N993AT

Part: PIN — BROKEN (ZONE 200) · airframe 62,138 hrs · 44,602 cycles

ATO- APPROX 80KTS DUE TO PREDICTIVE WINDSHEAR WARNING. FOUND COAXIAL CABLE PIN BROKEN. REPLACED SAME. OPS NORMAL.(7952152)

Part: UNKNOWN — ODOR (CABIN) · airframe 62,157 hrs · 44,618 cycles

FWD FAS SAYS THAT GOT A GOOD WIFT OF THE DIRTY SOCK SMELL ON CLIMB OUT. NO OTHER COMPLAINTS ON ACFT. FUME WAS SHORT TERM MAYBE A MINUTE OR TWO. TROUBLESHOT ODOR SMELL PER NO GO ODI PREVENTION REF TO LOG 1327715 FOR CORRECTIVE ACTION (7952142)

Part: LANYARD — UNSECURE (GIRT BAR) · airframe 61,651 hrs · 44,111 cycles

DOOR 1R EMERGENCY SLIDE ARMING BAR DETACHED AND BROKEN. MEM DELTA MX NOTIFIED. REINSTALLED GIRT BAR LANYARD ON 1R EMERGENCY SLIDE IAW AMM 25-61 (7587364)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 60,486 hrs · 43,031 cycles

THE EMERGENCY LIGHT SERVICE CHECK FOUND THE LIGHTED SIGNS ABOVE THE AFT OVERWING EXITS ON LEFT & RIGHT SIDES TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT IN REF WITH B717 WDM 33-51-11 PG 4 SHEET 3 OF 3, DELTA AVIONICS JOB AIDS TO EMERGENCY LIGHT BATTERY PACK B5-230. THE BATTERY IN THE BATTERY PACK WAS REPLACED IN REF WITH B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7093977)

Part: OVEN — CONTAMINATED (ZONE 900) · airframe 60,390 hrs · 42,943 cycles

SHIP 9538 -DIV/SMK/DE- THE FLIGHT CREW NOTED SMOKE IN COCKPIT WHILE ENROUTE TO MCI. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT WAS DIVERTED TO A NORMAL SAFE LANDING IN ORD. CORRECTIVE ACTION: MAINTENANCE INSPECTED THE GALLEY OVEN CONNECTOR, AND NO TROUBLE WAS FOUND. DURING REPLACEMENT OF THE OVEN, BURNT RESIDUE WAS DISCOVERED IN THE OVEN CUBICLE. OPERATIONAL CHECK OF THE OVEN WAS GOOD. (LP #6911289)

Part: UNION — LEAKING (ZONE 700) · airframe 59,978 hrs · 42,597 cycles

SHIP 9538 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE RIGHT HYDRAULIC SYSTEM SHOWING A LOSS IN QUANTITY. THE QRH WAS COMPLIED WITH, BUT AN ALTERNATE GEAR EXTENSION WAS NOT REQUIRED. CORRECTIVE ACTION: MAINTENANCE CYCLED THE MLG DOORS WITH THE GEAR HANDLE UP AND FOUND THE MAIN LANDING GEAR CONTROL VALVE UNION LOOSE AND LEAKING. MAINTENANCE REPLACED THE O-RING AND RESECURED THE UNION. LEAK CHECK WAS GOOD. (LP #6930946)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,915 hrs · 42,544 cycles

DURING THE SERVICE CHECK THE FWD OVERWING EMERGENCY EXIT UPPER DOOR LIGHTS ON BOTH LT & RT SIDE WERE FOUND NOT ILLUMINATED. MAINTENANCE REPLACED THE B5-121 BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #6930904)

Part: NONE — NONE (NONE) · airframe 59,915 hrs · 42,544 cycles

-AD- ACCOMPLISH ER/A 622306-14AD SECTION I B717 FUSELAGE STA 1178.558 ALTERNATIVE INSPECTION FOR PREVIOUS REPAIR. ACCOMPLISH ER/A 622306-14AD SECTION I FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-622306 ADDED FOR AC 9538. **REDEFERRED LOG TO QC, ESTAB MON INSP** COMPLIED WITH ER/A 622306-14AD SECTION 1 REV ORIGINAL. NO FURTHER DAMAGE FOUND. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 04DEC24 AND LOG COMMENTS. (LP #0656471)

Part: HPC — DAMAGED (RT ENGINE) · airframe 58,871 hrs · 41,619 cycles

SHIP 9538 -ATO- ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO SUSPECTED RIGHT ENGINE SUSPECTED COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND DAMAGE TO 3RD AND 4TH STAGE HPC. REPLACED RIGHT ENGINE. (LP 5271438)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,683 hrs · 41,449 cycles

THE AFT ACCESORY COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY LIGHT BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-03. OPERATIONAL TESTS ARE GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5731034)

Part: RELEASE CABLE — MISROUTED (DOOR SLIDE) · airframe 58,683 hrs · 41,449 cycles

IMPROPER ROUTING OF MANUAL RELEASE CABLE FOR SLIDE AT FORWARD SERVICE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00695: MANUAL INFLATION CABLE FOR SLIDE AT FORWARD SERVICE WAS REINSTALLED CORRECTLY PER B717-200 AMM 25-61-03 400- 801. (LP #0350278)

Part: PAN — CRACKED (BS 403-413) · airframe 58,681 hrs · 41,448 cycles

CRACK ON PAN LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 FWD CARGO DOOR. SUMMARY OF NRC 00212: INNER AND OUTER PAN ON LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 AT FWD CARGO COMPARTMENT DOOR WERE REPAIRED PER ER/A 617729-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617729-14 REV 5. ASSOCIATED ER/A 14-617729 ADDED FOR AC 9538, (LP #0348611)

