N990AT

Part: SKIN — WORN (ZONE 300) · airframe 61,167 hrs · 44,205 cycles

SHIP 9528 LEADING EDGE UPPER SKIN PANEL / FASTENERS WORN ALONG OUTER PERIMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 620349-14 (1245364).

Part: FUEL LINE — LEAKING (ZONE 100) · airframe 60,655 hrs · 43,735 cycles

SHIP 9528 -DIV- TO ORD DUE TO LEFT FUEL QUANTITY LOSS. CORRECTIVE ACTION: MAINTENANCE FOUND A LEFT SHROUDED FUEL RETURN TO TANK LINE AND COUPLING LOOSE AND LEAKING, REPLACED THE INNER AND OUTER FUEL SHROUD "O" RINGS. ALL OPS AND LEAK CHECK GOOD.(7294538)

Part: CABLE — DISCONNECTED (SLIDE) · airframe 59,091 hrs · 42,349 cycles

THE GIRT BAR RETAINER WITH THE CABLE WAS DISCONNECTED FROM THE SLIDE BUSSLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. *** CONTRACT MAINTENANCE EVENT - OCM: 291111 *** REATTACHED GIRT BAR RETAINER AND CABLE PER B717 AMM 25-61. ALL CHECKS GOOD. OK FOR SERVICE. (LP #4285690)

Part: PAN — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACKS ON INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00726: INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620733-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620733-14 REV 2 ASSOCIATED ER/A 14-620733 ADDED FOR AC 9528. (LP #0617529)

Part: PAN — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK PAN INTERNAL SIDE FWD EDGE ON BEAM #4 AND #5 (2 EA) AT AFT CARGO DOOR. SUMMARY OF NRC 00129: INNER PAN ON FWD EDGE BETWEEN BEAM #4 AND #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620739-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620739-14 REV 4. ASSOCIATED ER/A 14-620739 ADDED FOR AC 9528. (LP #0614490)

Part: PAN — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK PAN INTERNAL SIDE OF AFT EDGE ON BEAM #3, #4, AND #5 AT AFT CARGO DOOR. SUMMARY OF NRC 00127: INNER PAN OF AFT EDGE ON BEAM #3 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 620695-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 620695-14 REV 2. ALSO (ET) HFEC INSPECTION WAS ACCOMPLISHED ON PAN INTERNAL SIDE OF AFT EDGE ON BEAM #4 AND #5 AT AFT CARGO DOOR. NO CRACKS WERE FOUND PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. ASSOCIATED ER/A 14-620695 ADDED FOR AC 9528. (LP #0605726)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACK ON EXTERNAL FUSELAGE SKIN EDGE, AROUND HANDLE ON PASSENGER DOOR (L1). SUMMARY OF NRC 00302: EXTERNAL FUSELAGE SKIN EDGE AROUND HANDLE ON PASSENGER DOOR (L1) WAS REPAIRED PER ER/A 620705-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620705-14 REV 1. ASSOCIATED ER/A 14-620705 ADDED FOR AC 9528. (LP #0604372)

Part: DOOR — BROKEN (ZONE 600) · airframe 58,982 hrs · 42,251 cycles

-AD- BROKEN INBD BUTE DOOR OUTBD EDGE AT RH WING. (AD) SUMMARY OF NRC 00171: INBD BUTE DOOR OUTBD EDGE AT RH WING WAS REPAIRED PER ERA 618696-14TR REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-618696 ADDED FOR AC 9528. (LP #0598854)

Part: SKIN — DAMAGED · airframe 58,982 hrs · 42,251 cycles

CREASE IN FUSELAGE SKIN WAS FOUND ON REPAIR AREA. SUMMARY 00593: CREASE WAS REPAIRED PER ER/A 620891-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620891-14 REV 0. ACCOMPLISH SECTION II REPETITIVE INSPECTION INSTRUCTIONS WITHININ EVERY 8,000 FLIGHT CYCLES INTERVALS AFTER 26SEP24 PER ER/A 620891-14 REV ORIGINAL SECTION II. ASSOCIATED ER/A 14-620891

Part: ANGLE — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 58,982 hrs · 42,251 cycles

CORROSION ON DOOR JAMB ANGLE AND DOOR JAMB WEB BTW STA Y=200-210 AND X=56 AT FWD PASSENGER DOOR JAMB (L1). SUMMARY OF NRC 00450: CORROSION LEVEL 2. DOOR JAMB ANGLE WAS REPLACED AND DOOR JAMB WEB BTW STA Y=200-210 AND X=56 AT FWD PASSENGER DOOR JAMB WAS REPAIRED PER ER/A 620717-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 620717-14 REV 1. ASSOCIATED ER/A 14-620717 ADDED FOR AC 9528. (LP #0590428)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACKS ON FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSELAGE. SUMMARY OF NRC 00020: FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSELAGE WAS REPAIRED PER PRI 620514-14 REV 5 AND ER/A 620514-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR, TIME CONTROLLED ITEMS SEC II. AT TIME OF ACCOMPLISHMENT ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS, WITHIN EVERY 24 MONTHS AFTER 25SEP24 LOG PAGE #0575970. ASSOCIATED ER/A 14-620514 ADDED FOR AC 9528. (LP #0576565)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACK ON FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSELAGE. SUMMARY OF NRC 00049: FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSELAGE WAS REPAIRED PER ER/A 620582-14 REV ORIG. SECTION I PERMANENT REPAIR PERFORM A GENERAL VISUAL INSPECTION (DVI) PER NDTSP MANUAL PART 9, 09-00-06 WITHIN EVERY 24 MONTHS AFTER 13SEP24 PER ER/A 620582-14 REV ORIGINAL SECTION II. THIS ACTIVITY IS MONITORED PER LOG PAGE #0574024. ASSOCIATED ER/A 14-620582 ADDED FOR AC 9528. (LP #0575631)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACK ON LONGERON 5LH, 8LH, 16LH, 5RH, 7RH, AND 9RH STA 1022 AT PAX CABIN. SUMMARY OF NRC 00404: LONGERONS 5LH, 8LH, 16LH, 5RH, AND 7RH STA 1022 AT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. ON LONGERON 9RH STA 1022 (ET) (HFEC) INSPECTION WAS ACCOMPLISHED AND NO CRACK WAS FOUND PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #0573580)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,982 hrs · 42,251 cycles

CORROSION ON FLOOR SUPPORTS (2 EA) BTW STA=1022 TO STA=1053 ON X=56, AND -X=20 AT PAX CABIN. SUMMARY OF NRC 00835: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) BTW STA=1022 TO STA=1053 ON X=56, AND -X=20 AT PAX CABIN WERE REPLACED PER B717 SRM 51-30-07-0G FIG 9, DWG 9936656-64, AND B717 SRM 51-41-02-0G, 51-41-05-0G. (LP #0572117)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACK ON LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN. SUMMARY OF NRC 00509: LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0568424)

Part: PAN — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACK ON PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR. SUMMARY OF NRC 00301: PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0566607)

