N961AT

Part: CABLE — TWISTED (TAILCONE RELEASE) · airframe 57,099 hrs · 40,471 cycles

SHIP 9520 DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. CORRECTIVE ACTION: PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER B717-200 AMM 53-52-01-830-802 ONLY STEP E. (1) (S). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. (1262442)

Part: CABLE — TWISTED (TAILCON RELEASE) · airframe 57,099 hrs · 40,471 cycles

DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER AMM 53-52-01-830-802 ONLY STEP E. (1) (S). (1262180)

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 57,099 hrs · 40,471 cycles

SHIP 9520 CRACK OF 0.350IN LENGTH WAS FOUND ON LH OVERWING FRAME STA Y=737 IN REFRENECE TO CARD 5310-01439-01B / JOB 068-0003, STEP 4. LEFT OVERWING FRAME STA Y=737 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (1258141)

Part: FUEL TANK — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,099 hrs · 40,471 cycles

EXFOLIATION ON LOWER SKIN OF CENTER FUEL TANK ON STA Y= 756 AND X= 43 AT LEFT MLG WHEEL WELL. LEFT MLG WHEEL WELL WAS REPAIRED PER ER/A 629799-14AD REV. (1258160)

Part: SEAL — LEAKING (ZONE 800) · airframe 57,099 hrs · 40,471 cycles

DURING STATIC LEAK CHECK, WATER LEAKS WERE FOUND ON INSIDE OF FWD AND AFT LT OVERWING EMERGENCY EXIT DOORS. EXIT DOOR JAMB FILLER FWD AND AFT LT WERE REPLACED PER AMM 53-12-01 AND STATIC LEAK CHECK WAS PERFORMED PER AMM 52-21-01-790-801 AND NOT LEAKS WERE FOUND. (1259464)

Part: RELEASE MECH — OUT OF POSITION (ZONE 300) · airframe 57,099 hrs · 40,471 cycles

IN REFERENCE AMDS 5352-4002 DURING INSTALL TAILCONE SLIDE WAS FOUND TAILCONE RELEASE MECHANIS CAM OUT POSITION. TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER AMM 53-52-03 (1257600)

Part: NONE — NONE (NONE) · airframe 57,099 hrs · 40,471 cycles

SHIP 9520 DTA ER/A 629799-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 10-OCT-25. CORRECTIVE ACTION: REPAIRED PER DTA ER/A 629799-14 (1250137)

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 56,071 hrs · 39,509 cycles

EXIT SIGN ABOVE AFT TAIL DOOR INOPERATIVE. MAINTENANCE REMOVED THE SIGN ASSEMBLY, FOUND WIRES DISCONNECTED, SECURED WIRES, AND THE LIGHT NOW OPERATIONALLY CHECKS GOOD IAW B717 AMM 33-51. (LP #7244583)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 56,071 hrs · 39,509 cycles

IN THE AFT TAIL SECTION, ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A BAD BATTERY PACK. THE BATTERY PACK WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LOCATION B5-260. (LP #7244582)

Part: CABLE — BROKEN (ZONE 800) · airframe 56,054 hrs · 39,494 cycles

THE FLIGHT ATTENDANT FOUND THAT THE FRONT SERVICE DOOR EMERGENCY CABLE TO BAR WAS BROKEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A NEW 1R DOOR SLIDE LATCH/LANYARD ASSEMBLY. FUNCTIONAL CHECK WAS GOOD PER B717 CMM 25-60-03. AIRCRAFT HAS RETURNED TO SERVICE. (LP #7244532)

Part: SKIN — GOUGED (ZONE 300) · airframe 55,886 hrs · 39,360 cycles

BANANA FAIRING ATTACH SCREWS HAVE GOUGED INTO THE L/H STABILIZER SKIN PANEL. MAINTENANCE REPLACED LH VERT STAB SKIN TIP PER B717 SRM 51-40. (LP #6408784)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,491 hrs · 39,010 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROW 15 TO 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK FOR CORRESPONDING LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #6601810)

Part: DOOR — MISSING (POWER DOOR) · airframe 55,559 hrs · 39,061 cycles

EXTERNAL POWER RECEPTACLE DOOR MISSING. FWD TO CDL 52-47-01 ON 15DEC24 IN LEX. FLIGHT CREW PLACARD INSTALLED. ON 14JAN25 MAINTENANCE INSTALLED A NEW DOOR ASSY PER B717 AMM 24-24. OPERATIONAL CHECK WAS GOOD. CDL & PLACARDS REMOVED. (LP #0711663)

Part: DOUBLER — CRACKED (ZONE 200) · airframe 55,147 hrs · 38,721 cycles

-AD- FUSELAGE PLATE SKIN DOUBLERS STA Y=1178 BTW L1-L3 LH CRACKED. ACCOMPLISH ER/A 546495-14AD REV A SECTION III FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-546495 ADDED FOR AC 9520. C/W ERA 546495-14AD REV A SECTION 3. CLOSED LOG AND REMOVED MONITOR INSP. (LP #0650668)

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 54,655 hrs · 38,291 cycles

FOUND L/H AND R/H OVERWING EXIT DOOR SIDE PANEL IDENTIFIER SIGN INOPERATIVE. CONFIRMED NO POWER AT PIN 1 OF EITHER EEI. VERIFIED GOOD GROUND. POWER SUPPLY B5-118 TO EEI SIGNS (L2-834 AND L2-835). FOUND FUSES F3 AND F4 BLOWN IN POWER SUPPLY. REPLACED POWER SUPPLY B5-118 PER B717 AMM 33-50. ALL CHECKS ARE GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #0528533)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,454 hrs · 37,209 cycles

THE FORWARD OVERWING LOWER EXIT EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDES ARE INOPERATIVE. MAINTENANCE REPLACED B5-118 BATTERY EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL AND ALL PANELS ARE CLOSED. (LP #5003415)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,106 hrs · 36,922 cycles

BOTH EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4996665)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,106 hrs · 36,922 cycles

BOTH OF THE FWD EMERGENCY DOOR FLOOR IDENTIFIER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 341 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4996664)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,041 hrs · 36,867 cycles

THE EXIT SIGN IS MISSING OVER DOOR 1L. MAINTENANCE INSTALLED A NEW EXIT LIGHT COVER PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4996630)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,816 hrs · 36,666 cycles

THE EMERGENCY LIGHTS REMAIN ON WHILE IN THE "ARM" POSITION. T/S PER B717 FIM 33-50 AND WDM 33-51, PG 2. L2-788, L2-789, AND L2-740 WERE ON IN FLIGHT. ISOLATED AND REPLACED BATTERY AND POWER SUPPLY ASSEMBLY B5-123, PER B717 AMM 33-51. ALL OPERATIONS ARE NOW NORMAL. CHECKS GOOD PER FIM. (LP #7071572)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,806 hrs · 36,659 cycles