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 58,681 hrs · 41,448 cycles

DURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC SERIAL 00682: FORWARD ENTRY PASSENGER DOOR SLIDE ASSEMBLY WAS REPLACED WITH SERVICEABLE SLIDE ASSEMBLY PER B717 AMM 25-61-01 AND PART NUMBER WAS VERIFIED PER B717-200 IPC25-61-50-01 ITEM -001J. (LP #0347356)

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 58,681 hrs · 41,448 cycles

DURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 682: FORWARD ENTRY PASSENGER DOOR SLIDE ASSY WAS REMOVED AND REPLACED WITH A SERVICEABLE SLIDE ASSY PER B717 AMM 25-61-01 AND PART NUMBER WAS VERIFIED PER B717-200 IPC25-61-50-01 ITEM -001J. (LP #0347161)

Part: HINGE — EXCESS PLAY (LT WING TE FLAP) · airframe 58,681 hrs · 41,448 cycles

FREEPLAY ON JOINT BTW FLAP AND FLAP OUTBD HINGE AT LH WING. LT WING FLAP OUTBD HINGE WAS REPAIRED IN ACCORDANCE WITH PRI 617504-14 REV 2 AND ER/A 617504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 09MAY24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IAW PROCEDURES ESTABLISHED IN FAA AC 120-93. ASSOCIATED ER/A 14-617504 ADDED FOR ACFT.

Part: STRAP — CORRODED (BS 200-208 L18L) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON WEB STRAP BTW STA Y=200/208 AND LONGERON 18L. (PAX CAB). SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB STRAP BTW STA Y=200/208 AND LONGERON 18L WAS REPAIRED PER ER/A 617656-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617656-14 REV 0. ASSOCIATED ER/A 14-617656 ADDED FOR ACFT.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION WAS FOUND ON HSTB HOLE #27 RH. SUMMARY OF NRC 00650: RH HORIZONTAL STABILIZER BARREL NUT HOLE #27 WAS REPAIRED IN ACCORDANCE WITH ER/A 617762-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS: REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 12MAY24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. UNDER LOG PAGE #0342523. ASSOCIATED ER/A 14-617762 ADDED FOR AC 9538. (LP #0344903)

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 58,681 hrs · 41,448 cycles

CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00679: CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1. (LP #0343135)

Part: VANE — DENTED (RT WING TE FLAP) · airframe 58,681 hrs · 41,448 cycles

DENTS ON AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING. SUMMARY OF NRC 00238: AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING WAS REPAIRED PER ER/A 617597-14 REV ORIGINAL. ASSOCIATED ER/A 14-617597 ADDED FOR AC 9538. (LP #0342649)

Part: DOUBLER — CORRODED (BS 617-636) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTEMENT. SUMMARY OF NRC 00631: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 617630-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617630-14 REV 3 AFTER ACCOMPLISHMENT OF SECTION I REPAIR, ACCOMPLISH AN INITIAL INSPECTION PER SECTION II WITHIN 8,000 FLIGHT CYCLES AND THEN ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 8,000 FLIGHT CYCLES THEREAFTER. PER ER/A 617630-14 REV. ORIG. SECTION II, UNDER LOG. 0340849. 0340849. (LP #0342313)

Part: SUPPORT ANGLE — CRACKED (BS 1022) · airframe 58,681 hrs · 41,448 cycles

CRACKS (2 EA) ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L ALSO 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA. SUMMARY OF NRC 00400: CRACK ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA WAS REPAIED PER ER/A 617503-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617503-14 REV 4 AND ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0340730)

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 58,681 hrs · 41,448 cycles

CRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0002: SCUFF PLATE AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 542149-14TR REV B, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-542149 ADDED FOR AC 9538. (LP #0339236)

Part: PAN — CRACKED (AFT CARGO) · airframe 58,681 hrs · 41,448 cycles

CRACKS ON PAN FWD EDGE AND AFT EDGE BETWEEN BEAM #2 AND #3 AT AFT CARGO DOOR. SUMMARY OF NRC 00366: AFT CARGO DOOR ASSY WAS REMOVED PER AMDS 5231-4002, WAS REPLACED WITH SERVICEABLE AFT CARGO DOOR ASSY, AND WILL BE INSTALLED WITH AMDS 5231-4004. (LP #0336365)

Part: FRAME — CORRODED (BS 870 L29L&R) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. (LP #0334766)

Part: ANGLE — CORRODED (BS 157-200) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200. SUMMARY OF NRC 00345: CORROSION LEVEL 2. CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200 WAS REPAIRED PER PRI 617406-14 REV 2 AND ER/A 617406-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #0333332)

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN. SUMMARY OF NRC 00415: CORROSION LEVEL 2. FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV B AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0330065)

Part: FLOOR SUPPORT — CORRODED (BS 157-200) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV WB AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0331695)

Part: FRAME — CRACKED (BS 1178) · airframe 58,681 hrs · 41,448 cycles

CRACK ON FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA. SUMMARY OF NRC 00401: FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA WAS REPAIRED PER B717 SRM 53-30-08-2R. PERFORM A VISUAL INSPECTION EVERY "C" CHECK REPETIVE NORMAL MAINTENANCE PER B717 SRM 53-30-08-2R PROCEDURE 10 PAR 6, TABLE 202. (LP #0324974)

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,681 hrs · 41,448 cycles

CRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA WAS REPAIRED PER PRI 617480-14 REV 1 AND ERA 617480-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617480.

