N927UP

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE:C NLG W/W BS 290 LBL 0 SUSPECT CRACKS IN ROW OF RIVETS AT NLG CEILING. AREA CUTOUT IAW SRM 51-40-2 FIG 1, HFEC NDF. REPAIRED CUTOUT IAW SRM 51-10-2 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, NLG WW BS 263 AND BS 267 ROW OF RIVETS HAVE SUSPECT CRACKS ABOVE RT AFT PRESSURE PANEL. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC NDF REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, NLG WW BS 259 SUSPECT CRACKS AT RIVETS AT RT AFT PRESSURE PANEL FWD EDGE. HFEC CONFIRMED CRACKS. AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC CONFIRMS DEFECT FREE CUTOUT. REPAIRED CUTOUT IAW SRM 51-40-2 FIG 1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, TO REMOVE RT BS 930 FITTING, PARTIAL SHELF ATTACHING BS 930 TO 940 MUST BE REMOVED, ON REMOVAL OF PARTIAL SHELF AT STR 14 BS 930-940, 3 SUSPECT CRACKS WERE DETECTED ON MOST UPPER HORIZONTAL FLANGE (FWD SIDE) ON BS 940 FITTING. REPAIR CARRIED OUT IAW SRM 51-20-2 & BOEING DRAWING 65C15732.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE:C AREA OF SURFACE CORROSION ON SKIN AT BS 1090 S12L. AREA REPAIRED IAW SMRO EO 2003-055-002 AND UPS FILE 727-53-20131.

Part: SUPPORT BRACKET — CRACKED (T/E FLAP) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE:C RT WING I/B MID FLAP GUIDE ROLLER SUPPORT BRACKET CRACKED AT UPPER CHORD REAR SPAR JUST O/B OF NR 6 FLAP TRANSMISSION. ROLLER SUPPORT REPLACED IAW SRM 51-30-02 AND BOEING DRG 65-16201.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, SUSPECT CRACK AT NR 3 RT COCKPIT WINDOW CUTOUT AFT LWR CORNER. REPAIR CARRIED OUT IAW SRM 51-30-02, 53-30-03, 51-10-02 & 51-20-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, RT 930 FITTING HS SUSPECT CRACK AT AFT O/B FLANGE AT FLOOR LEVEL. REPAIR & REPLACEMENT OF BS 930 FITTING & ASSOCIATED STURCTURAL ITEMS CARRIED OUT IAW SMRO EO 2003-055-001 UPS ENGINEERING FILE 727-53-20 130.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, CABIN AIR PRESS LEAK FROM NR 1 VHF ANTENNA CUTOUT (AFT). ON INVESTIGATION A SUSPECT CRACK FOUND AT ANTENNA CUTOUT. HFEC INSPECTION CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM PT 6 51-00-00 FIG 4. CRACKEDCONFIRMED & MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3. SSID FORM SL V BL 8-10 HAS BEEN SUBMITTED.

Part: PANEL — CRACKED (NLG WW) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, DURING PRESSURE LEAKAGE CHECK IN NLG WW A 3 INCH CRACK WAS FOUND ON RT CEILING. DAMAGED PART OF WEB CUTOUT REMOVED IAW SRM 51-40-2. DE-RIVETED IAW SRM 51-30-02. HFEC INSPECTION CARRIED OUT AROUND CUTOUT IN NWW ON RT CEILING IAW B727 NDTM PT 6 51-00-00 RESULT NDF. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, NLG WW BS 243 ROW OF RIVETS BELOW RT FWD PRESSURE PANEL HAVE CRACKS. HFEC CORFIRMED CRACKS, AREA CUT OUT IAW SRM 51-40-2 FIG 1. HFEC COFIRMS NDF ON CUTOUT, REPAIRED IAW SRM 51-40-2 FIG 1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE:C SUSPECT CRACK ON ACTUATOR FITTING I/B LUG I/B FACE BELOW BOLT HOLE AIRSTAIRS ACTUATOR. HFEC CONFIRMED CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-30-02 AND DRAWING 65C13874. BOLT ALSO FOUND WORN, REPLACED IAW 52-62-71. OPS CHECKED SATISFACTORY, RIG CHECKED SATISFACTORY.

Part: FITTING — DAMAGED (NLG DRAG BRACE) · airframe 51,468 hrs · 38,137 cycles

INSPECTION TYPE: C, REPLACED NLG DRAG BRACE FITTING AS PER EO B727-5340-0167.

Part: BEAM — CRACKED (BS 1183 RBL 26) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CRACK INDICATION AT BS 1183 BEAM RBL 26.83 WL 250 APPROX. REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX D

Part: BEAM — CRACKED (BS 1183) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CRACK INDICATING AT BS 1183 BEAM LBL 26.83 WL AT 250 APPROX REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX D

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C, CORROSION ON CHORD AT FLOOR LEVEL AT BS 1177 RT O/B. CHORD REPLACED IAW SRM 51-30-02 AND DRAWING 65-19606.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C, SURFACE CORROSION ON FUSELAGE SKIN INTERNAL AT BS 254.5 BETWEEN STR 5L & 6L. REPAIR CARRIED OUT IAW DRAWING 692161 & UPS EO B727-5310-1371 APPENDIX E.

Part: SEAT TRACK — CORRODED (BS 655-710 LBL62) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CORROSION ON SEAT TRACK AT BS 660 AND BS 680 LBL 62.5 SEAT TRACK REPLACED BS 655 BS 710 LBL 62.5 IAW SRM 53-10-5 FIGURE 1

Part: RIB — CRACKED (#3 SLAT) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C RIB CRACKED ON LE SLAT #3, RIB LOCATED I/B OF O/B TRACK #3 SLAT REMOVED TO CARRY OUT REPAIR ON CRACKED RIB IAW MM 27-81-11 CRACKED RIB REPAIRED IAW SRM 57-50-3 FIG 9 #3 SLAT INSTALLED AFTER REPAIR COMPLETED IAW MM 27-81-11

Part: SKIN — CRACKED (BS 211.8 R/H) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3 USING 0.063" DOULER IAW EO B727-5330-0795-G

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C ON REMOVAL OF AFT LWR STOP WHICH IS CRACKED, DOOR FRAME FOUND CRACKE D AT LWR END ON FWD ENTRY DOOR REPAIR CARRIED OUT IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO 727-52-20009

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CORROSION BETWEEN SKIN & INTERNAL DOUBLER AT BS 1180 BETWEEN S10L & 9L. REPAIR CARRIED OUT IAW SRM 51-10-6 & 53-30-3, DAMAGE CUT OUT IAW 51- 10-6. REPAIRED IAW 51-10-2 AND 53-30-3 FIG 1 STEP 4.

