N928UP

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A.

Part: CONTROL ROD — LACK OF LUBE (WING AILERON)

INSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPUT ROD REMOVED AND REINSTALLED ON SPOILER MIXER FOR T/S NO CHANGE

Part: PITOT TUBE — DAMAGED (FIRST OFFICERS)

INSPECTION TYPE:IN AT FL 33.0 CAPTS ALT 33,000 FT F/OS ALT 32820 FT CAPTS A/S 296 KNOTS F/OS A/S 294.5. STANDBY ALT 33,200. TESTED CAPT AND FO ALT PER MM 34-12-05. TESTS GOOD. TESTED CAPT AND FO MACH A/S PER MM 34-12-06. TESTS GOOD F/OS PITOT TUBE DAMAGED BEYOND LIMIT PER MM 34-11-21 P601. REMOVED F/OS PITOT TUBE AND INSTALLED F/OS PITOT TUBE PER MM 34-11-21. VERIFIED PITOT SYSTEM INTEGRITY (F/O) PER 34-11-02.

Part: HEAT EXCHANGER — LEAKING (HYD SYSTEM)

INSPECTION TYPE:C, RT WING HYDRAULIC HEAT EXCHANGER LEAKING HYD FLUID INTO NR 3 TANK. ACCOMPLISHED RIGHT WING HYDRAULIC COOLER ANTI-ROTATION PLATE REPLACEMENT IAW AVITAS ENGINEERING REPAIR ORDER AVHM-187RO-1.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C, LEFT WHEEL WELL CASTING FRAME BS 930 SHOWS CRACK TO LOWER END STR 18L. INSTALLED REPAIR AT BS 930 CASTING FRAME IAW UPS EO B727-5310-2611B.

Part: SKIN — BULGED (CARGO DOOR)

INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGING AT BS 610, STR 4L. INSTALLED DOUBLER REPAIR IAW 52-30-01.

Part: ANGLE — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLACED I/B VERT ANGLE IAW SRM 51-30-2.

Part: SKIN — BULGED (CARGO DOOR)

INSPECTION TYPE:C, MAIN CARGO DOOR OUTER SKIN BULGED AT BS 490, STR 4 LEFT. INSTALLED REPAIR AT MAIN CARGO DOOR SKIN IAW SRM 52-30-01.

Part: ANGLE — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REMOVED AND REPLACED 2 ANGLES IAW SRM 57-10-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREVIOUS REPAIR ABOUT 1 INCH LONG. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 51-40-2.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C, NOSE LANDING GEAR WHEEL WELL TOP CEILING BS 272, LBL 15 SHOWS CRACK RUNNING BETWEEN RIVETS, ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IAW SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C CK, NLG W/W TOP CEILING RBL 15 AND BS 272 CRACK INDICATION ALONG FASTENER ROW ABOUT 2.5 INCHES LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.

Part: SKIN — BULGED (FUSELAGE)

INSPECTION TYPE:C, SKIN BULGING AT STR 2L, STA 441. ACCOMPLISHED REPAIR IAW UPS EO B727-5310-1371E.

Part: SKIN — BULGED (FUSELAGE)

INSPECTION TYPE:C, SKIN BULGING BETWEEN STR 5R AND STR 6R AT STA 481. INSTALLED REPAIR DOUBLER IAW UPS EO B727-5310-1371E.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C CK, NLG W/W LT SIDEWALL BS 243 TO LWR SHOWED CRACK AROUND FASTENER, ABOU T 1 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS272 LWR OF AFT ACCESS DOOR CRACK INDICATION RUNNING BETWEEN FASTENER ROW, 1.5 INCH LONG. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE:C CK, NLG W/W RIGHT SIDEWALL BS 251 AFT OF FWD ACCESS DOOR, CRACK INDICATION ALONG FASTENERS ROW, ABOUT 4.5 INCHES. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 51-40-2.

Part: SKIN — BULGED (FUSELAGE)

INSPECTION TYPE:C, BULGE IN SKIN AT STA 260 LEFT WL 270. REPAIRED PER UPS EO B727-5310-1371E.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW)

INSPECTION TYPE:C CK, LEFT WHEEL WELL STA 913 UPLOCK SUPPORT ASSY, CRACK AT AFT SUPPORT FRAME. CRACK VERIFIED BY NDT. REPAIRED STA 913 SUPPORT FRAME IN ACCORDANCE WITH UPS EO B727-5310- 1896B, KIT INSTALLED. (P/N 65C-27194-25).