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK ON BELOW CUSP WEB BTW STA Y=520 LOWER FACE X=-44 AND STA Y=650 X=-46 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00230: CUSP WEB BTW STA Y=520 LOWER FACE X=-44, WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4, PAR 5, FIG 216. THE CUSP WEB ON STA Y=650 X=-46 WAS REPLACED UNDER NRC 00413. (LP #0565482)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,982 hrs · 42,251 cycles

CORRODED HORIZONTAL FLOOR SUPPORTS AT W1 ON STA Y=180 X-9 TO X-43 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.044", STA Y=196 X 16 TO X 43 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.044", STA Y=200 X 5 TO X-5 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.049", STA Y=200 X 9 TO X 13 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.035", THEREFORE IT IS OUT OF LIMITS. SUMMARY OF NRC 00751: CORROSION LEVEL 2. FLOOR SUPPORTS AT W1 ON STA Y=180 X-9 TO X-43; STA Y=196 X 16 TO X 43; STA Y=200 X 5 TO X-5; STA Y=200 X 9 TO X 13 WERE REPLACED PER DWG S2929169 REV BW AND PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0562395)

Part: PAN — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK ON PAN INTERNAL EDGE BTW BEAM #1 AND #2 AT AFT CARGO DOOR AFT EDGE. SUMMARY OF NRC 00126: INNER PAN ON INTERNAL AFT EDGE BTW BEAM #1 AND #2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0561817)

Part: DOUBLER — WORN (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

WEAR ON INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00289: INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 16 REPAIR 16. (LP #0558908)

Part: LONGERON — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK ON LONGERON 17LH SIDE STA=1022 AFT OF BULKHEAD. CRACK ON LONGERON 12RH SIDE STA=1022 FWD OF BULKHEAD. CRACK ON LONGERON 14 RH STA=1022 FWD OF BULKHEAD AT PAX CABIN. SUMMARY OF NRC 00380: LONGERON 17LH SIDE STA=1022 AFT OF BULKHEAD WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON LONGERON 12RH SIDE STA=1022 FWD OF BULKHEAD AND LONGERON 14 RH STA=1022 FWD OF BULKHEAD AT PAX CABIN. NO CRACKS WERE CONFIMED PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #0556722)

Part: FRAME — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACKED FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX. SUMMARY OF NRC 00386: FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0554632)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,982 hrs · 42,251 cycles

CORROSION ON REPAIR DOUBLER OF JAMB WEB STA Y=954 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00264: CORROSION LEVEL 2. JAMB WEB STA Y=954 AND LONG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PRUCEDURE 2 REPAIR 2. (LP #0554348)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACKS WERE FOUND ON SKIN AT COCKPIT ON AFT UPPER CORNER CUTOUT SLIDING WINDOW. SUMMARY OF NRC 00718: CRACKS ON AFT UPPER CORNER CUTOUT SLIDING WINDOW ON SKIN AT COCKPIT WERE REPAIRED PER B-717-200 SRM 56-10-02-2R PROCEDURE 1 REP 1 FIG 201. PERFORM EXTERNAL GVI OF REPAIR DOBLER AT RH AFT UPPER CORNER CUTOUT SLIDING WINDOW STA 120 BTW PROJECTION LONG 6RH TO LONG 7RH EVERY C CHECK PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 STEP 6 A TABLE 203. (LP #0553609)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,982 hrs · 42,251 cycles

CRACKED CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT. SUMMARY OF NRC 00413: CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT WAS REPLACED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0551885)

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

ELONGATED HOLES ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONGATED HOLES ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO WERE REPAIRED PER B717-200, SRM 51-70-10-02-2R REPAIR 1. (LP #0552860)

Part: FLOORBEAM — CRACKED (ZONE 200) · corrosion level 2 · airframe 58,982 hrs · 42,251 cycles

CORROSION ON FLOOR SUPPORT ON W1 STA Y=198 TO Y=160 X=-5.5 TO X=-9 AT PAX CABIN. SUMMARY OF NRC 00748: CORROSION LEVEL 2. SUPPORT WAS REPLACED ON W1 STA Y=198 TO Y=160 X=-5.5 TO X=-9 AT PAX CABIN PER B717-200 SRM 51-41-01-0G. (LP #0552652)

Part: WEB — DAMAGED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

ELONGATED HOLE ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONGATED HOLE ON WEBS (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO WERE REPAIRED PER B717-200, SRM 51-70-10-02-2R REPAIR 1. (LP #0552858)

Part: HINGE FITTING — DAMAGED (ZONE 500 FLAP) · corrosion level 2 · airframe 59,904 hrs · 43,073 cycles

CORROSION AND SCRATCHES ON HOLES OF OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTBRD WING FLAP HINGE FITTING AT LH WING. SUMMARY OF NRC 00785: CORROSION LEVEL 2. OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTB WING FLAP HINGE FITTING AT LH WING WAS REPAIRED PER PRI 620738-14 REV 0 & ER/A 620738-14 REV ORIGINAL. ASSOCIATED ER/A 14-620738 ADDED FOR AC 9528. (LP #0551076)

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 58,982 hrs · 42,251 cycles

CRACK ON INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00231: INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-00-2R REPAIR 1. (LP #0540825)

Part: COVER — DETACHED (SEAT 13B) · airframe 58,851 hrs · 42,128 cycles

EMERGENCY LIGHT COVER AT SEAT 13B CAME OFF. MAINTENANCE RESECURED THE COVER BACK ONTO THE SEAT PER B717 AMM 25-21. (LP #6193590)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,629 hrs · 41,931 cycles

DURING SERVICE, FOUND THE EMERGENCY LIGHTS IN AFT CABIN AT ROWS 24-29, TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN BATTERY PACK PER B717 AMM 33-55. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #5640369)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,574 hrs · 41,882 cycles

BOTH RT AND LT AFT EMERGENCY DOOR EXIT SIGNS OVER WINGS DO NOT ILLUMINATE.T/S PER B717 FIM 33-50. REPLACED EMERGENCY BATTERY FOR POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5640344)

Part: DOOR FRAME — DAMAGED (AFT CARGO) · airframe 57,719 hrs · 41,160 cycles

RAMP REPORTS DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGE PER B717 SRM 53-20-15-2R REPAIR 10 OPTION 2. FABRICATED, TREATED, & PAINTED REPAIR PARTS PER B717 SRM 53-20-15-2R-10 OPTION 2. INSTALLED PARTS -11 & -13 PER B717 SRM 53-20-15-2R REPAIR 10 OPTION 2. RII COMPLIED WITH. SEALED AND PAINTED IAW B717 SRM 53-20-15. OK FOR SVC. REINSPECT AFTER 8000 CYCLES. (LP #9376522)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,839 hrs · 40,440 cycles

DURING RH OVERWING FRAME REMOVAL, STA 655 TO 715 CUSP WEB WAS FOUND BROKEN. SUMMARY OF NRC 00093: CUSP WEB RH ON STA 655 TO 715 WAS FABRICATED AND REPLACED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4, SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2970129)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,839 hrs · 40,440 cycles

