N771FD

Part: WINDOW — SPARKS (COCKPIT) · airframe 81,467 hrs · 31,893 cycles

DURING PREFLIGHT, SELECTED WINDOW HEAT SWITCHED ON AND IMMEDIATELY HAD RIGHT SIDE WINDOW PRODUCE LARGE SPARK AND AND BEGIN SMOKING. WINDOW SPIRAL HEAT CORD AND TEST WINDOW HEAT, BOTH ACCOMPLISHED, ALSO REF AMM 30-41-00-5 FOR WINDOW HEAT TEST OK.

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 81,261 hrs · 31,753 cycles

DURING ROTO PROBE OF OPEN HOLES AT RH BS 1640 PER EO F-5310-E0344602. A CRACK INDICATION WAS NOTED IN THE BOTTOM INBD HOLE. THE CRACK IS IN THE FRAME AT APPROX. 3:00 O'CLOCK. COMPLIED WITH EA F-5310-T0361948 AND COMPLETED ALL STEPS 1-17 FUSELAGE - MAINFRAME - CRACK INDICATION AT RH STA 1640 FUSELAGE FRAME WEB AT S-14R, LOWER INBD HOLE LOCATION - FREEZE PLUG REPAIR. MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 81,261 hrs · 31,753 cycles

FLOOR PANEL 221AF IS DELAMINATED FLOORBOARD 221AF FABRICATED ON TRAVELER # T21/1555527 IAW DWG SRZ-25-005 MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 81,261 hrs · 31,753 cycles

FLOOR PANEL 222AF IS DELAMINATED FLOOR BOARD 222AF FABRICATED ON TRAVELER # T21/1555539 IAW SRZ-25-005 MAJOR REPAIR

Part: PROXIMITY SENSOR — CONTAMINATED (EMERGENCY EXIT) · airframe 81,160 hrs · 31,679 cycles

PASSING 13000 FT IN DESCENT TO KRST, RECEIVED EICAS ALERT L WING SLIDE . EMER DOORS LIGHT ALSO ILLUMINATED ON OVERHEAD PANEL. COMPLIED WITH QRH. NO OTHER UNUSUAL INDICATIONS. PERFORMED BITE TEST ON PROX BOX AND FOUND CODE 373 CONVERTS TO SENSOR S10373 REF B757 FIM 32-09-802 CLEANED THE GREASE FROM PROX SENSOR REF B757 SWPM 20-20-00 PERFORMED TEST OF SLIDE COMPARMENT DOOR SENSOR REF AMM 52-71-00-5 OPS CK GOOD EICAS MESSAGE CLEARED AND EMER DOOS LIGHT WENT OUT A/C OK FOR SERVICE

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 81,119 hrs · 31,651 cycles

RAMP REPORTED L1 DOOR WOULD NOT OPEN FULLY. OPENS PARTIALLY AT THE TOP. BOTTOM STAYS ENGAGED. REMOVED FROM MEL STATUS. COMPLETED ADJUSTMENT OF L1 DOOR GUIDE ARM REF. B757 AMM 52-11-04-2, AND DOOR ADJUSTMENT/TEST REF. B757 AMM 52-11-00-5. OPS CHECK GOOD. DOOR LINING INSTALLED REF. B757 AMM 52-11-02-4. OK FOR SERVICE.

