N921UP

Part: FITTING — BROKEN (O2 BOTTLE)

INSPECTION TYPE:IN OXYGEN BOTTLE ATTACHING HARDWARE BROKEN. *S/D* REMOVED AND REPLACED MS FITTING ON BLOWOUT LINE AND UPPER 02 BOTTLE CLAMP. REMOVED AND REPLACED 02 BOTTLE. LK CHECK GOOD.

Part: SWITCH — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A CO PILOTS EMERG 0XYGEN SWITCH FAILS TO FULLY CLOSE ***SUPPLEMENTAL MRR*** REPLACED CO-PILOTS REGULATION W/SERVICABLE RUGULATION AND REPLACED W ITH SERVICABLE BOTTLE. LEAKED CHECK OK OPS CHECK PER 727 MM CHPT 35- 11-31 AND 12-15-11

Part: MOTOR — FAILED (TE FLAP) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, O/B ALT FLAP MOTOR NOT RETRACTING FLAPS. REPLACED MOTOR IAW MM 27-51-141.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 312 RBL 24. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 318 AND LBL 4. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON AFT O/B AND FWD FLANGES OF BS 930 FUSELAGE FITTING BETWEEN S18A AND S19 LT. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611 APPENDIX 8.1

Part: FITTING — CORRODED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, DUE TO EXCESSIVE CORROSION IN BS 940 LT FITTING FASTENER HOLES, REPLACE FITTING BS 940 LT. REPLACED IAW UPS EO B727-5310-4501 APPENDIX C.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED. STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG NR 65-18636 AND SRM 51-30-2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. REPAIR CARRIED OUT IAW SRM 51-30-2 DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORZ STIFFENER AT BS 900 APPROX IS CRACKED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG 65-18636 AND SRM 51-30-2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORIZ STIFFENER AT BS 900 APPROX IS CRACK ED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. REPAIR CARRIED OUT IAW DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, ENG NR 1 FWD MOUNT, PITTING CORROSION FOUND IN FWD BOLT HOLES I/B, O/B. REPAIR CARRIED OUT IAW EOJ NR B727-5440-11592.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT PITTING CORROSION FWD IN BOTH I/B MOUNT HOLES. REPAIR CARRIED OUT IAW EO B7274401592.

Part: BEAM — CRACKED (BULKHEAD) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, CRACK FOUND AT BS 1183 BULKHEAD VERTICAL BEAM RBL 26.83 AT WL 259.5. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631.

Part: BEAM — CRACKED (BULKHEAD) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, FOUR CRACKS FOUND AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AT WL 257 AND WL 260. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631AND BOEING DRG 65C34406.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, SKIN CRACKS AT BS 203.8 RT AT WL 18 AND WL 20. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, SKIN CRACK AT BS 243.7 WL 19 LT. CRACKED AREA OF SKIN CUT OUT IAW SRM 53-30-3 FIG 3. HFEC C/O IN ALL ACCESSED HOLES AND AROUND PERIFERY OF CUTOUT. POST FASTENER REMOVAL AND SKIN CUTOUT IAW B727 NDTM. NO DEFECTS FOUND IN FASTENER HOLES AND CUTOUT. CRACK FOUND TO BE REMOVED BY CUTOUT.

Part: BRACKET — CRACKED (NR 3 ENGINE T/R) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACE IAW MM 20-80-01.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, EVIDENCE OF CORROSION TO S18A FLANGE (HORIZ) AT BS 870 LT. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 51-30-2 AND SMRO EO 2000-38-003 AND EO B727-5330-3815 UPS ENGINEERING FILE NR 727-53-2292.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 46,781 hrs · 34,052 cycles

INSPECTION TYPE:C, BILGE IN SKIN (SUSPECT CORROSION) AT BS 1030 ABOVE STR 18 LT. GILL LINER REMOVED IAW MM 25-52-02. CORROSION ON EXTRUSION FOUND TO BE CORRODED AND OUTSIDE LIMITS SRM 53-30-01. NEW EXTRUSION INSTALLED IAW SRM 51-30-02. GILL LINER INSTALLED IAW MM 25-52-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,800 hrs · 15,449 cycles

INSPECTION TYPE: C CARGO BAY FLOOR SUPPORT LONGTITUDINAL BEAMS CRACKED TWO PLACES, BS 2020, BL 0, BS 1988, LBL 30 FLOOR SUPPORT BEAMS REPAIRED IAW SRM 53-10-07

Part: SUPPORT — CORRODED (RT TE FLAP)

INSPECTION TYPE: AD, RT SUPPORT ASSEMBLY INBOARD FLAP TRACK FORWARD CORRODED. SUPPORT ASSEMBLY REPLACED IAW BOEING DRAWING NR 65 19297, SHEET 3, REV E.

