N905UP

Part: MOTOR — INOPERATIVE (TE FLAPS) · airframe 14,664 hrs · 9,012 cycles

FLAPS FAILED TO EXTEND WHILE ON APPROACH INTO KEGE. DIVERTED TO KDEN FOR LANDING. EMERGENCY DECLARED. MAINTENANCE REPLACED A FAULTY FLAP PDU (POWER DRIVE UNIT). OPS CHECKS OK. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (NR 3 ENG FUEL)

NR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED.

Part: PRESSURE PANEL — CRACKED (NOSE WHEEL WELL) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW AFT PRESSURE PANEL DAMAGED AREAS REPAIRED IAW SRM51-40-2 FIG 1

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTOUT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A DEFECT FREE CONDITION, AREA REPAIR IAW SRM 51-40-2 F IG 1.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-02 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED OUT SRM 51-40-02 FIG 1.

Part: BOLT — CRACKED (MLG TRUNNION) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FOUND SHEARED. ON REMOVAL OF LT MLG, AFT BEARING MOUNTING JOURNAL FOUND CRACKED & PIECE BROKEN OFF. END OF JOURNAL.BEARING RETAINING BOLT SHEARED & SLIGHT DAMAGED TO BEARING. REF NRC 609755 FOR AFT TRUNNION BEARING REPLACEMENT. REF TC 1249 FOR LT MLG REPLACEMENT & SMRO EO 2002-061-007U PS. UPS ENGINEERING FILE NO. 727-54-20021

Part: PRESSURE PANEL — CRACKED (NOSE WHEEL WELL.) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA CUT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CUTOUT NDF, REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1

Part: FITTING — CRACKED (BS910) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B

Part: FITTING — CRACKED (BS 910) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B

Part: PIN — CORRODED (HORIZ STAB) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01.

Part: SPAR — CRACKED (RT TE FLAP) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FASTENER HOLE. REPAIRED PER EO.B727-5750-3582.

Part: INTERCOSTAL — CRACKED (VERT BEAM 17.8) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65-16350 S HEET 6 & 65C15764 SH. 5 & SRM 51-30-2

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF IAW EO B727-5310-11743. REPAIR ANGLES INSTALLED WET WITH SEALANT IAW EO B727-5310-11743 REPAIR COMPLETED ON EO B727-5310-11743

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,653 hrs · 43,468 cycles

INSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956

Part: RELAY — FAILED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. REMOVED R70 RELAY. OPS CHECKS GOOD.

Part: STIFFENER — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT MLG ACT BEAM SUPPORT PANEL PER B727 SRM 51-40-3

Part: SLIDE — INOPERATIVE (CABIN)

INSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25-60-14.

Part: PANEL — CRACKED (RT WING) · airframe 43,132 hrs · 42,979 cycles

INSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANEL. REPAIRED PER SRM 51-40-2.

Part: SKIN — CRACKED (SPOILER) · airframe 47,122 hrs · 42,975 cycles

INSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IAW SRM.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOOD AS PER 33-50.

Part: SKIN — CRACKED (LE FLAP)

INSPECTION TYPE:C FOUND R/H OUTBRD FOREFLAP WITH A 3/8 INCH CRACK AT HINGE CUTOUT. REPLACED R/H OUTBRD FOREFLAP IAW M/M 27-51-11. OK PER SAME

Part: DOUBLER — CRACKED (WS 340)

INSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. STOP DRILLED CRACK PER SRM 51-10-1 PG 6B.

Part: RIB — CRACKED (NR 4 SLAT ACT)

INSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CRACKED. REPLACED RIBS IAW SRM AND DRAWING 657276, REINSTALLED NR 4 SLAT EYE BOLT IAW MM 27-81-32.

Part: BOTTLE PIN — CORRODED (BS 870)

INSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.

Part: STRINGER — CRACKED (BS 380)

INSPECTION TYPE-D, S21L HAS CRACK AT FASTENER HOLE AT STATION 380. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.

