LED TO RIGHT HYDRAULIC SYSTEM FAILURE. COMPLIED WITH QRH, DECLARED AN EMERGENCY. AIRCRAFT WAS AIRBORNE FOR APPROXIMATELY 7-10 MINUTES AFTER RECEIVING THE HYDRAULIC SYSTEM FAILURE INDICATIONS. INSTALLED PRESSURE LINE, BOTH SUPPLY AND CASE DRAIN LINES CONNECTED AND BLOCKS AND SUPPORT BRACKETS INSTALLED. AS WELL AS ALL OTHER CLAMPS AND HARDWARE IAW AMM 20-10-20, LEAK CKS GOOD. INSTALLED Y-DUCT BOOT SEAL TO THE DUCT FLANGE AND ANTI- ICE SUPPLY AT Y-DUCT IAW AMM 36-11-01. LEAK CKS GOOD. INSTALLED ALL PYLON/STRUT ACCESS PANELS IAW AMM 54-53-00. RETURN TO A/C NORMAL CONFIG, OK FOR SVC

Part: DRIVE UNIT — FAILED (TE FLAPS) · airframe 97,304 hrs · 38,619 cycles

WHEN CONFIGURING TO LAND AT SLC IT WAS VERY DIFFICULT TO MOVE FLAP LEVER FROM 20 TO 25 DETENT. WHEN I FINALLY WAS ABLE TO MOVE FLAP LEVER TO 25, WE RECEIVED A TE FLAP DISAGREE EICAS AND LIGHT. FOLLOWED QRH. EMERGENCY DECLARER. FACT 09MAR21 15:45 SLC U INSPECTED FLAPS AND FOUND #1 FLAP DRIVE OVERLOAD INDICATION POPPED. RESET OVERLOAD INDICATION, LUBED FLAP DRIVE AND CYCLED FLAPS. OVERLOAD INDICATION REMAINED IN. REF AMM 12-13-06-30, FIM 27-51 FT 808 FIG 105, AND TECH TIPS 18-0042 ATA 27.

Part: ACTUATOR — INOPERATIVE (AFT CARGO DOOR) · airframe 97,220 hrs · 38,570 cycles

MAIN CARGO DOOR WILL NOT CLOSE. FOUND BOTH LINKS ON AFT MAIN CARGO DOOR ACTUATOR BROKEN. RAISED CARGO DOOR WITH SLING REF B757 AMM CH 52-32-00-4 SO CARGO COULD BE OFFLOADED. REMOVED, REPLACED MAIN CARGO DOOR FWD ACTUATOR SUPPORT LINK ASSY, REF EO F-5230-E0352184-A PART1, 757MM 52-32-04-4 AND 757MM 52-32-00-4. REMOVED MAIN CARGO DOOR AFT ACTUATOR AND ACTUATOR SUPPORT LINK ASSY. REPLACED AFT MCD LIFT ACTUATOR PN 1U1168 SN 373 IAW 757 AMM 52-32-04-4 AND AFT LIFT ACTUATOR SUPPORT ASSY PN B57-52-004-01 REF WRI 52-30-8938, EO F-5230-E0352184-A PART 1. LEAK CHECK AND OPS CHECK GOOD.

Part: STRAP — DAMAGED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT FUSELAGE CIRCUMFERENTIAL STRAP AT STA 1620 FROM STRINGER S-28L TO S-29R PUNCTURED, DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED CIRCUMFERENTIAL SPLICE STA 1620 S-27L TO S27R, IAW SRM 51-40-02 AND DWG 146N3810. MAJOR REPAIR.

Part: STRINGER SPLICE — DAMAGED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT STRINGER S-29L STRINGER SPLICE AT STA 1620 PUNCTURED AND STRINGER FROM STA 1623 TO STA 1630 DEFORMED. REMOVED AND REPLACED STRINGER SPLICE AT STA 1620 S-29L, IAW SRM 51-40-02 AND DWG 146N3820. FOUND STRINGER NOT TO BE DEFORMED IT WAS PRELOADED FROM THE DAMAGED STRINGER SPLICE. MAJOR REPAIR.

Part: STRINGER CLIP — DAMAGED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT STRINGER CLIP AT S30 STA 1616 TO STA 1623 SEPARTED FROM SKIN AND HAS SHEARED FASTENERS AND SURFACE CORROSION. REMOVED AND REPLACED SPLICE STA 1616 TO STA 1623 S-30, IAW SRM 51-40-02 AND DWG 146N3821. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

LOWER FUSELAGE SKINS BETWEEN STA 1540 AND STA 1640 STRINGERS S-30 TO S-26L HAS NUMEROUS PLACES OF DAMAGE. COMPLIED WITH EA F-5330-T0358203 TITLED: FUSELAGE-SECTION 46 LOWER SECTION-REPAIR OF FUSELAGE SKIN INPACT DAMAGE AT STA 1624; S-29L AND EA F-5330-T0358205 TITLED: FUSELAGE-SECTION 46 LOWER SECTION-REPAIR OF FUSELAGE SKINS-CONTAINER IMPACT DAMAGE AT STA 1545-1620 STRINGER S-26L TO S-29L. MAJOR REPAIR.

Part: STRINGER — BENT (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT STRINGER S-27L BETWEEN STA 1588 TO STA 1600 BENT AND DEFORMED. REPAIRED STRINGER S-27L AT STA 1570, IAW SRM 53-00-03-2R. REPAIR BETWEEN STA 1570-STA 1620. MAJOR REPAIR.

