N909UP

Part: PUMP — FAILED (HYD SYSTEM) · airframe 18,682 hrs · 11,549 cycles

WHITE AT CRUISE ALTITUDE OF 43000 LOST B SIDE HYDRULIC ENGINE PUMP, DIVERTED TO ICT. EMERGENCY DECLARED. REMOVED #2 HYDRAULIC PUMP P/N: 66166 S/N: A0517P AND INSTALLED OVERHAULED HYDRAULIC PUMP P/N: 66166 S/N: LG43P IAW CE750 AMM 29-10-02. THRUST TECH ACCESSORIES FAA FORM 8130-3, FORM TRACKING #103799, WORK ORDER #24176 CP163304, APPROVAL# OTBR527K, AND DATE 09/AUG/2024. COMPLIED WITH BLEEDING OF HYDRAULIC SYSTEM IAW CE750 AMM 12-10-15. OPS & LEAK CHECKED HYDRAULIC PUMP NO DEFECTS NOTED AT THIS TIME.

Part: SPEED BRAKE — FAULTED · airframe 17,394 hrs · 10,532 cycles

DURING DESCENT TO KASE WHEN SPEED BRAKES DEPLOYED THE AIRCRAFT EXPERIENCED AN COMMANDED ROLL TO THE RIGHT. WITH SPEED BRAKES RETRACTED AIRCRAFT LEVELED OUT. CREW DIVERTED TO TO KAPA AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. A MAINTENANCE INSPECTION OF THE SPEED BRAKES WAS ACCOMPLISHED. SPEED BRAKES LINKAGES/ROD ENDS WERE INSPECTED AND GROUND OPERATIONAL CHECK PERFORMED WITH NO DEFECTS NOTES. CREW STATED THEY WERE IN ICING CONDITION AT THE TIME AND THE OCCURRENCE MAY HAVE BEEN CAUSED BY ICING ON THE SPEED BRAKES. A SUCCESSFUL OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: OPTICAL SENSOR — DIRTY (TE FLAPS) · airframe 17,380 hrs · 10,825 cycles

ON APPROACH TO KTEB, FLAPS SELECTED FROM 0* TO 15*, FLAPS FAILED TO EXTEND. CREW FOLLOWED CHECKLIST. EMERGENCY WAS DECLARED, DIVERTED TO SWF AND 0* FLAP LANDING PERFORMED. LANDING WAS UNEVENTFUL. MAINTENANCE CLEANED THE FLAP CONTROL HANDLE OPTICAL SENSORS. GROUND OPERATIONAL CHECKS PERFORMED WITH NO DEFECTS NOTED. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOTOR — DEFECTIVE (TE FLAPS) · airframe 16,274 hrs · 10,153 cycles

SUPPLEMENTAL INFORMATION. ON APPROACH FLAP SELECTED TO 5 POSITION RESULTED IN 'FLAP FAIL' MESSAGE. SLATS EXTENDED AND FOLLOWED CHECKLIST. EXECUTED A MISSED APPROACH AND DIVERTED TO KDEN DUE TO LONGER RUNWAY FOR FLAPS FAIL LANDING. LANDING WAS UNEVENTFUL. MAINTENANCE ISOLATED THE DISCREPANCY TO A FAULTY FLAP POWER DRIVE UNIT. REPLACED SAME. GROUND OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — INTERMITTENT (TE FLAPS) · airframe 16,139 hrs · 10,087 cycles

AFTER TAKE-OFF DURING CLIMB "FLAPS FAIL" CAS MESSAGE RECEIVED. FLAPS AT '0*' AND SLATS RETRACTED. WOULD NOT RESET. EMERGENCY DECLARED AND DIVERTED TO KMEM. FOLLOWED CHECKLIST AND LANDED WITH FLAPS AT '0*'. MAINTENANCE REPLACED THE LEFT FLAP RESOLVER (POSITION SENSOR). GROUND OPERATIONAL CHECK COMPLIED WITH. NO DEFECTS NOTED. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT ASSEMBLIES AT CABIN ENTRY AND CREW ENTRY DOOR BATTERIES DEAD. RECHARGED BATTERIES, OPS CHECKS OKAY.

Part: LIGHT — INOPERATIVE (L1 DOOR)

INSPECTION TYPE:PFLT L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01, OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:IN CREW ENTRANCE DOOR EMERGENCY EXIT LIGHT WENT DIM SHORTLY AFTER TESTING LIGHTS. REPLACED BATTERIES WITH CHARGED UNITS. OPS CHECKED GOOD IAW MM 33-51-01 PG 104. P/N S106

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, OVERHEAD LIGHTS ABOVE CREW ENTRY DOOR INOP. REPLACED BATTERIES IAW 33-50-00. OPS CHECKS GOOD.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C CRACK IN MLG WEB BS 938 O/B AFT CORNER ADJACENT TO STR 18A LWR FASTENER ROW IN RT MLG WW CRACK DRESSED OUT AND NDT CONFIRMED REMOVAL SRM51-10-1 WEB REPAIRED IAW SRM 51-20-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C TAIL SKID LT LWR TENSION TIE REAR TERMINAL FITTING CRACKED. LT LWR TENSION TIE AFT FITTING REMOVED AND NEW ONE INSTALLED IAW DRAWING 65-25992.

