N933UP

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0067, S/N OFF 42-11, S/N O N 27025. OPS CHECKS GOOD

Part: WINDSHIELD — FAILED (COCKPIT)

FIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOOD

Part: FIRE LOOP — INOPERATIVE (NR 3 ENGINE)

INSPECTION TYPE:IN ENG NR 3 A-LOOP WILL NOT TEST. *S/D* FOUND CONNECTOR D354J CONTAMINATED WITH DIRT AND MOISTURE. CLEANED SAME THOROUGHLY. TESTED NORMAL. M209166 CLEARED.

Part: STRUCTURE — CRACKED (NR 4 SLAT)

INSPECTION TYPE:PRE NR 4 LEADING EDGE SLAT CRACKED. AWAITING LOG PAGE ENTRY.

Part: FLAP TRACK — CORRODED (NR 1 FLAP) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B HAVE LIGHT SURFACE RUST (CORROSION C57-581-06.00-03). REMOVED CORROSION FROM NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20235.

Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20232.

Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20232.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION ON UPPER SURFACE OF SHEAR WEB AT BS 640, WL 208 LBL 63. SHEAR WEB REPLACED AT STA 630 - 660, LBL 45-LBL 62, WL 208 PER ER NR 00-0952.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, STRINGER FITTING IS CRACKED AT BS 365 STR 26L. REMOVED AND REPLACED STRINGER FITTING.

Part: SKIN — CORRODED (RUDDER) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:C, CORROSION ON LWR RUDDER RT SKIN AT STA 120.6 IN BELOW FRONT SPAR. REPAIRED PER SRM 55-20-3 PG 1 STEP 3 & 4 AND SRM 51-40-5 PG 20 & 22 STEP 13 A-I.

Part: FITTING — CRACKED (KRUGER FLAP) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, NR 1 K-FLAP O/B ATTACH LUG FITTING ON K-FLAP UPPER O/B SIDE IS CRACKED. REMOVED AND INSTALLED NEW K-FLAP ASSY PER MM 27-81-01.

Part: MOUNT — CORRODED (FLAP TRACK) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AFT ATTACH MOUNT BLOCK OUT OF LIMITS IAW SRM 51-30-2. REMOVED AND REPLACED MOUNT BLOCK IAW SRM 51-30-5.

Part: FITTING — CORRODED (FLAP TRACK) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, NR 6 FLAP TRACK SPOILER BEAM MOUNT FITTINGS CORRODED OUT OF LIMITS IAW SRM 51-30-2 ON RT WING. FOUND WHILE WORKING NRC 178771. REMOVED CORRODED MOUNT FITTINGS AND REPLACED WITH NEW PART IAW SRM 51-30-2.

Part: FLAP TRACK — CORRODED (WING) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, NR 5 FLAP TRACK IS RUSTED AT MAIN LANDING GEAR DOOR FWD FITTING ATTACH BOLTS. REMOVED AND REPLACED FLAP TRACK PER TC 57-581-04-4D.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION (SDN C57-581-04.00-04) IN BORE OF SPINDLE FOR NR 6 FLAP CARRIAGE. REMOVED AND REPLACED NR 6 FLAP CARRIAGE PER MM 25-51-03.

Part: STRINGER — CRACKED (RT WING) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, RIGHT WING UPPER STR 17 OUTSIDE OF RIB AT WS 304 IS CRACKED. REMOVED CRACK STRINGER SECTION. FABRICATED AND INSTALLED NEW SECTION, ALL WORK DONE IAW SRM 57-10-4, 51-20-1, 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) FWD CARGO BAY BS 660 FLOORBEAM FWD SIDE UPPER FLANGE LOWER SURFACE AT LBL 45 TO LBL 50. REMOVED CORROSION IN DESCREPANT AREA AT LBL 45 IN A 2.4 X 1.0 X .030 ORIGINAL THICKNESS .240 OUT OF LIMITS. REMOVED UPPER CHORD OF FLOORBEAM AT BS 660 LBL 8-LBL 72. FABRICATED NEW UPPER CHORD AND REPAIR PARTS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY STA 540 FLOORBEAM FWD SIDE, UPPER FLANGE, LWR SURFACE AT LBL 45. REMOVED CORROSION ON UPPER CHORD LOWER FLANGE IN AN AREA OF 1.0 X 2.0. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 5. CUT OFF TOP OF CHORD OF BS 540 LBL 10 TO LBL 65. FABRICATED REPAIR TEE CHORD AND OTHER REPAIR PIECES AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, MAIN DECK FLOOR WEB FITTING CORRODED (C53-224-01.00-03) BETWEEN LEFT CREASE BEAM AND DITCHING PAN, FWD OF BS 1183 BULKHEAD BS 1180 LBL 65, WL 208. REMOVED AND REPLACED FLOOR WEB FITTING IAW SRM 51-30-05, 53-10-01, 51-10-06.