Part: SHEAR TIE — BENT (ZONE 100) · corrosion level 2 · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT SHEAR TIE AT STRINGER S-29L TO S-30 DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02. FABED ON VTMAE TRAVELER T20/1525019 STA 1620 AND DRAWING 140N2002. MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT SHEAR TIE AT STA 1620 FROM STRINGER S-28L TO S-29L SHEARED, CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1620 S-28L TO S-29L, IAW SRM 51-40-02. FABED SHEAR TIE ON VT MAE TRAVELER T20/1524174. PART MARKED AS FX-140N2002-248, IAW GMM 7-0-1001 AND DRAWING 140N2002. MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

AFT CARGO COMPARTMENT SHEAR TIE AT STA 1600 STRINGER S-27L TO S-28L SHEARED/CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1600 S-27L TO S-28L, IAW SRM 51-40-02. FABED ON VTMAE TRAVELER T20/1524173 AND DRAWING 140N2002. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 97,049 hrs · 38,472 cycles

FUSELAGE SKIN HAS DENT AND CREASE DAMAGE BETWEEN STA 1520 AND STA 1540 STRAINGERS S-25L TO S-26L. COMPLIED WITH EA F-5330-T0358196 PART 1 TITLE: FUSELAGE-SECTION 46 LOWER SECTION REPAIR OF FUSELAGE SKIN INPACT DAMAGE AT STA 1520-1540 S-26L. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 765) · corrosion level 2 · airframe 96,714 hrs · 38,273 cycles

MAIN DECK, BS 765 RT INBD CREASE BEAM WAS CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, AND OUT OF LIMITS IAW SRM 53-30-13, FIG 101. REPAIRED THE CREASE BEAM IAW SRM 53-00-13-2R, REP 1, ALT 1.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 96,380 hrs · 38,068 cycles

PDIS 926 27-50 8236 07MAR20 RNO FACT U LOGPAGES:3215684 EXTENDING FLAPS FROM 15*- 20* RECEIVED TE FLAP DISAGREE CAUTIN MESSAGE. FLAPS STOPPED MOVING AT 17*. COMPLIED WITH QRH, LANDED UNEVENTFULLY. FACT 07MAR20 14:20 RNO U RETURNED A/C BACK TO NORMAL CONFIG. PERFORMED SYSTEM OPS OF SLATS AND TE FLAP SYSTEM I.A.W. M/M 27_51_00_2_0 AND FIM 27_51_00_815_808. OPS NORMAL. NO HISTORY AND NO FAULTS LOGGED. A/C TO CONTINUE.

Part: SKIN — DAMAGED (BS 510-515 S26L) · airframe 96,248 hrs · 37,991 cycles

THE LH SIDE OF THE FUSELAGE FROM STA 510-515 2"-4" DOWN FROM STR 26L HAS SEVERAL DEEP PITS FROM LIGHTNING STRIKE. REPAIRED DAMAGE IN FUSELAGE SKIN CAUSED BY LIGHTNING STRIKE. INSTALLED DOUBLER REPAIR PER EA F-5330- T0351859.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,954 hrs · 37,791 cycles

FORWARD CARGO COMPARTMENT, BS 740 JUST ABOVE STRINGER 22R FRAME IS CRACKED AT TOOLING HOLE. VERIFIED BY HFEC (OPEN HOLE) INSPECTION, CIRCLED HOLE IN BLACK.

Part: DOOR — CRACKED (L2) · airframe 95,954 hrs · 37,791 cycles

POSSIBLE CRACK ON L2 DOOR UPPER HINGE CUTOUT ALL WORK ACCOMPLISHED IAW EA F-5210-T0348085 P1 DOORS - PASSENGER/CREW - CARGO - L -2 DOOR FORWARD FRAME UPPER HINGE CUT-OUT SRM REPAIR - RSC TRACKING.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

AFT CARGO COMPT STA 1440 AT STR 29R TAPERED FILLER ON STRINGER HAS EXFOLIATING CORROSION. FOUND TAPERED FILLER AT STA 1440 STR 29R OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW SRM 53-00-03-1A FIG 101. FABRICATED NEW TAPERED FILLER IAW DWG 146N3821 REV P AND REV B. TAPERED FILLER WAS REMOVED AND INSTALLED ON N00785.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

AFT PIT - BS 1440, STR. 29 RT HAS CORROSION ON I/B SIDE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA 1180-1200 LBL44.5 SEAT TRACK FANGE CORRODED EVALUATED SEAT TRACK STA 1180-1200 LBL 44.5 ORIG MAT .070 REM .00 LOSS .070 OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, 51-40-05 AND 53-60-52 AND DWG 146N5123 REV -.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA 1040-1055 BLO CORROSION ON SEAT TRACK FLANGE. REMOVED CORR ON SEAT TRACK (FLANGE) SUPPORT STA 1040-1055 BL0 IAW SRM 51-10- 02. ORIG MAT.070 REM .054 LOSS .016 OUT OF LIMITS IAW SRM 53-00-52 FIG 101. REMOVED, LOCATED, DRILLED, TRIMMED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 144N8031 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN STA 1195 BL0 SEAT TRACK FLANGE CORRODED.