Part: SLAT — CRACKED (#6 SLAT LE) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C DENTS ON SLAT POSITIONS 6 & 8 DENTS RE-WORKED IAW SRM 51-40-1 HFEC INSP. CARRIED OUT IAW NDT MANUAL, PART 6 51-00-00 FIG 4 - #8 S LAT NDF. #6 SLAT SKIN CRACKED & CRACK ENDS MARKED. #6 SLAT REPAIRED IAW SRM 57-30-03 SLAT REMOVED & INSTALLED IAW MM 27-81-11

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C CRACK IN DOOR FRAME AT AFT UPPER CORNER OF FWD ENTRY DOOR DOOR FRAME REPLACED IAW SMRO EO 2002-031-001 UPS ENGINEERING FILE NO. 727-52-20008

Part: STOP FITTING — CRACKED (FWD ENTRY DOOR) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009

Part: STOP FITTING — CRACKED (LWR AFT ENTRY D) · airframe 50,867 hrs · 37,633 cycles

INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, ATTACH BRACKET LOCATED ON LT 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DERIVETED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-20- 01, BRACKET INSTALLED IAW SRM 51-30-02.

Part: BRACKET — CRACKED (FUSELAGE)

INSPECTION TYPE:C CK ATTACH BRACKET LOCATED ON LT BS 870 FITTING IS CRACKED ALONG BEND LINE. BRACKET DE-RIVETED. HEAT TREATMENT. BRACKET FABRICATED. BRACKET INSTALLED.

Part: SUPPORT FITTING — CRACKED (NR 7 FLAP TRACK) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, NR 7 FLAP TRACK ATTACH FITTING ON REAR SPAR CRACKED. FITTING REPLACED IAW SRM 51-30-02 AND DRAWING 65-16201.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, SUPPORT FITTING ON RT WING REAR SPAR AT WS 620 APPROX CRACKED. REPLACED SUPPORT FITTING WITH PART FABRICATED IAW DRAWING 69-16227.

Part: SKIN PANEL — CORRODED (LT ELEVATOR) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER AT FS 238. SKIN REPLACED IAW DRAWING NR 65-25640.

Part: LINK — CORRODED (RT MLG TRUNNION) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, RT MAIN LANDING GEAR TRUNNION LINK CORRODED EXCESSIVELY AROUND SPLINED AREA, CHROME ALSO DAMAGED DUE TO CORROSION. RT TRUNNION LINK REPLACED IAW MM 32-11-01.

Part: PANEL — CORRODED (LT ELEVATOR)

INSPECTION TYPE:CCK CORROSION IN LT ELEVATOR UPPER SKIN UNDER STATIC DISCHARGER. UPPER SKIN REPLACED IAW DRAWING NR 655640.

Part: CASTING — CORRODED (NR 7 SPOILER) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, NR 7 SPOILER INBOARD HINGE CASTING CORRODED. REPLACED NR 7 SPOILER INBOARD HINGE CASTING IAW SRM 51-30-02.

Part: SKIN PANEL — CORRODED (RT ELELVATOR.) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, CORROSION ON RT ELEVATOR UNDER STATIC DISCHARGER UPPER SKIN PANEL. SKIN PANEL REPLACED IAW BOEING DRAWING 65-25639.

Part: FITTING — CRACKED (NLG DRAG BRACE) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C NLG DRAG BRACE FITTING NDT COMFIRMED 2 CRACKS LOCATED ON THE SIDE OF INTERCOSTAL ATTACH FLANGE REF B727-5340-0166 FOR NDT CONFIRMATION. CARRIED OUT REPAIR AS PER EO B727-5340-0167MPI RAISED NR 12786.

Part: FITTING — CORRODED (RT MLG WW) · airframe 50,003 hrs · 36,811 cycles

INSPECTION TYPE:C, RT MLG UPLOCK ROLLER SUPPORT FITTING HAS EVIDENCE OF CORROSION BETWEEN SHIM AND FITTING AT UPPER ATTACH POINT. REPLACED FITTING IAW OHM 20-50-01.

Part: FLOORBEAM — CORRODED (BS 560)

INSPECTION TYPE:C&SI, DURING REPAIR OF FLOORBEAM 560 BETWEEN RBL 45.5 & 62.5 ADDITIONAL CORROSION FOUND AT FLANGE DURING INCORPERATION OF REPAIR ANGLES. FLOORBEAM BS 560 REPAIRED IAW SRMO EO 99-14-012 REV 1 UPS ENGINEERING FILE NR 727-53-2445.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE:C&SI, CRACK INDICATION IN WING CENTER SECTION RT WING TERMINAL FITTING, LWR O/B FASTENER HOLE, BS 870. REPAIRED IAW SMRO EO 99416RI UPS EO NR B727-5710-11557-A.

Part: SPAR CHORD — CORRODED (BS 870)

INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION WEB BS 870 RBL 70.5 TO LBL 70.5 LWR CHORD, REAR SPAR FOUND CORRODED. REPLACEMENT CHORD INSTALLED IAW SNN MRO EO NR 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.

Part: SPAR WEB — CORRODED (BS 870)

INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION UPPER CHORD REAR SPAR BS 870, WEB FOUND CORRODED RBL 70.5 TO LBL 70.5. WEB REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.

Part: WEB — CRACKED (BS 870)

INSPECTION TYPE:C&SI, BS 870 BBL 15 LT SIDE AIR CONDITIONING DOOR SUPPORT WEB STRUCTURE ATTACHED TO LWR END OF BS 870 BLKHD FOUND CRACKED. WEB REPAIRED IAW B727 SRM 51-40-2.

Part: CLEVIS — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C&SI SUPPORT STRUT ABOVE NR 2 ENGINE HORIZ FIREWALL LUG CRACKED AT LWR ATTACHMENT POINT. NR 2 ENGINE STRUCTURE SUPPORT STRUT LWR CLEVIS REPLACED PER SRM 51-30-2.

Part: SPAR — CORRODED (BS 870)

INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT FLANGE UPPER CHORD REAR SPAR BS 870 CENTER SECTION AT RBL 35 APPROX. UPPER CHORD REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.

