N970AT

Part: BRACE — DAMAGED (ZONE 600) · airframe 60,799 hrs · 43,763 cycles

PER DAL ENGINEERING REQUEST: PERFORM INSPECTIONS ON REAR SPAR AT RT WING. LOWER FLAP BRACE DOUBLER AT STA XRS 164 ON LOWER SURFACE AND REAR SPAR OF RH WING WERE REPAIRED PER PRI 626006-14 (1177079)

Part: DOUBLER — CRACKED (ZONE 500) · airframe 60,770 hrs · 43,741 cycles

CRACK ON DOUBLER BTW STA: XRS164 AND 150.450 AT LT WING. LOWER SURFACE OF LT WING WAS REPAIRED PER ER/A 626343-14AD (1165171)

Part: REPAIR — CRACKED (ZONE 500) · airframe 60,770 hrs · 43,741 cycles

LEFT WING, LOWER SURFACE, LOWER FLAP BRACE DOUBLER AT XRS 164 HAS A CRACK IN TIME LIMITED REPAIR. REPAIRED LOWER WING SKIN AND SPAR PER ERA 626343-14AD (1158212).

Part: SKIN — DENTED (ZONE 100) · airframe 60,766 hrs · 43,739 cycles

DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R AT CTR LOWER FUSELAGE. SUMMARY OF NRC 00025: DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R WERE REPAIRED PER ER/A 625374-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-625374 ADDED FOR AC 9532. (LP #0900728)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,713 hrs · 41,885 cycles

ON SERVICE CHECK THE EMERGENCY EXIT SIGN ABOVE THE L1 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-235 PER B717 AMM 33-51. LIGHT OPERATION NOW CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5307990)

Part: WINDOW — MISSING (SEAT 17A) · airframe 58,936 hrs · 42,061 cycles

17A OUTER GLASS WINDOW MISSING ON POST FLIGHT INSPECTION. REPLACED OUTER PANE AT SEAT 17A PER B717 AMM 56-20. NO LEAKS A/C OK FOR SVC. (LP #5307957)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT AFT CARGO DOOR. SUMMARY OF NRC-00071: PAN ON 3 AREAS AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 608442-14, REV ORIGINAL, SECTION I AND PRI 608442-4, REV 1. (LP #2763196)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

IN REF TO CARD AD A.A. 5530-01048-03: PERFORM PERMANENT REPAIR (VERTICAL STABILIZER SPLICE BAND). SUMMARY OF NRC-00504: 48 HOLES OF VERTICAL STABILIZER LEADING EDGE STA ZFS=52.267. WERE MEASURED AND 26 HOLES OF 1/4" DIAMETER AND 5 HOLES OF 3/16" DIAMETER WERE FOUND OUT OF LIMITS. THEREFORE, THESE HOLES WERE REAMED AND BUSHINGS WERE FABRICATED AND INSTALLED IN ACCORDING WITH B717-200 SRM 55-30-01-2R, REPAIR 6. DUE TO ARE ONLY ALLOWED 24 HOLES, IT WAS NECESSARY TO MAKE A REPAIR. REPAIR DOUBLER WAS FABRICATED PER SERVICE GENERAL REPAIR DRAWING SG95550001 REV B AND INSTALLED PER B717-200 SRM 55-30-01-2R, REPAIR 7, AND AD 5530-01048-03. PERFORM DVI INITIAL EACH 4400 CYCLES AND REPETITVE 4400 CYCLES PER B717 SRM 55-30-01-2R-7 PAR 5. A. (LP #2760596)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

DURING TEST OF EMERGENCY LIGHTS, THE OVERWING LIGHTS STAY ON WITH THE SWITCH AT THE FORWARD ATTENDANT PANEL, IN THE OFF POSITION. SUMMARY OF NRC 00565: THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717-200 AMM 33-51-06. TEST OK. (LP #2759937)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON FRAME CLIP STA Y=1028 AFT CARGO. SUMMARY OF NRC 00566: CORROSION LEVEL 2. FRAME CLIP STA Y=1028 AFT CARGO WAS REPLACED PER B717-200 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND SRM 51-41-05-0G PAR 8 AND 51-41-02-0G. ALSO WAS FABRICATED PER DWG 9912243-219 REV. JS. (LP #2759564)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CUT ON LANYARD ASSY CABLE OF DOOR 1 LEFT ESCAPE SLIDE (L1). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00568: LANYARD ASSY CABLE OF DOOR 1 LEFT ESCAPE SLIDE WAS REPLACED PER B717-200 AIPC 25-61-01-01 ITEM 95. (LP #2758347)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

ELONGATED HOLES ON CARGO TRACK BTW STA Y408 TO Y427, LONGERONS 27L AND 28L AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00200: CARGO TRACK BTW STA Y408 TO Y427, LONGERONS 27L AND 28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 4 REPAIR 4. (LP #2753643)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00489: LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER ER/A 607622-14 REV. ORIGINAL SECTION I PERMANENT REPAIR AND ER/A 607622-14 REV. ORIGINAL PRI REV, 2. PART A. ASSOCIATED ER/A 14-607622 ADDED FOR AC 9532. (LP #2750530)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON LONGERON END RH L24 APROX STA Y=1002 OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00256: CORROSION LEVEL 2. LONGERON END RH L24 APROX STA Y=1002 OF AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR. 8. (LP #2745776)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE, IN REFERENCE TO LP 1614671 AND LP 1614671. SUMMARY OF NRC 00535: FUSELAGE EXTERNAL SKIN BTW STA Y=229 TO 237 AND L-17L TO L-18L WAS PERMANENT REPAIRED PER B717-200 SRM 53-10-01-2R REPAIR 10, FIG. 202 SHEET 1. CLASS 1. PERFORM A REPETITIVE GVI EVERY 8,000 CYCLES PER B717 SRM 53-10-01-2R PROCEDURE 10, STEP 8. A. TABLE 202. MAINTENANCE REQUIREMENTS - CLASS I REPAIRS. (LP #2742176)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS (3 EA) ON FWD PAN FROM BEAM #1 AND BEAM #4 OF FWD CARGO DOOR. ALSO CRACK (1 EA) ON UPPER PAN CLOSE OF AFT HINGE. SUMMARY OF NRC 00093: CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS (3 EA) ON FWD PAN FROM BEAM #1 AND BEAM #4 OF FWD CARGO DOOR. ALSO CRACK (1 EA) ON UPPER PAN CLOSE OF AFT HINGE.WERE REPAIRED PER B-717-200 PER SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIG 201. (LP #2741999)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE. SUMMARY OF NRC 00525: DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 229 AND L-17L TO L-18L AT FUSELAGE WAS ATTENDENTED WITH LOG 1614618, 1614633, & 1614629 AND FOUND WITHIN ALLOWABLE LIMITS AND EXTERNAL FUSELAGE SKIN BTW STA Y=229 TO 237 AND L-17L TO L-18L PERMANENT REPAIR WAS PERFORMED PER B717-200 SRM 53-10-01-2R REPAIR 10 FIG.202 SHEET 1. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. IN REFERENCE TO LP 1614671. (LP #2740928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