Part: DRUM — CORRODED (RT MLG) · airframe 51,826 hrs · 40,151 cycles

INSPECTION TYPE:SI, RT MLG MANUAL EXTENSION CABLE DRUM IS CORRODED. REMOVED AND REPLACED PER MM 32-34-01.

Part: CHORD — CORROSION (LT WING SPAR)

INSPECTION TYPE:C CORROSION (C57-581-03-00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.

Part: SPAR CHORD — CORRODED (WING)

INSPECTION TYPE-C,CORROSION (C57-581-03.00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.

Part: SEAT TRACK — CRACKED (BS 760)

INSPECTION TYPE:C WHILE ACCESSING OVERWING FRAMES FOUND SEAT TRACK AT STA 760 RBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED SEAT TRACK FROM BS 760 TO BS 848 PER 727 SRM 53-10-5 AND 51-30-2.

Part: SKIN — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLAP PER MM 27-81-01 AND ADJUST/TEST PER 727 MM 27-81-00.

Part: SKIN — CORRODED (RT ELEVATOR)

INSPECTION TYPE-C ,CORROSION RT ELEVATOR AROUND BASE OF O/B STATIC WICK. REPLACED SKIN PER SRM 51-30-2 AND SRM 55-20-3.

Part: FOREFLAP — CORRODED (LT TE FLAP)

INSPECTION TYPE-C, LEFT WING O/B FOREFLAP HAS .25 X 3.5 AREA OF DELAMINATION. TAP TESTED, FOUND ADDITIONAL DELAMINATION. FOUND CORRSION ON SPAR. REPLACED O/B FOREFLAP.

Part: S DUCT — CRACKED (NR 2 ENGINE)

INSPECTION TYPE:C NR 2 ENGINE S DUCT HAS 5 INCH CRACK IN THE CENTER SECTION 4 RIBS FWD OF THE PRODUCTION BREAK, LT SIDE APPRX 8:00 POSITION. REMOVED DAMAGED AREA AND PERFORMED A FILLER AND DOUBLER REPAIR PER SRM 54-10-3, SRM 51-40-2 AND MM 51-20-151.

Part: SKIN — CORRODED (LT ELEVATOR)

INSPECTION TYPE-C, CORROSION (C55-300-10.00-01) ON LT ELEVATOR AROUND I/B STATIC WICK BASE. REMOVED CORROSION OUT OF LIMITS, REPLACED SKIN PANEL. ALL WORK DONE PER SRM 55-20-1, 55-20-2 AND MM 23-61-00.

Part: CONTROL VALVE — FAILED (LT PACK)

INSPECTION TYPE N/A, LEFT PACK TRIPPED OFF LIGHT ON LANDING ROLLOUT. LEFT PACK SWITCH DID NOT TURN OFF, WHITE SMOKE ENTERED COCKPIT. LOST CONTROL OF PACK EVEN WITH SWITCH OFF. LEFT PACK VLV STUCK OPEN, CYCLED VLV TO CLOSED POSITION AND ITEM DEFERRED PER MEL 21-2-2 ACCOMPLISHED DMP PROCEDURES 21-2-1.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT EMERGENCY EXIT LIGHT INOP. FOUND BOTH BATTERIES TO BE DEAD AND OUT OF DATE. REMOVED AND REPLACED TWO BATTERIES PER MM33-50-10. SYSTEM GROUND CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT WOULD NOT TEST, BATTERIES OK. REPLACED LIGHT ASSY.

Part: LINE — CRACKED (RT MLG DOOR)

INSPECTION TYPE-N/A, ON GEAR RETRACTION RIGHT MAIN GEAR DID NOT RETRACT, A HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. A PRESSURE WAS ZERO AND QUANTITY WAS ZERO. EXTENDED GEAR MANUALLY IN ACCORDANCE WITH AOM. FOUND RT MLG HYDRAULIC DOOR UP LINE CRACKED. INSTALLED TEMPORARY FLEX LINE WITH NEW CLAMP AND HARDWARE ISSUED DEFERRAL PER MMOC D141726, LINE INSTALLED PER GMM 3-24-1. LEAK CHECKED GOOD. INSTALLED RIGID LINE, LEAK CHECKED GOOD. THIS CLEARS D141726 (P/N 65-17843-209).

