N952AT

Part: DOUBLER — NOT REPORTED (ZONE 000) · airframe 64,876 hrs · 46,722 cycles

EXISTING REPAIRS FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED DOUBLER INSPECTION PER ERA 625837-14 AD (7976471)

Part: FITTING — LEAKING (ZONE 500) · airframe 64,553 hrs · 46,417 cycles

FUEL LEAK THROUGH FLAP HINGE BRACE FITTING ATTACHING FASTENERS AT LEFT WING STA XRS=164. LH WING AFT LOWER SKIN DOUBLER AT STA XRS= 164 WAS REPAIRED PER PRI 624486-14 (1157598)

Part: SKIN — LEAKING (ZONE 600) · airframe 64,553 hrs · 46,417 cycles

RIGHT WING LOWER SKIN, XRS -164 AT FLAP BRACE FITTING FUEL LEAK TIME LIMITED REPAIR. REPAIRED RH LOWER WING SKIN PER ERA 625837-14AD REV ORIGINAL SECTION I TIME LIMITED REPAIR. REPETITIVE INSPECTION EVERY 90 DAYS FROM AUG 15 PER ERA 625837-14AD (1154482)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,550 hrs · 46,416 cycles

CORROSION ON DOUBLER REPAIR, BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2. SUMMARY OF NRC 00010: CORROSION LEVEL 2. DOUBLER REPAIR BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2 WAS MANUFACTURED AND REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP #0785056)

Part: SAFETY PIN — MISSING (ZONE 800 SLIDE) · airframe 64,550 hrs · 46,416 cycles

MISSING SAFETY PIN OF SLIDE R1 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 THE NRC 00084: SAFETY PIN WAS INSTALLED ON SLIDE R1 DOOR PER B717-200 AMM 25-61-03-000-801 STEP B.(1).(D). (LP #0786038)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 64,143 hrs · 46,074 cycles

THE CABIN CEILING MOUNTED EMERGENCY LIGHT AT 2AB IS INOPERATIVE. FORWARD TO MEL 33-51-01A. PLACARDS INSTALLED. ON 18NOV24 MAINTENANCE REPLACED THE 2AB CABIN CEILING STANBY LIGHTING ASSEMBLY PER B717 AMM 33-52. OPERATIONAL CHECK WAS GOOD. MCO AND PLACARD WERE REMOVED. (LP #4014744)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 63,354 hrs · 45,385 cycles

PANELS 1-5 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY B5-227 BATTERY PER B717 AMM 33-51. (LP #6208532)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 63,238 hrs · 45,276 cycles

AIRCRAFT 9511, DURING SVC CHECK FOUND MID CABIN EMER LIGHTS INOP.CORRECTIVE ACTION: REPLACED MID CABIN EMER LIGHTS BATTERY PACK. (LP 6209356)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 60,175 hrs · 42,597 cycles

CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2. CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 606467-14 REV ORIGINAL SECTION 1 (PERMANENT REPAIR) AND PRI 606467-14 REV 0 TO 4. INSPECTION REQUIREMENTS: ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY 8,000 FLIGHT CYCLES AFTER SECTION I: PERMANENT REPAIR IAW ER/A. ASSOCIATED ER/A 14-606467 ADDED FOR AC 9511. (LP #2667225)

Part: UNKNOWN — UNKNOWN · airframe 60,175 hrs · 42,597 cycles

INTERFERENCE BETWEEN FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00060: FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2667393)

Part: UNKNOWN — UNKNOWN · airframe 60,175 hrs · 42,597 cycles

INTERFERENCE BETWEEN FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00105: FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2667399)

Part: UNKNOWN — UNKNOWN · airframe 60,175 hrs · 42,597 cycles

AFT SPLICE BTW L-28R TO L-28L REMOVAL, FOUND CRACK ON SPLICE FRAME AT STA 636. SUMMARY OF NRC 00244: SPLICE FRAME AT STA 636 WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #2664206)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

AFTER DOOR ASSEMBLY, CORROSION WAS FOUND ON SETTLEMENT AREA AT DOOR PANEL P/N 5971074. SUMMARY OF NRC 0240: LEVEL CORROSION 2. (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SETTLEMENT AREA AT DOOR PANEL. WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.090 IN. REMAINING THICKNESS IS 0.025". THEREFORE, PANEL IS OUT OF LIMITS PER B717-200 SRM 53-01-01-1A PROCEDURE 1 AD 1 PAR 4 AND DCMD/BOEING NDT SPM PART. 4 FIG 9. DOOR ASSEMBLY WAS REPLACED PER DWG 5971074 REV C. (LP #2659571)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ON LONGERION 30 RH BTW STA Y=1031 TO STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00195: CORROSION LEVEL 2. LONGERON SECTION 30 FROM STA Y=1022 TO Y=1053 AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717-200 SRM 51-41-05-0G STEP 8. AND 51-41-02-0G STEP 12. (LP #2658625)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ALONG LONGERON L30 FROM STA Y=900 TO Y=1022 AT AFT CARGO COMPARTMENT C2. SUMMARY OF NRC 00178: CORROSION LEVEL 2. NEW SECTION LONGERON L30 FROM STA Y=900 TO Y=1022 WAS INSTALLED PER B717-200 SRM 51- 41-05-0G. (LP #2658653)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ON FUSELAGE SKIN ON STA Y=1053 BTW STR 29 LH TO STR 29 RH AT AFT CARGO COMPARTMENT. CORROSION WAS FOUND ON PRODUCTION DOUBLER. SUMMARY OF NRC 00241: CORROSION LEVEL 2. DOUBLER ON STA 1053 BTW LONGERON 28RH TO 28LH WAS REPLACED PER B717 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2654031)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29. SUMMARY OF NRC 00174: CORROSION LEVEL 2. SECTION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #2652378)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ON FRAME CLIP AND SKIN ON AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG L30. SUMMARY OF NRC 00182: CORROSION LEVEL 2. SECTION ON FRAME CLIP AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG 29RH TO 29LH WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2 FIG 201 AND BOEING DWG 9912243-63 REV JS. SKIN ON AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG L30 WAS CLEANED PER DAL PS 900-1-2-1 N .01. VISUAL INSPECTION WAS PERFORMED ON AREA AND NO DAMAGE WAS FOUND AFTER CLEANING PER B-717-200 SRM 51-10-04-0G PAR. 26. (LP #2650763)

Part: NONE — NONE · corrosion level 2 · airframe 60,165 hrs · 42,589 cycles

CORROSION ON INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00193: CORROSION LEVEL 2. INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 WAS REPLACED PER B-717 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2651008)

Part: NONE — NONE · airframe 60,165 hrs · 42,589 cycles

CRACKED PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00235: PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2644886)