THE EMERGENCY LIGHTS OVER 1L AND 1R DOORS CAME ON IN FLIGHT AND WERE FLICKERING AT A FAST FREQUENCY. CEILING LIGHT OUTSIDE FIRST CLASS LAV ALSO FLICKERED ALONG WITH THE EMERGENCY DOOR LIGHTS. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK B5-259 PER B717 AMM 33-51. (LP #7071564)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,806 hrs · 36,659 cycles

EMERGENCY LIGHTS OVER L1 AND L2 DOORS STAY ILLUMINATED. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. *** CONTRACT MAINTENANCE EVENT - OCM: 271512 *** DISCONNECTED AND RECONNECTED THE BATTERY POWER SUPPLY TO L1 AND L2 DOORS EMERGENCY EXIT LIGHTS PER B717 AMM 33-51-03. LIGHTS OPERATE NORMALLY. AIRCRAFT IS OK FOR SERVICE. (LP #7071562)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,800 hrs · 36,656 cycles

THE EMERGENCY LIGHTS WERE FLICKERING AT THE L1 DOOR, COCKPIT OVERHEAD, AND OVERHEAD PANEL IN THE CABIN DURING FLIGHT. MAINTENANCE INSPECTED BATTERY PACK B5-123 AND B5-235 PER B717 WD 33-51-12. FOUND BATTERY PACK B5-235 WITH THE BATTERY CONNECTOR BROKEN. REPLACED THE BATTERY PACK B5-235 AS PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #7071548)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,779 hrs · 36,639 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS IN THE FWD GALLEY INOPERATIVE. SLAVED IN A NEW BATTERY CHARGER UNIT FOR BOTH, AND BOTH LIGHTS FUNCTIONED NORMALLY. MAINTENANCE REPLACED THE BATTERY CHARGER UNIT (B5-118) REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. MAINTENANCE ALSO REPLACED THE BATTERY CHARGER AND BATTERY FOR B5-123 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7071514)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,775 hrs · 36,637 cycles

THE EMERGENCY LIGHTS AT THE TAIL EXIT DOOR AND FORWARD OVERWING EXIT ARE INOPERATIVE. A TERMINAL LUG WAS RE-CONNECTED CORRECTLY AND BATTERY PACKS (B5-235) AND (B5-118) WERE REPLACED PER B717 AMM 33-51-04. TEST OK. (LP #6535998)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

WEAR ON INNER SKIN NEAR TO AFT HINGE, ALSO NEAR TO FWD LATCH FITTING, AT AFT CARGO DOOR. SUMMARY OF NRC 00446: INNER SKIN NEAR TO AFT HINGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 612398-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612398-14 REV 0. WEAR ON INNER SKIN NEAR TO FWD LATCH FITTING AT AFT CARGO COMPARTMENT DOOR WAS REMOVED PER B717-200 SRM 52-00-00-1A PAR 4C FIGURE 103 AND AREA NEAR TO FWD LATCH FITTING AT AFT CARGO DOOR WAS MEASURED AS FOLLOWS: ORIGINAL THICKNESS: 0.050". REMAINING THICKNESS: 0.041". MATERIAL REMOVED: 0.009". THEREFORE, IT IS WITHIN LIMITS PER B717-200 SRM 52-00-00-1A PAR 4C FIGURE 103. ASSOCIATED ER/A 14-612398 ADDED FOR AC 9520. (LP #0015565)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

A MISSING CLAMP WAS FOUND ON THE LATCH CABLE (2 EA) FOR THE TAILCONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00700: LATCH CABLE CLAMPS (2 EA) WERE INSTALLED, LUBE AND ADJUSMENT AT ALL TAILCONE MECHANISM RELEASE SYSTEM PER B717-200 AMM 20-50-01-911-801 AND 53-52-01-830-802. (LP #0013393)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON INTERNAL PRODUCTION DOUBLER BTW EXTERNAL SKIN AND LOWER PAN, AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0285: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW EXTERNAL SKIN AND LOWER PAN, AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PER ERA 611792-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND 04OCT25. NOTE TO ENGINEER: A DAMAGE TOLERANCE EVALUATION (DTE) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED BY FAA ADVISORY CIRCULAR 120-93. FOLLOW UP UNDER LOG 0011686. ASSOCIATED ER/A 14-611792 ADDED FOR AC 9520. (LP #0012729)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00570: INNER PAN ON STOP #3 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 612182-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612182-14 REV. 1. ASSOCIATED ER/A 14-612182 ADDED FOR AC 9520. (LP #0013173)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

SEVERAL CORROSION AROUND OF AFT CARGO DOOR JAMB. SUMMARY OF NRC 0007: CORROSION LEVEL 2. AFT CARGO DOOR JAMB WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 PAR 5 FIGURE 201. (LP #0002390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002. SUMMARY OF NRC 00565: CORROSION LEVEL 2. CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002 WERE REPAIRED PER SRM 53-20-05-2R REPAIR 1 FIG 201 (SHEET 1). (LP #0003346)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON CUSP WEB STA Y=965 X=-56 AT CPAX. SUMMARY OF NRC 00669: CORROSION LEVEL 2. CUSP WEB STA Y=965 X=-56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2993211)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON CAP STA Y=1022RH LONGERON 7RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00386: CAP STA Y=1022RH LONGERON 7RH INNER STRUCTURE WAS REPAIRED PER ER/A 611872-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-611872 ADDED FOR AC 9520. (LP #2993707)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION REMOVAL RESULTED IN THE FRAME THICKNESS AT STA Y=275 LONG 30 TO BE OUT OF LIMITS. FWD CARGO. SUMMARY OF NRC 00543: CORROSION LEVEL 2. FRAME AT STA Y=275 LONG 30 FWD CARGO WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2993220)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACKS (2 EA) ON PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00445: PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #2990723)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON CUSP WEB STA Y=370 X=-54 AT CPAX. SUMMARY OF NRC 00668: LEVEL CORROSION 2. CUSP WEB STA Y=370 X=-54 AT CPAX WAS REPAIRED PER B717 SRM-53-00-55-2R PROCEDURE 4 AND 51-41-05-0G PAR 8. (LP #2991582)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L. SUMMARY OF NRC 00036: CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L.WAS REPAIRED PER PRI 611843-14 REV 2 AND ERA 611843-14 REV ORIGINAL. SECTION I PERMANENT REPAIR.TIME COTROLLED ITEMS: SEC II COVERED WITH LP 2991508. (LP #2991960)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00103: CORROSION LEVEL 2. FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND 51-41-02-0G. (LP #2988881)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON REPAIR DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS (PAX CABIN). SUMMARY OF NRC 00405: CORROSION LEVEL 2. DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS WERE REPLACED PER B717 SRM 53-00-55-2R-4- REPAIR 4. (LP #2989020)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX. SUMMARY OF NRC 00311: CORROSION LEVEL 2. WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 ITEM 32 AND DWG: 9936535 REV CS. (LP #2985149)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON GENERATION FLOOR PANEL FLOOR PANELS WERE FABRICATED AND REPLACED PER DWG 9952521 REV BB, DWG 9956320 REV G, DWG 9956336 REV G AND B717-200 SRM 51-20-05-0G. (LP #2984188)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=579 ON X=-56 AND (1 EA) BTW STA Y=794 AND STA Y=813 ON X=-56 AT PAX CABIN. SUMMARY OF NRC 00323: CORROSION LEVEL 2. CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=579 ON X=-56 AND (1 EA) BTW STA Y=794 AND STA Y=813 ON X=-56 AT PAX CABIN WERE REPLACED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 AND 51-41-05-0G PAR 8. (LP #2982932)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 WAS REPAIRED PER B717-200 SRM-53-00-00-2R. PROCEDURE 2. (LP #2978089)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 AT CPAX WAS REPAIRED PER B717-200 SRM-53-00-00-2R. PROCEDURE 2. (LP #2978093)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 (INTERNAL SIDE) AT PAX CABIN. SUMMARY OF NRC 00329: CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #2978082)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON LONGERON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00385: LONGERON ON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #2976393)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