Part: BULKHEAD WEB — CRACKED (BS 218) · airframe 58,681 hrs · 41,448 cycles

CRACKED BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00647: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0321848)

Part: CUSP WEB — CORRODED (BS 217-237) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB. SUMMARY OF NRC 00346: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 209. REPLACED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 209 AND 51-41-02-0G PAR. 4. (LP #0319981)

Part: CUSP WEB — CORRODED (BS 889-908) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN. SUMMARY OF NRC 00396: CORROSION LEVEL 2. LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND PER DWG 9910151 REV CH. (LP #0315344)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 58,681 hrs · 41,448 cycles

ELONGATED HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS FOUND STA ZFS=52.267 IN REF NRC 0525. SUMMARY OF NRC 00611: HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS REPAIRED PER B717-200 SRM 55-30-01-2R PROCEDURE 6. (LP #0313974)

Part: CUSP WEB — CRACKED (BS 663) · airframe 58,681 hrs · 41,448 cycles

CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN. SUMMARY OF NRC 00394: CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0307832)

Part: LONGERON — CRACKED (BS 1022 L5L&R) · airframe 58,681 hrs · 41,448 cycles

CRACKS ON LONGERON (3 EA) 5L, 5R, AND 17L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA. SUMMARY OF NRC 0245: LONGERON (2 EA) 5L & 5R AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA WERE REPAIRED PER B-717-200 SRM 53-00-05-2R REPAIR 2 AND LONGERON 17LH STA Y=986 TO 1052 WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05 0G. (LP #0306748)

Part: MEMBRANE — CORRODED (BS 200-270) · corrosion level 2 · airframe 58,681 hrs · 41,448 cycles

CORROSION ON LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN IN REFERENCE NRC 00391. SUMMARY OF NRC 00591: CORROSION LEVEL 2. LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0301180)

Part: CUSP WEB — CRACKED (BS 606) · airframe 58,681 hrs · 41,448 cycles

CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN PAX. SUMMARY OF NRC 00393: CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN, WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0300915)

Part: BULKHEAD WEB — CRACKED (BS 218) · airframe 58,681 hrs · 41,448 cycles

CRACKED BULKHEAD WEB SYA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00283: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0290830)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,304 hrs · 41,115 cycles

SHIP 9538 -ATB/GEAR/DE- THE AIRCRAFT WAS RETURNED TO THE DEPARTURE AIRPORT AFTER THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE DISCOVERED THE GROUND SENSING MECHANISM WAS OUT OF ADJUSTMENT. AFTER BEING RE-ADJUSTED THE GROUND SENSING SYSTEM CHECK GOOD AND ALL GEAR SWINGS WERE NORMAL. (LP #4294462)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,181 hrs · 40,130 cycles

LIGHTING STRIKE FOUND AT STA 1189 AT RBL 2 AT A FASTENER. LIGHTING STRIKE STA 1189 FOUND TO BE OUT OF LIMITS PER B717 SRM 53-01-01-A1 PROCEDURE 2. CUTOUT DAMAGE, FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND FILLER IAW B717 SRM 53-00-00-2R-2. TREATED AND PRIMED DOUBLER AND FILLER IAW B717 SRM 53-00-00-2R-2. INSTALLED DOUBLER AND REPAIR FILLER AT STA 1189 RBL 2 IAW B717 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2818929)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,198 hrs · 40,145 cycles

LIGHTING STRIKE FOUND AT STA 106 AT LBL 5 AWAY FROM FASTENER DRILLED OUT DAMAGE TO .311 PER B717 SRM 53-02-01-2R REPAIR 1. BHEC INSPECTED OPEN HOLE PER B717 SRM 53-02-01-2R REPAIR 1 WITH NO DEFECTS NOTED. FABRICATED, LOCATED. AND DRILLED REPAIR DOUBLER IAW B717 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. TREATED, PRIMED, AND INSTALLED DOUBLER IAW B717 SRM 53-00-00-2R.(LP #2819325)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,600 hrs · 39,634 cycles

AIRCRAFT 9538, EMERGENCY LIGHTS ROW 3-11 INOP. CORRECTIVE ACTION: REPLACED THE BATTERY PACK B5-227. (LP 9653534)

Part: LAMP — FAULTED (EMERGENCY LIGHT) · airframe 56,068 hrs · 39,201 cycles

F/A REPORTS THAT THE EMERGENCY EXIT SIGN OVER DOOR 1L IS FLASHING DURING FLIGHT. MAINTENANCE RELAMPED THE EMERGENCY EXIT SIGN AT 1L. OPERATIONAL CHECK IS OK REF B717 AMM 33-50. (LP #9501344)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 56,005 hrs · 39,144 cycles

LEFT WING, CORROSION FOUND AROUND FUELING CAP. REMOVED CORROSION AT XRS 425 STR 2 LT WING AND REPAIRED IAW ERA 604553-14 REV O. ASSOCIATED ER/A 14-604553.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 56,005 hrs · 39,144 cycles

LEFT WING UPPER SURFACE: PAINT BUBBLING WITH EVIDENCE OF POSSIBLE CORROSION AT TWO LOCATIONS JUST AFT OF #3 SLAT. REMOVED CORROSION AT XRS 317 STR 2 LH WING AND REPAIRED PER ERA 604553-14 REV O, SRM 57-10-01-1A PROCEDURE 1.

Part: FLOOR SUPPORT — CORRODED (BS 192-200) · corrosion level 2 · airframe 56,005 hrs · 39,144 cycles

CORROSION ON FLOOR SUPPORT AT RBL 7 STA 192-200. SUMMARY SEE NRC 001-0010 2500-2647/058 00306: REPLACED FLOOR SUPPORT REF B-717 DWG 9936534. (LP #2540869)

Part: SUPPORT — DAMAGED (GIRT BAR) · airframe 56,005 hrs · 39,144 cycles

THE R-1 DOOR CUTOUT GIRT BAR SUPPORT BACKUP FITTINGS SUPPORT WEB IS DAMAGED. REPLACED SUPPORT REF DWG 9957828.

