N989AT

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 60,895 hrs · 43,583 cycles

AIRCRAFT 9527, MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT CABIN. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY PACKS B5-227 AND B5-230 PER B717 AMM 33-51. OPS CHECK GOOD. (LP 6564077)

Part: LIGHT SYS — INOPERATIVE (OVERWING EMERGEN) · airframe 59,660 hrs · 42,545 cycles

DURING SERVICE NOTED THAT THE LH AND RH AFT OVERWING AND RH FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY B5-119 REF B717 AMM 33-51. BOTH AFT OVER WING LIGHTS WORK BUT RH FWD STILL INOPERATIVE. FOUND GROUND LOOSE FOR L2-832. RESECURED GROUND AND LIGHT OPERATION CHECKS GOOD. OK FOR SERVICE. (LP #6593471)

Part: DUCT — TEMP REPAIR (ZONE 400) · airframe 59,705 hrs · 42,578 cycles

CRACK ON RIGHT ENG BYPASS DUCT NEAR PRECOOLER INLET WAS TEMPORARILY REPAIRED. RE-INSPECTION REQUIRED PER ER/A 620571-14 REV ORIGINAL. REFER TO LOG #0580374 FOR PRIOR INSPECTION. SECTION 4 INSPECTION MUST BE ACCOMPLISHED BETWEEN 220 AND 180 FLIGHT CYCLES PER ERA 620571-14 REV ORIGINAL. **REDEFERRED LOG TO QC, ESTAB MON INSP BETWEEN 180-220 CYCLES. MECHANIC: C/W ONE TIME INSP PER ERA 620571-14 REV ORIG SECT IV. NO FURTHER DAMAGE NOTED. OKAY TO CLOSE MONITOR. REFER TO LOG #6593489 FOR MON TRACKING OF SECT V AT 420 CYCLES. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 04DEC24 AND LOG COMMENTS. (LP #9980685)

Part: HINGE — EXCESS PLAY (ZONE 600 FLAP) · airframe 59,201 hrs · 42,207 cycles

FREEPLAY WAS FOUND ON RH WING FLAP OUTBD HINGE AREA. SUMMARY OF NRC 00781: RH WING FLAP OUTBD HINGE WAS REPAIRED PER ER/A 620752-14 REV ORIGINAL AND PRI 620752-14 REV 2 AND WAS INSTALLED PER B717-200 AMM 27-55-03 400-801. ASSOCIATED ER/A 14-620752 ADDED FOR AC 9527. (LP #0562049)

Part: PAN — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

CRACK ON PAN FWD EDGE IN LOWER SIDE AT FWD CARGO COMPARTMENT DOOR. RE-WRITE REASON: TECHNICAL REFERENCE USED DOES NOT APPLY TO FWD CARGO COMPARTMENT. ALSO, AFTER DOUBLERS REMOVED CRACKS WERE FOUND ON PAN BTW BEAM 1 AND 2 AND ELONGATED HOLES ON INNER/OUTER PAN. ALSO, CRACK ON SEAL RETAINER 1 EA. SUMMARY OF NRC 00790: PAN FWD EDGE IN LOWER SIDE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 620631-14 REV ORIGINAL. ASSOCIATED ER/A 00-620631 ADDED FOR AC 9527. (LP #0560588)

Part: PAN — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

CRACK ON AFT PAN WAS FOUND BTW BEAM 1 AND 2 AT AFT CARGO DOOR (REF NRC NBR 00640). SUMMARY OF NRC 00693: AFT INNER PAN BTW BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620224-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620224-14 REV 2. ASSOCIATED ER/A 14-620224 ADDED FOR AC 9527. (LP #0557093)

Part: SKIN — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON SKIN, SHEAR CLIP, AND SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESORY COMPARTMENT (IN REFERENCE TO ERA 95-520358-14 REV ORIGINAL FIGURE 4). SUMMARY OF NRC 00592: SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESORY COMPARTMENT WAS REPAIRED PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II: REPETITIVE INSPECTION, WITHIN 3,000 CYCLES FROM TIME OF REPAIR INSTALLATION FROM 10SEP24, AND REPEAT WITHIN EVERY 3,000 CYCLES THEREAFTER IN REFERENCE TO ER/A 620225-14 REV ORIGINAL SEC II. (LP #0551930)