Part: SKIN — BULGED (FUSELAGE)

INSPECTION TYPE:C CK, FUSELAGE AFT RIGHT BS 1333 STR 8R TO STR 10R, SKIN BULGE AND FASTENERS PULLING THROUGH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 54-30-3 FIG 7.

Part: LIGHT — INOPERATIVE (COCKPIT)

EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. CANIBALIZED EMERGENCY LIGHT ASSY FROM AIRCRAFT 907 OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN)

INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT ROBBED FOR ACFT 910. INSTALLED FWD ENTRY DOOR EMERGENCY EXIT LIGHT, OPS CHECK GOOD.

Part: SKIN — DELAMINATED (RUDDER TAB)

INSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3.

Part: CLEVIS — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.

Part: DUCT — CRACKED (NR 3 ENGINE)

INSPECTION TYPE:C, ENGINE NR 3 ANTI-ICE DUCT CRACKED AT BRACKET NEAR ANTI-ICE VALVE. DUCT REPAIRED PER SMRO EO 99-17-005 (UPS ENGINEERING FILE NR 727-30- 0009).

Part: WEB — CORRODED (BS 1130-1183)

INSPECTION TYPE:C, CORROSION ON SHEAR WEB LBL 24.75 STA 1130-1183. WEB REPAIRED IAW SRM 51-40-2.

Part: BALANCE PANEL — CORRODED (NR 5 ELEVATOR)

INSPECTION TYPE:C, NR 5 ELEVATOR BALANCE PANEL RT HAS EVIDENCE OF CORROSION ON PANEL TO HINGE ATTACH RACK. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6. BALANCE PANEL REPLACED AND INSTALLED IAW MM 27-30-21.

Part: ANGLE — CRACKED (BS 850)

INSPECTION TYPE:C, FLOOR SUPPORT CRACKED BS 850 LBL 45.5. FLOOR SUPPORT ANGLE REPAIRED IAW SRM 57-20-1.

Part: MOUNT — CORRODED (NR 1 ENGINE)

INSPECTION TYPE:C, CORROSION FOUND ON NR 1 ENG, FWD MOUNT HOLE AFT I/B HOLE ONLY (PITTING CORROSION). INVESTIGATED AND REPAIRED IAW SMRO EO 99-17-002 UPS ENGINEERING FILE NR 727-54-0088.

Part: RIB — CRACKED (NR 6 LE SLAT)

INSPECTION TYPE:C, NR 6 SLAT RIB AT IB SIDE OF ACTUATOR HAS SMALL CRACK IN FWD LOWER RADIUS. RIB REPAIRED IAW SRM 57-50-3.

Part: MOUNT — CORRODED (NR 3 ENGINE)

INSPECTION TYPE:C, CORROSION FOUND ON NR 3 ENG FWD MOUNT HOLES AT TRUNNION FITTING ATTACH (PITTING CORROSION). REPAIRED IAW SRMO EO 99-17-003 (UPS ENGINEERING FILE NR 727-54-0089).

Part: SUPPORT — CORRODED (BS 1140)

INSPECTION TYPE:C, CORROSION FOUND ON AFT LT LAVATORY PARTITION SUPPORT ON FLOOR STRUCTURE BS 1140 LBL 24.75-LBL60. TOP HAT SECTION REPLACED IAW SRM 51-10-1.

Part: FIREWALL WEB — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555.

Part: SUPPORT — CORRODED (BS 1174)

INSPECTION TYPE:C, CORROSION FOUND ON AFT LAVATORY SUPPORT PARTITION FLOOR STRUCTURE BS 1174 LBL 24.75. TOP HAT SECTION REPLACED IAW SRM 51-10-1.

Part: STIFFENER — CRACKED (NR 4 SPOILER)

INSPECTION TYPE:C, NR 4 SPOILER IB ATTACH VERTICAL LEG CRACKED VERTICAL STIFFENER. REPLACED IAW DWG 69-16201.

Part: BRACKET — CRACKED (NR 1 TR UNIT)

INSPECTION TYPE:C, ENGINE NR 1 THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.

