N902UP

Part: INDICATOR — MALFUNCTIONED (CARGO FIRE)

FIRE INDICATION IN LWR FWD PIT. CREW CLOSED BELL TESTED SYSTEM & FIRE INDICATION RETURNED. CREW DECLARED EMERGENCY & SHOT FIRE BOTTLE. A/C LANDED WITHOUT FURTHER INCIDENT. CFR CONFRIMED NO FIRE. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYSTEM ADJUSTMENT & TEST FOUND MX & SYS OK LIGHTS ILLUM DETECTOR F1717=ODB TESTED LOWER CARGO SMOKE DETECTION SYSTEM, NO FAULTS NOTED, OPS CHECK GOOD PER MM 26-18-00 THIS CLEARS MEL 26-19-1-2, PLACARD REMOVED.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A BOTH EMERGENCY LIGHT BATTERY PACKS LOW. REMOVED AND REPLACED BATTERY, OPS CHECK NORMAL.

Part: BULLET — CRACKED (NR 3 ENGINE)

INSPECTION TYPE:S-10 ENGINE 3 SPINNER CRACK FOUND DURING SEG-10 CHECK. HAS 1 INCH CRACK AT BOLT HOLE. REMOVED AND REPLACED NR 3 ENG SPINNER FAIRING IAW MM 72-30-10. OPS NORMAL AT THIS TIME.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY)

INSPECTION TYPE: LOWER CARGO SMOKE DETECTOR SYS MX LIGHT ILLUMINATED. REMOVED AND REPLACED TWO SMOKE DETECTORS REF MM 26/18/00 S/N IN FWD 11363 S/N OUT FWD 3740 S/N IN AFT 2356 S/N OUT AFT 5107.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B727 MM 33-50-101 OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (LIGHT PACK)

BOTH EMERGENCY EXIT LIGHT BATTERY PACK LIGHTS VERY DIM FADE TO NEAR FAILURE IN 30 SECONDS. REPLACED BOTH BATTERIES IN BOTH LIGHT PACKS AS REQUIRED STEADY ILLUMINATION OPS CK OK

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:IN, COCKPIT EMERGENCY EXIT DOOR LIGHTS INOP. INSTALLED EMERGENCY LIGHT AND OPS CK OK IAW MM 25-60-00, P/N ON 10-60091-10, S/N ON 28518.

Part: ANGLE — CRACKED (BS 940-950)

INSPECTION TYPE:C, RIGHT MLG WHEEL WELL O/B AFT SIDE, HORIZONTAL SHELF 10 BELOW PRESS DECK BETWEEN FS 940 FORGING AND FS 950 FORGING, LOWER O/B ATTACH ANGLE CRACKED. REMOVED DAMAGED AREA AND INSTALLED FITTING AS PER B727-5310-4177A AT RIGHT MLG WHEEL WELL O/B AFT SIDE HORIZONTAL SHELF 10 O/B ATTACH ANGLE AS PER UPS EO B727-5310-4177-A.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS GREW DIM. REPLACED BATTERIES IN BOTH EMERGENCY EXIT LIGHTS.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, DURING SECURE CHECK FOUND EMERGENCY EXIT LIGHTS (BOTH) DID NOT WORK. REPLACED BATTS IN BOTH EMERGENCY EXIT LIGHT ASSY, OPS CK'S NORMAL PER MM 33-50-101.

Part: BATTERY PACK — DISCHARGED (L1 DOOR)

INSPECTION TYPE-N/A, EMER LIGHT AT L-1 DOOR WILL NOT SHUT OFF. REMOVED AND REPLACED EMER BATT PACK PER MM 33-50-01, OPS CK GOOD. (P/N 10-0067-7) (S/N 3893) ON, (S/N 26993) OFF.

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

ON PDC, FWD ENTRY EEL WOULD NOT TEST. REMOVED AND REPLACED EEL BATT PACKS, OPS CHECK GOOD.

Part: BATTERIES — DISCHARGED (PAX DOOR)

INSPECTION TYPE:PDC ON PDC, FWD ENTRY DOOR EMERGENCY EXIT LIGHT WOULD NOT TEST. FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES REPLACED AND TESTED AS PER M/M 33-50-101. OPS CHECKED SERVICEABLE.

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

FWD ENTRY DOOR OVERHEAD EMERG LIGHT DIM ON TEST. REMOVED AND REPLACED BATT PACK OPS CHECK GOOD PER MM 33-50-01.

Part: FRAME — CRACKED (BS 880.45)

INSPECTION TYPE:D, WINDOW FRAME BS 880.45 RT FOUND CRACKED FWD TOP CORNER. REPLACED IAW BOEING DRG NR 65C-18383 AND EO B727-5310-3057.

