N571FE

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 88,592 hrs · 31,621 cycles

1 LEFT DOOR SLIDE/RAFT LIGHT REMAINS ON. REMOVED AND REPLACED SLIDE RAFT ASSEMBLY.

Part: UNKNOWN — ODOR (A/C PACK) · airframe 88,294 hrs · 31,427 cycles

A/C PACKS EMIT A STRONG ODOR. OPERATED ALL THE PACKS AND UNABLE TO DETECT ANY ODORS IAW MM 21-53-00-7 A/C OK TO CONTINUE.

Part: SWITCH — MALFUNCTIONED (FAIL DETECTOR) · airframe 88,048 hrs · 31,265 cycles

LEVEL 3 ALERT "AIR MANF 3 FAIL" REMOVED & REPLACED #3 WING MANIFOLD FAIL DETECTOR SWITCH IAW MD10 MM36-23-03-4 & 36-23-03-5. RAN #3 ENGINE FOR LEAK TEST OF MANIFOLD SYS 3 PER MD10 JRH. ALL INDICATIONS NORMAL.

Part: RIB — DAMAGED (RT WING) · airframe 87,102 hrs · 30,666 cycles

DURING EXTENSION OF THE INBD SLATS, DROOPED SLAT CONTACTED PANEL 616EB, CAUSING DAMAGE TO PANEL AND RIB. REMOVED AND REPLACED THE NUT PLATE STRIP IAW SRM 51-30-01. CUT OUT DAMAGE ON THE FORMER IAW SRM 57-00-01, STEP 20, FIG. 10. INSTALLED A REPAIR IAW SRM 57-00-01, FIG. 10.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 86,108 hrs · 30,084 cycles

DURING WALK AROUND POST FLIGHT CHECK L1 DOOR WAS INADVERTENLY ARMED AND SLIDE ACCIDENTLY FELL OUT. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-61-01-2-4, A/C OK FOR SERVICE .

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 86,108 hrs · 30,084 cycles

L1 DOOR AIR BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR AIR RESERVOIR BOTTLE IAW M/M 52-10-01-2. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 84,313 hrs · 29,035 cycles

L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELAMPED LIGHT ASSY IAW SMP. ACFT OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 84,313 hrs · 29,035 cycles

L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-01. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESSURE, ONCE EACH FLIGHT DAY.

Part: VALVE — FAILED (FUEL DUMP) · airframe 84,294 hrs · 29,026 cycles

AFTER FUEL DUMP LT DUMP VALVE FAILED IN OPEN POSITION. R & R FUEL DUMP VALVE IAW 28-30-02. OPERATIONS & LEAK CHECK GOOD.

Part: SKIN PANEL — DENTED (LT WING) · airframe 84,291 hrs · 29,022 cycles

LEFT WING, TOP OTBD TE PANEL BETWEEN SPOILER 4 & 5, APPROX STATION XW619 & XW692. R & R SKIN PANEL IAW EA T8-5720-T-0325706 P1.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 84,291 hrs · 29,022 cycles

CENTER CARGO AFT SMOKE DETECTOR FAILED. TEST REPLACED LOWER CTR CARGO SMOKE DETECTOR IAW AMM 26-14-01-4. PERFORMED CARGO SMOKE DETECTOR OPERATIONS TEST IAW AMM 26-14-01-5. OPERATIONS CHECKED GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

RIGHT STATION 595, BULKHEAD WEB HAS APPROX .500 CRACK AT LONGERON 43R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER, DOUBLER & FINGER DOUBLER & INSTALLED IAW SRM 51-40-00 FIG 25 VOL 1 & EA 8-5310-T0324747.

Part: PLACARD — DAMAGED (ZONE 200) · airframe 84,291 hrs · 29,022 cycles

MAIN DECK FLOOR, FWD BALL MAT AREA FROM BS 608 - 792, LT SIDEWALL TO RT SIDEWALL, DECALS FOR CARGO LOADING PART NUMBERS & LOCATION REFERENCE ARE EITHER WORN, DAMAGED OR ERODED, 2016-05-27. CREATED TO ADD INFO TO SDR 16-1654. R & R DAMAGED PLACARDS IAW DWG 81608-11, REF WC 000659.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

RIGHT STATION 595, BULKHEAD WEB HAS APPROX .500 CRACK AT LONGERON 39R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED IAW SRM 51-40-00 FIG 25 & EA 8-5310-T0-324747.

Part: SKIN — CRACKED (PYLON FAIRING) · airframe 84,291 hrs · 29,022 cycles

NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1 & SRM 57-00-01 FIG 4, SHEET 2 VOL 1.

Part: SKIN — CRACKED (PYLON FAIRING) · airframe 84,291 hrs · 29,022 cycles

NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

SEAT TRACK DAMAGED AT STATION 755, RBL 8 R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 84,291 hrs · 29,022 cycles

LEFT WING PYLON LE, LOWER OTBD SURFACE IS CRACKED. INSTALLED DOUBLER & FILLER IAW EA 8-5710-T0325368.

Part: ANGLE — CRACKED (LT WING) · airframe 84,291 hrs · 29,022 cycles

LEFT WING, LT FUELING STATION DOOR, OTBD LANDING IS CRACKED. REPAIRED CRACK IAW SRM 57-00-01 FIG 140.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 39R, HAS A 2 INCH CRACK. REPAIRED TEE CAP IN REF TO EA 8-5310-T0324747

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 43R, HAS A 2 INCH CRACK. REPAIRED THE RT STA 595 BULKHEAD TEE CAP AT LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0324747.

Part: PANEL — DELAMINATED (RT WING) · airframe 84,291 hrs · 29,022 cycles

RIGHT MAIN WW PANEL ARC 0269-504 IS DELAMINATED, AREA MARKED NR 15 ON BOTTOM SIDE OF PANEL. REPAIRED IAW SRM 51-71-00 VOL II & PREPPED. PAINTED IAW SRM 51-21-02.

Part: SKIN — DAMAGED (ACM DOOR) · airframe 84,291 hrs · 29,022 cycles

NUMBER 2 ACM DOOR, LOWER FWD CORNER DAMAGED. REPAIRED DOOR IAW DPS 3.69-5 & SRM 52-00-01 VOL 1 FIG 4 SHEET 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

AFT CARGO COMPARTMENT, FOUND EXFOLIATION CORROSION ON THE NR 3 SEAT TRACK AT STATION 1841 - 1877, RBL 30R. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A SHEET 7.