Part: BRACKET — CRACKED (NR 3 TR UNIT)

INSPECTION TYPE:C, ENGINE NR 3 THRUST REVERSER FAIRING MID SUPPORT BRACKED CRACKED. BRACKET REPLACED IAW MM 78-30-00.

Part: STRINGER — DAMAGED (BS 420)

INSPECTION TYPE:C, ON REMOVAL OF DENTED SKIN, STRINGER FOUND DAMAGED. REPLACED DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1.

Part: HINGE — CRACKED (AFT CARGO DOOR)

INSPECTION TYPE-N/A, AFT LOWER CARGO DOOR FORWARD HINGE CRACKED OFF DOOR. REPLACED FWD FITTING AND CHECKED GAPS AND CLEARANCES PER M/M 52-31-01, OPS CHECK GOOD (P/N 19667-4) ON, OFF (P/N 6-19667-3A) TAG 21956.

Part: CHORD — CORRODED (BS 880.5)

INSPECTION TYPE-SI, WHILE WORKING CUSTOMER ID 664363 FUSELAGE 136 FOUND CORROSION ON LOWER SURFACE OF LOWER PRESSURE BOX CHORD AT BS 880.5, RBL 65, WL 199. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-6, REPAIRED PER SRM 53-10-8.

Part: ANGLE — CORRODED (BS 259)

INSPECTION TYPE:SI CORROSION (SDN C53-111-01.00-01) ON VERTICAL L ANGLE AT BS 259, LBL 26, WL 155 TO WL 165. CORROSION REMOVAL OUT OF LIMITS, REMOVED DAMAGED L ANGLE, FABRICATED REPAIR PARTS, INSTALLED PER SRM 51-40-4.

Part: STIFFENER — CORRODED (BS 328)

INSPECTION TYPE-SI, CORROSION ON LOWER END OF VERTICAL STIFFENER ON NLG WHEEL WELL BS 328 LBL 15, WL 171. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 303)

INSPECTION TYPE-SI, CRACK ON SIDE OF INTERCOSTAL AT STA 303 LBL 51, WL 261. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1, 53-10-2, 51-10-2, 51-30-5.

Part: SEAT TRACK — CORRODED (BS 870-1130)

INSPECTION TYPE-SI, SEAT TRACK STA 870 TO 1130 RBL 25 HAS AREAS OF CORROSION AND MECHANICAL DAMAGE. REMOVED CORRODED AND MECHANICAL DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPAIR PARTS IAW 53-10-5, 51-30-5, 51-30-8, 51-20-2.

Part: CHORD — CORRODED (BS 334/351)

INSPECTION TYPE-SI, CORROSION ON LOWER NOSE CHORD AROUND NUT PLATES BETWEEN BS 334 AND BS 351 RBL 17. REMOVED AND REPLACED LOWER NOSE CHORD IAW SRM 51-30-2, 51-10-2, 51-20-04, MM 51-20-151.

Part: CHORD — CORRODED (BS 380/328)

INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON NLG WHEEL WELL MID CHORD BS 318 AND BS 328 RBL 15 WL 170. REMOVED CORROSION PART OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-2, 51-20-4, 51-20-151.

Part: CHORD — CORRODED (BS 351)

INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON NLG DOGHOUSE FLOOR SUPPORT CHORD AT BS 351 RBL 30 WL 170 (BELOW FLOOR). REMOVED CORROSION PART OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-21-151, 51-10-2, 51-30-2, 51-20-4 AND 51-30-5.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-SI, FWD CARGO DOOR INBD SIDE OF FRAME CRACKED BELOW UPLATCH HOOK. STOP DRILLED CRACK, FABRICATED REPAIR PARTS, INSTALLED PER SRM 51-30-2.

Part: BULKHEAD — CRACKED (BS 178)

INSPECTION TYPE-SI, CRACK IN BS 178 BULKHEAD RBL 9, WL 232. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-9, 51-30-2.

Part: STIFFENER — CORRODED (BS 255)

INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON HORIZONTAL STIFFENER AT BS 255 RBL 26, WL 165. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 51-10-6.

Part: STRINGER — CRACKED (WS 656)

INSPECTION TYPE-SI, RW CRACK FOUND ON VENT STRINGER 13 FLANGE AT WS 656. ACCOMPLISHED VENT STRINGER REPAIR IAW UPS EO B727-5710-0314.