Part: LINK — CORRODED (RT MLG)

INSPECTION TYPE: AD, RT MLG TRUNNION LINK HAS PITTING CORROSION ON FORWARD BEARING SURFACE. REPLACED TRUNNION LINK ASSEMBLY. INSTALLED IAW MM 32-11-01.

Part: FITTING — LEAKING (RT WING)

INSPECTION TYPE:AD, FUEL LEAK AT RT WING BEHIND LANDING GEAR TRUNNION FITTING, ONLY STAINS. THIS MRR RESUBMITTED TO INCLUDE TRUNNION FITTING, FUEL LEAK REPAIRED IAW SMRO EO 99-35-001. TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.

Part: FITTING — LEAKING (LT WING)

INSPECTION TYPE:AD FUEL LEAK AT LT WING BEHIND LANDING GEAR TRUNNION FITTING. THIS MRR RESUBMIT TO INCLUDE TRUNNION FUEL LEAK. REPAIRED IAW SMRO EO 99-35-01 TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.

Part: ANGLE — CORRODED (BS 700)

INSPECTION TYPE:C, CORROSION ON 'T' ANGLE ON FAIRING UNDER AIR CONDITIONING EQUIPMENT AT BS 700. REPAIRES IAW SRM 51-40-2 FIG 1.

Part: STRINGER — CRACKED (BS 870)

INSPECTION TYPE:C, DURING ACCOMPLISHMENT OF RT 870 PARTIAL REPLACEMENT CRACK DISCOVERED AT FASTENER HOLE, LWR TANG, STR 13 AFT OF FITTING FLANGE. RT 870 FITTING REPLACED IAW UPS EO B727-5310-3056-B APPD E.

Part: HINGE — CRACKED (WS 686.5)

INSPECTION TYPE:C, RIGHT O/B AILERON HINGE CASTING CRACKED AT WS 68605 APPROX (I/B CASTING I/B BALANCE BAY). REPLACED CASTING IAW DRG 65-19260.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C, FRAME CRACKED SECOND FROM AFT AT MID TRACK ATTACH POINT ON AFT CARGO DOOR MOVABLE FAIRING. FRAME REPAIRED IAW SRM 51-40-3 FIG 1.

Part: HINGE — CORRODED (RT AILERON)

INSPECTION TYPE:C, RIGHT I/B AILERON CENTER HINGE FITTING CORRODED. REPLACED HINGE FITTING IAW MM 27-10-01.

Part: HINGE — CORRODED (RT AILERON TAB)

INSPECTION TYPE:C, RIGHT O/B AILERON TAB HINGES CORRODED. RIGHT O/B AILERON TAB HINGES REMOVED AND REPLACED IAW MM 27-10-41.

Part: SKIN — LOOSE (VERT STAB)

INSPECTION TYPE:C, VERTICAL STAB LT SIDE, SKIN LOOSE ADJACENT FASTENERS STR 57 AREA BELOW STAB GEARBOX FWD CUTOUT. REPAIR CARRIED OUT IAW SRM 55-30-5 FIG 4.

Part: CASTING — CORRODED (RT AILERON)

INSPECTION TYPE:C, RIGHT O/B AILERON TAB ROD HINGE CASTING CORRODED. HINGE CASTINGS REMOVED AND REPLACED IAW MM 27-10-41.

Part: SKIN — DELAMINATED (RUDDER TAB)

INSPECTION TYPE:C, UPPER RUDDER TAB RT SIDE HAS EVIDENCE OF DELAMINATION T/E AREA, AFT OF CENTER HINGE FITTINGS. REPAIRED IAW SRM 51-40-10 FIG 1.

Part: BRACKET — CRACKED (NR 3 ENGINE TR)

INSPECTION TYPE:C, ENG NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND MM 78-30-00.

Part: BRACKET — CRACKED (CARGO COMPT)

INSPECTION TYPE:C, ON INSPECTION OF THE FWD CARGO BAY CEILING, CARGO DOOR UPLOCK RETAINING BRACKET FOUND CRACKED. REPLACED BRACKET IAW SRM 51-20-1 FIG 3.

