N893AT

Part: RELAY — FAULTED (ZONE 200) · airframe 54,319 hrs · 39,296 cycles

EMERGENCY LIGHTS FLICKER ON AND OFF DURING FLGHT. REMOVED AND REPLACED RELAY R2-5133 PER B717 WDM 24-51-01. (8071400)

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 54,319 hrs · 39,296 cycles

SEAT ROWS 23-29 CEILING EMER LIGHTS GO OFF AFTER SHORT TIME. REMOVED AND REPLACED BATTERY FOR PACK B5-231 PER B717 AMM 33-51. (8071402)

Part: RELAY — FAULTED (ZONE 200) · airframe 54,319 hrs · 39,296 cycles

EMERGENCY LIGHTS FLICKER ON & OFF. REMOVED & REPLACED RELAY R2-5133 REF AIPC 24-50-22-01 ITEM 40, WDM 33-51-11. OPS CHECK NORMAL AT THIS NORMAL AT THIS TIME. (7961086)

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 54,319 hrs · 39,296 cycles

ONCE AIRBORNE, ALL EMERGENCY LIGHTS CAME OM AND WOULD NOT RESET ROW 25/22 EMER LIGHTS ARE OUT & EXIT LIGHT OUT AT EMER EXIT. EMER LIGHTD WENT OUT WHEN LDG GEAR CAME DOWN, CAME BACK ON AFTER LAND. PERFORMED EMERGENCY LIGHTING SYSTEM OPS CHK. OPS CHK GOOD. OK FOR SVC. (7961080)

Part: SLIDE — DEFLATED (ZONE 300) · airframe 54,206 hrs · 39,194 cycles

SLIDE IN TAIL CONE FOUND DEFLATED IN TAIL COMPARTMENT. REMOVED TAIL CONE SLIDE IAW AMM 25-61-02. INSTALLED NEW TAIL CONE SLIDE IAW WC 2561-9006 (7585377)

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 300) · airframe 54,177 hrs · 39,163 cycles

ATO- APPROX 85KTS DUE TO RUDDER RESTRICTED MESSAGE. PERFORMED RUDDER THROW LIMIT FUNCTIONAL TESTS AND RUDDER INSPECTIONS. NO DEFECTS NOTED, OPS NORMAL. (7585374)

Part: PSEU — FAILED (ZONE 700) · airframe 52,842 hrs · 37,942 cycles

SHIP 9553 -MISC/DE- THE CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "PROXIMITY SWITCH ELECTRONIC UNIT FAIL" MESSAGE ILLUMINATING. THE FLIGHT LANDED WITHOUT FURTHER ISSUE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE OPERATIONAL CHECK WAS GOOD. (LP #7177972)

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,399 hrs · 37,560 cycles

CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO BIN. SUMMARY OF NRC 00064: CORROSION LEVEL 2. THE AFT CARGO DOOR JAMB AT AFT CARGO BIN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0796316)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,399 hrs · 37,560 cycles

CORROSION WAS FOUND ON THE AFT CARGO COMP TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022. SUMMARY OF NRC 00133: CORROSION LEVEL 2. THE TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022 WAS FABRICATED PER DWG S2922357 AND REPLACED PER B717 SRM 51-41-01-OG. (LP #0790027)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,109 hrs · 35,611 cycles

DOOR 1L & 1R EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT STA B5-118 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9376629)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

DAMAGE T: HOLE CAUSED BY TOOLING DAMAGE ON ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00680: ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIRED PER PRI 606710-14 REV 1 AND PER ER/A NO. 606710-14 REV ORIGINAL, SECTION I, PERMANENT REPAIR. ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY 3,000 COMPONENT FLIGHT CYCLES AFTER SECTION I, PERMANENT REPAIR UNDER LP #2670884. (LP #2672344)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00679: DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIRED PER B717-200 SRM 51-70-13-2R-1. ALSO WEIGHT AND BALANCE ON ELEVATOR R/H WAS PERFOMED PER B717-200 SRM 51-60-02-0G, THE ELEVATOR R/H WEIGHT VALUE OF CHECKWEIGHTS SUSPENDED AND NOSE HEAVY MOMENT WERE 12.85LBS/-683.1 LBS/IN. (LP #2666487)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE). SUMMARY OF NRC 00479: CORROSION LEVEL: 2. LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE) WAS REPAIRED PER ER/A 605807-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 605807-14 REV 4. ASSOCIATED ER/A 14-605807 ADDED FOR AC 9553. (LP #2664997)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00682: CORROSION LEVEL 2. RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT AFT CARGO COMPARTMENT WERE REPLACED PER DWG 5936663 AND B717-200 SRM 51-41-01-0G. (LP #2656482)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

FOUR (4) CRACKS WERE DISCOVERED ON THE FUSELAGE SKIN. SUMMARY OF NRC 00157: PERMANENT REPAIR ON FUSELAGE SKIN WAS ACCOMPLISHED PER ER/A 566828-14 REV. B SECTION III: DAMAGE TOLERANCE PERMANENT REPAIR AND PRI 566828-14, REV. 3 AND ACCOMPLISH SECTION IV: GENERAL VISUAL INSPECTION EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION III: PERMANENT REPAIR. MONITORED UNDER LOG 2649251 PER ER/A 566828-14 REV B. ASSOCIATED ER/A 14-566828 ADDED FOR AC 9553. (LP #2653967)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00673: CORROSION LEVEL 2. FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1 REPAIR 1 FIGURE 212. (LP #2653627)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON LONGERON 30, BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00255: CORROSION LEVEL 2: LONGERON 30 BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT WAS PERMANENTLY REPAIRED PER B-717-200 SRM 53-20-05 REPAIR 1 PAR. 4 FIG. 201. (LP #2651320)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

CRACKS (2 EA) ON FRAMES AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. SUMMARY OF NRC 00320: FRAMES (2 EA) AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642050)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

RE-WRITE TO NRC #00493: DUE TO INADEQUATE STEERING OF THE RELATED STATIONS. THIS NRC IS TO CLARIFY THE CORRECT LOCATION FOR EACH STRUCTURAL ELEMENT. CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX BTW STA. Y=157 TO Y=200; AND BTW BL (X)=45 (-X)=45. SUMMARY OF NRC 00676: CORROSION LEVEL 2. FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX BTW STA Y=157 TO Y=200; AND BTW BL (X)=45 (-X)=45 WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2642303)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55. SUMMARY OF NRC 00518: CORROSION LEVEL 2. FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55 WERE REPLACED PER B717-200 SRM 51-41-08-0G, 51-41- 02-0G, AND DWG 5952262 REV: K, DWG 9936534 REV BW. (LP #2641075)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