Part: FRAME — CORRODED (BS 910)

INSPECTION TYPE-SI, WHILE WORKING CUSTOMER CARD 664487 INT 149 FOUND CORROSION AROUND FASTENER HOLES ON FRAME BS 910 LBL 29 WL 297. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 53-10-4, 53-30-2, 51-20-0.

Part: BRACKET — CORRODED (BS 740)

INSPECTION TYPE-SI, CORROSION ON EXPANSION LINK BS 740, RBL 13, WL 165. REMOVED AND REPLACED EXPANSION LINK SRM 51-10-1, 53-10-1, 51-30-2.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION TYPE-SI, CORROSION ON TOP OF FLOORBEAM BS 328 RBL 12 TO 16 WL 208 TASK CARD NR C53-224-03-1B. REPLACED FLOORBEAM DAMAGED SECTION PER SRM 53-10-1 AND 53-10-8.

Part: STIFFENER — CORRODED (BS 255)

INSPECTION TYPE-SI, CORROSION ON HORIZONTAL STIFFENER AT BS 255, LBL 26, WL 165. ACCOMPLISHED EXTRUDED SECTION REPAIR IAW SRM 51-40-4.

Part: FLOORBEAM — CORRODED (BS 420)

INSPECTION TYPE-SI, CORROSION FLOORBEAM BS 420, RBL 45 TO 60, WL 208 OF LOWER SIDE AT UPPER FLANGE. CUT OUT DAMAGED SECTION OF FLANGE AND ACCOMPLISHED REPAIR IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 1110-1130)

INSPECTION TYPE-D, SEAT TRACK STA 1110 TO 1130 RBL 45 HAS CORROSION ON TOP AND BOTTOM OF FLANGES. REMOVED ALL CORROSION AND REMOVED AND REPLACED SEAT TRACK SPLICES IAW SRM 53-10-5 AND 51-10-6.

Part: TRACK — CORRODED (NR 4 TE FLAP)

INSPECTION TYPE-SI, NR 4 FLAP TRACK 2 HOLES AT SPOILER BEAM ATTACH POINT HAVE PITTING CORROSION. REMOVED AND REPLACED TRACK IAW SRM 51-30-2, 51-30-5, 51-10-1.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE-SI, UPON REMOVAL OF THE R/W I/B AILERON FOUND THE CENTER HINGE FITTING AIM CORRODED. REMOVED AND REPLACED IAW OHM 57-50-01 AND MM 27-10-01.

Part: BRACKET — CORRODED (BS 740)

INSPECTION TYPE-SI, CORROSION (C53-132-01.00-02) ON EXPANSION LINK BS 740, LBL 13, WL 165. REMOVED AND REPLACED IAW SRM 51-10-1, 53-10-01, 51-10-01.

Part: SEAT TRACK — CORRODED (BS 340-480)

INSPECTION TYPE-SI, SEAT TRACK STA 340 TO 480 LBL 25 HAS CORROSION ON FLANGES AND A LOOSE BOLT AT STA 580. REMOVED CORROSION AND OUT OF LIMITS IAW SRM 53-10-1 AND REPLACED TRACK IAW SRM 51-30-8, 51-10-2, 51-20-151 MM AND SRM 51-30-2.

Part: FITTING — CORRODED (NR 8 TE FLAP)

INSPECTION TYPE-SI, NR 8 FWD FLAP TRACK FITTING CORRODED AT FLAP TRACK ATTACH LUG. FITTING WAS OUT OF LIMITS PER SRM AND REPLACED WITH NEW IAW SRM 51-30-2 AND OHM 20-50-03.

Part: STRINGER — CORROSION (BS 362)

INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 22, BS 362. REMOVE AND REPLACE PER SRM 53-10-03 AND SRM 51-30-5, MM 51-20-151 AND SRM 53-11-00.

Part: SKIN — CORRODED (BS 697)

INSPECTION TYPE-SI, CORROSION (C53-224-01.00-01) ON SKIN SURFACE BS 697 RBL 17. REPAIRED SKIN IAW SRM 53-30-3 SRM 53-30-2 SRM 51-30-2 SRM 51-10-02.

Part: TRACK — CORRODED (NR 2 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 2 FLAP TRACK FWD ATTACH FITTING MOUNT LUG IS PITTED AND BUSHING IS MIGRATED. REMOVED AND REINSTALLED NEW FWD FITTING IAW SRM 51-30-2 AND OHM 20-50-03.

