N917FD

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 52,488 hrs · 24,839 cycles

DURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS CHECK GOOD.

Part: HINGE FITTING — CRACKED (BS 1640 S14L) · airframe 52,325 hrs · 24,721 cycles

DURING ROTO INSPECTION OF LH STA 1640 S-14L. A CRACK INDICATION WAS NOTED IN OUTBD UPPER HOLE AT 2 O'CLOCK (VIEW LOOKING AFT) REMOVED AND REPLACED WITH NEW HINGE FITTING #146N8762-17 AT STA 1640 LH IAW WITH EA F-5310-T0378328 PT1 FUSELAGE - MAINFRAME - STA 1640 S-14L - CRACK IN HINGE FITTING OF OUTBOARD HOLE. MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 52,325 hrs · 24,721 cycles

MAIN CABIN FLOORBOARD PANEL 232MJF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MJF ON VT MAE TRAVELER T24/1738386 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 52,325 hrs · 24,721 cycles

MAIN CABIN FLOORBOARD PANEL 251MUF DAMAGED. FABRICATED ZONE 250, 251MUF FLOORBOARD PANEL ON VT MAE TRAVELER T24/1738388 IAW DWG SRZ 25-005 REV "R" MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 52,325 hrs · 24,721 cycles

MAIN CABIN FLOORBOARD PANEL 252MUF BROKEN. FABRICATED ZONE 250 FLOORBOARD PANEL 252MUF ON VT MAE TRAVELER T24/1738390 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 52,325 hrs · 24,721 cycles

ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VT MAE TRAVELER # T24/1738161 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 52,325 hrs · 24,721 cycles

MAIN DECK FLOORBOARD PANEL 231MFF DAMAGED FABRICATED ZONE 230 FLOORBOARD PANEL 231MFF ON VT MAE TRAVELER # T24/1738381 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 52,325 hrs · 24,721 cycles

ZONE 220 COURRIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221BF ON VT MAE TRAVELER # T24/1738060 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 52,325 hrs · 24,721 cycles

ZONE 220 COURIER FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222MAF ON VT MAE TRAVELER # T24/1738162 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 52,325 hrs · 24,721 cycles

MAIN CABIN FLOORBOARD PANEL 231MEF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231MEF ON VT MAE TRAVELER # T24/1738374 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 52,124 hrs · 24,564 cycles

LOST CABIN PRESSURE DESCENDING THROUGH APPROX FL 280. RECEIVED CABIN ALTITUDE WARNING MESSAGE. CABIN ALTITUDE SHOWED 10,000 & CLIMBING AT 500 FT/MIN. EMERGENCY DECLARED & DESCENDED RAPIDLY TO 10,000 FT, NORMAL RATE TO 5,000. WHILE LEVEL AT 5,000 FT, CABIN ALTITUDE EVENTUALLY SHOWED 5,000 FT. FOR DURATION OF FLT, CABIN ALTITUDE MATCHED ACFT ALTITUDE & CABIN DESCENT RATE MATCHED ACFT DESCENT RATE. EXECESSIVE CABIN PRESSURE LEAK PERFORMED IAW AMM 05-51-24, FOUND DURING TEST EQUIP COOLING OVERBOARD EXHAUST VALVE FULLY CLOSED POSITION & NO HAVE LEAKS. ALSO TEST PERORMED IAW AMM 21-58-05-5 OK. R&R BOTH CABIN PRESSURE CONTROLLERS IAW AMM 21-31-02-4, R & R DIFFERENTIAL PRESSURE SENSOR IAW 21-33-04-4.

Part: MICROPHONE — FAULTED (N/A) · airframe 51,898 hrs · 24,399 cycles

LEFT RADIO TRANSMITS INTERMITTENTLY. WHEN ATC IS ABLE TO HEAR THE TRANSMISSION THEY REPORT ONLY BEING ABLE TO HEAR 3 BY 5. A LOUD STATIC ACCOMPANIES EVERY TRANSMISSION. REF. FRM FIM 23-12 FT 802 FOR VHF COMMUNICATIONS TRANSCEIVER BITE PROCEDURE / L VHF ANTENNA M245 IS ON TOP OF FUSELAGE. R&R LEFT VHF TRANSCEIVER AS PER AMM 23-12-01-4. TEST SATIS. A/C OK FOR SERVICE. REMOVED AND REPLACED CAPTAIN HAND MIC AS PER SMP. PERFORMED VHF COM SYSTEM TEST AS PER AMM 23-12-00-5-99. TEST SATIS. MEL CLOSED. A/C OK TO CONTINUE.

Part: METERING VALVE — FAILED (BRAKE SYSTEM) · airframe 51,635 hrs · 24,253 cycles

RT HYD QTY EICAS MESSAGE IN FLIGHT, FOLLOWED BY RT HYD ENGINE PUMP EICAS MESSAGE, FOLLOWED BY RT HYD SYS PRESS MESSAGE. EMERGENCY DECLARED. CHECKED BOTH ANTI-SKID SHUTTLE IAW AMM: 29-11-24-4. REMOVED RT HYD RESERVOIR PRESSURE RELIEF VALVE IAW MM 29-11-24-4, AMM: 32-42-07-4. REMOVED LT AND RT ANTISKID SHUTTLE VALVES MODULES IAW AMM 32-42-07-4. AMM 32-41-03-4-2. R & R RT BRAKE METERING VALVE IAW MM 32-41-03-4-2.

Part: SOCKET — FAILED (L1 DOOR) · airframe 51,311 hrs · 24,092 cycles

AT BLOCK IN THE SLIDE ARM LIGHT ON DOOR L1 IS BURNT OUT. SERVICED L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT WITH NEW BULB WITH NO HELP. TRIED WITH THE LENS & BULB HOLDER OF THE OTHER SIDE WITH NO HELP. CONFIRMED GOOD ADJUSTEMENT OF THE GIRT BAR & ITS ASSOCIATED PROX SWITCHES S10214 & S10215 IAW AMM 52-11-25-5. REPLACED LIGHT ASSY AND L1 SLIDE KORY SWITCH, TEST OK. ORIG SUB DATE: 9/6/2022

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FOUND DAMAGE ON FLOOR PANEL AT POS. 11RON STA 1300 RBL 55.00 SEE JOBCDID ON 53211717 PERFORMED PERMANENT REPAIR PER SRM 53-00-50-2R, PARAGRAPH 3.C,FIG/ 201. REV. 135.0. REPAIR MATERIAL P/N: BMS 8-301,CL. 2. B/N:0001285056. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 51,103 hrs · 23,957 cycles

FOUND CORROSION ON SEAT TRACK RBL 24 BETWEEN STA 1520-1540 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52, FIG.201 REPAIR 1

Part: SKIN — NONE · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 16.5" DIMENSION 4.0"-4.3" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R. REF. SRM 53-80-01-2R. REV. 135.0. MAJOR REPAIR

Part: SKIN — NONE · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 RBL 16.5" DIMENSION 4.3"-4.2" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R.REV. 135.0. MAJOR REPAIR.

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

SUSPECTED REPAIR ON APU FIREWALL AT STA 1885.2 UPPER PART (APU SUPPORT STRUT L/H SIDE) THE REPAIR COMPLY WITH SRM 53-80-08-2R, NO DAMAGE OR DEVIATION NOTED, AND REPAIR EVALUATED PER EO F-5100-7-5001. MAJOR REPAIR

Part: NONE — NONE · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD FLAP OUTBD TRAILING EDGE LWR SKIN ADJACENT NO 5 SPOILER PERFORMED WORK STEPS PER EA 000710. MAJOR REPAIR.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 51,103 hrs · 23,957 cycles

FOUND DENT ON HORIZONTAL STABILAIZER R/H SIDE LWR SKIN , SIZE : D=0.0231" L=2.79" W=2.46" PERFORMED HOT BOND REPAIR PER SRM 51-70-10,REPAIR 4,REF. SRM 55-10-01-1A,FIG. 101,DETAIL I,TABLE I,NOTE I. REP. DIM. : 5.5".REP. LOC. :56" FROM I/B AND 3.5" FROM AUXILIARY SPAR. REV. 135.0 17/1/22. REPAIR MATERIAL P/N:BMS 5-129, B/N: 2015D. MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR ON APU FIRE WALL AT STA 1885.2 LWR PART THIS REPAIR COMPLY WITH SRM 53-80-08-2R, AND NO DAMAGE OR DEVIATIONS NOTED, AND REPAIR ASSESSMENT PERFORMED PER E.O F-5100-7-5001. MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REOAIR/SPLICE AT AFT CARGO STA 1540-1560 RBL 13 THIS REPAIR COMPLY WITH SRM 53-60-53-2R, NO DAMAGE OR DEVIATIONS NOTED, AND PERFORMED REPAIR ASSESSMENT PER E.O F-5100-7-5001. MAJOR REPAIR

Part: NONE — NONE (NONE) · airframe 51,103 hrs · 23,957 cycles

SUSPECTED REPAIR/SPLICE OUTER CREASE BEAM R/H STA 1400-1420 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.O # F-5310-T0368544, CREASE BEAM OUTBOARD CHORD, STA 1400-1420, S-17R, EXISTING UNAPPROVED REPAIR, PERMANENT REPAIR. MAJOR REPAIR

Part: SKIN — DENTED (ELEVATOR) · airframe 51,103 hrs · 23,957 cycles

FOUND DENT ON ELEVATOR R/H SIDE LWR SKIN , SIZE : D=0.0130" L=0.839" W=0.691" PERFORMED REPAIR PER SRM 51-70-17,REF. SRM 55-20-01-2R,FIG. 201,TABLE I.REV. 135.0,17/1/22.REP. DIM.:5,5". REP LOC.:17"FROM AFT EDGE AND AT ELEV STA 74. MATERIAL P/N: EA9390,B/N:JH1FAF7944. MAJOR REPAIR.