MISSING RELEASE CABLE AND CLIP RETAINERS (2 EA) ON TAILCONE SLIDE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00130: NEW DEPLOYMENT CABLE WAS INSTALLED PER B717-200 AMM 25-61-02 400-801 AND CLIP RETAINERS WERE INSTALLED PER SAFRAN AEROSYSTEMS EVACUATION CMM 25-66-20. (LP #2974755)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON FRAME 17LH STA Y=1037LH (INNER STRUCTURE) AT CPAX. SUMMARY: FRAME 17LH STA Y=1037LH (INNER STRUCTURE) WAS REPAIRED PER B717-200 SRM 53-20-07-02-4, PAR 5(A)(4) TO (7) AND 51-41-05-0G PAR 8. (LP #2974201)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON CUSP WEB LH SIDE STA Y=920 IN REF NRC 00402 CPAX. SUMMARY OF NRC 00594: CORROSION LEVEL 2. CUSP WEB LH SIDE STA Y=920 WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4. (LP #2972822)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON LONGERON END (2 EA) STA 1053 L- 28L AND L-27L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY: NEW END LONGERON WAS INSTALLED PER B717 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #2972954)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

A HOLE WAS FOUND AT LOWER SURFACE OF LH INBOARD SLAT (CLOSE TO ATTACHING POINT OF SLAT TRACK 1). SUMMARY OF NRC 00546: LOWER SURFACE OF LH INBOARD SLAT (CLOSE TO ATTACHING POINT OF SLAT TRACK 1) WAS REPAIRED PER B717-200 SRM 57-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2968759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 52,774 hrs · 36,636 cycles

CORROSION ON PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 X=10 TO X=-10 AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00409: CORROSION LEVEL 2. PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 X=10 TO X=-10 AT AFT PRESSURE BULKHEAD WAS REPLACED PER DWG PL 5910130 REV ET, AND B717-200 SRM 51-40-02-0G. (LP #2968703)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

WEAR ON CAM ASSY OF TAIL CONE RELEASE MECHANISM AT THE 10:00 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC #00025: BASE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52-03. (LP #2969910)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

CRACK ON EXTERNAL FUSELAGE NEAR RH AFT HINGE AT NOSE LANDING DOOR. SUMMARY OF NRC 00407: EXTERNAL SKIN WAS REPAIRED PER B717-200 SRM 53-10-01-2R-11 PAR. (K). (LP #2964851)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,774 hrs · 36,636 cycles

A CRACK WAS FOUND ON THE OUTER PAN STA 389 ON FWD CARGO COMPARTMENT DOOR (UPPER EDGE). SUMMARY OF NRC 00522: AREA ON OUTER PAN STA 389 ON FWD CARGO COMPARTMENT DOOR (UPPER EDGE) WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2962737)

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,277 hrs · 36,258 cycles

THE CEILING PANELS 1-8, 11-13, AND OVERWING EXIT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AT B5-227, B5-120, B5-231, AND REPLACED THE POWER SUPPLY UNIT B5 -227 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6727999)

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 51,317 hrs · 35,566 cycles

THE AFT CABIN EMERGENCY LIGHTS ARE FLASHING IN THE ARMED POSITION. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY AND POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL. (LP #6142124)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 51,267 hrs · 35,528 cycles

ROW 26C EMERGENCY LIGHT IS NOT ILLUMINATING. MAINTENANCE SUSPECTS A BAD EMERGENCY BATTERY POWER SUPPLY PACK, REPLACED THE BATTERY PACK IAW AMM 33-51-03. EEPL SYSTEM NOW OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,774 hrs · 35,194 cycles

FOUND AFT WING EMERGENCY EXIT DOOR LOWER LIGHTS INOPERATIVE ON BOTH THE LEFT AND RIGHT SIDES. MAINTENANCE REPLACED THE BATTERY CHARGER B5-119 PER B717 AMM 33-51. NO HELP. NO POWER AT TERMINAL BLOCK 53-388 PIN 1. FOUND NEW BATTERY CHARGER BAD FROM STOCK. REPLACED SAME PER B717 AMM 33-51 AGAIN AND THE OPERATIONAL CHECK WAS GOOD. (LP #5813750)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,994 hrs · 34,620 cycles

THE EMERGENCY LIGHTS AT ROW 20 AFT TO LAVS AND AFT OVERWING UPPER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PACKS AT STA 726 (ROW 20), STA 803 (ROW 22), AND STA 879 (ROW 25) PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #5528031)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,322 hrs · 33,469 cycles

EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROW 19AB UPPER AND LOWER EXIT, SIGN, AND 19CDE LOWER EXIT SIGN. MAINTENANCE FOUND BOTH LOWER LIGHT ASSEMBLIES AT 40 OHMS AND REPLACED THE RIGHT SIDE. INSTALLED POWER SUPPLY IAW SSM 33-51. OPS CHECKED GOOD. THE AIRCRAFT WAS OK FOR SERVICE.

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 48,265 hrs · 33,420 cycles

AFT CARGO FRAME WAS CORRODED AT BS 1022, STRINGER 30. REMOVED THE DAMAGE SECTION OF FRAME AND INSTALLED A NEW SECTION OF FRAME, IAW SRM 53-20-07-2R 4.

Part: WARNING LIGHT — FALSE ACTIVATION (TAIL SECTION) · airframe 47,739 hrs · 33,023 cycles

DECLARED AN EMERGENCY ON APPROACH, DUE TO THE TAIL TEMP HIGH WARNING INDICATION REPEATEDLY. FOLLOWING THE FIRST INDICATION THE CREW COMPLIED WITH THE QRH AND SECURED THE LEFT PACK AND BLEED. THE MESSAGE INITIALLY WENT OUT, BUT CAME BACK WITHIN 2 MINUTES. THEN THE RIGHT PACK AND BLEED WERE TURNED OFF, BUT AT THE SAME TIME THE AIRCRAFT ENTERED ICING CONDITIONS. IT WAS AT THAT POINT THE EMERGENCY WAS DECLARED TO GET A CONTINUED DESCENT AND EXPEDITED APPROACH. THE LANDING WAS UNEVENTFUL, SCANNED THE TAIL SECTION, NO ABNORMALITIES WERE FOUND. MAINTENANCE ACCOMPLISHED A COMPLETE INSPECTION AND NO PNEUMATIC LEAKS WERE FOUND. THE PODS CONTROLLER WAS REPLACED AND B LOOP D1-1038 WAS REPLACED IAW AMM 36-23.