Part: SKIN — DENTED (FUSELAGE) · airframe 95,954 hrs · 37,791 cycles

LT FUSELAGE OUTER SKIN AT FS 215 AROUND S-21L HAS A DENT. EVALUATED DENT ON SKIN STA. 215 AROUND S-21L A\Y FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A. HFEC IAW NDTM PT6 51-00-19 CRACK NOTED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, AND INTALLED DOUBLER IAW SRM 53-00-51-2R REP 29. FABRICATED AND INSTALLED FILLER IAW SRM 53-00-51-2R REP 29.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA. 1015 - 1021 BLB 24.75 FLOORBEAM T CHORD CORRODED.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA. 1680 - 1720, BL0 RBL53 FLOOR WEB CORRODED ALL WORK ACCOMPLISHED IAW EA F-5310-T0348184 P1 FUSELAGE - MAINFRAME - AFT SHEAR DECK PLATE CORROSION REPAIR FROM STA 1681 TO 1720 NEAR RBL 51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA. 920 - 1040 RBL 24.75 FLOOR BEAM T CHORD CORRODED REMOVED CORR ON T-CHORD STA 920-1040 RBL 24.75 IAW SRM 51-10-02. ORIG MAT .090 REM .045 LOSS .045 OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 REMOVED, LOCATED, DRILLED, TRIMMED AND INSTALLED NEW T-CHORD IAW SRM 51-40-02 AND DWG 111N5202 REV J.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,954 hrs · 37,791 cycles

MAIN CABIN BETWEEN STA. 1620 - 1640 RBL 44.5 SEAT TRACK FLANGE CORRODED REMOVED CORR ON SEAT TRACK FLANGE STA 1620-1640 RBL 44.5 IAW SRM 51-10-02. ORIG MAT. .070 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05 AND 51-40-08 AND 53-60-52-01 FIG 101.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 95,575 hrs · 37,561 cycles

REMOVE AND REPLACE LBL 45.50 SEAT TRACK FROM BS440 TO BS680 COMPLIED WITH - EQUIP AND FURNISH - CARGO - LOADING SYSTEM - INTERIM REPAIR FOR DAMAGE SEAT TRACK LOBE, STA 579.95 LBL 45.50 EA# TF - 2550-T0343358 P3.

Part: THERMAL SWITCH — FAILED (LT ENGINE) · airframe 95,160 hrs · 37,307 cycles

LT ENG STRUT OH DET 1 EICAS MESSAGE ON STATUS PAGE DURING CLIMB OUT TO 360. FOUND THERMAL SWITCH S10196 GIVING AN OVERHEAT DETECTION INDICATION BEFORE TEMPERATURE THRESHOLD. REMOVED AND REPLACED THERMAL SWITCHES S10194, S10195, AND S10196 FOR THE LEFT STRUT OVERHEAT LOOP 1, OPS CHECK GOOD IAW AMM 26-12-01-4.

Part: CIRCUIT CARD — FAILED (OVERHEAT SYS) · airframe 95,156 hrs · 37,306 cycles

WHILE CLIMBING THROUGH FL340 TO 360, LT ENGINE OVHT EICAS MESSAGE ON. PERFORMED QRH, LIGHT EXTINGUISHED AT 1.28 EPR. IAW FIM R&R AFOLDS CARD IAW AMM 26-10-01-4 AND PERFORMED TEST TEST GOOD.

Part: UNKNOWN — MALFUNCTIONED (SPOILERSYS) · airframe 95,071 hrs · 37,263 cycles

AT SPEEDBRAKE DEPLOYMENT A ROLE TO THE LEFT OCCURS WITH A DISPLACEMENT OF THE YOKE TO THE RIGHT. AT DEPLOYMENT YOKE DISPLACES 1.5 UNITS ON AILERON TRIM INDICATOR, ONCE DEPLOYED THE YOKE IS DISPLACE 1.0 UNITS TO THE RIGHT. PERFORMED OPERATIONAL TEST OF SPOILER/SPEED BRAKE SYSTEM IAW AMM 27-61-00-5, WITH NO DEFECTS NOTED. PHYSICALLY VERIFIED THAT ALL SPOILER SURFACES CANNOT BE MOVED WHEN DEPLOYED. PERFORMED BITE TEST OF ALL SCMS IAW FIM 27-09-00, NO FAULTS FOUND. VERIFIED THAT ALL PCA TEMPS WERE WITHIN SIMILAR RANGE AND FOUND NONE OVERHEATED. PERFORMED SUCCESSFUL LAND 30 TEST IAW AMM 22-00-02-2, AND FOUND NO FAULTS. A/C HAS NO HISTORY AND IS OK TO CONTINUE SERVICE AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 95,014 hrs · 37,220 cycles

RT R1 DOOR EXTERIOR SLIDE LIGHT INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY M00730 PER MM CH 33-51-07-2. A/C READY FOR CONT SERVICE.

Part: BRACKET — LOOSE (LT WING TE FLAP) · airframe 94,185 hrs · 36,755 cycles

FLAP FAIRING BRACKET FOR 573HB IS LOOSE. REPAIRED THE LT, INBD MAIN FLAP IAW SRM 57-53-02-2R, REPAIR 3, AND EA F-5750-T0334988, PI.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 94,185 hrs · 36,755 cycles

LEFT WING NR 3 SLAT UPPER SURFACE HAS A DENT AT CENTER OF SLAT AT T\E. REPAIRED THE LT WING SLAT IAW SRM 51-70-10-2R, PARAG 8 AND 20.

Part: SEAT TRACK — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 94,185 hrs · 36,755 cycles

MAIN CABIN, BS 1640 - 1660, RBL 45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED CORROSION IAW SRM 51-10-02-0G, 100 PERCENT LOSS. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1640-1680) · corrosion level 2 · airframe 94,185 hrs · 36,755 cycles

MAIN CABIN, BS 1640 - 1680, LBL45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED THE CORROSION IAW SRM 51-10-02 WITH 100 PERCENT MATERIAL LOSS. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G.