Part: TRACK — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 3 FLAP TRACK SPOILER BEAM MOUNT PAD CORRODED. REMOVED TRACK AND ROUTED TO MACHINE SHOP AND REWORK TRACK ON FAB NR 47285 AND OHM 57-40-1 AND PO NR IML244734, ILM244733 AND SRM 51-30-2 AND WILL BE REINSTALLED ON TC NR C57-581-04-3D WINGS 104.

Part: FLAP TRACK — CORRODED (NR 2 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 2 FLAP TRACK FRONT MOUNT FORKS HAVE CORROSION ON INNER FACE. REMOVED AND REPLACED IAW SRM 51-30-2, OHM 57-40-1, FAB NR 47282 AND MM 27-51-31.

Part: SKIN — CRACKED (BS 1218)

INSPECTION TYPE-SI, CRACK INDICATION NOTED IN RT 4 SECTION SKIN BS 1218.5, WL 220, AFT ROW MARKED IN RED. REPAIRED IAW SRM 53-30-3.

Part: SKIN — GOUGE (BS 499)

INSPECTION TYPE-SI, GOUGE ON INTERIOR SKIN BS 499, LBL 56, WL 177. REPAIRED GOUGE IAW SRM 53-30-01.

Part: SKIN — CRACKED (BS 235.8)

INSPECTION TYPE-SI, CRACK INDICATION NOTED IN RT 41 SECTION SKIN, BS 235.8, WL 218.5 AFT ROW MARKED IN RED. REPAIRED IAW SRM 53-30-3.

Part: SKIN — CORRODED (BS 680/682)

INSPECTION TYPE-SI, CORROSION (B727-5330-0509) SKIN LAP IS PILLOWING BS 680 TO 682 STR 19 LT. REPAIRED PER SRM 53-30-01.

Part: SKIN — DELAMINATED (NR 9 SPOILER)

INSPECTION TYPE-SI, NR 9 SPOILER HAS AN AREA OF DELAMINATION 6 IN FROM L/E AT I/B END. REPAIRED IAW SRM 57-50-6.

Part: SKIN — CORRODED (BS 351)

INSPECTION TYPE-SI, MISSING AND DISHED FASTENERS ON EXTERIOR SKIN ABOVE NOSE JACK PAD AT LONGITUDINAL LAP, BS 351, RBL 70, WL 180. REPAIRED IAW EO B727-5330-0509 AND SRM 53-30-03.

Part: RIB — CRACKED (NR 6 LE FLAP)

INSPECTION TYPE-SI, NR 6 SLAT O/B RIB END 2ND IN FROM O/B END IS CRACKED. REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-01.

Part: FITTING — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-SI, NR 4 K-FLAP CENTER L/E HINGE FITTING IS CORRODED. REMOVED AND REPLACED PER SRM 51-30-2.

Part: HYD MODULE — FAILED (A-HYD SYST)

INSPECTION TYPE N/A, INFLIGHT HAD HYD A-SYS OVERHEAT. FOLLOWED CHECKLIST, TURNED PUMPS OFF AFTER OVERHEAT EXT, TURNED PUMPS BACK ON AND GOT 200 LBS PRESS PER PUMP. A TOTAL OF 500 PSI WAS ATTAINED WITH BOTH PUMPS, QTY WAS GOOD. PROCEEDED WITH LOSS OF HYD SYS-A CHECKLIST. WHILE MANUAL EXTENDING FLAPS THE OUTBOARDS WOULD NOT EXTEND, GOT ALL LEADING EDGE DEVICES. REMOVED AND REPLACED HYDRAULIC SYS-A MODULAR IAW MM 29-11-00, LEAKED CHECKED GOOD. (P/N 65-17821-14) (S/N 2381A) ON, (P/N MR29108-60) OFF.

Part: LINING — WEAR DAMAGE (NR 2 ENG INTAKE)

INSPECTION TYPE-C, DAMAGE TO ATTENUATION LINING ON NR 2 ENGINE (S/N 81058). REPAIRED IAW UPS EO TAY 7230-8339-A.

Part: FRAME — CRACKED (BS 940)

INSPECTION TYPE-C, CRACKS FOUND IN BS 940 FRAME. FRAME REPLACED PER UPS EO B727-5310-4501.