Part: SKIN — NONE · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 7" DIMENSION 4.5"-5.0" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R.REF. SRM 53-80-01-2R REV. 135.0. MAJOR REPAIR

Part: NONE — NONE · airframe 51,103 hrs · 23,957 cycles

UNDOCUMENTED EXISTING REPAIR ON L/H WING INBD MAIN FLAP LWR SKIN APPROX WS 231.5 PERFORMED WORK STEPS PER EA 000711

Part: NONE — NONE · airframe 51,103 hrs · 23,957 cycles

CABIN STA 680 FOUND CORROSION ON BEAM EXISTING REPAIR LBL22-RBL12 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368538, SECTION 43, FLOOR BEAM ASSY, STA 680, UPPER CHORD, LBL 25 TO RBL 12, CORROSION, REPAIR MAJOR REPAIR

Part: SEAT TRACK — CORRODED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 1320-1360 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 45.5 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52.FIG.201 REPAIR 1

Part: SEAT TRACK — GOUGED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN STA 582 FOUND DEEP GOUGE/CHAP MARK AT SEAT TRACK LBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368307, STA 440-680, LBL 45.5, SEAT TRACK, CROWN, MATERIAL LOSS, PERMANENT REPAIR. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 560-580 FOUND ELONGATED HOLE BL 0 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0368383, ELONGATED HOLE AT HORIZONTAL FLANGE OF SEAT TRACK AT BS 0 BETWEEN STA 560/580 FREEZE PLUG AND REPAIR STRAP INSTALLATION. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN STA 660 FOUND CORROSION ON SEAT TRACK LBL 58.22 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 1200-1240 FOUND 2 PLACES WONGATED HOLES ON SEAT TRACK RBL 24.75 DAMAGED SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED PER SRM 53-00-52-2R, REPAIR 3 AND SRM 51-40-02 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 1340-1380 FOUND SEVERAL CORROSION ON SEAT TRACK RBL 24.75 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52. FIG.201, REPAIR 1

Part: FLOORBEAM — CORRODED (BS 1200) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 1200 FOUND CORROSION ON BEAM BETWEEN RBL 3-RBL 19 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368550: SECTION 45, FLOOR BEAM ASSY, STA 1200, UPPER CHORD, RBL 3 TO RBL 19, CORROSION, REPAIR. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (N/A) · airframe 51,103 hrs · 23,957 cycles

CABIN BETWEEN STA 560-580 FOUND CORROSION ON SEAT TRACK RBL 24.7 PERFORMED SEAT TRACK REAPAIR PER SRM 53-00-52 2R, FIG.201 REPAIR 1 MAJOR REPAIR

Part: STRAP — CORRODED (CABIN) · airframe 51,103 hrs · 23,957 cycles

CABIN STA 1420 FOUND CORROSION ON INTERCOSTAL STRAP RBL 24.75 AND RBL 45.5 PERFORMED FLOOR BEAM REPAIR STABILIZATION STRAP PER SRM 53-00-51-2R, FIG.201 REPAIR 13 MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (CARGO) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL P.N 118662181-19 AT STA 680 NIR CARGO DOOR FOUND BROKEN PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARAGRAFH 3.D, FIG 201. REPAIR MATERIAL P/N: BMS8-301 CL-2. B/N: 0001285056. REV. 135.0. MAJOR REPAIR.

Part: TORQUE RING — CHAFED (NR 2 ENGINE DUCT) · airframe 51,103 hrs · 23,957 cycles

ENG NO 2 OUTBORD C-DUCT ON THE UPPER FWO SIDE THERE IS A BROKEN PIECE FROM THER PANEL PERFORMED REPAIR PER SRM 51-71-03, REF. SRM 54-30-70-2R, FIG. 201,DETAIL I,TABLE I. REP. DIM.:3.5" X 2". REP. LOC.: UPPER EDGE OF TORQUE RING,R/H. REV. 135.0. REPAIR MATERIAL P/N: EA9390, B/N: JH1FAF7944. MAJOR REPAIR.

Part: PANEL — CRACKED (NR 2 NACELLE) · airframe 51,103 hrs · 23,957 cycles

PYLON NO 2 THERE IS A CRACK ON PANEL NO 444DR FEO SIDE PERFORMED HOT BOND REPAIR PER SRM 51-70-04,REF. SRM 54-50-70-2R,FIG. 201,DETAIL I,TABLE I.REP. DIM.: 2,5" X 2,5",REP. LOC.:FWD BOTTOM EDGE. REV.135.0. 17/1/22. MATERIAL : BMS8-139,B/N:92M0073723. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (N/A) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL FOUND BROKEN AT STA 1715.45 PN 11864182-42 PERFORMED WET LAYUP REPAIR FOR MENTIONED FLOOR PANEL PER SRM 53-00-50-2R, PARGRAPH 3.D, FIG.201 REPAIR MATERIAL P/N: BMS 8-301 CL 2. B/N D001285056. REV.135.0. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 221BF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207.P/N: N917FD-N00308-221BF. B/N: 20353968. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 221MBF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00309-221MBF. B/N: 20353938. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL P.N 11861182-2 FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF ENGINEERING DISPOSITION OF RFTA NO: 02859-0207.P/N: N917FD-N00314-222MEF. B/N: 20354009. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 222MAF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207. P/N: N917FD-N00312-222MAF. B/N: 20353949. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 222AF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005.REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00311-222AF. B/N: 20353964. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 221AF FOUND WORN REPLACED FLOOR PANEL REP FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO:02859-0207. P/N: N917FD-N00310-221AF. B/N: 20353953. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 51,103 hrs · 23,957 cycles

FLOOR PANEL NO 222MDF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207. P/N: N917FD-N00313-222MDF. B/N:20354003. MAJOR REPAIR.

Part: SKIN — TORN (APU DOOR) · airframe 51,103 hrs · 23,957 cycles

APU INLET DOOR OUTBD LOWER EDGE IS BROKEN PERFORMED REPAIR PER SRM 53-80-31-2R,REPAIR 1,FIG. 201. MATERIAL P/N:EA9390 , B/N:JH1FAF7944. REV. 135.0. 17/1/22. REP. DIM.: 4" X 2". REP. LOC.: O/B LOWER FWD EDGE. MAJOR REPAIR.

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

EVALUATE REPLACED PART AT FRAME AT STA 231.25 BL-0 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368488, FRAME AT STA 231.5 BTWN LBL-20, RBL-20, REPLACEMENT OF NON SATISFACTORY FRAME REPAIR. MAJOR REPAIR

Part: NONE — NONE · airframe 51,103 hrs · 23,957 cycles

EVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 340 RBL-53-LBL-53 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0368523, FLOOR BEAM AT STA 345, BTW LBL 53 TO RBL 53, SRM REPAIR WITH MINOR DEVIATIONS MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

EVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 377 LBL-45 PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA# F-5310-T0368447: EXISTING REPAIR AT STA 377, BETWEEN RBL17 AND LBL 45, TRACKING MAJOR REPAIR

Part: NONE — NONE · airframe 51,103 hrs · 23,957 cycles

EVALUATE EXISTING REPAIR AT FRAME AT STA 1000 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-150687B, FRAME SPLICE REPAIR AT STA 1000 BETWEEN S-5L & S-5R. MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

EVALUATE EXISTING DOUBLER REPAIR AT FUSELAGE SKIN BETWEEN STA 1701-1720 STR 15L- 17L PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5330-T0368557, STA 1701-1720 S-15/S-16 L, EXISTING EXTERNAL REPAIR , DEVIATION FROM APPROVED DATA, TRACKING

Part: NONE — NONE (N/A) · airframe 51,103 hrs · 23,957 cycles

EVALUATE EXISTING REPAIR AT FRAME AT STA 1020 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA # F-5310-150688 B, EXISTING REPAIR AT FRAME STA 1020 B/T STR 5L -5R. MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 51,084 hrs · 23,948 cycles

PDIS 917 33-20 3360 05APR22 CDG FACT U LOGPAGES:3301983 LEFT MAIN CABIN DOOR SLIDE (L1 SLIDE) LIGHT NOT ILLUMINATED ONCE ARMED. FACT 05APR22 00:14 CDG RELAMPED PER AMM 33-24-00-2. OPS CHECK OK, A/C OK TO CONTINUE.

Part: NONE — NONE (N/A) · airframe 50,854 hrs · 23,721 cycles

PDIS 917 25-60 2831 19OCT21 MAN OPEN U R1 ARMED (SLIDE) LIGHT DOES NOT ILLUMINATE WHEN R1 DOOR IS MECHANICALLY ARMED MEL 19OCT21 20:14 MAN U RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 29OCT21 "MEL 25-66-05-A: R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VERIFY AND RECORD IN AML/EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE." R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP C/7290539 CLEAN AND REGREASE GIRT BAR AND FLOOR FITINGS IAW AMM 25-66-10-2. R1 SLIDE INDICATION TEST OK IAW AMM 25-66-00-0. MEL CLOSED. A/C OK FOR SERVICE.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 50,774 hrs · 23,638 cycles

EMERGENCY LIGHT DOOR 1L (SLIDE GND ILLUMINATION LT) INOP BULB REPLACED ACC AMM 33-51-06-2-1 REV 124.17. OPS TEST SATIS.