Part: FORMER — CRACKED (RT HORIZ STAB) · airframe 84,291 hrs · 29,022 cycles

RIGHT HORIZONTAL STABILIZER INBD, LE FIXED SEGMENT HAS A 1" CRACK AT THE NOSE RIB LOWER AFT CORNER, EMANATING FROM ONE FASTENER TO THE EDGE OF THE NEXT, JUST INBD OF THE REMOVED LE SECTION, APPROX STATION XFS 88.83. REMOVED DAMAGED LE FORMER, INSTALLED LE FORMER IAW DWG AQLC7051-12.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 84,291 hrs · 29,022 cycles

FORWARD CARGO BAY FLOORBOARD AT STATION 735, LBL 20, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOORBOARD IAW SRZ-25-005.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 84,291 hrs · 29,022 cycles

CAC FINGER DOUBLER CORRODED & CRACKED AT SPLICE STATION 1129, MARKED OTBD OF LONGERON 48L. REPAIR IAW SRM 53-20-00 FIG 6.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 84,291 hrs · 29,022 cycles

FORWARD CARGO PIT FLOORBOARD PANEL AT STATION 959, LBL 70, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.

Part: SKIN PANEL — CRACKED (RT HORIZ STAB) · airframe 84,291 hrs · 29,022 cycles

RIGHT UPPER AFT HORIZONTAL STABILIZER SKIN PANEL INBD AFT CORNER HAS A .400 INCH CRACK. CRACK STOP DRILLED IAW WC 55X1203ALI-P4 FIGURE 2 TABLE 1. CRACK FOUND TO BE LIMITS. TRACKING TO BE ACCOMPLISHED ON WC AT 80 FLIGHT HOUR INTERVALS.

Part: SPAR CAP — CRACKED (RT WING) · airframe 84,291 hrs · 29,022 cycles

RIGHT WING REAR SPAR LOWER CAP, CRACK LOCATED AT STATION XORS 412. CRACK STARTS ON AFT EDGE & CONTINUES ALONG HORIZONTAL AFT FLANGE THRU ONE BOLT HOLE FWD INTO RADIUS. CRACK IS APPROX 1.5 INCHES IN LENGTH. REPAIRED RT AFT, LOWER REAR SPAR CAP CRACK IAW EA 8-5710-T0324727.

Part: SKIN — DENTED (TE FLAP) · airframe 84,291 hrs · 29,022 cycles

RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 245, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.

Part: SKIN — DENTED (TE FLAP) · airframe 84,291 hrs · 29,022 cycles

RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 253, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.

Part: PANEL — DELAMINATED (LT WING) · airframe 84,291 hrs · 29,022 cycles

LEFT WING, PANEL 541JB HAS A DENT & IS DELAMINATING AT THE CORNER. REPAIRED LT WING PANEL 541JB IAW SRM 51-71-00 VOL 2.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 827 hrs · 28,150 cycles

R1 DOOR PNEUMATIC EMER ASSIST BOTTLE PRESS LOW ON PREFLIGHT. SERVICED R1 DOOR AIR RESERVOIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y= 1761 X= -25 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA AT STA Y=1621, X=-25 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING AFA0055 REVISION L AND INSTALLED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=-5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STA Y= 1781, X= -5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING AFA0054 REVISION K AND INSTALLED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

AFT CARGO COMPARTMENT SHEAR CLIP ANGLE, TWO EACH, AT STATION 1821 BETWEEN L51L TO L51R BILGE AREA FOUND WITH SURFACE CORROSION. CORROSION ON SHEAR CLIP 02 EACH AT AFT CARGO COMPARTMENT STA 1821 BETWEEN LONGERON 51L TO LONGERON 51R REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DOUGLAS DRAWING AGA3788 REVISION L AND INSTALLED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · airframe 82,029 hrs · 27,733 cycles

LOWER CTR CARGO COMPARTMENT BILGE AREA STA=1721 X=5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STATION Y=1721, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING ADA0112 REVISION R AND INSTALLED AS PER SRM 51- 31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: STANCHION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STATION 1781 X=10 RT LOWER SECTION. AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STA 1781 X= -10 (RT) REMOVED AND REPLACED WITH FABRICATED STANCHION AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW STANCHION FABRICATED FABRICATED AS PER DOUGLAS DRAWING AFA3225 REVISION AC. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER FWD CARGO COMPARTMENT BILGE AREA AT STATION = 939 X = 5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER FORWARD CARGO COMPARTMENT BILGE AREA AT STA=939, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING ADA0112 REVISION R AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1741 X=5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE AREA SHEAR CLIP STA Y=1741, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING AFA0010 REVISION L AND INSTALLED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1761 X= 5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STA Y=1761 X= 5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING AFA0055 REVISION L AND INSTALLED AS PER SRM 51-30-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 102.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION =1776 X=-35 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO BILGE AREA STA=1776, X=-35 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER DRAWING AFA3906 REVISIN E AND INSTALLED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (LT WING) · airframe 82,029 hrs · 27,733 cycles

DUE TO EXISTING REPAIR DOUBLER REMOVED FOR ACCESS, FOUND CRACK AT LT WING FIXED LEADING SKIN XOS 906. CRACK SKIN AT LEFT HAND WING FIXED LEADING SKIN XOS 906 CARRIED OUT REPAIR AS PER EA 8-5730-T0310420 P1 TITLE (WINGS - PLATES AND SKINS - LT WING - FIXED LEADING EDGE SKIN - EXISTING REPAIR FOUND AT XOS 906) REPEAT INSPECTION (VISUAL INSPECTION) TO BE CARRIED OUT AS PER EA# 8-5730-T0310420 P2 24 MONTHS. FOR WORK DETAILS REFER TO WRI 57308341. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 82,029 hrs · 27,733 cycles

MAIN DECK R3 DOOR FORWARD JAMB BOX LOWER WEB FOUND CRACKED ON EXISTING REPAIR. AREA CRACKED EXISTING REPAIR DOUBLER AT MAIN DECK R3 DOOR JAMB REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW REPAIR DOUBLER FABRICATED AND ACCOMPLISHED REPAIR AS PER SRM 53-50-00 FIGURE 19 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122. REPETITIVE INSPECTION REQUIRED PER SRM 53-50-00 FIGURE 19 VOLUME I. INITIAL INSPECTION ON 15000 FLIGHT CYCLES AND REPETITIVE INSPECTION ON 6500 FLIGHT CYCLES. METHOD - HFEC AROUND REPAIR DOUBLER LOOKING FOR JAMB INNER SKIN CRACK..