DURING ATTENTION OF NRC 00399, FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FOUND CORRODED OUT OF LIMITS. SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FABRICATED AND REPLACED PER B717-200 SRM 51-30-07-0G FIG 9, 51-41-02-0G, AND 51-41-05 -0G. (LP #2737932)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR. SUMMARY OF NRC 00397: CORROSION LEVEL 2. FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G AND WAS FABRICATED PER DWG 5910085-15 REV. DJ. (LP #2737612)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN. SUMMARY OF NRC 00402: CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN WAS REPAIRED PER ER/A 607699-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607699-14 REV 0. ASSOCIATED ER/A 14-607699 ADDED FOR AC 9532. (LP #2736118)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN. SUMMARY OF NRC 00299: CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN WAS REPAIRED PER ER/A 607681-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607681-14 REV 0. ASSOCIATED ER/A 14-607681 ADDED FOR AC 9532. (LP #2735995)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON MEMBRANE FROM STA Y=150 TO Y=218 AND -X=47 TO -X=60 AT PAX CABIN (CPAX). SUMMARY OF NRC 00389: CORROSION LEVEL 2. MEMBRANE FROM STA Y=150 TO Y=218 AND -X=47 TO -X=60 AT PAX CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 FIG. 201. (LP #2731857)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1. SUMMARY OF NRC 00400; CORROSION LEVEL 2. FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1 WAS FABRICATED PER DWG 5910085 REV DJ AND REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2732197)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON UPPER MEMBRANE FROM STA Y=150 TO Y=170 AND -X=47 TO -X=60 AT PASSENGER CABIN. SUMMARY OF NRC 00528: CORROSION LEVEL 2. WEB FROM STA Y=150 TO Y=170 AND -X=47 TO -X=60 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G AND WAS FABRICATED PER DWG 9936534-179 REV BW. (LP #2728025)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

AD. CRACK WAS FOUND ON RH OVERWING FRAME, LENGTH=0.600 IN IN REF TASK CARD 5310-01436-01D JOB #084-0004 STEP 7. SUMMARY OF NRC 00322: OVERWING FRAME RH LENGTH=0.600 IN. IN REF TASK CARD 5310-01436-01D JOB #084-0004 STEP 7 WAS REPLACED PER B717-200 TASK CARD 5310-01436-03B JOB 151-0002 STEP 9. ASSOCIATED AA 5310-01436 ADDED FOR AC 9532. (LP #2724095)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

REWRITE. SECONDARY NRC IN REF NRC 311: CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=427 AT PAX CABIN. SUMMARY OF NRC 00525: CORROSION LEVEL 2. REPAIR DOUBLER WAS FABRICATED AND REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR. 5B (9), FIG: 211, GENERAL NOTES (SHEET 7), B717-200 SRM 51-41-02-0G. (LP #2723052)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,386 hrs · 39,897 cycles

CORROSION ON FWD FACE BELOW FLOOR BULKHEAD RBL 20 AND LBL 20 STA 1053 AT PAX CABIN. SUMMARY OF NRC 00429: CORROSION LEVEL 2. GUSSETS ON FWD FACE BELOW FLOOR BULKHEAD RBL 20 AND LBL 20 STA 1053 AT PAX CABIN WERE REPLACED PER DWG 3925389 ITEM 1 & 2 AND B717-200 SRM 51-41-05-0G PAR 8(A). (LP #2721687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN. SUMMARY OF NRC 00419: DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4. (LP #2718821)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655, LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00287: CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655 LONGERONS AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG.203 AND CUSP WEB MEMBRANE STA Y655 LONGERONS 18L WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG.205. (LP #2715292)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

CRACK ON INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00291: INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #2710430)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00427: FASTENERS HOLES COUNTER SINK AND DIAMETER ON LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE MEASURED AND FOUND WHITHIN LIMITS PER SERVICE GENERAL DRAWING SG95550001. TOOL USED: VERNIER DIGITAL P/N:500- 196-30 S/N:A22238374 D/D: 15/SEP/23 IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". ASSOCIATED AA 5530-01048 ADDED FOR AC 9532. (LP #2702866)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,386 hrs · 39,897 cycles

SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00428: FASTENERS HOLES COUNTER SINK AND DIAMETER ON RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). WERE MEASURED AND FOUND WHITHIN LIMITS PER SERVICE GENERAL DRAWING SG95550001. TOOL USED: VERNIER DIGITAL P/N:500- 196-30 S/N:A22238374 D/D: 15/SEP/23 IN REF AMDS 5530-01048-02: " AA 5530-01048" AND "AD 2018-10-08". ASSOCIATED AA 5530-01048 ADDED FOR AC 9532. (LP #2703734)

Part: NONE — NONE · airframe 56,243 hrs · 39,784 cycles

FOUND LOWER AFT CORNER OF L1 DOOR DAMAGED AFTER AIRCRAFT ARRIVAL. INSPECTED DAMAGE AREA. REMOVED REQ FASTENERS AND CUT OUT DAMAGE PER B717 SRM 52-10-01-2R-1. PREFORMED DAMAGE CONTAINMENT REF NDT SPM 06.10.01.001 PROCEDURE 1 NO DEFECTS AND OPEN HOLE REF NDTSPM 06.10.01.003 PROCEDURE 3 NO DEFECTS NOTED. DELTA QC5399 FABBED REPAIR PARTS PER B717 SRM 52-10-01-2R-1. TREATED & PRIMED PER B717 52-10. INSTALLED REPAIR PER B717 SRM 52-10-01- 2R-1. RII COMPLETED DELTA QC 1988. (LP #9178660)