Part: RIB — CRACKED (BS 656.5)

INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727-5710-0314.

Part: STRINGER — CRACKED (BS 420)

INSPECTION TYPE-D, CRACK AT FASTENER HOLE OF STRINGER 21R AT STATION 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1, DETAIL 2.

Part: STRINGER — CRACKED (BS 380)

INSPECTION TYPE-D, SUSPECT CRACK ON S22R FASTENER HOLE ST STA 380. REPAIRED CRACK IAW SRM 51-10-3 FIG 2.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE-D, CRACK IN FASTENER HOLE AND FASTENER MISSING ON S21R AT BS 400. REPAIRED CRACK IAW SRM 51-10-3, FIG 2.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE-D, STRINGER 23L AT STATION 400 CRACKED AT FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1.

Part: STRINGER — CRACKED (BS 440)

INSPECTION TYPE:D SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.

Part: RIB — CRACKED (WS 656.5)

INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314 FIG 13.

Part: STRINGER — CORRODED (BS 260-277)

INSPECTION TYPE:D STRINGER ON TOP OF NOSE WHEEEL WELL AT BL 0, BS 260 TO 277 IS CORRODED. STRINGER SECTION REPAIRED IAW SRM 53-10-3.

Part: STRINGER — CRACKED (BS 440)

INSPECTION TYPE:D, SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2.

Part: STRINGER — BROKEN (BS 420)

INSPECTION TYPE-D, STRINGER 23R BROKEN AT STA 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1 DETAIL 2.

Part: FRAME — CRACKED (BS 420)

INSPECTION TYPE:D CRACK ON UPPER FLANGE OF FRAME AT BS 420, BL 0. REPAIR CARRIED OUT ON UPPER FLANGE IAW SRM 51-40-3, FIG 1.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE-D, SLIDING FAIRING 2ND AFT FRAME HAS A CRACK AT THE UPPER SLIDING TRACK ATTACH POINT. CRACK STOP DRILLED PER SRM 51-10-1, REPAIRED FRAME IAW SRM 51-40-3 FIG 1.

Part: STRAP — CRACKED (WINDOW POST)

INSPECTION TYPE:D ON ACCOMPLISHMENT OF EDDY CURRENT INSPECTION OF RT E-F WINDOW POST PER EO B727-5310-0012, CRACKS FOUND ON 3 HOLES COMMON TO REPAIR STRAP. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-24-012, REF UPS ENGINEERING FILE NUMBER 727-5310-2066.

Part: FITTING — CORRODED (BS 360-380)

INSPECTION TYPE:D, 9G BARRIER NET ATTACH FITTING ON FLOOR LBL 20 BETWEEN BS 360-380 HAS SEVERE CORROSION. 9G FITTING AT LBL 20 REPLACED IAW SRM 51-30-02.

Part: WEB — CORRODED (BS 830)

INSPECTION TYPE:D, COROSION ON WEB RBL 10 BS 830 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: TRACK — CRACKED (BS 1010)

INSPECTION TYPE-D, CARGO TRACK SECTION BS 1010 RT SIDE HAS SIZEABLE CRACK. RT FWD TRACK REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 1180)

INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND CUSP ANGLE BS 1180 STR 17R. CORRODED SKIN AT BS 1180 STR 17R REPAIRED PER SRS EO 98-24-006 REF UPS ENGINEERING FILE NR 727-53-2063.

Part: CLIP — CRACKED (CENTER WING)

INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333.

Part: CLIP — CRACKED (CENTER WING)

INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333.

Part: WEB — CRACKED (BS 885)

INSPECTION TYPE-D, CRACK ON VERTICAL WEB ABOVE KEEL BEAM RBL BS 885 APPROX. VERTICAL WEB ABOVE KEEL BEAM REPAIRED IAW SRM 51-40-02.