A.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 RH (REF CARD 5310-01436-04D). SUMMARY OF NRC 00072: OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717 AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9528. (LP #2968061)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,839 hrs · 40,440 cycles

A.D. CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-04D). SUMMARY OF NRC 00073: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER B717 AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9528. (LP #2968068)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,839 hrs · 40,440 cycles

A.D. CRACK OF 0.200 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=715.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00071: OVERWING FRAME AT STA Y=715.000 LH WAS REPLACED PER B717 AMDS 5310-01436-03A. ASSOCIATED AA 5310-01436 ADDED FOR AC 9528. (LP #2968045)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,839 hrs · 40,440 cycles

DURING LH OVERWING FRAME REMOVAL, STA 655 TO 715 CUSP WEB WAS FOUND BROKEN. SUMMARY OF NRC 00094: CUSP WEB LH ON STA 655 TO 715 WAS FABRICATED AND REPLACED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4; 51-41-02-0G, AND 51-41-05-0G PAR.8. (LP #2968543)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,961 hrs · 39,695 cycles

THE TAIL CONE SLIDE COVER IS LOOSE AND THE SLIDE UNRAVELING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED THE SLIDE ASSEMBLY AND PIN INSTALLED. THE TAIL SLIDE WAS REPLACED IAW CARD 2561-9006. WORK ACCOMPLISHED ON LOG 2729625. RII INSPECTION ACCOMPLISHED QC 5121. (LP #2729859)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,961 hrs · 39,695 cycles

THE AFT TAIL SLIDE RETAINER CABLE CLIP IS BROKEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE CLIP IAW CMM 25-66-20. RII C/W QC5219. (LP #2730102)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,362 hrs · 39,188 cycles

SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS ARE OUT. MAINTENANCE REPLACED THE OVERHEAD EXIT ROW EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9882433)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,268 hrs · 39,102 cycles

THE PILOT NOTICED THAT THE EMERGENCY EXIT SIGN WAS MISSING ABOVE THE SERVICE DOOR. MAINTENANCE REATTACHED THE LENSE COVER.

Part: BATTERY PACK — INOPERATIVE · airframe 55,177 hrs · 39,022 cycles

DURING SERVICE CHECK, THE L1 DOOR EMERGENCY LIGHT WAS FOUND TO COME ON AND OFF. MAINTENANCE REPLACED THE BATTERY PACK B5-235 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9579903)

Part: NONE — NONE · airframe 53,851 hrs · 37,783 cycles

THE AFT BULKHEAD DOOR EXIT IDENTIFIER EMERGENCY LIGHT AND THE TAIL COMPARTMENT EMERGENCY VENTRAL LIGHTS ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-260, PER B717 AMM 33-51. (LP #8759477)

Part: SPOILER — DELAMINATED (ZONE 600) · airframe 18,107 hrs · 13,934 cycles

CRACK,LEFT AND RIGHT LOWER RADIUS OF FRONT CHANNEL AT ACTUATOR FITTING, WORN DOWN STOPS.

Part: PAN — CORRODED (LAVATORY DRAIN) · corrosion level 2 · airframe 52,355 hrs · 36,460 cycles

LAV DRAIN PAN CORRODED INSIDE AROUND DUMP CHUTE. (MARKED) SUMMARY SEE NRC 001-0292:2550-2003/001 00222: REPLACED LAV DRAIN PAN PER ER/A 570608-14 REV ORIGINAL. (LP #1942348)

Part: SHEAR TIE — CORRODED (BS 974) · airframe 52,355 hrs · 36,460 cycles

SHEAR TIE AFT CARGO AT STA 974 HAS CORROSION. SUMMARY, SEE NRC 00351: TASK CARD NUMBER 001-0292:2550-2003/ 007 REPLACED SHEAR TIE AT STATION 974 REF BAC DWG 9958215. (LP #1941017)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 52,355 hrs · 36,460 cycles

CORROSION CAUSED PAINT BUBBLING IN SEVERAL AREAS OF THE AFT CARGO LOWER DOOR JAMB. (MARKED). SUMMARY SEE NRC 001-0373:5231-2002/001 00177: REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #1939785)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 52,355 hrs · 36,460 cycles

SEAT TRACK CORRODED AT FORWARD GALLEY LOCATED AFT OF R-1 DOOR- MARKED. SEAT TRACK RUNS UP UNDER GALLEY. VISIBLE TRACK IS CORRODED. REPAIRED SEAT TRACK PER B717 SRM 53-20-52-2R. (LP #1937160)

Part: STRINGER — CORRODED (BS 908-946 S29L) · airframe 52,355 hrs · 36,460 cycles

REF NRC 231: C2 CHECK - CORROSION IN CENTER OF STRINGER STR29L STA 908-946. REPLACED STRINGER 29L PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1936823)

Part: SHEAR TIE — CORRODED (BS 946) · corrosion level 2 · airframe 52,355 hrs · 36,460 cycles

THE SHEAR TIE AFT CARGO AT STA 946 HAS CORROSION. SUMMARY SEE NRC 001-0292:2550-2003/005 00349: REPLACED SHEAR TIE PER B717 SMR 51-40-08. (LP #1934168)

Part: PAN — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 52,355 hrs · 36,460 cycles

FORWARD CARGO DOOR JAMB PAN CORRODED IN MANY LOCATIONS- MARKED. SUMMARY SEE NRC 001-0374:5231-2003/001 00209: REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 6. (LP #1931552)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,506 hrs · 34,915 cycles

THE CEILING EMERGENCY LIGHTS FROM SEAT ROW 15 TO SEAT ROW 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, PER B717 AMM 33-51. TEST WAS GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,506 hrs · 34,915 cycles

THE FORWARD SERVICE DOOR AND L1 DOOR EXIT IDENTIFIER LIGHTS (L2-832, L2-833) ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, PER B717 AMM 33-51. TEST GOOD. OK FOR SERVICE.

Part: CABLE — OUT OF ADJUST (TAILCONE) · airframe 49,687 hrs · 34,191 cycles

THE TAIL CONE RELEASE TEST FAILED WITH THE AFT BULKHEAD DOOR. MAINTENANCE ADJUSTED THE AFT BULKHEAD DOOR ARM ASSEMBLY PULL CABLE REF B717 AMM 53- 52. OPERATIONAL CHECK IS NOW FUNCTIONAL. (LP #1518530)

Part: ENGINE — ODOR (NR 1) · airframe 47,847 hrs · 32,758 cycles

THE FLIGHT CREW DIVERTED DUE TO ODOR CIRCULATING IN THE FLIGHT DECK AND CABIN AFTER ROTATION. THE FLIGHT ATTENDANTS REPORTED THE SMELL AND HAZE DURING CLIMB AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE.