AFTER REMOVAL OF FORWARD JAM PAN SEALS,CRACK WAS FOUND ON THE FWD SEAL. SUMMARY OF NRC 00626: REPAIR DOUBLER WAS INSTALLED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1 AND SRM 51-41-02-0G. (LP #2642198)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

CRACKS (3 EA) ON FRAMES AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. SUMMARY OF NRC 00319; FRAMES (3 EA) AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642292)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55. SUMMARY OF NRC 00519: CUSP WEB WAS FABRICATED PER DWG 9936535 REV CS AND CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55 WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4, 51-41-05-0G PAR 8, AND 51-41-08-0G PAR7. (LP #2637685)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

SECONDARY NRC IN REF NRC #00493: SEVERAL DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)=15 TO (-X)=42. SUMMARY OF NRC 00660: DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)= 15 TO (-X)=42 WERE REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2636349)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON L-22LH, Y STA 845 AT FILLET FAIRING STRUCTURE. SUMMARY OF NRC 00277: CORROSION LEVEL 2. LONGERON STA 845 STR 22LH WAS REPLACED PER DWG 5911420 REV: AE AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2636166)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

SECONDARY NRC, IN REF NRC 00618: CORROSION ON MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH. SUMMARY OF NRC 00650: CORROSION LEVEL 2. REPAIR OF MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH WAS PERFORMED PER B-717 SRM 53-00-55-2R REPAIR 4. (LP #2635227)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

A.A. A.D. CRACK WAS FOUND OF 0.437" LENGTH ON FRAME STA Y=715 RH SIDE IN REF CARD 5310-01436-04D JOB #074-0004 STEP: 13. SUMMARY OF NRC 00329: FRAME STA Y=715 RH SIDE WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G IN REF. A.A. WORK CARD: 5310-01436-03B. (LP #2633915)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1). SUMMARY OF NRC 00531: CORROSION LEVEL 2. FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2633854)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

WEAR ON CABLE TAIL CONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00290: CABLE TAIL CONE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52-01. (LP #2633730)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

CRACK ON INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00584: INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED AND REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 2, 51-41-02-0G, AND 51 -41-05-0G. (LP #2631523)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

IN REF NRC #00492: CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG 212 SHEET 1 AND 51-41-05-0G. (LP #2632152)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG.212 SHEET 1 AND 51-41-05-0G. (LP #2632222)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT. SUMMARY OF NRC 00331: CORROSION LEVEL 2. SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2629599)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON LH CENTER SEAT TRACK X=44 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00523: CORROSION LEVEL 2. LH CENTER SEAT TRACK AND SPLICE WAS REPLACED ON X=44 FROM STA Y=200 TO Y=256 PER B717-200 SRM 53-20-52-2R-PROCEDURE 5. (LP #2629217)

Part: NONE — NONE · airframe 48,027 hrs · 33,844 cycles

SECONDARY NRC, IN REF NRC 00488 CORROSION ON LH CUSP WEB BTW STA Y=560 - 579 AND BTW Y=609 TO 617. SUMMARY OF NRC 00612: CUSP WEB LH BTW STA Y=560 TO 579 AND BTW Y=609 TO 617 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP. 4 AND 51-41-02-0G. (LP #2628041)

Part: NONE — NONE · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00524: CORROSION LEVEL 2. RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2625411)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 48,027 hrs · 33,844 cycles

CORROSION ON ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX. SUMMARY OF NRC 00476: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I-2 AND 51-41-02-0G. (LP #2623765)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

IN REF NRC 00294: CRACK ON FWD PAN OF FWD CARGO DOOR ON BEAM 5. SUMMARY OF NRC 00628: FWD PAN OF FWD CARGO DOOR ON BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2621821)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

CRACK ON FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3. SUMMARY OF NRC 00294: FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2622016)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

CRACK ON INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE). SUMMARY OF NRC 00315: INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE) WAS FABRICATED AND REPLACED PER DWG 9955763 REV. M, B717-200 SRM 51-41-01-0G, 51-41-02 -0G, AND 51-41-05-0G. (LP #2622010)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 48,027 hrs · 33,844 cycles

IN REF TO NRC 00497: FABRICATE CUSP WEB. SUMMARY OF NRC 00497: CUSP WEB WAS FABRICATED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2618064)

Part: UNKNOWN — UNKNOWN · airframe 48,027 hrs · 33,844 cycles

WORN ON PREVIOUS REPAIR (2EA) OF FWD CARGO DOOR BARRIER LATCHES. SUMMARY OF NRC 00547: REPAIR DOUBLERS WERE REPLACED PER ER/A 559579-14MA REV ORIGINAL, SECTION I. PERMANENT REPAIR ASSOCIATED ER/A 14-559579 ADDED FOR AC 9553. (LP #2618071)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 48,027 hrs · 33,844 cycles

CRACK WAS FOUND AT AFT BRACKET OF LOWER LINNER SUPPORT BRACKETS. SUMMARY OF NRC 00619: AFT BRACKET (ANGLE) OF PASSENGER DOOR L1 IN LOWER INTERNAL STRUCTURE WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-02-0G AND DWG 5914121 REV. AV. (LP #2616255)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 48,027 hrs · 33,844 cycles

CRACK ON INTERCOSTAL OF CPAX FLOOR SUPPORT AT STA 636 AND X=0. SUMMARY OF NRC 00168: CRACK ON INTERCOSTAL OF CPAX FLOOR SUPPORT AT STA 636 AND X=0 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #2613685)

Part: NOT ENTERED — NOT ENTERED · airframe 48,027 hrs · 33,844 cycles

CRACK ON INTERCOSTAL IN L1 PASSENGER DOOR INTERNAL STRUCTURE AFT SIDE. SUMMARY OF NRC 00316: CRACK ON INTERCOSTAL IN L1 PASSENGER DOOR INTERNAL STRUCTURE AFT SIDE WAS REPAIRED PER B717-200 SRM 52-10- 02-2R-7 REPAIR 7. (LP #2608672)

Part: NOT ENTERED — NOT ENTERED · airframe 48,027 hrs · 33,844 cycles

CRACKED INTERCOSTAL ON INTERNAL STRUCTURE OF THE L1 PAX DOOR (FWD UPPER SIDE). SUMMARY OF NRC 00314: CRACKED INTERCOSTAL ON INTERNAL STRUCTURE OF THE L1 PAX DOOR (FWD UPPER SIDE) WAS REPAIRED PER B717-200 SRM 52-10-02-2R-8 REPAIR 8. (LP #2608676)