Part: NONE — NONE · airframe 54,777 hrs · 38,468 cycles

THE EMERGENCY LIGHTS AT LOCATIONS POWERED BY B5-123 BATTERY PACK ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51, AT THE B5-123 LOCATION. THE EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD. (LP #9217075)

Part: LIGHT — INOPERATIVE · airframe 54,401 hrs · 38,109 cycles

THE AFT OVERWING EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY TRAY FOR EXIT LIGHT POSITION B5-230 IAW B717 AMM 33-51-00. OPERATIONAL CHECK WAS GOOD. (LP #6884529)

Part: NONE — NONE · corrosion level 2 · airframe 54,401 hrs · 38,109 cycles

CORROSION UPPER WING SURFACE AT STA 324 & STR 5 (RIGHT WING). BLENDED CORROSION AT STA 324 STR 5 RH WING UPPER SURFACE PER B717 SRM 51-10-04. C/W HFEC INSPECTION PER ERA 598953- 14 REV 0. NO INDICATIONS NOTED. C/W UT REMAINING THICKNESS CHECK PER ERA 598953-14 REV 0. ACCOMPLISHED SECTION 1 TIME-LIMITED REPAIR ERA 598953-14. ASSOCIATED ER/A 14-598953 ADDED FOR AC 9532. (LP #2213974)

Part: UNKNOWN — UNKNOWN · airframe 54,231 hrs · 37,958 cycles

THE EMERGENCY EXIT SIGN ABOVE THE FWD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE #2 EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 35-51. OPERATIONAL CHECK WAS GOOD. (LP #8250120)

Part: NONE — NONE · airframe 54,203 hrs · 37,932 cycles

FLIGHT CREW DECLARED AN EMERGENCY DUE TO A REPORT OF A SEPERATED TIRE. THE AIRCRAFT MADE A NORMAL SAFE LANDING AND UN-EVENTFUL TAXI AT ATL. MAINTENANCE INSPECTED ALL TIRE/WHEEL ASSEMBLIES PER B717 AMM 32-41. NO DAMAGE WAS FOUND AND EVERYTHING WAS IN GOOD CONDITION. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #8436994)

Part: LENS — DETACHED (EXIT SIGN) · airframe 52,557 hrs · 36,474 cycles

THE FORWARD EXIT SIGN COVER FELL OF ON LANDING AND COULD NOT BE FOUND. LATER, MAINTENANCE REINSTALLED THE EMERGENCY EXIT COVER. OPERATIONAL CHECK WAS OK. EMERGENCY LIGHTS OPERATE OK PER B717-AMM 33-50. (LP #7568382)

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 52,252 hrs · 36,214 cycles

THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK, B5-125, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7603721)

Part: NONE — NONE (NONE) · airframe 55,528 hrs · 39,143 cycles

DAMAGE TOLERANCE EVALUATION REQUIRED FOR ERA 590529-14. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (23 MAR 2023). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. SEE ERA 590529-14 REV. ORIG. ASSOCIATED ER/A 14-590529 ADDED FOR AC 9532. ERA 590529-14 REV A IS CURRENT, NEW LP 2477061 CREATED TO TRACK DTA, THIS LP MAY BE CLOSED. TERMINATED LOG PER LINE 4 COMMENTS. REMOVED MONITOR INSP PER ALERT 01NOV22 AND LOG COMMENTS. (LP #1762947)

Part: HINGE — EXCESS PLAY (LT WING TE FLAP) · airframe 51,978 hrs · 35,998 cycles

THE LT O/B FLAP HINGE HAS EXCESSIVE PLAY AT HINGE BOLT. DEFERRED FOR SDR REPORTING. NRC 331: REPAIRED PER PRI 590529-14 REV 0,1,2,3,&4 AND ER/A 590529-14 REV ORIG. (LP #1761231)

Part: RING — DETACHED (R1 DOOR SLIDE) · airframe 51,978 hrs · 35,998 cycles

THE R1 SLIDE PACK MANUAL DEPLOYMENT RING IS NOT ATTACHED TO THE CABLE. MAINTENANCE REPLACED THE R-1 DOOR SLIDE REF ROUTINE TASK CARD 2561-9005. (LP #1760202)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 51,978 hrs · 35,998 cycles

CORROSION AT MULTIPLE SPOTS AFT CARGO DOOR CUT OUT. (MARKED) PER NRC 00173 001-0371:5230-2002/002, MAINTENANCE APPLIED TOP COAT OF POLY. TASK COMPLETE PER B717 SRM 53-20-15-2R-7. (LP #1757922)

Part: FORMER — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,978 hrs · 35,998 cycles

FORMER AT FS 889 CORRODED AT BL0. PER NRC 001-0291:2550-2003/018 00336 TASK COMPLETE. REPLACE FORMER PER DWG #9923486 AND REF B717 SRM 53-20- 07-2R PROCEDURE 3. (LP #1757932)

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 52,022 hrs · 36,035 cycles

RT MLG TRUNNION FITTING ATTACH LUG FOR FIXED SIDE STRUT AFT FACE PITTED AND CORRODED. NRC 005-0001:08-5740-9- 0052/002 00009: REPAIRED PER PRI 590053-14 REV 0, 1, AND 2 AND ER/A 590053-14 REV ORIGINAL. (LP #1733182)

Part: TRUNNION — GOUGED (LT MLG) · airframe 52,022 hrs · 36,035 cycles

LMLG TRUNNION FITTING FIXED SIDE BRACE ATTACH LUG BORE HAS STRAIGHT LINE GOUGE FROM FRONT TO BACK AT BOTTOM OF BORE. NRC 006-0001:08-5740-9- 0051/005 00020 REWORKED FITTING IAW B717 OHM 57-40-1, PRI 590055-14, AND ER/A 590055-14 REV ORIGINAL. (LP #1729599)

Part: PANEL — MISSING (NACELLE) · airframe 50,958 hrs · 35,192 cycles

DURING B-CHECK, MAINTENANCE FOUND THAT PANEL 330KB WAS MISSING. MAINTENANCE INSTALLED A NEW PANEL (MPN 5910412-151) IAW AMM 06-33.