Part: NONE — NONE · airframe 60,165 hrs · 42,589 cycles

CRACKED BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00236: BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (LP #2642758)

Part: NONE — NONE · airframe 60,165 hrs · 42,589 cycles

SECONDARY IN REF TO AMDS 5310-01436-01A: CRACK ON CUSP MEMBRANE WEB AT STA 674 L-18 LH. SUMMARY NRC 00198: CUSP MEMBRANE WEB AT STA 674 L-18 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2637942)

Part: NONE — NONE · airframe 60,165 hrs · 42,589 cycles

CRACK ON CUSP MEMBRANE WEB AT STA 696 L-18 LH. SUMMARY OF NRC 0209: CUSP MEMBRANE WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2636060)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,696 hrs · 42,177 cycles

THE EXIT SIGN AT DOOR 1R IS MISSING. MAINTENANCE REPLACED THE MISSING LENS IAW B717 AMM 33-51. (LP #8566118)

Part: BATTERY PACK — INOPERATIVE · airframe 58,741 hrs · 41,329 cycles

THE TAIL COMPARTMENT (CATWALK) AFT EMERGENCY CEILING LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-116, PER B-717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #8057681)

Part: STRIP — MISSING · airframe 58,606 hrs · 41,213 cycles

THE EMERGENCY ESCAPE PATH LIGHTING STRIP AT ROW 19AB IS MISSING. MAINTENANCE INSTALLED A NEW EEPL INDIGO TAPE STRIP AND END CAPS. THE LUMINESCENT STRIP IS NOW OK FOR SERVICE. (LP #2243238)

Part: BATTERY — INOPERATIVE · airframe 58,543 hrs · 41,154 cycles

THE EMERGENCY LIGHTS IN THE AFT CABIN ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT LOCATION R5-260. ALL OPERATIONS ARE NOW NORMAL REF B717 AMM 32-51. (LP #8663449)

Part: BATTERY — INOPERATIVE · airframe 58,514 hrs · 41,130 cycles

THE AFT CABIN EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY EXIT LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8663444)

Part: NONE — NONE · airframe 57,850 hrs · 40,532 cycles

THE EMERGENCY LIGHTS BATTERY PACK AT B5-119 WAS INOPERATIVE FOR ROW 20DC EMERGENCY PATH LIGHTS. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT B5-119. THE EMERGENCY LIGHTS OPERATIONAL CHECK WAS NORMAL REF B717 AMM 33-51-04. (LP #5363034)

Part: NONE — NONE · airframe 57,379 hrs · 40,125 cycles

THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8076597)

Part: NONE — NONE · airframe 57,099 hrs · 39,851 cycles

FOUND TAIL CONE SLIDE COVER OPEN AND SLIDE IS LAYING LOOSE. MAINTENANCE REPLACED THE TAIL CONE SLIDE IAW AMDS CARD 2561-9006 (QC 5199). (LP #7806042)

Part: FLOORBEAM — CRACKED (CABIN) · airframe 55,840 hrs · 38,768 cycles

REF NRC 131. CRACK FOUND EXTENDING THROUGH MULTIPLE ATTACH FASTENERS ON FLOOR BEAM STA 737. LOCATED RT SIDE OF A/C JUST I/B OF THE OVERWING EXIT FUSELAGE FRAMES. MARKED. NRC 131. MAINTENANCE REPLACED FLOOR BEAM PER DWG #5940863 & INSTALL FLOOR PANELS PER B717 AMM 53-21-01. (LP #1744527)

Part: SLIDE — UNSECURE (TAILCONE) · airframe 54,829 hrs · 37,884 cycles

DURING A SERVICE CHECK, FOUND TAILCONE SLIDE COVER DISLODGED AND PACK NOT SECURE. REPLACED THE TAILCONE SLIDE PACK IAW WC 2561-9006 AND AMM 25-61.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,829 hrs · 37,884 cycles

PASSENGER CABIN FWD LT & RT OVERWING EMERGENCY EXIT IDENTIFIERS SIDE PANE SIGNS INOPERATIVE. REPLACED THE B6-118 BATTERY PACK TRAY IAW WDM 33-51-14 PG 3. 1A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,487 hrs · 37,572 cycles

THE EMERGENCY EXIT SIGNS AT OVERWING EXIT 19A AND 19B WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY & BATTERY. FOLLOW-UP OPERATIONAL CHECK WAS GOOD. (LP #6924852)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,140 hrs · 37,279 cycles

THE FORWARD ENTRY DOOR AND WING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE FORWARD ENTRY DOOR AND WING EXIT DOOR LIGHTS IAW B717 AMM 33-51-03. OPERATIONAL TEST WERE NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #6947437)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,638 hrs · 36,883 cycles

THE AFT TAIL CONE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE RIGHT LAVATORY AND THE OPERATION CHECK OF OVERHEAD TAIL CONE EMERGENCY LIGHTS WAS GOOD. (LP #6561511)

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 51,705 hrs · 35,476 cycles

CORROSION ON LOWER BOLT ALSO AT INBOARD FLAP FWD HINGE FITTING (AI). NRC 00289: CORROSION LEVEL 2, LT LOWER BOLTS AND LT INBOARD WING FLAP HINGE FITTING WAS REPLACED PER AMM 57-55-25. (LP #0983390)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,705 hrs · 35,476 cycles

CORROSION ON AFT BULKHEAD FRAME ON STA 1022 BTW L 26L TO L28R. (C2). NRC 00310: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW L 26L TO L26R WAS REPAIRED PER SRM 53-20-07-2R REPAIR 3. (LP #0976403)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

CRACK ON FUSELAGE SKIN AT STA 1076 LONGERON 14R (FUS). NRC 00061: CRACK ON FUSELAGE SKIN AT STA 1076 LONGERON 14R WAS REPAIRED PER ETI-17-19-019 R2 AND ER/A 575932-14 REV. ORIGINAL. ACCOMPLISH ER/A 575932-14 SECTION II. AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR FOLLOWED UNDER LOG #0965525. ASSOCIATED ER/A 00-575932 ADDED FOR AC 9511. (LP #0971509)

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

DAMAGED CUSP WEB MEMBRANE FROM STA Y=889 TO Y=908 LT SIDE BTW X=44 AND X=54. NRC 00191: CUSP WEB MEMBRANE FROM STA Y=889 TO Y=908 LT SIDE BTW X=44 AND X=54 WAS REPLACED PER ETI-17-19-032 REV. 1 AND ER/A 575994-14 REV. ORIGINAL. ASSOCIATED ER/A 00-575994 ADDED FOR AC 9511. (LP #0969915)