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

AFT CARGO COMPARTMENT WEB FLOOR SUPPORT AT STATION 1900 X=18 LT CRACKED & CORRODED. FLOOR SUPPORT BEAM (WEB) TRIMMED AND REMOVED AS PER SRM 53-00-01 FIGURE 8 VOLUME I REVISION 101. REPAIR CHANNEL AND FILLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGURE 8 VOLUME I REVISION 101. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=16 FRAME ANGLE FOUND CORROSION. ACCOMPLISHED REPAIR AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122. TO PERFORM INITIAL INSPECTION AT 12,000 FLIGHT CYCLE AND REPETITIVE INSPECTION AT 8,000 FLIGHT CYCLE PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 101.

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 82,029 hrs · 27,733 cycles

LEFT WING INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND MINOR SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMITS AS PER CMM 57-44-07 REVISION 62. EXISTING HOLE DIAMETER = 2.554 INCHES. FINAL HOLE DIAMETER = 2.5625 INCHES. MAXIMUM ALLOWABLE DIAMETER = 2.531 INCHES. NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 REVISION 62 AND EA 8-5750-T0310363 P1, TITLE: WINGS - FLIGHT SURFACES - 8-5750-5002- LT WING - INBD FLAP FWD OUTBD HINGE BRACKET ASSY - CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 82,029 hrs · 27,733 cycles

LOWER FWD CARGO COMPARTMENT CEILING AREA BETWEEN STATION =919 - 939, X=80 SEAT TRACK SPLICE FOUND WITH MINOR CORROSION. REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW REPAIR SPLICE FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (LT WING) · airframe 82,029 hrs · 27,733 cycles

LT WING UPPER SKIN FUEL TANK ACCESS PANEL 535AT CUT OUT AFT EDGE FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 8-5710-T0310364 P1 TITLE: WINGS - BASIC WING STRUCTURE - LT WING - UPPER FUEL TANK ACCESS (535AT) COVER ATTACHMENT BOLT HOLE CRACK NEAR EXISTING REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 82,029 hrs · 27,733 cycles

RIGHT WING NR 3 LE SLAT OTBD LE ANTI- ICE DUCT ACCESS PANEL ATTACHMENT SUPPORT BRACKET CRACKED. CARRIED OUT REPAIR AS PER EA 8-5750-T0310665 PART 1 TITLE: WING - FLIGHT SURFACES - RT WING 3 SLAT LOWER TEE CAP CRACK - SECTION REPLACEMENT AND SPLICE REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122. APPROVED AS TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. APPROVAL IS FOR THE NEXT 24 MONTHS.

Part: DOOR FRAME — CRACKED (L3 DOORWAY) · airframe 82,029 hrs · 27,733 cycles

MAIN DECK CARGO L3 DOOR FWD FUSELAGE DOOR FRAME LOWER LIGHTENING HOLE WEB FOUND CRACKED. REPAIRED IAW SRM 53-50-00 FIGURE 19 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — DENTED (LE SLAT) · airframe 82,029 hrs · 27,733 cycles

RIGHT WING LE SLAT NR 8 INNER CTR SKIN FOUND WITH DENT. CARRIED OUT REPAIR AS PER EA 8-5750-T0310671 PART 1 TITLE: WINGS - FLIGHT SURFACES - RT WING NR 8 SLAT ASSY INNER SKIN DENT - SRM REPAIR - RSC TRACKING. REPAIR SKIN AND DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 31 VOLUME I REVISION 101 AND EA 8-5750-T0310671 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SKIN — DENTED (LE SLAT) · airframe 82,029 hrs · 27,733 cycles

RIGHT WING LE SLAT NR 3 SKIN FOUND WITH DENT. SKIN REPAIRED PER SRM 57-10-10 VOLUME I FIGURE 31 REVISION 101. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-20-100 REVISION 122. EA 8-5730-T0310790 P1 TITLE: WINGS - PALATES AND SKINS - RT WING NR 3 SLAT INNER SKIN DENTS - SKIN SECTION AND SPLICE REPAIR PER SRM - RSC TRACKING PURPOSE.

Part: SKIN — LOOSE (LT WING) · airframe 82,029 hrs · 27,733 cycles

LEFT WING UPPER FIXED TE PANEL JUST OTBD OF AILEORN FOUND LOOSE. REPAIRED IAW SRM 57-10-00 FIGURE 86 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CHAFED (LT WING) · airframe 82,029 hrs · 27,733 cycles

LEFT WING FIXED LE JUST OTBD NR 8 OF SLAT FOUND CHAFED. REPAIRED IAW EA 8-5730-T0310619 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 82,029 hrs · 27,733 cycles

AIR CONDITIONING BAY AFT PRESS BULKHEAD WEB CRACKED AT BS 595 BETWEEN LONGERONS 38 & 39L. REPAIRED IAW EA 8-5310-T0310372 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CHAFED (LT WING) · airframe 82,029 hrs · 27,733 cycles

LT WING FIXED LE JUST OTBD OF NR 8 SLAT FOUND CHAFED. REPAIRED IAW EA 8-5730-T0310619 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — DENTED (LT WING) · airframe 82,029 hrs · 27,733 cycles

LEFT WING LOWER FIXED TE PANEL JUST OTBD OF AILERON FOUND EDGE DENTED. REPAIRED IAW SRM 51-21-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CHAFED (LT WING LE SLAT) · airframe 82,029 hrs · 27,733 cycles

LEFT WING NR 3 SLAT UPPER TE FOUND CHAFED. REPAIRED IAW SRM 51- 21-01 VOLUME II REVISION 101. 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 122.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 82,029 hrs · 27,733 cycles

AIR CONDITIONING BAY AFT PRESSURE BULKHEAD TEE FITTING CRACKED ACROSS FASTENER INSTALLATION BS 595 BETWEEN LONGERONS 38 & 39L. REPAIRED IAW EA 8-5310-T0310372 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SWITCH — FAULTY (NR 2 ENGINE) · airframe 81,410 hrs · 27,412 cycles

LEVEL TWO ENG 2 OIL FILTER ALERT RECEIVED DURING CRUISE FLIGHT AT FL350. ALERT WAS INTERMITTENT FOR A FEW MINS, THEN WENT OUT WITH NO REDUCTION IN THRUST. ALERT RETURNED 1.5 HOURS LATER, REDUCED THRUST TO 85 % N1. ALERT STAYED OFF UNTIL DESCENT INTO KMEM WHEN IT RETURNED INTERMITTENTLY. ELECTED TO SHUT ENG DOWN. OIL PRESS & TEMP WERE SAME AS OTHER ENGS. COMPLETED INSTALLATION OF NR 2 ENG OIL STRAINER CLOGGING SWITCH REF AMM 79-35-01-2. COMPLETED INSTALLATION OF NR 2 ENG LOW OIL PRESSURE SWITCH REF AMM 79-34-01-2. RAN NR 2 ENG PER JRH WITH ALL OPS GOOD AND LEAK CKS GOOD. A/C OK OFR SERVICE.