Part: TEST SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 50,355 hrs · 23,327 cycles

EMERGENCY LIGHT TEST SWITCH ABOVE DOOR 1L DOES NOT ILLUMINATE WHEN PUSHED AND EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN TEST SWITCH PUSHED. IDENTIFIED PARTS SWITCH ASSEMBLY. FOUND WIRE AT NO CONNECTION AT SWITCH S10292 LOOSE. RECONNECTED AND FUNCTION TESTED, IAW B757 AMM 33-51-00-5 SWITCH NOW OPERATES NORMALLY. A/C GOOD FOR SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 50,237 hrs · 23,186 cycles

AIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2. LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN. NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BLOCK 1 FOUND CABIN ALT PRESS CONTROLLER 2 INOPERABLE. PRESS/TEST FAILED TO ILLUM TEST INDICATION. REMOVED AND REPLACED CABIN ALT AUTO CONTROLLER 2, IAW AMM 21-31-02-4, OPS AND INDCATION NOW NORMAL. OK FOR SERVICE CABIN PRESS CONTROLLER MPN 2117388-6 S/N 94-A0753.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 50,237 hrs · 23,186 cycles

AIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2 . LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN . NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BOCK 1 FOUND CABIN ALT PRESS CONTROLLER 2 INOP. PRESS/TEST FAILED TO ILLUM TEST INDICATION. REMOVED AND REPLACED CABIN ALT AUTO CONTROLLER 2 IAW AMM 21-31-02-4, OPS AND INDCATION NOW NML. OK FOR SVC CABIN PRESS CONTROLLER MPN# 2117388-6 S/N# 94-A0753

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 50,074 hrs · 23,035 cycles

DOOR 4R FORWARD SCUFF PLATE CRACKED. WELD REPAIRED DOOR 4R FORWARD SCUFF PLATE IAW DRAWING NR SR57-53-003.

Part: ATTACH BRACKET — CRACKED (ZONE 400) · airframe 50,074 hrs · 23,035 cycles

LOOSE FASTENERS ON STRUT NR 2 AFT SAILBOAT FAIRING DIRECTLY ABOVE DRAIN TUBES FAIRING REMOVED IAW SRM 51-40-02 WORN FASTENER HOLES FOUND IN FAIRING SKIN AND SUPPORT STRUCTURE, FAIRING ATTACH BRACKET FOUND TO BE CRACKED. REPLACED AFT FAIRING SKIN, SUPPORT CHANNEL AND AFT FAIRING ATTACH BRACKET IAW SRM 51-40-02 BOEING DRAWING NUMBERS 313N5042 AND 313N5020.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 50,074 hrs · 23,035 cycles

AFT SCUFF PLATE ,AT DOOR 2R LOWER FUSELAGE SKIN CUTOUT CRACKED . SCUFF PLATE REMOVED IAW SRM 51-40-02. SCUFF PLATE REPAIRED IAW FEDEX REPAIR DRAWING SR57-53-003. SCUFF PLATE INSTALLED IAW SRM 51-40-02.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 50,074 hrs · 23,035 cycles

PYLON NO.1 AFT FAIRING CRACKED AT HEATSHIELD JUST ABOVE DRAIN OUTLETS CRACKED FAIRING REMOVED IAW SRM 51-40-02, OVERSIZED HOLES FOUND ON FAIRING SUPPORT STRUCTURE, REPAIR CARRIED OUT IAW FEDEX EA # F-5430-T0353727 P1 TITLE NACELLES / PYLON- SKIN/ PLATES / PANELS - PYLON #1 AFT FAIRING HEATSHIELD ATTACH STRUCTURE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

DUE TO FASTENER HOLE CORROSION DAMAGE, DOOR 4R UPPER FITTING PN 146N8761-16 REQUIRES REPLACEMENT. DOOR 4R UPPER FITTING PN 146N8761-16 REPLACED IAW DRAWING 146N8738, SRM 51-40-02 AND EA F-5310-T0354066 (P1) TITLE :FUSELAGE- MAINFRAME- DISCREPANT HOLES IN DOOR 4R UPPER HINGE FITTING.

Part: FRAME — CRACKED (FLAP TRACK) · airframe 50,074 hrs · 23,035 cycles

NR 6 AFT FLAP TRACK FAIRING 672CB HAS DAMAGE ON FORWARD OUTBOARD FRAME. REPLACED FRAME IAW SRM 51-40-02 AND DRAWING 113N1752 ALSO REFER TO EA F-5720-T0353885 TITLE: WING-SECONDRY WING STRCT- NR 6 AFT FLAP TRACK FAIRING FRAME.

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 50,074 hrs · 23,035 cycles

FWD CARGO COMPARTMENT FLOOR PANEL BSTA 820 LBL 10 HAS MINOR GOUGE EVALUATE FOUND OUTSIDE SRM LIMITS AND CARRIED OUT PERMANENT REPAIR ON FLOOR PANEL 12 121CF 11" FROM L/H SIDE AND 25.5" FROM AFT EDGE BSTA 820 LBL 10 IAW DRAWING SR57-53- 001 AND SRM 51-40-02 THIS IS A MINOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

CABIN FLOOR BOARD # 221MBF TOP LAYER DAMAGED REPAIRED FLOOR PANEL 221MBF IAW SRM 53-00-50 REV 129

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

CABIN FLOOR BOARD 221AF TOP LAYER DAMAGED REPAIRED FLOOR BOARD 221AF IAW SRM 53-00-50 REV 129

Part: BRACKET — CORRODED (RT MLG WW) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

EVIDENCE OF CORROSION ON AILERON CABLE GUIDE BRACKET IN R/H MLG WHEEL WELL FORWARD WALL OUTBOARD SIDE. .CABLE GUIDE BRACKET REPLACED IAW SRM 51-40-02 BOEING DRAWING NUMBERS 274N1048 AND 274N1055.

Part: RETAINER — CRACKED (CARGO BAY) · airframe 50,074 hrs · 23,035 cycles

TWO AREAS OF POSSIBLE CRACKS IN SEAL RETAINER FWD CARGO DOOR, CUTOUT LOWER CORNER AND 22" FROM LOWER AFT CORNER REPAIRED TWO AREAS ON FORWARD CARGO DOOR SEAL RETAINER IAW EA F-5340- T0353716 PT1. THIS IS A MINOR REPAIR

Part: SKIN — DENTED (FUSELAGE) · airframe 50,074 hrs · 23,035 cycles

DENT ON FUSELAGE SKIN AT BSTA 1691 BETWEEN STR 14-15 L/H EVALUATED DENT OF FUSELAGE SKIN BS1691 BETWEEN STR 14-15 L/H IAW SRM 53-00-01-1A AND FOUND TO BE OUTSIDE SRM LIMITS DUE TO PROXIMITY TO ADJACENT LAP JOINT. REFER TO FEDEX EA F-5330-T0353565 TITLE FUSELAGE- PLATES AND SKINS-DENT AT BSTA1691, 1.5" BELOW STR 14L/H FOR DENT LEAVE AS IS REPAIR.

Part: ATTACH BRACKET — CRACKED (NR 1 PYLON) · airframe 50,074 hrs · 23,035 cycles

PYLON #1 AFT FAIRING AFT HEATSHIELD ATTACH BRACKETS CRACKED REPLACED CRACKED BRACKETS IAW BOEING DRAWING # #313N052 AND SRM 51-40-02

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

UPPER DECK FLOOR PANEL DAMAGED BSTA 1681 LBL 60.20 REPAIRED UPPER DECK FLOOR PANEL IAW SRM 53-00-50 REV 129

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

FLOOR PANEL DAMAGED BSTA 1681 LBL 12" REPAIRED FLOOR PANEL IAW SRM 53-00-50 REV 129

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

FLOOR PANEL DAMAGED BSTA 1681 LBL 12" REPAIRED FLOOR PANLE IAW SRM 53-00-50 REV 129

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

EVIDENCE OF CORROSION ON FLOORBEAM UPPER SURFACE BS 365 RBL46 CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-51-1A. AREA REPAIRED IAW EA F-5310-T0353724.

Part: FILL PORT — CORRODED (LT WING) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

L/H OVERWING FILL PORT HAS EVIDENCE OF CORROSION REMOVED CORROSION AT L/H WING FILL PORT AREA IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 57-20-01-1A. REPAIRED L/H FILL PORT AREA IAW SRM 57-20-01 REPAIR 7 THIS IS A MAJOR REPAIR.

Part: FILL PORT — CORRODED (RT WING) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

R/H OVERWING FILL PORT HAS EVIDENCE OF CORROSION REMOVED CORROSION AT R/H WING FILL PORT AREA IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 57-20-01-1A REPAIRED R/H FILL PORT AREA IAW SRM 57-20-01 REPAIR 7 THIS IS A MAJOR REPAIR .

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

FLOOR PANEL AT BSTA 560-680 HAS LARGE DENT ON TOP SKIN REPAIRED FLOOR PANEL IAW SRM 53-00-50 REV 129

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,074 hrs · 23,035 cycles

FORWARD CABIN FLOOR BOARDS # 222 MAF, FOUND TOP LAYER OF BOARDS DAMAGES REPAIRED FLOOR PANEL 222MAF IAW SRM 53-00-50 REV 129

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

CORROSION @ ANGLE AFT OF BULK CARGO B/S 1715 RBL 25 STR 17 EVALUATED CORRODED STIFFENER ANGLE AT BS 1715 RBL 25 IAW SRM 53-60-51-1A AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER ANGLE AT BS 1715 RBL 25 IAW SRM 51-40-02 AND BOEING DRAWING # 146N5221.