Part: NONE — NONE · airframe 47,145 hrs · 33,039 cycles

SHIP 9553 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC WHILE DUE TO THE #1 ENGINE BEING DIFFICULT TO CONTROL DURING CLIMB. THE ENGINE WAS NOT SHUT DOWN. THE LANDING AT THE SCHEDULED ARRIVAL AIRPORT WAS UNEVENTFUL. MAINTENANCE COULD NOT FIND ANY SOURCE FOR THE TROUBLE, BUT REPLACED BOTH THE HIGH-STAGE PNEUMATIC VALVE AND THE HIGH-STAGE PILOT VALVE. ALL ENGINE PARAMETERS CHECKED GOOD AND THE AIRCRAFT HAS RETUNED TO SERVICE. (LP #9059986)

Part: NONE — NONE · airframe 45,993 hrs · 31,996 cycles

DURING CCK AT QRO, A 0.500 INCH LONG CRACK AFFECTING SKIN 5936436-102 (M/F 0.050 INCH THICK 2024-T3 CLAD SHEET) AND A 1.800 INCH LONG CRACK AFFECTING INNER DOUBLER 5936436-39 (M/F 0.025 INCH THICK 7075-T6 CLAD SHEET) WERE FOUND AT STA 1022, BETWEEN L13R-L13R. LP #0465673 WAS CLOSED IN ERROR. OPENED NEW LOG. ACCOMPLISHED REINSPECTION PER ERA 566828-14 REV A SECTION II. NO FURTHER DAMAGE FOUND. UPDATED MASK TO REFLECT ERA 566828-14. **REDEFERRED LOG TO QC, ESTAB MON INSP **00-0653-8-3180 S/N 09553 REP **00-0653-8-3181 S/N 09553. DEF TASK STEPS: INSP TIME STANDARD HOURS CYCLES DAYS CHECK BY DATE INITIAL REPETITIVE 3000 TERMINATING 9000 COMPLETED--> INITIAL: REPETITIVE: TERMINATED: LOG UPDATE ONLY: Y. (LP #2133008)

Part: NONE — NONE · airframe 45,993 hrs · 31,996 cycles

CRACKS ON SCUFF PLATE AT AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00160: SCUFF PLATE WAS REPAIRED PER ER/A 542149- 14TR REV.B SECTION I: PERMANENT REPAIR. (LP #2130791)

Part: NONE — NONE · corrosion level 2 · airframe 45,993 hrs · 31,996 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0008: CORROSION LEVEL 2, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B-717 SRM 53-20-15-2R AND SRM 51-41-02-0G AND 51-41-05-0G PAR. 8 FIG. 12 AND 13. (LP #2130516)

Part: NONE — NONE · airframe 45,993 hrs · 31,996 cycles

CRACKED LONGERON 2 RH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00099: LONGERON 2 RH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2 FIG. 201. (LP #2123109)

Part: NONE — NONE · airframe 45,993 hrs · 31,996 cycles

CRACKED LONGERON 2 LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00100: LONGERON 2 LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2 FIG. 201. (LP #2123104)

Part: PSEU — FAILED (SLAT SYSTEM) · airframe 44,436 hrs · 30,632 cycles

SHIP 9553 - THE CREW DECLARED AN EMERGENCY FOR A PSEU FAILURE WITH ASSOCIATED SLAT OVER SPEED WARNING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE LEFT SLAT CHANNEL B PROXIMITY SENSOR. (LP #7568504)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,742 hrs · 30,090 cycles

THE TAILCONE SLIDE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY LIGHTS BATTERY, B5-116, PER B717 AMM 33-51. (LP #7593826)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,516 hrs · 29,913 cycles

ALL FOUR UPPER OVER WING EMERGENCY EXIT SIGNS HAVE INOPERATIVE LIGHTS. MAINTENANCE REPLACED THE BATTERY PACKS AT ROW 19EDC AND 20DC, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: GASKET — DAMAGED (RT MLG WW PANEL) · airframe 42,262 hrs · 28,815 cycles

RIGHT WHEELWELL SLANT PANEL LEAKING. GASKET IS DAMAGED. MAINTENANCE REPLACED THE SLANT PANEL GASKET REF B717 AMM 53-32-02. LEAK CHECK IS GOOD. (LP #1484805)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 41,996 hrs · 28,613 cycles

THE MID CABIN OVERHEAD EMERGENCY SIGN LENS IS MISSING. MAINTENANCE INSTALLED A NEW LENS. EEPL ARE OK FOR SERVICE PER B717 AMM 33-51. (LP #5371965)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,086 hrs · 27,267 cycles

AFT EQUIPMENT BAY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5551070)

Part: LEVER — OUT OF ADJUST (TAILCONE RELEASE) · airframe 38,603 hrs · 26,279 cycles

TAILCONE DEPLOYMENT FAILED TEST USING INTERNAL RELEASE HANDLE. READING LESS THAN MINIMUM REQUIREMENT. MAINTENANCE ADJUSTED BOTH BOTTOM AND UPPER RIGHT LATCH LEVERS IAW AMM 53-52-01 830-802. THE TAILCONE OPERATION NOW TESTS PROPERLY IAW AMDS W/C 5352-2001.

Part: SKIN — CRACKED (BS 1022) · airframe 37,471 hrs · 25,450 cycles

CRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 14R TO 15R. THE SKIN & DOUBLER WERE REPAIRED IAW ETI-17-18-047, REV 3, AND ER/A 566828-14, REV ORIGINAL.

Part: SKIN — DENTED (TE FLAP VANE) · airframe 37,461 hrs · 25,444 cycles

DENT ON RT FLAP LOWER MOVEABLE VANE LOWER SKIN -5" FROM OUT EDGE. RT FLAP LOWER MOVEABLE VANE LOWER SKIN WAS REPAIRED PER SRM 57-53-01-2R PROCEDURE 1 PAR 4 AND SRM 51-70-02.

Part: CHANNEL — CORRODED (FWD CARGO DOOR) · airframe 37,461 hrs · 25,444 cycles

WEAR ON THE CORNERS OF THE FWD CARGO DOOR BARRIER. LOWER FORWARD AND LOWER AFTER CORNERS OF DOOR BARRIER CHANNEL WERE BLENDED AND UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1, AND 2. FOUND OUT OF LIMITS AND LOWER AFTER EDGE OF DOOR BARRIER CHANNEL WAS REPAIRED IAW ER/A 559579-14 MA, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (NLG RT) · airframe 37,461 hrs · 25,444 cycles

CRACKED RT NLG DOOR FRAME BEAM BS 40. THE RT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AFTER THE DAMAGE WAS REMOVED. NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.