Part: SEAT TRACK — CORRODED (BS 345-365) · corrosion level 2 · airframe 94,185 hrs · 36,755 cycles

MAIN CABIN SEAT TRACK BS 365 - 345, LBL 6 HAS CORROSION. REMOVED THE CORROSION AND FOUND 100% LOSS IAW SRM 51-10-02, & 53-00-52-1A. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 AND SRM 51-40-02-OG. FABRICATED THE NEW SEAT TRACK IAW DWG 3504-NC-2.

Part: SIGHT GAUGE — CLOUDY (PAX DOOR SLIDE) · airframe 93,985 hrs · 36,634 cycles

LEFT ENTRY DOOR INSPECTION WINDOW FOR SLIDE PRESSURE GAUGE IS HAZED, MAKING IT DIFFICULT TO READ. CLEANED THE SIGHT WINDOW IAW AMM: 20-30-02-2. OK FOR SERVICE.

Part: COMPUTER — OUT OF ADJUST (PITCH CONTROL) · airframe 93,677 hrs · 36,462 cycles

AIRCRAFT PITCH CONTROL HAS LAG ON PREFLIGHT CONTROL CHECK AND ON ARRIVAL PITCH AXIS WAS STIFF AND SEEMED TO HAVE A DELAY IN CONTROL. ADJUSTED AND TESTED OF ELEVATOR FEEL COMPUTER IAW AMM 27-31-19-4. LEAK AND OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: WARNING BELL — FALSE ACTIVATION (FIRE DETECTION) · airframe 93,601 hrs · 36,419 cycles

TRIED TO SWITCH TO GROUND POWER AFTER BLOCKIN, THE FIRE BELL SOUNDED FOR 10 SECONDS. NO FIRE LIGHTS ILLUMINATED. NO OTHER INDICATIONS OF FIRE OR ANY OTHER MALFUNCTION. STARTED THE APU AND SHUTDOWN THE LEFT ENGINE. FIRE DETECTION SYSTEM OPS CHECKED NORMAL IAW MM 26-11-00-5.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 925 hrs · 35,683 cycles

FIRE BELL ACTIVATED AT LIFTOFF, NO VISUAL INDICATIONS OF FIRE, COULD NOT CANCEL BELL. R & R BELL CHIME WARNING CARD AS REQUIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 922 hrs · 35,543 cycles

PROTRUDING DENTS, STATION 643, STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.

Part: SKIN — GOUGED (TE FLAP) · airframe 922 hrs · 35,543 cycles

LEFT WING INBD FLAP, UPPER SURFACE HAS 1 EACH DEEP GOUGE AT WS 270. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.

Part: SKIN — GOUGED (TE FLAP) · airframe 922 hrs · 35,543 cycles

LEFT WING INBD FLAP, UPPER SURFACE HAS 2 EACH DEEP GOUGE AT WS 258. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.

Part: SKIN — DENTED (BS 630) · airframe 922 hrs · 35,543 cycles

PROTRUDING DENTS, BS 630 STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.

Part: SKIN — GOUGED (NR 2 PYLON) · airframe 922 hrs · 35,543 cycles

NUMBER 2 ENG AFT PYLON, INBD SIDE HAS A GOUGE. ACCOMPLISHED WORK IAW EA F-5480-T0319007 P 1.

Part: SKIN — BULGED (BS 395) · airframe 922 hrs · 35,543 cycles

SKIN BULGE AT UPPER LOBE BS 395, BETWEEN STRINGERS 6 - 7R. REMOVED DAMAGED AREA IAW SRM 53-00-01-2R. FABRICATED DOUBLER IAW SRM 53-00-01-2R. INSTALLED THE DOUBLER IAW SRM 53-00-01-2R FIG 201 REPAIR 16.

Part: LIGHT — UNSECURE (COCKPIT) · airframe 921 hrs · 35,494 cycles

AFTER BLOCK IN, UNARMED, LIGHT ON EMER LIGHT PANEL FELL OUT. R & R THE UNARMED SWITCH LIGHT ASSEMBLY IAW AMM 33-13-00-2. OPERATIONS CHECKED GOOD. ACFT OK TO CONTINUE.

Part: GOVERNOR — MALFUNCTIONED (RT ENG FUEL FLOW) · airframe 91,224 hrs · 34,886 cycles

THE RT ENGINE SPOOLED UP UNCOMMANDED WITH BOTH THROTTLES AT IDLE. WHEN ON FINAL AT 2000' AGL, 170 KNOTS, WITH LT ENG IN FLIGHT IDLE, THE RT ENGINE WAS APPROXIMATELY 1.33 EPR, 74% N1 590 EGT, N2, N3 & FUEL FLOW ALL CORRESPONDING TO THE RT ENG STABILIZED AT A HIGH PWR SETTING. THE LT ENGINE WAS NORMAL AT ALL TIMES. DURING SUBSEQUENT APPROACH THE RT ENGINE REMAINED AT A HIGH POWER SETTING WITH THE RT THROTTLE AT IDLE. QRH PROCEDURES FOLLOWED TO SHUTDOWN RT ENGINE. REPLACED RT ENGINE FUEL FLOW GOVERNOR IAW AMM 73-21-01-4-4.

Part: STRINGER — CORRODED (BS 1440 S29L) · corrosion level 2 · airframe 90,345 hrs · 34,219 cycles

CORROSION ON STRINGER 29L BS 1440. CUT OUT DAMAGED STRINGER, FABRICATED AND INSTALLED REPAIR ON STRINGER IAW SRM 53-00-03 FIG. 201 REPAIR 2, 51-40-02, 51-40-03, AND SRM 53-00-00 PAGE 1 GENERAL.