Part: SEAT TRACK — CORRODED (BS 770)

INSPECTION TYPE:C, TO FACILITATE REPAIR OF FRAME 783.95 LT, SEAT TRACK MUST BE REMOVED. ON REMOVAL, SEAT TRACK WAS FOUND TO BE CORRODED AT BS 770 LBL 62.5. NEW SEAT TRACK SECTION SPLICED IAW SRM 53-10-5 FIG 1.

Part: BRACKET — CRACKED (NR 1 ENGINE TR)

INSPECTION TYPE:C, ENG NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND MM 78-30-00.

Part: BRACKET — CRACKED (LT ELEVATOR)

INSPECTION TYPE:C, SUSPECT CRACK ON LT ELEVATOR REAR SPAR ON BRACKET AT TAB ROD CUTOUT. CRACKED BRACKET REPLACED IAW DRAWING 65-25635.

Part: FRAME — DAMAGED (BS 825.95)

INSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON FIRST FASTENER HOLE BELOW FLOOR AT BS 825 .95 RT. AFTER CLEAN UP THIS HOLE IS OUTSIDE LIMITS PER EO B727-5310-5 474 PAGE 9. FRAME REPAIRED IAW B727-5310-5474 APPENDIX C REF SMRO EO 99-12-002 AND UPS EO B727-5310-11383.

Part: FRAME — DAMAGED (BS 783.95)

INSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 783.95 LT. AFTER CLEAN UP, HOLE WAS OUTSIDE LIMITS PER EO B727-5310- 5474 PAGE 9. DAMAGED HOLE TAKEN TO 0.370 AND FREEZE PLUG INSTALLED IAW SRM 51-10- 7 REF SMRO EO 99-12-002 AND UPS EO B727-5310-11383-A. REPAIR TO FRAME RESULTING FROM OVERSIZING OF HOLE, CARRIED OUT IAW EO B727-5310-5474 APPX C.

Part: FRAME — DAMAGED (BS 848.95)

INSPECTION TYPE:C, MECHANICAL DAMAGE ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 848.95 LT. ON CLEAN UP, HOLE WAS OUTSIDE LIMITS PER PAGE 9 OF EO B727-5310 -5474. REPAIR TO FRAME CARRIED OUT IAW EO B727-5310-5474 APPENDIX C REF SMRO EO 99-12-002 AND UPS EO B727-5310-11383 FOR FREEZE PLUG INSTALLATION.

Part: FITTING — CRACKED (BS 480)

INSPECTION TYPE:C, SUSPECT CRACK ON FWD FLANGE OF BS 480 FITTING LT SIDE AT STR 17. REPAIR CARRIED OUT IAW SMRO EO 99-12-003R1 AND UPS ENGINEERING FILE NUMBER 727-53-2125.

Part: BULKHEAD — CRACKED (BS 930)

INSPECTION TYPE:C, CRACK ON RT KEEL BEAM BULK HEAD BS 930 WL 158. REPAIRED IAW SRM 51-40-2.

Part: FRAME — CRACKED (BS 312)

INSPECTION TYPE-D, CRACK IN FRAME 312 BETWEEN STR 26L AND LOWER CHORD. REPAIR CARRIED OUT IAW SRM 53-10-4 FIG 11.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE-D, CORROSION EVIDENT AT VARIOUS ANCHOR NUT LOCATIONS ALONG UNDERSIDE OF TOP CHORD OF FLOORBEAM BS 344. TOP CHORD OF FLOORBEAM REPLACED IAW BOEING DRAWING 65-16316.

Part: FRAME — CORRODED (BS 480)

INSPECTION TYPE-D, SURFACE CORROSION ON FRAME AT STR 26L BS 480. REPAIRED IAW SRM 53-10-4 FIG 13.