Part: RELAY — INOPERATIVE (LANDING GEAR) · airframe 81,191 hrs · 27,297 cycles

UPON FLAP RETRACTION FROM 5 DEGREES TO UP AFTER TAKEOFF, WARNING AURAL FLAPS SOUNDED UNTIL FLAPS SELECTED TO PREVIOUS POSITION. WHEN GEAR WAS RAISED, HAD BRAKING ACTION SCALE APPEARED. RAN QRH ABNORMAL NON-ALERT GND SENSING FAILURE CHECKLIST. WHILE LT & RT GND SENSOR CB'S PULLED, ACFT APPEARED TO SENSE AIR MODE. PRIOR TO CB'S PULLED AUTOPILOT DID ENGAGE. FCP FUNCTIONS WORKED, PRESS CONTROLLER WORKED. DISCOVERED SHORT TO GND ON WIRE SEGMENT B102-4980-20. WIRE SHORTED BEHIND EQUIPMENT PANEL. REPAIRED WIRE B102-4980-20 IAW STD WIRING PRACTICES MANUAL. WHEN ATTEMPTING TO OPERATIONS CHECK GND SENSE RELAYS LT GND SENSE CB IS POPPING. LT GND SENSING 12 RELAY R2-5897 INTERNALLY SHORTED, CAUSING CB B1-91 LT GND SENSING TO POP & KEEP IT FROM RESETTING. R & R R2-5897, LT & RT GND SENSING, NOW TESTED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 81,185 hrs · 27,293 cycles

ON TAKEOFF ROTATION, HAD INDICATED GND MODE, FPV WITH LEGS, & BRAKING ACTION INDICATOR. GEAR RETRACTED NORMALLY BUT WITH FLAP RETRACTION RECEIVED A TAKEOFF WARNING HORN. FOLLOWED QRH PROCEDURE, GROUND SENSOR FAILURE, WHICH DIRECTED RTB. CYCLED FLAPS TO VERIFY NO FAULTS. ALSO PERFORMED RTS ON EPCU AND VIA`S NO FAULTS NOTED.

Part: WIRE — CHAFED (COCKPIT) · airframe 81,185 hrs · 27,294 cycles

UPON FLAP RETRACTION FROM 5 DEG TO UP AFTER T/O WARNING AURAL, FLAPS, SOUNDED CONTINUOUSLY UNTIL FLAPS SELECTED TO PREVIOUS POS. WHEN GEAR WAS RAISED, HAD BRAKING ACTION SCALE APPEARED. RAN QRH ABNORMAL NON-ALERT, GND SENSING FAILURE, CHECKLIST. WHILE LT & RT GND SENSOR CB'S PULLED, AIRCRAFT APPEARED TO SENSE AIR MODE. PRIOR TO CB'S PULLED AUTOPILOT DID ENGAGE. FCP FUNCTIONS WORKED, PRESS CONTROLLER WORKED. SHORT TO GND ON WIRE SEGMENT B102-4980-20, WIRE SHORTED BEHIND EQUIP PANEL. REPAIRED WIRE B102-4980-20 IAW STD WIRING PRACTICES MANUAL. WHEN ATTEMPTING TO OPERATIONS CHECK GND SENSE RELAYS, LT GND SENSE CB POPPING. LT GND SENSING 12 RELAY R2-5897 INTERNALLY SHORTED, CAUSING CB B1-91 LT GND SENSING TO POP & KEEP IT FROM RESETTING. R & R R2-5897, LT & RT GND SENSING, NOW TESTED GOOD.

Part: UNKNOWN — VIBRATION (NR 1 ENGINE) · airframe 80,107 hrs · 26,716 cycles

ENGINE VIBRATION NOTED IN CRUISE FLIGHT. CLIMB WAS NORMAL. AS POWER WAS REDUCED AT TOP OF CLIMB, VIBRATION WAS NOTED AND DETERMINED TO BE ENGINE NR1. VIBRATION WAS MOST PROMINENT AT APPROX 95 PERCENT NI. AT LOW POWER SETTINGS VIBRATION WAS LESS AND NO VIBRATION NOTED DURING DESCENT. INSPECTED NR 1 ENGINE THROUGHLY, LOOKING AT EACH ACCESSORY COMPONENTS, GEARBOX MOUNT BRACKETS, AS WELL AS REVERSER, CORE AND FAN COWL ATTACHMENT FITTINGS WITH NO VISIBLE SIGNS OF BROKEN OR MISSING HARDWARE . INSPECTED ALL FAN BLADES FOR SHINGLING OR EXCESSIVE RUB, ALL OK. RAN NR 1 ENGINE IAW MD10 JRH CH 5 TO 96 PERCENT N1 FOR 5 MINUTES WITH NO VIBRATIONS FELT THROUGH THROTTLES OR YOKE. ALSO INSPECTED ALL FLAPS, AILERON AND ELEVATORS, ALL CHECKED GOOD. ALL 3 PACK INLET & EXHAUST DOORS GOOD. UNABLE TO DUPLICATE DISCREPANCY ON GROUND AS WAS DISCRIBED IN FLIGHT. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1800-1821) · corrosion level 2 · airframe 79,646 hrs · 26,462 cycles

AFT CARGO BAY FLOOR SUPPORT CORROSION BS 1800 - 1821. REMOVED GUSSET IAW SRM 51-31-01. FABRICATED NEW FLOOR SUPPORT IAW SRM 53-15-01. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-31-01, VOL II. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 79,634 hrs · 26,455 cycles

RT WING REAR SPAR LWR CAP AFT OTBD HOLE IS CRACKED. XORS 345.750 REAMED HOLE TO A DIA OF .328". HFEC INSP NO CRACK NOTED IAW EA 8-5710-163354. COLD WORKED 1EA HOLE IAW SRM 51-12-01 VOL II. FINAL REAM OF HOLE TO A DIA OF.341. FASTENER INSTALLATION ACCOMPLISHED ON WC E 8-5710-7-5007,P1. NO FURTHER ACTION REQUIRED. MAJOR REPAIR

Part: SPAR — CRACKED (ZONE 500) · airframe 79,634 hrs · 26,455 cycles

LEFT WING REAR SPAR LWR CAP FWD OTBD HOLE IS CRACKED. REAMED HOLE TO DIA OF .328". HEFC INSPECTION, NO CRACK NOTED IAW EA 8-5710-163353. COLD WORKED 1EA HOLE IAW SRM 51-12-01, VOL II. FINAL REAMED HOLE TO DIA OF .341". FASTENER INSTALLATION ACCOMPLISHED ON WC E-8-5710-7-5007 PT 2. NO FURTHER ACTION REQUIRED. MAJOR REPAIR.