Part: STIFFENER — CORRODED (CENTERWING)

INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT STIFFENER BETWEEN UPPER & LWR WING CENTER SECTION SPAR CHORDS RBL 45. STIFFENER REPLACED IAW DRAWING 65-16202.

Part: SPLICE — DAMAGED (BS 580)

INSPECTION TYPE:C&SI, DAMAGE TO SPLICE PLATE AT STA 580 BETWEEN STR 25R AND STR 26R. REPLACED IAW SRM 53-10-2 FIG 3.

Part: ANGLE — CRACKED (BS 380)

INSPECTION TYPE: C & SI, E & E BAY CRACK ON FLOOR SUPPORT ANGLES AT BS 380 OVER STRINGER 25R. REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10-2.

Part: ANGLE — CRACKED (BS 474)

INSPECTION TYPE:C & SI, E & E BAY CRACK ON FLOOR SUPPORT ANGLE BS 474 OVER STRINGER 26R. ANGLE REPLACED IAW SRM 53-10-2 FIG 7.

Part: ANGLE — CORRODED (BS 720)

INSPECTION TYPE:C&SI FWD CARGO BAY BS 720 CORROSION ON FRAME CHORD ANGLE AT STRINGER 27 LT APPROX. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO EXCEED LIMITS CORRODED SECTION OF CHORD ANGLE WAS REMOVED IAW SRM 51-40-3 AND ANGLE REPAIR WAS CARRIED OUT IAW SRM 51-40-3 FIG 1.

Part: STRINGER — CORRODED (BS 448)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON STRINGER 23R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED IAW SRM 53-10-02 FIG AND SRM 53-10-3 FIG 1.

Part: STRINGER — CRACKED (BS 448)

INSPECTION TYPE: C & SI, SUSPECT CRACK ON STRINGER 21R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED IAW SRM 53-10-02.

Part: STRINGER — CORRODED (BS 490)

INSPECTION TYPE:C&SI, FWD CARGO BAY BS 490 CORROSION ON STRINGER 21R. REPLACED WITH NEW PIECE IAW SRM 53-10-3 FIG 1.

Part: T-SECTION — CORROSION (BS 600)

INSPECTION TYPE:C&SI, FWD CARGO BAY BS 600 CORROSION ON RT CEILING PANEL ATTACH T-SECTION AT VARIOUS ANCHOR NUTS POINTS. T-SECTION REPLACED IAW SRM 51-40-3.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE: C & SI, SUSPECT CRACK AT STR 25 RT BS 420 AT FRAME ATTACH POINT ON STRINGER LWR FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.

Part: STRINGER — CRACKED (BS 380 & 400)

INSPECTION TYPE:C&SI STR CRACKED BS 380 AND 400 AT FRAME ATTACH POINTS RT SIDE. REPAIRED IAW SRM 53-10-3 FIG 1.

Part: STRINGER — CRACKED (BS 380-420)

INSPECTION TYPE: C & SI, STRINGER 23 CRACKED BS 380, 400 AND 420 AT FRAME ATTACH POINTS LT SIDE. STRINGER REPAIRED IAW 53-10-3 FIG 1.

Part: ANGLE — CORRODED (BS 219.8)

INSPECTION TYPE:C&SI, FRAME SUPPORT ANGLE CORRODED AT BONDING WIRE ATTACH POINT BS 219.8 RBL 35. FRAME SUPPORT ANGLE REPLACED IAW SRM 51-30-2 & SRM 53-10-2.

Part: INTERCOSTAL — CRACKED (BS 480)

INSPECTION TYPE:C&SI CRACK IN INTERCOSTAL AT BS 480 STR 27R. REPAIRED IAW SRM 51-30-02, 51-20-01, 51-10-2 AND 51-30-2.

Part: STRUCTURE — CRACKED (BS 520)

INSPECTION TYPE:C&SI FWD CARGO DOOR CUT-OUT STRUCTURE CRACKED AT BS 520 NEAR STRINGER 21 AT STOP NR 4. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1 AND DRAWING 65-18385.

Part: PANEL — CORRODED (NR 1 FUEL TANK)

INSPECTION TYPE: C & SI, RT WING NR 1 FUEL TANK ACCESS PANEL CORRODED AND CRACKED. REPLACED NR 1 FUEL TANK ACCESS PANEL IAW MM 20-8-11.

Part: FLOORBEAM — CORRODED (BS 940)

INSPECTION TYPE:C&SI, DURING REPLACEMENT OF LT BS 940 FITTING, FLOORBEAM AT BS 940 LBL 7 0 - LBL 45 LWR CHORD, FOUND CORRODED. FLOORBEAM REPAIRED IAW EO SMRO 99-14-005 UPS ENGINEERING FILE NR 727-53-2134.

Part: SPLICE — CRACKED (BS 480)

INSPECTION TYPE: C & SI, CRACK ON AFT OF STRINGER SPLICE ON STR 28L BS 480. STRINGER SPLICE REPLACED IAW SRM 53-10-02 FIG 9 AND SRM 53-10-3 FIG 1.

Part: CONE BOLT — GOUGED (NR 2 PYLON)

INSPECTION TYPE:C7SI, NR 2 PYLON GOUGES ON RT CONE BOLT HOUSING. REPAIRED IAW SMRO EO 99-14-017RI & MM 71-21-11 UPS ENGINEERING FILE NR 727-54-0086.

Part: SKIN — CORRODED (BS 870)

INSPECTION TYPE:C&SI, SURFACE CORROSION ON RT 870 FITTING AT CENTER TANK TORQUE SKIN. REPAIR CARRIED OUT IAW SMRO EO 99-14-03 UPS ENGINEERING FILE NR 727-57-2064.

Part: HINGE — CRACKED (MLG MANUAL DOOR)

INSPECTION TYPE: C & SI, NLG MANUAL EXT DOOR HINGE STIFF, LT MLB MANUAL EXT DOOR HINGE CRACKED. HINGES REPLACED IAW SRM 51-30-02.

Part: HINGE — CORRODED (RT AILERON TAB)

INSPECTION TYPE:C+SI, RIGHT I/B AILERON TAB O/B HINGE CORRODED (CASTING). REPAIR CARRIED OUT IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 540-560)

INSPECTION TYPE: C & SI, FWD CARGO BAY CORROSION ON STRINGER 23L AT BS 540 TO BS 560. REPAIR CARRIED OUT IAW SRM 51-10-6 & SRM 53-10-3 FIG 2.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE:C+SI, RIGHT I/B AILERON TAB PUSHROD MAST FITTING CORRODED. RIGHT I/B AILERON TAB MAST IS REPLACED IAW SRM 51-30-2.