Part: STRINGER — DAMAGED (BS 740-760)

INSPECTION TYPE-D, BS 740 LT REPLACEMENT STR END AND STR AT 15L FOUND DAMAGED WITH EXISTING ELONGATED HOLES. STR END FITTING REPLACED (P/N 69-14469-3) AND INSTALLED IAW DRG NR 65C- 13724 STR SECTION BETWEEN BS 740 AND 760 LT REPLACED IAW SRM 53-10-2 FIG 9 AND INSTALLED IAW SRM 51-30-10.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-D, THREE CRACKS IN UPPER MID FRAME OF LWR FWD CARGO DOOR FRAME SECTION. REPLACED IAW SRM 51-30-2 AND DRAWING NR 65-18620.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE-D, CORROSION ON ANCHOR CLIP HOLE ON UPPER AND LOWER SURFACE OF FLOORBEAM TOP CHORD BS 312 LBL 19. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7.

Part: FRAME — CORRODED (BS 380)

INSPECTION TYPE-D, SURFACE CORROSION IN FLANGE OF FRAME BS 380 BETWEEN STR 24R AND 25R CARRIED OUT REPAIR ON FLANGE IAW SRM 51-40-3.

Part: VERT STIFFENER — CRACKED (CENTER TANK)

INSPECTION TYPE-D, CRACK AT TOP END OF VERTICAL STIFFENER NR 4 FROM O/B ON LT SIDE ON SPANWISE BEAM NR 1 STA 820 APPROX SECOND BAY OF CENTER TANK. REPAIRED IAW SRM 51-40-4 FIG 1.

Part: TIE POINT — CRACKED (BS 870)

INSPECTION TYPE-D, TANK LACING POINT ON REAR WALL STA 870 OF CENTER FUEL TANK CRACKED. TIE POINT IS SECOND FROM O/B ON RIGHT SIDE OF TANK REAR WALL. REMOVED AND INSTALLED TIE POINT IAW SRM 51-30-1.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE-D, CRACK IN FWD LOWER CARGO DOOR INNER SKIN 12 INCHES UP FROM THE BOTTOM OF THE DOOR, EXTENDING INWARD 1 INCH FROM THE AFT EDGE OF THE SKIN. REPAIR CARRIED OUT IAW SRM 52-30-1.

Part: BRACKET — CRACKED (BS 540)

INSPECTION TYPE-D, SUSPECT CRACK IN BRACKET AT FRAME 540 LBL 70. BRACKET REPLACED IAW SRM 51-30-2.

Part: BRACKET — CRACKED (BS 560)

INSPECTION TYPE-D, SUSPECT CRACK IN BRACKET END OF FRAME 560 LBL 70. BRACKET REPLACED IAW SRM 51-30-2.

Part: THRESHOLD — CORRODED (BS 302)

INSPECTION TYPE-D, CORROSION ON UNDERSIDE OF COCKPIT DOOR THRESHOLD WEB SUPPORT STA 302 RBL 12 - LBL 12. FABRICATED NEW WEB IAW SRM 51-20-1 FIG 7, INSTALLED IAW SRM 51-30-2.

Part: STRINGER — CRACKED (WS 656.5)

INSPECTION TYPE-D, NR 9 STR CRACKED LT WS 656.50. REPAIRED IAW B727-5710-0314 APP8.3.

Part: STRUCTURE — CORRODED (BS 342)

INSPECTION TYPE-D, CORROSION IN SEVERAL AREAS OF PARTITION SUPPORT STRUCTURE (FWD LAV AT ORY) BS 342 RBL15 - RBL 60 TOP CHORD. NEW SECTION FABRICATED FROM EXTRUSION BAC 1510-355 AND FITTED IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 378)

INSPECTION TYPE-D, CORROSION ON STR 26R BS 378. REPAIRED IAW SRM 53-10-3.

Part: STRAP — CORRODED (BS 340)

INSPECTION TYPE-D, CORROSION EVIDENT ON STRAP AT BS 343 RBL 20 ANCHOR NUT HOLE. NEW STRAP FABRICATED IAW SRM 51-20-1 AND FITTED PER SRM 51-30-2.

Part: PULLEY CASTING — CORRODED (NR 2 FLAP TRACK)

INSPECTION TYPE-D, FLAP POSITION CABLE PULLY CASTING ATTACHED TO NR 2 FLAP TRACK HAS CORROSION. PULLEY CASTING REPLACED IAW MM 20-80-01.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-D, BS 740 LT FITTING CRACKED BS 740 LT FITTING. REPLACED IAW UPS EO B727-5310-7477 BOEING DRG- NR 65C13724 AND SRS EO 97-34-012 UPS ENG FILE NUMBER NR 727-53-1975.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE-D, CORROSION AT STA 312 FLOORBEAM TOP CHORD ANCHOR NUT HOLE LBL 2. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7.