Part: MODULE — FAILED (MLG CONTRL LVR) · airframe 81,000 hrs · 31,567 cycles

AFTER SELECTING LANDING GEAR DOWN "GEAR" AMBER LIGHT ILLUMINATED AND "GEAR DISAGREE" EICAS MESSAGE APPEARED. AFTER SEVERAL SECONDS THE EICAS MESSAGE AND LIGHT BOTH EXTINGUISHED. PERFORMED BITE PROCEDURE ON PSEU PER FIM 32-09 FAULT TREE 802. FAULT CODES APPEARED AS FOLLOWING : (424) (423) (422) (421) AMM 32-31-01-4 , 32-09-04-4 - REMOVED AND REPLACED LANDING GEAR CONTROL MODULE M937 UP TO STEP 3.D (11). STARTED TO DO THE SYSTEM TEST OF THE POSITION INDICATION AND WARNING AND COULD NOT GET PAST 2.G(11). NO GEAR DOOR EICAS MSG AND GETTING A CONFIG A CONFIG GEAR NOT DOWN WARNING. REMOVED AND REPLACED PSEU AS PRECAUTIONARY - NO HELP STILL GETTING FAULT CODES FOR LANDING GEAR SYSTEM 1 AND 2 FAULT CODES 421, 422, 423, 424. REF FIM 23-09 F/T 802 SHEET 10 NEEDS WIRES CHECKED PER FAULT CODE TABLE 104. FURTHER T/S REQUIRED. PERFORMED CONITNUITY AND SHORT TESTS OF WIRES FROM LANDING FROM LANDING GEAR LEVER MODULE TO PSEU REFERENCING B757 FIM 32-09 FAULT TREE 802 SHEET 10 TABLE 104 AND WDM 32-61-12 AND 32-61-11. NO DEFECTS NOTED. CONTINUED WITH LANDING GEAR MODULE INSTALL REF AMM 32-31-01-4. COMPLETED STEPS 3.D. 11 AND 3.D.12. OPS TEST GOOD. REQUIRES EGPWS OPS TEST STEP 3D.14. ACCOMPLISHED EGPWS TEST FOR LANDING GEAR DISCRETE INPUT TEST. LANDING GEAR MODULE INPUTS TEST GOOD WITH EGPWS SYSTEM. REF B757 MM SEC 34-46-98-5-0 SEC 3.I.3.B

Part: CVR — MALFUNCTIONED (COCKPIT) · airframe 79,714 hrs · 30,704 cycles

WHILE AT CRUISE AT 15,000 FEET FROM KBUF TO KSYR, RECEIVED "MAIN CARGO FIRE" EICAS AND MASTER WARNING. SMOKE FILLED COCKPIT. DECLARED EMERGENCY, RAN QRH, IMMEDIATE DIVERT INTO KROC. FULL STOPPED ON RUNWAY AND EGRESSED AIRCRAFT VIA LEFT SLIDE. REPLACED RECIRC FILTER ON WRI 21-20-3902 PN P199753, NO DEFECTS OR ABNORMAL INDICATION ONFILTERS. REPLACED CVR PN 980-6032-001 SN 03088, AND FDR PN980-4700-042 SN 5715 ON WRI 23-70-3900. INSPECTED AIRCONDITION BAYS, NO DEFECTS NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 79,714 hrs · 30,704 cycles

WHILE AT CRUISE AT 15,000 FEET FROM KBUF TO KSYR, RECEIVED "MAIN CARGO FIRE" EICAS AND MASTER WARNING. SMOKE FILLED COCKPIT. DECLARED EMERGENCY, RAN QRH, IMMEDIATE DIVERT INTO KROC. FULL STOPPED ON RUNWAY AND EGRESSED AIRCRAFT VIA LEFT SLIDE. PER FIM 21-00-01-3 STEP 2 REQUIRES LEFT & RIGHT ENGINE RUN. ACOMPLISHED ENGINE RUNS PER JRH. NO ODOR OR SMOKE NOTED. ALL INDICATIONS ON LEFT AND RIGHT ENGINE RUN WERE NORMAL. REPLACED RECIRC FILTER ON WRI 21-20-3902 PN P199753, NO DEFECTS OR ABNORMAL INDICATION ON FILTERS. REPLACED CVR PN 980-6032-001 SN 03088, AND FDR PN980-4700-042 SN 5715 ON WRI 23-70-3900. INSPECTED AIRCONDITION BAYS, NO DEFECTS NOTED.