Part: SPINDLE — CORROSION (TE FLAP TRACK)

INSPECTION TYPE-D, SURFACE CORROSION IN BORE OF SPINDLE OF NR 3 FLAP TRACK CARRIAGE. FLAP TRACK CARRIAGE REPLACED REF OHM 57-58-11.

Part: WEB — CRACKED (NR 1 TR UNIT)

INSPECTION TYPE:D, ENGINE NR 1 THRUST REV AFT VERTICAL WEB SUSPECT CRACK AT 12 O'CLOCK POSITION AT HYD PIPE BRACKET ATTACH. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: BOLT — CORRODED (WS 224.5)

INSPECTION TYPE-D, NR 5 FLAP TRACK ATTACH BOLT CORRODED. BOLT CHANGED IAW MM 27-51-31.

Part: ANGLE — CORRODED (BS 740)

INSPECTION TYPE-D, CHORD ANGLE AT BS 740 LT (P/N 65-15940-24) HAS CORROSION ON O/B SECTION. CHORD REPAIRED IAW DRAWING 65C13724 AND SRS ENGINEERING ORDER 98-24- 004, REF UPS ENGINEERING FILE NUMBER 727-53-2064.

Part: BRACKET — CORRODED (BS 745)

INSPECTION TYPE-D, CORROSION ON BRACKET STIFFENER AT LBS 745 APPROX STR 24 POSITION WL 167.5. REPLACED BRACKET IAW DRAWING 64-08333.

Part: BARRELL NUT — CORRODED (NR 1 FLAP TRACK)

INSPECTION TYPE-D, NR 1 FLAP TRACK BARRELL NUT CORRODED AND WASHER UNDER HEAD OF ATTACH BOLT CORRODED. BARRELL NUT AND WASHER CHANGED PER MM.

Part: FRAME — CRACKED (BS 560)

INSPECTION TYPE:D SUSPECT CRACK IN OUTER FLANGE OF FRAME 560 RT. FLANGE REPAIRED IN IAW SRM 53-10-4, FIG 11.

Part: PANELS — CORRODED (LT WING)

INSPECTION TYPE-D, LT WING NR 18 TANK ACCESS PANEL BOLT ON TYPE SEAL GROOVE CORRODED, ALSO NR 17 AND NR 19. PANELS REPLACED, THEN CLOSED PER TC C57-571-01-1D.

Part: BOLT — CORRODED (NR 2 FLAP TRACK)

INSPECTION TYPE-D, NR 2 FLAP TRACK ATTACH BOLT AND BARRELL NUT CORRODED. BOLT AND BARRELL NUT REPLACED PER MM27-51-31.

Part: BOLT — CORRODED (NR 4 FLAP TRACK)

INSPECTION TYPE-D, NR 4 FLAP TRACK ATTACH BOLTS AND NUT CORRODED. NUT AND BOLTS REPLACED IAW MM 20-80-01.

Part: CLAMP RING — CORRODED (WS 185)

INSPECTION TYPE-D, NR 2 TANK ACCESS PANEL RT WING SHOWING EVIDENCE OF FRETTING CORROSION ON CLAMP RING. CLAMP RING REPLACED PER TC NR C57-571-01-2D.

Part: PANEL — CORRODED (WS 70)

INSPECTION TYPE:D LT WING TANK FROMT SPAR ACCESS PANEL NR 1 CORRODED. PANEL REPLACED IAW MM 28-11-21.

Part: STRINGER — DENTED (BS 560-580)

INSPECTION TYPE-D, BS 560 TO 580 LT STR 20 HAS DENT IN FUSELAGE. REPAIR CARRIED OUT IAW EO 98-24-003 UPS ENGINEERING FILE NR 727-53 -2060.

Part: SKIN — CRACKED (PAX DOOR)

INSPECTION TYPE:D, CRACK ON FWD ENTRY DOOR SKIN .25 EITHER SIDE OF RIVET AT BS 344 STR 9. REPAIR CARRIED OUT IAW SRS EO 98-24-007 UPS ENGINEERING FILE NO 727- 52-0195.