Part: SUPPORT — BROKEN (BS 1010)

INSPECTION TYPE:C+SI, BROKEN DUCTING SUPPORT AT LT BS 1010 LBL 42.5. DUCTING SUPPORT REPLACED, FABRICATED IAW SRM 51-20-1.

Part: NUT — CORRODED (BS 540-560)

INSPECTION TYPE:C&SI SURFACE CORROSION AROUND A/NUTS BS 540 - 560 LT LBL 24.75. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 53-10-5 FIG 1.

Part: BALANCE PANEL — CRACKED (RT ELEVATOR)

INSPECTION TYPE:C&SI NR 2 BALANCE PANEL AFT HINGE FWD HALF CRACKED RT SIDE. REPLACED NR 2 BALANCE PANEL AFT HINGE FWD HALF IAW 27-30-21 MM.

Part: SKIN — CORRODED (BS 860)

INSPECTION TYPE:C&SI, CORROSION AROUND FASTENER HEADS WING CENTER SECTION UPPER SKIN BS 860 RBL 60. REPAIRED IAW SMRO EO 99-14-014 UPS ENGINEERING FILE NR 727-57-2065.

Part: ANGLE — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, CORROSION ON FACE OF RISER ABOVE NR 12 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-D.

Part: SEAL — CRACKED (BS 860)

INSPECTION TYPE:C&SI, ON REMOVAL OF VAPOR SEAL AT BS 870 RAMP PLATE AT BS 860 LBL 60 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-40-3.

Part: SKIN — CORRODED (BS 860)

INSPECTION TYPE:C&SI, CORROSION AROUND FASTENER HEAD WING CENTER SECTION UPPER SKIN BS 860 LBL 60. REPAIRED CARRIED OUT IAW SNN MRO EO 99-14-013 UPS ENGINEERING FILE NR 727-57-2061.

Part: ANGLE — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, CORROSION ON RISER FACE ABOVE NR 14 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-A.

Part: ANGLE — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, CORROSION ON FACE OF RISER ABOVE NR 11 FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-A.

Part: ANGLE — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, CORROSION EVIDENT ON RISER FACE ABOVE NR 13 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-A.

Part: ANGLE — CORRODED (AIRSTAIRS)

INSPECTION TYPE:C+SI, RISER SURFACE CORRODED ABOVE NR 10 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-A.

Part: BEAM — CRACKED (BS 930)

INSPECTION TYPE: C & SI, CRACK FOUND ON LONGITUDINAL BEAM IN KEEL AREA RT SIDE BS 930 WL 160 APPROX. NEW BEAM FABRICATED IAW DRG NR 65-28900, NEW BEAM INSTALLED IAW SRM 51-30-2.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 1 FLAP TRACK ATTACH FITTING ON I/B AND O/ B FACES. CORROSION REMOVED IAW SRM 51-10-06, REPAIR CARRIED OUT IAW SMRO EO 99-14-002 UPS ENGINEERING NR 727-57-2074.

Part: STRINGER — CORRODED (BS 1080)

INSPECTION TYPE:C&SI AFT CARGO BAY CORROSION ON STRINGER 19 R AT BS 1080. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 AND 51-10-02 AND DRAWING 65-18385.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 8 FLAP TRACK ATTACH FITTING I/B AND O/B FACE. REPAIR CARRIED OUT IAW SMRO EO 99-14-002 UPS ENGINEERING FILE NR 727-57-2074.

Part: MOUNT — CORRODED (NR 1 ENGINE)

INSPECTION TYPE:C&SI, PITTING CORROSION IN BORE OF HOLES IN NR 1 ENG FWD MOUNT FITTING. REPAIRED IAW SMRO EO 99-14-011 UPS ENGINEERING FILE NR 727-54-011.

Part: BEAM — CRACKED (BS 930)

INSPECTION TYPE: C & SI, CRACK FOUND ON LONGITUDINAL BEAM IN KEEL AREA LT SIDE BS 930 WL 160 APPROX. NEW BEAM FABRICATED IAW FRG NR 65-28900, BEAM INSTALLED IAW SRM 51-30-2.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 7 FLAP TRACK ATTACH FITTING ON I/B FACE. REPAIRED IAW SMRO EO 99-14-002 ENGINEERING FILE NR 727-57-2074.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 2 FLAP TRACK ATTACH FITTING ON I/B FACE. REPAIR CARRIED OUT IAW SMRO EO 99-14-002 UPS ENGINEERING FILE NR 727-57-2074.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:C&SI SUSPECT CRACKS ON SLAT RIBS AT NR 4 SLAT ACTUATOR ATTACH POINT. REPLACED CRACKED RIBS IAW DRAWING NR 65-17276.

Part: CARGO TRACK — CRACKED (BS 1090)

INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1090 RBL 14 IS CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5.

Part: CARGO TRACK — CRACKED (BS 1070)

INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1070 RBL 14 IS CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5.

Part: TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE: C & SI, CORROSION IN HOLES E & C IN NR 5 FLAP TRACK. REPAIRED IAW UPS EO B727-5742-0651-J.

Part: PAD — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, CORROSION ON NR 5 FLAP TRACK AFT PAD. REPAIR CARRIED OUT IAW OHM 20-20-01 AND UPS EO B727-5742-0651-J.

Part: CHANNEL — CRACKED (BS 1070)

INSPECTION TYPE:C&SI AFT CARGO BAY FLOOR CHANNEL CRACKED AT BS 1070 LBL 3. REPAIRED CHANNEL IAW SRM 53-10-5 AND 53-10-2 FIG 8.

Part: SKIN — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:C+SI, NR 6 LE SLAT O/B TRACK SKIN TO TRACK ATTACH BRACKETS CRACKED. BRACKETS REPLACED IAW SRM 51-30-02.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, CORROSION ON NR 5 FLAP TRACK FWD LUGS I/B AND O/B FACES. REPAIR CARRIED OUT IAW SMRO EO 99-14-008 UPS ENGINEERING FILE NR 727-58-2078.

Part: STRUCTURE — CORRODED (NR 2 ADF ANTENNA)

INSPECTION TYPE: C & SI, CORROSION ON SUPPORT STRUCTURE FOR NR 2 ADF ANTENNA. REPLACED SUPPORT STRUCTURE IAW SRM 53-10-2 FIG 3.