Part: FRAME — DAMAGED (BS320 STR22R TO) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C FRAME DAMAGED AT BS 320 STR22R STR27R (HOLES DAMAGED) FRAME REPLACED IAW SRM 51-30-02 AND DRWG 65-18420

Part: BRACKET — CRACKED (FUSELAGE) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C CRACK ON EDGE OF FLOOR PANEL SUPPORT BRACKET AT STA 755 LBL 50. NEW BRACKET FITTED IAW SRM 51-30-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C CORROSION ON LAP S24R BS 295 CPCP NEAR REPAIR REQUIRED SKIN REPLACEMENT WHICH ENCOMPASSED THIS DAMAGE , SKIN REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C SUSPECT CRACK AT TAIL SKID COMPT, RT UPPER TENSION TIE END FITTING CRACK CONFIRMED BY NDT, FITTING REPLACED IAW DRAWING.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 57,251 hrs · 51,010 cycles

INSPECTION TYPE:C MAIN CARGO DOOR FWD AND AFT HINGES CRACKED. ON INVESTIGATION HINGES FOUND CORRODED BEYOND LIMITS, HINGES REPLACED IAW OHM 20-50-01

Part: STRINGER — CRACKED (BS 676) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, CRACKS FOUND AT 2 FASTENER HOLES AT PRESSURE DECK UPPER SURFACE AT BS 880 - 890 RBL 23. REPAIR CARRIED OUT IAW DRAWING 65-89360 & SRM 53-10-9 & SRM 51-30-2.

Part: FRAME — CRACKED (LT MLG DOOR) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE: C, LT MLG WING DOOR (OUTER HALF) O/B DOOR FRAME AFT CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 51-10-2 & SRM 51-40-3

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, DURING RECTIFICATION OF CORROSION BETWEEN TEAR STRAP SKIN AT BS 680 S6L, INDICATIONS OF SUSPECT CORROSION ALSO FOUND AT BS 660 S4L TO S3L AT TEAR STRAP. NEW TEAR STRAP INSTALLED IAW SRM 53-30-4.

Part: INTERCOSTAL — CRACKED (BS 830) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C CRACK ON INTERCOSTAL AT STR 17R AT BS 830 INTERCOSTAL REPLACED IAW SRM 51-30-1

Part: WEB — CORRODED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK AT BBL 15L. REPAIR CARRIED OUT IAW SRM 51-40-2.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, DURING NDT INSP OF RT MLG WHEEL WELL PRESSURE WEB CRACK WAS FOUND ON WEB AT BS 940 RBL 33 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-2 & DRAWING 659360.

Part: RIB — CRACKED (#6 SLAT) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C SUSPECT CRACK IN #6 SLAT RIB, O/B OF SLAT ACTUATOR DAMAGED RIB REPAIRED IAW SRM 57-30-3

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 580 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-10-6, SRM 53-30-3.

Part: WEB — CORRODED (BS 1183) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C CORROSION ON CABIN FLOOR WEB FWD OF BS 1183 BLK OF BBL 12R ***CPCP*** WEB REPLACED IAW SRM 51-10-01

Part: SKIN — CORRODED (STAB STA. 80) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPROX FWD OF REAR SPAR ***CPCP*** REPAIR CARRIED OUT IAW SRM 55-10-3

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, RT MLG SUPPORT ANGLE CORRODED AT PRESSURE DECK SURFACE 2 AREAS, RBL 23 BS 880 TO 882. RT MLG SUPPORT ANGLE REPLACED IAW SRM 51-40-4.

Part: SUPPORT BRACKET — CRACKED (BS 910) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C BS 910 FRAME FWD FLANGE LWR CORNER SUPPORT BRACKET CRACKED REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-2

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,145 hrs · 51,603 cycles

INSPECTION TYPE:C, SUSPECT CORROSION AT TEAR STRAP LOCATION BS 560 S4R TO S3R. REPAIR CARRIED OUT IAW SRM 51-30-2 & SRM 53-30-3.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT A/C ENTRANCE WILL NOT TEST. REPLACED BATTERIES.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT BATTERY DEAD R&R EMERGENCY LIGHT BATTERIES OPERATION CHECKS NORMAL

Part: FRAME — CORRODED (BS 300 - 306)

INSPECTION TYPE:C, RIGHT MID CHORD IS CORRODED BS 300-306 WL 170 RBL 18, ACCESS RT MID CHORD. INSTALLED NEW MID CHORD REPLACED ACCESSED STRUCTURE PER SRM.*

Part: SEAT TRACK — CORRODED (BS 577 - 591)

INSPECTION TYPE:C CORROSION IN FWD CARGO BAY ON SEAT TRACK IN 3 AREAS AT RBL 14 BS 577, BS 585, AND BS 591 ON UPPER AND LOWER SURFACE. REMOVED CORROSION FROM OUTBOARD FLANGE ROM BS 577 TO BS 593 RBL 14. REMOVED .020 FROM ORIG .070, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK FROM BS 545 TO BS 660. FABRICATED NEW SEAT TRACK AND INSTALLED ALL WORK DONE IAW SRM 53-10-1, SRM 53-10-5, SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 312)

INSPECTION TYPE:C WHILE WORKING CUST ID NR 113675 FOUND CORROSION ON SHEAR TIE AT BS 312 BELOW STR RT SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED SHEAR TIE WITH NEW ITEM PER SRM 51-40-2 AND 51-30-2.