Part: SKIN — CRACKED (BS 1189) · airframe 37,461 hrs · 25,444 cycles

CRACKED FUSELAGE SKIN, BS 1189.604 LONGERON L22R. THE SKIN WAS REPAIRED IAW SRM 53-00-00-2R-1, FIGURE 201.

Part: LIFE VEST — OUT OF POSITION (CABIN) · airframe 36,892 hrs · 25,104 cycles

MAINTENANCE FOUND THAT THE LIFE VESTS WERE BLOCKING THE EMERGENCY EXIT DOOR AFTER THE REVENUE FLIGHT ARRIVED. THE LIFE VESTS WERE REPOSITIONED TO THEIR PROPER LOCATION PER B717 AMM 25-62. (LP #4135006)

Part: SHAFT — BROKEN (TAILCONE RELEASE) · airframe 35,514 hrs · 24,120 cycles

DURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THAT THE RELEASE SHAFT WAS BROKEN. MAINTENANCE REPLACED THE CAM LATCH/LOCK ASSEMBLY. THE TAILCONE WAS ADJUSTED AND RIGGED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII WAS COMPLETED FOLLOWING MAINTENANCE.

Part: LIGHT — OUT OF ADJUST (EXTERIOR) · airframe 34,990 hrs · 23,718 cycles

LT AFT EMERGENCY LIGHT INOPERATIVE. ADJUSTED LT AFT EXTERIOR EMERGENCY LIGHT PER B717 AMM 35-54. CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,994 hrs · 23,029 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO NORMAL OPERATIONAL CONDITION.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 33,969 hrs · 23,010 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN DIFFUSER COVER OVER DOOR L1 WAS DAMAGED. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,228 hrs · 22,439 cycles

DURING SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TWO CABIN EMERGENCY POWER SUPPLIES AND BATTERIES IAW AMM 33-51.

Part: OVEN — SMOKE (GALLEY) · airframe 32,979 hrs · 22,233 cycles

CREW REPORTED THE FORWARD GALLEY OVEN SMOKING FROM TOP VENT. CABIN CREW PULLED OVEN CIRCUIT BREAKER AND SMOKE SUBSIDED. MAINTENANCE FOUND PLASTIC INSIDE OVEN HAD BEEN BURNING. THE OVEN WAS REPLACED IAW AMM. COMPLIED WITH NO GO ODI PREVENTION FOR SMOKE IN CABIN.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,962 hrs · 22,225 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR THE FWD OVERWING HATCH WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CORRODED (BS 696-715) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 696 THROUGH 715, LBL 43 THROUGH LBL 59. VIEW FROM UNDER CABIN FLOOR BOARDS. REPARIED CENTER WING BOX UPPER SKIN BS 696 THROUGH 715, LBL 43 THROUGH LBL 59 IAW PRI 540753-14, REV 0-REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753 ADDED FOR AC 9553.

Part: CUSP WEB — DAMAGED (BS 656-715) · airframe 32,380 hrs · 21,737 cycles

CUSP WEB FROM BS 656-715, RT SIDE HAS A CRACK AND SEVERAL FASTENER HOLES TORN. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PAGE 298, REPAIR 4.

Part: SKIN — CORRODED (BS 696-715) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS, BETWEEN BS 696 THROUGH 715 RBL, 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN AT BS 696 THROUGH 715, RBL 43 THROUGH RBL 59 IAW PRI 540753-14, REV 0-REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753 ADDED FOR AC 9553.

Part: PAN — CRACKED (BS 756) · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN RT WINDOW PAN, BS 756 UPPER FWD CORNER CRACKED. REPLACED PASSENGER CABIN RT WINDOW PAN BS 756 IAW SRM 51-41-02 AND DWG 5936019, SHEET 3.

Part: SKIN — CORRODED (BS 715-737) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 715 THROUGH 737, LBL 43 THROUGH LBL 59, VIEW FROM UNDER CABIN FLOORBOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 715, THROUGH 737, LBL 43, THROUGH LBL 59 IAW PRI 540753-14, REV 0-REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753, ADDED FOR AC 9553.

Part: FRAME — CRACKED (BS 674) · airframe 32,380 hrs · 21,737 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD AREA RT SIDE BS 674 BETWEEN LONGERONS 23R AND 24R WING FRONT SPAR FWD FACE SUPPORT PLATE CRACKED IN RADIUS. REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD AREA RT SIDE BS 674 BETWEEN LONGERON 23R AND 24R WING FRONT SPAR FWD FACE SUPPORT PLATE IAW DG NR 5971094, SHT 1 AND SRM 51-40-08, SRM 51-40-02.

Part: CUSP WEB — DAMAGED (BS 655-715) · airframe 32,380 hrs · 21,737 cycles

BS 655-715, LBL 59, CUSP WEB DAMAGE AT INBD EDGE COMMON TO SEAT TRACK. REPAIRED CUSP WEB AT BS 655-715, RBL 59, LT SIDE IAW SRM 53-00-55, PAGE 298, REPAIR 4.

Part: SKIN — CORRODED (BS 674-696) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN STA 674 THROUGH 696, RBL 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 674 THROUGH 696, RBL 43 THROUGH RBL 59 IAW PRI 540753-14, REV 0-REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753, ADDED FOR AC 9553.

Part: FRAME — CRACKED (BS 674) · airframe 32,380 hrs · 21,737 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD AREA LT SIDE BS 674 BETWEEN LONGERONS 23L AND 24L WING FRONT SPAR FWD FACE SUPPORT PLATE CRACKED IN RADIUS. REPLACED FORWARD CARGO COMPARTMENT AFT BULKHEAD AREA LT SIDE BS 674 BETWEEN LONGERON 23L AND 24L WING FRONT SPAR FWD FACE SUPPORT PLATE IAW DWG 5971094, SHT 1 AND SRM 51-40-08, SRM 51-40-02.

Part: FUEL CELL — DAMAGED (BS 708) · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX FUEL TANK UPPER SKIN BS 708, RBL 50: 2 FASTENERS HOLES ELONGATED. REPAIRED CENTER WING BOX FUEL TANK UPPER SKIN AT BS 708, RBL 50, 2 FASTENER HOLES IAW PRI 540750-14, REV 0, PRI 540753-14, REV 0- REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753 ADDED FOR AC 9553.

Part: SKIN — CORRODED (BS 674-696) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 674 THROUGH 696, LBL 43 THROUGH LBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN BS 674 THROUGH 696, LBL 43 THROUGH LBL 59 IAW PRI 540753-14, REV 0-REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753 ADDED FOR AC 9553.