Part: LIGHT — MISSING (CABIN) · airframe 47,553 hrs · 32,876 cycles

DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHT AT SEAT 19AB MISSING. INSTALLED A NEW LIGHT SECTION. CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,020 hrs · 32,566 cycles

LEFT & RIGHT AFT OVERWING EXIT IDENTIFIERS FOUND TO BE INOPERATIVE. (5 LTS). MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-119) PER B717 AMM 33-51. ALL OPERATIONAL CHECKS WERE NORMAL. (LP #3885940)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,644 hrs · 32,329 cycles

EMERGENCY LIGHTS AT ROWS 24-28 INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-03. CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (BS 636) · airframe 46,338 hrs · 32,133 cycles

CRACKED INTERCOSTAL BS 636, BL 0 ON CEILING AREA AT FWD CARGO COMPARTMENT. THE INTERCOSTLE WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.

Part: TAPER PIN — NOT REPORTED (NLG) · corrosion level 2 · airframe 44,632 hrs · 30,877 cycles

TAPER PINS FAIL INSPECTION FORECAST 95-0532-8-0010. REPLACED NLG DRAG BRACE REF AMM 32-22-05.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,147 hrs · 30,527 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEATS 1B & 1C IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,973 hrs · 30,393 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 20BCD IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE LT WHEEL WELL AREA, ZONE 145, CARD 1. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED IAW ER/A 546499-14, REV ORIGINAL. HFEC BLENDED AREA AND NO ADDITIONAL DAMAGE WAS FOUND. ASSOCIATED ER/A 00-546499 ADDED FOR AC 9520.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE. RIGHT WHEEL WELL AREA, ZONE 144, CARD 1. REPAIR WAS ACCOMPLISHED IAW ER/A 546499-14, REV ORIGINAL, HFEC ON BLENDED AREAS WAS PERFORMED AND NO ADDITIONAL DAMAGE WAS FOUND.

Part: CUSP WEB — CORRODED (BS 157-187) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON CUSP WEB UPPER/LOWER SURFACE AT BS 157 TO 187 BETWEEN X=-54 AND X=-60 LOWER AREA OF R1 DOOR JAMB. W1, SM, CARD 87, ZONE 200. SERVICE DOOR JAMB PAN AND CUSP ANGLE WERE REPAIRED IAW ER/A 546506-14, REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 1178) · airframe 43,137 hrs · 29,713 cycles

CRACK ON PRODUCTION DOUBLER BS 1178 CANT BETWEEN LONGERON NR 1 AND NR 2 LT AT AFT ACCESSORY COMPARTMENT, SM. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 546495-14, REV ORIGINAL, PERFORM REPETITIVE INSPECTIONS AT EVERY, C-CHECK OR 3000 CYCLES WHICHEVER COME FIRST UNDER LOG 2535716 ON BOTH SIDE OF REPAIR IAW ER/A 546495-14, REV ORIGINAL SEC II, DCA 200402137.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 44,044 hrs · 30,449 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620KB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.

Part: CARGO TRACK — CORRODED (BS 817-900) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON LEFT CARGO TRACK FROM BS 817 TO 900. CARGO TRACK WAS REPLACED IAW SRM 53-20-52, 51-41-05 AND 51-41-01.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 44,044 hrs · 30,449 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620QB. ACCESS PANEL WAS REPLACED AND LEAK CHECKED.

Part: SKIN — CRACKED (BS 1133) · airframe 43,137 hrs · 29,713 cycles

CRACK ON SKIN BS 1133 BETWEEN LONGERON 2-3R AT OUTER FUSELAGE SKIN AREA. SKIN WAS REPAIRED IAW ETI-17-16-035, ER/A 546487-14AD, REV. ORIGINAL. ASSOCIATED ER/A 00-546487 ADDED FOR AC 9520.

Part: SKIN — DAMAGED (BS 1004-1045) · airframe 43,137 hrs · 29,713 cycles

ENLONGATED HOLES ON FUSELAGE SKIN AND LONGERON 26 LT FROM BS 1004 TO 1045. SKIN REPAIRED IAW ETI-17-16-060, REV. 2 AND ER/A 546557-14, REV. ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 44,044 hrs · 30,449 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL. THE ACCESS PANEL WAS REPLACED AND A. LEAK CHECK WAS PERFORMED.

Part: CARGO TRACK — CORRODED (BS 900-1022) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 900 TO 1022. THE CARGO TRACK WAS REWORKED IAW SRM 51-10-04 PAR. 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-41-05 AND 51-41-01.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 44,044 hrs · 30,449 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620HB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.

Part: FINGER DOUBLER — CORRODED (BS 1002-1022) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON INTERNAL STRUCTURE BETWEEN BS 1002 TO 1022, LONGERON 26L AT AFT CARGO COMPARTMENT. FINGER DOUBLER WAS REPLACED BY EXCESSIVE CORROSION IAW SRM 53-03-07, FIG 212 AND 51-41-02.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF WING ACCESS PLATE NR 520CB. CARD 38, ZONE 500. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 620LB. ZONE 600, CARD 35. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON WING ACCESS PLATE 520CT AT SETTLEMENT AND COUNTERSKIN AREA. ZONE 500, DUE TO CORROSION FOUND ON ACCESS PLATE NR 520CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620CT. ZONE 600, DUE TO CORROSION FOUND ON ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF WING ACCESS PLATE 520HB. ZONE 500. CORROSION ON COUNTERSKIN AT FUEL ACCESS PLATE 520HB WAS REMOVED, AND MAX DIAMETER ALLOWABLE IS 0.532 AND MAX DIAMETER MEASURED IS 0.565 IN AND WERE FOUND 3 HOLES ADJACENT OUT OF LIMITS. THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 57-10-01.

Part: LONGERON — CORRODED (BS 929-1022) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON LONGERON 29LT AND SPLICE FROM BS Y=929 TO 1022 AT AFT CARGO COMPARTMENT, C2, SM. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED, MEASURED, ORIGINAL THICKNESS: 0.125" REMAINING THICKNESS 0.110" THEREFORE IT'S WITHIN LIMITS IAW SRM 51-10-04, PAR 26, 21 AND 15 53-00-00, FIG 103. DUE TO EXCESSIVE CORROSION LONGERON ON BS Y=970 TO 1010 AND SPLICE WERE REPLACED IAW SRM 53-00-05, FIG 201, 51-41-02, AND 51-40-05. EQUIPMENT: PANAMETRICS 35DL PLUS TRANSDUCER SONPEN V260RM EXP DATE 25AUG16.