Part: SKIN — PULLED (FWD CARGO DOOR) · airframe 48,136 hrs · 33,198 cycles

METAL PULLED AWAY FROM FWD CARGO DOOR FWD EDGE DOOR CUTOUT. MID SPAN APPROX 7" LONG X .027 WIDE. IN ACCORDANCE WITH R/I REFORMED SKIN AND REMOVED FASTENERS PERFORMED DVI AND FOUND NO FURTHER DAMAGE TO SEAL DEPRESSOR OR UNDERLYING STRUCTURE. ACCOMPLISHED SERFACE HFEC . NO CRACK AND HFEC OPEN HOLE PER RI 573347-14. SEALED AND RE INSTALLED FASTENERS. COMPLIED WITH RI 573347-14 REV ORIG. ER/A 573347-14 REV ORIG PERMANENT REPAIR INSTRUCTIN MUST BE ACCOMPLISHED PRIER TO CLOSING THIS LOG. REPETITIVE INSPECTION EVERY 500 HOURS AND TERMINATING AT C CHECK. (LP4712632)

Part: LIGHT — UNSECURE (CABIN) · airframe 46,428 hrs · 31,973 cycles

SEAT MOUNTED EMERGENCY LIGHTING IS DAMAGED / INOPERATIVE AT 26C. MAINTENANCE RESECURED THE EMERGENCY LIGHT PER AMM 33-51. SYSTEM IS NOW OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (R1 DOOR) · airframe 51,978 hrs · 35,998 cycles

A/C DAMAGED 22 IN AFT OF R-1 DOOR. PREFORMED TIME LIMITED REPAIR PER B717 SRM 53-02-01 PARA 5.A(3) REPAIR 1. TEMP REPAIR IS LOCATED AT STA 208 STR 16R, VISUAL INSPECTED PER B717 SRM 53-02-01, NO DEFECTS FOUND, O.K. TO CONTINUE ON QC DEFERRAL. REMOVED EXTERNAL DOUBLER AND CLEANED SKIN PER B717 SRM 51-40-02. BLENDED OUT DAMAGE PER SRM 53-02-01-2R C/W HFEC REQ PRE B717 SRM 51-02-01-2R. FABRICATED AND INSTALLED INTERNAL DOUBLER AND EXTERNAL DOUBLER PER B717 SRM 53-02-01-2R FIG 202. (LP #3115314)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 44,007 hrs · 30,252 cycles

EMERGENCY LIGHT COVER CAME OFF FROM CEILING. SECURED EMERGENCY LIGHT COVER IAW AMM 33-51. CHECKED NORMAL.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

DAMAGE LOWER ANGLE AT LT CUSP WEB BETWEEN STA Y=889 AND STA Y=908 AND STA X=54 AND X=60 AT PASSENGER CABIN. DUCT OF ANTI-ICE SYS WAS REMOVED IAW AMM 30-10-07, PAGE BLOCK 401. SPLICE WAS REMOVED IAW SRM 51-41-05, SPLICE WAS FABRICATED IAW SRM 53-20-01, FIG 1, NEW ANGLE WAS INSTALLED IAW SRM 51-41-05, DUCT OF ANTI-ICE SYS WAS INSTALLED IAW AMM 30-10-07, PAGE 401. LEAK TEST WAS PERFORMED IAW AMM 30-10-00, AND NO LEAK WAS FOUND.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 42,616 hrs · 29,225 cycles

CRACK ON UPPER OUTER RT CUTOUT OF RT WINDSHIELD, SETTLEMENT AREA, AYP, SERIAL 00620. WINDSHIELD RETAINER WAS REPLACED IAW AMM 20-60-01 914-801, SRM 51-41-02, SRM 51-40-08, DWG 9966436, REV ORIGINAL, DWG NR 5911356, REV DJ.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACKED FRAME STA 1225 CANT AND 7 HRS POSITION AT AFT ACCESSORY COMPARTMENT, SM, SN 00519. HFEC WAS ACCOMPLISHED, 01 CRACK WERE FOUND OF 1.65" IAW MD NDT SPM 06-10-01.001. VISUAL INSPECTION WAS PERFORMED NOT DISCREPANCIES WERE FOUND HFEC INSPECTION WAS ACCOMPLISHED ON TRIM OUT AREA, NO CRACKS WERE FOUND IAW ETI-17-16-116, STEP 4 EQUIPMENT USED ON STEP 5. REPAIR PARTS WERE INSTALLED ER/A 550288-14, REV ORIGINAL.

Part: STRUCTURE — CRACKED (RT WING) · airframe 42,616 hrs · 29,225 cycles

CRACK ON SETTLEMENT AREA HOLES OF T/E FIXED STA XW=530 AT RT WING. T/E FIXED STA XW=530 AT RT WING WAS REPAIRED IAW ETI-17-16-122 REV 1 AND ER/A 550301-14, REV ORIGINAL, ASSOCIATED ER/A 00-550301.

Part: CARGO TRACK — CORRODED (BS 820-1022) · corrosion level 2 · airframe 42,616 hrs · 29,225 cycles

CORROSION ON LT CARGO TRACK BS 820 - 1022 BETWEEN LONGERONS 27 AND 28L AT AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.

Part: SKIN — CRACKED (BS 1133) · airframe 42,616 hrs · 29,225 cycles

CRACK AT FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2 AND 3R. REPAIRED IAW ETI-17-16-115 REV. 2 AND ER/A 549302-14AD REV. ORIGINAL.

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 42,616 hrs · 29,225 cycles

CRACKED FWD CHANNEL ON RIGHT MLG WW CUTOUT DOOR AREA. REPLACED THE CHANNEL IAW SRM 51-41-01, 51-41-02, 51-41-05, 51-40-08, 51-10-04 PARAGRAPH 15, 21, AND AMM 20-50-02-917-801.