Part: HAT SECTION — CORRODED (BS 304-344)

INSPECTION TYPE-D, CORROSION ON UPPER SURFACE OF TOILET THRESHOLD SUPPORT BS 304 TO 344 RBL 12 - RBL 17 (TOP HAT SECTION). NEW SECTION OF TOILET THRESHOLD SUPPORT FABRICATED FROM EXTRUSION BAC 1510-335 AND FITTED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 295-349)

INSPECTION TYPE-D, FWD ENTRY DOOR THRESHOLD SILL CHORD ANGLE CORRODED AND CRACKED BETWEEN BS 295 TO 349 AT LBL 54-LBL 61. NEW THRESHOLD ANGLE INSTALLED IAW SRM 51-30-2.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 3 FLAP TRACK SPOILER SUPPORT PAD HAS CORROSION. REPAIRED IAW SRS EO 9734-005 UPS ENG FILE NUMBER 727-57-1896.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-D, CORROSION ON NR 7 FLAP TRACK FWD LUGS. REPAIR CARRIED OUT IAW SRS EO 97-34-009 UPS ENG FILE NUMBER 727-57- 1899.

Part: BOTTLE PIN — CORRODED (RT WING/BODY)

INSPECTION TYPE-D, CORROSION ON FLANGE OF RT WING BODY FITTING BOTTLE PIN RT FWD BOTTLE PIN. REPLACED IAW MM 51-41-00.

Part: FLAP TRACK — CORRODED (TE FLAP)

INSPECTION TYPE-D, NR 4 FLAP TRACK SPOILER SUPPORT PAD HAS CORROSION. REPAIRED IAW UPS EO B727-5740-0651-J SECTIONS 1, 2 AND 9.

Part: BRACKET — CRACKED (NR 1 PYLON)

INSPECTION TYPE-D, SUSPECT CRACK ON CONTROL QUADRANT SUPPORT BRACKET IN L/E OF NR 1 PYLON BRACKET. REPLACED IAW MM 76-12-41.

Part: FLOOR SUPPORT — CORRODED (BS 355)

INSPECTION TYPE-D, RT NWW KEEL FLOOR SUPPORT ANGLE FOUND CORRODED BS 355. REPAIRED FLOOR SUPPORT IAW SRM 51-40-4 FIG 1.

Part: FLAP TRACK — CORRODED (TE FLAPS)

INSPECTION TYPE-D, NR 3 FLAP TRACK CORROSION IN ATTACH HOLES C, D, E, F, G BUSHINGS INSTALLED IAW OHM 57-40-01.

Part: WEB — CRACKED (NLG WW)

INSPECTION TYPE-D, DUE TO MULTIPLE PREVIOUS REPAIRS AS WELL AS ADDITIONAL CONFIRMED CRACKES REPLACE RT NWW WEB. PRESSURE WEB REPLACED IAW BOEING DRG 65-18414.

Part: HINGE FITTING — CRACKED (LT AILERON)

INSPECTION TYPE-D, LT O/B AILERON SECOND HINGE FITTING FROM O/B AT WS 725.50 IS CRACKED. REPLACED HINGE FITTING IAW DRG NR 65-19276.

Part: BLKHD STIFFNER — CHAFED (BS 1183)

INSPECTION TYPE-D, HYD LINE FROM A-SYSTEM MODULE HAS CHAFED REAR PRESSURE BULKHEAD BS 1183 HORIZONTAL STIFFENER AT WL 208 LBL 30 APPROX. REPAIRED IAW SRS EO 97-34-011 UPS ENG FILE NUMBER 727-53-1974.

Part: SILL — CRACKED (CARGO DOOR)

INSPECTION TYPE-N/A, .375 INCH CRACK AFT EDGE OF SILL PLATE, FWD LOWER CARGO DOOR. REMOVED SILL PLATE FOR WELD AND REINSTALLED SILL PLATE, THIS CLEARS D-132804.

Part: SILL — CRACKED (CARGO DOOR)

INSPECTION TYPE-N/A, .375 INCH CRACK FWD EDGE OF SILL PLATE FWD LOWER CARGO DOOR. REMOVED SILL PLATE FOR WELD AND REINSTALLED SILL PLATE, THIS CLEARS D-132803.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT REMAINS ILLUMINATED WHEN OVERHEAD SWITCH IS IN THE OFF POSITION. REPLACED COCKPIT EMERGENCY EXIT LIGHT PN 10-0067-7 WITH PN 10-0067-9 IAW 33-50-101, TESTS GOOD (S/N 19251) OFF, (S/N 1800) ON.