Part: CONDUIT — DAMAGED (NR 2 ENGINE)

INSPECTION TYPE:MOD, NR 2 ENGINE FUEL SOV CONDUIT WAS DAMAGED AT FWD END AND WIRING INSULATOR WAS PEELED OFF. INSTALLED NEW CONDUIT PER EO 00-0148. INSTALLED NEW WIRE IAW MM 28-22-11.

Part: ANGLE — CORRODED (BS 949)

INSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/GANGLE AT BS 949, WL 198, LBL 39. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 51-30-2, 53-10-1 AND 51-30-5.

Part: ANGLE — CORRODED (BS 949)

INSPECTION TYPE:C CORROSION (C53-100-01.00-02) ON L/ANGLE AT BS 949, WL 198, LBL 29.5. REMOVED, FABRICATED AND INSTALLED NEW L ANGLE. WORK DONE IAW SRM'S 53-10-1, 51-30-5 AND 51-30-2.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE: N/A, EMERGENCY EXIT LIGHT FWD ENTRY DOOR INTERMIT (REPEAT ITEM). ACCOMPLISHED VOLTAGE CHECK IAW MM 33-50-01, OPS CHECK GOOD. REPLACED LIGHT MOUNT, DISCOVERED A POOR CONTACT.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT OVER FOWARD ENTRY DOOR COMES ON INTERMITTENLY WITH CORRESPONDING OVERHEAD PANEL SWITCH IN ARM POSITION. REMOVED AND REPLACED BATTERY PACK IN UNIT OVER FORWARD ENTRY DOOR. OPS CHECK NORMAL.

Part: SPAR — CRACKED (RT WING)

INSPECTION TYPE-N/A, RT WING REAR SPAR U-CHANNEL CRACKED BETWEEN LIGHTENING HOLES DIRECTLY OVER RT MAIN LANDING GEAR STRUT, (MARKED IN RED). REPAIRED CRACKED AREA AS PER EO B727-5720-10177-A, INSTALLED REPAIR DOUBLER.

Part: PITOT — CONTAMINATED (LT FUSELAGE)

LOST CAPTAINS AIRSPEED INDICATOR ON TAKEOFF ROLL CONTINUED TAKEOFF NOTICED STBY AIRSPEED INDICATOR INOP AT 10,000 FT, WINDSHEAR/GRD PRX CAME ON THROUGH 500 FT. AFTER TAKEOFF LOST EPR 3, 2, 1 ABOUT 10 SECONDS APART THROUGH 12,000. FOUND NUMEROUS WORMS AND WATER IN CAPT'S PITOT SYS, FLUSHED SYS WITH NITROGEN, ALL DEBRIS REMOVED. PERFORMED PITOT/STATIC TEST PER MM 34-12 -06 . SYS OPS CHK OK. REMOVED AND REPLACED NR 1 ADC PRECAUTIONARY DUE TO WATER IN PITOT LINE P/N ON AND OFF 503FAD1-1, S/N ON 1881 OFF 1702.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, INOP EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR. INSTALLED SERVICEABLE FWD ENTRY DOOR EMER EXIT LIGHT ASSY, BATTERIES TEST GOOD.

Part: SPAR CHORD — CORRODED (WING)

INSPECTION TYPE:SI, CENTER SECTION UPPER REAR CHORD HAS EVIDENCE OF CORROSION SEPARATED FROM WEB LBL 6-36 WL 190. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED REAR SPAR UPPER CHORD, SPLICE AND WEB ALL WORK DONE PER EWO NR 97-2109, UPS FILE NR 727-57-1820, EWO NR 97-2152, UPS FILE NR 727-57-1821.

Part: BEAM — DAMAGED (MLG)

INSPECTION TYPE-SI, WHILE WORKING CUST ID C57-581-04-30 DISCOVERED O/B HOLE ON MLG BEAM COMMON TO NR 4 FLAP TRACK O/B HOLE TO HAVE THE UPPER SURFACE DAMAGED. REPAIRED PER EWO 97-2153 AND ENGINEERING FILE NR 727-57-1817 UPS.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE-SI, CORROSION LT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO NR 97-2111, UPS FILE NR 727-55-0347.

Part: SILL — CORRODED (CARGO DOOR)

INSPECTION TYPE-SI, SSID (F-12) HFEC INSP OF UPPER SURFACE OF INNER SILL CHORD OF MAIN CARGO DOOR AT LBL 70 WL 208 BODY STATIONS 488, 501, 510 TO 520 525, 535, 550, 570, 580, 590 AND 600 EXHIBITS CORROSION INDICATIONS. REMOVED CORROSION FROM SILL AND INSTALLED REPAIR DOUBLER IAW EWO NR 97-2130 UNDER UPS FILE NR 727-53-1895.

Part: FRAME — CORRODED (RT EMER EXIT)

INSPECTION TYPE-SI, RT FWD EMERGENCY EXIT HAS CORROSION ON ITS HANDLE HOUSING. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — CORRODED (LT WING)

INSPECTION TYPE-SI, LEFT WING LOWER SKIN CORRODED AT FLAP TRACK ATTACH POINT. REPAIRED PER EWO 97-2100 AND UPS ENG FILE NR 727-57-1803.

Part: FRAME — CORRODED (LT EMRG EXT)

INSPECTION TYPE-SI, CORROSION AROUND HANDLE HOUSING ON LT AFT EMERGENCY EXIT. REMOVED CORRODED FRAME PROCURED NEW FRAME AND INSTALLED IAW SRM 51-30-2.