Part: LONGERON — CORRODED (BS 927-1037) · airframe 43,137 hrs · 29,713 cycles

CORROSION ON LONG 28 LT AND SPLICE FROM BS Y=927 TO Y=1037 AT AFT CARGO COMPARTMENT C2, SM, ZONE 180, CARD 5. CORROSION ON LONG 28 LT FROM BS Y=927 TO BS 1037 AT AFT CARGO COMPARTMENT WAS REMOVED IAW SRM 51-10-04, PAR. 26, 21, AND 15. MEASURE: ORIGINAL THICKNESS IS 0.170" AND MINIMUM REMAINING IS 0.161" THEREFORE WITHIN LIMITS IAW SRM 53-20-05 AND 53-00-00, FIG. 103. SPLICE WAS REPLACED IAW SRM 53-00-05. REPAIR 2 EQUIPMENT: OLYMPUS 38 DL PLUS EXP DATE 27OCT16. TRANSDUCER SONOPEN V260RM.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE NR 520MB. SM, CARD 40, ZONE 500. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520 MB WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUNTERSINK MAX DIAMETER IS 0.532 IN AND MAX DIAMETER MEASSURE IS 0.538 IN THEREFORE IS OUT LIMITS AND FUEL ACCESS PLATE WAS REPAIRED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE 520EB. SM, CARD 34, ZONE 500. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED ON ACCESS PLATE 520EB AND WAS MEASURED MAX. DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND MORE 2 ADJACENT HOLES OUT OF LIMITS IAW SRM 57-10-01. THEREFORE ACCESS PLATE IS OUT LIMITS AND WAS REPLACED.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTER SKIN OF FUEL ACCESS PLATE NR 620FT. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620 FT WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUNTERSINK MAX DIAMETER IS 0.660" AND MAX DIAMETER MEASURE IS 0.680" IN THEREFORE IS OUT LIMITS AND FUEL ACCESS PLATE WAS REPAIRED IAW SRM 57-10-01.

Part: STRUCTURE — CORRODED (BS 900-910) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON INTERNAL STRUCTURE BETWEEN BS 900 TO 910 BETWEEN LONGERON 25 TO 26L. STRUCTURE REPAIRED IAW SRM 53-02-01, REPAIR 1, 51-40-08, AND 51-10-04 PAR 15-21-37 AND 51-41-02.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AND COUNTERSKIN AREA OF WING ACCESS PLATE NR 620CB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSKIN WERE REMOVED IAW SRM 57-10-01, MAX DIAMETER ALLOWABLE ON COUNTERSKIN IS 0.532", MAX DIAMETER MESURED IS 0.545" AND WERE FOUND 3 ADJACENT HOLES AT FUEL ACCESS PLATE 620CB, THEREFORE IS OUT LIMITS, WAS REPLACED IAW AIPC 57-23-01.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620EB. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED MAX DIAM ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS 0.565" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SRM 57-10-01. THEREFORE IS OUT LIMITS AND ACCESS PLATE WAS REPLACED IAW IPC 57-22-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF FUEL ACCESS PLATE NR 620MB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 620MB WAS REMOVED IAW SRM 57-10-01 MAX DIAMETER ALLOWABLE ON COUNTERSINK IS 0.532" MAX DIAMETER MEASURED IS 0.590", WERE FOUND 3 HOLES ADJACENT THEREFORE IS OUT LIMITS AND WAS REPLACED IAW AIPC 57-23-01.

Part: ANGLE — CRACKED (BS 1168) · airframe 43,137 hrs · 29,713 cycles

CRACKED ANGLES BS 1168 BETWEEN LONGERON 3RTO 2L. ANGLES REPLACED IAW DWG 9911860, REV L AND SRM 51-41-02 AND SRM 51-41-05.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON SETTLEMENT AND COUNTERSINK OF WING ACCESS PLATE NR 620DT. RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED, MAX DIMENSION ALLOWABLE 0.660" MAX DIAMETER MESURED ARE 0.675" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SRM 57-10-01. THEREFORE IS OUT OF LIMITS AND ACCESS PLATE WAS REPLACED IAW IPC 57-22-01-01.

Part: FRAME — CRACKED (BS 1116) · airframe 43,137 hrs · 29,713 cycles

CRACK ON FRAME ANGLE BS 1116, LONGERON 15L AT AFT ACCESSORY COMPARTMENT. THE ANGLE WAS REPLACED IAW DWG 5913595 REV.AP AND SRM 51-41-05, 51-41-02.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,137 hrs · 29,713 cycles

DAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14 REV ORG.

Part: CHANNEL — CRACKED · airframe 43,137 hrs · 29,713 cycles

CRACKS ON CHANNEL OF FLOOR PANEL NR 222 X. CHANNEL WAS REPAIRED IAW SRM 53-20-50, FIG 201. HFEC INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-001.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 43,137 hrs · 29,713 cycles

CRACKED RT CUSP WEB AT X -44 TO X -54 BETWEEN BS 218 AND 237 AT CABIN FLOOR STRUCTURE. REPAIR ON CUSP WEB IAW SRM 53-00-55, FIG 219, REP 4.

Part: DOOR — WORN · airframe 43,137 hrs · 29,713 cycles

MAINTENANCE DISCOVERED THAT THE AFT CABIN BULKHEAD EMERGENCY ESCAPE DOOR WAS WORN AND DAMAGED ON THE LOWER INBD SIDE. THE DAMAGE AREA WAS REPAIRED IAW SRM 52-10-02. REPAIR 15 AND 16.

Part: CUSP WEB — DAMAGED · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON RT CUPS WEB, UPPER AND LOWER SURFACE, X 54 TO X 60, BS 436 TO 465, 503 TO 522, 522 TO 579. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 203, 51-41-02, AND 51-41-05 FROM BS Y=436 TO Y=465 AREA WAS REINSPECTED AND NO CORROSION WAS FOUND. RII COMPLETED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,137 hrs · 29,713 cycles

DAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14, REV. ORIGINAL.

Part: CUSP WEB — CORRODED (BS 952) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

EXCESSIVE CORROSION ON RT CUSP WEB BS 952. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 205, RII COMPLETED BY INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,137 hrs · 29,713 cycles

CRACKED EXTERNAL SKIN AROUND OF HOLD OPEN LOCK HOUSING AT MAIN L1 DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-10-01, REP 4, FIG 201. LENGTH CRACK = 0.270", RII COMPLETED.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 43,137 hrs · 29,713 cycles

DAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14.

Part: ATTACH ANGLE — CRACKED (BS 1022) · airframe 43,137 hrs · 29,713 cycles

CRACK ON ANGLE TO ATTACH LT AFT ENGINE PYLON SUPPORT BULKHEAD, BS Y=1022 BETWEEN LONGERONS 6 TO 7L ALSO LONGERONS 16 TO 17L. ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-10-14, PAR. 21 AND 15.

Part: PAN — CRACKED · airframe 43,137 hrs · 29,713 cycles

CRACK ON INNER PAN APPROXIMATELY BS 200, AFT EDGE, BETWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. INNER PAN WAS REPAIRED IAW SRM 52-10-02, REP 2, FIG 201. LENGTH OF CRACKS: 1.800", 2.400".