Part: MODULE — UNKNOWN (MLG) · airframe 79,706 hrs · 30,696 cycles

RECEIVED RED CONFIGURATION LIGHT, RED GEAR NOT DOWN EICAS MESSAGE, AND WARNING HORN INTERMITTENLY FROM TOP OF DECENT TO 4000 FEET MSL. PERFORMED TROUBLESHOOTING OF LANDING GEAR CONFIGURATION WARNING PROBLEMS IAW FIM 31-51 FAULT TREES 814 AND 817. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED THE LANDING GEAR CONFIGURATION WARNING MODULE AS A PRECAUTION DUE TO ITEMS INTERMITTENT HISTORY IAW AMM 31-51-04-4. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 79,690 hrs · 30,685 cycles

FOUND DAMAGE TO L1 DOOR AT UPPER LEFT CORNER INSTALLED REPAIR IAW SRM 52-10-01-2R, AND EA F - 5210-T0348898 PT 1, PAINTED AND SEALED IAW SRM 52-10-01-2R, INSTALLED DOOR LINER AND CONNECTED HANDLE IAW AMM 52-11-02-4.

Part: BOTTLE — EMPTY (L1 DOOR) · airframe 79,669 hrs · 30,669 cycles

ON MAINT PREFLIGHT FOUND L-1 DOOR ASSIST BOTTLE NITROGEN DEPLETED. SLIDE NOT DEPLOYED. R & R L-1 EMERGENCY POWER RESERVIOR IAW MM 52-11-30-4.

Part: SKIN — DAMAGED (LT WING TOP) · airframe 79,586 hrs · 30,594 cycles

PREVIOUS REPAIR ON TOP OF LEFT HAND WING TIP DISBONDED WS. 780 REMOVED DAMAGED AREA AND PREPARED REPAIR IAW B 757 SRM 57-20-01-2R FIG 201 AND 51- 70-10-2R REPAIR 4 PARAG. 3A AND B,APPLIED FILLER AND DOUBLER REPAIR AT LEFT HAND WING TIP WS 780 IAW B 757 IAW B 757 SRM 51-70-10-2R REPAIR 4.

Part: SKIN — DELAMINATED (LT WING) · airframe 79,585 hrs · 30,593 cycles

DELAMINATION FOUND ON NO STEP AREA TOP OF LEFT WING TIP EXTERIOR SKIN WSTA. 780. REMOVED DELAMINATION FOR EVAL. IAW B SRM 57-20-01-2R AND 51-70-10,CUT OUT AREA DAMAGED,APPLIED FILLER AND DOUBLER REPAIR AT LEFT EXTERIOR SKIN WSTA 780 IAW SRM 51-70-10-2R FIG 204 REP. 4.

Part: FRAME — GOUGED (FUSELAGE) · airframe 79,585 hrs · 30,593 cycles

GOUGED FRAME STA 231.25 BL0 IN FORWARD ACCESORY COMPARTMENT. BLENDED GOUGED AREA ON FRAME STA 231.25 BL- 0 IAW SRM 51-10-02-0G, AFTER FURTHER EVALUATION FOUND DAMAGED TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DETAIL II, CUT OUT DAMAGED AREA IAW SRM 53-00-07-2R FIG 202 DETAIL I, FABRICATED AND INSTALLED REPAIR ANGLE, FILLER AND SHIELD IAW SRM 53-00-07-2R FIG 202 REPAIR 7.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,245 hrs · 30,370 cycles

ON APPROACH WHEN GEAR SELECTED DOWN, SHOWED 3 GREEN BUT WE GOT A GEAR DISAGREE CAUTION MESSAGE AND LIGHT. QRH RAN AND LIGHT EXTENGUISHED. GEAR SHOWED DOWN AND 3 GREEN THE WHOLE TIME. PSEU BITE TEST RESULTS: 067, 094, 090, 086, 083, 421, 422, 423, 424. VERIFY RESULTS: 003 CARD. SUSPECT FAULTY PSEU. CLEARED MESSAGES. CHECKED GEAR HANDLE FREEDOM OF MOVEMENT PER FIM FAULT CODE 32-30-17-00, WHICH POINTS TO GEAR HANDLE NOT BEING FULLY IN DETENT POSITION. HANDLE MOVES FREELY AND OPS CK GOOD PER AMM 32-31-00-5. AS A PRECAUTION, REPLACED PSEU PER AMM 32-09-04-4. DURING BITE TEST, PSEU FAULTED LEFT GEAR DOOR CLOSE SENSOR SYSTEM 2 (CODE 076). SEE WRI 32-10-3319 FOR ACTION TAKEN FOR THIS FAULT. NO OTHER FAULTS DISPLAYED. A/C OK FOR SERVICE.