Part: SUPPORT ANGLE — DAMAGED (LT WING TE FLAP) · airframe 79,634 hrs · 26,455 cycles

LEFT OTBD FLAP INBD HINGE UPPER ANGLE HAS BROKEN SUPPORT. REMOVED BROKEN SUPPORT IAW SRM 51-31-01, VOL 2. FABRICATED NEW SUPPORT IAW SRM 51-31-01, VOL 2 PAGE 63, SRM 51-21-01, VOL 2, PAGE 17, SRM 51-10-00 VOL 2, PAGE 62 AND DWG ARC0744. INSTALLED SUPPORT ANGLE IAW SRM 51-31-01 VOL 2, PAGE 1. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 79,634 hrs · 26,455 cycles

SKIN MISREPAIRED BS 869 - 889 FROM L43L TO L48L. REPAIRED IAW SRM 51-31-01, VOL II.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 79,634 hrs · 26,455 cycles

RT OTBD FLAP UPPER SURFACE SKIN IS SEPARATED FROM STRUCTURE DUE TO PULLED THRU FASTENERS 60" FROM OTBD END. REPAIRED IAW SRM 57-10-00, FIG 7, VOL I. MAJOR REPAIR.

Part: BULKHEAD WEB — CRACKED (BS 1381) · airframe 79,310 hrs · 26,260 cycles

LEFT BULKHEAD FWD UPPER SIDE HAS TWO CRACKS PROTUDING OUT OF LIGHTNING HOLE 12 INCHES AFT OF BS 1381. REPAIRED CENTER WW WEB AREA USING SRM 30 53-00-01, VOL 1, PAGES 50 - 53.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 78,826 hrs · 26,012 cycles

APPROX 43 MINUTES AFTER TAKE OFF, RECEIVED FWD 2 FLASHING, DISCHARGED SWITCH INDICATION, FOLLOWED SHORTY BY A TRIDENT TONE AND MOMENTARY LEVEL 3 FWD CARGO FIRE INDICATION. DIVERTED AND DECLARED EMERGENCY, DISCHARGED NR 2 BOTTLE. OPS TESTED NORMAL IAW MM 31-42-00-0, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (R1 DOOR SLIDE) · airframe 78,026 hrs · 25,574 cycles

R1 DOOR EVAC SLIDE REMOTE PRESS TO REST LIGHT INOPERATIVE, RELAMPED AND REPLACED BATTERIES NO HELP. RELAMP PTT LIGHT SWITCH WITH 338 3 VOLT BULBS,TEST CHECKED NORMAL INSTALLED NEW BATTERIES PRECAUTIONARY, REMOVED CONTROL STICKER, ALL OPS GOOD.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 77,634 hrs · 25,387 cycles

CORROSION ON FLOORBEAM TEE, STA 1110, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA, FABRICATED FILLER, 2 REPAIR ANGLES AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8 FIG 8, 51-30-5 AND 51-30-2.

Part: FAN — ODOR (E/E BAY) · airframe 75,213 hrs · 24,151 cycles

WHILE IN CRUISE AT FL 340 HEARD A THUMPING NOISE FROM THE RADOME OR AVIONICS COMP AREA. ALMOST IMMEDIATELY STARTED DETECTING A BURNING ODOR. COMPLIED WITH THE PHASE ONES AND QRH AND DIVERTED. UPON ENTERING COCKPIT NOTICED NO VISIBLE SMOKE, FOUND AVIONICS RACK FAN 3 CB POPPED. FOUND NR 3 AVIONICS FAN C/B POPPED UPON ENTERING COCKPIT. NO PAST HISTORY. REMOVED COVER TO INSPECT WIRING AT FAN AREA, NO DISCREPANCIES NOTED. OK FOR FLIGHT. MOCC NOTIFIED. TRANS ITEM TO MEL. R & R NR 3 AVIONICS COOLING FAN PER AMM 21-26-02-4 OPS CHECK GOOD, CIRCUIT BREAKER REMAINS CLOSED.

Part: WARNING LIGHT — ILLUMINATED · airframe 75,083 hrs · 24,093 cycles

PDIS: DURING PREFLIGHT FLASHING DISCHARGE SWITCH ON OVERHEAD CARGO FIRE PANEL AND DISCHARGE FIRE AGENT MESSAGE EAD. CONTACTED FIRE DEPARTMENT AND THEY RESPONDED. NO FIRE NOTED. REMOVED AND REPLACED NR 1 FIRE EXTINGUISHER CONTAINER (135LB) IAW MM 26-22-01-4, FIRE SYSTEM TEST GOOD.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,104 hrs · 23,620 cycles

MCD LWR JAMB SUPPORT NR 5 FITTING HOLE NR C (FWD OUTBOARD) HAS CORROSION. REAMED HOLE, FABRICATED BUSHING, NDT HOLE, INSTALLED BUSHING AND REAMED NEW BUSHING IAW MAE TRAVELER T8/757301, NTSPN 06-10-01 AND SRM 53-50-00 FIG 17. MAJOR REPAIR, RII, RDR AND SDR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 74,104 hrs · 23,620 cycles

UPPER CARGO COMPARTMENT SEAT TRACK 107L, FS 979 HAS A WORN LOBE AND HOLE OUT OF ROUND. BLENDED AREAS IAW SRM 53-70-00 FIG 5 SHT 1 2 ORIGINAL .145 AFTER REWORK .120 MAT. LOSS .025 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHT 1. FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR T8/758243. FABRICATED NEW SPLICE HASTS AND PLATES UNDER MAE TRAVELER NR T8/75849.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 74,104 hrs · 23,620 cycles

UPPER CARGO COMPARTMENT SEAT TRACK 1072, FS 1053 LOBE 1/2 MISSING. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1(SHEET 1). FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR T8/758248. BLENDED AREA (LOBE) IAW SRM 53-70-00. ORIGINAL .420, AFTER REWORK .230, OUT OF LIMITS. REMOVED AND REPLACED SIDEWALL GRILLS AND SIDEWALL GRILL ANGLES IAW SRM 51-31-01.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 74,104 hrs · 23,620 cycles

MAIN DECK SEAT TRACK AT STA 849, LBL 75 HAS GOUGE MARK. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1,FIG 1, SHT 1. FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR 78/758027 IAW SRM 53-70-00. BLENDED GOUGE OUT OF LIIMITS .240 AFTER REWORK MAX REWORK .260 IAW SRM 53-70-00. REMOVED AND REPLACED 2 FLOOR PANELS STA 823-999 LBL 48-75 IAW AMM 53-21-08-02.