Part: ANGLE — CRACKED (BS 1150)

INSPECTION TYPE:C&SI AFT CARGO BAY ANGLE ON FLOOR CHANNEL AT BS 1150 RBL 4 IS CRACKED ANGLE REPLACED IAW SRM 53-10-2 FIG 8.

Part: CASTING — CORRODED (RT AILERON)

INSPECTION TYPE:C&SI, RIGHT O/B AILERON LOCKOUT CASTING HAS SURFACE CORROSION AROUND QUADRANT PIVOT BOLT. REPAIR CARRIED OUT IAW SRM 27-10-2 & 51-30-8.

Part: PAD — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 5 FLAP TRACK FWD PAD. REPAIRED IAW UPS EO B727-5742-0651-J.

Part: CHANNEL — CRACKED (BS 1130)

INSPECTION TYPE: C & SI, AFT CARGO BAY FLOOR CHANNEL CRACKED AND DENTED AT BS 1130 RBL 9. FLOOR CHANNEL REPAIRED IAW SRM 53-10-05 FIG 4 & SRM 53-10-2.

Part: CARGO TRACK — CRACKED (BS 1070)

INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1070 LBL 18 IS CRACKED. REPAIRED IAW SRM 53-10-5.

Part: STIFFENER — CORRODED (RT MLG WW)

INSPECTION TYPE:C&SI, CORROSION ON UPPER END OF VERT STIFFENER ATTACHED TO FWD BULKHEAD OF RT WHEEL WELL BBL 40 APPROX. VERTICAL STIFFENER AND NESTING REPLACED IAW DRG NR 65-16330.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 2 FLAP TRACK FWD LUGS (O/B LUG O/B FACE, I/B LUG I/B AND O/B FACES). REPAIRED IAW SMRO EO 99-14-006 ENGINEERING FILE NR 727-57-2080.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 8 FLAP TRACK FWD LUGS (O/B LUG I/B 7 O/B FACES I/B LUG I/B AND O/B FACES). REPAIRED IAW SMRO EO 99-14-010 ENGINEERING FILE NR 727-57-2076.

Part: S DUCT — CRACKED (BS 1243)

INSPECTION TYPE:C&AI, CRACK ON INTERNAL SKIN OF 'S' DUCT AT BS 1243 AT 9 O'CLOCK POSITION. REPAIR CARRIED OUT IAW SRM 54-10-03 FIG 201.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 3 FLAP TRACK FWD LUGS (O/B LUG I/B FACE I/B LUG I/B AND O/B FACES). REPAIRED IAW SMRO EO 99-14-007 UPS ENGINEERING FILE NR 727-57-2079.

Part: GUSSET — CRACKED (VERT STAB)

INSPECTION TYPE: C & SI, VERT STAB MAIN BOX INTERIOR 9TH COMPARTMENT FROM TOP, RIB TO SKIN ATTACH GUSSET CRACKED AT S7 RT. GUSSET REPLACED IAW SRM 51-20-1 FIG 7.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 7 FLAP TRACK FWD LUGS (O/B LUG O/B FACE I/B LUG I/B AND O/B FACES). REPAIRED IAW SMRO EO 99-14-009 ENGINEERING FILE NR 727-57-2077.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, NR 3 FLAP TRACK HOLES D AND C CORRODED. REPAIRED CARRIED OUT IAW OHM 57-40-01.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, NR 6 FLAP TRACK CORRODED. REPLACED NR 6 TRACK IAW MM 57-51-31.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE: C & SI, NR 3 FLAP TRACK AFT HOLE G CORRODED. REPAIR CARRIED OUT IAW OHM 57-40-01.

Part: WINDOW FRAME — CRACKED (BS 980)

INSPECTION TYPE:C&SI MAIN CARGO DECK WINDOW FRAME STRUCTURE CRACKED AT BS 980 LEFT S11 WINDOW FRAME REPLACED IAW DWG NR 65-19851 NES SEAL FITTED REF MM 56-20-00.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE: C & SI, PITTING CORROSION ON NR 1 FLAP TRACK O/B FACE ALONG ROLLER MATING SURFACE. REPLACED FLAP TRACK IAW MM 27-51-31.

Part: BRACKET — CRACKED (LT WING TIP)

INSPECTION TYPE: C & SI, LT WING TIP LENS ATTACH BRACKET AFT LWR END CRACKED. REPLACED BRACKET IAW SRM 51-30-2.

Part: HANDLE CUTOUT — CRACKED (CARGO DOOR)

INSPECTION TYPE: C & SI, AFT CARGO DOOR SUSPECT CRACK IN HANDLE CUTOUT. REPAIRED IAW SRM 51-10-02.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE: C & SI, SUSPECT CRACK ON MCD SKIN LWR EDGE BS 550. REPAIRED IAW SRM 52-20-2.

Part: SKIN — CORRODED (RT ELEVATOR)

INSPECTION TYPE:C, ON REMOVAL OF RT ELEVATOR STATIC DISCHARGER ELEVATOR SKIN FOUND CORRODED. ELEVATOR SKIN PANEL REPLACED IAW DRAWING 65-25640.

Part: FITTING — CRACKED (BS 487.1)

INSPECTION TYPE:C, MAIN CARGO DOOR SUPPORT LATCH FITTING AT BS 487.1 CRACKED. LATCH SUPPORT FITTING REPLACED IAW B727-5310-0437.

Part: SKIN — CUT (BS 740)

INSPECTION TYPE:C EXISTING CUTOUT ON FUSELAGE SKIN AT BS 740 BETWEEN STR 17 RT AND 18 RT REPAIR CARRIED OUT IAW SRS EO 98-22-009, REF UPS ENGINEERING FILE NUMBER 727-53-2050.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE:C, CRACK FOUND ON LT BS 940 FITTING ROW ONE SECOND HOLE AFT CRACK. REMOVED AND RETAINED IAW SRM 51-10-1. REFER TO SRS EO 98-22-0 07, REFERENCE UPS ENGINEERING FILE NUMBER 727-53-2049, FOR COMPLETION OF REPAIR.

Part: FITTING — CRACKED (LT MLG DOOR)

INSPECTION TYPE:C, LT MLG WING DOOR AFT HINGE FITTING ON NR 4 FLAP TRACK CRACKED. HINGE FITTING REPLACED IAW SRM 51-30-03 AND MM 21-80-01.