Part: NONE — NONE · corrosion level 2 · airframe 56,446 hrs · 39,499 cycles

CORROSION ON FLOOR SUPPORT AT LBL 7 STA 178-200. SUMMARY SEE NRC 001-0010:2500-2647/059 00307: TREATED AND PAINTED AREA, REPLACED FLOOR SUPPORT REF BOEING DWG 9936534. (LP #2537090)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,998 hrs · 39,140 cycles

THE AFT CATWALK EMERGENCY EXIT LIGHTS ARE OUT. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY IN THE AFT CABIN LOWERED CEILING. OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,973 hrs · 39,121 cycles

DURING TRANSIT CHECK, FOUND AFT BULKHEAD EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY IAW AMM 33-51. CHECK WAS GOOD. AIRCRAFT READY FOR SERVICE.

Part: NONE — NONE · airframe 54,059 hrs · 37,441 cycles

A FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN AT L1 DOOR IS FLICKERING. MAINTENANCE REPLACED THE B5-235 BATTERY PACK. OPERATIONAL CHECK IS GOOD. (LP #8380198)

Part: NONE — NONE · airframe 54,012 hrs · 37,394 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN TO LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001. FUNCTIONAL CHECK WAS SATISFACTORY. (LP #8380172)

Part: NONE — NONE · airframe 53,801 hrs · 37,187 cycles

THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN AT THE TAILCONE IS INOPERATIVE. MAINTENANCE RELAMPED THE EMERGENCY EXIT SIGN LIGHTS AT THE TAILCONE PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #2042081)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,072 hrs · 36,520 cycles

FOUND THAT THE EMERGENCY LIGHTS AT B5-260 BATTERY LOCATION WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT BATTERY LOCATION B5-260 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7807254 )

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 52,278 hrs · 35,877 cycles

UPON POWER UP FOR THE FIRST FLIGHT OF THE DAY, THE AFT TAILCONE EMERGENCY EXIT LIGHT WOULD CONTINUE TO BLINK ON AND OFF. REPOWERED UP THE AIRCRAFT WITH THE SAME ISSUE. ALSO, THE ENTIRE TAILCONE LIT UP AS WELL. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY POWER SUPPLY LOCATED BETWEEN THE 2 AFT LAVATORIES PER AMM 33-51-03. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6877103)

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 52,250 hrs · 35,858 cycles

THE CAT WALK LOWER EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-260 TO BE FAULTING. THE EMERGENCY LIGHT BATTERY POWER SUPPLY B5260 WAS REPLACED PER B717 AMM 33-51-03. ALL EMERGENCY LIGHTS NOW CHECK GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6872290)

Part: RIB — CORRODED · corrosion level 2 · airframe 52,054 hrs · 35,711 cycles

CORROSION AT STA 927 BOTTOM OF RIB FROM LONGERONS 29R TO 29L. MARKED IN RED REF N/R 351. TRANSFERRED FROM NRC 217. REPAIRED REF B717 SRM 53-20-07-2R. (LP #1729895)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 52,141 hrs · 35,779 cycles

THE AFT CARGO LOWER DOOR JAMB IS CORRODED IN NUMEROUS PLACES - MARKED. MAINTENANCE REPAIRED REF B717 SRM 53-20-15-2R PROCEDURE 7. (LP #1725722)

Part: PRESSURE BLKHD — PUNCTURED (BS 110) · airframe 51,954 hrs · 35,629 cycles

WORKING PRI 589215-14 TO REPAIR WHERE THE PRESSURE BULKHEAD, AT STA 110, HAD BEEN PUNCTURED BY CONTACT WITH LANDING GEAR STRUCTURE. COMPLETED PRI 589215-14 REV 0 1 2 3 4. COMPLETING ER/A 589215-14 REV A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,575 hrs · 35,283 cycles

IT WAS NOTED THAT THE EMERGENCY LIGHT L2-790 FORWARD SIGN ASSEMBLY WENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235 PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #6812995)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,157 hrs · 34,898 cycles

AFT EQIPMENT COMPARTMENT EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY B5-260 PER B717 AMM 33 -51. (LP #6520568)

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,602 hrs · 34,406 cycles

DURING SERVICE CHECK, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THE POWER SUPPLY BATTERY B5-235 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT IS OK FOR SERVICE. (LP #6694852)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,301 hrs · 33,415 cycles

THE EMERGENCY LIGHT BATTERY CHARGER AT 25E WENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER IAW B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6141432)

Part: SKIN — CORRODED (RT SPOILER)

SKIN CORROSION AND LIGHTNING STRIKE DAMAGED O/B SPOILER UPPER SURFACE.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHTS) · airframe 48,248 hrs · 32,694 cycles

MULTIPLE EMERGENCY LIGHT INTERIOR BULBS WERE OUT IN THE TAIL COMPARTMENT. MAINTENANCE RELAMPED ALL OF THE TAIL CONE EMERGENCY SIGNS.

Part: SKIN — DAMAGED · airframe 47,904 hrs · 32,444 cycles

UNIDENTIFIED REWORKED AREA ON WING SKIN, UPPER SURFACE, AFT OF FRONT SPAR AFT OF #3 SLAT. (M). NRC 001-0296 5720-2003/002 00152: PRI 575373-14 REV A REV O-1. REWORKED AREA WAS REPAIRED PER ER/A 575373-14 REV A ITEMS 1-12. (LP #0946139)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 47,904 hrs · 32,444 cycles

REF AA 5530-01048 AND AD 2018-10-08RIGHT HAND SIDE VERTICAL STAB LEADING EDGE ATTACH (2EA) HOLES HAVE CRACK INDICATIONS, FIRST 2 HOLES ABOVE SPLIT LINE (MKD). NRC 075-0001:5530-01048-02/002 00226: PRI 575376-14 REV 0-1. CRACK WAS REPAIRED PER ER/A 575376-14 REV 0. (LP #0943047)

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,835 hrs · 32,397 cycles

CORROSION ON AFT CARGO DOOR JAMB. REPLACED DOOR JAMB REF SRM 53-20-15-2R PROC 7.