Part: SKIN — DELAMINATED (NR 7 SPOILER)

INSPECTION TYPE-C, NR 7 SPOILER HAS A 4 BY 5 AREA OF DELAMINATION ON LOWER SURFACE O/B FWD CORNER. REPAIRED DELAMINATION IAW SRM 57-50-06 FIG 5.

Part: SEAT TRACK — CRACKED (BS 660)

INSPECTION TYPE:C SEAT TRACK CRACKED AT BS 660 LBL 65. REMOVED AND REPLACED SEAT TRACK AT BS 660 LBL 65.

Part: SKIN — CORRODED (NR 4 LE FLAP)

INSPECTION TYPE-C, NR 4 K-FLAP O/B BONDING JUMPER HOLE HAS CORROSION AROUND OLD BONDING JUMPER LOCATION. CORROSION REWORK OUT OF LIMITS IAW UPS EO B727-5740-3980 (SRM ADDENDOM) REPAIRED NR 4 K-FLAP AT OLD BONDING JUMPER LOCATION IAW SRM 57-50-3.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND LT 930 FRAME CRACKED AT WL 228. REPAIRED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.

Part: RIB — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE-C, NR 5 K-FLAP I/B LOWER BONDING JUMPER ON K-FLAP HAS CRACK EMANATING FROM HOLE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON NR 5 K-FLAP I/B RIB AT BONDING JUMPER PER SRM 57-50-3.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND RT 930 FRAME CRACKED AT WL 228. REPAIRED CRACKED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.

Part: FITTING — CORRODED (BS 740)

INSPECTION TYPE:C CORROSION ON UNDERSIDE OF HORIZONTAL FLANGE OF BS 740 BODY FITTING LBL 65 WL 207. BODY FITTING REPAIRED IN ACCORDANCE WITH BFG ER 97-2479 AND UPS ENGINEERING FILE DOCUMENT 727-53-1959.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE P/F, EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AT COCKPIT DOOR. REPLACED BATTERIES ON EMERGENCY BAT PACK LIGHT (S/N 39810).

Part: SUPPORT FITTING — MISDRILLED (BS 940)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. REMOVED DAMAGED AREA AND REPAIRED PER EO 727-53-1754.

Part: BULLNOSE — CORRODED (NR 1 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW MM 27-81-0 AND OHM 57-51-01.

Part: SKIN — DELAMINATED (RT TE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT AFT O/B FLAP 3 FEET I/B, 1 INCH LONG BY .125 INCH WIDE DELAMINATION MPIP-6098. REPAIRED PER SRM 51-40-06.

Part: STRINGER — CRACKED (WS 629)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RWS 629.0 STR 12 HAS A CRACKED VENT STR TAB. REPAIRED STR 12 RWS 629.0 IAW UPS EO B727-5710-0314 APP 8.3.

Part: FRAME — CORROSION (BS 720)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AFT SIDE OF FRAME WEB BS 720 BL 0 WL 159. REPAIRED IAW SRM 53-10-1, 51-40-2, 51-10-2, 51-30-2.

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE REPORTED, FWD ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD ENTRY LIGHT ASSY, CK NORMAL.

Part: EEL — MALFUNCTIONED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT ASSY AS YOU ENTER CABIN, WOULD NOT WORK WHEN LIGHTS ARMED AND POWER SHUTDOWN. ASSY WOULD ONLY WORK WITH SWITCH ON, ON THE ASSY ITSELF. REMOVED AND REPLACED ASSY USING ORIGINAL BATTERIES, OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 328)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208. ALSO, HAS MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED FLOORBEAM PER 727 SRM 53-10-8 FIGURE 7 AND EO 727-53-1686.

Part: EEL BATT PACK — LOOSE (ENTRY DOOR)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR MUST BE BANGED ON TO MAKE WORK. FOUND BATT PACK LOOSE. CLEANED DOOR CONTACT PINS AND RESECURED BATT PACK. OPS CK NORMAL MM 33-50-00.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT BATTERY PACK DIM. REMOVED AND REPLACED BATTERY LIGHT PACK.

Part: EEL — INOPERABLE (CABIN)

WHILE ON GROUND IN CLEVELAND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.