Part: DOOR FRAME — CRACKED (NLG) · airframe 42,616 hrs · 29,225 cycles

CRACKED LEFT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14 FIG 201.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 42,616 hrs · 29,225 cycles

LIGHTNING STRIKE AT RT GEARED ELEVATOR TAB (BROKEN FIBERS). REPAIRED IAW SRM 51-70-09 REP 5, REMOVED AND INSTALLED IAW AMM 27-31-05.

Part: FLOOR PANEL — CORRODED · airframe 42,616 hrs · 29,225 cycles

CORROSION, CRACKED, LOOSE FASTENERS ON FLOOR PANEL. CORROSION REMOVED IAW SRM 51-10-04 PAR 26

Part: CHANNEL — CRACKED (BS 47) · airframe 42,616 hrs · 29,225 cycles

CRACKED RT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE CHANNEL WAS REPAIRED IAW SRM 53-10-14 FIG 201.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,616 hrs · 29,225 cycles

CORROSION ON LONGERON 30 BETWEEN STA Y=994 AND Y=905 AT AFT CARGO COMPARTMENT. LONGERON 30, FRAME CLIPS, AND SPLICES BETWEEN STA Y=897 AND Y=1012 WERE REMOVED IAW SRM 51-41-05, 51-41-02, AND 53-20-05, REPAIR 1, FIG 201. NEW LONGERON 30 BETWEEN STA Y=897 AND Y=1012 WAS ADJUSTED, DRILLED, PAINTED, AND INSTALLED IAW SRM 51-40-08 AND 53-20-, REPAIR 1, FIG 201. NEW SPLICE REPAIR AND STRAPS WERE INSTALLED IAW SRM 53-20-05, REP 1, FIG 201. FRAME CLIPS AND SPLICES WERE INSTALLED BETWEEN STA Y=897 AND Y=1012 IAW SRM 51-41-05, 51-41-02, 51-41-01.

Part: ACCESS PANEL — CORRODED (WING) · airframe 42,616 hrs · 29,225 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PLATE 620CB, NRC 00624. CORROSION WAS REMOVED IAW SRM 51-10-04, PAR 26. COUNTERSINK AREAS WERE MEASURED MAXIMUM COUNTERSINK DIAMETER, ALLOWABLE DOOR, PN ARB0975, IS 0.532" MAXIMUM DIAMETER MEASURED IS 0.610. THEREFORE IS OUT OF SERVICE DUE TO EXCESSIVE DAMAGE IN 3 AREAS. COUNTERSINK ADJACENT, THEREFORE IS OUT OF LIMITS IAW SRM 57-10-01 CONDITION II AND FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW IPC 57-23-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACKED RT NLG DOOR SUPPORT STA 64, SM, SN 00590. SUPPORT WAS REPLACED IAW SRM 51-41-05 AND DWG 9910088, REV LP 2675427.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON INTERCOSTAL STA Y=1076 X=-19 Z=5 AT AFT CABIN PRESSURE BULKHEAD. INTERCOSTAL WAS REPLACED IAW DWG 5917579, REV, ED ITEM -325, SRM 51-41-05 AND SRM 51-41-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON FRAMES STA Y=674 AND Y=696 AT RT KEELBEAM AREA, SM NRC 308. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES, STA Y=674 AND Y=696 AT RT KEELBEAM AREA. NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW NDT SPM 06-10-01.001 EQUIPMENT: MENTOR, CN 1137 EXP: 24JUN17.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACKED FRAME 715 BETWEEN LONGERON 27/28 AT KEELBEAM AREA, SM, NRC 00552. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02, 51-41-05, AND 51-10-04, PAR 15,21,26 AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME STA Y=715 BETWEEN LONGERON 27/28 AT KEEL BEAM AREA. NO CRACKS WERE FOUND AFTER DAMAGE, REMOVED IAW NDT SPM 06-10-01.001 EQUIPMENT: MENTOR, CN 1137, EXP: 24JUN17.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON FRAMES STA Y=674 AND Y=696 AT LT KEELBEAM AREA, SM NRC 00306. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES STA Y=674 AND Y=696 AT LEFT KEELBEAM AREA. NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW NDT SPM 06-10-01.001 EQUIPMENT: MENTOR, CN 1137, EXP: 24JUN17.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON GENERATION FLOOR CHANNEL NR 221, TF, SM, NRC 00226. CRACK WAS STOP DRILLED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-41-02, SRM 51-20-09, AND SRM 53-20-50, REPAIR 5, FIG 202. HFEC INSPECTION WAS PERFORMED AT END OF CRACK. NO CRACKS WERE FOUND BEYOND IAW NDT SPM 06-10-01.001 EQUIPMENT.

Part: WEB — WORN (VENTRAL DOOR) · airframe 42,616 hrs · 29,225 cycles

WEAR ON LOWER WEB LT SIDE INTERNAL STRUCTURE AT AFT CABIN BULKHEAD VENTRAL DOOR, SN 594, DUE TO EXCESSIVE DAMAGE, WEAR ON LOWER WEB LT SIDE INTERNAL WILL BE REPAIRED. RETAINERS WERE REMOVED IAW SRM 51-41-01, LOWER WEB ON LT SIDE. INTERNAL STRUCTURE WAS MEASURED WITH ULTRA-SONIC TEST. ORIGINAL THICKNESS OF THE, .090" AND MINIMUM REMAINING THICKNESS OF .065", LENGTH=2.000", AND WIDTH=.250". THEREFORE OUT OF LIMITS IAW SRM 52-10-02. REPAIR DOUBLER WAS FABRICATED AND HEAT TREATED IAW SRM 52-10-02, REP 15 AND 51-32-01. DOUBLER WAS INSTALLED IAW SRM 51-41-05 AND 51-41-02. RETAINERS WERE INSTALLED IAW SRM 51-41-01.