Part: LEVER — NO TEST (TAILCON) · airframe 46,020 hrs · 31,125 cycles

DURING TAILCONE DROP TEST, THE EXTERNAL TAILCON RELEASE FAILED THE TEST. ADJUSTED THE LOCK PIN LEVER AND NOW OPS CHECKED GOOD IAW AMM 53-52-01 830-802.

Part: CHANNEL — CRACKED (BS 749) · airframe 42,752 hrs · 28,889 cycles

CRACK ON CHANNEL BS 749 INBD EDGE AT RT MLG INNER DOOR. THE CHANNEL WAS REPAIRED IAW ETI-17-17-025, REV 5, AND ER/A 554172-14, REV ORIG.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

RT MLG WHEEL WELL CORROSION ON CTR FUEL TANK SKIN STA Y=755 AND X=-50 AT SLANT PRESSURE PANEL AREA 5310-2003 (FYT). CORROSION WAS ATTENDED PER ETI-17-17-022 REV 4 AND ER/A 554158-14 REV ORIGINAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

WING BOX CABIN AREA CORROSION ON UPPER FACE WING BOX RT BTW STA Y=674 TO 696 X=-54 TO X=-60 (WING BOX). REPAIR WAS ACCOMPLISHED PER ETI-17-17-022 REV 4 AND ER/A 554158-14 REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 812-1022) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON CARGO TRACK BS 812 - 1022. THE CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26 AND FOUND OUT OF LIMITS IAW SRM 53-20-52 101. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-41-01, AND SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FLOOR SUPPORT UNDER FIRST OFFICER`S SEAT TRACK, BS 120 TO 145, RBL 28. THE SEAT TRACK WAS REPLACED IAW 51-41-01 AND 53-10-51 FIG1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 42,752 hrs · 28,889 cycles

FWD CARGO DOOR HAD A CRACKED INNER PAN ON BEAM NR 5 AT BS 419. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R, REP. 1.

Part: INTERCOSTAL — CRACKED (BS 377) · airframe 42,752 hrs · 28,889 cycles

FWD CARGO BAY HAS A CRACK ON INTERCOSTAL BS 377 UPPER SIDE AT FWD CARGO DOOR. THE CRACKED INTERCOSTAL WAS REPLACED IAW SRM 51-41-02 0G AND 51-41-05.

Part: LONGERON — CORRODED (BS 1002-1008) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

AFT CARGO BAY HAD CORROSION ON LONGERON 24R, BS 1002 - 1008, THE LONGERON WAS REPLACED IAW SRM 51-41-05.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 42,752 hrs · 28,889 cycles

CRACK INNER PAN AND FITTING ON BEAM NR 1 LOWER EDGE AT STA: Y= 408 FWD CARGO COMPARTMENT DOOR STRUCTURE. TASK CARD NR 0088-0644: 52-31-2005/021. FINDING REPAIRED PER SRM 52-30-02 2R-1 REP 1. FITTING WAS REMOVED PER SRM 51-41-01 0G AND 51-41-05 0G. NEW FITTING WAS FABRICATED PER DGW 3926046. NEW FITTING WAS INSTALLED PER SRM 51-41-01 0G AND 51-41-05 0G. SEAL RETAINER WAS INSTALLED PER SRM 51-41-01 0G.

Part: FRAME — CORRODED (BS 908) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FRAME ANGLE BS 908, LONGERONS 26L - 26R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS FABRICATED AND INSTALLED IAW DWG 9912243 REV.JS.

Part: BEAM — CRACKED (NLG WW) · airframe 42,752 hrs · 28,889 cycles

CRACK ON BEAM LT SIDE X=18 BTW STA Y=37 TO 69 APPROX AT NOSE WHEEL WELL. BEAM LT WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIG 201 AND 51-41-02, 51-41-05.

Part: BEAM — CRACKED (NLG WW) · airframe 42,752 hrs · 28,889 cycles

CRACK ON BEAM RT SIDE X=-18 BTW STA Y=37 TO 69 APPROX AT NOSE WHEEL WELL. BEAM RT WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIG 201 AND 51-41-02, 51-41-05.

Part: PAN — CRACKED (CARGO DOOR) · airframe 42,752 hrs · 28,889 cycles

CRACK IN FWD INNER PAN BELOW BEAM NR 5 ON THE FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02 2R-1, REP 1.

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON RUBSTRIP OF LT WING ACCESS PANEL. THE RUBSTRIP WAS REPLACED IAW SRM 57-10-01- REP. 3 PAR. 6.

Part: CHANNEL — CRACKED · airframe 42,752 hrs · 28,889 cycles

CRACK ON CHANNEL OF FLOOR PANEL. REPAIRED IAW SRM 51-20-05.

Part: FRAME — CRACKED (BS 694) · airframe 42,752 hrs · 28,889 cycles

CRACKED FRAME ANGLE BS 694 IN THE MLG WW. REPAIRED IAW SRM 51-70-11-2R.

Part: GRILL — CORRODED · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON RT AIR GRILL FRAME NR 1. THE AIR GRILL FRAME WAS REPAIRED IAW SRM 51-70-11-2R, FIG 201.

Part: ANGLE — CRACKED (LT OVERWING DOOR) · airframe 42,752 hrs · 28,889 cycles

CRACKED AFT UPPER ANGLE INTERNAL STRUCTURE ON LT FWD OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735 REV: G.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 42,752 hrs · 28,889 cycles

CRACKED FWD UPPER ANGLE INTERNAL STRUCTURE OF THE RT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735 REV G.

Part: ANGLE — CRACKED (OVERWING EXIT) · airframe 42,752 hrs · 28,889 cycles

CRACKED AFT UPPER ANGLE NR 2 ON INTERNAL STRUCTURE OF THE RT FWD OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735 REV G, AND SRM 51-41-05.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON FLOOR PANEL 221S. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50, FIG 202, SHEET 1. STOP DRILLED AND NO CRACKS WERE FOUND IAW SRM 53-20-50, FIG. 202.