Part: SKIN — CORRODED (BS 715-737) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

CENTER WING BOX UPPER SKIN IS CORRODED IN SEVERAL LOCATIONS AROUND FASTENER HEADS BETWEEN BS 715 THROUGH BS 737, RBL 43 THROUGH RBL 59, VIEW FROM UNDER CABIN FLOOR BOARDS. REPAIRED CENTER WING BOX UPPER SKIN AT BS 715 THROUGH BS 737, RBL 43, RBL 59 IAW PRI 540753-14, REV 0 AND ER/A 540753-14, REV ORIGINAL ASSOCIATED ER/A 14-540753 ADDED FOR AC 9553.

Part: PAN — CRACKED (BS 794) · airframe 32,380 hrs · 21,737 cycles

PASSNEGER COMPARTMENT BETWEEN BS 794 AMD BS 813 FWD BOTTOM WINDOW PAN AFT OF BS 794 IS CRACKED AS MARKED IN CORNER LT SIDE. REPLACED PASSENGER COMPARTMENT WINDOW PAN LT BS 794 AND BS 813 IAW SRM 51-41-02 AND DWG 5936019, SHEET 1.

Part: SHEAR TIE — CORRODED (BS 889) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO BAY BILGE AREA, BS 889.5 BETWEEN LONGERON 30 AND 29L AREA SHEAR TIE IS CORRODED IN CORNER AS MARKED. REMOVED CORROSION ON AFT CARGO BS 889.5 SHEAR TIE BETWEEN LONGERON 30 AND 29L, REMOVED CORROSION IAW SRM 51-10-01. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. FABRICATED & LOCATED NEW SHEAR TIE IAW DWG 9915508, REV E. TREATED AND PRIMED IAW SRM 51-10-04. APPLIED TOP COAT IAW AMM 51-10-00-370-803. INSTALLED NEW SHEAR TIE IAW DWG 9915508, REV E. APPLIED CIC IAW SRM 51-10-01.

Part: LONGERON — CORRODED (BS 889) · airframe 32,547 hrs · 21,869 cycles

AFT CARGO BAY BILGE AREA, BS 889.50, LONGERON 30 AREA FRAME IS CORRODED TOP SURFACE IN BOTTOM CURVED FLANGE AS MARKED.

Part: STRUCTURE — CRACKED (BS 1200) · airframe 32,380 hrs · 21,737 cycles

TAIL SECTION INTERIOR UPPER LT SIDE BS 1200 CANT AFT END OF VENT BOX CRACKED.

Part: CARGO TRACK — CORRODED (BS 954) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO BAY AREA BS 954 BETWEEN LONGERON 28R AND 27R. TRACK IS CORRODED TOP SURFACE. BLENDED OUT CORROSION. .042 REMAINING FOUND TO BE OUT OF LIMITS IAW 53-20-52 SRM. FABRICATED NEW TRACK IAW DWG 5936663-535, ALODINED, PRIMED AND INSTALLED TOP COAT IAW SRM 51-10-04 & AMM 51-10-00. INSTALLED TRACK IAW SRM 51-40-02 AND DWG 5936663.

Part: DOOR SILL — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO DOOR LOWER SILL HAS MUTIPLE AREAS OF CORROSION. BLENDED OUT CORROSION. ORIGINAL .050 REMAINING .031, LOSS .019 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15. REPAIRED LOWER SILL IAW SRM 53-20-15, REPAIR 7.

Part: FRAME — CRACKED (LT MLG WW) · airframe 32,380 hrs · 21,737 cycles

LEFT WW UPPER FWD OTBD FRAME CRACKED. STOP DRILLED CRACK AT LT WHEEL WELL UPPER FWD OTBD FRAME AND COMPLETED REPAIR IAW SRM 53-20-02. REPAIR 3, RESTORED FINSHES. DOOR FIT AND FAIR AND LANDING GEAR RETRACTION FUNCTIONAL CHECKS ACCOMPLISHED ON JC 3230-2001 & 3210-2001.

Part: STRUCTURE — CRACKED (BS 1200) · airframe 32,380 hrs · 21,737 cycles

TAIL SECTION INTERIOR UPPER RT SIDE BS 1200 CANT AFT END OF VENT BOX CRACKED AT PREVIOUS REPAIR. REPAIRED CRACKED VENT BOX AT BS 1200 RT SIDE IAW ER/A 540752-14, REV 0, NO DEVIATIONS.

Part: THRESHOLD — CORRODED (BS 954-977) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO BAY BILGE AREA BS 954 TO BS 977 DOOR THRESHOLD WEB IS CORRODED 20 EA AREAS TOP SURFACE MARKED. BLENDED CORROSION FOUND TO BE 100 PERCENT MATERIALS LOSS. REPLACED WEB IAW SRM 51-40-02 AND DWGS NR 5910158.

Part: WEB — CORRODED (BS 947-954) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT PIT FORWARD DOOR CUTOUT THRESHOLD WEB CORRODED IN SEVERAL LOCATIONS BETWEEN STATIONS 947 AND 954. LONGERONS 26-25R MARKED. BLENDED OUT CORROSION ORIGINAL .040" REMAINING .028", LOSS .012". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-10, SRM 51-40-02.

Part: STRAP — CORRODED (BS 892) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO STRAP AT BS 892, LONGERON 30 IS CORRODED NEAR FASTENER ON UPPER SURFACE. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED NEW SPLICE ON WO 033609-1600-0006 INSTALLED IAW DWG 5919707.

Part: ANGLE — CORRODED (LT WW BULKHEAD) · corrosion level 2 · airframe 33,928 hrs · 22,975 cycles

LEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 30 INCHES OUTBOARD OF INBOARD WHEEL WELL BULHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PRI ER/A 540747-14 REV 0 AND ER/A 540747 ORIGINAL.

Part: ANGLE — CORRODED (LT WW BULKHEAD) · corrosion level 2 · airframe 33,928 hrs · 22,975 cycles

LEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIG. AND PRI ER/A 540747-14 REV O.