Part: LIFE VEST — MISSING (COCKPIT) · airframe 77,997 hrs · 29,487 cycles

ON PREFLIGHT, CAPTAIN/S LPU WAS MISSING. INSTALLED CAPTAINS LIFE VEST AT REAR OF CAPTS SEAT, REF DRAWING B57-25-011. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 1880) · airframe 77,916 hrs · 29,433 cycles

BS 1880, APU FIREWALL, FWD LOWER, RT SIDE, HAS A CRACK. REPAIRED IAW B757 SRM 51-40-02, AND 53-80-08-08-2R.

Part: FRAME — CORRODED (BS 1640) · corrosion level 2 · airframe 77,916 hrs · 29,433 cycles

BS 1640 FRAME, BETWEEN STRINGERS 9 AND 10R HAS CORRODED. REPAIRED THE FRAME IAW EA F-5310-T0333417.

Part: BULKHEAD — CRACKED (BS 1800) · airframe 77,916 hrs · 29,433 cycles

BS 1880, APU FIREWALL, FWD, LOWER, RT SIDE, A REPAIR HAS A CRACK. REMOVED THE REPAIR AT BS 1880, ON THE APU FIREWALL IAW SRM 51-40-02. FABRICATED A NEW DOUBLER IAW 53-80-08-2R AND INSTALLED NEW DOUBLER IAW SRM 53-80-08-2R.

Part: SWITCH — FAILED (SPOILERS) · airframe 77,398 hrs · 29,121 cycles

ON TAKEOFF ROLL, WITH POWER STABILIZED, AT ABOUT 50 KNOTS THE SPOILERS EICAS ALERT AND AUREL WARNING APPEARED. REJECTED TAKEOFF AND ALERT DISAPPEARED AT ABOUT 40 KNOTS. R & R SPEED BRAKE HANDLE POSITION SWITCH IAW MM 31-51-03-4, AND W/D32-42-12. OPS CHECKED THE SPEED BRAKE HANDLE POSITION SWITCH, OPS CHECKED OK IAW AMM 31-51-03-4

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS) · airframe 77,398 hrs · 29,121 cycles

DURING TAKEOFF ROLL AT ABOUT 50 KNOTS, RECEIVED A SPOILERS EICAS MESSAGE AND WARNING TONE. TAKEOFF WAS REJECTED AND SPOILERS EICAS WENT AWAY AS AIRCRAFT REACHED TAXI SPEED ON ABORT. REMOVED AND REPLACED THE SPOILER CONTROL MODULE IAW AMM 27-09-00-2, OPS CHECKED NORMAL.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 77,255 hrs · 29,020 cycles

AFTER TAKEOFF, RECEIVED A LE SLAT ASYM EICAS MESSAGE AND LEADING EDGE ANUNCIATOR, WHEN FLAPS WERE SELECTED FROM FLAPS 1 TO THE UP POSITION. COMPLIED WITH QRH PROCEDURE, RETUNED TO DEPARTURE. RECONNECTED RT LEADING EDGE SLAT DRIVE COUPLING TO ANGLE GEARBOX IAW AMM 27-81-15-4-0. RIG AND OPS CHECKED IAW AMM 27-81-00-5. OK FOR SERVICE.