Part: FRAME — CRACKED (BS 696) · airframe 47,847 hrs · 32,756 cycles

CRACK INDICATION OF THE UPPER RADIUS OF THE FRAME TAB. CRACK LENGTH APPROXIMATELY 1/8 IN. NRC 066-0002:5310-01436-01B/001 00042: REPLACED LT OVER-WING FRAME AT STA 696 PER AMDS WORK CARD 5310- 01436-03A.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 47,077 hrs · 32,216 cycles

EMERGENCY LOWER LIGHTS WERE FOUND INOPERATIVE AT 21B AND 20CDE. MAINTENANCE FOUND THAT THE BATTERY PACK AT STA 804 HAD FAILED. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51-18. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5547384)

Part: LANYARD — OUT OF POSITION (R2 DOOR) · airframe 46,473 hrs · 31,792 cycles

THE RIGHT HAND CABIN DOOR (NR 2) GIRT BAR COVER IS OFF AND IS PREVENTING THE DOOR FROM FULLY OPENING. MAINTENANCE FOUND THE SLIDE RELEASE CABLE PINS TO BE OUTSIDE OF THE DOOR CLIPS. THE SLIDE LANYARD WAS REINSTALLED IN THE PROPER POSITION IAW AMM 25-61. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 45,718 hrs · 31,277 cycles

THE L1 DOOR UPPER EXIT SIGN WAS MISSING. MAINTENANCE INSTALLED A NEW EXIT SIGN IAW AMM 33-51.

Part: LENS — LOOSE (SIGN) · airframe 45,057 hrs · 30,809 cycles

THE EMERGENCY EXIT SIGN LENS IN THE CABIN WAS FOUND LOOSE. MAINTENANCE REPAIRED THE SIGN LENS AT THE L1 DOOR. OPS CHECKED OK IAW AMM 33-51. OK FOR SERVICE.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 44,182 hrs · 30,257 cycles

CEILING EMERGENCY LIGHT INOPERATIVE AT 17CDE. FOUND A LOOSE WIRE ON THE SOCKET. SECURED THE CONNECTOR. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,336 hrs · 29,717 cycles

OVERWING EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 43,308 hrs · 29,698 cycles

EMERGENCY EXIT DIFFUSER LENS UNSECURE. SIGN COVER SECURED. OK FOR SERVICE.

Part: STUD — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 43,354 hrs · 29,729 cycles

CORROSION ON RT FLAP HINGE FITTING AROUND OF OUTBD LOWER STUD XW 251. RT CENTER FLAP HINGE FITTING, WING FLAP HINGE MOUNTING STUD WERE REPLACED IAW AMM 57-55-25 AND HYDRAULIC LINES AND ACTUATOR CYLINDER WERE REMOVED AND INSTALLED IAW AMM 27-55-03 AND LEAK AND OPS TESTED OK.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 43,299 hrs · 29,693 cycles

CRACKED VERTICAL STABILIZER FRONT SPAR CAP LT SIDE BELOW ZFS=52.267. THE VERTICAL STAB FRONT SPAR CAP WAS REPAIRED IAW ER/A 560934-14AD, REV ORIGINAL AND ETI-17-17-169, REV 3.

Part: SKIN — CRACKED (BS 1037) · airframe 43,299 hrs · 29,693 cycles

CRACK ON FUSELAGE SKIN BS 1037, LONGERON 14R. THE SKIN WAS REPAIRED IAW ER/A 560879-14, REV ORIGINAL, AND ETI-17-17-142, REV 6.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON LT AND RT FWD AND AFT CARGO TRACK IN THE AFT CARGO BAY. THE CARGO TRACKS WERE REPLACED IAW SRM 51-41-01-0G, AND 51-41-02-0G.

Part: SKIN — CORRODED (BS 660-756) · corrosion level 2 · airframe 43,299 hrs · 29,693 cycles

CORROSION THE UPPER SKIN BETWEEN BS 660 AND 756, LBL 40 AND 60. REPAIRED IAW ER/A 560894-14, REV ORIGINAL. AND ETI-17-17-151, REV 1.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON AFT LOWER CARGO DOOR FRAME. THE SECTION OF THE DOOR FRAME AND REPAIR SPLICE WERE REPLACED IAW SRM 53-20-15-2R-7.

Part: GUSSET — CORRODED (CARGO DOOR AREA) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON GUSSETS ABOVE CARGO DOOR FRAME WEB. THE GUSSET WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-05-0G, AND DWG 5913537, REV D.

Part: FRAME SPLICE — CORRODED (BS 946) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON FRAME CAP SPLICE, BS 946 BETWEEN LONGERONS 27L TO 28L. THE FRAME SPLICE WAS REPLACED IAW DWG 9919603, REV CC, AND SRM 51-41-05-0G.

Part: SKIN — CORRODED (BS 727-756) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON UPPER SKIN BS 727 TO 756. REPAIRED IAW ETI-17-17-162 R1 AND ER/A 560922-14, REV ORIGINAL.

Part: STIFFENER — CRACKED (BS 813) · airframe 43,298 hrs · 29,692 cycles

CRACK ON VERTICAL STIFFENER LOWER EDGE ON BS 813 AT AFT CARGO BAY. STIFFENER WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG 201.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 43,298 hrs · 29,692 cycles

CRACKED FLOORBEAM AT BS 737, RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05-0G, AND 51-41-02-0G.

Part: HINGE — DAMAGED (AFT CARGO DOOR) · airframe 43,298 hrs · 29,692 cycles

ELONGATED HOLES OF AFT/FWD HINGES ON AFT CARGO DOOR (C2). THE HINGES WERE REPLACED IAW AMM 52-31-02.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON FINGER DOUBLER BTW STA Y=937 TO Y=943 BTW LONG 25R TO 26R AT AFT CARGO COMPARTMENT IN REF NRC S/N 00321 (CCT). CORROSION LEVEL 2. FINGER DOUBLER SECTION Y=937 TO 943 WAS REPLACED PER SRM 51-41-02-0G AND DWG 5911424 REV CZ.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON CUSP ANGLE BELOW FORWARD GALLEY SERVICE DOOR JAMB FROM STA Y= 159 TO Y= 208. CORROSION LEVEL 2 ON CUSP ANGLE BELOW FWD GALLEY SERVICE DOOR FROM STA Y=159 TO Y=208 WAS REPAIRED PER ETI-17-17-144 REV 2 AND ER/A 560881-14 REV ORIGINAL.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON CENTER WING UPPER SKIN PLATE RT SIDE REF STA Y 746, BTW XCW 22 TO XCW 49. CORROSION LEVEL 2. CENTER WING UPPER SKIN WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI-17-17-151 REV 1.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

SEVERAL CORROSION POINTS ON CENTER WING UPPER SKIN PLATE BTW Y=660 AND Y=756, BTW X=22 AND X=26, ALSO ON Y=750 BTW X=22 AND X=44. CORROSION LEVEL 2. CENTER WING UPPER SKIN PLATE WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI-17-17-151 REV 1 AND AREA WITHIN LIMITS WAS ATTENDED WITH NRC 577.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON CENTER WING UPPER SKIN PLATE RT SIDE FROM STA Y 664 TO Y 715 BTW XCW 43 AND XCW 58. CORROSION LEVEL 2. CENTER WING UPPER SKIN PLATE RT WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI 17-17-151 REV 1 AND AREAS WHITIN LIMITS WAS ATTENDED WITH NRC 577.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CRACK ON FUSELAGE SKIN STA Y=1076 LONG 14L. FUSELAGE SKIN STA Y=1076 LONG 14L WAS REPAIRED (PERMANENT REPAIR) PER ER/A 560880-14 REV ORIGINAL AND ETI-17-17-143 REV 2.