Part: TIP — CORRODED (RT ELEVATOR)

INSPECTION TYPE:C, CORROSION ON LOWER SKIN RT ELEVATOR TIP IN AREA OF STATIC WICK. ELEVATOR SKIN PANEL REPLACED IAW DRAWING 65-25640.

Part: FITTING — CORRODED (WS 330.5)

INSPECTION TYPE:C, NR 6 FLAP TRACK MIDFAIRING FWD HINGE CASTING HAS LIGHT SURFACE CORROSION FITTING REPLACED IAW SRM 51-30-02.

Part: FAIRING — CORRODED (NR 1 TE FLAP)

INSPECTION TYPE:C, NR 1 FLAP TRACK MID FAIRING FWD HINGE CASTING CORRODED. CASTING REPLACED IAW SRM 51-30-02.

Part: WEB — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, ON GAINING ACCESS TO CRACKED CENTER WEB OF FWD CARGO DOOR, DISCOVERED WEBS FWD AND AFT CRACKED. ALSO, WEBS REPLACED IAW DRAWING 65-18620.

Part: CASTING — CORRODED (WS 450)

INSPECTION TYPE:C, ON REMOVAL OF NR 4 SPOILER ACTUATOR SUPPORT CASTING, CASTING FOUND TO BE BADLY CORRODED. CASTING REPLACED IAW DRAWING 65-17351 AND SUPPORT ANGLES REPLACED IAW DRAWING 65-16201.

Part: FIREWALL — CRACKED (BS 1387.85)

INSPECTION TYPE-C, WEB OVER NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1387.85 IS CRACKED. WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: SKIN — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE:C SUSPECT CRACK ON NR 5 KREUGER FLAP OUTER SURFACE AT BULLNOSE MID HINGE CUTOUT. KREUGER FLAP REPLACED IAW MM 27-81-01.

Part: FAIRING — CRACKED (TE FLAP TRACK)

INSPECTION TYPE-C, NR 5 FLAP TRACK AFT FAIRING CRACK AT AFT INBOARD CORNER. FLAP FAIRING REPAIRED IAW UPS EO B727-5750-3837.

Part: ANGLE — CRACKED (LT TE FLAP)

INSPECTION TYPE-C, LWR CHORD ANGLE ON LT INB MIDFLAP INB CARRIAGE SUPPORT STRUCTURE CRACKED. LWR CHORD ANGLE REPLACED IAW SRM 51-30-02.

Part: BEAM — CORRODED (RT HORIZ STAB)

INSPECTION TYPE-C, RT STAB UPPER SURFACE T/E BEAM HAS SEVERAL AREAS OF CORROSION FROM I/B TO O/B. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-1. BEAM REPLACED IAW DRAWING NR 65-22987.

Part: TRACK — DAMAGED (LT TE FLAP)

INSPECTION TYPE:C, LT WING INB FLAP INB FLAP TRACK DAMAGED DUE TO SHEARED DEAD WEIGHT ROLLER. REMOVED NR 4 FLAP TRACK IAW MM 27-51-31. INSTALLED NEW TRACK IAW MM 27-51-31.

Part: FITTING — CRACKED (WS 491.5)

INSPECTION TYPE:C, NR 12 SPOILER SUPPORT FITTING CRACKED AT I/B CORNER OF CASTING. REPLACED SUPPORT FITTING IAW DRAWING 65-16201.

Part: CASTING — CRACKED (NR 4 TE FLAP)

INSPECTION TYPE-C, NR 4 FLAP TRACK TEAR DROP FAIRING SPIGOT CASTING CRACKED. REPLACED CASTING IAW MM 27-50-00.

Part: ANGLE — CRACKED (NR 3 SPOILER)

INSPECTION TYPE:C, NR 3 SPOILER ACTUATOR CASTING INBD SUPPORT ATTACH ANGLE CRACKED. REPLACED SUPPORT ANGLES IAW DRAWING 65-16201, BOTH ANGLES REPLACED TO CASTING REPLACEMENT.

Part: BRACKET — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C, LT ELEVATOR BRACKET ON REAR SPAR AT ELEV STA 66.5 APPROX CRACKED. OPENED ELEVATOR SKIN IAW SRM 51.30.2, ANGLE BRACKET REPLACED IAW DRAWING NR 69-19144 ELEVATOR SKIN CLOSED IAW DRAWING NR 65-25635.

Part: HINGE — CORRODED (CARGO DOORWAY)

INSPECTION TYPE-C, ON REMOVAL OF MAIN CARGO DOOR, DEEP CORROSION FOUND ON HINGE SECTIONS OF FUSELAGE. MAIN CARGO DOOR FUSELAGE ATTACH HINGE SECTIONS (6 OFF) REPLACED IAW DRAWING 65-25337.

Part: CASTING — CRACKED (NR 5 TE FLAP)

INSPECTION TYPE-C, NR 5 FLAP CARRIAGE LWR DEAD WEIGHT ROLLER CASTING CRACKED. FITTING AND ASSOCIATED HARDWARE REPLACED IAW OHM 57-58-02.

Part: ANGLE — DAMAGED (WS 445)

INSPECTION TYPE:C NR 4 SPOILER ACTUATOR CASTING OUTBD SUPPORT ATTACH ANGLE HOLES BADLY ELONGATED. REPLACED ATTACH ANGLES IAW SRM 51-30-2.

Part: BEAM — CORROSION (LT HORIZ STAB)

INSPECTION TYPE-C, SURFACE CORROSION ON LT STAB UPPER T/E BEAM FROM I/B TO O/B END. T/E BEAM REPLACED IAW DRAWING NR 65-22987.

Part: WEB — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, SUSPECT CRACK ON INNER UPPER WEB OF FWD LOWER CARGO DOOR WEB. REPLACED IAW DRAWING 65-18620.

Part: RIB — CRACKED (LT TE FLAP)

INSPECTION TYPE-C, SUSPECT CRACK IN LT I/B FLAP I/B CARRIAGE SUPPORT STRUCTURE. RIB CHORD REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 480-620)

INSPECTION TYPE-C, SURFACE CORROSION ON SEAT TRACK BS 480 AND 620 APPROX LBL 62.5. NEW SECTION OF SEAT TRACK FABRICATED FROM EXTRUSION STOCK. SEAT TRACK REPAIRED IAW SRM 53-10-5, FIG 3.