Part: STIFFENER — CORROSION (BS 750)

INSPECTION TYPE-D, LIGHT SURFACE CORROSION AT BS 750 APPROX LT SIDE WL 1675 APPROX AT STR 27 POSITIONS. REPLACED STIFFENER IAW DRW 64-08333.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-D, AFT CARGO DOOR LOWER FORWARD FRAME CRACKED. FRAME REPLACED IAW DRAWING 65C16422.

Part: BOTTLE PIN — CORROSION (BS 740)

INSPECTION TYPE-D, RT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.

Part: SPAR — CORRODED (LT WING)

INSPECTION TYPE-D, CORROSION ON LT WING CENTER SECTION FRONT SPAR LOWER CHORD AT APPROX LBL 100. REPLACED FRONT LOWER CENTER TANK CHORD IAW DRAWING 64-8333.

Part: BOTTLE PIN — CORRODED (BS 740)

INSPECTION TYPE:D, LT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00.

Part: PANELS — CORRODED (WS 519-656.5)

INSPECTION TYPE-D, CORROSION IN SEAL RECESS ON RT WING FUEL TANK BOLT ON ACCESS DOORS NR 15, 16, 17, 18 AND 19. PANELS REPLACED AND THEN CLOSED PER TC C57-571-01-2D.

Part: BRACKETS — CRACKED (NR 3 ENG TR)

INSPECTION TYPE-D, ENGINE NR 3 THRUST REV FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. BRACKETS REPLACED IAW MM 78-30-00.

Part: PANEL — CORRODED (WS 70)

INSPECTION TYPE-D, NR 1 FRONT SPAR TANK ACCESS PANEL CORRODED, RT WING. REFER TO TC C57-571-01-2D FOR ACCESS PANEL AND CLAMP RING REPLACEMENT/INSTALLATION.

Part: TRACK — CORRODED (NR 6 FLAP TRACK)

INSPECTION TYPE-D, PITTING CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AT ATTACH POINT TO AUXILIARY SPAR. SHIM MANUFACTURED AND INSTALLED PER SRS ENGINEERING ORDER 98-24-009 REF UPS ENGINEERING FILE NUMBER 727-57-2000.

Part: SKIN — CRACKED (BS 243.7)

INSPECTION TYPE-D, CRACK AT RT BS 243.7 WL 226 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3.

Part: SKIN — CRACKED (BS 203.8)

INSPECTION TYPE-D, CRACK LOCATED AT RT BS 203.8 WL 222 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3.

Part: BULKHEAD — CRACKED (BS 178)

INSPECTION TYPE-D, SUSPECT CRACKS ON FWD FACE OF B/H 178 WL 204 APPROX. DEFECT REPAIRED IAW DRW 65C36289 USING EO B727-5310-4290.

Part: SKIN — CRACKED (BS 243.7)

INSPECTION TYPE-D, CRACK LOCATED AT LT BS 243.7 WL 220 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3.

Part: PUSH ROD — CORROSION (LT AILERON)

INSPECTION TYPE-D, CORROSION ON LT O/B AILERON PUSH ROD ATTACH LUG. REPLACED PUSH ROD ATTACH WG CASTING IAW DRAWING NR 65-21766.

Part: TRACK — CORRODED (NR 3 FLAP TRACK)

INSPECTION TYPE-D, PITTING CORROSION ON UPPER SURFACE OF NR 3 FLAP TRACK AT ATTACH POINT TO AUXILIARY SPAR. SHIM FABRICATED AND INSTALLED IAW SRS 98-24-008, REF UPS ENGINEERING FILE NUMBER 727-57-2001.

Part: FRAME — CRACKED (BS 600)

INSPECTION TYPE-D, SUSPECT CRACK IN FRAME 600 JUST ABOVE STR 18 RT. REPAIRED CRACK AT STATION 600, STR 18 RT IAW SRM 53-10-4.