Part: ANNUN PANEL — INOP (LANDING GEAR)

PILOT REPORTED THAT ON INITIAL GEAR EXTENTION NLG GREEN LIGHT DID NOT ILLUMINATE, RECYCLED GEAR AND DID NOT GET GREEN NLG LIGHT (RED UNSAFE LIGHT WAS OUT). ON SUBSEQUENT APPROACH, GEAR WAS LOWERED AND NLG GREEN LIGHT DID NOT ILLUMINATE. VISUALLY CHECKED AND VERIFIED NOSE GEAR. REPLACED LANDING GEAR ANNUNCIATOR PANEL. OPS CHECK OK.

Part: GATE BEAM — CRACKED (FWD ENTRY DOOR)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON FWD ENTRY DOOR LWR GATE BEAM CRACKED LWR FWD CORNER IN RADIUS. INSTALLED REPAIR PER SRM 51-10-01, 51-30-02.

Part: STRINGER — CORRODED (BS 970-1130)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3L, STA 970-1130. INSTALLED REPAIR PER SRM 51-10-06, 51-30-02, 51-10-02, 51-40-05, 53-10-01, 53-10-04.

Part: FLOORBEAM — CORRODED (BS 328)

DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES IN FLOORBEAM STA 328, LBL 23 AND 48, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6666A.

Part: FLOORBEAM — CORRODED (BS 560)

DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND FLOOR BOARD HOLES IN FLOORBEAM STA 560, RBL 45-65, LBL 0-25, LBL 57-63, ON BOTTOM SIDE OF TOP CHORD. INSTALLED REPAIR PER SRM 53-10-08.

Part: SEAT TRACK — CORRODED (BS 620-740)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 620 TO 740 RBL 25, WL 208. INSTALLED REPAIR PER SRM 53-10-05, 51-30-02.

Part: SEAT TRACK — CORRODED (BS 620-740)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT STA 299 LBL 0 TO 12, WL 208. INSTALLED REPAIR PER SRM 51-30-02.

Part: FRAME — CORRODED (BS 360)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FRAME IN BOLT HOLES BETWEEN STRINGERS 21L AND 21R, BS 360. INSTALLED REPAIR PER UPS EO B727-5310-6725.

Part: SKIN — CORRODED (RT WING)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7606 RIGHT WING. INSTALLED REPAIR PER SRM 57-30-03, AND UPS ENGINEERING FILE NR 727-57-1091.

Part: STIFFENER — CORRODED (BS 747)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BREATHER WEB AND STIFFENER ABOVE DELTA BEAM BL 0, WL165, BS 747. INSTALLED REPAIR PER SRM 51-40-02, 51-30-02, MM 20-10-05.

Part: STRINGER — CORRODED (BS 996-1130)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6L, STA 996-1130. INSTALLED REPAIR PER SRM 53-10-03, 53-10-01, 51-10-02, 51-20-151, 53-10-04.

Part: FLOORBEAM — CORRODED (BS 921)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM BOTTOM CHORD AFT SIDE STA 921, WL 201. INSTALLED REPAIR PER UPS EO B727-5310-6692.

Part: EXPANSION LINK — CORRODED (BS 860)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AROUND BUSHINGS AT STA 860, LBL 25, WL 207. INSTALLED REPAIR PER SRM 51-10-01, 51-10-02, MM 51-20-151.

Part: FLOORBEAM — CORRODED (BS 312)

DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES IN FLOORBEAM STA 312, LBL 2, 18, AND 43, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6693A.

Part: SEAT TRACK — CORRODED (BS 953-1130)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGES STA 953 TO 1130 RBL 61, WL 208. INSTALLED REPAIR PER SRM 53-10-01, 53-10-05, 51-30-02, 51-10-02, MM 51-20-151.

Part: WINDOW POST — CRACKED (FLIGHT DECK)

DURING D-CHECK, MAINTENANCE FOUND CRACK UNDER REPAIR IN E TO F WINDOW POST. THE RIGHT SIDE, IS NOT CONTAINED BY STOP DRILL OR RIVET HOLE. CRACK IS BETWEEN THE 1ST AND 2ND SCREW FROM THE BOTTOM OF THE NR 3 WINDOW. REPAIRED PER UPS EO B727-5310-0012.

Part: STRINGER — CRACKED (BS 743)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON STRINGER 17R BS 743, RBL 70.5. INSTALLED REPAIR PER SRM 51-40-04.