Part: CUSP WEB — CORRODED (BS 911-913) · corrosion level 2 · airframe 42,843 hrs · 29,386 cycles

EXCESIVE CORROSION ON CUSP WEB BS 911-913 AND X -54 TO -60 . DAMAGE WAS REMOVED AND A REPAIR WAS FABRICATED IAW SRM 53-00-55 RAPAIR 4 FIG 216.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 42,616 hrs · 29,225 cycles

ELONGATED HOLE ON FUEL ACCESS PLATE 520LB, SN 575. HOLE WAS REWORKED IAW SRM 57-10-01, PAR 5, CONDITION II, 3. HOLE AND COUNTERSINK WERE MEASURED WITH ID 0.3435" AND COUNTERSINK 0.613" THEREFORE WITHIN LIMITS OF REPAIR IAW SRM 57-10-01, PAR 5 CONDITION II. BUSHING WAS FABRICATED IAW SRM 57-10-01, PAR 5 CONDITION II WITH OD 0.345" AND COUNTERSINK 0.508". REWORK AREA WAS TREATED IAW SRM 51-10-04, PAR 21 NEW BUSHING REPAIRS WERE INSTALLED IAW SOPM 20-10-7 PAR 5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,616 hrs · 29,225 cycles

EXCESSIVE CORROSION ON CUSP WEB BETWEEN STA 478-STA 481 BETWEEN X-54--60 ON REF SN CARD 300, SN 00548. DAMAGE WAS REMOVED IAW SRM 53-00-55, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT, SPM 06-10-01.001 ALONG TRIM LINE AND NO CRACKS WERE FOUND. REPAIR PARTS WAS FABRICATED AND INSTALLED IAW SRM 53-00-55 AND 51-41-05.

Part: ANGLE — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 42,616 hrs · 29,225 cycles

DAMAGED ON LOWER ANGLE AT RT CUSP WEB BETWEEN STA Y=579 AND STA Y=598 AND X=-54 AND X=-60 AT PASSENGER CAB, SN 00300. SPLICE WAS REMOVED DUE TO EXCESSIVE CORROSION IAW SRM 51-41-05, AND NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-20-01, FIG 51-20-09 AND 51-41-05.

Part: PAN — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON RT RING PAN AFT UPPER CORNER, STA Y= 832 AT CABIN PASSENGER RT SIDE, SN 00206. DAMAGE WAS REMOVED IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=832 CABIN PASSENGER RT SIDE. NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 56-20-02, REPAIR 1, FIG 202, AND SRM 51-41-02 AND 51-41-05.

Part: PAN — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON LT RING PAN FWD LOWER CORNER, STA Y= 598 AND Y= 889 AT CABIN PASSENGER LEFT SIDE, S/N 00207. DAMAGE WAS REMOVED IAW SRM 56-20-02 REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=598 AND 889 AT CABIN PASSENGER LT SIDE. NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 56-20-02, REPAIR 1, FIG 202, AND SRM 51-41-02, AND 51-41-05.

Part: PAN — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK ON RT RING PAN FORWARD UPPER CORNER, STA Y= 636 AND Y= 696 AT CABIN PASSENGER RT SIDE, SN 00203. DAMAGE WAS REMOVED, IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=636 AND 696 AT CABIN PASSENGER RT SIDE, NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 56-20-02, REPAIR 1, FIGURE 202, AND 51-41-02 AND 51-41-05.

Part: BEAM — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE ON STA 389, UPPER EDGE OF BEAM 5, SN 00529. PAN UPPER EDGE ON STA 389 UPPER EDGE OF BEAM 5 WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.100".

Part: BEAM — CRACKED (FUSELAGE) · airframe 42,616 hrs · 29,225 cycles

CRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE STA 408 UP OF BEAM 5 SN 00530. PAN UPPER EDGE ON STA 408 UP OF BEAM 5 WAS REPAIRED SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.400".

Part: FRAME — CRACKED (BS 1474) · airframe 42,616 hrs · 29,225 cycles

CRACKED FRAME BS 1474 AND X -20. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 2, 51-30-2 AND 51-30-5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,582 hrs · 29,198 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FORWARD CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,493 hrs · 26,666 cycles

DURING LINE CHECK, FOUND BULBS OUT IN L1 DOOR EXIT SIGN, RT AFT OVERWING EXIT SIGN AND LT FORWARD OVERWING EXIT SIGN. REPLACED BULBS AND OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,385 hrs · 26,592 cycles

DURING LINE CHECK, THE LEFT NR 1 OVERWING EXIT EMERGENCY SIGN LIGHT WAS INOPERATIVE. THE SIGN WAS REPLACED THE LAMP AND CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,106 hrs · 26,362 cycles

LEFT OVER WING EMERGENCY BATTERY PACK FAILED OPS CK. REPLACED EMERGENCY LIGHT BATTERY PACK PN AD803949-1, SN ON 152426, SN OFF 136813, OPS CHECKED GOOD IAW AMM 33-51-06.

Part: FRAME — CRACKED (BS 674) · airframe 39,106 hrs · 26,361 cycles

DURING FRAME BS 674 LT INSPECTION, NOTED CRACK IN UPPER RADIUS OF THE FRAME TAB, OVER WING FRAME. REPAIRED IAW ER/A 534641-14AD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,406 hrs · 25,774 cycles

DURING LINE CHECK, NOTED COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY B5-123 AND CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,555 hrs · 25,116 cycles

RIGHT AFT OVERWING EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,555 hrs · 25,116 cycles

CATWALK 3RD AFT EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 37,453 hrs · 25,053 cycles

MAIN CABIN FWD CEILING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 218 TO 220. R & R CUSP WEB IAW SRM & DWG.

Part: TRACK — CORRODED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

LEFT FALSE SEAT TRACK CORRODED BETWEEN BS 140 TO 200, LBL 7. R & R TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 256, LBL 16. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 160 TO 200, LBL 44. REPAIRED SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

BLOCK SUPPORT CORRODED AT BS 200, LBL 22. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

INTERCOSTAL CRACKED AT BS 1023, LONGERON 28R. R & R INTERCOSTAL IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 37,453 hrs · 25,053 cycles

L1 DOOR EXIT SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: PANEL — CRACKED (LT WING) · airframe 37,453 hrs · 25,053 cycles

LEFT WING INBD BUTTE DOOR AT FWD WEB PANEL OTBD END CRACKED. REPAIRED PANEL IAW EA.