Part: BEARING — FAILED (L1 DOOR HANDLE) · airframe 89,717 hrs · 33,767 cycles

L1 DOOR UNABLE TO BE CLOSED FROM THE OUTSIDE, THE EXTERNAL HANDLE WON`T COME OUT TO THE FULLY FLARED (BUTTERFLY) POSITION. REPLACED CAM FOLLOWER BEARINGS IN EXTERIOR HANDLES IAW MM 52-11-13-2, PROCEDURE E, THROUGH (R). TO SUPPORT FITTING NR 16. DOOR HANDLE INSTALLED IAW MM 52-11-13-2. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 89,520 hrs · 33,629 cycles

L1 DOOR ASSIST BOTTLE LOW. REPLACED L1 EMERGENCY POWER RESEVOIR IAW AMM 52-11-30-4.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 89,496 hrs · 33,612 cycles

DURING OPENING OF LT MAIN ENTRY DOORWAY, SLIDE BUNDLE FELL FROM STORAGE CONTAINER. REMOVED SLIDE. INSTALLED L1 SLIDE PACK IAW AMM 25-66-01-4.

Part: DOOR — MISSING (RT NACELLE) · airframe 88,940 hrs · 33,234 cycles

RT ENGINE IDG SERVICING DOOR MISSING. R AND R DOOR IAW SRM 51-40-02.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 88,916 hrs · 33,219 cycles

L1 DOOR WILL NOT DISARM PROPERLY. CANNOT MOVE TO DISARM WITHOUT MOVING HANDLE ALSO. HANDLE DOES NOT POSITIVELY GO INTO DISARM BAND. REMOVED ACCESS COVER FOR DOOR SLIDE. FOUND GRIT BAR NOT GOING LOW ENOUGH TO SLIDE INTO FLOOR FITTINGS MM REF 25-66-01-4; 25-66-10-2. FOUND FWD GIRT BAR CRANK CAM OUT OF ADJUSTMENT. ADJUSTED VERTICAL POSITION OF THE CAM ASSY TO CORRECT DIMENSION IAW MM 52-11-25-5. OPS CHECKED NORMAL.

Part: SEAL — DIRTY (COCKPIT WINDOW) · airframe 88,628 hrs · 33,033 cycles

VERY LOUD SQUEEL (AIR NOISE) ON THE BOTTOM OF THE R2 WINDOW. NOISE STARTED ABOUT 6.0 PSID ON CLIMBOUT AND WAS VERY LOUD AND DISTRACTING. REMOVED SMALL DEBRIS FROM R2 WINDOW FRAME, CLEANED AND INSPECTED R2 WINDOW SEAL. SEAL IS IN VERY GOOD CONDITION. CHECKED R2 WINDOW OPERATION, NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE. REF MM 56-11-02-5 AND FIM 56-11.

Part: SKIN — PUNCTURED (NR 1 SLAT) · airframe 88,617 hrs · 33,019 cycles

LEFT NR 1 SLAT HAS A PUCTURE AT 55.5 INCHES FROM INBD EDGE AND 6.5 INCHES FROM T/E OF SLAT HOLE IS .5" X .75". REMOVED DAMAGED SKIN AND CORE, FABRICATED CORE PLUG AND DOUBLER, BONDED AND SEALED REPAIRED AREA IAW SRM 51-70-10, REPAIR NR 2 AND EA F-5750-155424, ON NR1 SLAT, MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 88,606 hrs · 33,011 cycles

FUSELAGE SKIN DAMAGED DURING INSTALATION ON SURROUND STRUCTURE AT STA 439 BETWEEN S-2L TO S-3L COMPLIED WITH EA F-5330-146550 REF FAA FORM 8110-3. MAJOR REPAIR.

Part: BUSHING — GOUGED (NR 2 PYLON) · airframe 88,606 hrs · 33,011 cycles

RIGHT PYLON OTBD WING STRUT BUSHING HAS GOUGES. R & R BUSHING IAW SOPM 20-50-03 AND EA F-5720-146285. MAJOR REPAIR

Part: SKIN — DAMAGED (LT STRUT) · airframe 88,606 hrs · 33,011 cycles

LEFT PYLON, LT SIDE SKIN AT P/P STA 204 HAS ELONGATED HOLE. NACELLE/PYLON - SKIN GOUGE ADJACENT TO TOOLING HOLE, COMPLIED WITH/ REPAIR IAW EA F-5450-146516. THIS IS A CAT "A" MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1654) · airframe 88,606 hrs · 33,011 cycles

FUSELAGE INTERIOR UPPER DOOR REINFORCEMENT STRAP HAS GOUGE APPROX AT STA 1653 ABOVE R-4 DOOR CUTOUT. ACCOMPLISHED FUSELAGE MAIN FRAME- SECTION 46 - UPPER DOOR SILL STRAP REPAIR, BS 1654, IAW EA F-5310-146288, DATED 04/25/2011. REF FORM 8100-9 DATED 05/19/2011. FIRST STAGE APPROVAL, DTI MUST BE ISSUED WITHIN 24 MONTHS FROM DATE OF FORM. MAJOR REPAIR.