Part: GUSSET — CRACKED (RT PYLON) · airframe 51,703 hrs · 35,475 cycles

CRACK ON GUSSET AT PYLON SUPPORT BULKHEAD STA 1022 LONGERON 7R. (CPAX). NRC 00429: GUSSET AT PYLON SUPPORT BULKHEAD STA 1022 LONGERON 7R WAS REPAIRED PER ETI-17-19-023 REV. ORIGINAL AND ER/A 575672-14 REV. ORIGINAL. (LP #0970015)

Part: ACCESS PANEL — DAMAGED (RT WING) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

ELONGATED HOLES ON FUEL ACCESS PANELS #620CB, 620EB, 620GB, AND 620QB AT RT WING (AD). NRC 00553: CORROSION LEVEL 2, HOLES ON FUEL ACCESS PANELS #620CB, 620GB, AND 620QB AT RT WING WERE REWORKED PER SRM 57-10-01-2R AND BUSHING WERE FABRICATED PER SRM 57-10-01-2R AND INSTALLED PER SRM 57-10-01-2R-2 STEP 5B 3(F), FUEL ACCESS PLATE 620EB WAS REPLACED UNDER NRC 00576 ON LOG 0967373; TOOL USED: CHAMFER GAGE EXP. DATE 25JUN19 N/C 1489 AND CALIPER DIGITAL EXP. DATE 10SEP19 N/C 1739. (LP #0970019)

Part: GUSSET — CRACKED (LT PYLON) · airframe 51,703 hrs · 35,475 cycles

CRACK ON GUSSET AT PYLON SUPPORT BULKHEAD STA 1022 LONGERON 7L. (CPAX). NRC 00428: GUSSET AT PYLON SUPPORT BULKHEAD STA 1022 LONGERON 7L WAS REPAIRED PER ETI-17-19-023 REV. ORIGINAL AND ER/A 575672-14 REV. ORIGINAL. ASSOCIATED ER/A 00-575672 ADDED FOR AC 9511. (LP #0969997)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

CRACK AT FUSELAGE SKIN AROUND LT AFT FIXED NLG DOOR HINGE AREA. (FUS). NRC 00026: FUSELAGE SKIN AROUND LT AFT FIXED NLG DOOR HINGE AREA WAS REPAIRED PER SRM 53-10-01-2R. REPAIR 11. (LP #0966970)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION OUT OF LIMITS IN REFERENCE NRC 553 CORROSION FUEL ACCES PLATE #620EB. NRC 00576: CORROSION LEVEL 2, FUEL ACCES PLATE #620EB WAS REPLACED PER SRM 51-10-01-2R AND PART NUMBER WAS VIRIFIED PER IPC 57-23-01-01 ITEM 385J. (LP #0967373)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

NRC 482: FUSELAGE SKIN WAS FOUND CRACKED STA 120 (CPIL). NRC 00555: UPPER WINDOW FRAME AFT CORNER LT FUSELAGE SKIN WAS REPAIRED PER SRM 56-10-02-2R-1. (LP #0966013)

Part: LONGERON — CRACKED (BS 1022) · airframe 51,703 hrs · 35,475 cycles

CRACK ON LONGERON 6 RH AT STA 1022. (CPAX). NRC 00433: SECTION LONGERON 6 RH BTW STA 1002 TO 1049 WAS REPLACED (SPLICE REPAIR) PER B717-200 SRM 51-41-02 B717-200 SRM 51-41-05 AND 53-00-05-2R. (LP #0962698)

Part: FLOOR SUPPORT — CRACKED · airframe 51,703 hrs · 35,475 cycles

CRACK FLOOR SUPPORT BTW STA Y=636 AND BELOW TIE TRACK LH AT FWD CARGO COMPARTMENT (CCD). NRC 00336: CRACK FLOOR SUPPORT STA Y=636 AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0962962)

Part: LONGERON — CRACKED (BS 1022) · airframe 51,703 hrs · 35,475 cycles

CRACK ON LONGERON 8 RH AT STA 1022. (CPAX). NRC 00434: SECTION LONGERON 8 RH BTW STA 1002 TO 1049 WAS REPLACED (SPLICE REPAIR) PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0962700)

Part: FLOORBEAM — CRACKED (BS 655) · airframe 51,703 hrs · 35,475 cycles

CRACK FLOOR SUPPORT ON AFT BULKHEAD IN STA Y=655 UNDER SIDE TIE TRACK RH AND LH. (CCD). NRC 00335: CRACK FLOOR SUPPORT ON AFT BULKHEAD IN STA Y=655 UNDER SIDE TIE TRACK RH AND LH WAS REPLACED PER B717-200 SRM 51-41-01 AND 51-41-02. (LP #0962703)

Part: LONGERON — CRACKED (BS 1022) · airframe 51,703 hrs · 35,475 cycles

CRACK ON LONGERON 7LH AT STA 1022. (CPAX). NRC 00431: SECTION LONGERON 7 LH BTW STA 1012 TO 1049 WAS REPLACED (SPLICE REPAIR) PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0962964)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION ON FUEL ACCESS PLATE #620JB, 620HB, AND 620DB IS OUT OF LIMITS. NRC 00575: CORROSION LEVEL 2, FUEL ACCES PLATE #620JB, 620HB, AND 620DB WERE REPLACED PER B-717-200 SRM 51-10-01-2R AND EFECTIVITY WAS VERIFIED PER B-717-200 IPC 57-22-01. (LP #0961372)

Part: ACCESS PANEL — CORRODED (WING) · airframe 51,703 hrs · 35,475 cycles

IN REFERENCE NRC 00551 FUEL ACCESS PLATES #620CT, 620DT, 620AT, AND 620FT ARE CORRODED OUT OF LIMITS (AD). NRC 00558: CORROSION LEVEL 2, FUEL ACCESS PLATES #620CT, 620DT, 620AT, AND 620FT WERE REPLACED PER B717-200 SRM 57-10-01-2R REPAIR 2 PAR 5 AND EFECTIVITY WAS VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 020, 065. (LP #0959753)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

IN REFERENCE NRC 00550 FUEL ACCESS PLATES #520CT, 520DT, 520DB, AND 520FT ARE OUT OF LIMITS (AI). NRC 00559: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT, 520DT, 520FT, AND 520DB WERE REPLACED PER B717-200 SRM 57-10-01-2R REPAIR 2 PAR 5 AND EFECTIVITY WAS VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 065, 020 AND IPC 57-23-01-01 ITEM 430. (LP #0959756)

Part: LONGERON — CRACKED (BS 1022) · airframe 51,703 hrs · 35,475 cycles

CRACK FUSELAGE LONGERON BTW STA Y=1022 AND L5L AT AFTER CABIN AREA(CPAX). NRC 00477: SECTION LONGERON 5 LH BTW STA 1002 TO 1049 WAS REPLACED PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0958701)