Part: SPAR CHORD — CHAFED (VERT STAB)

INSPECTION TYPE-SI, CORROSION RT FIN MID SPAR CHORD (S-7) IS CHAFED AND FRETTING AT FS 225.7. REPAIRED PER EWO 97-2111 AND UPS ENG FILE NR 727-55-0347.

Part: SKIN — CORRODED (WS 870)

INSPECTION TYPE-SI, WHILE WORKING CUST CARD NR 510847 FUSE 152 FOUND UPPER SIDE OF LOWER CENTER WING SKIN TO BE CORRODED AT STA 870 RBL 56. REMOVED CORROSION AND REWORKED SKIN IAW EWO 97-2132 UNDER FILE NR 727-57-1811.

Part: SUPPORT FTG — CORRODED (NR 11 SPOILER)

INSPECTION TYPE-SI, NR 11 SPOILER ACTUATOR FITTING LOWER MOUNT BOLT HOLES CORRODED. REMOVED AND REPLACED NR 11 SPOILER ACTUATOR SUPPORT FITTING IAW MM 27-51-131 MM 27-61-81 MM 27-61-01 AND SRM 51-30-2.

Part: FITTING — CRACKED (BS 950)

INSPECTION TYPE-SI, CRACK INDICATIONS ON RT 950 BODY FORGING FORWARD O/B FLANGE AFT ROW BETWEEN STR 10R AND 11R. REPAIRED RT 950 BODY FORGING PER UPS EO B727-5310-3012.

Part: ACTUATOR FTG — CORRODED (NR 4 SPOILER)

INSPECTION TYPE-SI, NR 4 SPOILER SUPPORT FITTING LOWER MOUNT HOLES CORRODED. REMOVED AND REPLACED NR 4 SPOILER ACTUATOR FITTING IAW MM 27-61-01, MM 27-51-131, MM 27-61-81 AND SRM 51-30-2.

Part: SPAR CHORD — CORRODED (WING)

INSPECTION TYPE-SI, WHILE WORKING CUSTOMER CARD 510847, FOUND THE LOWER CENTER SPAR CHORD TO BE CORRODED. REMOVED CORRODED SPAR CHORD PROCURED NEW SPAR CHORD AND INSTALLED IAW EWO 97-2136 UNDER FILE NR 727-57-1812.

Part: STIFFENER — CORRODED (REAR SPAR)

INSPECTION TYPE-SI, WHILE WORKING CUST CARD 510847 FOUND ALL STIFFENERS ON THE REAR SPAR WEB TO BE CORRODED. REMOVED CORRODED STIFFENERS, PROCURED NEW STIFFENERS AND INSTALLED IAW SRM 51-30-2.

Part: ACTUATOR FTG — CORRODED (NR 12 SPOILER)

INSPECTION TYPE-SI, NR 12 SPOILER ACTUATOR FITTING LOWER MOUNT BOLTS CORRODED. REMOVED NR 12 SPOILER FITTING FOUND TO BE OUT OF LIMITS. REPLACED NR 12 SPOILER FITTING PER MM 27-61-81.

Part: FRAME — CORRODED (BS 360)

INSPECTION TYPE-SI, CORROSION AT BS 360 FRAME ON FWD AND AFT SIDE LBL 27 BBL 0. REMOVED CORRODED WEB, PROCURED NEW WEB PART NR M7RC10740965-16318-63 AND INSTALLED PARTS SRM 53-10-4.

Part: FITTING — CORRODED (LT AILERON)

INSPECTION TYPE-SI, LT WING O/B AILERON I/B HINGE FITTING IS CORRODED AT ROD END LUG. CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED LUG, REPLACED PER SRM 51-30-2, OHM 57-50-11.

Part: SUPPORT — CORRODED (BS 277)

INSPECTION TYPE-SI, CORROSION ON FLOOR SUPPORT AT STA 277 TO STA 293 LBL 13 WL 208. REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW REPAIR PARTS, INSTALLED IAW SRM 51-20-1, 51-30-2.

Part: RIBS — CRACKED (NR 8 LE FLAP)

INSPECTION TYPE-SI, NR 8 SLAT HAS 2 CRACKS ON RIB AT SLAT STA 365.5. REMOVED AND REPLACED SLAT ASSY IAW MM 27-81-11.

Part: CASTING — CORROSION (RT WING/FUS)

INSPECTION TYPE: SI. R/W AFT BOTTLE PIN WING AND BODY FORGING BUSHINGS ARE WATER CONTAMINATED. REPAIRED R/W AFT BOTTLE PIN WING AND BODY FORGING PER SB 727-57- 0152 AND UPS SRM ADDENDUM B727-5710-1910D.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: SI. WHILE WORKING NRC 511244, FOUND CORROSION ON LOWER RUDDER LT SIDE EXTERIOR SKIN AT AFT EDGE OF BULLNOSE RUB STRIP AT BOTTOM END CAP. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED AND REPLACED SKIN PER SRM'S 55-40-1, 51-10-2, 51-30-2, MM 51-20-151.

Part: CASTING — CORROSION (LT WING/FUS)

INSPECTION TYPE: SI. L/W AFT BOTTLE PIN WING AND BODY FORGING BUSHINGS ARE WATER CONTAMINATED. REPAIRED L/W AFT BOTTLE PIN WING AND BODY FORGING PER SB 727-57-0152 AND UPS SRM ADDENDUM B727-5710-1910D.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: SI. WHILE WORKIING NRC 511244, FOUND CORROSION ON LOWER RUDDER R EXTERIOR SKIN AT TRAILING EDGE OF BULLNOSE RUB STRIP AT STA 82.2 TO STA 156.6. CORROSION REMOVAL ON SKIN WAS OUT OF LIMITS, REMOVED AND REPLACED SKIN PER SRM'S 55-40-1, 51-30-3, MM 51-20-71.