Part: BULKHEAD — GOUGED (NLG WW) · airframe 50,074 hrs · 23,035 cycles

GOUGE FOUND ON NLG WHEEL WELL FWD BULKHEAD AT BS 263 NEAR BL0 DAMAGE REMOVED IAW SRM 53-10-08-1A AND FOUND TO BE OUTSIDE LIMITS, ORIGINAL MATERIAL THICKNESS .090" MATERIAL REMOVED 0.030" MAX ALLOWABLE 0.009". REPAIR CARRIED OUT IAW FEDEX EA # F-5330-T0353795 (P1) TITLE: FUSELAGE - PLATES & SKINS -FWD BULKHEAD AT BSTA 263 GOUGE DAMAGE.:

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

EVIDENCE OF CORROSION ON FLOORBEAM, UPPER CHORD, LOWER SURFACE, AT BS1681 RBL 24 ADJACENT TO ANCHOR NUTPLATE. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-51-1A. PREVIOUS UPPER CHORD REPLACEMENT REPLACED IAW EA F-5310-T0353625 P1 TITLE: FUSELAGE -MAINFRAME-CORROSION ON EXISTING REPAIR ON TOP CAP OF MAIN DECK FLOORBEAM AT BS 1681.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

CORROSION FOUND ON CABIN FLOOR SEAT TRACK @ BSTA 1180-1195 RBS 45.5 CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52- 1A. SEAT TRACK REPLACED FROM BS 1180 TO BS 1280 RBL 45.5 IAW SRM 51-40-02 AND BOEING DRAWING # 146N5130

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

SHEAR DECK STIFFENER AT BS1706 RBL 51.50 WL 208 CORRODED BEYOND LIMITS EVALUATED CORRODED STIFFENER ANGLE AT BS 1706 RBL 51.5 IAW SRM 53-60-51-1A AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER ANGLE AT BS 1706 RBL 51.5 IAW SRM 51-40-02 AND BOEING DRAWING # 146N5221.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

EVIDENCE OF CORROSION ON SHEAR DECK STIFFENER AT BS1715 BETWEEN RBL33 AND RBL 39 WL 208 REMOVED CORRODED SHEAR DECK STIFFENER AT BS 1715 RBL 33 TO RBL 39 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-60-51-1A. REPLACED STIFFENER IAW SRM 51-40-02.AND BOEING DRAWING # 146N5221

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,074 hrs · 23,035 cycles

EVIDENCE OF CORROSION ON SHEAR DECK STIFFENER AT BS1715 RBL10 - RBL16 WL208 REMOVED CORRODED STIFFENER AT BS 1715 RBL 10 - RBL 16 AND FOUND CORROSION TO BE BEYOND LIMITS IAW SRM 53-60-51-1A. STIFFENER REPLACED IAW SRM 51-40-02 AND BOEING DRAWING # 146N5221

Part: SLAT — CORRODED (LT WING) · airframe 50,074 hrs · 23,035 cycles

LT WING NR 1 LEADING EDGE SLAT HEAVILY CORRODED. REPLACED NR 1 LEADING EDGE SLAT IAW AMM 27-81-02 P/N OFF 114N4002-133 S/N OFF A1-0087 P/N ON 114N4002-153 S/N ON A1-0622 TAG NR 34G492.

Part: VALVE — LEAKING (BRAKE) · airframe 49,739 hrs · 22,767 cycles

STARTED BOTH ENGINES WITH BRAKES SET. ON SELECTION OF AFTER START FLAPS 5, MASTER CAUTION, R HYD SYS PRESS, R HYD RSVR PRESS, R HYD QTY HYD QTY L 0.94 - C 1.01 - R 0.0 RF HYD PRESS L 2910 - C 3110 - R 30

Part: VALVE — LEAKING (HYDRAULIC SYS) · airframe 49,739 hrs · 22,767 cycles

PDIS 917 29-30 0753 14OCT19 TLV OPEN U LOGPAGES:3025445 STARTED BOTH ENGINES WITH BRAKES SET. ON SELECTION OF AFTER START FLAPS 5, MASTER CAUTION, R HYD SYS PRESS, R HYD RSVR PRESS, R HYD QTY HYD QTY L 0.94 - C 1.01 - R 0.0 RF HYD PRESS L 2910 - C 3110 - R 30 THIS DISCREPANCY HAS BEEN ENTERED IN ERROR DISCREPANCY HAS BEEN REASSIGNED TO NEW ACN: 917 NEW ATA: 29-02 NEW NBR: 0000754 CHANGE ON : 14OCT19 20:28 INPT TRM 453617 FACT 14OCT19 20:28 MEM DUMMY FACT CREATED BY MCUAD

Part: SKIN — DAMAGED (LE SLAT) · airframe 49,478 hrs · 22,517 cycles

MDIS 917 57-50 0329 14MAY19 LGG OPEN U REF WRI: 0500/0327. DURING BIRD STRIKE INSPECTION, FOUND LT LEADING EDGE SLAT NR 5 DAMAGED. SLAT REQUIRES REPLACEMENT. R&R NR 5 LEADING EDGE SLAT IAW 27-81-01-4. OPS CHECK SATIS. A/C OK TO CONTINUE.

Part: RETAINER — CORRODED (BS 900) · corrosion level 2 · airframe 49,446 hrs · 22,480 cycles

EVIDENCE OF CORROSION ON RH MLG WHEEL WELL CUT OUT FWD EDGE SEAL RETAINER REMOVED CORROSION IAW SRM 51-10-02 REPAIRED AREA IAW E.A. # F-5350-T0346239 P1

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 49,298 hrs · 22,364 cycles

PDIS 917 22-10 0031 10JAN19 TLV OPEN U LOGPAGES:3019020 UNCOMMANDED NOSE DOWN. A/P CENTER, FL 210 PASSING FL 220, 4500 FPM RATE OF DESCENT, SPEED WINDOW CLOSED, NO A/P FAULT LIGHT. A/P DISCONECTED. VERY HEAVY YOKE ON PULL OUT MN. MEL 10JAN19 17:13 TLV U RELEASED FOR SERVICE PER MEL : 22-10-01-A CATEGORY : C EXPIRATION : 20JAN19 "MEL 22-10-01-A: __C___ (IDENTIFY L, C OR R) AUTOPILOT - INOP." A/C RELEASE IAW MEL 22-10-01-A : "C" AUTOPILOT - INOP CAT - C EXP. 22JAN2019 CTL NR 7170202 C/7170202 OPS CHECK ON FCC. & TEST 30 & 40 PER AMM 22-00-02-2.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,130 hrs · 22,204 cycles

DURING S-CHECK FOUND ON LT SIDE EMERGENCY EXIT LIGHTS AND OUTSIDE BEAM LAMP NOT ILLUMINATED DURING EMERGENCY LIGHT TEST AMM: TF-3350-T0338038 REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IN ACC WITH AMM 33-51-07-2. TEST FOUND OK

Part: ACTUATOR — WORN (NLG DOOR) · airframe 49,059 hrs · 22,133 cycles

ON TAKEOFF WE HAD 'GEAR DOORS' AND 'GEAR DISAGREE' EICAS AND AMBER 'DOORS' AND 'GEAR' LIGHTS ON GEAR PANEL. ALSO HAD ASSOCIATED NOISE THAT GEAR WAS NOT RETRACTING. ACCELERATING THROUGH 190KTS LIGHTS AND EICAS EXTINGUISHED. ON PREVIOUS LEG THE GEAR HAD TAKEN LONGER THAN NORMAL TO RETRACT BUT WE HAD RECEIVED NO WARNINGS OR LIGHTS. DURING LG INSPECTION, FOUND RIGHT GEAR DOOR ACTUATOR HEAD CONNECTION TO GEAR DOOR WITH UNACCEPTABLE PLAY. FOUND ALL FOUR DOOR BUSHINGS WORN. REMOVED AND REPLACED ALL FOUR BUSHINGS PER MM 32-12-01-4 AND 32-32-12-4. ALL TESTS OK REPLACED NOSE LANDING GEAR DOOR ACTUATOR IAW AMM 32-34-03-4 PERFORMED TEST SYSTEM OK.

Part: ACTUATOR — OBSTRUCTED (SPOILER) · airframe 48,868 hrs · 22,012 cycles

ON LANDING SPOILERS DID NOT DEPLOY AUTOMATICALLY FROM THE ARMED POSITION X. F/O MANUALLY DEPLOYED SPOILERS ON ROLL OUT X WE RECEIVED AN AUTO SPEED BRAKE EICAS MSG. DURING INSPECTION, FOUND A PIECE OF PAPER INSIDE AUTOSPEED BRAKE MECHANISM ACTUATOR. PAPER REMOVED AND OPS TEST OK.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 48,817 hrs · 21,981 cycles

MAIN CARGO FLOOR PANEL 251MWF DAMAGED.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 48,817 hrs · 21,981 cycles

MAIN CARGO FLOOR PANEL 251MVF DAMAGED.

Part: SKIN — DENTED (BS 1909) · airframe 48,817 hrs · 21,981 cycles

DENT FOUND ON THE FUSELAGE SKIN AT BS 1909.4, 1 O'CLOCK POSITION.

Part: SKIN — DENTED (BS 1913) · airframe 48,817 hrs · 21,981 cycles

FUSELAGE SKIN DENTED AT BS 1913.4, 11:30 O'CLOCK POSITION.

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 48,817 hrs · 21,981 cycles

CORROSION ON THE SEAT TRACK UPPER FLANGE AT BS 1640, LBL 45.5.

Part: GATE — CORRODED (L2 DOOR) · airframe 48,817 hrs · 21,981 cycles

L2 DOOR UPPER GATE HAS CORROSION ON THE LOWER EDGE.

Part: TRANSDUCER — OUT OF ADJUST (ELEVATOR) · airframe 48,804 hrs · 21,968 cycles

STICK SHAKER ACTIVATED WITH PITCH 30 DEGREES HIGH AND AIRSPEED AS LOW AS 93 KNOTS WITH CENTER AUTOPILOT ENGAGED DURING A GO AROUND, MCDP FAULTED LAST LEG. TROUBLESHOT IAW FIM 34-12 / FT813 FOR DIAGNOSTIC CODES 112080, 132080, AND 122080, ALL TESTED GOOD. TROUBLESHOT IAW FIM 22-20 FT838 FOR DIAGNOSTIC CODE 132440, BLOCK 73, TROUBLESHOT IAW FIM 22-02 FAULT TREE 838, BLOCK 73. FOUND THE LEFT ELEVATOR NEUTRAL SHFT TRANSDUCER OFFSET. ADJUSTED THE TRANSDUCER IAW AMM 22-12-04-4. PERFORMED AUTOLAND TEST 30 AND 40 IAW AMM 22-00-02-2. ALL TESTS PASSED.