Part: LATCH FITTINGS — CORRODED (CARGO DOOR)

INSPECTION TYPE-C, MAIN CARGO DOOR LATCH FITTINGS PINS SEIZED. ALL LATCH FITTINGS REPLACED SRS EO 96-27-005.

Part: SUPPORT BEAM — CORRODED (MLG)

INSPECTION TYPE-C, INCORRECT BOLTS PITTED. CORROSION FOUND IN MLG SUPPORT BEAM WHEN BOLTS REMOVED. REWORKED IAW UPSEO 727-5740-0727, SRS EO 96-27-011, EO 96-27-012.

Part: SKIN — CORRODED (BS 441)

INSPECTION TYPE-C, CORROSON ON SKIN AT BUTT JOINT BS 441 54L TO 53R. REPAIRED PER APPENDIX 8.5 OF B727-5310-1371E.

Part: ANGLE — CORRODED (BS 760.95)

INSPECTION TYPE-C, CORROSION ON FLOOR SUPPORT ANGLE AT BS 760.95 AND U/S OF CASTING AT 870 RT. CORROSION ON FLOOR SUPPORT ANGLE REMOVED AND TREATED AND CASTING REPAIRED PER SRS EO 96-27-06.

Part: HINGES — CORRODED (MAIN CARGO DOOR)

INSPECTION TYPE-C, FORWARD AND AFT MAIN CARGO DOOR HINGES SEVERLY CORRODED. REPLACED HINGES.

Part: SKIN — CRACKED (BS 936)

INSPECTION TYPE-C, CRACK FOUND IN SKIN BEHIND STR 18A AT RT BS 936. REPAIRED IAW UPS EO B727-5330-3815-A.

Part: FLOOR BEAM — CRACKED (BS 370)

INSPECTION TYPE-C, CRACK FOUND ON FLOOR BEAM UPPER FLANGE AT BS 870 AT ATTACH POINT TO BS 870 FITTING RT SIDE. REPAIRED IAW SRS EO 96-27-012.

Part: SUPPRT BRACKET — CRACKED (TE MID FLAP)

INSPECTION TYPE-C, MID FLAP INTERNAL STRUCTURE LT AND RT INB CRACKING IN RIB SUPPORT BRACKETS. BRACKETS REPLACED AS NECESSARY.

Part: DOOR SILL — CORRODED (MAIN CARGO DOOR)

INSPECTION TYPE-C, SEVERAL AREAS OF CORROSION AS WELL AS A NUMBER OF HOLES DUE TO CORROSION IN MAIN CARGO DOOR SILL. REPLACED SILL.

Part: LOWER BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE-C, CRACK IN LOWER BEAM OF MAIN CARGO DOOR AT BS 580. REPAIRED IAW SRS EO 96-27-007.

Part: ATTACH FITTING — CORROSION (BS 870)

INSPECTION TYPE-C, CORROSION FOUND ON LOWER SURFACE OF THE AFT UPPER FLANGE OF THE BS 870 FITTING AT FLOOR BEAM ATTACH. REPAIR IAW SRS EO 96-27-006.

Part: FLAP TRACK — CORRODED (LT TE FLAP)

INSPECTION TYPE-C, L/W I/B FLAP TRACK CORRODED AND CORROSION ON BOLT HOLE IN LG BEAM FOR FLAP TRACK ATTACH. REPAIRED PER UPS EO B727-5742-0651-1 AND SRS EO 96-27-011.

Part: SILL — CORRODED (CARGO DOOR)

INSPECTION TYPE-C, CARGO DOOR SILL CORRODED. REPLACED SILL.

Part: RETRACT MECH — LACK OF LUBE (NLG)

CREW REPORTED, NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT AND RED DOOR LIGHT ON FWD PANEL. MAIN GEAR EXTENDED NORMALLY AND ALL GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. JACKED NOSE GEAR AND LUBED NOSE GEAR, RETRACTED AND EXTENDED GEAR SEVERAL TIMES AND OPS CHECK GOOD.

Part: EEL BATTERY — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN SWITCHED TO ON. REPLACED EMERGENCY EXIT LIGHT BATTERY, OPS CK NORMAL.

Part: RIB — CORRODED (VERT STAB)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON RT UPPER RIB CHORD AT RBL 70.5, BS 760, FORWARD TWO FASTENER HOLES. INSTALLED REPAIR PER UPS EO B727-5710-1271F.