Part: BEAM — CRACKED · airframe 43,137 hrs · 29,713 cycles

CRACK ON BEAM NR 1, FWD EDGE AT MAIN ENTRANCE DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. LENGTH OF CRACK = 0.800".

Part: SKIN — WORN (PAX DOOR) · airframe 43,137 hrs · 29,713 cycles

WEAR ON EXTERNAL SKIN APPROXIMATELY STATION 170, LOWER EDGE AT MAIN ENTRANCE DOOR. EXTERNAL SKIN, LOWER EDGE, WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2 HFEC INSPECTION WAS PERFORMED AND NO CRACKS WERE FOUND. PERFORM INSPECT DECAL CONDITION EVERY "C" CHECK IAW TOPP 30-10-70.

Part: CUSP WEB — CORRODED (BS 674-680) · airframe 43,137 hrs · 29,713 cycles

CRACK ON LT CUSP WEB BETWEEN X 50 TO X 54, BS 674 - 680. CUSP WEB REPAIRED IAW SRM 53-00-55, FIG 226.

Part: CUSP WEB — CORRODED (BS 940) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

EXCESSIVE CORROSION ON RT CUSP WEB BS 940. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215.

Part: CUSP WEB — CORRODED (BS 794-813) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

EXCESSIVE CORROSION ON RT CUSP WEB BETWEEN X-54/60, BS 794 TO 813, CARD 111, ZONE 200. RT CUSP WEB WAS REPAIRED BETWEEN BS 794-813 IAW SRM 53-00-55, FIG 216.

Part: SEAT TRACK — CRACKED (BS 737) · airframe 43,137 hrs · 29,713 cycles

CRACKED BEAM BELOW SEAT TRACK X=-54 AT BS 737, PAX CAB, SM, ZONE 140, CARD 6, WB, CARD 6, ZONE 140. BEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05. LONG CRACK: 2.000".

Part: CUSP WEB — CORRODED (BS 995) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

EXCESSIVE CORROSION ON LT CUSP WEB BETWEEN X=54/60 AND BS 995, CARD 110, ZONE 200. LT CUSP WEB BETWEEN X=54/60, BS Y=995 WAS REPAIRED IAW SRM 53-00-55, FIG 215.

Part: FRAME — CRACKED (BS 674-715) · airframe 43,137 hrs · 29,713 cycles

CRACK ON FRAME BS 674 - 689, AND BS 715, LONGERON 25RT AT UNDERWING BARREL KEEL BEAMS. FRAME REPAIRED IAW SRM 53-00-00, FIG 201.

Part: PAN — CRACKED (BS 370) · airframe 43,137 hrs · 29,713 cycles

CRACK ON FWD PAN BS 370 BETWEEN BEAMS 2 AND 3 AT FWD CARGO COMPARTMENT DOOR. PAN WAS REPAIRED IAW SRM 52-30-02, FIG.201, 51-41-02, 51-41-04, 51-41-01, 51-10-04 PAR 15.

Part: SKIN — WORN (CARGO DOOR) · airframe 43,137 hrs · 29,713 cycles

WORN EXTERNAL SKIN AT EDGE BETWEEN BEAMS 1 AND 3 AT AFT CARGO COMPARTMENT DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-00-01, REPAIR 8, FIG 204.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 43,137 hrs · 29,713 cycles

CRACKED INTERCOSTAL X=0, BS 636 TO 617 AT CEILING AREA OF FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00, FIG 201.

Part: FRAME — CRACKED (BS 674) · airframe 43,137 hrs · 29,713 cycles

CRACK ON FRAME BS 674, LONGERON 25L AT UNDER WING BARREL KEEL BEAMS. THE FRAME WAS REPAIRED IAW SRM 53-00-00, REPAIR 1, FIG 201.

Part: FRAME — CRACKED (BS 689) · airframe 43,137 hrs · 29,713 cycles

CRACKED FRAME BS 689, LONGERON 26L AT KEEL BEAM AREA. THE FRAME WAS REPARED IAW SRM 53-00-00, REPAIR 1, FIG 201.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,137 hrs · 29,713 cycles

CRACK ON NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE L1 DOOR. NR 1 BEAM WAS REPAIRED IAW SRM 51-41-02, 51-41-01, SRM 52-10-02, FIG 202, SHEET 8, 51-20-09, 51-41-03, AND 51-10-04, PAR 15.

Part: DOUBLER — CORRODED (BS 579-598) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON DOUBLER ATTACH INNER FUSELAGE SKIN AND CUSP WEB BETWEEN X=54 TO X=60 BS 579 TO 598, RT SIDE. CORROSION WAS REMOVED, AREA WAS MEASURED. ORIGINAL THICKNESS: 0.080" REMAINING THICKNESS: 0.041" THEREFORE ITS OUT OF LIMITS AND DOUBLER WAS REPLACED IAW SRM 51-10-04, PAR 26, 53-00-00, FIG 103, 51-41-05 AND DWG N. 9910151.

Part: SKIN — GOUGED (BS 408-420) · airframe 43,137 hrs · 29,713 cycles

GOUGES ON EXTERNAL SKIN BETWEEN BS 408-420 BETWEEN BEAM 2 AND LOWER EDGE AT FWD CARGO COMPARTMENT DOOR. SKIN WAS REPAIRED IAW SRM 52-00-01, FIG 202.

Part: CUSP WEB — CORRODED (BS 408-427) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

AWR EXCESSIVE CORROSION ON RT CUSP WEB BETWEEN BS 408 AND BS 427 IN REF CARD 59, ZONE 200. CARD 96, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 408 AND STA 427 IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 203, REPAIR 4, DWG 9930538, REV BR, 51-10-04 PAR 21/15, SRM 51-41-05 AND 51-40-03, PAR 17.

Part: CUSP WEB — CORRODED (BS 245-249) · corrosion level 2 · airframe 43,137 hrs · 29,713 cycles

CORROSION ON CUSP WEB BS 245 TO 249, RT SIDE IN REF CARD 59, ZONE 200. CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 244 TO BS 249 RT SIDE IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 215, REPAIR 4, SRM 53-20-51, FIG 1 ITEM 14, 51-10-4 PAR 21/15, 51-41-05, AND 51-40-03, PAR 17.

Part: CUSP WEB — CRACKED (BS 368-375) · airframe 43,137 hrs · 29,713 cycles

CRACKED RT CUPS WEB BETWEEN X=54 TO X=60, BS 368 TO 375. CUSP WEB WAS REPAIRED IAW SRM 53-00-05, FIG 214 AND 51-41-05, 51-41-02, 51-10-04 AND 51-40-08 TRIMOUT WAS ACCOMPLISHED.