Part: LONGERON — CRACKED (BS 1022) · airframe 51,703 hrs · 35,475 cycles

CRACK ON LONGERON 6LH AT STA 1022. (CPAX). NRC 00432: SECTION LONGERON 6 LH BTW STA 1002 TO 1049 WAS REPLACED PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0958705)

Part: LONGERON — CORRODED (BS 927-1007) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION ON LONGERON #30 FROM STA Y=927 TO Y=1007 AT AFT CARGO COMPARTMENT (CCT). NRC 00253: CORROSION LEVEL 2, SECTION LONGERON 30 FROM STA Y=900 TO Y=1012 WAS REPLACED (SPLICE REPAIR) DUE EXCESSIVE CORROSION PER B717-200 SRM 53-20-05-2R-1. (LP #0955764)

Part: TEE FITTING — CRACKED (BS 408) · airframe 51,703 hrs · 35,475 cycles

CRACK ON ANGLE "T" LOWER EDGE STA Y= 408 AT FWD CARGO DOOR (PTAS). NRC 00554: ANGLE "T" WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9957664 REV. N. (LP #0955845)

Part: FLOOR PANEL — DELAMINATED · airframe 51,703 hrs · 35,475 cycles

DELAMINATION ON FLOOR PANELS #221BF, 221HF, 221FF, 221JF, AND 221AF. (W-1). NRC 00501: FLOOR PANELS #221BF, 221HF, 221FF, 221JF, AND 221AF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0953908)

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 51,703 hrs · 35,475 cycles

DELAMINATION ON FLOOR PANEL #221LF. (W-1). NRC 00503: FLOOR PANEL #221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0953896)

Part: LINER — CRACKED (NOT REPORTED) · airframe 51,703 hrs · 35,475 cycles

CRACK ON LINER PANEL 211EF (CPIL). NRC 00407: LINER PANEL 211EF WAS REPAIRED PER B717-200 SRM 53-00-00-2R. (LP #0954932)

Part: CUSP WEB — CRACKED (BS 427-446) · airframe 51,703 hrs · 35,475 cycles

CRACK ON CUSP WEB BTW STA Y=427/Y=446 RH X=65. NRC 00298: CUSP WEB BTW STA Y=427/Y=446 RH X=65 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 215. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON CUSP WEB BTW STA Y=427/Y=446 RH X=65. NO CRACKS WERE FOUND AFTER DAMAGE TRIM OUT PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001 (EQUIPMENT: NORTEC 500S C/N: 1891 EXP. 27AUG19). (LP #0953347)

Part: PAN — CRACKED (WINDOW) · airframe 51,703 hrs · 35,475 cycles

CRACKED RING PAN IN STA Y=851 AND L=12R, Y=889 AND L=12R, Y=889 AND L=14R, Y=908 AND L=14R. ALSO Y=946 AND L=14R AT CPAX. RING PAN REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, FIG 202. TYPE B. (ET)(HFEC) WAS ACCOMPLISHED ON RING PAN STA Y=851/L=12R; Y=889/L=12R; Y=889/L=14R; Y=908/L=14R; Y=946/L=14R CPAX, PER NDT SPM PART 6, 06-10-01.001, NO CRACKS WERE FOUND AFTER TRIM OUT.

Part: PAN — CRACKED (WINDOW) · airframe 51,703 hrs · 35,475 cycles

CRACK RING PAN IN STA Y=908 AND L=14L, Y=870 AND L=12L, Y=851 AND L=12L. ALSO Y=832 AND L=12L AT CPAX. RING PAN REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, FIG 202. TYPE B. (ET)HFEC INSPECTION WAS ACCOMPLISHED ON RING PAN IN STA Y=908 AND L=14L, Y=870 AND L=12L, Y=851 AND L=12L, Y=832 AND L=12L AT CPAX AFTER TRIM OUT AND NO CRACKS WERE FOUND PER NDT SPM PART 6, 06-10-01.001.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

CRACK ON FLOOR SUPPORT AT WING BOX AREA STA Y=655 BTW X=44 AND X=-44. FLOOR SUPPORT AT WING BOX AREA STA Y=655 BTW X=44 AND X=-44 WAS REPLACED PER SRM 51-41-05.

Part: FITTING — CRACKED (BS 390) · airframe 51,703 hrs · 35,475 cycles

CRACK ON INNER FITTING NEAR LOWER EDGE STA Y=390 AT FWD CARGO DOOR (PTAS). NRC 00178: INNER FITTING WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0950665)

Part: FITTING — CORRODED (BS 210) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION ON FITTING STA Y=210 AND X=-11 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00378: CORROSION LEVEL 2, FITTING STA Y=210 AND X=-11 AT FWD WET AREA WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0950557)

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

EXCESSIVE CORROSION AT CUSP WEB BETWEEN STA 541/560 X=-65 IN REF NRC 00299. NRC 00549: CORROSION LEVEL 2, CUSP WEB BETWEEN STA 541/560 X=-65 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG. 215 TABLE 2. (ET) HFEC INSP WAS ACCOMPLISHED ON CUSP WEB BETWEEN STA 541/560 X=-65. AFTER CUT OUT NO CRACKS WERE FOUND PER DC/MD NDT SPM 06-10-01.001 (EQUIP. NORTEC 600 C/N 1601 EXP. 15-MAR-19). (LP #0950659)

Part: HOUSING — WORN (CRGO DOOR HANDLE) · airframe 51,703 hrs · 35,475 cycles

WEAR ON HOUSING AT FWD CARGO DOOR HANDLE (PTAS). NRC 00179: HOUSING WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0950064)

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=180 AND Y=200 AND X=-44 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00372: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA Y=180 AND Y=200 AND X=-44 WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #0949977)

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · corrosion level 2 · airframe 51,703 hrs · 35,475 cycles

CORROSION ON FLOOR SUPPORT STA Y=180 AND 200 BTW X=-9 TO X=-43 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00371: CORROSION LEVEL 2, FLOOR SUPPORT STA Y=180 AND 200 BTW X=-9 TO X=-43 AT FWD WET AREA WAS REPLACED PER B717-200 SRM 51-41-02 AND SRM 51-41-05. (LP #0949280)

Part: FLOOR PANEL — DELAMINATED · airframe 51,703 hrs · 35,475 cycles

DELAMINATION FLOOR PANEL #211ASF AND 211AQF. NRC 00498: FLOOR PANEL #211ASF AND 211AQF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0949287)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,831 hrs · 33,478 cycles

SKIN DAMAGE 3 FT AFT OF L1 DOOR JUST ABOVE CUSP LINE. FUSELAGE STATION Y236 BETWEEN LONGERON L17 AND L18. DENT 2 X 2.5 X .125 INCH DEEP WITH HORIZONTAL GOUGE .5 X .125 X .OO8 INCH DEEP. REMOVED DAMAGE SKIN FROM L18 TO L15 FSY 229 TO FSY 245.5. FABRICATED REPAIR PARTS PER SRM 53-00-01-2R-6. INSTALLED FLUSH SKIN REPAIR PER SRM 53-00-01-2R PROCEDURE 6. PAINTED AREA PER P/S 900-3-6 NR 36.