Part: ANGLE — CORRODED (RT WW BULKHEAD) · corrosion level 2 · airframe 33,928 hrs · 22,975 cycles

RIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 32,380 hrs · 21,737 cycles

AFT CARGO DOOR INTERNAL STRUCTURE AFT FRAME CRACKED ABOVE CENTER STOP FITTING. STOP DRILLED CRACKS, REMOVED FASTENERS, REMOVED FILLER FROM PAN. VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG 27991, CUT, FIT, LOCATED NEW DOUBLER & SHIMS IAW SRM 52-30-02 REPAIR 6. TREAT & PRIME NEW DOUBLER & SHIMS IAW SRM 51-10-04, STEP 15 AND STEP 21. INSTALLED REPAIR DOUBLER AND SHIMS IAW SRM 52-30-02, REPAIR 6. APPLIED TOPCOAT TO REPAIR IAW IAW AMM 51-10-00-370-805 AND INSTALLED DOOR SEAL IAW AMM 52-31-03-400-802, STEP. 1-7.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 32,380 hrs · 21,737 cycles

AFT CARGO DOOR INTERNAL STRUCTURE UPPER FWD CORNER FRAME CRACKED AT UPPER STOP FITTING. REMOVED DOOR SEAL, STOP DRILLED CRACKS, REMOVED FASTENER IN REPAIR AREA, REMOVED FILLER FROM PAN, VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG A63804, CUT, TRIMED AND LOCATED NEW DOUBLER REPAIR IAW B717 SRM 52-30-02 REPAIR 6 AND SHIMS, TREATED AND PRIMED NEW PARTS IAW SRM 51-10-04, STEP 15 & STEP 21 INSTALLED REPAIR DOUBLER AND SHIMS IAW SRM 52-30-02. REPAIR 6 APPLIED TOP COAT TO REPAIR AREA IAW AMM 51-10-00-320-805 AND INSTALLED DOOR SEAL IAW AMM 52-31-03-400-802, STEP 1-7.

Part: FLOOR PANEL — DAMAGED · airframe 32,380 hrs · 21,737 cycles

FLOOR PANEL 222SF DAMAGED. FABRICATED NEW HAT CHANNEL IAW DWG NR 9952521, REV BB ID:1, FRAME 1 OF 1. TREATED & PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 15 & 21. REPLACED NEW HAT CHANNEL TO FLOORBOARD IAW DWG 9952521, REV BB, ID: 1, FRAME 1 OF 1.

Part: BULKHEAD — CORRODED (BS 813) · corrosion level 2 · airframe 33,928 hrs · 22,975 cycles

AFT CARGO BAY BILGE AREA BS 813 BETWEEN LONGERON 28 AND 29R BULKHEAD HAS CORROSION. REPAIRED IAW ER/A 540745-14 REV O.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

LEFT CUSP WEB BETWEEN BS 465-484 HAS 3 AREAS OF CORROSION. LEFT CUSP WEB, FS 465-484 HAS 3 AREAS OF CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .004, .016 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLED & FABRICATED REPAIR DOUBLERS & INSTALLED, RESTORED ALL OF AREA TO ORIGINAL FINISH IAW SRM 51-41-01, 51-41-02, 51-41-06, 53-00-51, REPAIR 4, PAGE 257, FIG 208, AMM 53-22-01-401.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

LEFT CUSP WEB BETWEEN BS 446-465 HAS 2 AREAS OF CORROSION. LEFT CUSP WEB, FS 446-FS 465, 2 AREAS CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .005, .015 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLED & FABRICATED REPAIR DOUBLERS & INSTALLED, RESTORED ALL OF AREA TO ORIGINAL FINISH IAW SRM 51-41-01, 51-41-02, 51-41-06, 53-00-51. REPAIR 4, PAGE 257, FIG 208, AMM 53-22-01-401.

Part: ANGLE — CORRODED (LT MLG WW BLKHD) · corrosion level 2 · airframe 33,928 hrs · 22,975 cycles

LEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION, ROTOR PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIGINAL AND PRI ER/A540747-14 REV 0.

Part: HINGE FITTING — CRACKED (CARGO BAY) · airframe 32,380 hrs · 21,737 cycles

AFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FWD AND AFT ATTACH CLIPS CRACKED. REMOVED OLD, FABRICATED NEW, TREAT, PRIMED, APPLIED TOP COAT, APPLIED CIC. INSTALLED NEW AFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FWD AND AFT ATTACH CLIPS IAW SRM 51-10-04, PG 19-20, 24-25, 49-50, AMM 20-20-21-000-801, DWG 9919628, REV H, LABLED NEW PARTS IAW RSQM QC1-10-18, PAR 448.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 32,380 hrs · 21,737 cycles

PASSENGER FLOORBOARD 222AFF CRACK IN MIDDLE OF PANEL VERFIED MATERIAL FOR NEW HAT CHANNEL A TAG A53914 FABRICATED NEW HAT CHANNEL IAW DWG 9952521, REV BB ID1 FRAME 1 OF 1. TREATED AND PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 21 AND STEP 25 INSTALLED NEW HAT CHANNEL ON FLOORBOARD 222AFF IAW DWG 9952521, REV BB, ID1, FRAME 1 OF 1.

Part: SEAT TRACK — CORRODED (BS 522) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 522, RBL 22". REMOVED CORROSION ON PASSENGER CABIN INBD SEAT TRACK BS 522, RBL 22", CHECK MATERIAL ORIG "T" .115, LOSS OF .033, REMAINING MATERIAL OF .082 FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101, NEW SEAT TRACK INSTALLED ON JOB 4477156.

Part: SEAT TRACK — NOT REPORTED (BS 200-588) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

REPLACE MAIN CABIN SEAT TRACK BS 200-588, RBL 44.5. REPLACED SEAT TRACK BS 200-588, RBL 44.5 IAW DWG 5930547.

Part: SEAT TRACK — CORRODED (BS 488) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 488, RBL 22". REMOVED CORROSION OF CABIN SEAT TRACK AT BS 488, RBL 22 IAW SRM 53-20-52, PG 103, FIG 101 AND 51-10-04; FOUND TO BE WITH OUT LIMITS IAW SRM 53-20-52, FIG 101. REPLACEMENT OF SEAT TRACK REF WORK CARD 4477156.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN FLOOR PANEL 221ER HAS AREAS OF CORROSION ON FWD END OF PANEL. REMOVED CORROSION FROM FLOOR PANEL 221ER. PANEL WAS OUT OF LIMITS. NEW PANEL WAS LOCATED AND DRILLED TO FIT ACFT IAW DWG 9957828, REV AB ID:1 FRAME 2 OF 3, PANEL WAS TREATED & PRIMED AND TOPCOATED IAW 51-10-04-06-0, PAGE 21, PARAGRAPH 22, 51-10-04-06-0 PG 17, PARA 21 AMM-51-10-00-370-803.