Part: FLOORBEAM — MISREPAIRED (BS 324) · airframe 88,606 hrs · 33,011 cycles

FLOORBEAM REPAIR AT STA. 324, RBL 45 - RBL 60 UPPER TEE REQUIRES REPLACEMENT DUE TO NOT BEING IAW APPROVED DATA. REMOVED UPPER TEE ON FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW TEE. INSTALLED TEE, IAW SRM 51-40-02, AND DWG 141N2932, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 540-550) · airframe 88,606 hrs · 33,011 cycles

FUSELAGE EXTERNAL SKIN REPAIR AT STA 540-550, STR-27L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. R & R DOUBLER & FILLER STA 540-550 STR -27L IAW SRM 51-40-02 /SRM 53-00-01, FIG 201, TABLE I - III, REPAIR 15, W/ DOUBLER PN 2024-T3-071, BATCH 1941519. FILLER PN 2024T3, .051 & BATCH 1965845. HFEC CUTOUT IAW NTM 51-00-19. HFEC HOLES IAW NTM 51-00-16, CATEGORY B (REPAIR 15) LEFC METHOD OF INSP IAW NDT 53-00-06 WITH INITIAL AT; F/C 29,000 INTERVALS EVERY 3,000 F/C. MAJOR REPAIR CAT B.

Part: STRINGER — MISREPAIRED (BS 1450-1470 S28) · airframe 88,606 hrs · 33,011 cycles

EXISTING STRINGER REPAIRS AT STA 1450-1470, STR 28L REQUIRES REPLACEMENT DUE TO NOT BEING INSTALLED IAW APPROVED DATA. REMOVED AND REPLACED EXISTING STRINGER REPAIRS, BS 1450-1479, S28L, PER SRM 53-00- 03, REPAIR NR 2, DETAIL 1. FABRICATED HAT SECTION, 2EA., FILLER, ON TRAVELER# T11/880107, T11/880960, T11/880108. PART MARKED PER GMM 7-0-1001. CAT. "A" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 730-750) · airframe 88,606 hrs · 33,011 cycles

EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STA. 740, STR 25R REQUIRES REPLACEMENT DUE TO NOT BEING IN COMPLIANCE WITH APPROVED DATA. REMOVED EXISTING DOUBLER/FILLER, BS 730-750, S-25R. HFEC INSP. SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6 AND NTM 51-00-16, PT.6, NO CRACKS NOTED. FABRICATED DOUBLER & FILLER. INSTALLED NEW DOUBLER & FILLER PER SRM 53-00-01, REPAIR 15. ZONE "A", CAT. "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 740-760) · airframe 88,606 hrs · 33,011 cycles

SKIN REPAIR AT STA.740-760, STR 27R TO 28R REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED DOUBLER/FILLER AT BS 740-760, S-27R-S-28R, PER SRM 51-40-02. HFEC SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6, AND NTM 51-00-16, PT.6. NO CRACKS NOTED. FABRICATED DOUBLER, INSTALLED NEW DOUBLER/FILLER AT BS 740-760, S-27R-S-28R, PER SRM 53-00-01, REPAIR 15. ZONE "A", CAT. "B" MAJOR REPAIR.

Part: CHANNEL — MISMANUFACTURED (BS 1620-1640) · airframe 88,606 hrs · 33,011 cycles

UNABLE TO INSTALL CHANNEL SPLICE, BETWEEN STA 1620 TO STA 1640, RBL 60, WL 208.1, WILL HAVE SHORT EDGE CONDITION AT (1 EA) 0.100 HOLE LOCATION AT BS 1620 - 1640 RBL 60 A CREASE BEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118350449EZR06 AND MAE EA 757-5361-16-F3249. CLASSIFIED AS A MAJOR.

Part: FRAME — GOUGED (BS 1140, S2L) · airframe 88,606 hrs · 33,011 cycles

FRAME AT BS 1140, S2L, IS GOUGED. REMOVED DAMAGED SECTION OF FRAME IAW SRM 51-40-02. LOCATED, TRIMMED AND DRILLED FRAME AND SPLICES SRM 53-00-07, P.201/202, FIG 201. TREATED AND PRIMED FRAME AND SPLICES IAW SRM 51-20-01. INSTALLED FRAME REPLACEMENT AND 4 EA SPLICES IAW SRM 53-00-07, P 201/202, FIG.201, REPAIR NR 3, AT BS 1140, S2L, CAT "B" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1640) · airframe 88,606 hrs · 33,011 cycles

SECTION 46, STA 1640, LBL63.0 BETWEEN WL207-200 UNABLE TO LOCATE 657N3161-11 FITTING DUE TO EXISTING FASTENER HOLES ON THE FRAME, 2 EA ARE NOT POSITIONED AS DEPICTED ON DWG 657N3160, SH 2, REV D -FIGURE "E". AT BS 1640, LBL 63, WL 207, FRAME REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399EZ2R03 AND EA 757-5362-16-F3207, REV -, DATED 03/07/11. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY AND IS CLASSIFIED AS A MAJOR REPAIR. REF EA F-5310-146549, FOR DTA TRACKING, AND FORM 8110-3, DATED 05/24/2011, FOR FIRST STAGE APPROVAL.

Part: SEAT TRACK — DAMAGED (BS 1280) · airframe 88,606 hrs · 33,011 cycles

SEAT TRACK INSTL SEC46 UNABLE TO INSTALL 657N3311-1 SPLICE FITTING AT STA 1280 LBL 45.50, EXISTING FASTENER HOLES ON FLOORBEAM WEB ARE NOT POSITIONED ON DWG 657N3311, SH 5 AND SEAT TRACK 657N3318-7 REQ TO TRIM FWD EDGE FLANGE .300 APPROX TO MAINTAIN .100-.060 GAP WHICH WILL INTERFERE WITH INSTALLATION OF THE MOD. REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350420EZ2R02, AND EA 757-5365-16- F3195, REV. -, DATED 02/23/11. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY AND CLASSIFIED AS A MAJOR REPAIR. REF. 8110-3 DATED 05/24/11 FOR APPROVAL.