Part: BULKHEAD FRAME — CORRODED (BS 351)

INSPECTION TYPE:D, FRAME ON FWD SIDE OF B/H 351 LT SIDE IS CORRODED BETWEEN STR 22 AND 23. FRAME REPAIRED IAW SRM 53-10-4 FIG 13.

Part: FRAME — CRACKED (BS 580)

INSPECTION TYPE:D, SUSPECT CRACK IN OUTER CHORD OF FRAME 580 STR 17 L. REPAIRED FRAME IAW SRM 53-10-2.

Part: STRINGER — CORRODED (BS 450)

INSPECTION TYPE:D STRINGER 24 RIGHT HAS SURFACE CORROSION AT STA 445 AND 460. STRINGER SECTION REPAIRED IAW SRM 53-10-3.

Part: SKIN — DISBONDED (BS 1080-1183)

INSPECTION TYPE-D, DISBONDED SKIN REMOVED LEFT HAND 1183 TO BS 1080 FROM STRINGER 18 TO 26. REPAIR CARRIED OUT PER SRM ENGINEERING ORDER 98-12-007, REF UPS ENGINEERING FILE NUMBER 5330-2032 AND DRAWING 65-18386.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION TYPE:D, A NUMBER OF DEEP DENTS IN SKIN (FWD CARGO DOOR) SKIN HAS ALOT REPAIRS. SKIN REPLACED IAW DRW NO 65-8620.

Part: ANGLE — CRACKED (BS 560-580)

INSPECTION TYPE:D SUSPECT CRACK IN UPPER CHORD OF INTERCOSTAL BETWEEN BS 560-580 (JUST AFT OF 560) RBL 25. REPLACED CHORD ANGLE IAW SRM 51-40-3.

Part: ANGLE — CORRODED (BS 351)

INSPECTION TYPE:D, CORRODED ANGLE RT WALKWAY AFT SUPPORT AT ST 351. REPLACED ANGLE IAW SRM 53-10-2.

Part: FRAME — BROKEN (BS 600)

INSPECTION TYPE:D LOWER O/B CHORD OF FRAME 600 BROKEN OFF BETWEEN STRINGERS 25-25 LEFT, REPAIR IAW SRM 53-10-4 FIG 12.

Part: FRAME — CRACKED (BS 640)

INSPECTION TYPE:D CRACK IN UPPER CHORD OF FRAME 640 BETWEEN STRINGERS 21 AND 22 LT. FRAME AT BS 640 BETWEEN STR 21 AND 22L REPAIRED IAW SRM 53-10-4.

Part: ANGLE — CRACKED (NR 1 SPOILER)

INSPECTION TYPE:D NR 1 SPOILER ACTUATOR SUPPORT FITTING INB SUPPORT ANGLE HAS CRACKS AROUND LWR HOLE. REPLACED SUPPORT ANGLE IAW SRM 51-30-2.

Part: BOTTLE PIN — PITTING (BS 870)

INSPECTION TYPE:D PITTING ON FWD EDGE OF RT AFT REAR SPAR TO BODY BOTTLE PIN. BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: CLEAT — CRACKED (BS 560)

INSPECTION TYPE:D, SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 560 LT SIDE. CLEAT REPLACED IAW SRM 51-10-1 AND 53-10-2 FIG 3 HEAT TREATMENT REF.

Part: CLEAT — CRACKED (BS 600)

INSPECTION TYPE:D, SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 600 LT SIDE. CLEAT REPLACED IAW SRM 51-10-1 AND 53-10-2.

Part: STIFFENER — CRACKED (BS 178)

INSPECTION TYPE:D STIFFENER CRACKED BS 178, STR 17 R. CARRIED OUT REPAIR IAW SRM 51-40-3.

Part: INTERCOSTAL — CORRODED (BS 211-219)

INSPECTION TYPE:D INTERCOSTAL BETWEEN STR 219 AND 211 RT SIDE BL 25 APPROX CORRODED. REPLACED PER SRM 51-10-1 AND SRM 53-10-2.

Part: FRAME — CRACK (BS 540)

INSPECTION TYPE:D SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 540 LT SIDE. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.

Part: ACCESS PANEL — CORRODED (RT WING)

INSPECTION TYPE:D EXTENSIVE CORROSION ON NR 1 FRONT SPAR FUEL TANK ACCESS PANEL RT WING. REPLACED IAW MM 28-11-21.

Part: WEB — CORRODED (BS 870)

INSPECTION TYPE:D, RT MAIN WHEEL WELL CORROSION ON WEB AT BL 20 STA 870 BULKHEAD JUST BELOW FLOOR LEVEL. REPAIR CARRIED OUT IAW SRM 51-40-4.