Part: PANEL — MISSING (FUSELAGE) · airframe 48,484 hrs · 21,676 cycles

ON ARRIVAL, FOUND A PANEL MISSING AT THE RT OVERWING BODY BS 1147 - 1180. REPLACED THE PANEL IAW SRM 51-40-02.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 47,987 hrs · 21,259 cycles

DISAGREE ON DESCENT & APPROACH AFTER SELECTING ALT FLAPS 20 TEF EICAS RESOLVED, TWO MORE APPROACHES FLOWN WITH NORMAL FLAP OPERATION. FOUND NO RELATED EICAS MESSAGES FOR THIS FAULT, PERFORMED A READOUT OF EXISTING FAULTS AT FSEU NR 1 & 2, NO FAULTS RECORDED. NO FAULTS IN FLIGHT HISTORY FOR LAST LEG AT FSEU NR 1 & 2. PERFOMED TRAILING EDGE SYSTEM TEST ACC AMM 27-51-00-715-001 REV117.0. CYCLED FLAP/SLAT SYSTEM, FOUND NO BINDING OF SYTEM, FLAP/SLAT OPS GOOD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,472 hrs · 20,874 cycles

SEAT TRACK STATION 580, LBL 45.5, INBD SIDE FLANGE HAS A BROKEN AREA. R & R SEAT TRACK FROM STATION 440 - 680, LBL 45.50 IAW SRM 51-40-02, STA MOBLE 757-200SF & SRM 53-00-00.

Part: SHEAR TIE — CORRODED (BS 1440) · airframe 47,472 hrs · 20,874 cycles

AFT CARGO COMPARTMENT, BS 1440, RBL 22 UNDER TRANSITION PANEL, BRACKET ATTACHED TO INTERCOSTAL & TIE DOWN HAS CORROSION. R & R SHEAR TIE ATTACH BRACKET ON INTERCOSTAL IN AFT CARGO COMPARTMENT IAW SRM 51-40-02 & DWG 146N5421 REV A & B.

Part: ATTACH ANGLE — CORRODED (BS 1440) · airframe 47,472 hrs · 20,874 cycles

AFT CARGO COMPARTMENT, BS 1440 UNDER TRANSITION PANEL, INTERCOSTAL ATTACH ANGLE HAS CORROSION. R & R INTERCOSTAL ATTACH ANGLE AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 & DWG 146N8522 REV E.

Part: SKIN — DAMAGED (BS 490-491) · airframe 46,123 hrs · 19,843 cycles

LIGHTNING STRIKE LOWER FUSELAGE SKIN BS 490 - 491, STRINGER 27R. REPAIRED IAW EA F-5330-T0307177 PART 1.

Part: SKIN — DAMAGED (BS 418) · airframe 46,123 hrs · 19,843 cycles

LIGHTNING STRIKE ON LOWER FUSELAGE SKIN BS 418 STRINGER 25R, SIX INCHES ABOVE GROUND POWER RECEPTACLE. REPAIRED IAW EA F-5330-T0307106 PART 1.

Part: SKIN — DAMAGED (BS 669) · airframe 46,123 hrs · 19,843 cycles

LIGHTNING STRIKE LOWER FUSELAGE SKIN BS 669, 2.5 INCHES ABOVE STRINGER 28R. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01 FIG 201 REPAIR 15.

Part: SKIN — DAMAGED (BS 539) · airframe 46,123 hrs · 19,843 cycles

LIGHTNING STRIKE LOWER FUSELAGE SKIN BS 539, STRINGER 28R. REMOVED DAMAGE, FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01 FIG 201 REPAIR 15.

Part: SLIDER — DISLODGED (GIRT BAR) · airframe 46,073 hrs · 19,801 cycles

AT BLOCK OUT WHEN RAMP CLOSED R1 DOOR, DOOR WOULD NOT CLOSE. GIRT BAR FITTING HAS FALLEN OUT OF SLIDE & WAS FOUND ON DOOR SILL LEDGE. FOUND FWD SLIDER ON GIRT BAR HAD BECOME DISLODGED. RESET SLIDER & OPERATIONS CHECKED IAW 757 MM 25-66-10-2 GIRT BAR & FLOOR FITTINGS, CHECKED SATISFACTORY.

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 45,851 hrs · 19,649 cycles

ATTEMPTED TO RAISE GEAR AFTER TAKEOFF. GEAR FAILED TO RETRACT. RECEIVED A GEAR DISAGREE CAUTION EICAS AND GEAR DOORS WARNING EICAS. DOOR LIGHTS ON GEAR INDICATION PANEL ILLUMINATED. GEAR HANDLE LOWER AND REGAINED THREE GREEN ON AND DOORS LIGHT OUT. REMOVED & REPLACED NOSE GEAR ACTUATOR IAW MM 32-34-03-4. LEAK CHECK PERFORMED & FOUND SATISFACTORY, PERFORMED SEVERAL NOSE GEAR DOOR OPENING & CLOSING IN ORDER TO BLEED HYDRAULIC. NOW, FWD NOSE GEAR DOORS ARE FULLY OPENING. NOSE GEAR RETRACTION/EXTENSION COMPLIED WITH IAW MM 32-34-00-5. ALL TESTS PASSED.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 45,828 hrs · 19,628 cycles

EMERGENCY EXIT LIGHT BURNED OUT. R & R BULB IAW MM 33-51-00-2. ACFT OK FOR SERVICE.

Part: PLACARD — DISLODGED (PAX DOOR) · airframe 45,048 hrs · 18,952 cycles

LEFT ENTRY DOOR ESCAPE SLIDE ARMED, LEVER PLACARD MISSING, FOUND PLACARD INSIDE DOOR COVER, PLACARD INSTALLED.

Part: GIRT BAR — OUT OF ADJUST (PAX DOOR) · airframe 44,766 hrs · 18,687 cycles

LT MAIN ENRTY DOOR ARMING HANDLE WOULD NOT MOVE TO POSITIONED WITH NORMAL FORCE APPLIED. FOUND GIRT BAR NOT PROPERLY ALIGNED, ADJUSTED GIRT BAR IAW MM 25-60-00-0-0. ARMING FUNCTION IS OK. ARMING FUNCTION TESTED IAW MM 25-66-00-00-0. ALL CHECKED OK.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 44,740 hrs · 18,651 cycles

ON APPROACH, FLAPS SET AT 20; SELECTED FLAPS 25 & RECEIVED " T/E FLAP DISAGREE" EICAS MESSAGE. FLAPS WERE STUCK AT APPROX 21 WITH A SLIGHT SPLIT IN NEEDLES. DIVERTED. AT BLOCK IN STATUS MESSAGE " FLAP/SLAT ELEC". FOUND LT FLAP TRANSMITTER FAULTY. REPLACED LT FLAP TRANSMITTER. TEST GOOD, FINAL CLOSED.

Part: PROXIMITY SENSOR — INOPERATIVE (R1 DOOR GIRT BAR) · airframe 44,724 hrs · 18,632 cycles

SLIDE ARM LIGHT ON RT CREW ENTRY DOOR INOPERATIVE. GIRT BAR PROXIMITY SENSOR REPLACED IAW AMM 25-66-11. OPS TEST CARRIED OUT OK.

Part: COVER — OUT OF ADJUST (LIGHT SWITCH) · airframe 44,720 hrs · 18,628 cycles

EMERGENCY LIGHT DOES NOT OPERATE NORMALLY. EMERGENCY LIGHT SWITCH OPERATES NORMAL IAW MM 33-51-00-5-0, CONFIRMED EMERGENCY LIGHT FUNCTIONS FINE. AJUSTED IAW SWITCH COVER. ALL CHECKED OK.

Part: GIRT BAR — OUT OF ALIGNMENT (L1 DOOR) · airframe 44,720 hrs · 18,628 cycles

LEFT MAIN ENRTY DOOR ARMING HANDLE WOULD NOT MOVE TO ARM, POSITIONED WITH NORMAL FORCE APPLIED. FOUND GIRT BAR NOT PROPERLY ALIGNED, ADJUSTED GIRT BAR IAW MM 25-60-00-0-0. ARMING FUNCTION IS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,717 hrs · 18,626 cycles

RT CREW DOOR SLIDE LIGHT IS INOPERATIVE. RELAMPED AND PERFORMED OPS CHECKED IAW AMM 52-11-20-5-0.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,705 hrs · 18,615 cycles

DAMAGE FOUND ON SKIN PANEL 192AR APPROX RT BS 740-760. REWORKED ON EA F-5330-157912. NDT CARRIED OUT, NO DEFECTS APPARENT.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,705 hrs · 18,615 cycles

DAMAGE FOUND UNDER PANEL 196ER APPROX RT BS1300-1350 ON SKIN. REWORKED IAW EA F-5330-157914 . NDT PERFORMED, NO DEFECTS APPARENT.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,705 hrs · 18,615 cycles

DAMAGE FOUND UNDER WTB PANEL 192BR APPROX RT BS 760-820. . REWORKED ON EA F-5330-157912. NDT CARRIED OUT WITH NO DEFECTS APPARENT.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,705 hrs · 18,615 cycles

DAMAGE FOUND ON SKIN PANEL 195DL APPROX BS 1240-1300. REWORKED IAW EA F5330-157913 NDT INSPECTION CARRIED OUT, NO DEFECTS APPARENT.