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON RUB STRIP OF FUEL ACCESS PANEL ON RT WING. THE RUB STRIP WAS REPLACED IAW SRM 57-10-01 2R-3, REP 3, PAR 6.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 42,752 hrs · 28,889 cycles

CRACKED DOOR FRAME WEB BS 207 LONGERON 11L. THE DOOR FRAME WEB WAS REPAIRED IAW SRM 53-10-15-2R.

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON RT RUB STRIP AT UPPER FUEL ACCESS DOOR 620FT. THE CORROSION WAS REMOVED IAW SRM 57-10-01 2R-3, REP 3, PAR 6.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 42,752 hrs · 28,889 cycles

DELAMANATED FLOOR PANEL IN THE COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FUEL TANK ACCESS PANEL 620FT AND 620DT. REPLACED THE ACCESS PANELS.

Part: FRAME — CRACKED (BS 679) · airframe 42,752 hrs · 28,889 cycles

CRACKED FRAME ANGLE BS 679, MLG WHEEL WELL CANTED KEEL. FRAMES WERE REPAIRED IAW SRM 51-70-11 2R.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,752 hrs · 28,889 cycles

CRACKED FRAME CLIP ON STA 1022 BTW LONG 13 /14 LT. REPAIR ON FRAME CLIP WAS ACCOMPLISHED PER. SRM 53-00-06 REPAIR 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,752 hrs · 28,889 cycles

CRACKED FRAME CLIP ON STA 1022 BTW LONG 13 /14 RT. REPAIR ON FRAME CLIP WAS ACCOMPLISHED PER SRM 53-00-06.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON SETTLEMENT AREA OF FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW DWG #9936534-179 REV BW.

Part: PAN — WORN · airframe 42,752 hrs · 28,889 cycles

AFT CABIN BULKHEAD DOOR WORN ON RT LOWER INTERNAL PAN AT VENTRAL STAIR DOOR. OUT OF LIMITS. REPAIRED IAW SRM 52-10-02 2R, REPAIR 16.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FLOOR SUPPORT STA Y=256 BTW X=-22 TO X=22 AT PAX CABIN IN REF NRTC 406 (AMDS 5300-2010). SUPPORT WAS REPLACED PER SRM 51-40-08 AND SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FLOOR SUPPORT STA Y=145 X=-46 AT COCKPIT. FLOOR SUPPORT WAS REPLACED PER SRM 53-10-51, SRM 51-40-08, AND SRM 51-41-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

CORROSION ON SETTLEMENT OF RT CONSOLE STA Y=145 X=-45 AT COCKPIT. SETTLEMENT ANGLE OF RT CONSOLE ON STA Y=145 X=-45 AT COCKPIT WAS REPLACED PER SRM 51-41-02, 51-41-01, AND DWG 9936533-11 REV CM.

Part: FLOOR SUPPORT — CORRODED (BS 148-218) · corrosion level 2 · airframe 42,752 hrs · 28,889 cycles

SEVERAL CORROSION POINTS ON FLOOR SUPORTS BS 148 AND 218, RBL 7 AND 54. FLOOR SUPPORT REPLACED IAW SRM 51-41-01 AND SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,752 hrs · 28,889 cycles

CORROSION ON FLOOR SUPPORTS STA Y=200 BTW X=12 TO X=-7). FLOOR SUPPORTS WERE REPLACED PER SRM 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,752 hrs · 28,889 cycles

CRACKED RT CUSP WEB STA Y=953 BTW X=-54 TO X=-60 (AMDS 5300-2020) (CPAX) (IN REF CARD 00194). CUSP WEB STA Y= 953 WAS REPAIRED PER SRM 53-00-55 REPAIR 4 FIG 212. HFEC WAS ACCOMPLISHED ON RT CUSP WEB STA Y=953 BTW X=-54 TO X=-60 CPAX PER NDT SPM 06-10-01.001, NO CRACKS WERE FOUND AFTER TRIM OUT.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,752 hrs · 28,889 cycles

CRACK ON LT CUSP WEB AT STA Y= 674. HFEC INSPECTION WAS ACCOMPLISHED AND CRACKS WERE FOUND (1.500") AND (2.500") PER NDT SPM 06-10-01.001. DAMAGE WAS REMOVED PER SRM 53-00-55 2R-4 REPAIR 4 FIG 212. CUT OUT WAS TREATED AND PAINTED PER SRM 51-10-04 PAR 21 AND 15. REPAIR PARTS WERE FABRICATED PER SRM 53-00-55-2R-4 REPAIR 4 FIG 212. (HFEC)WAS ACCOMPLISHED PER B717 NDTSPM 06-10-01.001 NO CRACKS WERE FOUND AFTER CUT OUT ON STA LT SIDE CUSP WEB STA Y=674. DOUBLER AND FILLER WAS TREATED AND PAINTED PER SRM 51-10-04 PAR 15 AND 21. DOUBLER AND FILLER REPAIR WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON LT RING PAN AT STA Y= 909 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56-20-02 REP 1 FIG 202. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON RT RING PAN AT STA Y= 889 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE TRIM-OUT PER NDT SPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56-20-02 REP 1 FIG 202. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON LT RING PAN AT STA Y= 831 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56--20-02 REP 1 FIG 202 REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON LT RING PAN AT STA Y= 877 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56-20-02 REP 1 FIG 202. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (CABIN) · airframe 42,752 hrs · 28,889 cycles

CRACK ON LT RING PAN AT STA Y= 637 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56-20-02 REP 1 FIG 202. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,865 hrs · 28,258 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE CABIN DOOR VERTICAL EMERGENCY EXIT LIGHTS AT BOTH L1 AND L2 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,797 hrs · 26,573 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,747 hrs · 26,533 cycles

DURING SERVICE CHECK FOUND OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKS NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,676 hrs · 26,474 cycles

OVERWING EMERGENCY LIGHT. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS REF AMM 33-51.