Part: CREASE BEAM — DAMAGED (BS 1620-1640) · airframe 88,606 hrs · 33,011 cycles

UNABLE TO INSTALL 657N4308-1 CHANNEL SPLICE, BETWEEN STA.1620 TO STA 1640, LBL60.00 WL208.1; WILL HAVE SHORT EDGE MARGIN CONDITION AT -1 EA.- 0.10" HOLE LOCATION. AT BS 1640, LBL60, WL208 A CREASE BEAM REPAIR WAS ACCOMPLISHED. CLASSIFIED AS A MAJOR.

Part: SKIN — MISREPAIRED (BS 775) · airframe 88,606 hrs · 33,011 cycles

FUSELAGE SKIN REPAIR 60" AFT OF L2 DOOR, 6" ABOVE FLOORLINE REQUIRES REPLACEMENT, DUE TO NOT COMPLYING TO APPROVED DATA. REMOVED AND REPLACED DOUBLER AT BS 775, S16L-S17L, PER SRM 51-40-02, AND SRM 53-00- 01, REPAIR 16, BATCH 1928869, PER SRM 53-00-01, FIG.201, P.203, TABLE 1 AND 2. HFEC CUTOUT WITH NO CRACKS NOTED, PER NTM 51-00-19, PT.6, AND HFEC HOLES WITH NO CRACKS NOTED PER NTM 51-00-16, PT.6. THIS IS A CAT. "B" MAJOR REPAIR, PER SRM 53-00-01, REPAIR NR 16, WITH THE FOLLOWING TRACKING; INITIAL AT 16,000 FC, THEREAFTER EVERY 3,000 FC, LFEC METHOD OF INSPECTION.

Part: SEAT TRACK — GOUGED (BS 1075-1180) · airframe 88,606 hrs · 33,011 cycles

SEAT TRACK AT STA 1075-1180, RBL45.50 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS. SEAT TRACK FROM BS 1075-1180, RBL 45.5, OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, P 102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 00019046632 AND INSTALLED IAW SRM 53-40-52/ 51-40-02, AT BS 1075-1180, RBL 45.5. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 274-285) · airframe 88,606 hrs · 33,011 cycles

EXISTING FUSELAGE SKIN REPAIR AT STA 274-285, STR 16L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED AND REPLACED EXTERNAL FUSELAGE SKIN DOUBLER / REPAIR AT STA 274- 285, STR 16L IAW SRM 53-00-01 FIG 201 REPAIR 15. CAT. "B" REPAIR WITH SUPPLEMENTAL INSPECTIONS REQUIRED. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1075-1180) · airframe 88,606 hrs · 33,011 cycles

SEAT TRACK AT RBL24.75 FROM STA 1075-1180 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS, SEAT TRACK FROM BS 1075-1180, RBL 24.75 OUT OF LIMITS IAW SRM 53-00-52, FIG101, DETAIL 1, P.102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 000194663 AND INSTALLED AT BS 1075-1180, RBL 24.75, IAW SRM 53-40-52 / 51-40-02. MAJOR REPAIR.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 88,606 hrs · 33,011 cycles

VERTICAL STABILIZER LT FIXED T/E BEAM IS CRACKED AT RUD STA 97.354 SDR ENTERED IN ERROR. CONSIDERED MINOR REPAIR

Part: FRAME — DAMAGED (BS 1640) · airframe 88,606 hrs · 33,011 cycles

FRAME STA 1640, RBL 63, WL 208 HAS INCOMING DAMAGE, 2 EA AREAS ON INBD J ANGLE, 2 EA GOUGES AND THE WEB HAS CUT. FRAME REPAIRED

Part: SILL — MISREPAIRED (BS 1290-1405) · airframe 88,606 hrs · 33,011 cycles

REPAIR ON DOOR SILL/CREASE BEAM AT STA 1370, WL 208, RBL 62 REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R CREASE BEAM CHORD, FROM BS 1290-1405, RBL 62, PN: 146N8326-2, BATCH NR 2032339, IAW SRM 51-40-02, AND DWG 146N8326. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1640) · airframe 88,606 hrs · 33,011 cycles

FRAME STA 1640, RBL63, WL208 HAS 2 EA AREAS OF DAMAGE INBD JANGLE HAS EEA GOUGES AND THE AFT FRAME WEB HAS CUT (INCOMING DAMAGE FOUND AFTER FLOORBEAM REMOVAL) THIS SDR WAS GENERATED IN ERROR. THE ABOVE DISCREPANCY IS CAPTURED ON THE FAA FORM 337, WHICH IS ISSUED TO THE ACFT AT THE END OF THE CONVERSION.