Part: SKIN — CRACKED (BS 1087) · airframe 47,894 hrs · 32,868 cycles

SKIN IS CRACKED AT LAP, BS 1087, LONGERON 14R. REPAIRED IAW ER/A 561280-14, REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,703 hrs · 35,475 cycles

ER/A 561324-14 SECT I ISSUED FOR CORROSION BETWEEN L-29R & L-30R. FOLLOW ON ACTION IS REQUIRED. 561324 SECT II DUE WITHIN 24MONTHS OR 6600 CYCLES, WHICHEVER OCCURS FIRST. DTA IS REQUIRED. ASSOCIATED ER/A 00-561324 ADDED FOR AC 9511. CHANGED INSP TASK. ER/A REV A IS CURRENT. SEE LP 0915617 FOR NEW FOLLOW ON ACTION. (LP #0179676)

Part: SKIN — CORRODED · corrosion level 2 · airframe 47,894 hrs · 32,868 cycles

CORROSION IN BELLY SKIN BY THE LAV WASTE TANK VENT. COMPLIED WITH PRI 561324-14 REV 0 AND REPAIRED REF ER/A 561324-14 REV ORIG.

Part: SKIN — CRACKED (BS 1087) · airframe 50,449 hrs · 34,572 cycles

FOUND A CRACK IN THE FUSELAGE SKIN AT BS 1087, LONGERON 14R. REPAIRED IAW ER/A 95-561280.

Part: ANGLE — CRACKED · airframe 46,694 hrs · 31,952 cycles

SKIRT ANGLE CRACKED AT UPPER FWD HINGE POINT JUST FWD OF YOKE. REMOVED DAMAGE IAW SRM 54-50-02 2B-1 STEP 6. FABRICATED A REPAIR IAW SRM 54-50-02 2R-1, REPAIR 1 THRU STEP 6.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,661 hrs · 31,233 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR BOTH OF THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD. (LP #9268508)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,446 hrs · 31,083 cycles

MAINTENANCE DETERMINED THAT THE BATTERY FOR THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED AREA AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,921 hrs · 30,626 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT PANELS 11, 12, AND 13 WERE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING AND REPLACED IT ALONG WITH THE BATTERIES IN THE POWER SUPPLY. THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: UNKNOWN — HAZE (AFT CABIN) · airframe 43,447 hrs · 29,542 cycles

ON APPROACH, THE F/A'S REPORTED A HAZE AND ELECTRICAL ODOR IN THE AFT CABIN. RAN PACKS WITH ENGINES AND APU NO SMOKE NOTED. INSPECTED ALL CABIN LIGHTS AND EMERGENCY POWER PACKS NTF. INSPECTED AFT HANDSET, BLOWER MOTOR BOTH LAVS, COFFEEMAKERS AND OVENS CK GOOD. FOUND SIGN OF DISCOLORATION AND SMOKE COMING FROM RT TEMP CONTROL OUTLET DUCT. REPLACED SAME. OPENED ALL PSU PANELS AND INSPECTED WIRING WITH NO DEFECTS NOTED. INSPECTED 8TH AND 13TH BLEED VALVE DUCTS FOR PRESENCE OF OIL, NONE NOTED. RAN BOTH ENGINES AT HIGH POWER AND BOTH PACKS HOT AND COLD WITH NO DEFECTS NOTED. INSPECTED ALL EMERGENCY LIGHT BATTERY PACKS AND SIDEWALL LIGHT SOCKETS WITH NO TROUBLE FOUND. CARGO AREAS, ELECTRONIC EQUIPMENT BAY ALL CHECK GOOD. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. ACFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,427 hrs · 29,528 cycles

ALL F/A SMELLS BURNING PLASTIC ON APPROACH; PRIMARILY IN FORWARD CABIN. NO TROUBLE FOUND. REPLACED COALESCER BAGS AND PERFORMED DUCT BURN-OUT IAW AMM 21-54.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,083 hrs · 29,227 cycles

CATWALK HANDRAIL EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,083 hrs · 29,227 cycles

CATWALK AFT EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: SLIDE — OUT OF ADJUST (TAIL) · airframe 43,083 hrs · 29,227 cycles

TAIL COMPARTMENT SLIDE SIGHT GLASS OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,484 hrs · 28,120 cycles

EMERGENCY LIGHT POWER SUPPLIES INOPERATIVE, BETWEEN B5-123 & B5-230. R & R POWER SUPPLY IAW MM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

AFT CARGO COMPARTMENT BARRIER DOOR, FOUND INBD SIDE OF U CHANNEL CRACKED AROUND FASTENER HOLE. REPAIRED U CHANNEL IAW SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 41,484 hrs · 28,120 cycles

LEFT OVERWING EMER EXIT IDENTIFIER HOUSING BROKEN. R & R IDENTIFIER IAW AMM.

Part: HOUSING — BROKEN (CABIN) · airframe 41,484 hrs · 28,120 cycles

RIGHT OVERWING EMER EXIT IDENTIFIER, HOUSING BROKEN. R & R IDENTIFIER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,484 hrs · 28,120 cycles

EMERGENCY EXIT LIGHTS BULB INOPERATIVE. RELAMPED BULB IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN NR 5 CEILING PANEL, LT EMER LIGHT HOUSING & LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM. .

Part: SPRING — WORN (GIRT BAR) · airframe 41,484 hrs · 28,120 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTINGS SPRING WORN. R & R FITTING ASSEMBLY IAW AMM.

Part: SPRING — WORN (GIRT BAR) · airframe 41,484 hrs · 28,120 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTINGS SPRING WORN. R & R FITTING ASSEMBLY IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR, STRUCTURE ANGLE SUPPORT CRACKED AT BS 715, RBL 44. R & R SUPPORT IAW DWG & SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR STRUCTURE SEAT TRACK FITTING SUPPORT CRACKED AT BS 737, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR STRUCTURE ANGLE SUPPORT CRACKED AT BS 715, LBL 44. R & R SUPPORT IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR STRUCTURE SEAT TRACK FITTING SUPPORT CRACKED AT BS 737, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CENTER WING SECTION UPPER SKIN PANEL CORRODED. REPAIRED SKIN IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CRACKED BETWEEN BS 908 - 889, BETWEEN LBL 44 TO 60. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB TO SEAT TRACK FLANGE CRACKED, BETWEEN BS 832 - 889, LBL 44. R & R CUSP WEB IAW DWG & SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT SIDE OF KEEL BEAM FORMER, CRACKED AT BS 674. R & R FORMER IAW SRM & EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

LEFT KEEL BEAM FORMER CRACKED AT BS 679 ON OTBD END. R & R FORMER IAW EA.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR MEMBRANE CRACKED AT BS 169, RBL 26. REPAIRED MEMBRANE IAW SRM.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR MEMBRANE CRACKED AT BS 168.75, RBL 49. REPAIRED DOUBLER IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FORWARD CABIN FLOOR MEMBRANE DOUBLER CORRODED BETWEEN BS 160 TO 180, BETWEEN RBL 43 TO RBL 60. REPAIRED DOUBLER IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FORWARD CABIN FLOOR MEMBRANE CORRODED BETWEEN BS 200 TO 219, BETWEEN RBL 26 TO RBL 60. R & R MEMBRANE IAW DWG & SRM.