Part: SKIN — CRACKED (LT WING) · airframe 44,705 hrs · 18,615 cycles

LEFT WING NR 1 SLAT INNER COVE PANEL CRACKED AT INBD TRACK FITTING LT WING NR 1 SLAT INNER COVE PANEL REPLACED, IAW DWG 114N4075 AND IAW SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 600) · airframe 44,705 hrs · 18,615 cycles

RT WING SLAT NR 10 INNER COVE SKIN CRACKED AT INBD TRACK FITTING. REPLACED IAW DWG 114N4075 AND IAW SRM 51-40-02.

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 44,705 hrs · 18,615 cycles

REAR SPAR AT LT AFT BOOST PUMP UPPER BONDING POINT CORRODED. REWORKED IAW ATTACHED EA F5700-157909. MINOR REPAIR.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 44,705 hrs · 18,615 cycles

RT WING CORROSION ON UPPER WING SKIN PANEL 1 T/E OVER HANG LOWER SURFACE. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01 PG103. AREA REWORKED IAW EA F-5700-157911 AND SRM 51-10-02.

Part: ATTACH BRACKET — CRACKED (ZONE 400) · airframe 44,705 hrs · 18,615 cycles

REVERSE FLOW CONTROLLER MOUNTING PLATE CRACKED, MOUNTING PLATE FABRICATED IAW DWG 312N5857.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,705 hrs · 18,615 cycles

LAP JOINT PITTING CORROSSION FOUND STARTING FROM BS 660 TO 760 STRINGER 19 RT. CORROSSION IS WITHIN .1 OF UPPER LAP JOINT SKIN. FOUND DURING EA F-5330-157904 PART 1 ITEM 1 SCRIB LINE INSPECTION. INSPECTION REPAIR C/OUT ON EA F-5330-157904.

Part: SHEAR TIE — CRACKED (BS 1300 S20-21R) · airframe 44,705 hrs · 18,615 cycles

SHEAR TIE AT BS 1300 S20-21R FOUND CRACKED. SHEAR TIE FABRICATED IAW DWG 140N2202 & INSTALLED IAW SRM 51-4

Part: SKIN — DETERIORATED (BS 1260-1300) · airframe 44,705 hrs · 18,615 cycles

RIGHT FUSELAGE SKIN AREA BELOW WING TO BODY FAIRING BS 1260-1300 HAS SURFACE FINSH DETERIORATION UNDER THE BEAD OF SEALANT.

Part: SKIN — BURNED (BS 350-365.25) · airframe 44,705 hrs · 18,615 cycles

LIGHTNING STRIKE FOUND BETWEEN FR 350 - 365.25 AT STRINGER 4L LOCATION. FASTENER REPLACED IAW SRM 53-00-01 SECTION 2 PARA 3. MINOR REPAIR.

Part: SKIN — CORRODED (ZONE 500) · airframe 44,705 hrs · 18,615 cycles

CORROSION ON LEFT WING DUCT L/E PANEL, CORROSION CLEANED AND FOUND TO BE MINIMAL AND TO BE WITHIN SRM LIMITS 57-41-01, AREA SURFACE FINISH RESTORED.

Part: SKIN — CORRODED (ZONE 500) · airframe 44,705 hrs · 18,615 cycles

CORROSION ON LEFT WING FIXED L/E CAVITY, FWD OF WING VALVE. CORROSION CLEANED AND FOUND TO BE MINIMAL AND WITHIN SRM LIMITS 57-41-01, AREA SURFACE FINISH RESTORED.

Part: SKIN — CORRODED (BS 761-764) · corrosion level 2 · airframe 44,705 hrs · 18,615 cycles

PITTING CORROSION FOUND AT BS 761-764, STRINGER 19R. REPAIRED IAW EA F-5330-157904.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,626 hrs · 18,536 cycles

DURING SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RT SLIDE LIGHT LAMP. REPLACED IAW AMM 33-51-06, REV 102.1.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 43,441 hrs · 17,745 cycles

DURING TEST OF EMERGENCY EXIT LIGHTS, THE LIGHTS ABOVE THE R-1 DOOR AND COCKPIT DOOR COME ON DIM FOR A FEW SECONDS AND THEN GO OUT. VERIFIED BATTERY DISCHARGED. HAD GOOD POWER, 28VDC, AT PIN 2 ON C/P D66 FOR CHARGER. SUSPECT BAD CHARGER. R & R CHARGER AND BATTERY PACK IAW AMM P TO F SUPPLEMENT 33-51-07. ALL OPS TEST GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 43,438 hrs · 17,743 cycles

ON PRE-DEPARTURE CHECK FOUND THE FLIGHT DECK COCKPIT DOOR EMERGENCY EXIT LIGHT TO BE INOP. R & R BATTERY PACK IAW AMM REF 33-51-00-5-0. OPS CK WAS NORMAL. PREMATURE REMOVAL/INSTALLATION. R & R BATTERY PACK IAW AMM REF 33-51-00-5-0, OPS CK WAS NORMAL.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 42,195 hrs · 17,019 cycles

RAMP CREW ATTEMPTED TO OPEN DOOR L1 WITH SLIDE ARMED, SLIDE FELL OUT OF DOOR. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 10OCT09 "MEL 52-11-01-A: L1 DOOR SLIDE - INOP. " PLACED SLIDE IN CREW LUGGAGE AREA. INSTALLED SLIDE COVER BACK ON DOOR. BLOCK OUT CALL. ITEM PLACED ON MEL. DOOR 1L SLIDE INOP. OUTSIDE DOOR HANDLE DOES NOT DISARM EMERGENCY SLIDE WHEN YOU OPEN THE L1 DOOR. PREFORM ADJ TEST OF THE OUTSIDE DOOR HANDLE DISARM FEATURE PER MM 52-11-20-5, DOOR HANDLE WHEN PULLED TO THE FULL OUT BUTTERFLY POSITION DISARMS THE DOOR SLIDE PROPERLY. PARTS UPDATE WILL NEED DOOR ASSIST RESEVOIR ASSY . HANDLE MECHANISM INSTALLED AND RII BUYBACK DONE UNDER WRI 52-10/0731. INSTALLED A NEW ESCAPE SLIDE AND EMERGENCY POWER RESERVOIR REF. AMM 757-52-11-30-4.

Part: FUEL/OIL COOLER — DIRTY (LT ENGINE) · airframe 42,193 hrs · 17,017 cycles

ON CLIMBOUT, LT ENGINE LOST POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. WHEN THROTTLE ADVANCED ENGINE ROLLED BACK. THRUST MANAGEMENT COMPUTOR BEGAN RECYCLING THROUGH CON, GA, TO MODES. CTR AUTOPILOT BECAME VERY SLUGGISH AND WOULD NOT RESPOND ENGINE, OK IN LOWER POWER BAND. REMOVED FUEL OIL COOLER AND DISASSEMBLED UNIT, FOUND LARGE AMOUNT OF DEBRIS ON THE INLET SIDE OF THE COOLER. INSPECTED TANKS FOR DEBRIS, FOUND FACE MASK IN O/B BAY OF LT CENTER HIP TANK MASK & FILTER DISINTERGRATED & CHARCOAL PARTICULATES SPILLING INTO TANKS.REMOVED MASK. FUEL COOLED OIL COOLERS, LP FUEL PUMPS, REPLACED ON BOTH ENGINES FUEL LINES INSPECTED, CLEANED/PURGED FUEL TANKS INSPECTED AND CLEANED

Part: SKIN — CORRODED (NR 8 SLAT) · airframe 42,045 hrs · 16,916 cycles

NR 8 L/E SLAT, L/E HAS (3) AREAS OD INTERGRANULAR CORROSION AT WS 548.50, 32" OF I/B EDGE; WS 537.50, APPROX. 43" OF O/B EDGE AND WS 459.50, APPROX. 32" O/B OF I/B EDGE. ACCOMPLISHED CORRSION REPAIR IAW EA F-5740-123985. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 42,045 hrs · 16,916 cycles

RIGHT LOWER WING T/E HAS CORROSION AT WBL 740- 806.5 REMOVED CORRODED PANEL SKIN IAW SRM 51-40-02. INSTALLED NEW PANEL SKIN RT WING LOWER SURFACE AT WBL 775.5-740. IAW SRM 51-40-02. CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1661-1681) · airframe 42,045 hrs · 16,916 cycles

FLOORBEAM AT BS 1661, REQUIRES REMOVE AND REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED WEB AT BS 1661-1681, AND FLOORBEAM BS 1661, LBL 63-RBL 63, IAW SRM 51-40-02. ANODIZED NEW FLOORBEAM PER DWG 146N5110. FABRICATED NEW FLOORBEAM PER DWG 146N5110. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-02. TREATED AND PRIMED NEW FLOORBEAM IAW SRM 51-20-01. PAINTED NEW FLOORBEAM IAW AMM 51-21-00-7. INSTALLED WEB, RBL 5, BS 1661-1681, AND NEW FLOORBEAM AT BS 1661, LBL 63-RBL 63, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT, A MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (BS 1681) · airframe 42,045 hrs · 16,916 cycles

CREASE BEAM HAS 2 DAMAGED HOLES, APPROX. BS 1681, RBL 60. FOUND DURING REMOVAL. AT BS 1681, RBL 57, CREASE BEAM INNER CHORD REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350449EZ2R03 AND MAE EA 757-5365-16-F2031, REV. A, DATED 05/06/2009. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. REPAIR IS CLASSIFIED AS A CAT. A MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1640-1681) · airframe 42,045 hrs · 16,916 cycles

FLOORBEAM AT BS 1640, REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED FLOORBEAM AND FASTENERS AT R4 AND L4 DOOR, S17L/R, BS 1640-1681, IAW SRM 51-40-02. ANODIZED NEW FLOORBEAM PER DWG 146N5110. FABRICATED NEW FLOORBEAM PER DWG 146N5110. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-05. TREATED AND PRIMED NEW FLOORBEAM IAW SRM 51-20-01. PAINTED NEW FLOORBEAM IAW AMM 51-21-00-7. INSTALLED NEW FLOORBEAM AND FASTENERS TO R4 AND L4 DOOR IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (BS1150-1210) · airframe 42,045 hrs · 16,916 cycles

WHILE REMOVING DELETED PARTS PER MAE STUB BEAM MOD, PRODUCTION FOUND NUMEROUS ELONGATED HOLES IN THE CREASE BEAM INNER CHORD AT BS 1180, RT, INCOMING CONDITION, FROM BS 1150-1210, AT RBL 63, CREASE BEAM INNER CHORD REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C NR 118350453CZ2R03 AND MAE EA 757-5341-16-F2029, REV NEW. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1320) · airframe 42,045 hrs · 16,916 cycles

FLOORBEAM AT BS 1320, RBL 24 -45, IS CORRODED ON UPPER CAP AT BS 1320, BETWEEN RBL 24 -45, FLOORBEAM REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C NR 118350519EZ2R01, AND MAE EA 757-5365-16-F1992, REV A, DATED 04/30/2009.