Part: SKIN — CRACKED (WING)

INSPECTION TYPE-D, SUSPECT CRACK IN UPPER T/E SKIN PANEL ADJACENT TO NR 5 SPOILER PANEL O/B HINGE CUTOUT. REPAIR CARRIED OUT IAW SRM 57-30-04 FIG 10.

Part: SKIN — CRACKED (NR 8 LE SLAT)

INSPECTION TYPE:D, CRACKS AT NR 8 SLAT UPPER SIDE AT AFT I/B HOOK ATTACH HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3.

Part: SKIN — CRACKED (BS 235.8)

INSPECTION TYPE-D, CRACK AT RT BS 235.8 WL 222 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3.

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE-D, AFT CARGO DOOR NUMBER ONE FITTING CRACKED (NR 1 FWD FITTING). NEW FITTING INSTALLED IAW DRAWING 65C18422.

Part: FIREWALL WEB — CRACKED (BS 1387.85)

INSPECTION TYPE:D, WEB AT BS 1387.85 LT OVER NR 2 HORIZONTAL FIREWALL IS CRACKED. NEW WEB FABRICATED AND INSTALLED IAW DRAWING NR 65-17555.

Part: RIB — CRACKED (NR 2 LE SLAT)

INSPECTION TYPE:D, NR 2 LE SLAT RIB CRACKED ADJACENT TO ANTI-ICE DUCT (TELESCOPIC). NR 2 SLAT RIB REPAIRED IAW SRM 51-40-2.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE-D, REPLACE RT BS 870 TERMINAL FITTING. FITTING REPLACED IAW UPS EO B727-5310-3056 AND DRAWING 65C23231.

Part: MOUNT — WORN (NR 2 LE SLAT ACT)

INSPECTION TYPE-D, NR 2 LE SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. REPLACED MOUNTING IAW SRM 51-30-02.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE-D, REPLACE LT BS 870 TERMINAL FITTING. FITTING REPLACED IAW UPS EO B727-5310-3056 AND DRAWING 65C23231.

Part: FITTING — CRACKED (BS 870)

INSPECTION TYPE-D, CRACKS FOUND ON BS 870 TERMINAL FITTING LT AND RT. BOTH BS 870 LT AND RT TERMINAL FITTINGS REPLACED.

Part: MOUNTING — WORN (NR 2 LE SLAT ACT)

INSPECTION TYPE:D NR 2 L/E SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. MOUNTING REPLACED IAW EO B727-5720-1058.

Part: BOTTLE PIN — CORRODED (BS 870)

INSPECTION TYPE:D RT BS 750 REAR SPAR BOTTLE PIN FOUND CORRODED (PITTING CORROSION). PIN REPLACED IAW WITH MM 57-41-00.

Part: LIGHT — FLASHES (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT FLASHES INTERMITTENTLY IN FLIGHT. INSPECTED WIRING AT CONTROL SWITCH, INSPECTED CONNECTORS TO LIGHT AS SYS, SIMULATED TURBULENCE TO VERIFY INTEGRITY, COULD NOT DUPLICATE PROBLEM. SYSTEM CKS NORMAL.

Part: LIGHTS — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT FLASHES INTERMITTENTLY IN FLIGHT. INSPECTED WIRING FOR CONTROL SWITCH, CKS OK. INSPECTED CONNECTORS TO LIGHT ASSYS, CHKS OK. CK'D INTEGRITY OF UNITS DURING SIMULATED TURBULENCE, NO PROBLEMS FOUND. COULD NOT DUPLICATE PROBLEM. EMERGENCY LIGHT SYSTEM OPS CKS NORMAL.