Part: RIB — CRACKED (NR 5 LE SLAT)

DURING 'C' CHECK, MAINTENANCE FOUND NR 5 SLAT RIB CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-50-3.

Part: ATTACH POINTS — CORRODED (NR 6 K-FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP ATTACH POINTS CORRODED ON K-FLAP SIDE. REPLACED FLAP PER MM 27-81-01.

Part: ANGLE — CORRODED (NLG COMPT)

DURING 'C' CHECK, MAINTENANCE FOUND NOSE LANDING GEAR LOWER LT ANGLE CORRODED. REPLACED CHORD PER SRM 51-30-2, 51-50-1, 51-40-2.

Part: WEDGE — DELAMINATED (LT AILERON)

DURING 'C' CHECK, MAINTENANCE FOUND LT AILERON O/B TRAILING EDGE WEDGE IS DELAMINATED. REPLACED WEDGE PER SRM 51-80-6, 51-10-2, 51-30-2, MM 27-10-41.

Part: FITTING — CRACKED (BS 500)

DURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR LATCH SUPPORT FITTINGS IN THE FUSELAGE STRUCTURE CRACKED AT BS 500. REPLACED FITTING PER UPS EO B727-5310-0437.

Part: DOOR FRAME — CRACKED (MAIN CARGO DOOR)

DURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR AFT SIDE FRAME CRACKED AT DRIFT PIN RECEPTACLE AT I/B RADIUS. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-2, 51-40-3, 51-10-2.

Part: CORE — DAMAGED (RT TE FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING I/B AFT FLAP CORE WATER DAMAGED. REPLACED FLAP PER MM 27-51-02.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING 'C' CHECK MAINTENANCE FOUND LT I/B AFT FLAP TRAILING EDGE IS DELAMINATED ON TRAILING EDGE. REPLACED FLAP PER MM 27-51-02.

Part: AILERON — CORRODED (LT AILERON)

WHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AILERON CONTROL ROD FITTING CORRODED AROUND BOLT HOLE. REPLACED AILERON PER MM 27-10-11.

Part: WEDGE — CORRODED (RT MID FLAP)

WHILE IN 'C' CHECK, MAINTENANCE FOUND TRAILING EDGE WEDGE ON RT I/B MID FLAP CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2 AND OHM 20-50-01.

Part: FLAP — CORROSION (NR 3 K-FLAP)

WHILE IN 'C' CHECK MAINTENANCE FOUND NR 3 K-FLAP O/B HINGE O/B LUG UPPER AND LOWER BOLT HOLES HAVE PITTING AROUND O/B SIDE. REPLACED K-FLAP PER MM 27-81-00.

Part: FLAP — CORROSION (NR 6 K-FLAP)

WHILE IN 'C' CHECK MAINTENANCE FOUND NR 6 K-FLAP O/B HINGE LUG ATTACH POINT HAS CORROSION UNDER TOP BOLT O/B SIDE. REPLACED K-FLAP PER SRM 57-51-1 AND MM 27-81-01.

Part: SKIN — CRACKED (BS 259.7-277)

WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL SKIN AT BS 259.7-277. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3, 51-30-5, 51-20-21, 51-30-2.

Part: SKIN — DELAMINATED (RT AILERON TAB)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT I/B AILERON TAB, T/E LWR SURFACE. INSTALLED REPAIR PER SRM 51-40-6, 51-80-3.

Part: WEDGE — DELAMINATED (LT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, MID FLAP TRAILING EDGE WEDGE, I/B END, UPPER SURFACE. INSTALLED REPAIR PER SRM 51-40-6.

Part: SKIN — DELAMINATED (LT TE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, AFT FLAP TRAILING EDGE. NORDERED NEW FLAP ASSY.

Part: SKIN — DELAMINATED (LT AILERON TAB)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B AILERON TAB, TRAILING EDGE. INSTALLED REPAIR PER SRM 51-80-3 AND 51-40-6.

Part: FLOOR — DELAMINATED (BS 294.5-312)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON WALKWAY PANEL AT STA 294.5-312, RBL 25, WL 169. REPLACED PER SRM 51-40-2, 53-10-2, 51-10-2, MM 51-20-151, AND 51-30-2.