Part: FLOORBEAM — CORRODED (BS 1030)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1030 RBL 0-65 LBL 0-65, WL 208. INSTALLED REPAIR PER UPS EO B272-5310-6711.

Part: FLOORBEAM — CORRODED (BS 1110)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1110 RBL 0-65 LBL 0-65, WL 208. INSTALLED REPAIR PER UPS EO B272-5310-6728.

Part: SEAT TRACK — CORRODED (BS 740)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGES STA 740, AND BARE ALUMINUM ON FLANGES STA 420-480 AND 500-540 LBL 25 WL 208. INSTALLED REPAIR PER SRM 53-10-01.

Part: SKIN — CORRODED (RT WING)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7607 RIGHT WING. INSTALLED REPAIR PER SRM 57-30-03.

Part: STRINGER — CORRODED (BS 682)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 26L BS 682, LBL 23. INSTALLED REPAIR PER SRM 53-10-01, 53-10-2.

Part: STRINGER — CORRODED (BS 673)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 19R, BS 673, ON STRINGER SPLICE. INSTALLED REPAIR PER SRM 53-10-01, 53-10-2, 51-10-06, 51-01-02, 51-30-02, 53-10-03, MM 51-20-151.

Part: STRINGER — CORRODED (BS 970-1130)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2R, STA 500-520, 580-740. INSTALLED REPAIR PER SRM 51-10-06, 51-30-02, 51-10-02, 51-40-05, 53-10-01, 53-10-04, AND MM 51-20-151.

Part: EXPANSION LINK — CORRODED (BS 750)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK UNDER NUTPLATES AT STA 750, BL 0, WL 207.5. INSTALLED REPAIR PER SRM 51-30-02, 53-10-01.

Part: SEAT TRACK — CORRODED (BS 990)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK COUNTER SINKS, STA 990, LBL 45, WL 208. INSTALLED REPAIR PER SRM 51-30-08, 51-10-02, 53-10-05.

Part: SHEAR TIE — CORRODED (BS 680)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE AND FAIL-SAFE STRAP BS 680, STR 19R. INSTALLED REPAIR PER SRM 51-10-02, 51-30-05, 51-20-04.

Part: FLOORBEAM — CORRODED (BS 540)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 540 RBL 10 LBL 7, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6726A.

Part: FLOORBEAM — CORRODED (BS 600)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 600 RBL 45-65 LBL 10-56 WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6714A.

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

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON END OF HAT CHANNEL STA 304-344, RBL 13, WL 208. INSTALLED REPAIR PER SRM 51-30-02, 51-01-02, 51-10-06, 51-20-01, MM 51-20-31.

Part: SKIN — CORRODED (RT WING)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7608 RIGHT WING. INSTALLED REPAIR PER UPS ENGINEERING FILE 727-57-1091.

Part: INTERCOSTAL — CORRODED (BS 314)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON AFT FLANGE OF INTERCOSTAL STA 314, RBL 17 TO 40, WL 208. INSTALLED REPAIR PER SRM 51-10-01, 51-10-02, 51-30-01, MM 51-20-151.

Part: SEAT TRACK — CORRODED (BS 485)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK SPLICE, STA 485, LBL 44, WL 208. INSTALLED REPAIR PER SRM 51-30-02, 51-10-02.

Part: FLOORBEAM — CORRODED (BS 1090)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1090 LBL 45-65 WL 208. INSTALLED REPAIR PER UPS ENGINEERING FILE NR B727-53-1484.

Part: FLOORBEAM — CORRODED (BS 680)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 680 LBL 38-51 RBL 45-65, WL 208. INSTALLED REPAIR PER SRM 53-10-08.

Part: FLOORBEAM — CORRODED (BS 640)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 640 RBL 60-63 LBL 45 RBL 25, LBL 48 ON BOTTOM OF UPPER CHORD. INSTALLED REPAIR PER UPS EO B727-5310-6712A.

Part: STRINGER — CORRODED (BS 670-740)

DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3L, STA 670-740. INSTALLED REPAIR PER SRM 53-10-03, 51-30-02.

Part: INTERCOSTAL — CRACKED (BS 219-227)

DURING "C" CHECK MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 219-227, RBL 240-243.5, WL 227. REPLACED PER MM 51-20-151, SRM 51-30-02, 51-10-02.

Part: G BEAM — CORRODED (BS 256)

DURING "C" CHECK MAINTENANCE FOUND CORR ON G-BEAM STA 256, LBL 13, RBL 25, WL 208. REPLACED PER SRM 51-30-02, 51-10-01.