Part: SPLICE — CORRODED (SEAL DEPRESSOR) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORRODED LOWER SEAL DEPRESOR SPLICES AT FWD CARGO DOOR FRAME. THE SEAL DEPRESSOR SPLICES WERE REPLACED IAW SRM 53-20-15-0I-1, FIG 1, SHEET 2, AND 51-41-02-0G.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON UPPER RT WING SKIN AFT EDGE BETWEEN XCW -22 TO XCW -58 ON THE RT MLG WHEEL WELL. REPAIRED IAW ETI-17-17-151, REV 1, AND ER/A 560894-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1133) · airframe 43,298 hrs · 29,692 cycles

CRACKED LONGERON 2R, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 43,298 hrs · 29,692 cycles

DELAMINATED FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R, REP 3.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 43,298 hrs · 29,692 cycles

CRACKED DOOR FRAME LBL 46, LBL 17, AND RBL 17 AT NLG WHELL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, REPAIR 2, FIG 201.

Part: LONGERON — CRACKED (BS 1144) · airframe 43,298 hrs · 29,692 cycles

CRACK ON LONGERON 3R, BS 1144. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

Part: LATCH — CORRODED (R1 DOOR AREA) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION SLIDE LATCHES BS 160 TO 200, RBL 54. THE SLIDE SUPPORTS WERE REPLACED IAW SRM 51-40-08-0G.

Part: GRILL — CORRODED · airframe 43,298 hrs · 29,692 cycles

CORROSION ON FRAME GRILL NR 1 RT AT PAX CABIN. THE FRAME GRILL WAS REPAIRED IAW SRM 53-00-00-2R-2, AND DWG 5956960, REV AM.

Part: WEB — CORRODED (BS 200-218) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON WEB BETWEEN BS 200 TO 218, RBL 44 AND 54. THE WEB WAS REPLACED IAW SRM 53-20-51-0I-1, FIG 1, SHEET 1, 51-41-08-OG, AND SRM 51-41-05-OG.

Part: WEB — CORRODED (BS 148-200) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON UPPER & LOWER WEB BETWEEN BS 148 TO 200, RBL 54 TO 58. THE WEB WAS REPLACED IAW SRM 53-10-51-0I-2, FIG 1, 51-70-10-2R-2, FIG 201, 51-41-02-0G, AND 51-41-05-0G.

Part: CUSP WEB — CRACKED (BS 240-256) · airframe 43,298 hrs · 29,692 cycles

CRACKED RT CUSP WEB BETWEEN BS 240 TO 256. BETWEEN THE SEAT TRACKS RBL 54 TO 44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 223.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON FLOOR SUPPORT BS 200 TO RBL 46. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, 51-10-04-0G, PAR 21, 15, AND 51-41-02-0G.

Part: CUSP WEB — CRACKED (BS 235) · airframe 43,298 hrs · 29,692 cycles

CRACK ON THE RT CUSP WEB BS 235, RBL 44. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: CHANNEL — DAMAGED (COCKPIT) · airframe 43,298 hrs · 29,692 cycles

CRACKED CHANNEL AND DISBONDED TRIM ON THE FLOOR PANEL 211AKF IN THE COCKPIT. THE CHANNEL WAS REPAIRED AND TRIM WAS BONDED IAW SRM 53-20-50-2R, FIG 201, AND 51-20-05-0G.

Part: SUPPORT ANGLE — CORRODED (BS 170) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON THE SUPPORT ANGLE AT BS 170, RBL 56. THE SUPPORT ANGLE WAS REPLACED IAW SRM 53-10-15-0I-2-01, FIG 1, AND 51-41-05-OG.

Part: SKIN — WORN (L1 DOOR) · airframe 43,298 hrs · 29,692 cycles

WEAR ON THE L1 DOOR HOLD OPEN HOOK EXTERNAL SKIN CUTOUT. THE SKIN WAS REPAIRED IAW ETI-17-17-146, REV ORIGINAL AND ER/A 560884-14, REV ORIGINAL.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 43,298 hrs · 29,692 cycles

CRACKED FLOOR PANEL 211PF IN THE COCKPIT. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON UPPER BARREL NUT, BOLT, AND BARREL NUT BORE AT RH HORIZONTAL STABILIZER HSS 6.625 AND BARREL NUT NR 11 FROM REAR TO FRONT SPAR. A PERMANENT REPAIR WAS PERFORMED ON THE BARREL NUT BORE NR 11 IAW ER/A 560888-14, REV ORIGINAL, AND ETI-17-17-147, REV 1, AND A NEW UPPER BARREL NUT AND BOLT WERE INSTALLED IAW AMM 20-20-22.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

DENT ON FUSELAGE SKIN BTW STA Y=465 TO Y=470, BTW LONG 20L TO 21L IN REF MON JOB 112-0001. DENT ON FUSELAGE SKIN BTW STA Y=465 TO Y=470, BTW LONG 20L TO 21L IN REF MON JOB 112-0001. PERMANENT REPAIRED WAS PERFORMED PER DWG SG09530002 AND SRM 51-41-02 OG, 51-41-05 0G.

Part: SKIN — CRACKED (RUDDER) · airframe 43,298 hrs · 29,692 cycles

CRACKED RUDDER SKIN LT SIDE LWR EDGE ON AREA OF "PAINT OR REWORK REQUIRES BALANCING" PLACARD. RUDDER SKIN LT SIDE LWR EDGE WAS REPAIRED PER SRM 55-00-00-2R-1.

Part: FORMER — CRACKED (BS 737) · airframe 43,298 hrs · 29,692 cycles

CRACKED RT FORMER, BS 737 AT KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1.

Part: FORMER — CRACKED (BS 694) · airframe 43,298 hrs · 29,692 cycles

CRACKED FORMER ON BS 694 AT KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1.

Part: SEAT TRACK — CORRODED (BS 200-256) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON THE RT SEAT TRACK BETWEEN BS 200 TO 256, RBL 22. THE SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R, AND SRM 51-40-08-0G.

Part: FORMER — CRACKED (BS 679) · airframe 43,298 hrs · 29,692 cycles

CRACKED FORMER ON BS 679 AT KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1.