Part: MODULE — FAILED (MLG LEVER) · airframe 764 hrs · 28,486 cycles

ON APPROACH, LOWERED THE LG. GEAR DISAGREE EICAS ALERT ALONG WITH CORRESPONDING AMBER GEAR LIGHT. WIGGLED GEAR HANDLE SEVERAL TIME. EICAS & GEAR LIGHT EXTINGUISHED, LANDED SAFELY. R & R THE LANDING GEAR CONTROL LEVER MODULE. OPS CHECKED GOOD IAW AMM 32-31-01-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

FUSELAGE EXTERNAL SKIN DENTED AT BS 743, 3" BELOW STRINGER 3L. ACCOMPLISHED EA F-5330-T0315854 PT 1. CROWN SKIN HAS A DENT WITH CREASE, FORM 8110-3 DATED 04 16 15 ATTACHED. THIS IS A CAT B REPAIR, MAJOR REPAIR.

Part: SKIN — DAMAGED (TE FLAP) · airframe 763 hrs · 28,339 cycles

RIGHT INBD FLAP HAS CONTACT DAMAGE, DENT APPROX 1.5" DIAMETER. FINAL REPAIR DIMENSIONS 4.0" DIAMETER, DOUBLER, LOCATED 85.5" FROM MF STATION 300.38 & 21.5 FWD OF TE. REPAIRED RT INBD FLAP UPPER SURFACE IAW SRM 51-70-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

SCRIBE LINE DAMAGE AT LAP SEAM 19R, BS 660 - 662. COMPLIED WITH EA F-5330-T0317014 B PT 1. FUSELAGE, PLATE & SKINS, SCRIBE LINE LRTS INSPECTIONS STRINGER 19R, STATION 660.9 - 662.0. MAJOR REPAIR CAT B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

SCRIBE LINE DAMAGE AT LAP SEAM 14R, BS 530 - 533. COMPLIED WITH EA F-5330-T031688 A PT 1. FUSELAGE, PLATES & SKINS SECTION 43, SCRIBE LINE LRTS INSPECTIONS, STRINGER 14R, BS 530.87 - BS 533.091, 2.21" LG. MAJOR REPAIR CAT B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

SCRIBE LINE FOUND AT STRINGER 26LT, STATION 1659.7 - 1663.5, DEPTH IS .0015", LENGTH IS 3.80", FWD .02", MID .02", AFT .02", FROM LAP. ACCOMPLISHED EA F-5330-T317267 PT 1. FUSELAGE PLATES & SKINS, SCRIBE LINE LRTS INSPECTIONS. THIS IS A CAT A REPAIR. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 706-712) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

PITTING CORROSION ON LOWER SKIN AT LAP SEAM 26L, BS 709 - 712. ACCOMPLISHED EA F-5330-T0314641 DATE 04 21 15. FUSELAGE SKIN BLEND REPAIR BS 706 - 712 & STRINGER 26L. THIS IS A CATEGORY A REPAIR. CLASSIFIED MAJOR REPAIR.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 763 hrs · 28,339 cycles

LEFT INBD FLAP UPPER ACCESS PANEL IS CHAFED ON THE UPPER SURFACE. REPAIRED LT INBD FLAP UPPER ACCESS PANEL IAW SRM 51-70-10 REPAIR 4. CLASS A MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

SCRIBE LINE DAMAGE FOUND AT LAP SEAM 14L, BS 767 - 769. COMPLIED WITH EA F-5330-T0315549, PT 1. FUSELAGE SKIN REPAIR BETWEEN BS 760 - 775 & STRINGER 13L - 15L, REV NEW, DATED APRIL 03, 2015. FAA FORM 8100-9 ATTACHED. MAJOR REPAIR CAT B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

MDC FLOORBEAM AT STATION 1681, UPPER CHORD UNDERSIDE SURFACES, HAS AREAS WITH CORROSION, AT & AROUND NUTPLATES, LBL 58 - RBL 58. REMOVED DAMAGE IAW SRM 51-10-02. CHECKED LIMITS FOUND AREA AT STATION 1681, RBL 24 TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM AT STATION 1681, RBL 24 IAW SRM 53-00-51 REPAIR NR 2 FIG 201. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