Part: FRAME — CRACKED (BS 294.5)

DURING "C" CHECK MAINTENANCE FOUND CRACK ON FRAME AT STA 294.5 WL 255 AT STR 10L. REPLACED PER SRM 51-10-01, 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 259.5-277)

DURING "C" CHECK MAINTENANCE FOUND CORR ON INTERCOSTAL STA 259.5-277, LBL 13-15, WL 208. REPLACED PER SRM 51-10-20, MM 51-20-151.

Part: SKIN — DELAMINATED (LT TE FORE FLAP)

DURING "C" CHECK MAINTENANCE FOUND DELAMINATION ON LT I/B FORE FLAP 36 INCHES TO 54 INCHES FROM I/B END. REPLACED PER SRM 51-40-06, AND BOEING OHM 57-52-01.

Part: SPAR — CORRODED (VERT FIN)

DURING "C" CHECK MAINTENANCE FOUND CORR ON VERTICAL FIN, RT SIDE, MID SPAR CORRODED AND CHAFED AT AFT ATTACH POINT FOR ACCESS PNL 9602. INSTALLED REPAIR PER UPS EO 727-55-0277.

Part: SKIN — CORRODED (RT HORIZ STAB TE)

DURING "C" CHECK MAINTENANCE FOUND CORR. ON RT HORIZONTAL STAB UPPER T/E IN BAY NR 5 NEAR O/B END. REPLACED PER SRM 51-30-2, 55-10-06.

Part: BEAM — CRACKED (AFT CARGO DOOR)

DURING "C" CHECK MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 4 TRANSVERSE BEAM IN O/B RADIUS. REPAIRED PER SRM 51-10-01, 51-30-02, AND MM 52-31-53.

Part: STRINGER — CORRODED (BS 680-700)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 9R, STA 680-700. REPAIRED PER SRM 51-30-2, 53-10-3.

Part: STRINGERS — CRACKED (BS 294.5)

DURING "C" CHECK MAINTENANCE FOUND CRACKS ON STRINGERS 14 AND 15 LEFT AT BS 294.5. REPAIRED PER UPS EO 8727-5310-1259-F.

Part: SPAR — CORRODED (VERT FIN)

DURING "C" CHECK MAINTENANCE FOUND CORR ON LT VERT. FIN MID SPAR AT AFT ATTACH POINT FOR ACCESS PNL 9601 PANEL SUPPORT. REPAIRED PER UPS EO 727-55-0276.

Part: FORGING — CRACKED (BS 738)

DURING "C" CHECK MAINTENANCE FOUND 3 EACH CRACKS EXTENDING FROM PREVIOUS STOP DRILLS ON 740 FORGING BS 738, BELOW STR 20L ON FORGING FOOT. NDI FOUND 4 CRACKS AND REPAIRED PER SRM 51-10-1.

Part: FLOOR BEAM — CORRODED (FS 500)

DURING "C" CHECK MAINTENANCE FOUND CORR AROUND FLOOR BOARD HOLES IN FLOOR BEAM STA 500, RBL 10-45, WL 208. REPAIRED PER UPS ENGINEERING FILE 727-53-1490.

Part: FITTING — CORRODED (RT TE MID FLAP)

DURING "C" CHECK MAINTENANCE FOUND CORR. ON RT I/B MID FLAP I/B CARRIAGE FITTING BORE. REPLACED PER SRM 51-10-01.

Part: FITTING — CORRODED (LT TE MID FLAP)

DURING "C" CHECK MAINTENANCE FOUND CORR. ON LT I/B MID FLAP I/B CARRIAGE FITTING BORE. REPLACED PER SRM 51-10-01.

Part: RIB — WORN (RUDDER)

DURING "C" CHECK MAINTENANCE FOUND LOWER RUDDER, LOWER BULLNOSE CLOSURE RIB, WEB IS WORN THROUGH. REPLACED WEB PER SRM 55-10-01.

Part: SEAT TRACK — CORRODED (FS 414-480)

DURING "C" CHECK MAINTENANCE FOUND CORR ON SEAT TRACK FLANGE LBL 44, WL 208, STA 414-480, BOTTOM SIDE. REPAIRED PER SRM 51-30-2, 53-10-5, 51-10-2.

Part: STRINGER — CORRODED (BS 277-294)

DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 6L, STA 277-294, UPPER AND LWR FLANGE. REPLACED PER SRM 51-30-02, 51-10-02.