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

FABRICATED PARTS IN REFERENCE NRC 00592 AND PRI 620225-14 REV 0. MANUFACTURE SHEAR CLIP (AFT ACCESS). CRACK WAS FOUND ON SHEAR CLIP IN REFERENCE NRC 00592: FABRICATE SHEAR CLIP PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV OROGINAL, SECTION I PERMANENT REPAIR. SUMMARY OF NRC 00765: SHEAR CLIP WAS FABRICATED PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND INSTALLED UNDER NRC 00592, LOG PAGE #0551930. ACCOMPLISH SECTION II: REPETITIVE INSPECTION, WITHIN 3,000 CYCLES FROM TIME OF REPAIR INSTALLATION FROM 10SEPT24, AND REPEAT WITHIN EVERY 3,000 CYCLES THEREAFTER PER ERA 620225-14 REV ORIGINAL UNDER LOG PAGE #0551515. ASSOCIATED ER/A 14-620225 ADDED FOR AC 9527. (LP #0553037)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00754: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0542411)

Part: ACCESS PANEL — CORRODED (ZOEN 300) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

CORROSION INSIDE HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX. SUMMARY OF NRC 00399: CORROSION LEVEL 2. HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX WAS REPAIRED PER ER/A 620168-14 REV ORIGINAL, SECTION 1: PERMANENT REPAIR. ASSOCIATED ER/A 14-620168 ADDED FOR AC 9527. (LP #0541568)

Part: BARREL NUT — CORRODED (ZONE 300) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

CORROSION IN BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER IN REF NRC 00400. SUMMARY OF NRC 00649: CORROSION LEVEL 2. BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 620136-14 REV 3 & ER/A 620136-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-620136 ADDED FOR AC 9527. (LP #0541553)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00516: CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN WERE FABRCATED AND REPAIRED PER DWG 9910151 REV CH, B717 SRM 51-70-10-2R PROCEDURE 2 FIGURE 201 AND 53-00-00-2R-4 FIG 218. (LP #0535302)

Part: FORMER — CRACKED (ZONE 800) · airframe 59,201 hrs · 42,207 cycles

CRACK FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR. L1. SUMMARY OF NRC 00118: FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0533710)

Part: PAN — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

CRACK ON AFT PAN INTERSECTION WITH BEAM #5, CRACK ON FWD PAN INTERSECTION WITH BEAM #3 , 3) CRACK ON FWD PAN INTERSECTION WITH BEAM #5 ON FWD CARGO DOOR. SUMMARY OF NRC 00132: AFT PAN INTERSECTION WITH BEAM #5, FWD PAN INTERSECTION WITH BEAM #3, AND FWD PAN INTERSECTION WITH BEAM #5 ON FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0532471)

Part: CAP — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN. SUMMARY OF NRC 00554: CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN WAS REPAIRED PER ERA 620017-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620017-14 REV 1. ASSOCIATED ER/A 14-620017 ADDED FOR AC 9527. (LP #0529059)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN. SUMMARY OF NRC 00553: LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #0527480)

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

CRACK ON INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00361: INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT WERE REPLACED PER B717-200 SRM 51- 41-02-0G AND 51-42-05-0G AND SPRINGS WERE REMOVED AND INSTALLED PER B717-200 AMM 27-26-06. (LP #0527441)