MDC FLOORBEAM AT STATION 1681, UPPER CHORD UNDERSIDE SURFACES, HAS AREAS WITH CORROSION, AT & AROUND NUTPLATES, LBL 58 - RBL 58. REMOVED DAMAGE IAW SRM 51-10-02. CHECKED LIMITS FOUND AREA AT STATION 1681, RBL 24 TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM AT STATION 1681 RBL 24 IAW SRM 53-00-51 REPAIR 2 FIG 201. MAJOR REPAIR.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

FORWARD PIT, BS 839 - 860, RT KEEL BEAM EXTENSION CORRODED. REMOVED CORROSION RT KEEL BEAM STATION 839 - 860, STRINGER 28L - 29R IAW SRM 51-10-02. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-30-12 FIG 101 DETAIL 1. COMPLIED WITH EA F-5310-T0315372 PT 2 FOR REPAIR. MAJOR REPAIR.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

FORWARD PIT, BS 839 - 860, LT KEEL BEAM EXTENSION CORRODED. REMOVED CORROSION LT KEEL BEAM, STATION 839 - 860, STRINGER 28L - 29R IAW SRM 51-10-02. CHECKED LIMITS, OUT OF LIMITS IAW SRM 53-30-12 FIG 101 DETAIL 1. REPAIRED IAW F-5310-T0315372 PT 1 EA, MAJOR REPAIR.

Part: BULKHEAD — CHAFED (LT PYLON) · airframe 763 hrs · 28,339 cycles

LEFT NACELLE STRUT BULKHEAD AFT LOWER LT CORNER SURFACE HAS CHAFED AREA, NACELLE STATION 202. COMPLIED WITH EA F-5450-T0315113 PT 1. AFT BULKHEAD CHAFE REPAIR NACELLE STATION 201.02. MAJOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

AFT PIT STRINGER 19L, STATION 1456, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA NO ALLOWABLE DAMAGE IN THE SRM. R & R STRINGER FROM STATION 1416 - 1456, STRINGER 19L IAW SRM 51-40-02. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 763 hrs · 28,339 cycles

LEFT NACELLE STRUT UPPER SPAR, RT CHORD CRACKED, NACELLE STATION 136. ACCOMPLISHED EA F-5450-T0315257 PT 1. MAJOR REPAIR CAT B.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 763 hrs · 28,339 cycles

RIGHT INBD FLAP, LOWER SURFACE TE WEDGE HAS THREE DENTS, OTBD OF AFT FLAP 5.5" FROM TE. REPAIRED IAW 51-70-10 REPAIR 4. MAJOR REPAIR.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 763 hrs · 28,339 cycles

RIGHT INBD AFT FLAP OTBD UPPER CORNER SKIN HAS DELAMINATION. REPAIRED IAW 51-70-04 PARA 4. MAJOR REPAIR.

Part: STRINGER SPLICE — CORRODED (BS 1460) · airframe 763 hrs · 28,339 cycles

AFT CARGO COMPARTMENT AT STATION 1460, STRINGER 23L, SPLICE IS CORRODED.

Part: STRINGER SPLICE — CORRODED (BS 1460) · airframe 763 hrs · 28,339 cycles

AFT CARGO COMPARTMENT AT BS 1460, STRINGER SPLICE 21L CORRODED.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 763 hrs · 28,339 cycles

VERTICAL STAB SKIN LT SIDE ONE EACH BUTTON HEAD FASTENER INSTALLED. BETWEEN BS 1790 & FSS 245.6. REPAIRED VERTICAL STAB SKIN LH FWD SIDE IAW SRM 51-70-10, PARAGRAPH 19, BS 1790, FSS 245.6. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

AFT LOWER FUSELAGE, TWO EACH DENTS WITH SCRATCHES AT STATION 1394, BETWEEN STRINGER 27R - 28R. ACCOMPLISHED EA F-5330-T0315686, P T 1.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 76,304 hrs · 28,338 cycles

SMOKE IN COCKPIT & CABIN AT CLIMB POWER WITH LT PACK RUNNING. TURNING OFF PACK STOPS SMOKE REF SERVICE TIP MM 79-00-95-901. DEFERRED LT PACK IAW MEL 2151A. AIRPLANE SOLD AS IS ON 27 FEB 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.