Part: FERRULE — DAMAGED (CABIN) · airframe 43,298 hrs · 29,692 cycles

DAMAGE FERRULES ON FLOOR PANELS #221BF, 221CF, 221KF, 221JF, 221FF, 221EF, 221DF, 211ALF, 211ASF, 221WF, 221UF, 221VF, 222ACF, 222AHF, 222AMF, 222APF, 222AVF, 222AUF, 222ATF, 223DF, AND 223BF (CPAX). NRC 00512: FLOOR PANELS #221JF AND 221BF WERE REPLACED PER B-717 SRM REPAIR (3) 53-20-50 AND FERRULES DAMAGE WERE REPLACED IN FLOOR PANELS #221KF, 221FF, 221CF, 221DF, 221UF, 221WF, 221EF, 211ALF, 211ASF, 221VF, 222AHF, 222AMF, 222AVF, 223DF, 223BF, 222ACF, AND 222APF PER B-717 SRM 53-20-50-2R REP 3 AND FLOOR PANEL #222ATF WAS REPAIRED PER B-717 SRM 53-20-50-2R REP 3 AND FLOOR PANEL #222AUF WAS PERFORMED WITH NRC 00511. (LP #0195754)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,298 hrs · 29,692 cycles

DELAMINATED FLOOR PANELS #221AF, 221JF, 221VF, 22TF, 222AUF, AND 223GF (CPAX). NRC 00511: FLOOR PANELS #221AF, 221JF, AND 223GF WERE REPLACED PER B-717 SRM REPAIR (3) 53-20-50 AND FLOOR PANEL #221VF WAS PERFORMED WITH THE NRC 00512 AND FERRULES ON FLOOR PANEL #222AUF WERE REPLACED PER B-717 SRM 53-20-50-2R REP 3. AND THIS NRC HAS A TYPO ERROR, THE FLOOR PANEL REPORTED WAS 22TF AND MUST BE 222TF AND FLOOR PANEL #222TF WAS RE-INSPECTED AND NO DAMAGES WERE FOUND PER B-717 AMM 05-21-02. (LP #0195762)

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON THE FLOOR SUPPORT BS 200, LBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, 51-41-02-0G, AND 51-41-01-0G.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 43,298 hrs · 29,692 cycles

CRACKED CHANNELS ON FLOOR PANELS #221NF, 222AJF, 222EF, 221TF, 222AF, 222AFF, 222XF, AND 222SF AT PAX CABIN. NRC 00456: FLOOR PANELS #221NF, 222AJF, 222EF, 221TF, 222AF, 222AFF, 222XF, AND 222SF WERE REPAIRED PER B717 SRM 53-20-50-2R AND 51-41-02-0G. (LP #0194398)

Part: FLOOR SUPPORT — CORRODED (BS 196-200) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON FLOOR SUPPORT BS 196 - 200, LBL 56. THE FLOOR SUPPORT WAS REPLACED IAW SRM SRM 53-10-51-0I-2, AND 51-41-05-0G.

Part: CUSP WEB — CORRODED (BS 807-808) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 807 TO 808, LBL 54 TO 58. CUSP WEB WAS REPAIRED PER B717 SRM 53-00-55-2R-4, FIG. 215.

Part: CUSP WEB — CORRODED (BS 570) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB UPPER & LOWER SURFACES BETWEEN RBL 44 AND 60, BS 570. REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.

Part: CUSP WEB — CORRODED (BS 920-923) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON THE RT CUSP WEB BETWEEN BS 920 TO 923, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.

Part: CUSP WEB — CORRODED (BS 397-400) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON RT CUSP WEB, BS 397 TO 400, RBL 54 TO 58. REPAIRED IAW SRM 53-00-55-2R-4, FIG 206.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB SURFACE BTW X=54 AND X=60 STA Y= 649. LT CABIN FLOOR CUSP WEB SURFACE BTW X=54 AND X=60 STA Y= 649 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 215.

Part: HOUSING — WORN (L1 DOOR) · airframe 43,298 hrs · 29,692 cycles

HIDDEN SEVERE WEAR ON HOUSING AT L1 DOOR HOLD OPEN HOOK EXTERNAL SKIN CUTOUT (DR). HOUSING WAS REPLACED PER SRM 51-41-02-0G AND DWG 4955948 REV D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CRACK ON FRAME STA Y=1037 BTW LONG 17-18 RT AT PAX CABIN. FRAME STA Y=1037 BTW LONG 17-18R AT PAX CABIN WAS REPAIRED PER SRM 53-20-07-2R-4 FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=44 AND X=60 STA 905. LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=44 AND X=60 STA 905 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 216.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CRACK ON RT CABIN FLOOR CUSP WEB BTW X=-54 AND X=-60 STA Y=703. RT CABIN FLOOR CUSP WEB BTW X=-54 AND X=-60 STA Y=703 WAS REPAIRED PER SRM 51-41-02-0G AND 53-00-55-2R-4 FIG 215.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,298 hrs · 29,692 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=44 AND X=60 STA Y=551. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R-4 FIG 215.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

CRACK ON SHEAR CLIP (3 E/A) STA Y=1022 BTW LONGS 16-17L, 14-13L, ALSO 14-13R AT PAX CABIN. SHEAR CLIP (3 E/A) STA Y=1022 BTW LONGS 16-17L, 14-13L, ALSO 14-13R AT PAX CABIN WERE REPLACED PER SRM 51-20-09, 51-41-02-0G, AND 51-41-05-0G.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 43,298 hrs · 29,692 cycles

SUNKEN FASTENER ON LT CABIN FLOOR CUSP WEB STA Y=662 BTW X=54 AND X=60 ALSO RT CUSP WEB ON STA Y=560 BTW X=-54 AND X=-60. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R-4 FIG 215.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 43,298 hrs · 29,692 cycles

CRACKED FITTING ON LOWER EDGE AND BS 389 IN THE FWD CARGO DOOR INTERNAL STRUCTURE. FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,298 hrs · 29,692 cycles

CRACK ON AFT EDGE OF OUTER PAN BELOW CLIP BETWEEN BEAMS 1 AND 2 AT FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-4.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,298 hrs · 29,692 cycles

CRACK ON FWD EDGE OF OUTER PAN BELOW CLIP BETWEEN BEAMS 1 AND 2 AT FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-4.

Part: LANYARD — MISROUTED (R1 DOOR SLIDE) · airframe 43,298 hrs · 29,692 cycles

LANYARD IMPROPERLY ROUTING ON R1 DOOR SLIDE. THE SLIDE WAS REPLACED IAW AMM 25-61-03.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,298 hrs · 29,692 cycles

CRACKED NR 1 & 3 BEAMS ON THE L1 DOOR INTERNAL STRUCTURE AFT SECTION. THE NR 1 BEAM WAS REPAIRED IAW SRM 52-10-02-2R-7. HFEC WAS ACCOMPLISHED ON BEAM NR 3, NO CRACKS WERE FOUND IAW NDTSPM PART 6, 06-10-01.001.