Part: ANGLE — CORRODED (BS 740)

INSPECTION TYPE-C, CORROSION FOUND ON BS 740 LOWER FRAME LOWER CHORD ANGLE BETWEEN S23R AND S24R. LOWER CHORD REPAIR CARRIED OUT IAW UPS MAJOR REPAIR AUTHORIZATION FILE NR 727-53-1875.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, REPLACE BS 740 FITTING RT DUE TO CRACKED BEYOND LIMITS. BS 740 RT TERMINAL FITTING REPLACED IAW EO B727-5310-7477 USING KIT NR 65C13724-96.

Part: DOOR FRAME — CRACKED (GALLEY DOOR)

INSPECTION TYPE-C, CRACKS ON MID GALLEY DOOR FRAME AT FWD UPPER CORNER. MID GALLEY DOOR FRAME SECTION REPLACED PER SRM 51-30-2 AND IN CONJUNCTION WITH EO B727-5330-2639 REF NRC 513079.

Part: SKIN — CORRODED (BS 364)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 364 BETWEEN S6 AND 7 LT. AREA REPAIRED IAW EO B727-5310-1371 APP 8.5.

Part: SKIN — CORRODED (BS 1090)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 BETWEEN S14R AND S12R. CORRODED / DISBONDED AREA OF INTERNAL DOUBLER REMOVED. CORRODED AREA OF SKIN REMOVED PER SRM 51-10-6. HFEC CARRIED OUT IAW NDT PT6 51-00 -00 FIG 4, NO DEFECTS INDICATED. AREA REPAIRED PER UPS MAJOR REPAIR AUTHORIZATION FILE NR 727-53-1869.

Part: SEAT TRACK — CRACKED (BS 760)

INSPECTION TYPE-C, CRACK ON FLANGE OF SEAT TRACK AT BS 760 RBL 45.5. SEAT TRACK REPLACED IAW SRM 51-30-2.

Part: BRACKET — CRACKED (BS 360)

INSPECTION TYPE-C, 9G NET ATTACH FITTING AT S10L TO S9L FOUND TO BE SEPARATED FROM ATTACH CHANNEL PART NR 69-35276-3. ATTACHMENT BRACKET P/N 66-20231-3 REPLACED IAW MM 25-56-201.

Part: FLOORBEAM — CORRODED (BS 930)

INSPECTION TYPE-C, CORROSION ON UNDERSIDE OF FLOORBEAM STN 930 RBL 55.5. HFEC CARRIED OUT IAW NDT PT6 51-00-00 FIG 4, NO DEFECTS INDICATED. REPAIR CARRIED OUT PER UPS MINOR REPAIR AUTHORIZATION FILE NR 727-53- 1870.

Part: BEAM — CRACKED (BS 1183)

INSPECTION TYPE-C, CRACKS FOUND AT BS 1183 LBL 36.83 VERTICAL BEAM BETWEEN WL 233 AND WL 253. TWO CRACKS 1 INCH LONG EITHER SIDE OF VERTICAL BEAM 'T' ANGLE AT WL 238. REPAIR CARRIED OUT IAW EO B727-5311-0631 APP C.

Part: SKIN — GOUGE (BS 515)

INSPECTION TYPE-C, GOUGE IN FUSELAGE SKIN BS 515 BETWEEN S21R AND S22R. REPAIR CARRIED OUT IAW UPS MINOR REPAIR AUTHORIZATION FILE NR 727-53 -1868.

Part: HINGE — CORRODED (CARGO DOOR)

INSPECTION TYPE-C, FWD AND AFT HINGE HALFS OF MAIN CARGO DOOR ARE CORRODED AND OUTSIDE LIMITS. FWD DOOR HINGE REPLACED IAW OHM 52-36-61. AFT HINGE DRESSED OT AND FOUND WITHIN LIMITS PER OHM 52-36-62.