Part: FITTING — CRACKED (BS 580)

INSPECTION TYPE:C, MAIN CARGO DOOR SUPPORT LATCH FITTING AT BS 580 CRACKED. LATCH SUPPORT FITTING REPLACED IAW B727-5310-0437.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, CRACK IN TOP FRAME OF FWD CARGO DOOR. FRAME REPLACED IAW DRAWING 65-18620.

Part: BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE:C ON REMOVAL ON MAIN CARGO DOOR CORROSION DISCOVERED ON UPPER BEAM. BEAM REPLACED IAW SRM 51-30-2 AND SRM 51-10-06 AND SRS EO 98-22-002, REF UPS ENGINEERING FILE NUMBER 727-52-0191.

Part: CASTING — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, TOP AFT CORNER CASTING CRACKED ON MAIN CARGO DOOR. TOP AFT CORNER FITTING ON MAIN CARGO DOOR REPLACED IAW SRM 51-30-2, REF BOEING DWG NR 65-25337.

Part: BULKHEAD FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, BULKHEAD FITTING BS 740 RT HAS CRACKS. RT BULKHEAD FITTING REPLACED IAW EO B727-5310-7477.

Part: CASTING — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, TOP FWD CORNER CASTING CRACKED ON MAIN CARGO DOOR. TOP FWD CORNER FITTING ON MAIN CARGO DOOR REPLACED IAW SRM 51-30-2, ALSO REF BOEING DWG NR 65-25337.

Part: BULKHEAD FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, (CHORD ANGLE) BULKHEAD FITTING BS 740 LT HAS CRACKS. LT BULKHEAD FITTING REPLACED IAW EO B727-5310-7477.

Part: SKIN — CRACKED (BS 211.8)

INSPECTION TYPE-C, CRACK BS 211.8 RT SIDE AT WL 219.5 ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3.

Part: CHORD — CORRODED (BS 340-351)

INSPECTION TYPE-C, CORROSION AT WALKWAY LEVEL LT SIDE ON T-CHORD AT BS 351 TO 340 APPROX. REPAIRED CHORD IAW SRM 51-40-4.

Part: SKIN — CRACKED (BS 243.7)

INSPECTION TYPE-C, CRACK BS 243.7 RT SIDE AT WL 222 APPROX ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3.

Part: ANGLE — CRACKED (NR 1 LE FLAP)

INSPECTION TYPE:C, SUSPECT CRACK IN NR 1 KREUGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEW FABRICATED ANGLE IAW SRM 51-10-1, PAGE 4.

Part: ANGLE — CRACKED (NR 2 LE FLAP ACT)

INSPECTION TYPE-C, SUSPECT CRACK IN NR 2 KRUEGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEWLY FABRICATED ANGLE IAW SRM 51-10-10, ANGLE INSTALLED IAW SRM 51-30-2.

Part: FLAP — CORRODED (NR 5 LE FLAP)

INSPECTION TYPE-C, NR 5 KREUGER FLAP CORRODED BEYOND SRM 57-50-1 LIMITS. NR 5 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.

Part: FLAP — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, CORROSION ON NR 4 KREUGER FLAP FOUND TO BE BEYOND LIMITS OF SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.

Part: FLAP — CORRODED (NR 6 LE FLAP)

INSPECTION TYPE-C, NR 6 KREUGER FLAP CORRODED BEYOND LIMITS OF SRM. NR 6 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.

Part: FITTING — CORRODED (BS 360)

INSPECTION TYPE-C, STR 22 LT END FITTING CORRODED BS 360. *S/D* STRINGER END FITTING REPLACED IAW BOEING DRAWING 65-18420.

Part: SKIN — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE-D, LT WING LE SLAT NR 3 CRACK AT RIVET HOLE ON LE SKIN CENTER. *S/D* HFEC INSPECTED PER NDT PT6 51-00-00 FIG4, CRACKS CONTAINED BY STOP DRILL HOLES. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 1.

Part: HINGE FITTING — CORRODED (RT AILERON)

INSPECTION TYPE-D, RT O/B AILERON NR 2 HINGE FITTING CASTING SHOWS SIGNS OF CORROSION. FITTING REPLACED IAW SRM 51-30-2.

Part: CASTING — CORRODED (AILERON CONTROL)

INSPECTION TYPE-D, ON REMOVAL OF AILERON CONTROL TURNAROUND PULLEY, BRACKET MOUNTING PULLEY FOUND TO BE SEVERELY CORRODED. *S/D* CASTING REPLACED IAW SRM 51-30-02.

Part: CASTING — CORRODED (RT AILERON TAB)

INSPECTION TYPE-C, RT I/B AILERON TAB O/B BEARING CASTING SHOWS SIGNS OF CORROSION. *S/D* FITTING REPLACED IAW SRM 51-30-2.

Part: PANEL — CORRODED (RT MLG WW)

INSPECTION TYPE-D, PANEL ON UNDERSIDE OF WALKING BEAM IN RT MAIN LANDING GEAR WHEEL WELL HAS SOME SURFACE CORROSION. *S/D* CORROSION FOUND TO BE OUTSIDE LIMITS PER SRM 51-10-01. PANEL REPLACED IAW SRM 51-30-2.

Part: CASTING — CORRODED (RT AILERON)

INSPECTION C-CHECK, RT INBOARD AILERON TURNAROUND PULLEY SUPPORT CASTING HAS CORROSION. CASTING REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE-C, NR 3 FLAP TRANSMISSION SUPPORT FITTING CORRODED IN MOUNTING HOLES FOR TRANSMISSION. *S/D* FLAP TRANSMISSION SUPPORT FITTING REPLACED IAW SRM 51-30-02.

Part: SKIN — CORRODED (BS 481)

INSPECTION TYPE-D, SUSPECT 10 TO 15 PERCENT MATERIAL LOSS BETWEEN S6R-S7R ON FWD SKIN AT BS 481 BUTT JOINT. *S/D* REPAIR CARRIED OUT IAW B727-5310-1371 APPENDIX 8.5.

Part: BRACKET — CORRODED (RT AILERON)

INSPECTION TYPE-C, RT INBAORD AILERON TURNAROUND PULLEY SUPPORT CASTING HAS CORROSION. ALSO, PLAY ON PULLEY (TURNAROUND PULLEY). *S/D* CASTING REPLACED IAW SRM 51-30-2. PLAY REMOVED BY BEARING REPLACEMENT PER MM 20-10-07.