Part: SEAT TRACK — WORN (BS 1638-1631) · airframe 74,104 hrs · 23,620 cycles

UPPER CARGO COMPARTMENT SEAT TRACK 75L, FS 1638L TO 1631L, HAS 3 WORN LOBES BLEND AREA IAW 53-70-00 FIG 5, SHEET 1 OF 2 ORIGINAL .145 AFTER REWORK .118 OUT OF LIMITS. REMOVED AND REPLACED FLOOR PANELS IAW AMM 53-21-08-2 STA 1561-1661 LBL 48-75 AND 1561-1661 LBL 75-108. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1. FABRICATED SEAT TRACK, SPLICE HAT AND PLATE ON TR NR T8/ 758025 AND T8/758026.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 74,104 hrs · 23,620 cycles

UPPER CARGO COMPARTMENT SEAT TRACK 107L, FS 1175L HAS SEAT TRACK LOBE BROKEN OFF. REMOVED AND REINSTALLED FLOOR PANEL, REMOVED AND REPLACED SEAT TRACK FAB NEW TRACK AND SPLICES ON MAE TRAVELERS T8/758247, T8/758229, SRM 53-21-08-2, 53-70-00 FIG 1. MAJOR REPAIR RII RDR AND SDR.

Part: GCU — INOPERATIVE (NR 2) · airframe 74,072 hrs · 23,598 cycles

AT CRUISE, NOTICED SLIGHT ELEC ODOR FOLLOWED BY LEVEL 2 ELEC ALERTS AND MOMENTARY GEN 2 OFF SWITCH ILLUMINATED. ODOR CONTINUED TO INCREASE COMPLETED PHASE 1, O2 MASKS DONNED. DIVERTED TO KSDF EVACUATED AIRCRAFT. DEPLOYED SLIDE 1L BLEW FIRE AGENT TO ALL THREE ENGINES AND APU. FOUND NR 2 GENERATOR GCU WITH BLACK SOOT AND EVIDENCE OF HEAT DAMAGE. REMOVED AND REPLACED NR 2 GCU. AS PRECAUTIONARY REMOVED AND REPLACED EPCU RAN ALL THREE ENGINES VERIFIED ALL ELECTRICAL SYSTEMS AND MOTOR INDICATIONS NORMAL.

Part: PIPE — LOOSE (HYD SYSTEM) · airframe 73,962 hrs · 23,537 cycles

HYD 3 ELEV OFF ALERT 45 MINUTES INTO FLIGHT. R&R RT MLG TRIM CYLINDER. PEFORMED GEAR RETRACTION.

Part: SKIN — CRACKED (ZONE 500) · airframe 71,749 hrs · 22,522 cycles

COMPLIED WITH EA NR 8-5710-102030 WING LT WING UPPER SKIN CRACKED AT XORS 585 ADJACENT TO STR 7. ACCOMPLISH PART 2 AT SUBSEQUENT C CHECKS CONCURRENT WITH MAINTENANCE WORK CARD 57SI5503-02 MAJOR REPAIR. COMPLIED WITH EA NR 8-5710-102030 WING LT WING UPPER SKIN CRACKED AT XORS 585 ADJACENT TO STR 7. ACCOMPLISH PART 2 AT SUBSEQUENT C CHECKS CONCURRENT WITH MAINTENANCE WORK CARD 57SI5503-02.

Part: SKIN — CORRODED (ZONE 100) · airframe 71,749 hrs · 22,522 cycles

FUSELAGE LOW EXTERNAL SKIN HAS EVIDENCE OF CORROSION WITH BULGED AREA AND SHEARED FASTENERS AT F/L 1851 STR 51L - 51R. REMOVED CORROSION AT STA 1851 ORIGNAL THICKNESS .063, MATERIAL LOSS .035, OUT OF LIMITS. FAB`D REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER AND FILLER.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 71,749 hrs · 22,522 cycles

DURING C CHECK AT MAE, FOUND SEAT TRACK AT FS 909-1129 LBL 28 GOUGED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01.

Part: SEAT TRACK — DAMAGED (BS 1541-1681) · airframe 71,749 hrs · 22,522 cycles

MAIN CARGO COMPT SEAT TRACK AT STA 1541-1681 LBL 8 DAMAGED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DAMAGED SEAT TRACK.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 71,749 hrs · 22,522 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT FS 1139 - 1239 RBL 8. BLENDED SEAT TRACK IAW SRM 53-70-00 FIG 5, FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1. SEAT TRACK FABRICATED ON MAE TRAVELER NR T7/666718. SPLICE PLATE AND HAT FABRICATED ON MAE TRAVLER NR T7/666719.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 71,749 hrs · 22,522 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT F/S 1079 - 1109 LBL8 BLENDED AREA IAW SRM 53-70-00 FIG 5. BEGINNING THICKNESS OF MATERIAL 0.145; REMOVED 0.060; OUT OF LIMITS IAW SRM 53-70-00 FIG 5. RECIEVED FROM FAB ON MAE TRAVLER NR T7/666714, SEAT TRACK; RECEIVED FROM FAB ON MAE TRAVLER NR T7/666715, SPLICE HAT AND SPLICE PLATE. INSTALLED NEW SEAT TRACK, HAT, AND SPLICE IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 71,749 hrs · 22,522 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT F/S 909 - 1039 RBL 75. BLENDED AREA IAW SRM 53-70-00 FIG 5. SEAT TRACK EXCEEDED LIMITS IAW SRM 53-70-00 FIG 5. REMOVED DAMAGED AREA STA 930-1030 RBL 75 IAW SRM 53-70-00 FIG 4. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T7/666392. FABRICATED HAT AND SPLICE FOR SEAT TRACK ON MAE TRAVELER NR T7/666393. INSTALLED NEW SEAT TRACK, SPLICE, AT HAT IAW SRM 53-70-00 FIG 1.