Part: ANGLE — CRACKED (BS 715) · airframe 38,775 hrs · 25,702 cycles

CRACKED VERTICAL ANGLE AT BS 715, LBL 22. FABRICATED AND REPLACED IAW DWG NR 9923417.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 38,775 hrs · 25,702 cycles

FOUND CRACKED FLOORBEAM WHILE INSPECTING OVERWING FRAME AT BS 737 LT. REPLACED FLOORBEAM IAW DWG 5910148.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,169 hrs · 25,215 cycles

DURING LINE CHECK, FOUND AISLE OVERHEAD EMERGENCY SIGN L2-791 INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY. LP 6909374.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,488 hrs · 24,004 cycles

AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW MM.

Part: FILTER — FAULTY (HYDRAULIC SYS) · airframe 36,461 hrs · 23,987 cycles

RIGHT HYD QTY WENT TO 0 ON DECENT INTO MSP, RT HYD PRESS ALSO TO 0. R & R RT HYD FILTER ASSEMBLY IAW MM.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 35,918 hrs · 23,622 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIRTY. CLEANED GIRT BAR IAW MM.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 35,918 hrs · 23,622 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIRTY. CLEANED GIRT BAR IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,800 hrs · 23,550 cycles

FWD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW SIP.

Part: RETAINER — BROKEN (R1 DOOR) · airframe 35,600 hrs · 23,421 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER BROKEN. REPAIRED RETAINER IAW SRM.

Part: COVER — UNSECURE (L1 DOOR) · airframe 35,550 hrs · 23,384 cycles

L1 DOOR SLIDE PACK COVER UNSECURED. SECURED L1 DOOR COVER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

RT CEILING EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 19. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

CEILING EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 6 TO ROW 8. R & R BATTERY PACK IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

VERTICAL SUPPORT CRACKED AT STATION 737, RBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

CANTED KEEL AREA HAS CRACKED FORMER ON LT SIDE AT STATION 694. R & R FORMER IAW SRM & DRAWING.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

RT CUSP WEB CRACKED AT STATION 674. REPAIRED WEB IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

VERTICAL SUPPORT CRACKED AT STATION 737, LBL 44. R & R SUPPORT IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

CANTED KEEL AREA CRACKED FORMER ON RT SIDE AT STATION 694. R & R FORMER IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT CUSP WEB CORRODED AT STATION 518. R & R WEB IAW SRM.

Part: FAIRING — CRACKED (HORIZ STAB) · airframe 33,842 hrs · 22,279 cycles

HORIZONTAL STAB FAIRING PANEL 350 CRACKED AT SKIN INNER SIDE. REPAIRED DOUBLER IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT UPPER AFT WINDOW PAN CRACKED AT STATION 851. REPAIRED DOUBLER IAW SRM & DRAWING.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT LOWER AFT WINDOW PAN CRACKED AT STATION 598. REPAIRED PAN IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

AFT BULKHEAD LT DOOR FRAME FITTING CRACKED AT STATION 1076, LONGERON 13L. R & R FITTING IAW SRM & DRAWING.

Part: WEB — CRACKED (RT HORIZ STAB) · airframe 33,842 hrs · 22,279 cycles

RT HORIZONTAL STAB REAR SPAR OTBD LINK WEB CRACKED AT OTBD SIDE OF NR 4 ELEVATOR HINGE. REPAIRED WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LONGERON CRACKED AT STATION 1022, LONGERON 7R. REPAIRED LONGERON IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT CUSP WEB CORRODED BETWEEN STATION 541 TO STATION 551. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

RT CUSP WEB CORRODED AT STATION 545. R & R WEB IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT LOWER FWD WINDOW PAN CRACKED AT STATION 617. REPAIRED PAN IAW SRM & DRAWING.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LT LOWER FWD WINDOW PAN CRACKED AT STATION 636. REPAIRED PAN IAW SRM & DRAWING.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

LOWER FORWARD WINDOW PAN CRACKED AT STATION 851. R & R DOUBLER IAW SRM & DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

FUSELAGE SKIN CORRODED BETWEEN STATION 850 TO STATION 880, BETWEEN LONGERON 29R & LONGERON 29L. REPAIRED SKIN IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

UNDER WING BARREL KEEL BEAM RT SIDE BS 715 FORMER CRACKED AT OTBD END. R & R FORMER IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 33,842 hrs · 22,279 cycles

RT WING LOWER PANEL CRACKED AT SW 164. REPAIRED SKIN IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

CANTED KEEL AREA CRACKED FORMER ON RT SIDE AT STATION 679. R & R FORMER IAW SRM & DRAWING.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

MAIN CABIN FLOOR PANEL 222RF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

CANTED KEEL AREA CRACKED FORMER INSIDE LT SIDE AT STATION 679. R & R FORMER IAW SRM & DRAWING.