Part: SUPPORT — CORRODED (BS 338)

INSPECTION TYPE: SI. CORROSION AROUND NUTPLATE HOLES ON FLOORBOARD SUPPORT BS 338 RBL 15-59 WL 207. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED, FABRICATED REPLACEMENT PART. ALL WORK DONE PER SRM'S 53-10-1, 51-10-2, 51-20-4 51-30-2, MM 51-20-31.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: SI. WHILE WORKING NRC 511244, FOUND CORROSION ON LOWER RUDDER RT EXTERIOR SKIN AT AFT EDGE OF BULLNOSE RUB STRIP AT RT STA 105.6-120.7. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED AND REPLACED SKIN PER SRM'S 55-40-1, 51-30-2, 51-10-2.

Part: SEAT TRACK — CORRODED (BS 470-475)

INSPECTION TYPE: SI. CORROSION UNDER NUTPLATES AND ON SPLICE PLATES BS 470-475, RBL 45 WL 207 SEAT TRACK. CORROSION REMOVAL OUT OF LIMITS, REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW SECTION, INSTALLED PER SRM 53-10-1, 51-10-1.

Part: SKIN — CORRODED (BS 650)

INSPECTION TYPE: SI. CORROSION ON SKIN AT STA 650 ABOVE STR 4R. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK DONE PER SRM'S 53-30-1 53-30-3, 51-20-10.

Part: FLOOR BEAM — CORRODED (BS 640)

INSPECTION TYPE: SI. WHILE WORKING CUST ID 510935, FOUND CORROSION ON TOP FLANGE OF FLOOR BEAM AT BS 640 WL 208 BL ZERO-LBL 25. REMOVED CORRODED FLANGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE-SI, WHILE WORKING NRC NR 511244 FOUND CORROSION ON UPPER RUDDER RT SIDE EXTERIOR SKIN AT AFT EDGE OF BULLNOSE RUBSTRIP AT R STA 242.5 TO 257. REMOVED CORRODED RUBSTRIP, PROCURED NEW RUBSTRIP AND INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: FRAME — CRACKED (BS 277)

INSPECTION TYPE:SI, FOUND CRACK IN FRAME STA 277 RBL 56 WL 225. REMOVED CRACKED PARTS, FABRICATED NEW PARTS AND INSTALLED NEW PARTS IAW SRM 51-30-2, ON CARD NR 510588.

Part: FITTING — CORRODED (NR 2 FLAP TRACK)

INSPECTION TYPE:SI, CORROSION NR 2 FLAP TRACK FWD ATTACH FITTING HAS RUST AROUND BOLT HOLE. CORROSION REMOVAL EXCEEDED DESIGN LIMITS PER BOEING DWR NR 65-32734. REMOVED AND REPLACED NR 2 FLAP TRACK FWD ATTACH FITTING PER SRM 51-10-6, INSTALLATION DONE ON TC NR C57-581-04-3D.

Part: HAT CHANNEL — CORRODED (BS 300-344)

INSPECTION TYPE:SI, WHILE WORKING CUST CARD NR 511592 DISCOVERED HAT CHANNEL AT RBL 15 BS 300-344, TO BE CORRODED. REMOVED CORRODED CHANNEL, FABRICATED NEW CHANNEL AND INSTALLED NEW CHANNEL IAW SRM 53-10-1.

Part: FITTING — CORRODED (NR 1 FLAP TRACK)

INSPECTION TYPE:SI, CORROSION NR 1 FLAP TRACK FWD ATTACH FITTING HAS RUST AROUND BOLT HOLE. CORROSION REMOVAL EXCEEDED DESIGN LIMITS PER BOEING DWR NR 65-32734. REMOVED AND REPLACED NR 1 FLAP TRACK FWD ATTACH FITTING PER SRM 51-10-6, INSTALLATION DONE ON TC NR C57-581-04-3D.

Part: FRAME — CRACKED (BS 277)

INSPECTION TYPE:SI, CRACK IN FRAME AT STATION 277, RBL 56 WL 219. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLERS AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-2, 51-30-2.

Part: RIB — CRACKED (NR 2 LE SLAT)

INSPECTION TYPE:SI, RIB CHORD ON NR 2 SLAT, AT SLAT STATION 313.136. REMOVED DAMAGED PORTION OF RIB, PROCURED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, 57-50-3.

Part: SPOILER — DELAMINATION (NR 15)

INSPECTION TYPE:SI, NR 5 SPOILER HAS A 5 BY 5 AREA OF DELAMINATION ON UPPER SURFACE, FROM L/E AND 16 FROM INBD END. REMOVED DAMAGE AND REPAIRED AREA IAW SRM 57-50-6 AND SRM 51-40-6.

Part: STRINGER TIE — CORRODED (BS 950)

INSPECTION TYPE:SI, IN THE MAIN CARGO STRINGER 4 LT BS 950, TIE HAS AREAS OF CORROSION. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW 53-10-1, SRM 51-30-2.