Part: TRIM TAB — CORRODED (RT AILERON)

DURING D-CHECK, MAINTENANCE FOUND CORR ON R/W, I/B AILERON TRIM TAB FWD O/B HINGE FITTING. REPAIRED PER SRM 51-30-2.

Part: STRINGER — CORRODED (BS 620-740)

DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 6L, BS 620-740. INSTALLED REPAIR PER SRM 53-10-3, 51-10-4.

Part: STRINGER — CORRODED (BS 630)

DURING D-CHECK, MAINTENANCE FOUND CORR UNDER STR CLIP, DIRECTLY UNDER STAND OFF ON STR 20R, BS 360, RBL 58. INSTALLED REPAIR PER SRM 51-20-4, 51-30-2.

Part: STRINGER — CORRODED (BS 380-460)

DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 2R, BS 380-460. INSTALLED REPAIR PER SRM 53-10-3, 53-10-4, 51-30-2, 52-13-95.

Part: RIB — CRACKED (NR 2 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 2 SLAT RIB IN FOOT RADIUS ON O/B SIDE OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1.

Part: RIB — CRACKED (NR 1 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 1 SLAT 3RD RIB FROM I/B END AT UPPER FWD FLANGE, COMMON TO UPPER SKIN. REPAIRED PER UPS EO 727-57-1083.

Part: RIB — CORRODED (NR 7 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT I/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT O/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1 AND UPS EO 727-57-1083.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT I/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1 AND UPS EO 727-57-1083.

Part: RIB — CRACKED (NR 1 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 1 SLAT 4TH RIB FROM I/B END AT UPPER FWD FLANGE, COMMON TO UPPER SKIN. REPAIRED PER UPS EO 727-57-1083.

Part: INTERCOSTAL — CORRODED (BS 259.5-277)

DURING D-CHECK, MAINTENANCE FOUND CORR ON INTERCOSTAL AROUND NUTPLATE HOLES BS 259.5-277, LBL13-15, WL208. REPAIRED PER SRM 53-10-01.

Part: CHORD — CORRODED (BS 219-227)

DURING D-CHECK, MAINTENANCE FOUND CORR STA 219-227, LBL 44, WL236, O/B CHORD. REPAIRED PER SRM 51-10-03, 51-30-02, MM 51-20-151.

Part: STRINGER — CORRODED (BS 673)

DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 18R, BS 673 ON STR SPLICE. INSTALLED REPAIR PER SRM 53-10-1, 53-10-2, 53-10-3, 51-10-2, 51-30-2, 51-20-151.

Part: FRAME — CORRODED (BS 440)

DURING D-CHECK, MAINTENANCE FOUND CORR ON FRAME BS 440, LBL 14-20, WL 155. INSTALLED REPAIR PER SRM 53-40-3, 51-20-21, 51-20-151.

Part: SKIN — CORRODED (BS 745)

DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 745, RBL 35, WL 208. REPAIRED PER UPS EO 727-57-1089.

Part: WEB — CORRODED (BS 1110)

DURING D-CHECK, MAINTENANCE FOUND CORR ON AFT DOOR CUT OUT FRAME WEB AT BS 1110, RBL 22. INSTALLED REPAIR PER SRM 51-40-2, 53-10-1, 51-30-2, 51-10-2, 51-20-4.

Part: SKIN — CORRODED (BS 758)

DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 758, RBL 66, WL 202. REPAIRED PER UPS EO 727-57-1089.

Part: SEAT TRACK — CORRODED (BS 847)

DURING D-CHECK, MAINTENANCE FOUND CORR ON SEAT TRACK FLANGE LBL 46, STA 847. INSTALLED REPAIR PER SRM 51-30-8.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT RIB, O/B SIDE OF I/B TRACK. INSTALLED REPAIR PER UPS EO 727-57-1083.

Part: FRAME — CRACKED (FWD CARGO DOOR)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON FWD CARGO DOOR, LWR FWD CORNER OF FRAME AT FWD CENTER GUIDE ROLLER BRACKET. REPAIRED PER SRM 51-10-01, 51-30-02.

Part: CLIP — CRACKED (BS 1148)

DURING D-CHECK, MAINTENANCE FOUND CRACK ON STRINGER CLIP AT BS 1148, RBL 48, WL 173. REPAIRED PER SRM.

Part: STRINGER — CORRODED (BS 370)

DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 22L, BS 370. INSTALLED REPAIR PER SRM 53-10-3, 51-40-3.