Part: ANGLE — CORRODED (APU INTAKE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

APU AIR INTAKE LOWER CUT OUT FLANGE IS EXFOLIATED. L REMOVE CORROSION FROM 2 EA ANGLES AT APE AIR INTAKE DUCT. LOWER CUT OUT YAW SUM 51-10-02. BLENDED TWO EACH ANGLES ORIGINAL MAT , LOSS .06 INCHES , REMAINING .000", FOUND 2EA. ANGLES OUT OF LIMITS AS PER SUM 53-00-03, NO ALLOWABLE DAMAGE. R & R 2 EA ANGLES IAW SUM 51-40-02 & DOG 148N3105. MAJOR REPAIR.

Part: DUCT — CORRODED (APU INTAKE) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

APU AIR INTAKE DUCT FWD CUT OUT FLANGE IS EXFOLIATED. REMOVED CORROSION FROM FWD CUT OUT FLANGE AT APU AIR INTAKE AS PER SRM 51-10-02. BLEND STRAP ORIG. MAT. .250", MAT. LOSS .250", REMAINING .000", FOUND OUT OF LIMITS AS PER SRM 53-00-01, FIG. 101, DETAIL II. REMOVED AND REPLACED FWD STRAP AS PER SRM 51-40- 02 AND DWG 148N3105. MAJOR REPAIR

Part: SKIN — DENTED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

AFT LOWER FUSELAGE SKIN DENT OUTWARD AT STATION 1730 BETWEEN STRINGER 27L - 28L.

Part: SKIN — CORRODED (FUSELAGE) · airframe 763 hrs · 28,339 cycles

AFT FUSELAGE, AFTER DRAIN MAST REMOVAL IT WAS FOUND THE EXTERNAL SKIN CORRODED UNDERNEATH OF DRAIN MAST BETWEEN BS 1661 - 1681, STRINGER 25R - 26R.

Part: STRINGER — CORRODED (BS 1671-1721) · corrosion level 2 · airframe 763 hrs · 28,339 cycles

AFT CABIN UNDER FLOOR BETWEEN STATION 1691 & 1701, STRINGER 29R CORRODED. REPLACED THE STRINGER IAW SRM 53-00-03, REPAIR 2 & SRM 51-40-02. MAJOR REPAIR.

Part: NONE — NONE (NONE) · airframe 763 hrs · 28,339 cycles

INCOMING REPAIR, STATION 1580 FRAME BETWEEN STRINGER 25L - 26L. DOES NOT COMPLY WITH CURRENT SRM.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 76,307 hrs · 28,339 cycles

MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1640 HAS SEVERAL CORRODED SPOTS. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DETAIL III, FIG. 101. REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND DWG 146N5089. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,307 hrs · 28,339 cycles

MDC FLOOR RT CREASE BEAM WEB CORRODED BETWEEN BS 1160 & STRINGER 6R - 17R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,307 hrs · 28,339 cycles

AFT CARGO COMPARTMENT, RT SIDEWALL STATION 1480 TO 1500, STRINGER 25R HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 AT AFT CARGO STATION1480 TO 1500, STRINGER 25R. ORIGINAL MATERIAL .070 INCHES, MATERIAL LOSS .003 INCHES, MATERIAL REMAINING .067 INCHES. NOT ALLOWABLE DAMAGE IAW SRM 53-00-03 FIG 101. REPAIRED STRINGER IAW SRM 53-00-03 FIG 201 REPAIR 2. THIS IS A CATEGORY A REPAIR MAJOR REPAIR.