Part: SPOILER — DELAMINATION (NR 6)

INSPECTION TYPE:SI, NR 6 SPOILER PANEL HAS 5 AREAS OF DELAMINATION 1 INCH BY 1 INCH, AND AN AREA OF DELAMINATION 6 INCH BY 8 INCH ON UPPER SURFACE. REMOVED DELAMINATION AND APPLIED REPAIR IAW SRM 57-50-6 AND MM 51-20-12.

Part: STRINGER — CRACKED (BS 743)

INSPECTION TYPE:SI, STRINGER 9 RT CRACKED AT BS 743. REMOVED CRACKED STRINGER SECTION, FABRICATED NEW STRINGER SECTION AND INSTALLED IAW SRM 51-30-2, 53-10-2.

Part: INTERCOSTAL — CRACKED (BS 1110-1130)

INSPECTION TYPE-SI, WHILE WORKIING TC NR 53-111-01-3C FOUND CRACKED INTERCOSTAL BS 1110 TO 1130, STR 25R AND MISSING FASTENERS AT BS 1110. REMOVED AND REPLACED INTERCOSTAL FROM BS 1110 TO 1130 STR 25R PER SRM 51-10-2, 51-30-2, 51-20-1.

Part: HINGE FITTING — CORRODED (LT AILERON)

INSPECTION TYPE:SI, L/W OUTBOARD AILERON, OUTBOARD CENTER WING SIDE HINGE FITTING, IS CORRODED AT NUTPLATE. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-30-2, 51-30-5.

Part: SPOILER — DISBONDED (NR 13)

INSPECTION TYPE:SI, NR 13 SPOILER X-RAY VIEW 1, 2, 3, 4 ,5, 6, HAS WATER ENTRAPMENT INDICATIONS NOTED. REPAIRED NR 13 SPOILER PER SRM 57-50-6.

Part: HINGE FITTING — CORRODED (LT AILERON)

INSPECTION TYPE:SI, L/W OUTBOARD AILERON, INBOARD CENTER WING SIDE HINGE FITTING, IS CORRODED AT NUTPLATE. REMOVED AND REPLACED HINGE FITTING IAW SRM 50-30-2, 51-30-5.

Part: SPOILER — DISBOND (NR 7 SPOILER)

INSPECTION TYPE-SI, NR 7 SPOILER X-RAY VIEWS 5, 6, 7, 8 HAS WATER ENTRAPMENT INDICATIONS NOTED. REMOVED DAMAGED AREAS, REPAIRED NR 7 SPOILER PER SRM 57-50-6.

Part: STRINGER — CORRODED (BS 351-360)

INSPECTION TYPE-SI, WHILE WORKING FUSE 129 (510824) FOUND STRINGER 25 RT STA 351 TO 360 TO BE CORRODED. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED STR 25 RT FROM STA 351 TO 360, FABRICATED NEW SECTION OF STRINGER, INSTALLED ALL WORK DONE PER SRM 51-10-2, 53-10-5, 53-10-3.

Part: STIFFENER — CORRODED (BS 320)

INSPECTION TYPE-SI, CORROSION, VERTICAL STIFFENER CORRODED AT BS 320 RBL 13 WL 170. CORROSION REMOVAL OUT OF LIMITS. REMOVED AND REPLACED VERTICAL STIFFENER AT BS 320 RBL 13 WL 170 PER SRM 51-10-6, 51-10-1, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-1020)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK AROUND NUT PLATE HOLES BS 870 TO 1020 LBL 65 WL 208. CORROSION REMOVAL OUT OF LIMITS. REMOVED SEAT TRACK SECTION FROM BS 8870 TO 1020 LBL 65 WL 208, FABRICATED NEW SECTION, INSTALLED ALL WORK IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-20-4.

Part: STIFFENER — CORRODED (BS 302)

INSPECTION TYPE-SI, CORROSION HORIZ STIFFENER CORRODED AT BS 302 RBL 11 WL 182. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED PART PER SRM 51-10-6, 51-10-1, 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 294.5-312)

INSPECTION TYPE-SI, CORROSION ON INTERCOSTAL AT BS 294.5-312 RBL 30 WL 207. CORROSION REMOVED WAS OUT OF LIMITS. REMOVED INTERCOSTAL, FABRICATED ANOTHER INTERCOSTAL, INSTALLED ALL WORK DONE IAW SRM 51-30-2, 53-10-1, 51-20-05.

Part: SPOILER — DISBOND (NR 11)

INSPECTION TYPE:SI, NR 11 SPOILER X-RAY VIEW 4, 5, 6, HAS WATER ENTRAPMENT INDICATIONS NOTED. REPAIRED NR 11 SPOILER PER SRM 57-50-6.

Part: SHEAR TIE — CRACKED (BS 488)

INSPECTION TYPE-SI, HFEC INSP EXHIBITS CRACK INDICATIONS IN RADIUS OF SHEAR TIE AT BS 488, 2 ABOVE STR 18 LT. REMOVED DAMAGED SHEAR TIE AT BS 488, STR 18 LT, FABRICATED NEW SHEAR TIE, INSTALLED PER SRM 53-10-4.

Part: STRINGER — CORRODED (BS 780-800)

INSPECTION TYPE-SI, CORROSION AND BARE METAL ON STR 3 LT STATION 780 TO 800. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-02.

Part: SEAT TRACK — CORRODED (BS 760-850)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK FROM STA 760 TO 850 LBL 25 WL 208 (MARKED). REMOVED AND REPLACED SEAT TRACK FROM 760 TO 850 LBL 25 WL 208 IAW SRM 51-30-2, 53-10-5, 51-30-8 AND 53 -10-1.