Part: SKIN — CRACKED (BS 328)

INSPECTION TYPE:D CRACKS FOUND IN BOTH UPPER AND LWR FWD ENTRY DOOR HINGE CUTOUTS. REPAIRED BOTH UPPER AND LWR FWD ENTRY DOOR HINGE CUTOUTS IAW EO B727- 5330-128.

Part: PANEL — CORRODED (WS 198)

INSPECTION TYPE:D LT WING FRONT SPAR FUEL TANK ACCESS PANEL CORRODED. ACCESS REPLACED IAW MM 28-11-2.

Part: RING CLAMPS — CORRODED (WS 716-491)

INSPECTION TYPE:D SEVERAL FUEL TANK ACCESS DOORS, RING CLAMPS HAVE FRETTING CORROSION LT WING. RING CLAMPS REPLACED IAW 28-11-21 MM 6 OFF PANEL NR'S 3, 5, 6, 7, 8, 9, 10 CORROSION REMOVED AND FOUND TO BE IN LIMITS OF SRM 57-30-03, REPROTECTED IAW SRM 57-30-03.

Part: WEB — CRACKED (BS 1387)

INSPECTION TYPE:D, SUSPECT CRACK ON LT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 657 555.

Part: SKIN — CORRODED (BS 1173-1183)

INSPECTION TYPE:D CORROSION BETEEN STR 1173-1185 RT BETWEEN STRS 22 AND 25 IN BETWEEN THE BONDED INTERNAL DOUBLER. DISBONDED INTERNAL DOUBLER AND SKIN REMOVED SKIN REPAIR CARRIED OUT IAW SRS EO 98-12-004.

Part: CARRIAGE — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE:D, NR 3 FLAP CARRIAGE SPINDLE LINK CORRODED. LINK ASSY REPLACED IAW OHM 57-52-01.

Part: CARRIAGE — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE:D, NR 3 FLAP CARRIAGE SPINDLE LINK SUPPORT CORRODED. LINK SUPPORT REPLACED IAW OHM 57-52-01.

Part: WEB — CRACKED (BS 1387)

INSPECTION TYPE:D, SUSPECT CRACK ON RT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4 . CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 6517 555.

Part: CARRIAGE — CORRODED (NR 8 TE FLAP)

INSPECTION TYPE:D NR 8 FLAP CARRIAGE HAS CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM.

Part: TUNING FORK — CRACKED (BS 870)

INSPECTION TYPE:D, TUNING FORK AT BS 870 STR 2 R CRACKED. TUNING FORK REPLACED IAW SRM51-30-2.

Part: RIB — CRACKED (WS 519)

INSPECTION TYPE:D CRACK ON RIB AT LWR SUPPORT ANGLE NR 6 SLAT BELOW O/B HOOK. REPAIRED IAW SRM 51-40-2.

Part: TORQUE TUBE — CRACKED (NR 2 LE FLAP)

INSPECTION TYPE:D, CRACK CONFIRMED IN NR 2 KRUEGER FLAP TORQUE TUBE STRUCTURE. REPLACED NR 2 KREUGER FLAP ASSY IAW MM 27-81-01.

Part: RIB — CRACKED (WS 410)

INSPECTION TYPE:D, NR 5 SLAT I/B RIB AT ACTUATOR ROD END CRACKED. CRACK REPAIRED IAW SRM 51-40-2.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECKS GOOD.

Part: ACT BRACKET — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED UNDER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, BOEING DRAWING 65-16269, SRM 51-30-2.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-C, NR 4 SLAT INBOARD TRACK, O/B ATTACH RIB IS CRACKED. REPAIRED RIB PER SRM 51-40-3.

Part: RIB — CRACKED (NR 7 LE SLAT)

INSPECTION TYPE-C, NR 7 SLAT RIB AT THE I/B SIDE OF ACTUATOR IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2.

Part: WEB — CRACKED (BS 1218)

INSPECTION TYPE-C, RT AFT LOWER TORQUE BOX I/B WEB AT STA 1218 IS CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-42.

Part: ATTACH RIB — CRACKED (NR 7 LE SLAT ACT)

INSPECTION TYPE-C, RT WING NR 7 SLAT ACTUATOR ROD END ATTACH O/B RIB IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2, 51-40-3.

Part: ACT BRACKET — CRACKED (NR 6 LE FLAP)

INSPECTION TYPE-C, RT WING NR 6 K-FLAP ACTUATOR O/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED REPLACEMENT BRACKET AND INSTALLED PER SRM 51-10-1, 51-30- 1, BOEING DRAWING 65-16275.

Part: BRACKET — CRACKED (BS 870)

INSPECTION TYPE-C, ATTACH CLIP CRACKED IN RADIUS AT LT W/W FWD UPPER STR 18A TO 870 FITTING. FABRICATED AND INSTALLED CLIP PER BOEING DRAWING 65-22419 AND SRM 51 -30-2.