Part: SEAT TRACK — CORRODED (BS 551) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 551, RBL 22". REPLACED PASSENGER CABIN INBD SEAT TRACK FROM BS 470 TO 580, RBL 22". TREATED AND PRIMED, TOPCOATED SEAT TRACK IAW SRM 51-10-04, PG 20,29, AND 49 AND INSTALLATION OF SEAT TRACK REF SRM 53-20-52 REPAIR 5.

Part: STRAP — CRACKED (DOOR FRAME) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

FORWARD CARGO COMPARTMENT DOOR JAMB LOWER SILL 4.5" SPLICE STRAP CORRODED 5" FWD OF LOWER FWD STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCPTABLE LIMITS ORGINAL MATERIAL .080 REF SRM 53-20-15, FIG 1, MATERIAL LOSS OF .040 USING SCRATCH GAUGE ID 35817, CAL DUE 09/15 ALLOWABLE LOSS IS .016 IAW SRM 53-00-00 FIG 103. REMOVED SPLICE -29 CLEANED AREA PRIMED AREA REF SRM AMM 51-10-00-370-803 INSTALLLED NEW SPLICE -29, REF SRM 51-41-02-0G-0 PA1-6 AND DWG NR 5910142-2, REV DG.

Part: DOOR FRAME — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

FORWARD CARGO COMPARTMENT DOOR JAMP LOWER SILL 4.5" SPLICE STRAP CORRODED 5" AFT STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCEPTABLE LIMITS, ORGINAL MATERIAL .080, REF SRM 53-20-15, FIG 1. MATERIAL LOSS OF .040 USING SCRATCH GAGE ID NR 35814 CAL DUE 09/15 ALLOWABLE LOSS IS .016 IAW SRM 53-00-00, FIG 103. REMOVED SPLICE -2G CLEANED AREA PRIMED AREA REF SRM 51-10-04, PA 18-21 TOP COATED SPLICE AND SILL AREA REF AMM 51-10-00-370-803 INSTALLED NEW SPLICE -29 REF SRM 51-41-02-0G AND DWG 5910142-2, REV DG.

Part: SEAT TRACK — CORRODED (BS 400) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CENTER SEAT TRACK CORRODED BS 400 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 323) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CTR SEAT TRACK CORRODED BS 323 RBL 43. REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 345) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CTR SEAT TRACK CORRODED BS 345 RBL 43. REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 295) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CENTER SEAT TRACK CORRODED BS 295 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 432) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CTR SEAT TRACK CORRODED BS 432 RBL 43. REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 460) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CENTER SEAT TRACK CORRODED BS 460 RBL 43. REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 608) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 608, RBL 22". REMOVED CORROSION, VERIFIED LIMITS, MAX MATERIAL LOSS -.020, MATERIAL LOSS .022, SEAT TRACK AT BS 608, RBL 22 OUT OF LIMITS. REMOVED SEAT TRACK SECTION 588-645, RBL 22, RECEIVED AND VERIFIED MATERIAL FABERCATED NEW SEAT TRACK SECTION, TREATED, PRIMED, APPLIED TOP COAT AND INSTALLED NEW SEAT TRACK SECTION, BS 588-645, RBL 22 IAW SRM 51-10-04, PG 19-21, 24-25, 28, 44-47,49. SRM 53-20-52, PG 104, 52-21-01-000-003, 51-41-05, PG 32, 63-21-01-400-803. DWG 5930565, REV BL.

Part: SEAT TRACK — CORRODED (BS 551) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CENTER SEAT TRACK CORRODED BS 551 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 488) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CTR SEAT TRACK CORRODED BS 488 RBL 43. REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 522) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

PASSENGER CABIN CENTER SEAT TRACK CORRODED BS 522 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.

Part: ATTACH BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 32,380 hrs · 21,737 cycles

RT WING FIXED L/E WING ROOT INBD SIDE WING TO BODY FAIRING MOUNT STRUCTURE ATTACH BRACKET CRACKED. REPLACED RT WING ROOT FIXED L/E WING TO BODY FAIRING MOUNT ATTACH BRACKET IAW SRM 51-42-02, PG 1-11 AND DWG 5919110 SH5.

Part: FLOOR SUPPORT — CORRODED (BS 180-188) · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 180-188 LBL 55. REMOVED OUT OF LIMITS FLOOR SUPPORT FABRCATED NEW SUPPORT AND INSTALLED AT CABIN FLOOR BS 154 TO 192 LBL -55 IAW SRM 51-40-02, 51-30-07, 51-40-08, 51-10-04.

Part: SEAT TRACK — CORRODED (BS 280) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

PASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 280, RBL 22. REMOVED CORROSION FROM SEAT TRACK AT BS 280, RBL 22" IAW SRM 53-20-52, PG 103, FIG 101 AND 51-10-04 USING A 10X MAG LENS. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, ALLOWABLE DAMAGE, FIG 101. REPAIRED IAW SRM 53-20-52, REPAIR 1, FIG 201.

Part: SEAT TRACK — CORRODED (BS 276) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

DURING LT SEAT TRACK INSPECTION, FOUND LT CENTER SEAT TRACK CORRODED TOP AND BOTTOM AT BS 276. REMOVED CORROSION ON SEAT TRACK AT BS 276, LBL 44.5. REPAIRED USING SEAT TRACK PLUG REPAIR IAW SRM 53-20-52. FIG 4, 201. AREA HAS BEEN TREATED, PRIMED, TOP COATED.

Part: FLOOR SUPPORT — CORRODED (BS 946-954) · corrosion level 2 · airframe 32,380 hrs · 21,737 cycles

AFT CARGO BAY BILGE AREA BETWEEN BS 954 AND BS 946, LONGERON 29R AND 30 FLOOR SUPPORT IS CORRODED TOP SURFACE WHERE CONECTS TO THE BILGE SKIN. BLENDED FLOOR SUPPORT AND CHECKED LIMITS IAW SRM 53-00-00. DAMAGE WAS 100 PERCENT MATERIAL LOSS. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-02 AND INSTALLED IAW DWG 9915578, ID1, REV A.

Part: SHIM — CORRODED (BS 986-994) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

AFT CARGO BAY THRESHOLD LT AND RT SHIMS FOR STRAP THAT GOES ON TOP OF DOOR THRESHOLD WEB BETWEEN BS 994 - 986, LONGERON 28 AND 29R CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 PAGE 105. FABRICATED NEW SHIM IAW DWG 5910158 REV DW. RESTROED FINISH IAW SRM 51-10-04.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 33,917 hrs · 22,969 cycles

CUSP WEB IS CORRODED BS 598 - 617, LBL 59. BLENDED CORROSION IAW SRM 51-10-04 AND SRM 53-00-55. ONE AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 53-00-55 REPAIR 4. INSTALLED REPAIR DOUBLERS AND FILLERS IAW SRM 53-00-55 REPAIR 4.