Part: RUDDER — CORRODED (RUDDER)

INSPECTION TYPE: SI. WHILE WORKING NRC 511244, FOUND CORROSION ON UPPER RUDDER LT SIDE EXTERIOR SKIN AT AFT EDGE OF BULLNOSE RUB STRIP AT R STA 220.8-242.1. FOUND CORROSION ON SKIN TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED AND REPLACED SKIN PER SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 344 LBL 65 WL 208. REMOVED AND REPLACED SEAT TRACK STA 344 LBL 65 WL 208 IAW SRM 51-30-5, 51-30-8, 51-10-2, 51-30-2 AND 53-10-1.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:SI, CORROSION ON UPPER CHORD OF STA 344 FLOORBEAM LBL 15 TO RBL 65 WL 208. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED UPPER CHORD AT LBL 10 TO RBL 65. REPLACED UPPER CHORD WITH NEW PART IAW SRM 53-10-8.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE: SI. WHILE WORKING 511244, FOUND CORROSION ON UPPER RUDDER R SIDE EXTERIOR SKIN AT AFT EDGE OF BULLNOSE AT RT STA 197.5 THROUGH 213.1. FOUND CORRODED SKIN TO BE OUT OF LIMITS PER SRM 51-20-1. REPLACED SKIN PER SRM 51-30-2.

Part: HINGE FITTING — CRACKED (AILERON)

INSPECTION TYPE-SI, O/B AILERON MIDDLE I/B HINGE FITTING CRACKED. HINGE FITTING REMOVED AND REPLACED WITH NEW FITTING PER SRM 51-30-2.

Part: SKIN — CORRODED (BS 582)

INSPECTION TYPE:SI, CORROSION ON SKIN STA 582 AND STA 587 ABOVE STR 4 RT. REMOVED CORROSION, FABRICATED REPAIR DOUBLERS AND INSTALLED REPAIR DOUBLERS AT STA 560 TO 600 IAW SRM 51-30-2, 51-10-2.

Part: SKIN — CORRODED (BS 670)

INSPECTION TYPE:SI, CORROSION ON SKIN AT STA 670 ABOVE STR 4R. REMOVED DAMAGED AREA CORRODED BEYOND LIMITS, FABRICATED REPAIR DOUBLER AND FILLER INSTALLED PER SRM 53-30-1, 53-30-3.

Part: SEAT TRACK — CORRODED (BS 600-620)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK FROM STA 600 TO 620 LBL 0. REMOVED CORRODED SECTION OF SEAT TRACK PROCURED NEW SECTION OF SEAT TRACK AND INSTALLED IAW SRM 51-30-2.

Part: FRAME — CORRODED (BS 351)

INSPECTION TYPE-SI, CORROSION ON FRAME AT BS 351 LBL 25-RBL 35 WL 145. REMOVED CORROSION FROM FRAME 3 BY 1.5 WITH 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED FRAME PER SRM 53 -10-1, 51-40-4.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 364 LBL 65 WL 208. SEAT TRACK SECTION REMOVED AND REPLACED WITH NEW SECTION IAW SRM 51-30-2, 51-30-5, 51-30-8.

Part: STRINGER — CRACKED (BS 818)

INSPECTION TYPE:SI, STR 7 LT CRACKED AT STA 818 (AREA MARKED). STOP DRILLED CRACK, NDT VERIFIED CRACK CONTAINED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-3.

Part: LIGHTS — INOPERATIVE (CREW ENTRANCE)

INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT OVER CREW ENTRANCE INOP. CLEANED CONNECTORS FOR BATTERIES, CKS OK.

Part: BATTERIES — DISCHARGED (COCKPIT)

INSPECTION TYPE: N/A. ROBBED EMERGENCY EXIT LIGHT ASSEMBLY FROM OVER COCKPIT DOOR AND CREW ENTRY DOOR NOTE: DEAD BATTERIES ON REQ. NR A452588. REPLACED BATTERIES ON COCKPIT EMERGENCY LIGHT ASSEMBLY. REINSTALLED, OPS CHECK GOOD. REPLACED BATTERIES ON CREW ENTRY, EMERGENCY LIGHT ASSY REINSTALLED, OPS CHECK GOOD. OK FOR SERVICE.

Part: RETRACT MECH — LACK OF LUBE (NLG)

SDF - ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. HANDLE HARDER TO MOVE THAN NORMAL. CHECKED OVER CENTER LINK AND LIBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECK TIME PER MM 32-32-00, WITHIN TIME LIMIT.

Part: RETRACT MECH — LACK OF LUBE (NLG)

SDF - CREW REPORTED ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. MAINTENANCE CHECKED OVER CENTER LINK AND LUBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECKED TIME PER MM 32-32-00, WITHIN TIME LIMIT.

Part: SKIN — CORROSION (RUDDER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER RUDDER SKIN ACCESS PANEL 9510. REMOVED CORROSION BY REMOVING BONDED SKIN, FABRICATED REPAIR PARTS AND FINAL INSTALLATION PER SRM 55-20-3.

Part: SKIN — CORRODED (BS 865-870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND UPON REMOVAL OF RBL 45 LONGITUDINAL BEAM, FUEL CELL UPPER SKIN TO BE CORRODED AT BS 865 TO 870, RBL 45 WL 178. BLENDED OUT CORROSION AND REPAIRED DOUBLER PER EO B727-5730-7514-A.