Part: ACT BRACKET — CRACKED (NR 6 LE FLAP)

INSPECTION TYPE-C RT WING NR 6 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, 51-30-1, BOEING DRAWING 65-16275.

Part: SEAT TRACK — CORRODED (LOWER CARGO)

INSPECTION TYPE-C, RT SEAT TRACK HAS LIGHT SURFACE CORROSION FULL LENGTH OF FWD LOWER CARGO. REPLACED SEAT TRACK PER SRM 51-30-2.

Part: LIGHT — INOPERATIVE (COCKPIT DOOR)

MAINTENANCE REPORTED ON PRE-DEPARTURE CHECK, EXIT LIGHTS IN COCKPIT FOUND INOPERATIVE. LIGHT ABOVE DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT WILL NOT ILLUMINATE WHEN TURNED ON. REPLACED BATTERIES IN BOTH EMERGENCY EXIT LIGHTS. OPS CHECK GOOD.

Part: FLOORBEAM — CRACK (BS 940)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON FLOORBEAM ATTACH FLANGE NEAR BS 940. REPAIRED IAW B727-5310-5596.

Part: FRAME — CRACKED (FS 760)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FRAME ON STA 760, LBL 72, WL 205. REPAIRED IAW B727-5310-7117-A.

Part: ANGLE — CORRODED (FS 920)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT B.S. 920, LBL 65, WL 189 AROUND LOWER FASTENERS. REPAIRED IAW SRM 51-10-2, 51-30-5, 51-30-2, 51-20-1, M/M 51-20-31.

Part: STIFFENER — CRACKED (NR 6 LE SLAT)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER R/W L/E NR 6 SLAT I/B TRACK I/B SIDE LOWER END SLAT STA 135.5. REPAIRED IAW SRM 51-30-2, 51-10-2, M/M 28-11-21, 36-00-01, OHM 20-50-01.

Part: FLOOR BEAM — CORRODED (FS 344)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION UNDER UPPER FLOOR BEAM FLANGE, FORWARD SIDE STA 344, RBL 2, WL 208. REPAIRED IAW SRM 51-20-1, 51-10-1, 53-10-8, 51-30-2.

Part: WEB — CORRODED (FS 351)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON B.S. 351 WEB AT RBL 217, WL 172. REPAIRED IAW SRM 51-40-2.

Part: SKIN — DELAMINATED (RUDDER TAB)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB ON LOWER RT SIDE. REPAIRED IAW SRM 51-40-9.

Part: WINDSHIELD SILL — CRACKED (FS 267)

WHILE IN C-CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL LT SIDE AT B.S. 267. REPAIRED IAW SRM 727-53-1620.

Part: SKIN — CRACKED (FS 1330)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SKIN AT BLOWOUT DOOR CUTOUT, B.S. 1333, LBL 48, WL 217. REPAIRED IAW SRM 51-10-2, 53-30-3, 51-30-2, 51-20-4, 51-10-1, 51-10-2, M/M 51-20-151.

Part: BOX FAIRING — CRACKED (FS 277)

WHILE IN C-CHECK MAINTENANCE FOUND CRACK EXTRUDING PAST STOP DRILL IN NOSE WHEELWELL SIDE BOX FAIRING. B.S. 277, RBL 23.5, WL 168. REPAIRED IAW SRM 51-10-2, 51-30-2, 51-21-1.

Part: RIB — CRACKED (WS 70.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142.

Part: WEDGE — DISBONDED (RT TE MID FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W O/B MID FLAP T/E WEDGE UPPER SURFACE DISBONDED. REPAIRED IAW SRM 57-40-6, 51-40-6.

Part: ANGLE — BROKEN (WS 120)

WHILE IN C-CHECK MAINTENANCE, FOUND BROKEN ANGLE SUPPORT BRACKET AT WING BASE LINE STA 120, BEHIND THE NR 8 SPOILER ACTUATOR FITTING. REPAIRED IAW SRM 51-20-1, 51-30-2.

Part: WEDGE — DELAMINATED (RT TE MID FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DISBONDED R/W I/B MID FLAP T/E WEDGE UPPER SURFACE AND WATER IN HONEY COMB. REPAIRED IAW SRM 51-40-6.

Part: STRAP — CORRODED (FS 351)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRAP B.S. 351, RBL 30, WL 172. REPAIRED IAW SRM 51-40-4.

Part: WINDSHIELD SILL — CRACKED (FS 269)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL RT SIDE AT B.S. 269. REPAIRED IAW SRM 53-30-3, 51-30-2.

Part: RIB — CRACKED (WS 70.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142-A.