Part: BEAM — MISINSTALLED (FUSELAGE) · airframe 88,606 hrs · 33,011 cycles

UNABLE TO INSTALL 657N3338-36 SPLICE AND 657N338-30 ANGLE CLIP AT STA 1180 RT DUE TO THE INCOMING CONDITION OF THE 144N5214-1 RT INBD CHORD LOCATION TOO FAR INBD. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION , ON MAE MOD W/C 118350453CZR03, AND EA 757-5341-16-F3189, REV.-, DATED 02/28/11. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY AND CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 88,606 hrs · 33,011 cycles

AFT CARGO STA. 1400 TO STA.1420 AT BL 0 FLOOR SUPPORT WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG. 101 DETAIL V, REMOVED AND REPLACED FLOOR SUPPORT WEB IAW SRM 51-40- 02 AND SRM 53-00-53, REPAIR CLASSIFIED AS MINOR SDR SUBMITTED IN ERROR PER BOEING 757 SRM 51-00-04

Part: FLOORBEAM — MISALIGNED (BS 700) · airframe 88,606 hrs · 33,011 cycles

STA 700 INCOMING REPAIR AT RBL40 WILL INTERFERE WITH PTF MOD. R & R FLOORBEAM AT STA 700, BETWEEN RBL 70 TO LBL 70". BAC1518-338/18A, BATCH NR 0001922129, IAW SRM 53-30-51, FIG 1, PAG-4 AND SRM 51-40-02, AND REINSTALLED ATTACH PARTS, FROM ITEM 3 THRU 12, IAW SRM- 51-40-02, & DWG 143N5014. MARKED PART IAW GMM 7-0-100-1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,606 hrs · 33,011 cycles

STA 377, FLOORBEAM, LBL-60 HAS CORROSION ON LAWER SIDE OF UPPER FLANGE AROUND NUT PLATE HOLES. REMOVED CORROSION AND CHECK LIMITS ORIG MAT. 0.125 AFTER REWORK 0.050. FOUND OUT OF LIMITS IAW SRM 53-00-51 DET III. R & R FLOORBEAM IAW SRM 51-40-02 WITH MAT PN BAC1518-338, MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1280) · airframe 88,606 hrs · 33,011 cycles

FRAME AT STA 1280 HAS GOUGES BETWEEN AREAS OF STR 11R-17R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P103; ORIGINAL MATERIAL IS .071", AFTER REWORK IS .050", LOSS IS .021". R & R FRAME SPLICE AT BS 1282, S12R-S13R, IAW SRM 53-00-07, FIG 201, REPAIR NR 3. BS 1280 FRAME, ITSELF, WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2. CAT "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING; INITIAL AT 10,000 FC, THEREAFTER EVERY 12,000 FC, USING LFEC METHOD.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 88,606 hrs · 33,011 cycles

BS 418-440, RBL 45, SEAT TRACK GOUGED. BLENDED AREA AND CHECKED LIMITS IAW SRM 53-00-52. ORIGINAL MATERIAL WAS .053", AFTER REWORKIS .047", LOSS WAS .060", FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. REMOVED SEAT TRACK AT BS 418-440, RBL 45, IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK FROM PN BAC 1520-792, BATCH NR 1904663, IAW SRM 53-10-52, FIG 1, DETAIL 2. INSTALLED NEW SEAT TRACK AT BS 418-440, RBL 45, IAW SRM 51-40-02. NEW PART, PART- MARKED FX141N5131 IAW SOPM 20-50-10. MAJOR REPAIR

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 88,606 hrs · 33,011 cycles

BS 418-440, RBL 24, SEAT TRACK GOUGED. BLENDED AREA IAW SRM 53-00-52, FIG 101, DETAIL 1. CHECKED LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, AND FOUND OUT OF LIMITS; BEFORE: .53", AFTER: .47", LOSS: .060". REMOVED SEAT TRACK IAW SRM 51-40-02, AT BS 418-440, RBL 24. FABRICATED NEW SEAT TRACK FROM PN BAC 1520-792, IAW SRM 53-10-02, FIG.1, DETAIL 2. INSTALLED NEW SEAT TRACK AT BS 418-440, RBL 24, IAW SRM 51-40-02. NEW PART, PART MARKED FX141N5131, IAW SOPM 20-50-10. MAJOR REPAIR

Part: FRAME — GOUGED (BS 1280) · airframe 88,606 hrs · 33,011 cycles

MDC FRAME AT STA 1280 HAS GOUGES ON AREAS BETWEEN STR S11L & S17L. REPAIRED IAW EA F-5310-146523, MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365.25) · airframe 88,606 hrs · 33,011 cycles

MAIN DECK, BS 365.25 FLOORBEAM, BETWEEN RBL 45 - 58, UNDERNEATH UPPER CHORD, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION BY BLENDING AREA IAW SRM 51-10-02 AREA OUT OF LIMITS. ORIGINAL MAT .125 AFTER REWORK .077 EXCEEDS MAX ALLOWABLE DAMAGE OF 10 PERCENT AREA OF DAMAGE 1.8" (L) X 1" (W). REMOVED DAMAGED AREA OF UPPER CHORD STA 365 IAW SRM 51-10-02. FABBED REPAIR CHORD FROM MAT BAC 1505-100880 REPAIR STRAPS ON TRAVELER T11/869650 AND REPAIR ANGLES ON TRAVELER T11/869649 IAW SRM 53-00-51, FIG 201, TABLE 1. INSTALLED REPAIR CHORD, ANGLES AND STRAPS IAW SRM 51-40-02. THIS IS A MAJOR REPAIR.

Part: FEEDER CABLE — BURNED (BS 405, S5L) · airframe 88,606 hrs · 33,011 cycles

POWER FEEDER CABLE, PN: W2800-0006-2/0, AT BS 405, S5L, IS BURNED AND ARCHED. STAND OFF SUPPORT ROD IS BURNED OFF AS WELL. R & R APU POWER FEEDER CABLE IAW SWPM 20-10-21, AND WDM 24-21-41. STANDOFF SUPPORT ROD DISPOSITIONED ON MOD W/C 118450613AZD. OPS CHECK IS GOOD IAW AMM 24-21-00-5. MINOR REPAIR.