Part: SKIN — DAMAGED · airframe 43,133 hrs · 29,571 cycles

ON ARRIVAL, FOUND A DENT AND GOUGES 28 INCHES AFT OF WATER SERVICE PANEL ON ACFT LEFT. REPAIRED IAW ER/A 560289-14.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 37,684 hrs · 25,489 cycles

WHILE AT 14,000' IN DESCENT, FLIGHT CREW NOTED AN ODOR IN THE COCKPIT ASSOCIATED WITH ELECTRICAL ODOR. WE HAD NO FURTHER INDICATIONS OF THE ISSUE AND THE SMELL DISSIPATED WITHIN 3 MINUTES. MAINTENANCE FOUND A BURNING PLASTIC ODOR COMING FROM GALLEY G1 OVEN. R & R F/C GALLEY OVEN IAW AMM 25-34. ALSO, FOUND COFFEEMAKER NR 2 HAVING A VERY STRONG BURNED ODOR. R & R NR 2 COFFEEMAKER IN G1 GALLEY, FWD RT TOP, IAW AMM 25-36. ALSO CHECKED E/E, FLIGHT COMPARTMENT AND F/C CABIN. NO OTHER INDICATIONS FOUND. THE ACFT HAS RETURNED TO SERVICE. LP 7336236.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,608 hrs · 23,721 cycles

DURING LINE CHECK, THE CEILING EMERGENCY LIGHT FIXTURE ABOVE ROWS 13AB AND 14AB WAS FOUND TO BE DAMAGED WITH THE BULB FALLING OUT. THE LIGHT FIXTURE AND LAMP REPLACED.

Part: LATCH — DIRTY (L1 DOOR) · airframe 33,548 hrs · 22,111 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCHES DIRTY. CLEANED LATCHES IAW MM & SRM.

Part: LATCH — DIRTY (R1 DOOR) · airframe 33,548 hrs · 22,111 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCHES DIRTY. CLEANED LATCHES IAW MM & SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT FS CUSP WEB CRACKED AT STATION 902. REPAIRED CUSP WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

WEB CORRODED AT STATION 200, RBL 44. R&R WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT FS CUSP WEB CRACKED AT STATION 218. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 33,548 hrs · 22,111 cycles

COCKPIT FLOOR PANEL 211ALF IS DAMAGED. R&R PANEL IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

VERTICAL STIFFENER CRACKED AT STATION 737, LBL 45. R&R SUPPORT IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

SHEAR TIE CRACKED AT FRAME 1152, LONGERON 1 FORMER. R&R TIE CLIP IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

SHEAR TIE CRACKED AT FRAME 1169, LONGERON 2L FORMER. R&R FORMER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FRAME CLIP CRACKED AT STATION 1146, LOWER SIDE. REPAIRED BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

LT FRAME ANGLE CRACKED AT 1178 LT SIDE. R&R CLIP IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

SHEAR TIE CRACKED AT STATION 1161, LONGERON 2R. R&R SHEAR TIE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

LT FS CUSP WEB CRACKED AT STATION 674. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FLOOR PANEL 222 AFF CRACKED. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 541-STATION 560. R&R CUSP WEB IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT FS CUSP WEB SPLICE CORRODED AT BS 579 TO BS 598. REPAIRED WEB SPLICE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 503 TO STATION 522. R&R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 889 TO STATION 908. R&R CUSP WEB IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT DOUBLER CORRODED BETWEEN STATION 889 TO STATION 908. R&R DOUBLER IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

FLOOR PANEL 222 XF CRACKED. REPAIRED PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CRACKED BETWEEN STATION 655-STATION 674. REPAIR DOUBLER IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

LT CUSP WEB CORRODED AT STATION 687. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FLOOR PANEL 222 NF CRACKED. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 617 & STATION 636. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

FLOOR PANEL 222 HF CORRODED. R&R PANEL IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FLOOR PANEL 222 ALF CRACKED. REPAIRED PANEL IAW SRM & MM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

FLOOR PANEL 222 AQF CRACKED. REPAIRED DOUBLER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 33,548 hrs · 22,111 cycles

AFT CARGO BARRIER DOOR FWD UPPER SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 484 & STATION 503. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED AT STATION 842. R&R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

LT CUSP WEB CORRODED BETWEEN STATION 579 & STATION 598. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT CUSP WEB CORRODED BETWEEN STATION 636 & STATION 655. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

SEAT TRACK CORRODED BETWEEN STATION-STATION 908, RBL 22. R&R SEAT TRACK IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

WEB CRACKED AT STATION 207, LONGERON 15L. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FLOOR PANEL 222 ASF CRACKED. REPAIRED PANEL IAW SRM & AMM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

FLOOR PANEL 222 SF CORRODED. REPAIRED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT FS CUSP WEB CORRODED AT BS 861. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

LT AFT NLG DOOR AFT HINGE CUT OUT CRACKED IN FS SKIN. REPAIRED DOUBLER IAW SRM & MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

RT AFT NLG DOOR AFT HINGE CRACKED AT CUT OUT IN FS SKIN. REPAIRED DOUBLER IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

AFT ACCESSORY COMPARTMENT SHEAR TIE CRACKED AT BS 1144, BETWEEN LONGERON 1R & 2R. R&R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

AFT ACCESSORY COMPARTMENT SHEAR TIE CRACKED AT BS 1144, BETWEEN LONGERON 1L & 2L. R&R SHEAR TIE IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

FWD CARGO DOOR CUTOUT LOWER JAMB CORRODED. R&R JAMB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

SEAT TRACK CORRODED BETWEEN STATION 266 TO STATION 410, RBL 44. R&R SEAT TRACK IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

AFT CARGO DOOR CUTOUT LOWER DOOR JAMB CORRODED. R&R PAN SECTION IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AMF DELAMINATED. R&R PANEL IAW SRM & AMM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 ACF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AGF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 BF DELAMINATED. R&R PANEL IAW SRM & AMM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 APF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 FF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AVF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 RF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 JF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 PF DELAMINATED. R&R PANEL IAW SRM & AMM.

Part: BONDING STRAP — CRACKED (FUSELAGE) · airframe 33,547 hrs · 22,111 cycles

RT WING TO BODY BONDING STRAP CRACKED AT STATION 653, LONGERON 19R. R&R STRAPS IAW SRM & DRAWING.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 WF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AAF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBEAM — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 LF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOOR BOARD 222 GF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,547 hrs · 22,111 cycles

CABIN FLOORBOARD 223DF DELAMINATED. R&R FLOORBOARD PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 221 UF DELAMINATED. R&R FLOOR PANEL IAW AMM & SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,247 hrs · 22,526 cycles

AFT CARGO DOOR CUT OUT LOWER DOOR JAMB CORRODED. REPAIRED PAN IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AHF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 AEF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 33,548 hrs · 22,111 cycles

FLOORBOARD 222 ABF DELAMINATED. R&R FLOOR PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 222 ATF DELAMINATED. R&R PANEL IAW SRM & AMM.

Part: ANGLE — CRACKED (SLAT TRACK) · airframe 33,548 hrs · 22,111 cycles

LT WING LE SLAT TRACK NR 12 INBD SIDE CRACKED AT ANGLE. R&R ANGLE IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,547 hrs · 22,111 cycles

CABIN FLOORBOARD 223BF DELAMINATED. R&R FLOORBOARD PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,548 hrs · 22,111 cycles

CABIN FLOORBOARD 221 WF DELAMINATED. R&R PANEL IAW SRM & MM.

Part: CABLE — LOOSE (R1 DOOR) · airframe 33,817 hrs · 22,276 cycles

R1 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE IAW SRM.