Part: FRAME — DAMAGED (BS 377) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 377 HAS NUMEROUS MISDRILLED HOLES BETWEEN S3L - S3R. INCOMING CONDITION. FRAME REPAIR WAS ACCOMPLISHED ON MAE W/C NR 118350395CZPR05 AND MAE EA 757-2550-16-F1953, REV A, DATED 04/23/2009. CLASSIFIED AS A CAT "A", MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1320) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 1320, HAS NUMEROUS MISDRILLED HOLES BETWEEN S-3L - S-3R. INCOMING CONDITION. FRAME REPAIR WAS ACCOMPLISHED ON MAE W/C NR 118350395CZPR05 AND MAE EA 757-2550-16-F1953, REV A, DATED, 04/23/2009. THIS NON-ROUTINE (N00962) IS FOR TRACKING PURPOSES ONLY. THIS REPAIR CLASSIFIED AS CAT "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1440) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 1440, HAS NUMEROUS MISDRILLED HOLES, S3L - S3R. INCOMING CONDITION. AT BS 1440, S3L - S3R, FRAME REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C NR 118350395CZPR05 AND MAE EA 757-2550-16-F1953, REV A, DATED 04/23/2009. THIS NON-ROUTINE (N00963) IS FOR TRACKING PURPOSES ONLY. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 760) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 760, HAS NUMEROUS MISDRILLED HOLES, S3L - S3R. FRAME REPAIR WAS ACCOMPLISHED ON MAE W/C NR 118350395CZPR05 AND MAE EA 757-2550-16-F1953, REV A, DATED 04/23/2009. CLASSIFIED AS A CAT A, MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 395) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 395, HAS NUMEROUS MISDRILLED HOLE , S3L - S3R. FRAME REPAIR WAS ACCOMPLISHED ON MAE W/C 118350395CZPR05 AND MAE EA 757-2550-16-F1953, REV A, DATED 04/23/2009. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME STA 1100, STR 3L-3R, HAVE MISDRILLED HOLES. CUT OUT DAMAGE FRAME SECTION IAW SRM 53-00-07. FABRICATED NEW FRAME SECTION MAE TRAV NR T9/787788, MAT 7075-0.080C, IAW SRM 53-40-07. INSTALLED FRAME SECTION STA 1100, STR 5L-5R, IAW SRM 53-00-07. REPAIR NR 1, CATEGORY A, MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 395) · airframe 42,045 hrs · 16,916 cycles

STA 395 STR 2R IS CRACKED. REMOVED DAMAGE IAW SRM 51-10-02 CUT-OUT DAMAGE STRINGER IAW SRM 53-0003 AT STA 395 STRINGER 2R, RECEIVED NEW CHANNEL ON MAE TRAVELER T9/ 788594 LOCATED AND DRILLED IAW SRM 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED FABRICATED HAT CHANNEL AND FILLER IAW SRM 53-00-03 REPAIR NR 1 AT STA 395 STRINGER 2R THIS IS AN "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: FRAME — MISALIGNED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME STA 1140, STR 3L-3R, HAVE MISDRILLED HOLES. CUT OUT DAMAGE IAW SRM 53-00-07. FABRICATED FRAME SECTION MAT- 7075-0.080C, IAW SRM 53-00-07. INSTALLED FRAME SECTION STA 1140, STR 5L-5R, IAW SRM 53-00-07. REPAIR NR 1, CATEGORY A, MAJOR REPAIR.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,045 hrs · 16,916 cycles

SHEAR DECK WEB FLANGE UPPER SURFACE HAS CORROSION STA 1681, BL0 - RBL58. REMOVED CORROSION, IAW SRM 51-10-02. FABRICATED DOUBLER REPAIR IAW SRM 53-60-51. INSTALLED DOUBLER REPAIR STA 1681, RBL30-RBL53, IAW SRM 53-60-51. REPAIR 2, CATEGORY A, MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME AT STA 980, HAS MISDRILLED HOLES BETWEEN STR 3L-3R. CUT OUT DAMAGE SECTION OF FRAME IAW SRM 53-00-07. FABRICATED NEW FRAME SECTION MAE TRAV NR T9/787791, MAT- 7075-0.090C, IAW SRM 53-40-07. INSTALLED FRAME SECTION, STA 980, STR 5L-5R, IAW SRM 53-00-07. REPAIR NR 1, CATEGORY A, MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME STA 1020, STR 3L-3R, HAS MISDRILLED HOLES. CUT OUT DAMAGE IAW SRM 53-00-07. FABRICATED FRAME SECTION MAE TRAV NR T9/787913, IAW SRM 51-40-05. INSTALLED ALL REPAIR PARTS STA 1020, STR 5L-5R, IAW SRM 53-00-07, REPAIR NR 1, CATEGORY A, MAJOR REPAIR.

Part: FRAME — MISALIGNED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME STA 1120, STR 3L-3R, HAVE MISDRILLED HOLES. CUT OUT DAMAGE FRAME SECTION IAW SRM 53-00-07. FABRICATED NEW FRAME SECTION MAE TRAV NR T9/787790, MAT- 7075-0.080C, IAW SRM 53-40-07. INSTALLED FRAME SECTION STA 1120, STR 5L-5R, IAW SRM 53-00-07. REPAIR NR 1, CATEGORY A, MAJOR REPAIR.

Part: FLANGE — CORRODED (SHEAR DECK) · airframe 42,045 hrs · 16,916 cycles

SHEAR DECK UPPER SURFACE FLANGE HAS SURFACE CORROSION STA 1681 BL0-LBL 52. REMOVED CORROSION IAW SRM 51-10-02 FOUND TO BE OUT AF LIMITS IAW SRM 53-60-51 L= 52.0 INCH, W= 3.0 INCH, D= 0.025 AT STA 1681 BL0- LBL 52. MADE REPAIR DOUBLER AND LOCATED AND DRILLED IAW SRM 53-60-51 REPAIR NR 2 FIG 201. TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-20-01. INSTALLED DOUBLER IAW SRM 51-40-02 AND 53-60-51. THIS IS A MAJOR REPAIR "A" REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: FRAME — DAMAGED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME AT STA 800 HAS NUMEROUS MISDRILLED HOLES BETWEEN STRG 3L AND 3R INCOMING CONDITION. CUT OUT DAMAGED FRAME SECTION ON STA 800 STR 5L TO 5R IAW SRM 53-00-07 FIG 201 SHEET 1 REPAIR 1. FABRICATE FRAME SECTION ON TRAVELER NR T9/ 787916. FABRICATED CHANNEL NR 1 ON TRAVELER NR T9/7878783, CHANNEL NR 2 ON TRAV NR T9 787884 LOCATED AND DRILLED HOLES ALL REPAIR PARTS IAW SRM 51-40-05. TREATED AND PRIMED ALL PARTS AND INSTALLED ALL REPAIR PARTS IAW SRM 53-00-07 FIG 201 REPAIR 1. THIS IS AN "A" CATEGORY REPAIR AT STA 800 BETWEEN STR 5L-5R MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: SUPPORT — DAMAGED (INTAKE DOOR) · airframe 42,045 hrs · 16,916 cycles

ANCHOR NUTS AT APU INTAKE DOOR CORRODED. REMOVED CORROSION AT ALL ATTACHMENTS POINTS, BS 1787-1825, S3R-6R IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-80-01/53-00-03 DET 2. REMOVED FWD STRAP AFT OUTER SPLICE STRAP, AFT INNER SPLICE STRAP, UPPER SUPPORT ANGLE & LOWER SUPPORT ANGLES IAW SRM 51-40-02. FABRICATED FWD STRAP, AFT SPLICE STRAPS, UPPER AND LOWER SUPPORT ANGLES, LOCATED & DRILLED ALL REPAIR PARTS IAW SRM 51-40-05. TREATED & PRIMED ALL REPAIR PARTS IAW SRM 51-20-01. INSTALLED FWD STRAP. INSTALLED UPPER AND LOWER SUPPORT ANGLES. INSTALLED UPPER & LOWER SUPPORT ANGLES, INSTALLED AFT INNER AND OUTER SPLICE STRAPS IAW SRM 51-40-02 THIS IS A CATEGORY "A" REPAIR.