Part: DOWNLOCK SWITCH — INOPERATIVE (RT MAIN GEAR)

INSPECTION TYPE-N/A, UNSAFE INDICATION RT MAIN GEAR. MANUAL GEAR EXTENSION CHKLIST ACCOMPLISHED, NO SAFE INDICATION. TOWER FLY-BY FOR POSSIBLE STATUS OF GEAR. DECLARED EMERGENCY REQUESTED CRASH CREWS. REMOVED AND REPLACED RT MAIN GEAR DOWNLOCK SWITCH IAW MM32-61-21, PERFORMED ADJ AND TEST IAW MM 32-61-21 AND OPS CHK GOOD.

Part: TE WEDGE — DELAMINATED (TE MID FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE HAS ONE DELAMINATION ON UPPER SURFACE 23 INCHES FROM INBOARD END. CUT OUT DAMAGE AREA, APPLIED FIBERGLASS, AND COMPLETED REPAIRS PER SRM 51-40-6, MM 51-20-151.

Part: BULLNOSE — CRACKED (NR 5 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP BULLNOSE CRACKED AT OUTBOARD LUG ATTACH POINT, INBOARD FASTENERS HOLES. REMOVED CRACKED BULLNOSE AND INSTALLED NEW BULLNOSE PER SRM 51-30-2, 51-30-8, M.M. 27-81-00.

Part: SKIN — CRACKED (LT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEADING EDGE INBOARD AFT FLAP, INBOARD CENTER TRACK CUT-OUT IS CRACKED. CONTAINED CRACK BY STOP DRILLING AND VERIFIED BY NDI. FABRICATED REPAIR PARTS AND INSTALLED. WORK DONE I/A/W SRM 57-50-4, 51-30-2.

Part: BONDING JUMPER — CORRODED (NR 2 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP OUTBOARD BONDING JUMPER UPPER ATTACH POINT IS PITTED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-50-1, CUT OUT DAMAGE AND REPAIRED PER SRM 57-50-3.

Part: STRINGER — CORRODED (BS 360)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 20 PERCENT MATERIAL LOSS AT BS 360, 3 INCHES TO THE RIGHT ON STR 1 MARKED BY NDI. REPAIRED PER E.O. B727-5310-1371E, SRM'S 51-10-2, 51-30-8, 51-20-4, AND 51-30-2.

Part: HAT CHANNEL — CORRODED (BS 344)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON PANEL SUPPORT AT FORWARD LAV STA 344, RBL 18, WL 208-UNDERSIDE. REMOVED AND INSTALLED NEW FABRICATED HAT CHANNEL. WORK DONE I/A/W SRM'S 53-10-1, 51-30-2.

Part: SKIN — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK INDICATION NOTED LT WINDSHIELD, UPPER SILL, LOWER AFT RIVET APPROX 8 O'CLOCK POSITION. CUT OUT DAMAGE AND REPAIRED PER SRM 53-30-3.

Part: FITTING — CORRODED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 HINGE BEARING BLOCK ON LT WING, OUTBOARD AILERON TO BE WORN AND HAVE EXCESSIVE PLAY, BACK AND FORTH, SIDE TO SIDE. (NOTE UPON REMOVAL OF BEARING BLOCK FOUND FITTING CORRODED). REMOVED AND INSTALLED NEW FITTING. WORK DONE I/A/W SRM'S 51-30-2, 51-30-5.

Part: LOWER CHORD — CRACKED (TE MID FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBOARD MID-FLAP, INBOARD AFT FLAP ACTUATING CUT-OUT LOWER CHORD IS CRACKED. REMOVED AND INSTALLED NEW FABRICATED PARTS. WORK DONE I/A/W SRM 51-30-2, 51-40-4.

Part: SKIN — DELAMINATED (NR 1 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 1 SPOILER HAS 2 AREAS OF DELAMINATION ON LOWER SURFACE AT THE INBOARD FORWARD CORNER AND ON THE OUTBOARD EDGE OF THE CENTER FITTING. REMOVED DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 57-50-1, 51-40-6.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMER EXIT LIGHTS INOP. REPLACED BATTERY PACK. OPS CK OK.