Part: BALLAST — UNSECURE (CARGO BAY) · airframe 69,580 hrs · 21,605 cycles

CARGO CAN IN LOWER FORWARD BELLY BROKE LOOSE DURING FLT AND BANGED EXCESSIVELY INTO SIDES AND FRONT OF LOWER FWD BELLY COMPARTMENT. EMERGENCY DECLARED IN AUSTIN. AFTER LANDING DISCOVERED THAT THE LOOSE CAN WAS IN FACT A LOOSE (UNSECURED) BALLAST PALLET IN POSITION 1L ON MAIN CARGO DECK. FOUND LOCKS FWD OF PALLET POSITION 1L NOT SECURED UP ALLOWING PALLET TO MOVE FWD ABOUT 20 INCHES HITTING LOCKS POSITIONED UP AT STA 506. INSPECTED ALL LOCKS, SEAT TRACKS AND FLOOR STRUCTURE AFFECTED BY PALLET MOVEMENT AND FOUND NO DAMAGE. A/C OK FOR SERVICE.

Part: DOUBLER — CORRODED (RT WING) · airframe 69,315 hrs · 21,486 cycles

DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.

Part: DOUBLER — CORRODED (LT WING) · airframe 69,315 hrs · 21,486 cycles

DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.

Part: SKIN — DAMAGED (TE FLAP) · airframe 69,315 hrs · 21,486 cycles

LT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECTION, NO CRACK FOUND. PERFORM DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.

Part: SKIN — DAMAGED (TE FLAP) · airframe 69,315 hrs · 21,486 cycles

DURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPECTION, NO CRACK FOUND. PERFORMED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.

Part: SKIN — DENTED (BS 555) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND DENT ON UPPER SKIN FUSELAGE AT STA 555 REF LONGERON 26 RT, DENT DIMENSION 2.0 X 2.0, 0.06 THICK. REWORKED DENT AREA IAW SRM 53-20-00 FIG 13. DYE CHECK FOR CRACK AND INSTALLED INT REPAIR DOUBLER IAW SRM 53-70-00 FIG 13.

Part: SPAR — DAMAGED (RT WING) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND DOUBLE HOLE 0.187* 0.291 ON TE. RT WING LOWER CAP AT STA XORS 728 AND HOLE OVALIZED IN FRG PANEL. NORMALIZED HOLE AND INSTALLED REPAIR BUSHING PER SRM 51-31-01 VOL II, REPAIRED PANEL PER SRM 57-00-01 FIG 4 SH 2.

Part: FRAME — NICKED (BS 469) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE' S CONVERSION FROM P TO F FOUND: AVIONIC COMPARTMENT AT STA 469 X= 33 WITH 2EA NICKS ON THE FRAME. BLEND OUT NICK AREA IAW SRM 53-00-01 FIG 1B, AND INSTALL FRAME REPAIR IAW SRM 53-30-00 FIG 4A.

Part: SKIN — DENTED (BS 1953) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: DENT ON SKIN LT SIDE STA 1953 LONG 29: 1 INCH LONG * 0.04 DEPTH. LONG 31: 2" LONG * 0.08 DEPTH. REWORK DENT AREA IAW SRM 53-20-00 FIG 13. DYE PENETRANT INSPECT FOR CRACK. INSTALLED REPAIR FINGER DOUBLER IAW SRM 53-20-00 FIG 13.

Part: SKIN — DENTED (BS 979-999) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: DENT AND NICK ON LOWER SKIN FUSELAGE AT STA 979-999 LONGERON 45-46 RT, DENT DIMENSION 2.5 X 4.5, 0.08. BLEND OUT NICKS AND VERIFIED LIMIT IAW SRM 53-00-01FIG 1A. REWORKED DENTS AREA IAW SRM 53-20-00 FIG 13, DYE PENETRANT INSP FOR CRACKS. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE' S CONVERSION FROM P TO F FOUND VERTICAL STABILIZER ON RUDDER RT SIDE STA ZFR 320.125, SEVERAL SWELLING THE SKIN. REPAIRED DAMAGED SECTION OF SKIN IAW 55-10-00 FIG 3 VOL I.

Part: SKIN — CORRODED (BS 1381) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: ON UPPER SURFACE OF CTR WING BOX AT STA 1381 LT SIDE X = 75'' CORROSION ON SKIN; REMOVED SLANT PANEL LT SIDE IAW MM 20-50-02, CUT ANGLE APB 7081-1 IAW SRM 53-40-00 FIG 11 SH 2. REMOVED CORROSION IAW SRM 51-21-00 PAG 28, CHECKED LIMITS IAW SRM 57-20-00 FIG 8A, COMPLETED WORK PER EA 8-5710-84088. REPLACED GASKET, P/N AEA 0487-1 QTY: 1

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND ON EXTERNAL SKIN AT STA 1119 STR 40 LT, BULGING WITH HEAD FASTENER BROKEN AND CRACK ON SKIN; ON STR 38 ONE FASTENER WITH HEAD BROKEN. ON STR 38, REPLACE FASTENERS PER SRM 51-35-01 PG 1-12; ON STR 40 REPAIR SKIN PER SRM 53-20-00 FIG 6 SHEET 3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION ROM P TO F FOUND PROCURED HOLE ON RADIUS FRAME DIM 4,00''. INSTALLED REPAIR ANGLE ON FRAME PER SRM 53-30-00 FIG 4A.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: ON FWD CARGO COMPARTMENT BTW STA 808-821 L 52, CORROSION ON SHOVEL END AND LONGERON. ACCOMPLISHED REMOVAL OF SHOVEL END, SPLICES. REMOVED CORROSION. REPAIRED IAW SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAG 1-12.

Part: DOUBLER — UNKNOWN (BS 959) · airframe 69,307 hrs · 21,478 cycles

DURING AIRPLANE'S CONVERSION FROM P TO F FOUND EXISTING REPAIR AT FUSELAGE STA 959, STR 41-38 RT. REPAIR IS CONFORM TO SRM 53-50-00 FIG 8 SH 14.

Part: SKIN — DELAMINATED (RT WING) · airframe 69,307 hrs · 21,478 cycles

DURING CONVERSION FOUND ON RT WING, LE UPPER SIDE, STA XW 346, WITH DELAMINATION. REPAIRED IAW SRM 57-00-01 FIG 4, SH 2. (OPEN)

Part: RETAINER — BROKEN (CARGO DOOR) · airframe 69,307 hrs · 21,478 cycles

ON CTR CARGO DOOR VANE STA 1781, BETWEEN STR 39/42, RETAINER FOR SEAL BROKEN, LENGTH 1,830 INCH, MISSING MATERIAL ON SKIN CUT OUT VANE. REMOVED SCUFF PLATE WEBS INTERNAL JAMB CARGO DOOR TO GAIN ACCESS PER MM 20-50-02 SRM 51-35-01; CUT RIB FAIRING AND 7280 AND ANGLE AFA7173. REMOVED DAMAGED SECTION OF SEAL RETAINER PER SRM 51-35-02, PAGE 3/9; CUT DAMAGED SECTION OF EXTERNAL SKIN IAW SRM 53-50-00; REPAIRED SKIN PER SRM 53-50-00, FIG 26. SPLICING RIB AND ANGLE PER SRM 53-00-01, FIG 8. SPLICING WEB INTERNAL JAMB DOOR PER SRM 53-00-01, FIG 10, SHT 1. REPLACED DAMAGED SEAL RETAINER PER SRM 51-35-01 PG 1/13; REINSTALLED REMOVED PARTS PER SRM 51-33-01, PG 36/47.