Part: STRINGER — CRACKED (BS 760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DURING PRESSURE LEAK OF FUEL VENT FOUND FORWARD VENT STRINGER WEB CRACKED AT LBL 26, STA 760 1 INCH LONG. REPAIRED PER UPS EO 727-57-1658.

Part: FRAME — CORRODED (BS 760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DISCOVERED CORROSION ON BS 760 FRAME WEB FWD SIDE LBL 70 WL 203. REMOVED CORROSION AND REPAIRED AREA PER EO B727-53-1691.

Part: SKIN — CRACKED (BS 265)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HFEC INSPECTION REVEALED CRACK INDICATIONS AT FASTNERS BS 264 AND 265, STRINGER 9 RT ON EXTERIOR SKIN. ACCESS THE DAMAGED AREA, CUTOUT AREA OF SKIN AND FABRICATED REPAIR PARTS. INSTALLED REPAIR PART AND REINSTALLED ITEMS REMOVED FOR ACCESS IAW SRM 53-30-3.

Part: SKIN — CORRODED (BS 775-785)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 775 TO 785 RBL 64. CUT OUT CORRODED SECTION OF FUEL CELL SKIN AND REPAIRED PER EO B727-5730-7507-A.

Part: SKIN — CORRODED (BS 770-800)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 770 TO 800, LBL 64. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. CUT OUT CORRODED SKIN AND REPAIRED PER EO B727-5730-7506-A.

Part: DOUBLED — CRACKED (BS 639)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MID GALLEY DOOR CUTOUT DOUBLER IS CRACKED AT BS 639.0 WL 274.25. STOP DRILLED CRACK, INSTALLED DOUBLER IAW EO B727-5330-2685.

Part: BALL NUT — WORN (LT TE FLAP)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT INBOARD TRAILING EDGE FLAP INBOARD JACKSCREW BALL NUT WORN. REMOVED AND REPLACED JACKSCREW ASSY PER OHM 27-54-04.

Part: SKIN — DELAMINATED (NR 8 SPOILER)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND NR 8 SPOILER HAS AN AREA OF 7 INCHES BY 7 INCHES DELAMINATED ON INBOARD FWD CORNER AND AREA 8 INCHES BY 8 INCHES DELAMINATED ON FWD OUTBOARD CORNER, BOTH ON UPPER SURFACE. REMOVED DAMAGED SKIN, VERIFIED DAMAGE REMOVAL, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-6.

Part: FLOOR BEAM — CORRODED (BS 344)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CENTER OF STA 344 FLOOR BEAM CORRODED AROUND FASTENER HOLES WHILE WORKING CARD 376276. REMOVED CORRODED PORTION OF FLOOR BEAM THAT WAS PREVIOUSLY REPLACED. FABRICATED REPLACEMENT BEAM PER SRM 53-10-2 AND 53-10-1. INSTALLED REPAIR PARTS PER SRM 51-10-2.

Part: FRAME — CRACKED (BS 805)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE WORKING NRC 376230, CRACK ON FRAME AT STA 805 RBL 66-70, WL 210. REPLACED FRAME SEGMENT PER SRM 51-30-2, 51-10-2, 51-20-1.

Part: ATTACH LUG — CORRODED (NR 6 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE HAS CORROSION AROUND LWR FASTENER HOLE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY. ARM ADDENDUM 727-5750-5542, 51-30-2, MM 27-81-01, 27-81-00.

Part: ATTACH LUG — CORRODED (NR 5 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE IS CORRODED AT BOTH FASTENER HOLES. REMOVED AND REPLACED K-FLAP ASSY PER MM 27-81-01, 27-81-00, E.O. B727-5750-5542.

Part: ANGLE — CRACKED (NR 2 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP ACT. ATTACH FITTING ON ACFT SIDE CRACKED AT INBD UPPER ANGLE. REMOVED AND REPLACED UPPER LT ANGLE ON NR 2 K-FLAP SUPPORT PER SRM 57-40-00 AND 51-30-2.

Part: ANGLE — CRACKED (CARGO DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ANGLE CRACKED FOR AFT HINGE INTERCOSTAL ON AFT CARGO DOOR. REMOVED DAMAGED ANGLE, INSTALLED NEW WEB AND ANGLE PER SRM 51-30-2, DWG 65-18625, SRM 51-40-01.

Part: ANGLE — CRACKED (WS 198)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED ATTACH ANGLE AT WS 198.0 ON THE UPPER REAR SPAR CHORD, RT SIDE. REMOVED DAMAGE ANGLE, FABED NEW PART AND INSTALLED. ALL WORK PER SRM 51-20-1, MM 27-51-00.

Part: BRACKET — CRACKED (WS 198)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED BRACKET AT WS 198.0 ON THE UPPER REAR SPAR CHORD LT SIDE. REMOVED DAMAGED BRACKET, FABED NEW ANGLE AND INSTALLED ALL PER SRM 51-20-1, MM 27-51-00.

Part: ATTACH LUG — CORRODED (NR 4 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 K-FLAP HAS PITTING CORROSION ON INBOARD ATTACH LUG OF BULLNOSE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY PER SRM 27-81-01, 27-81-00.

Part: CHECK VALVE — INOP (HYD SYS)

AFTER TAKEOFF, OIL FUMES APPEARED ON FLIGHT DECK. REMOVED AND REPLACED PNEUMATIC CHECK VALVES. RAN PACK. NO ODOR PRESENT.