Part: DOUBLER — DAMAGED (BS 954) · airframe 43,137 hrs · 29,713 cycles

PREVIOUS REPAIR DOUBLER WORN AND BENT, INNER PAN AND OUTER PAN BS 954 BETWEEN BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR. REPAIR DOUBLER WAS FABRICATE AND REPLACED IAW SRM 52-30-02, REPAIR 4, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1022-1060) · airframe 43,137 hrs · 29,713 cycles

CORROSION ON FLOOR SUPPORT X=44 BETWEEN BS 1022 TO 1060 AT LT PAX CABIN. FLOOR SUPPORT WAS REPLACED IAW DWG: 9981474, REV: L.

Part: SEAT TRACK — CORRODED (BS 609) · corrosion level 2 · airframe 44,044 hrs · 30,449 cycles

CORROSION ON SEAT TRACK X 44 AT BS 609. THE SEAT TRACK WAS REPAIRED IAW SRM 51-10-04 AND 53-20-52 FIG.201.

Part: FRAME — CRACKED (BS 715) · airframe 40,119 hrs · 27,267 cycles

OVERWING FRAME CRACKED AT STA 715 RT, CONDITION 3. FRAME REPLACED IAW AMDS WC 5310-01436-03B.

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 40,098 hrs · 27,253 cycles

RIGHT CUSP WEB CRACKED AT STA 674 BETWEEN INBD AND OTBD SEAT TRACKS. REPLACED CUSP WEB, MEMBRANE, IAW DWG 9910151 AND ER/A 532674-14.

Part: CUSP WEB — CRACKED (BS 655) · airframe 40,000 hrs · 27,182 cycles

FORWARD CARGO BAY BS 655, LBL 54 CUSP WEB CRACKED. INSTALLED A REPAIR IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CRACKED (BS 655) · airframe 40,000 hrs · 27,182 cycles

FORWARD CARGO BAY BS 655 RBL 54 CUSP WEB CRACKED. INSTALLED A REPAIR IAW SRM 53-00-55 REPAIR 4.

Part: DIODE — FAILED (EMERGENCY LIGHT) · airframe 39,229 hrs · 26,516 cycles

R1 OVERWING DOOR EMERGENCY EXIT MARKER FOUND INOPERATIVE DURING SERVICE CHECK. FOUND L2-788, LIGHT ASSY DISCONNECTED. CONNECTED THE LIGHT AND FOUND DIODE ASSY, R7-188, BAD. REPLACED THE DIODE ALONG WITH THE BATTERY AND POWER SUPPLY, CHECKED NORMAL.

Part: PIN — DISLODGED (TAILCONE) · airframe 38,795 hrs · 26,117 cycles

PILOT REPORTED THE AMBER CAUTION MESSAGE ILLUMINATED INDICATING THE TAILCONE WAS NOT SECURE. MAINTENANCE FOUND THE INTERNAL TAILCONE RELEASE HANDLE PIN DISLODGED FROM THE RETAINER CLIPS. THE LOCK CABLE WAS REINSERTED AND THE BALL END NOW MAKES PROPER CONTACT WITH THE SWITCH AS REQUIRED. THE REQUIRED INSPECTION OF THE INSTALLATION WAS COMPLETED AND THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,651 hrs · 26,016 cycles

TAIL COMPARTMENT AFT EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,651 hrs · 26,016 cycles

R1 DOOR EMERGENCY EXIT SIGN LOWER BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 38,651 hrs · 26,016 cycles

R1 DOOR EMERGENCY EXIT SIGN CRACKED. R & R SIGN IAW AMM.

Part: FITTING — MISSING (EVAC SLIDE) · airframe 38,045 hrs · 25,629 cycles

TAIL CONE EVACUATION SLIDE COVER MISSING AFT RETAINER CLIP. INSTALLED CLIP IAW AMM.

Part: SKIN — GOUGED (BS 229-237) · airframe 38,748 hrs · 26,074 cycles

SKIN GOUGED AT BS 229-237 BETWEEN LONGERON 6L AND 7L. REPAIRED, SKIN IAW SRM 53-03-01-2R-1, FIGURE 211, SHEET 3.

Part: FORMER — CRACKED (FUSELAGE) · airframe 38,045 hrs · 25,629 cycles

FORMER CRACKED AT BS 237, LONGERON 18L. R & R FORMER IAW DWG.

Part: SKIN — DENTED (BS 237) · airframe 38,748 hrs · 26,074 cycles

DENT ON LT FUSELAGE AT BS 237 AND 5" ABOVE LONGERON 18. REPAIRED SKIN IAW SRM 53-00-01-2R-6.S062052.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 38,045 hrs · 25,629 cycles

R1 DOOR CUT OUT LOWER SILL GIRT BAR SUPPORT FITTING CORRODED AT BS 174, RBL 53. R & R FITTING IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,469 hrs · 25,260 cycles

LT EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 19 TO ROW 23. R & R BATTERY AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,469 hrs · 25,260 cycles

RT EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 19 TO ROW 23. R & R BATTERY AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,921 hrs · 24,909 cycles

OVERHEAD EMERGENCY EXIT SIGN AISLE WIRES EXPOSED & SIGN LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 35,558 hrs · 24,080 cycles

OPS REPORTED THAT R1 DOOR GIRT BAR FELL OFF. RESTOWED R1 DOOR GIRT BAR NO OTHER MAINTENANCE REQUIRED REF AMM 25-61-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,276 hrs · 23,898 cycles

ONE FWD F/A'S FLASHLIGHT INOP (NOT BLINKING). RERACKED FWD F/A LOWER FLASHLIGHT PER AMM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FLOORBEAM SUPPORT FITTING CRACKED AT BS 727, LBL 44. REMOVED AND REPLACED FITTING IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FWD CARGO COMPARTMENT CUTOUT CORRODED AT FRAME BS 427 UPPER SURFACE BEHIND AFT CARGO DOOR LATCH PIN. REPAIRED PAN IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FWD CARGO COMPARTMENT INTERCOSTAL ATTACHMENT CLIP CRACKED AT FRAME STA 237 BETWEEN LONGERON 27 RIGHT & LONGERON 28 RIGHT BELOW RIGHT FLOOR TRACK. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FRAME CORRODED AT BS 889, BETWEEN STR 30L TO STR 29L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FRAME CORRODED AT BS 870, BETWEEN STR 30L TO STR 29L. REPAIRED FRAME IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

RIGHT SIDE CUSP WEB CORRODED BETWEEN BS 484 TO BS 583. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

LEFT SIDE CUSP WEB CORRODED BETWEEN BS 756 TO BS 737. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

FRAME CRACKED AT BS 1144, STR 1. REPAIRED SPLICE IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,020 hrs · 23,076 cycles

AFT ACCESSORY COMPARTMENT STRINGER CRACKED AT BS 1154, STR 2R. REPAIRED STRINGER IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 9 · airframe 34,020 hrs · 23,076 cycles

AFT CARGO DOOR JAMB LOWER AREA CORRODED BETWEEN BS 994 TO BS 1022, STR 6R. REPAIRED PAN IAW SRM.

Part: ATTACH ANGLE — CRACKED (BARRIER DOOR) · airframe 34,020 hrs · 23,076 cycles

AFT CARGO BARRIER DOOR FWD & AFT ATTACH ANGLES CRACKED AT FASTENER HOLES. REMOVED AND REPLACED ANGLES IAW SRM & DWG.