Part: WEB — CRACKED (BS 940-950)

INSPECTION TYPE-C, LT WHEEL WELL O/B ANGLE BETWEEN 940 AND 950 FITTINGS AT STR 18A IS CRACKED IN TWO PLACES. REMOVED STR 18A SILL WEB, FAB'D AND INSTALLED NEW WEB PER SRM 51-10-1, 51-30-2 AND DWG 65-22419.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, FS 740 BETWEEN STR 19R TO 20R FITTING WAS CRACKED BEYOND STOP DRILL. REPAIRED BS 740 RT FITTING PER EO B727-5310-8420-A

Part: ANGLE — CRACKED (NR 2 LE FLAP)

INSPECTION TYPE-C, LT WING NR 2 SLAT, RIB TO RIB ATTACH ANGLE HAS 5 INCH CRACK AT O/B HOOK. REMOVED ANGLE, FAB'D REPLACE ANGLE AND INSTALLED IAW SRM 57-50-2, 51-30-2.

Part: MOUNT ANGLE — CRACKED (NR 4 LE FLAP ACT)

INSPECTION TYPE-C, LT WING NR 4 SLAT ACTUATOR ROD END MOUNT ANGLE O/B AND I/B SIDES ARE CRACKED. REMOVED CRACKED FLANGE FROM I/B AND O/B RIBS, FAB'D AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING ANGLE FOR PANEL 8107 CRACKED. REMOVED FAB'D AND INSTALLED ANGLE PER BOEING DWG NR 65-19275 AND 51-30-2.

Part: CLIP — CRACKED (BS 970-990)

INSPECTION TYPE-C, MAIN CABIN AT STR 8L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (FUSELAGE)

INSPECTION TYPE-C, MAIN CABIN AT STR 7L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 1010, 1030, 1050. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (FUSELAGE)

INSPECTION TYPE-C, MAIN CABIN AT STR 9L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990, 1010, 1030. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (BS 970-1010)

INSPECTION TYPE-C, MAIN CABIN AT STR 6R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 1010. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: SKIN — CORRODED (BS 360)

INSPECTION TYPE-C, STA 360 BELOW SKIN LAP STR 19R TO 20R IS BEYOND ALLOWABLE LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, 51-10-2.

Part: ANGLE — CRACKED (BS 940-950)

INSPECTION TYPE-C, LT WHEEL WELL O/B ANGLE BETWEEN 940 AND 950 FITTINGS AT STR 18A IS CRACKED. FAB'D AND INSTALLED NEW CHORD ANGLE IAW SRM 53-10-02 AND 51-30-2.

Part: FRAME — CRACKED (BS 328)

INSPECTION TYPE-C, FRAME WEB CRACKED FS 328 STR 28L. STOP DRILLED CRACK PER SRM 51-40-2, NDT INSP FAB'D AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2 AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 620)

INSPECTION TYPE-C, FS 620 STR 26L HAS HEAVY CORROSION. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-30-2.

Part: CLIP — CRACKED (FUSELAGE)

INSPECTION TYPE-C, MAIN CABIN AT STR 7R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 1010, 1030, 1070. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (BS 970-990)

INSPECTION TYPE-C, MAIN CABIN AT STR 9R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 990. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (FUSELAGE)

INSPECTION TYPE-C, MAIN CABIN AT STR 8R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990, 1030 AND 1050. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: CLIP — CRACKED (FUSELAGE)

INSPECTION TYPE-C, FRAME TIE CLIPS CRACKED AT STR 6L, STATIONS 970, 990, 1010 AND 1030. REMOVED THE DAMAGED CLIPS, FAB'D REPLACEMENT PARTS AND INSTALLED PER SRM 51-10-1, 51-30-2 AND 53-10-2.

Part: CLIP — CRACKED (BS 1010-1050)

INSPECTION TYPE-C, MAIN CABIN AT STR 5L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 1010, 1050. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1.

Part: STRINGER — CORRODED (BS 600)

INSPECTION TYPE-C, HEAVY CORROSION ON STR 26L AT STA 600. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-30-2.