Part: LENS — CRACKED (CABIN) · airframe 41,484 hrs · 28,120 cycles

LEFT OVERWING EXIT LIGHT, COVER LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 41,484 hrs · 28,120 cycles

RIGHT OVERWING EXIT LIGHT COVER LENS CRACKED. R & R LENS IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT WW FWD VERTICAL DOOR CUT OUT CRACKED. R & R CUT OUT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

COCKPIT FLOOR SUPPORT CORRODED AT BS 148, RBL 46. R & R SUPPORT IAW DWG & SRM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 41,484 hrs · 28,120 cycles

LEFT WING FIXED LE MOST INBD SIDE, BONDING STRAP CRACKED. R & R STRAP IAW DWG & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

LEFT WW FWD BULKHEAD, CTR WING UPPER SKIN, INBD SIDE BEHIND PULLEYS CORRODED. REPAIRED SKIN IAW SRM & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 41,484 hrs · 28,120 cycles

RIGHT WING TO BODY, INBD SIDE OF INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT SIDE OF KEEL BEAM FORMER CRACKED AT BS 696. R & R FORMER IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

LEFT SIDE OF KEEL BEAM, INTERNAL FORMER CRACKED AT BS 715. R & R FORMER IAW SRM & DWG.

Part: ANGLE — CRACKED (LT AILERON) · airframe 41,484 hrs · 28,120 cycles

LEFT WING AILERON OTBD HINGE ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: DOUBLER — CRACKED (LT WING) · airframe 41,484 hrs · 28,120 cycles

LEFT WING FIXED LE, OTBD SIDE OF NR 3 SLAT TRACK ON LE DOUBLER CRACKED. R & R DOUBLER IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

LEFT SIDE OF KEEL BEAM, FORMER CRACKED AT BS 696. R & R FORMER IAW DWG & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 41,484 hrs · 28,120 cycles

LEFT WING FIXED LE OTBD SIDE OF NR 3 SLAT TRACK ON FIXED LE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT KEEL BEAM FORMER CRACKED AT BS 715. R & R FORMER IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

AFT ACCESSORY COMPARTMENT FRAME NR 4, FORMER CRACKED AT BS 1095, LONGERON 15R. R & R FORMER IAW SRM & DWG.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 41,484 hrs · 28,120 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR ATTACH FITTING LT & RT CORRODED. R & R FITTING IAW DWG & SRM.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

AFT GALLEY MOUNT CORRODED AT BS 217, RBL 12. R & R MOUNT IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

SEAT TRACK UPPER SURF CORRODED BETWEEN BS 898 TO 1022, LBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 9 · airframe 41,484 hrs · 28,120 cycles

RIGHT OTBD SEAT TRACK CORRODED BETWEEN BS 900 TO 1022. R & R SEAT TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 157 TO 196, LBL 44. R & R SUPPORT IAW DWG & SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

E & E COMPARTMENT FORMER CORRODED BETWEEN BS 110 TO BS 131, LONGERON 30. REPAIRED FORMER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT INBD SEAT TRACK CORRODED BETWEEN BS 589 TO 646. R & R SEAT TRACK IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FLOOR SUPPORT CORRODED AT BS 146, RBL 39. R & R SUPPORT IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB ANGLE CORRODED BETWEEN BS 217 TO 222, RBL 60. REPAIRED ANGLE IAW EA.

Part: STRIP — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FOUND WING TO BODY METAL STRIP CRACKED AT RT FUSELAGE APPROXIMATELY AT BS 870, LONGERON 19R. R & R METAL STRIP IAW DWG & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CORRODED AT BS 389, BETWEEN RBL 44 TO RBL 54. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 256, LBL 14. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO 200, RBL 7. R & R SUPPORT IAW DWG & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CORRODED BETWEEN BS 470 TO 503, RBL 5. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 17 TO LBL 44. R & R SUPPORT IAW DWG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 41,484 hrs · 28,120 cycles

AFT CARGO PIT DOOR UPPER AFT CORNER DOOR PAN CRACKED. REPAIRED PAN IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 41,484 hrs · 28,120 cycles

R1 DOOR EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

RIGHT CUSP WEB CORRODED AT BS 217, RBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FORMER CRACKED AT BS 1022, LONGERON 16R. R & R FORMER IAW DWG & SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FORMER CRACKED AT BS 1022, LONGERON 16L. R & R FORMER IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CRACKED AT BS 665, LBL 45. R & R CUSP WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

SEAT TRACK CORRODED BETWEEN BS 200 TO 580, RBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 - 580, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

FORWARD OF E & E DOOR JAMB CORRODED AT LONGERON 30. R & R JAMB IAW DWG & SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CRACKED BETWEEN BS 655 TO 715, LBL 54. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,484 hrs · 28,120 cycles

CUSP WEB CRACKED BETWEEN BS 655 TO 715, RBL 54. R & R CUSP WEB IAW SRM & DWG.

Part: SPOILER — DELAMINATED (RT WING) · airframe 41,484 hrs · 28,120 cycles

RIGHT WING OTBD SPOILER DELAMINATED. R & R SPOILER IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,252 hrs · 28,634 cycles

AFT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,191 hrs · 28,592 cycles

FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,345 hrs · 28,036 cycles

LT OVERHEAD EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 11 TO ROW 19. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,345 hrs · 28,036 cycles

RT OVERHEAD EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 11 TO ROW 19. R & R BATTERY IAW AMM.

Part: CHARGER — FAILED (CABIN) · airframe 40,350 hrs · 27,393 cycles

EMERGENCY EXIT LIGHT BATTERY CHARGER B5 116 FAILED OPERATIONS CHECK. R & R BATTERY CHARGER IAW AMM.