Part: ANGLE — CRACKED (TE FLAP TRACK) · airframe 37,453 hrs · 25,053 cycles

LEFT WING INBD SIDE OF THE MOST INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,453 hrs · 25,053 cycles

FRAME CORRODED AT BS 1022 LONGERON 30L. R & R FRAME IAW SRM & DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 37,453 hrs · 25,053 cycles

MAIN CABIN NR 1 CEILING PANEL EMER LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 37,105 hrs · 24,839 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. R & R SLIDE IAW MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,892 hrs · 24,715 cycles

FWD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW SIP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,354 hrs · 24,377 cycles

AFT FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW AMM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 36,064 hrs · 24,197 cycles

DIVERSION, CENTER WINDOW ARCED & APPEARS THE OUTER PANE CRACKED. R & R CENTER WINDSHIELD IAW MM.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 35,784 hrs · 24,009 cycles

L1 FLASHLIGHT INDICATOR OUT OF POSITION. REPOSITIONED FLASHLIGHT IAW MM.

Part: LANYARD — DETACHED (R1 DOOR) · airframe 35,377 hrs · 23,751 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD DETACHED. SECURED LANYARD IAW AMM.

Part: GIRT BAR — DETACHED (R1 DOOR) · airframe 35,377 hrs · 23,751 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DETACHED. SECURED GIRT BAR IAW AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 35,350 hrs · 23,732 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 35,204 hrs · 23,644 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE PER M/M.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,860 hrs · 23,436 cycles

FWD F/A FLASHLIGHT INOP. R & R BATTERY IAW MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 33,513 hrs · 22,591 cycles

RIGHT OVERHEAD EMERGENCY EXIT LIGHT INOP AT STA 73. CONNECTED WIRE IAW SWPM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CRACKED AT BS 351, RBL 45.0. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CRACKED AT BS 372, RBL 44.5. REPAIRED CUSP WEB IAW SRM.

Part: CAP — CRACKED (RT HORIZ STAB) · airframe 33,513 hrs · 22,591 cycles

RIGHT HORIZONTAL STABILIZER REAR SPAR BETWEEN I/B TO O/B SIDE, NR 2 AND NR 3 HINGE SUPPORT CAP, COMPOSITE CRACKED. REPAIRED STABILIZER IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

VERTICAL SUPPORT FITTING CRACKED AT BS 757, RBL 44.5. REMOVED AND REPLACED FITTING IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 33,513 hrs · 22,591 cycles

UPPER RIGHT WING CUTOUT FOR FUEL ACCESS PANEL 620DT, MATING SURFACE CORRODED. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 33,513 hrs · 22,591 cycles

CRACKED ANGLE L1 PASSENGER DOOR INTERNAL UPPER BEAM AFT CORNER. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CRACKED AT BS 676, RBL 44.5. REPAIRED CUSP WEB IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 33,513 hrs · 22,591 cycles

UPPER RIGHT WING CUTOUT FOR FUEL PANEL 620FT, MATING SURFACE CORRODED. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CRACKED AT BS 673, LBL 44.5. REPAIRED CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 33,513 hrs · 22,591 cycles

CRACKED ANGLE L1 PASSENGER ENTRY DOOR INTERNAL UPPER BEAM FWD CORNER. REMOVED AND REPLACED DOUBLER IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CORRODED BETWEEN BS 541 TO BS 560, RBL 59. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 446 TO STA 756. REPAIRED CUSP WEB PER SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 221 TF CRACKED AT BS 361, LBL 45.0. REPAIRED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 221 XF CORRODED BETWEEN BS 323 TO BS 360, RBL 45.0. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 222 HF CRACKED. REPAIRED FLOOR PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

CUSP WEB CORRODED BETWEEN BS 446 TO BS 465, RBL 59. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 221SF CORRODED AT BS 278, RBL 45.0. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 222MR CRACKED AT BS 494, RBL 45.0. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FLOOR PANEL 222 NF CORRODED AT BS 610, LBL 45.0. REPAIRED FLOOR PANEL IAW SRM.

Part: RING — CRACKED (CABIN) · airframe 33,513 hrs · 22,591 cycles

PASSENGER WINDOW RING CRACKED AT BS 579, LONGERON 15R. REPAIR WINDOW RING IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

CABIN FLOOR PANEL AGF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222AFF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

LONGERON CRACKED BS 1144, 2R. REMOVED AND REPLACED LONGERON IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222BF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

LONGERON CRACKED BS 1144, 2L. REMOVED AND REPLACED LONGERON IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FRAME CRACKED AT BS 715, LBL 54.5. REMOVED AND REPLACED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222PF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222LF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED. REMOVED AND REPLACED IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL NR 222AVF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222AMF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222ACF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222JF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222FF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 221IF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 2223DF DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FRAME CORRODED AT BS 889, BETWEEN L29L TO L29R. REPAIRED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,513 hrs · 22,591 cycles

MAIN CABIN FLOOR PANEL 222AAF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM.

Part: PAN — CORRODED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

FWD CARGO CUTOUT JAMB PAN CORRODED BETWEEN BS 370 TO BS 427, BETWEEN LONGERON 26R - 28R. REMOVED AND REPLACED PAN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,513 hrs · 22,591 cycles

NLG STRUT DOOR LEFT AFT HINGE CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — DAMAGED (VERTICAL STAB)

BIRD STRIKE ON UPPER VERTICAL STAB L/E. CUT OUT DAMAGED SECTION OF UPPER CAP L/E SKIN AND RIB. ACCOMPLISHED DOUBLER AND FILLER REPAIRS PER EA 17-55-03636IR AND B717 SRM 55-00-00.

Part: STRUCTURE — CORRODED (GALLEY)

COFFEEMAKER COMPARTMENT 102 AND 106, CORROSION. ACCOMPLISHED 102 AND 106 DOUBLER REPAIR PER B717 EA 17-25-03111IR.

Part: DOOR — GOUGED (LT WING)

LEFT WING T/E MID BUTE DOOR I/B END, GOUGED. ACCOMPLISHED MID BUTE DOOR I/B END DOUBLER REPAIR PER EA 17-57-03114IR.