Part: SKIN — DAMAGED (RT WING) · airframe 69,307 hrs · 21,478 cycles

RIGHT WING, INBOARD FLAP, UPPER SKIN WITH EXISTING REPAIR WITH DEFORMED AREA. REMOVED EXISTING REPAIR PER SRM 51-35-01, PAGE 1/13. CUT OUT DAMAGED AREA PER SRM 57-10-00, PAGE 85. PERFORMED NEW REPAIR PER SRM 57-10-00, PAGE 85.

Part: SKIN — NICKED (LT WING) · airframe 69,307 hrs · 21,478 cycles

LEFT WING LEADING EDGE, STA XORS 164 WITH NICKS. REPAIRED DAMAGED LEADING EDGE IAW SRM 57-10-00, FIG 28.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

EXISTING REPAIR ON FUSELAGE LOWER SKIN AT STA 695/715, LONG 51/52. REMOVED AND RETAINED EXTERNAL DOUBLER IAW SRM 51-35-01 AND SRM 51-33-01. REPAIRED FUSELAGE SKIN PER SRM 53-20-00, FIG 6, SHT 3. REINSTALLED REMOVED DOUBLER PER DWG SR10530038-11 AND GN 17-18.

Part: PANEL — DAMAGED (ZONE 300) · airframe 69,307 hrs · 21,478 cycles

HORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 15 WITH CRACK (0,51" LENGTH), P/N ALC7227-1. REMOVED OLD PANEL ALC7228-1 PER SB 55-16. REMOVED PANEL ALC7227-1 PER SB 55-16. REWORKED ALC7227-1 NEW PANEL PER SB 55-16. INSTALLED NEW PANEL ALC7227-1 PER SB 55-16.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

HORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 11 WITH CRACK ( 0,75" LENGTH), P/N ALC7228-. REMOVED ALC7228-1 OLD PANEL PER SB 55-16 FIG 4 GR 2. REWORKED NEW PANEL PER SB 55-16 FIG 4 GR 2. INSTALLED NEW PANEL PER SB 55-16 FIG 4 GR 2.

Part: SKIN — DENTED (ELEVATOR) · airframe 69,307 hrs · 21,478 cycles

HORIZONTAL STABILIZER, RT, UPPER SIDE, THE ELEVATOR HAVE SEVERAL DENTS, IN ADDED, 2EA REPAIRS WITH CHERRYMAX. REMOVED EXISTING REPAIR AT ELEVATOR, STA XE206, AND INSTALLED BIGGER REPAIR COVERING DENT LOCATED AT STA XE200 IAW SRM 55-10-00, FIG 8.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION, FOUND AT STA 330 X= 15 WITH CORROSION ON THE WEB FLIGHT COMPARTMENT FLOOR LINE. REMOVED CORROSION PER SRM 51-21-01 PAGE 28 (OUT LIMITS). DURING CONTROL CORROSION FOR LIMITS FOUND EA 2 CRACKS 2". REMOVED MEMBRANE IAW SRM 51-35-01 PG 1/13. REPLACED MEMBRANE IAW SRM 51-35-01 PG 1/13. (OPEN)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND 3 EXISTING REPAIRS AT STA 835- STA 855 REF LOG 48-44 LT SIDE. REMOVED EXISTING REPAIR PER SRM 53-20-00 FIG 6 SHT 5, PERFORMED NEW REPAIR PER SRM 53-20-00 FIG 6 SHEET 5. (OPEN)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION, FOUND AT STA 312 X=-45 WITH CORROSION ON THE WEB FLIGHT COMPARTMENT FLOOR LINE. REMOVED CORROSION PER SRM 51-21-01 PAGE 28 (WITHIN LIMITS). DURING CONTROL CORROSION FOR LIMITS, FOUND CRACK .50 INCH, CUT OUT DAMAGE IAW SRM 53-00-0. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2.

Part: SKIN — BULGED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND STA 348-366 X=0 WEB WITH REPAIR NOT CONFORM AND BULGE WITH CRACK. REMOVED WEB PER SRM 53-11-01, REPLACED WEB PER SRM 53-11-01, PERFORMED CUT PER DWG SP10530207-7001. (OPEN)

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND EXISTING REPAIR ON LOWER SKIN FUSELAGE AT STA 840-839 LONG 51-52. REMOVED EXISTING REPAIR PER SRM 53-20-00. PERFORMED NEW REPAIR PER SRM 53-20-00 FIG 6 SHEET 3.

Part: SKIN — DENTED (ELEVATOR) · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND 1 DENT WITH NICK ON THE LEADING EDGE OF DETACHABLE ELEVATOR OF LEFT HORIZONTAL STABILIZER BETWEEN THE STA XE 88.625 AND THE STA XE 93.975 (UPPER SIDE). REMOVED LEADING EDGE PANEL BETWEEN STA 88.625 TO STA 100.455 IAW MM 20-50-07. REPAIRED IAW 55-00-01, REINSTALLED LEADING EDGE IAW 20-50-01. (OPEN)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND AT STA 1741 STRUCTURE X=-17; X= 17 WITH CORROSION AND RETAINER X= 17 WITH CORROSION. REMOVED CORROSION FROM AFFECTED AREA PER SRM 51-21-01. PERFORMED CHECK LIMITS; THE MATERIAL REMOVED IS WITHIN LIMITS PER SRM 53-00-01. PROTECTED AREA PER SRM 51-21-01.

Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 69,307 hrs · 21,478 cycles

DURING INSPECTION FOUND AT STA 1701 FROM STR 45 RT TO 45 LT RETAINER WITH CORROSION. REMOVED CORROSION ON RETAINER PER SRM 51-21-01. PERFORMED CHECK LIMITS; THE MATERIAL REMOVED IS WITHIN LIMITS PER SRM 53-00-01. PROTECTED AREA PER SRM 51-21-01. (OPEN)