Part: SHEAR TIE — CRACKED (BS 328)

INSPECTION TYPE-C, SHEAR TIE CRACKED AT BS 328 AT NOSE LOWER LOBE AREA STR 28L. FAB'D SHEAR TIE AND INSTALLED PER SRM 51-40-02 AND SRM 51-30-2.

Part: RIB — CRACKED (NR 4 LE FLAP)

INSPECTION TYPE-C, LT WING, NR 4 SLAT L/E RIB IS CRACKED AT BOTTOM 8 INCHES I/B OF O/B END. REMOVED DAMAGED AREA PER SRM 57-50-3, FIG 9, FAB AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9.

Part: CARGO TRACK — CORRODED (BS 517)

INSPECTION TYPE-C, CORROSION ON LEFT CARGO TRACK, STA 517 LWR CARGO COMPT. REMOVED AND REPLACED TRACK PER SRM 51-30-2 (P/N 65-23410-4).

Part: ANGLE — CRACKED (WS 127)

INSPECTION TYPE-C, RT WING L/E RIB TO SPAR ANGLE WS 127 CRACKED. REMOVED, FAB'D AND INSTALLED ANGLE PER SRM 57-10-2, 57-10-3, 51-30-2, 51-10-2 AND DRAWING 69-20117.

Part: STRINGER — CRACKED (BS 1333)

INSPECTION TYPE-C, BS 1333 STR 16L IS CRACKED AT THE PRESS RELIEF DOOR. REPAIRED IAW SRM 53-10-3 AND 51-30-2.

Part: LIGHT — INOPERATIVE (COCKPIT)

MAINTENANCE REPORTED, COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM 33-50-101.

Part: INDICATOR — INOP (MAIN GEAR)

PILOT REPORTED RIGHT MAIN GEAR DOWN AND LOCKED GREEN INDICATING LIGHT DID NOT COME ON AFTER GEAR EXTENDED. CHECKED LIGHT BULBS AFTER RECYCLING GEAR, AND FOUND BOTH NOT WORKING. REPLACED ONE BULB AND INDICATOR WORKED. MAINTENANCE REPLACED BOTH BULBS, AND R-13 (RIGHT MAIN GEAR DOWNLOCK DELAY) AS A PRECAUTION. PINNED AND CYCLED GEAR SEVERAL TIMES. CHECKS OK AS PER MM 32-61-21.

Part: CHANNEL — CORRODED (BS 1343)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL STA 1343 LT SIDE. REPLACED PER UPS EO B727-5530-4601.

Part: UPPER CHORD — CRACKED (BL 760.95)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON UPPER CHORD, LT WING BL 760.95. INSTALLED REPAIR PER UPS EO B727-5710-1271E.

Part: CENTER CHANNEL — CORRODED (BS 1343)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL STA 1343. REPLACED PER UPS EO B727-5530-4601.

Part: CHANNEL — CORRODED (BS 1342)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL, BS 1342 RT. REPLACED PER UPS EO B727-5530-4601.

Part: RIB — CORRODED (LT WING)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT WING RIB UPPER CHORD AT LBL 70.5 TEE CLIP AND STRAP. INSTALLED REPAIR UPS EO B727-5710-1271.

Part: FITTING — CRACKED (BS 940)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FRAME FITTING AT THE FLOOR BEAM ATTACH FLANGE, BS 940, LT FWD SIDE. INSTALLED REPAIR PER UPS EO B727-5310-5596A.

Part: CHORD — CORRODED (BS 1343)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD, LT SIDE, BS 1343. REPLACED PER UPS EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1343)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD FTG, RT SIDE, BS 1343. REPLACED PER UPS EO B727-5530-4601.

Part: RING CHORD — CORRODED (NR 2 ENGINE)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RING CHORD ON NR 2 ENGINE AT BS 1352, AT EXISTING REPAIR. REPLACED PER UPS EO B727-7100-2729C.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, LWR OUTER CHORD, LT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, INNER UPPER CHORD, RT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, INNER UPPER CHORD, LT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, LWR OUTER CHORD, RT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601.

Part: EEL — INOP (FLIGHT DECK)

MAINTENANCE REPORTED FWD ENTRY DOOR EMER LIGHT INOP. REMOVED EMER LIGHT UNIT. REPLACED WITH SERVICEABLE UNIT, BATT CHARGE DATE 8-94. OPS CHECK OK. PER AMM 33-40.