Part: ANGLE — CORRODED (BS 748-760)

DURING D-CHECK, MAINTENANCE FOUND CORR ON ANGLE AT BS 748-760, RBL 63, WL 203. INSTALLED REPAIR PER SRM 51-10-6, 51-30-2, 51-10-1, 51-10-2, MM 51-20-151.

Part: SKIN — CORRODED (BS 7817)

DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 817, LBL 50, WL 198. REPAIRED PER UPS EO 727-57-1089.

Part: FLAP — CORRODED (NR 3 LE FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP O/B LOWER BONDING JUMPER ATTACH POINT. REPLACED K-FLAP PER MM 51-30-8.

Part: ANGLE — CRACKED (NR 3 CARGO DR)

DURING 'C' CHECK, MAINTENANCE FOUND AFT CARGO DOOR NR 13 O/B L ANGLE CRACKED IN RADIUS AT AFT VERTICAL TIE. REPLACED ANGLE ON AFT VERTICAL TIE PER SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (FS 211.8-218.8)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 211.8-218.8, RBL 25, WL 193. REPLACED INTERCOSTAL PER SRM 51-20-1, 51-20-21, 51-30-2, 53-10-1.

Part: FRAME — CRACKED (FS 804)

DURING 'C' CHECK, MAINTENANCE FOUND CRACK IN STA 804 FRAME CHORD AT STR 13R. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-3, 51-10-2.

Part: INTERCOSTAL — CRACKED (FS 500)

DURING 'C' CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT BS 500, LBL 52, WL 172. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-30-2, 51-20-1, 53-10-2.

Part: INTERCOSTAL — CORRODED (FS 211.8-218.8)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 211.8-218.8, LBL 25, WL 193. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2.

Part: CLIP — CRACKED (FS 970)

DURING 'C' CHECK, MAINTENANCE FOUND CRACKED STR CLIP AT STA 970, STR9R, WL 270. REPLACED CLIP PER SRM 51-30-2.

Part: CHANNEL — CORRODED (FS 1140)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL AT STA 1140, LBL 25-65, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1, 51-30-5, 51-30-2.

Part: SKIN — CORRODED (RT TE FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND RT WING I/B AFT FLAP I/B 75 INCHES HAS CORROSION ON SKIN. REPAIRED AREA PER SRM 51-40-6.

Part: STRINGER — CORRODED (FS 297)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 3L AT STA 297. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-2, 53-10-3.

Part: LUG — CORRODED (NR 6 LE FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP I/B LUG CORRODED. REPLACED NR 6 K-FLAP PER MM 27-81-01.

Part: STRINGER — CORRODED (FS 509.5)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 22L AT BS 509.5, LBL 52. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2, 53-10-3, 53-10-1.

Part: STRINGER — CORRODED (FS 538)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 23, BS 538, LBL 46 OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3.

Part: CLIP — CRACKED (FS 380)

DURING 'C' CHECK, MAINTENANCE FOUND STRINGER 26L CLIP CRACKED AT BS 380. REPLACED CLIP PER SRM 51-20-4.

Part: ANGLE — CORRODED (FS 342)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND SCREW HOLES IN L ANGLE ON TOP OF HAT CHANNEL AT STA 342, RBL 25-45, RBL 25-45, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1, 51-20-1, 51-10-2, 51-10-2, 51-10-6, 53-10-1.

Part: SKIN — CORRODED (FS 1078/1080)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT STA 1078 AND STRAP STA 1080 ABOVE STR 10R, WL 262. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3.

Part: STRINGER — CORRODED (FS 740-870)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 1 AT STA 740-870, BL 0. REPLACED STRINGER PSR SRM 53-10-3, 53-10-4, 53-10-4.

Part: CLIP — CRACKED (FS 990)

DURING 'C' CHECK, MAINTENANCE FOUND CRACKED STR CLIP AT STA 990, STR 8R, WL 278. REPLACED CLIP PER SRM 51-30-2.

Part: SWITCH — REQ ADJUST (RT MLG DOOR)

PILOT REPORTED, RT MLG DOOR UNSAFE AFTER RETRACTION WHEN HANDLE IN OFF POSITION. RECYCLED GEAR. OPS NORMAL. ADJUSTED RT MLG DOOR WARNING SWITCH PER MM 32-62-11. OPS CHECKED LANDING GEAR DOOR WARNING PER MM 32-62-11. CHECKS GOOD.