Part: COVER — BROKEN (R1 DOOR) · airframe 32,306 hrs · 21,337 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER BROKEN. REMOVED AND REPLACED COVER PER EA.

Part: COVER — LOOSE (R1 DOOR) · airframe 32,251 hrs · 21,302 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. REMOVED AND REPLACED COVER PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,186 hrs · 20,607 cycles

EMERGENCY LIGHTS INOP BETWEEN ROW 25 TO ROW 31. REMOVED AND REPLACED BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,787 hrs · 20,337 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 30,600 hrs · 20,217 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: DOOR FRAME — CORRODED (FWD CARGO)

FORWARD CARGO DOOR FRAME CORRODED. ACCOMPLISHED DOOR FRAME SPLICE REPAIR PER SRM 53-20-15.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 200, LONG RBL 23 TO RBL 50, CORROSION. ACCOMPLISHED FLOOR WEB REPAIR PER B717 SRM 53-00-00, 51-70-10, 51-41-02, 53-21-01 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LONG RBL 50, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 160, LONG LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 53-00-00 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LONG RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT FILLER REPAIR PER B717 SRM 53-00-00 AND 51-70-10.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 200, LONG RBL 18 TO RBL 27, CORROSION. ACCOMPLISHED FLOOR WEB REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-70-10 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, LONG RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 196, LBL 18, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, LONG RBL 36, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 237, LONG LBL 18, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LONG RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SCUFF PLATE — CORRODED (FUSELAGE)

R1 DOOR FWD SCUFF PLATE, CORROSION. ACCOMPLISHED FWD SCUFF PLATE REPLACEMENT PER B717 SRM 51-41-01 AND 51-41-02.

Part: SCUFF PLATE — CORRODED (FUSELAGE)

R1 DOOR AFT SCUFF PLATE, CORROSION. ACCOMPLISHED AFT SCUFF PLATE REPLACEMENT PER B717 SRM 51-41-01, 53-00-00, 51-20-09 AND 51-40-08.

Part: UNKNOWN — ODOR (CABIN)

AIRCRAFT HAS FOUL SMELLING ODOR LIKE AMMONIA AROUND FWD LAV BUSINESS CLASS TO THE COCKPIT AND IS MAKING CREW NAUSEATED, IT'S GRADUALLY GOTTEN WORSE AND IS VERY STRONG ON THE GROUND WITH DOORS SHUT. IT IS STILL NOTICEABLE IN THE AIR BUT MUCH WORSE WHEN A/C IS ON GROUND, LAV WAS SERVICED AND STILL SMELLED IT. UPON ARRIVAL INITIAL EVALUATION FOUND NO UNUSUAL SMELLS. INSPECTED OVERHEAD BINS, SEAT POCKETS, LAVS, AND GALLEY AREAS INCLUDING CARGO BINS. SERVICED LAVS, RAN A/C PACKS ON GROUND AND FOUND NO ODORS OR SMELLS, OK FOR SERVICE. RELEASED A/C.

Part: COVER — MISSING (EXIT SIGN)

EMERGENCY EXIT COVER IN FIRST CLASS IS MISSING. INSTALLED MISSING EXIT SIGN COVER PER 717 AMM 33-51. OK FOR CONTINUED SERVICE.

Part: FIXTURE — DEFECTIVE (CABIN)

RT FUSELAGE EMERGENCY EVAC LIGHT INOP. REMOVED AND REPLACED BULB AT EVAC LIGHT FIXTURES. RT FUSELAGE OPS CHECK GOOD.

Part: GAUGE — DEFECTIVE (EVAC SLIDE)

AFT ACCESSORY COMPARTMENT SLIDE PACK GAUGE NOT READABLE. REMOVED AND REPLACED TAIL CONE SLIDE IAW BOEING 717 AMM 25-61.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE SEAT 25-31 FED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY AND EMERGENCY BATTERY ASSEMBLY IAW BOEING AMM 717 33-51 PANEL LOCATION 222FR ABOVE ROW 24FED OVERHEAD BIN.

Part: LANYARD — BROKEN (EVAC SLIDE)

R1 DOOR EVAC SLIDE LANYARD BROKEN. REMOVED AND REPLACED R1 DOOR EVAC SLIDE LANYARD REF MM 25-61-01 AWI.

Part: LIGHT — INOPERATIVE (CABIN)

OVERHEAD EXIT LIGHT INOPERATIVE. REPLACED BULB. OPS CHECK GOOD. REF 33-10 AMM.

Part: PIN — LOOSE (EVAC SLIDE)

L1 SLIDE PINS ABOUT TO COME OUT. REMOVED AND REPLACED L-1 DOOR ESCAPE SLIDE, REF 25-61-01 AMM.

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 AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2989.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB HAS CORROSION. INSTALLED PERMANENT REPAIR AT AFT CARGO DOOR JAMB LOWER PAN SPLICE REPAIR AS PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: SKIN — DAMAGED (FUSELAGE)

FOUND LIGHTNING STRIKE AT FUSELAGE STA 370 APPROX STR 20L. INSTALLED EXTERNAL REPAIR DOUBLER WITH SKIN TRIMMED OUT OVER A LONGERON, IAW BOEING DWG 09530002.

Part: SKIN — DENTED (BS 229.9)

TWO DENTS AT FUSELAGE STA 229.9 ABOVE LONGERON 18 LEFT. INSTALLED FLUSH SKIN REPAIR PER SRM 53-00-01 FIG 201.

Part: NOSE BULLET — FAILED (RT ENGINE)

AT FL 300 IN LIGHT ICING RIGHT ENGINE PRODUCES HIGH VIB N1 (6.8) USED QRH HIGH ENG VIB PROCEDURE TRIED 4 TIMES AND AFTER LEAVING ICING, N1 VIBE DID NOT GO AWAY. F/A INFORMED ME THEY FELT UNUSUAL VIBRATIONS IN GALLEY. SHUT ENGINE DOWN AT 280 AND LANDED IN MEM. CORRECTIVE ACTION: PERFORMED GENERAL VISUAL INSPECTION OF RIGHT ENGINE INLET & EXHAUST NO DEFECT NOTED. INSPECTED MASTER MAGNETIC CHIP DETECTOR NO DEFECT FOUND AMM 72-00. INSPECTED NOSE CONE ASSEMBLY FOUND SEAL LOOSE UNSECURED. REMOVED AND REPLACED NOSE CONE ASSEMBLY PER AMM 72-38, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

UPON SERVICE CHECK, (ONE) EMERGENCY LIGHT BULB IN COCKPIT FAILED TO ILLUMINATE UPON TEST. RELAMPED, NOW BOTH BULBS OUT. TRIED ANOTHER BATTERY PACK, NO CHANGE. NOW (2) BATTERY PACKS INOPERATIVE. RELAMPED, BOTH BULBS (2 MC316) OPS CHECK GOOD WITH A KNOWN GOOD BATTERY PACK. INSTALLED BOTH BAD PACKS ON AT FORWARD GALLEY OUTBOARD WALL, OTHER AT FORWARD AISLE CEILING, OPS CHECK GOOD.