Part: SKIN — DENTED (BS 700-720) · airframe 42,045 hrs · 16,916 cycles

PROTRUSION DENT AT BS 700-720, S-25R - S-26R. EVALUATED DENT ON EXT FUSELAGE SKIN; FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201. TRIMMED DAMAGED SKIN AND FABRICATED REPAIR DOUBLER. TREATED AND PRIMED REPAIR DOUBLER AND BARE METAL IAW SRM 51-20-01. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, FIG 201, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING: INITIAL INSPECTION AT 37,500 FC; THEREAFTER EVERY 6,000 FC WITH HFEC.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 42,045 hrs · 16,916 cycles

SKIN AT BS 700 STRINGERS 23-24L, MISREPAIRED. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201 REPAIR NR 3. CLASSIFIED AS CATEGORY "B" MAJOR REPAIR .

Part: FRAME — DAMAGED (BS 1460) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 1460, S-3L - S-3R, HAS MISDRILLED HOLES. CUTOUT BS 1460 FRAME FROM S-5L - S-5R, IAW SRM 51-10-02/SRM 53-00-07. RECEIVED NEW FRAME ON MAE TRAVELER NR T9/787915 AND 2 CHANNELS ON MAE TRAVELER NR'S T9/787899 AND T9/787890. LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-00-07. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-07, FIG 201, REPAIR NR 1 AT BS 1460, S-5L - S-5R. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: STRINGER — DAMAGED (BS410-440) · airframe 42,045 hrs · 16,916 cycles

BS 418, S-1, STRINGER IS DAMAGED. REMOVED DAMAGED STRINGER SECTION AT BS 410-440, S-1, IAW SRM 53-00-03, FIG 201, REPAIR NR 1. FABRICATED STRINGER SECTION ON MAE TRAVELER NR T9/788595, FABRICATED SPLICE HAT SECTION ON MAE TRAVELER NR T9/788594. LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-40-05. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED ALL REPAIR PARTS AT BS 410-440, S-1, IAW SRM 53-00-03, FIG 201, REPAIR NR 1/SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1360) · airframe 42,045 hrs · 16,916 cycles

3 MISDRILLED HOLES AT S-2R, BS 1360, ON FRAME. CUTOUT DAMAGED FRAME SECTION AT BS 1360, S5L-5R, IAW SRM 53-00-07, FIG 201, REPAIR NR 1. FABRICATED FRAME SECTION ON MAE TRAVELER NR T9/787917, FABRICATED CHANNEL NR 1 ON MAE TRAVELER NR T9/787881, FABRICATED CHANNEL NR 2 ON MAE TRAVELER NR T9/787882. LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 51-40-05. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED ALL REPAIR PARTS AT BS 1360, S-5L - S-5R, IAW SRM 53-00-07, FIG 201, REPAIR NR 1. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1340) · airframe 42,045 hrs · 16,916 cycles

FRAME, BS 1340, S-3L - S-3R, HAS MISDRILLED HOLES. CUTOUT DAMAGED FRAME SECTION, FROM BS 1340, S-5L - S-5R, IAW SRM 53-00-07, FIG 201. REPAIR NR 1, LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 51-40-02. TREATED AND PRIMED ALL REPAIR PARTS IAW SRM 51-20-01. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-07, REPAIR NR 1 AT BS 1340, S-5L - S-5R. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS1000 S4L-4R) · airframe 42,045 hrs · 16,916 cycles

FRAME AT BS 1000, FROM S-3L - S-3R, HAS MISDRILLED HOLES. CUTOUT DAMAGED AREA OF FRAME, BS 1000, BETWEEN S-4R - S-4L, IAW SRM 53-00-07. REMOVED STRINGER CLIPS ON S-4L AND S-4R IAW SRM 51-40-02. RECEIVED NEW FRAME ON MAE TRAVELER NR T9/787787 AND CHANNEL 1 AND 2 ON MAE TRAVELER NR T9/787799 AND T9/787798. LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 51-40-02. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED REPLACEMENT FRAME AND CHANNELS IAW SRM 53-00-07, REPAIR NR 1. THIS REPAIR IS CLASSIFIED AS A CAT "A", MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

L1 DOOR FWD OF BS 377.5 INTERCOSTAL HAS CORROSION AROUND NUTPLATES. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-10-15 PG 105 DETAIL VI. FOUND TO BE OUT OF LIMITS. REMOVED INTERCOSTAL IAW SRM 51-40-02. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

CORROSION ON FLOOR SUPPORT FS 333 RBL 2. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET III. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 42,045 hrs · 16,916 cycles

FUSELAGE LOWER LOBE FRAME AT BS 231.25, BL 0 GOUGED. GOUGE FOUND TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-07. REMOVED DAMAGE SECTION FOR REPAIR IAW SRM 51-40-02. INSTALLED NEW REPAIR PARTS IAW SRM 51-70-11. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FLOORBEAM HAS CORROSION AT BS 340 RBL 48 UNDER UPPER TEE. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED DAMAGED AREA. REPAIRED IAW SRM 53-00-51 FIG 201 REPAIR NR 3. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FORMED SECTION OF CABIN FLOOR SUPPORT CORRODED ON LOWER SURFACE UNDER NUTPLATES FS 350-365 RBL 46. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04 FIG 101 DETAIL LL. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FLOOR SUPPORT CORRODED ON LOWER SURFACE UNDER NUTPLATES BS 350-365 RBL 24. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04 FIG 101 DETAIL LL. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 440-640) · airframe 42,045 hrs · 16,916 cycles

SEAT TRACK AT BS 440, RBL 24.5, FLANGE IS WORN. CHECKED LIMITS OF SEAT TRACK AT BS 440, RBL 24.5, IAW SRM 53-00-52, DETAIL 7, FIG 101 AND FOUND TO BE OUT OF LIMITS; L=1 INCH, W=.5 INCH, D=.035 INCH. REMOVED SEAT TRACK AT BS 440-640, RBL 24.5, IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK BATCH NR 0001541987, 201 INCH LONG, IAW SRM 51-10-02. TRIMMED AND LOCATED HOLES IAW SRM 51-40-02. TREATED AND PRIMED IAW AMM 51-21-00-7. INSTALLED NEW SEAT TRACK FROM BS 440-640, RBL 24.5, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 365-418) · airframe 42,045 hrs · 16,916 cycles

BS 365-418, RBL 45, SEAT TRACK SUPPORT IS CORRODED. REMOVED AND REPLACED SEAT TRACK SUPPORT IAW SRM 51-40-02/53-00-52. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG 102; L=2.0", W=2.0", D= .028". THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 365-418) · airframe 42,045 hrs · 16,916 cycles

BS 365-418, RBL 24, SEAT TRACK IS CORRODED. REMOVED AND REPLACED SEAT TRACK SUPPORT, IAW SRM 51-40-02. NEW SEAT TRACK SUPPORT FABRICATED. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, ORIGINAL MATERIAL THICKNESS .071", AFTER REWORK .041". THIS REPAIR IS CLASSOFIED AS A CAT. "A" MAJOR REPAIR.

Part: CHANNEL — CHAFED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

FRAME STA 1280 HAS A GOUGE BETWEEN S10R TO S12R. REMOVED DAMAGE FROM FRAME SECTION IAW SRM 53-00-07, FIG 201, PG 201. FABRICATED REPAIR PARTS. INSTALLED REPAIRS PARTS STA 1280, IAW SRM 53-00-07-DETAIL II. THIS IS A CATEGORY A, MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

BS 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED SEAT TRACK & FOUND TO BE DAMAGED AND SEVERAL DOUBLE HOLES IAW SRM 51-40-2. FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 FIG 201. INSTALLED NEW SEAT TRACK IAW SRM 51-40-2 AND SRM 53-00-52 FIG 201. CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

BS 377.5 FLOORBEAM HAS CORROSION UNDER UPPER TEE AT LBL 45.5. INSTALLED UPPER TEE AND REPAIR IAW SRM 51-00-51 FIG 201 REPAIR NR 3. THIS IS A CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — DENTED (ZONE 200) · corrosion level 2 · airframe 42,045 hrs · 16,916 cycles

UPPER TEE OF CABIN FLOORBEAM CORRODED ON TOP AND ON LWR SURFACE UNDER ONE NUTPLATE (LBL 13) FS 365 LBL 25-RBL 5. INSTALLED UPPER TEE REPAIR IAW SRM 53-00-51 FIG 201. REPAIR NR 3. THIS IS A MAJOR REPAIR CATEGORY "A".

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,045 hrs · 16,916 cycles

BS 365.5 FLOORBEAM UPPER TEE HAS CORROSION LBL 24.5. INSTALLED UPPER TEE AND REPAIR IAW SRM 53-00-51 FIG 201 REPAIR NR 3.THIS IS A CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — WORN (BS 377-440) · airframe 42,045 hrs · 16,916 cycles

BS 377-440, LBL 24, SEAT TRACK REQUIRES REPLACEMENT PER CUSTOMER REQUEST. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ASSY PER SRM 53-30- 52. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED PER SRM 51-20-01. INSTALLED NEW SEAT TRACK ASSY, BS 377-440, LBL 24, PER SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 42,045 hrs · 16,916 cycles

BS 418-440, RBL 24, SEAR TRACK IS GOUGED. REMOVED DAMAGED AREA IAW SRM 53-00-53, FIG 101, DETAIL 1. GOUGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53, FIG 101, DETAIL 1. ORIGINAL MATL. .180 INCH; AFTER REWORK; .060 INCH. REMOVED SEAT TRACK, BS 418-440, RBL 24, PER SRM 51-40-02. FABRICATED NEW SEAT TRACK, LOCATED, DRILLED PER SRM 51-40-05, 53-00-52, FIG 201, DETAIL 1 MATL BAC1520- 192. TREATED AND PRIMED NEW SEAT TRACK ASSY PER SRM 51-20-01. INSTALLED NEW SEAT TRACK ASSY, BS 418-420, RBL 24, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT 'A" MAJOR REPAIR.