Part: RIB — CRACKED (RT WING) · airframe 40,350 hrs · 27,393 cycles

RT WING NR 5 SLAT CLOSE OUT RIB INBD CRACKED AT BS 596. R & R RIB IAW DRAWING.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

R1 DOOR CUTOUT GIRT BAR FLOOR BRACKETS ATTACHMENT FITTINGS CORRODED. R & R FITTINGS IAW SRM & DRAWING.

Part: SPLICE — CORRODED (TE FLAP VANE) · airframe 40,350 hrs · 27,393 cycles

LT WING FIXED FLAP VANE INBD SPLICE CORRODED. R & R SPLICE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

FLOOR SUPPORT CORRODED AT BS 180, LBL 25. REPAIRED SUPPORT IAW DRAWING.

Part: RIB — CRACKED (LE SLAT) · airframe 40,350 hrs · 27,393 cycles

LT WING NR 5 SLAT STATION 596 CLOSE OUT RIB INBD CRACKED. R & R RIB IAW DRAWING.

Part: BRACKET — CRACKED (LE SLAT) · airframe 40,350 hrs · 27,393 cycles

LT WING FIXED LE AT SLAT TRACK NR 8 INBD SIDE SPRING GUARD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: VANE — CORRODED (TE FLAP) · airframe 40,350 hrs · 27,393 cycles

LT WING FLAP MOVABLE VANE AT LOWER SURFACE ALONG THE TE CORRODED. R & R VANE IAW AMM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 40,350 hrs · 27,393 cycles

L1 DOOR INTERCOSTAL CRACKED INSIDE HANDLE BOX. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

FLOOR SUPPORT CORRODED AT BS 200, BL 0. R & R SUPPORT IAW SRM & DRAWING.

Part: FITTING — CORRODED (TAILCONE) · airframe 40,350 hrs · 27,393 cycles

TAIL CONE EMERGENCY RELEASE CABLE FITTINGS CORRODED AT TRIANGLE CONNECTOR BRACKET. R & R FITTINGS IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

SEAT TRACK CORRODED AT BS 200, RBL 22. R & R SEAT TRACK IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

FALSE TRACK CORRODED AT BS 200, LBL 5. R & R TRACK IAW SRM & DRAWING.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 40,350 hrs · 27,393 cycles

R1 DOOR JAM LOWER AREA ADJACENT FLOOR BOARD PANEL ANGLE CORRODED. R & R PANEL IAW DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 180 TO BS 200, RBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: DOUBLER — CORRODED (TE FLAP VANE) · airframe 40,350 hrs · 27,393 cycles

LT WING 2ND FIXED FLAP VANE FROM INBD SIDE DOUBLER CORRODED AT AUXILIARY CAM ATTACHED POINT. REPAIRED DOUBLER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 8 TO RBL 35. R & R SUPPORT IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

LT WW FWD DOOR CUTOUT INBD BRACKET CRACKED. R & R BRACKET IAW DRAWING.

Part: BRACKET — CRACKED (LE SLAT) · airframe 40,350 hrs · 27,393 cycles

RT WING NR 5 SLAT INBD SIDE OF OTBD SLAT TRACK ANGLE CRACKED. R & R BRACKET IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

LT WING TO BODY FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 40,350 hrs · 27,393 cycles

RT WW DOOR FWD DOOR CUTOUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 40,350 hrs · 27,393 cycles

L1 DOOR EMERGENCY EVAC SLIDE PARTIALLY FELL OUT. R & R SLIDE IAW AMM.

Part: HOLDER — BROKEN (R1 DOOR) · airframe 40,556 hrs · 27,529 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER BROKEN. R & R HOLDER IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,461 hrs · 26,208 cycles

FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 37,653 hrs · 25,719 cycles

R1 SLIDE PULLED AS CATERING CART BEING PUT UP. PERFORMED INSPECTION ON R-1 DOOR SLIDE (EVAC SLIDE) IT APPEARS NORMAL REF 717 AMM 25-61-03.

Part: ROD END — BROKEN (LE SLAT) · airframe 51,440 hrs · 30,769 cycles

WHEN SLATS EXTENDED HAD AN ABRUPT RIGHT ROLL. LOST 300FT ALTITUDE. FOUND LEFT SLAT I/B EXTEND ACTUATOR ROD END BROKEN. REMOVED AND REPLACED ACTUATOR ROD END PER MM.

Part: FITTING — DIRTY (GIRT BAR) · airframe 36,741 hrs · 25,107 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO DISARM FROM FLOOR FITTING. CLEANED AND LUBED FITTINGS PER M/M.

Part: HOLDER — BROKEN (CABIN) · airframe 36,237 hrs · 24,767 cycles

FWD EMERGENCY FLASHLIGHT HOLDER BROKEN. RELAMPED HOLDER PER MM.

Part: BRAKE ASSY — CONTAMINATED (MLG WW) · airframe 35,873 hrs · 24,531 cycles

BRAKE PEDALS TRAVEL BEFORE STOP. BLED BRAKE ASSY PER MM.

Part: HYDRAULIC LINE — LEAKING (RUDDER) · airframe 35,629 hrs · 24,373 cycles

DIVERSION, HYDRAULIC QUANTITY LOW (FOUND RUDDER PRESSURE LINE LEAKING. REMOVED AND REPLACED PIPE ASSY PER MM.

Part: FUEL FILTER — LEAKING (RT ENGINE) · airframe 35,382 hrs · 24,225 cycles

DIVERSION - FUEL LEAK RIGHT ENG NOTED AT CRUISE FL 340 AFTER DISPLAY OF LAT FUEL UNBAL ALERT. REMOVED AND REPLACED RT ENG FUEL FILTER ASSY PER MM.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 35,381 hrs · 24,224 cycles

FUEL/BURN WAS 1900 LBS MORE THAN FLIGHT PLANNED. CROSS FEED 15000 LBS. DURING FLIGHT, ON APPROACH A/C FOLLOWING NOTICED SOMETHING TRAILING THE NR 1 ENGINE. FOUND LP FUEL FILTER BOWL O-RING EXPOSED AND FUEL LEAKING. REMOVED AND REPLACED O-RING & FILTER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED LAMP IAW MM 33-51.

Part: SHEAR TIE — CORRODED (FUSELAGE)

SHEAR TIE, STA 927, LONG 29L TO 29R, CORROSION. ACCOMPLISHED SHEAR TIE SPLICE DOUBLER PER B717 SRM 53-00-06. SEE NR 23551.

Part: SKIN PANEL — CRACKED (RT WING)

RIGHT WING T/E UPPER SKIN PANEL, CRACKED. ACCOMPLISHED T/E UPPER SKIN PANEL DOUBLER REPAIR PER B717 SRM 57-00-00, 51-10-04.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT DOOR THRESHOLD LOWER PAN, STA 389, LONG 28R, CORROSION. ACCOMPLISHED DOOR THRESHOLD LOWER PAN SPLICE REPAIR PER B717 SRM 51-41-02 AND 53-20-15. SEE NR 23514.