Part: SKIN — CORRODED (BS 481)

INSPECTION TYPE-D, SUSPECT 10 TO 15 PERCENT MATERIAL LOSS FROM JUST ABOVE S9R TO JUST ABOVE S10R AT BS 481 BUTT JOINT. *S/D* REPAIR CARRIED OUT IAW EO B727-531-1371 APPENDIX 8.5.

Part: FLAP — CORRODED (NR 2 LE FLAP)

INSPECTION TYPE-C, WIDE SPREAD PITTING CORROSION ON NR 2 KREUGER FLAP. CORROSION BEYOND REPAIRABLE LIMITS OF SRM 57-50-1. NR 2 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.

Part: RIB — CRACKED (NR 5 LE SLAT)

INSPECTION TYPE-D, SLAT 5 CRACK ON RIB AT WS 464 SLAT STA 120. CRACK APPROX .75 INCH LONG. *S/D* HFEC CARRIED OUT IAW NDT PT 6 51-00-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 9.

Part: STRINGER — CRACKED (WS 686)

INSPECTION TYPE-D, LT WING CRACK ON VENT STRINGER TAB NR 14 AT WS 686.5. *S/D* CRACKED TAB REMOVED PER SRM 51-10-6. HFEC CARRIED OUT IAW NDT PT 6 5 1-00-00 FIG 4, NO DEFECTS INDICATED. REPAIR CARRIED OUT IAW SB 727- 57A0159 FIGS 2 AND 4.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, ON INSPECTION OF BS 740 FITTING LT, CRACK AT LWR FASTENER HOLE FOUND TO BE PROGRESSED FROM LOWER FASTENER TO END OF FITTING. *S/D* HFEC INSPECTION CARRIED OUT IAW NDT PT6 51-00-00 FIG 4. CRACK FOUND TO HAVE PROGRESSED FROM LOWER FASTENER TO END OF FITTING. BS 740 LT REPAIR CARRIED OUT IAW UPS EO B727-5310-7497-A APPENDIX B.

Part: FITTING — CORRODED (LT AILERON)

INSPECTION TYPE-D, LT OUTBOARD AILERON HINGE FITTING 2ND HINGE OUTBOARD CORRODED IN BUSHING AREA. FITTING REPLACED IAW DWG 65-19275.

Part: ANGLE — CRACKED (BS 328)

INSPECTION TYPE-D, ON REMOVAL OF SKIN PANEL FRAME ATTACH ANGLE BS 328 BETWEEN S18L AND S19L FOUND CRACKED. *S/D* CRACK STOP TRIMMED, HFEC CONFIRMED PER NDT PT6 51-00-00 FIG 4. REPAIR CARRIED OUT IAW SRS EO 97-01-002 (UPS MINOR REPAIR AUTHORISATION FILE NO 727-53-1860).

Part: STRINGER — CORRODED (BS 520)

INSPECTION TYPE-D, INVESTIGATE EVIDENCE OF CORROSION ON STRINGER 26R BS 520. *S/D* STRINGER FOUND CORRODED BEYOND LIMITS PER SRM 51-10-6. STRINGER REPLACED IAW SRM 51-10-1 AND 51-30-2.

Part: HINGE FITTING — CORRODED (LT AILERON)

INSPECTION TYPE-C, LT OUTBOARD AILERON HINGE FITTING 4TH HINGE OUTBOARD CORRODED IN BUSH HOUSING. *S/D* FITTING REPLACED IAW BOEING DRAWING 65-19277.

Part: FITTING — CRACKED (NR 14 SPOILER)

INSPECTION TYPE-C, NR 14 SPOILER O/B CASTING SECURING SPOILER PANEL STOP IS CRACKED. CASTING REPLACED IAW SRM 51-30-02.

Part: SKIN — CORRODED (NR 1 LE FLAP)

INSPECTION TYPE-C, NR 1 KREUGER FLAP CORRODED CORROSION BEYOND LIMITS PER SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.

Part: ARM SUPPORT — CORRODED (LT AILERON)

INSPECTION TYPE-D, LT INBOARD AILERON MIDDLE HINGE SUPPORT ARM CORRODED. *S/D* AILERON MIDDLE HINGE SUPPORT ARM REPLACED IAW MM 27-10-01.

Part: SUPPORT — CORRODED (BS 348.2)

INSPECTION TYPE-C, AREA UNDER LAVATORY, CORROSION ON TOP-HAT SECTION AT LAVATORY ENTRY THRESHOLD AT BS 348.2 RBL 24.75. *S/D* NEW SECTION OF SUPPORT FABRICATED FROM EXTRUSION BAC 1510-335 AND FITTED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (LT TE MIDFLAP)

INSPECTION TYPE-C, REF STAR AIR NRC 235558 : TEMPORARY REPAIR CARRIED OUT TO LT OUTBOARD MID FLAP TRAILING EDGE INBOARD SIDE UPPER SKIN. *S/D* TEMPORARY REPAIR REMOVED AND PERMANENT REPAIR CARRIED OUT IAW SRM 51-4 0-6 FIG 25. FOKKER BOND TEST CARRIED OUT IAW B727 NDT MANUAL D6-48875 PART 4 CHAPT 51-40-00 FIG 1.

Part: SKIN — CRACKED (NR 5 LE SLAT)

INSPECTION TYPE-D, OUTER SKIN ON LOWER SURFACE OF NR 5 SLAT OUTBOARD END CRACKED APPROX 6 CM. HFEC INSPECTED PER NDT PT6 51-00-00 FIG 4, CRACK CONTAINED BY FASTENER HOLE AND STOP DRILL HOLE. REPAIR CARRIED OUT PER SRM 57-30-3 FIG 1.

Part: SKIN — CORRODED (NR 3 LE FLAP)

INSPECTION TYPE-C, PAINT BLISTERING FROM NR 3 KREUGER FLAP. SUSPECT CORROSION ON INVESTIGATION CORROSION FOUND TO BE OUTSIDE. REPAIR LIMITS OF SRM 57-50-1. NR 3 KREUGER FLAP REPLACED IAW MM 27-81-01.

Part: SKIN — CORRODED (BS 259-360)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL STRUCTURE AT BS 348 AND 312 BETWEEN S19 AND 20 LT. *S/D* NDT INSPECTION CARRIED OUT PER NDT PT 6 51-00-00 FIG 5, 20 PERCENT LOSS OF MATERIAL INDICATED.