Part: CHANNEL — CRACKED (RT MLG DOOR)

RIGHT MAIN LANDING GEAR DOOR Z-CHANNEL, CRACKED. ACCOMPLISHED MAIN LANDING GEAR DOOR Z-CHANNEL DOUBLER REPAIR PER B717 TRA 17-52-TR00139 FIG 2.

Part: ANGLE — CORRODED (FUSELAGE)

FORWARD ENTRY DOOR LOWER AFT FRAME CORNER WEB/ANGLE, STA 200 TO 208, LBL56, CORROSION. ACCOMPLISHED CORNER WEB/ANGLE REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05, AND B717 SRM 51-10-04.

Part: CHANNEL — CRACKED (LT MLG DOOR)

LEFT MAIN LANDING GEAR DOOR Z-CHANNEL, CRACKED. ACCOMPLISHED MAIN LANDING GEAR DOOR Z-CHANNEL DOUBLER REPAIR PER B717 TRA 17-52-TR00139 FIG 2.

Part: WEB — CORRODED (FUSELAGE)

FORWARD CABIN MAIN ENTRY SUBFLOOR WEB, STA 196, LBL 54, CORROSION. ACCOMPLISHED SUBFLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: ATTACH ANGLE — DAMAGED (STABILIZER)

RIGHT STAB ATTACH ANGLE FASTENER, STA 1152, SHEARED. ACCOMPLISHED ATTACH ANGLE REPLACEMENT PER EA 17-53-03024IR.

Part: ANGLE — CRACKED (FUSELAGE)

RIGHT VENT BOX UPPER FORWARD AND AFT ANGLE, CRACKED. ACCOMPLISHED ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: THRESHOLD — CORRODED (FUSELAGE)

FORWARD LAV THRESHOLD, CORROSION. ACCOMPLISHED THRESHOLD REPLACEMENT PER EA 17-25-02077IR.

Part: ANGLE — CRACKED (FUSELAGE)

LEFT VENT BOX FORWARD LOWER ANGLE, CRACKED. ACCOMPLISHED ANGLE REPLACEMENT PER B717 SRM 51-41-01 AND MM 20-60-01. SEE NR 566143 AND 566143-1.

Part: SEAT TRACK — CORRODED (CABIN)

FORWARD CABIN SEAT TRACK, STA 200 TO 332, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 53-20-52.

Part: PAN — CORRODED (FUSELAGE)

FORWARD CARGO JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN DOUBLER REPAIR PER B717 SRM 53-20-15.

Part: VANE — DENTED (TE FLAP)

RIGHT AFT MOVEABLE VANE, DENTED. ACCOMPLISHED MOVEABLE VANE COMPOSITE REPAIR PER B717 SRM 51-70-02.

Part: VANE — DENTED (TE FLAP)

RIGHT INBOARD FIXED VANE, DENTED. ACCOMPLISHED FIXED VANE COMPOSITE REPAIR PER B717 SRM 51-70-02.

Part: SEAT TRACK — CORRODED (CABIN)

FWD CABIN SEAT TRACK, STA 200 TO 332, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 53-20-52, 51/41-01, 51-10-04 AND 53-00-00.

Part: DOOR FRAME — CRACKED (FUSELAGE)

AFT OF FWD ENTRY DOOR CUTOUT FRAME UPPER FUSELAGE, STA 208, LONG 15L, CRACKED. ACCOMPLISHED UPPER FUSELAGE DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FITTING — CRACKED (FUSELAGE)

RIGHT FORWARD INBOARD MAIN LANDING GEAR DOOR CUTOUT "T" CLIP, CRACKED. ACCOMPLISHED MAIN LANDING GEAR DOOR CUTOUT "T" CLIP REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: STRUCTURE — CRACKED (RT MLG WW)

RIGHT AFT INBOARD WHEEL WELL, CRACKED. ACCOMPLISHED WHEEL WELL DOUBLER REPAIR PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD CABIN FLOOR SUPPORT, STA 196 TO 200, LBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CRACKED (FUSELAGE)

MAIN CABIN SUBFLOOR WEB, STA 218, RBL 44, CRACKED. ACCOMPLISHED SUBFLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 AND B717 SRM 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: DOOR FRAME — CORRODED (FUSELAGE)

R1 LOWER FWD AND AFT DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB REPLACEMENT PER B717 SRM 51-41-01.

Part: PANEL — CRACKED (MLG WW)

LEFT AFT INBOARD WHEEL WELL, CRACKED. ACCOMPLISHED WHEEL WELL DOUBLER REPAIR PER SRM 71-70-10 AND SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 9 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LENS — MISSING (CABIN)

CLEAR LIGHT LENS COVER MISSING 3D. INSTALLED LENS COVER ON EMERGENCY ESCAPE PATH LIGHTING AT SEAT 3D PER B717 AMM 33-51. CLEARS MDDR AND MEL.

Part: LIGHT — MISSING (CABIN)

EMERGENCY ESCAPE PATH LIGHTING SEAT 3D HAS BULB MISSING. RELAMPED SEAT LAMP ASSEMBLY PER B717 AMM 33-51. OPS CHECK GOOD. CLEARS MDDR AND MEL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK REF 717 AMM 33-51, OPS CHECK GOOD.

Part: NUT PLATE — DAMAGED (EMERGENCY LIGHT)

LEFT OVERWING EMERGENCY LIGHT HAS SCREW MISSING, NUT PLATE IS DAMAGED. INSTALLED SERVICEABLE DOME NUT REF SRM 51-41 AND 25-28.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT FLASHLIGHT BATTERY AND SECURITY STRAP, OK FOR SERVICE PER MM 25-60.

Part: SKIN — DENTED (FUSELAGE)

RT SIDE OF FUSELAGE APPROX 12 INCHES AFT OF THE MIDDLE OF R1 DOOR DAMAGED. DAMAGE IS A DENT 12 INCHES LONG X 7.5 INCHES WIDE AND .150 DEEP. A SCRATCH THAT WAS 9 INCHES LONG X .100 WIDE AND .006 DEEP HAS BEEN BLENDED. INSTALLED FLUSH REPAIR AT STA 218 BETWEEN LONG 17 AND 16 RIGHT HAND IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED 2024T3.063 DOUBLER, .025 2024T3 FINGERS AND .050 2024T3 FILLER.

Part: SKIN — DENTED (FUSELAGE)

A/C HAS DENT ON AFT SIDE OF L1 DOOR DUE TO HARD CONTACT JET WAY DRIVER. INSTALLED FLUSH REPAIR AT STA 229 TO STA 244 BETWEEN LONG 16 TO 18L IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED FINGERS DOUBLERS 2024T3.025, DOUBLERS 2024T3 .063 FILLER 2024T3.050 AND STRAP 2024T3.63.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND EXTERNAL EMERGENCY LIGHT BATTERY PACK WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW B717 MM 33-51.