Part: FRAME — CRACKED (BS 715) · airframe 30,938 hrs · 20,580 cycles

DURING SCHEDULED INSPECTION, FOUND FRAME BS 715 CRACKED EXCEEDING 1.0. REPLACED THE FRAME IAW AMDS CARD 5310-01436-03A.

Part: FRAME — CRACKED (BS 696) · airframe 30,938 hrs · 20,580 cycles

DURING SCHEDULED INSPECTION, FOUND LT OVERWING FRAME BS 696 CRACKED EXCEEDING .25. REPLACED THE FRAME IAW AMDS CARD 5310-01436-03A AND COMPLETED REQUIRED INSPECTIONS.

Part: CUSP WEB — CRACKED (BS 660) · airframe 30,930 hrs · 20,570 cycles

DURING INSPECTION, FOUND CUSP WEB CRACKED AT BS 660. INSTALLED A REPAIR IAW 53-00-55.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,440 hrs · 20,191 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT ALL OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT P5-119 FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 30,243 hrs · 20,045 cycles

DURING LINE CHECK IN SAV, NOTED FWD RT + LT OVERWING UPPER EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51.

Part: STIFFENER — CRACKED (BS 737) · airframe 30,110 hrs · 19,929 cycles

BS 737, LBL 54 VERTICAL STIFFENER CRACKED. REPLACED IAW SRM 51-41-02, 51-10-04, 51-40-08 & 51-41-02.

Part: STIFFENER — CRACKED (BS 737) · airframe 30,110 hrs · 19,929 cycles

BS 737, RBL 54 VERTICAL STIFFENER CRACKED. REPLACED STIFFENER IAW SRM 51-41-02, 51-40-08 & 51-10-04.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 280,310 hrs · 18,135 cycles

L1 DOOR EMERGENCY EXIT SIGN BULB LOOSE. SECURED BULB IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 280,310 hrs · 18,135 cycles

R1 DOOR EMERGENCY EXIT SIGN BULB LOOSE. SECURED BULB IAW MM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 27,580 hrs · 17,849 cycles

FLOOR WEB DOUBLER CORRODED AT BS 200, LBL 12. REPAIRED DOUBLER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 27,580 hrs · 17,849 cycles

MAIN CABIN FLOOR PANEL 222ADF DELAMINATED. REPAIRED PANEL 22ADF IAW AMM & SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 27,580 hrs · 17,849 cycles

LT ELEVATOR GEARED TAB DELAMINATED AT OTBD HINGE. REPAIRED TAB IAW SRM.

Part: CABLE — DISCONNECTED (TAILCONE) · airframe 27,580 hrs · 17,849 cycles

AFT ACCESSORY COMPARTMENT TAIL CONE EXTERNAL RELEASE HANDLE INDICATOR CABLE DISCONNECTED. RECONNECTED CABLE IAW AMM.

Part: CLOSEOUT PANEL — CRACKED (RT WING) · airframe 27,580 hrs · 17,849 cycles

RT WING SLAT TRACK NR 10 LOWER CLOSE OUT PANEL CRACKED. R & R PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,580 hrs · 17,849 cycles

AFT CARGO BARRIER DOOR HINGE ATTACH POINT ANGLE CRACKED AT LOWER FASTENER HOLE. R & R ANGLE IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 27,580 hrs · 17,849 cycles

C 1 DOOR JAMB PAN CORRODED. R & R PAN IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 27,580 hrs · 17,849 cycles

C 2 DOOR PAN CRACKED ON FWD SIDE. REPAIRED PAN IAW SRM.

Part: COVER — LOOSE (R1 DOOR) · airframe 28,010 hrs · 18,119 cycles

R1 DOOR SLIDE COVER LOOSE. R & R SLIDE COVER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,204 hrs · 15,748 cycles

GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOP SEATS ROW 1, 2, 3 & 10. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY LOCATION #222BR OPS CHECKS GOOD IAW B717 AMM 33-51.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR IAW SRM 53-20-15 FIG 201 REPAIR 7, FIG 201.

Part: FRAME — DAMAGED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: WEB — CORRODED (FUSELAGE)

E/E COMPARTMENT CEILING WEB, STA 173 TO 200, LBL 7 TO RBL 7, CORROSION. ACCOMPLISHED CEILING WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, LBL 15 TO RBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: SAFETY WIRE — IMPROPER PART (EVAC SLIDE)

TAIL CONE SLIDE HAS .025 INCH STEEL LOCK WIRE & SEAL INSTALLED THROUGH RELEASE T-HANDLE. RESAFTIED TAIL CONE SLIDE T-HANDLE REF TASK CARD 17-2561-3143.

Part: LANYARD — BROKEN (EVAC SLIDE)

LANYARD ON L1 DOOR SLIDE BROKEN. REMOVED AND REPLACED DOOR SLIDE LANYARD IAW MM 25-61. A/C OK FOR SERVICE.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 SLIDE PACK PRESSURE INDICATES OUT OF GREEN BAND. L1 DOOR SLIDE REMOVED AND REPLACED IAW 25-61. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE)

CANTED BULKHEAD STA 1178 LONGERON 17 RIGHT, FRAME HAS 1.87 INCH CRACK. REPAIR ACCOMPLISHED PER EA 17-53-022931 IR, AND B717 SRM 51-70-11.

Part: FRAME — CRACKED (FUSELAGE)

CANTED BULKHEAD FRAME STA 1178 LONGERON 17 LEFT HAS 1.75 INCH CRACK. REPAIR ACCOMPLISHED PER EA 17-53-022931 IR, AND B717 SRM 51-70-11.

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT ON FUSELAGE SKIN STA 446 BETWEEN STR 24L AND 25L OUT OF LIMITS. INSTALLED REPAIR AS PER B717 SRM 53-00-01 REPAIR 2.

Part: SLIDE — UNWANTED DEPLOY (TAIL CONE)

TAIL CONE AND TAIL SLIDE INADVERTENTLY DEPLOYED. REINSTALLED TAIL CONE ASSEMBLY REF MM 53-52-01. A/C FERRIED TO ATL FOR FURTHER MAINT. REINSTALLED NEW TAIL CONE SLIDE PER MM 25-61.

Part: STRUCTURE — CRACKED (FUSELAGE)

AFT FUSELAGE RIGHT HAND VENT BOX IS CRACKED AT TOP AFT CORNER. INSTALLED REPAIR OF AFT FUSELAGE RIGHT SIDE VENT BOX DRAIN PAN.