Part: PAN — CORRODED (FUSELAGE)

AFT LOWER CARGO COMPARTMENT DOOR JAMB PAN, CORROSION. ACCOMPLISHED DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15, 51-20-09, 51-40-08 AND EA 17-53-03732IR. SEE NR 23500.

Part: COVER — DETACHED (EVAC SLIDE)

R1 DOOR SLIDE HOLDER DETACHED FROM DOOR. REPLACED R1 DOOR SLIDE COVER REF MM 25-61.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

FLIGHT DECK EMERGENCY LIGHT SINGLE BULB INOP. RELAMPED EMERGENCY LIGHT, OPS GOOD REF MM 33-50.

Part: FRAME — DAMAGED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW TASK CARD 17-5310-2979.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2987.

Part: SPLICE — CORRODED (CARGO BAY)

FWD CARGO DOOR SEAL DEPRESSOR SPLICES, CORROSION. ACCOMPLISHED SEAL DEPRESSOR SPLICES REPLACEMENT PER B717 SRM 51-41-02, 51-41-08 AND B717 SRM 51-20-09.

Part: HINGE BRACKET — WORN (CARGO BAY)

FWD CARGO DOOR JAMB AFT HINGE BRACKET, WORN. ACCOMPLISHED BRACKET AND DOUBLER REPLACEMENT PER B717 SRM 51-41-01 AND B717 SRM 51-41-05.

Part: STRAP — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR STRAP AND SUPPORT, STA 160 TO 198, LBL 56, CORROSION. ACCOMPLISHED FLOOR STRAP AND SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE THRESHOLD PANEL AND GIRT BAR FITTING, STA 148 TO 200, RBL 56, CORROSION. ACCOMPLISHED THRESHOLD PANEL AND GIRT BAR FITTING REPLACEMENT PER B717 SRM 51-41-01.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 160 TO 200, LBL 10 TO RBL 56, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 160 TO 200, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER AND SPLICE REPAIR PER B717 SRM 51-70-10 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (FUSELAGE)

FOUR O'CLOCK POSITION CANTED FRAME, STA 1200.19, CRACKED. ACCOMPLISHED CANTED FRAME DOUBLER REPAIR PER B717 SRM 51-70-11 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: SPLICE PLATE — CORRODED (FUSELAGE)

RIGHT WING TO BODY FAIRING SPLICE PLATE, STA 851, CORROSION. ACCOMPLISHED SPLICE PLATE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR SUPPORT ANGLE, STA 191, RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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)

CABIN FLOOR SUPPORT, STA 200, RBL 10 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 215, RBL 55, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 10 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02458IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, RBL7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 460 TO 489, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02457IR.

Part: LANYARD — DETACHED (EVAC SLIDE)

R1 LANYARD DETACHED. PINS CAME OUT OF SLIDE. REPLACED SLIDE AT R1 DOOR. REF MM 25-61.

Part: WIRE — BROKEN (CABIN)

E-PATH LIGHTING ROWS 20-24 INOPERATIVE; FOUND DURING SERVICE CHECK. FOUND SIDEWALL TO 20 RT SEAT E-PATH WIRING BROKEN. REPAIRED WIRING IAW SWPM 20-10. E-PATH LIGHTING AT ROW 20-24 CHECKS GOOD IAW MM 33-51.

Part: SLIDE — DEPLOYED (R1 DOOR)

R-1 DOOR SLIDE DEPLOYED. REMOVED AND REPLACED R-1 EMERGENCY EVACUATION SLIDE IAW MM 25-61-03. OK FOR SERVICE.

Part: SENSOR — UNKNOWN (MLG)

DURING TAKEOFF ROLL AT ROTATION, FELT RIGHT SIDE SHIMMY. AFTER LIFT OFF, GOT A RIGHT GEAR UNSAFE INDICATION RED LIGHT ON COCKPIT AND CONFIG SYNOPTIC ALONG WITH PSEU FAIL ALERT. RIGHT ENGINE N1 VIBRATION ALERT AT 5.0. DECLARED EMERGENCY AND AIR RETURNED TO TPA. FOUND NR 3 TIRE BLOWN. REMOVED AND REPLACED NR 3 AND 4 TIRES. BOROSCOPED NR 2 ENGINE AND PERFORMED ENGINE RUN. NO DEFECTS FOUND. ALL INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT MLG DOWN AND LOCK SENSORS AND CONDUITS. PERFORMED GEAR SWINGS. ALL FUNCTIONS CHECK GOOD. REF NRWC'S N072076 AND N066367 FOR ALL WORK PERFORMED AND SIGNATURES.

Part: SEAT TRACK — CORRODED (FUSELAGE)

F/O AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK.

Part: WINDOW — FAILED (COCKPIT)

ON TAXI OUT F/O WINDOW FWD HAD ARCING AND ELEC SMOKE RT UPPER CORNER. TURNED OFF HEAT, ARCING AND SMOKE STOPPED. REPLACED F/O WINDSHIELD PER MM 56-11. OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — LOW (RIGHT)

RIGHT HYDRAULIC QUANTITY LOW. SERVICED RIGHT HYD SYSTEM TO FULL, BLEED HYD SYSTEM AND INSPECTED A/C FOR HYD LEAKS. NO LEAKS NOTED IAW B-717 AMM 12-13-01, A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY PATH LIGHT AT 31D DID NOT ILLUMINATE. REMOVED AND REPLACED BULBS AT EMERGENCY PATH LIGHT 31D IN REF TO MM 25-60 AND GMM 8103.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT, LOWER JAMB, SURFACE CORROSION. INSTALLED NEW LOWER FWD JAMB SECTION ON FWD CARGO DOOR CUTOUT AREA IAW B717 SRM 53-20-15 FIG 201. MATERIAL USED .040" 2024.0, HEAT TREATED TO T-3 PER GPS 98PMS.247PS.01.

Part: ODOR — DETECTED (CABIN)

RETURNED TO ATL AFTER TAKEOFF BECAUSE OF REPORTED SMELL OF SMOKE OR ELECTRICITY EMITTING FROM THE GALLEY 2 AREA. RAN LEFT AND RIGHT ENGINE AND BOTH PACKS, NO DEFECTS NOTED. CHECKED E & E AND CARGO COMPARTMENT REF M/M 49-10, 21-00, 71-00 AND 05-52.

Part: CONNECTOR — LOOSE (TAIL COMPARTMENT)

TAIL COMPARTMENT AFT THREE EMERGENCY LIGHTS ON LEFT SIDE DO NOT ILLUMINATE. FOUND CONNECTOR P1-116 LOOSE AT BATTERY PACK. RESECURED CONNECTOR IAW B717 WDW 33-51-13.