Part: BRACKET — CRACKED (RT WING) · airframe 33,842 hrs · 22,279 cycles

RT WING BONDING BRACKET CRACKED AT STATION 636. R & R BRACKET IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

UNDER WING BARREL KEEL BEAM LT SIDE BS 715 FORMER CRACKED AT OTBD END. R & R FORMER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

FORMER CRACKED AT BS 1152, LONGERON 2L. R & R FORMER IAW SRM & DRAWING.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

MAIN CABIN FLOOR PANEL 222AVF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

MAIN CABIN FLOOR PANEL 222 AHF DAMAGED. REPAIRED PANEL IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

FRAME CRACKED AT STATION 1152, LONGERON 2R. R & R SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

FRAME CRACKED AT BS 674, RBL 57. R & R FRAME IAW SRM & DRAWING.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 33,842 hrs · 22,279 cycles

LT WING BONDING STRAP CRACKED AT BS 636. R & R STRAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

FRAME CRACKED AT BS 715, RBL 57. R & R FRAME IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

SEAT TRACK CORRODED BETWEEN STATION 550 TO STATION 580, RBL 44.0. REPAIRED SEAT TRACK IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 33,842 hrs · 22,279 cycles

MAIN CABIN FLOOR PANEL 222APF DAMAGED. REPAIRED PANEL IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

C1 DOOR PAN CORRODED UNDER FLANGE. R&R PAN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,842 hrs · 22,279 cycles

RT VENT LOUVER UPPER AFT CLIP CRACKED. R & R CLIP IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,128 hrs · 23,109 cycles

FUSELAGE SKIN CORRODED BETWEEN STATION 850 TO STATION 880, BETWEEN LONGERON 29L TO LONGERON 29R. REPAIRED SKIN IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,817 hrs · 22,899 cycles

RT EMERGENCY FLOOR LIGHTING LOOSE AT ROW 12. SECURED LIGHT IAW MM.

Part: HOUSING — BROKEN (CABIN) · airframe 34,728 hrs · 22,839 cycles

RT EMERGENCY EXIT PATH LIGHT HOUSING BROKEN AT ROW 10. R&R HOUSING IAW AMM.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 34,619 hrs · 22,777 cycles

L1 DOOR GIRT BAR DIFFICULT TO ARM & DISARM. CLEANED GIRT BAR FLOOR ATTACHMENTS IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,554 hrs · 22,734 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK CAME LOOSE FROM DOOR. SECURED SLIDE IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,471 hrs · 22,681 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED L1 DOOR SLIDE PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 34,111 hrs · 22,459 cycles

RIGHT EMERGENCY EXIT LIGHT BROKEN AT ROW 10. SECURED LIGHT IAW SIP.

Part: WIRE — LOOSE (CABIN) · airframe 31,763 hrs · 20,957 cycles

RIGHT EMERGENCY LIGHT WIRE LOOSE AT ROW 27. SECURED WIRE PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,696 hrs · 20,250 cycles

EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ATTACH FITTING — CORRODED (GIRT BAR)

MAIN CABIN GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: CHANNEL — CORRODED (FUSELAGE)

MAIN CABIN GALLEY INBD LOWER SIDEWALL, CORROSION. ACCOMPLISHED GALLEY INBD LOWER SIDEWALL DOUBLER REPAIR PER EA 17-53-035391 IR SECTION 1. REPLACED DOOR FRAME CHANNEL PER B717 SRM 51-41-01 & SRM 51-41-02. SEE NR 725593.

Part: PANEL — CORRODED (GALLEY)

MAIN CABIN GALLEY BASE PANEL INBD AFT CORNER CORRODED. REPAIRED PER EA 17-53-03541 IR SECT 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 45 TO RBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52 REP 5, FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-03, 53-10-51, 51-10-04 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL 31 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: CHANNEL — CORRODED (FUSELAGE)

MAIN CABIN SUPPORT CHANNEL, STA 202, RBL 45, CORROSION. ACCOMPLISHED SUPPORT CHANNEL REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 5 TO LBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL 16 TO RBL 29, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 190 TO 200, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-41-02.

Part: STRINGER — CORRODED (FUSELAGE)

STA 1133, LONG 5L, CORROSION. OPEN DEFECT.

Part: STRUCTURE — CRACKED (FUSELAGE)

AFT FUSELAGE SPAR FRAME DOUBLER, STA 1140, LONG 2L, CRACKED. ACCOMPLISHED LONGERON SECTION REPLACEMENT AND SPLICE REPAIR PER B717 SRM 53-00-05 FIGURE 201 REPAIR 2. SEE NR 725602.

Part: COVER — OUT OF POSITION (EVAC SLIDE)

CREW REPORTED R1 DOOR SLIDE COVER FELL OFF. (REINSTALLED/ NOTED IN RESOLUTION/RE-INSEPCTION REQUIRED). REMOVED AND REPLACED R-1 DOOR SLIDE PER AMM 25-61.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS)

DURING EMERGENCY POWER TEST, RELAY CLOSED AND THEN FAILED TO OPEN. RESTARTED TEST (2X). EMERGENCY TEST FAIL (2X). REMOVED POWER FROM EMERGENCY AC BUS, APPLIED POWER AND PERFORMED EMERGENCY POWER TEST TWICE WITH NO DISCREPANCIES REF FIM 24-24 TASK 803.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FUSELAGE FRAME AT FS 870, AFT SIDE HAS CORROSION AT LONGERON 30. INSTALLED REPAIR SPLICE AT AFT CARGO COMPARTMENT FUSELAGE FRAME FS 870 AT LONGERON 30 IAW B717 SRM 53-20-07 REPAIR 3 FIG 201.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB CUTOUT AREA HAS CORROSION STA FROM 954 TO 994. INSTALLED AFT CARGO COMPARTMENT DOOR JAMB LOWER SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIGURE 201. SEE NR 3797, 3829 AND 2382.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 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 TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2990.

Part: BATTERY PACK — DISCHARGED (CABIN)

EPL INOP AT ROWS 1-10. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY AT POS NR 4 EPL, OPS OK M/M 33-51.

Part: SKIN — DENTED (FUSELAGE)

DENT AT P$237L LONG 18L AND RUNS FROM L18 UP 5 INCHES ABOVE L18 MEASURES 5 X 5 X .035. REPAIR DENT AT P$237L LONG 18C IAW B717 SRM 53-00-01 FIG 201.

Part: SLIDE — DEPLOYED (R1 DOOR)

R1 DOOR SLIDE DEPLOYED AND GIRT BAR WAS IN PLACE. R/R R-1 SLIDE PER AMM 25-61-03.