Part: FITTING — WORN (SPOILER)

LEFT WING INBOARD AND OUTBOARD SPOILER PANELS STOP PADS AND FITTINGS, WORN. ACCOMPLISHED STOP PADS AND FITTINGS DOUBLER REPAIR PER B717 SRM 51-41-02 AND TRA 17-57-TR000681.

Part: FASTENER — SHEARED (FUSELAGE)

VERTICAL STABILIZER ATTACH ANGLE HL329-5 HI-LOK FASTENER, STA 1152, LONG 1R, SHEARED. ACCOMPLISHED HL329-5 HI-LOK FASTENER PLUGGED PER EA 17-53-03113IR.

Part: FITTING — SHEARED (FUSELAGE)

SHEAR CLIP O/N 9911840-165 FASTENER, STA 1152, LONG 2L TO 3L, SHEARED. ACCOMPLISHED FASTENER PLUGGED PER EA 17-53-03112IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD AIRSTAIR HANDLE BASE FLOOR SUPPORT, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: LONGERON — CRACKED (NR 1 NACELLE)

NR 1 ENGINE APRON LOWER LONGERON AND UPPER FRAME, CRACKED. ACCOMPLISHED LOWER LONGERON AND UPPER FRAME DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: PANEL — CORRODED (FUSELAGE)

PASSENGER ENTRANCE AREA DOOR JAMB GAP PANEL, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: ATTACH FITTING — CORRODED (FUSELAGE)

GALLEY ENTRANCE FWD AND AFT GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE DOOR JAMB GAP PANEL, STA 200, RBL 54, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 33 TO RBL 46, CRACKED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE DOOR JAMB GAP PANEL, STA 170, RBL 56, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FINGER DOUBLER — CRACKED (FUSELAGE)

CABIN LONGERON FINGER DOUBLER, STA 208, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER DOUBLER FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201.

Part: SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SIDE GRILL SUPPORT, STA 200 TO 210, RBL 56, CORROSION. ACCOMPLISHED FLOOR SIDE GRILL SUPPORT REPLACEMENT PER B717 SRM 51-20-09, B717 SRM 51-40-08 AND B717 SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: ANGLE — MISSING (FUSELAGE)

FWD CARGO DOOR JAMB SPLICE ANGLE, MISSING. ACCOMPLISHED ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, LBL 35, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: MEMBRANE — CRACKED (FUSELAGE)

CABIN FLOOR WEB MEMBRANE SUB FLOOR, STA 218, RBL 46, CRACKED. ACCOMPLISHED FLOOR WEB MEMBRANE SUB FLOOR DOUBLER REPAIR PER B717 DWR SG09530019.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 34, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LIGHT — MISSING (CABIN)

EPL LIGHT BULBS AND CLEAR LENS MISSING AT SEATS 2D, 3D. REPLACED MISSING EPL LENS AT SEAT 2D, 3D, AND BULBS. OPS CHECK GOOD.

Part: COVER — DEFECTIVE (CABIN)

EXIT SIGN LIGHT COVER OVER ROW 1 NEEDS TO BE RE-INSTALLED. INSTALLED, TAPED IN PLACE (LEGIBLE AND WORKING) -- OPEN DEFECT.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

R1 DOOR EMERGENCY SLIDE PRESSURE INDICATOR IN RED ZONE. REMOVED AND REPLACED R1 DOOR SLIDE. OK FOR SERVICE REF 25-61.

Part: COWLING — DAMAGED (LT ENGINE)

LAVATORY CART BACKED INTO AIRPLANE. DAMAGE TO LEFT ENGINE COWLING AND BELLY OF AIRCRAFT. WORK COMPLETE ON AAR WORK ORDER 16623-1000-003 AND 16 EA NON-ROUTINES ON WORK ORDER 16623. SEE LOG PAGE 1505530 ITEM 1 FOR FERRY FLIGHT. C/W PRELIMINARY EA 17-53-02237IR INSTRUCTIONS. TECHNICIAN SIGN OFF- INSPECTOR SIGN OFF.

Part: COWLING — DAMAGED (LT ENGINE)

LAVATORY CART BACKED INTO AIRPLANE. DAMAGE TO LEFT ENGINE COWLING AND BELLY OF AIRCRAFT. WORK COMPLETE ON AAR WORK ORDER 16623-1000-003 AND 16 EA NON-ROUTINES ON WORK ORDER 16623. SEE LOG PAGE 1505530 ITEM 1 FOR FERRY FLIGHT. C/W PRELIMINARY EA 17-53-02237IR INSTRUCTIONS. TECHNICIAN SIGN OFF- INSPECTOR SIGN OFF.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN AT L1 DOOR DAMAGED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS PER B717 SRM 53-10-01 FIG 201.

Part: SKIN — DAMAGED (LT WING)

LEFT WING LEADING EDGE STA 15.136 HAS DEEP GROOVE WORN. REMOVED OLD REPAIR, INSTALLED NEW DOUBLER IAW B717 SRM 57-00-00 FIG 101.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT JAMB CORRODED. REMOVED CORRODED PAN, REPLACED AND INSTALLED SPLICE REPAIR PER B717 SRM 53-20-15.

Part: STRUCTURE — CORRODED (FUSELAGE)

AFT CARGO BILGE AREA CORROSION STA 927 LONG 29L. REMOVED CORRODED MEMBER, REPLACED AND REPAIRED PER B717 SRM 57-40-2 PG 1.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR)

R1 DOOR SLIDE ACCIDENTALLY DEPLOYED. INSTALLED SERVICEABLE R1 DOOR SLIDE PER MM 25-61. P/N OFF D29982-225, S/N OFF 2638, P/N ON D29982-225, S/N ON 2644.

Part: SKIN — GOUGED (BS 522 S28-29)

GOUGE IN LOWER FUSELAGE AT 522 IN BETWEEN LONGERONS 29-28. CUT OUT DAMAGE AREA BETWEEN L29 & L28, FABRICATED REPAIR 2024T3 -063 IAW B717 SRM 53-00-01, TREAT AND PRIME INSTALLED REPAIR ON A/C IAW B717 SRM 53-00-01. REF RES 06-0774 AND RES 06-0073, NO NOTABLE EFFECT ON WEIGHT AND BALANCE.