Part: BEAM — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK BEAM #1 AFT EDGE AT L1 DOOR PTAS. SUMMARY OF NRC 00320: BEAM #1 AFT EDGE AT L1 DOOR PTAS WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0526246)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, AFTER SEAT TRACK X = -44 BTW STA Y = 646 TO Y = 775 REMOVAL, CRACK ON HOLES AT WEB BTW STA 648 AND STA 650. CORRECTIVE ACTION: WEB BTW STA 648 AND STA 650 WAS REPAIRED PER B717 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2. (LP 0524830)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN. CPRRECTIVE ACTION: LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN WAS REPAIRED PER B717 SRM 56-10-02-2R-1. (LP 0519523)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACKS ON FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN. CORRECTIVE ACTION: FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP 0517945)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK ON RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX. CORRECTIVE ACTION: RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX WERE REPAIRED PER B717-200 SRM 56-20-02-2R REPAIR 1. (LP 0515789)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 51-41-02-0G. (LP 0516434)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK ON CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX) REPAIRED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2 FIG. 201. (LP 0516174)

Part: PAN — CRACKED (ZONE200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, INITIAL INSPECTION: CRACK ON LH RING PAN (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/UPPER) STA Y=851, (FWD/LOWER) STA Y= 851, (FWD/LOWER) STA Y=870, (FWD/LOWER) STA Y=908, (FWD/LOWER) STA Y=927, (FWD/UPPER/LOWER) STA Y= 946 AT CABIN PAX LH SIDE. CORRECTIVE ACTION: (ET) (HFEC) WAS ACCOMPLISHED ON LH RING PANS, CRACKS WERE FOUND AS FOLLOWS: LH RING PAN (FWD/UPPER) STA Y= 484 CRACK OF 0.200 IN, (FWD/LOWER) STA Y=636 CRACK OF 0.120 IN, (AFT/UPPER) STA Y=851 CRACK OF 0.200 IN, (FWD/LOWER) STA Y=908 CRACK OF 0.150 IN. AND (FWD/LOWER) STA Y=92 (FWD/UPPER/LOWER) STA Y= 946, (FWD/LOWER) STA Y=851, (FWD/LOWER) STA Y=870 NO CRACKS FOUND, PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001 AND (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/ UPPER) STA Y=851, (FWD/LOWER) STA Y=908 WERE REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1 REPAIR 1 PAR 5 B FIG. 202. (LP 0514440)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 210. (LP 0514363)

Part: CUSP WEB — CRACKED (ZONE 200) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK ON CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM. 53-00-55-2R PROCEDURE 4 FIG. 205. (LP 0514941)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CRACK ON LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R. PROCEDURE 2. REPAIR 2 FIG. 201. (LP 0514325)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. FIGURE 210. (LP 0514913)

Part: WEB — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, INITIAL INSPECTION: SEVERAL CRACKS BELOW INBD WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX. CORRECTIVE ACTION: WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX WAS REPAIRED PER B717-200 SRM 57-70-10-2R-2, PAR. 4 AND B717-200 SRM 51-41-02-0G. (LP 0512937)

Part: STRUCTURE — GROUND DAMAGE (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

AIRCRAFT 9527, FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. CORRECTIVE ACTION: PERMANENT REPAIR ON FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER WAS PERFORMED PER B717-200 SRM 53-20-15-2R, REPAIR 11, OPTION 1. PERFORMED VISUAL INSPECTION ON PERMANENT REPAIR OPTION 1, INITIAL & REPETITIVE EVERY 8,000 CYCLES AS MAINTENANCE REQUIREMENTS PER B717-200 SRM 53-20-15-2R-11 PAR 7 TABLE 202. (LP 0513045)

Part: BEAM — CRACKED (ZONE 800) · airframe 59,201 hrs · 42,207 cycles

CRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR. PTAS. SUMMARY OF NRC 00321: CRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9527. (LP #0507314)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00515: CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #0504361)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,201 hrs · 42,207 cycles

CRACK ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00552: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN, 1 CRACK WAS CONFIRMED ON LONG 6LH. PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001 AND LONGERON 06L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 FIG 201. (LP #0500549)

Part: BEAM — CRACKED (ZONE 100) · airframe 59,201 hrs · 42,207 cycles

CRACK WAS FOUND ON AFT BEAM 3 AT PAN. SUMMARY OF NRC 00254: PAN AFT SIDE BEAM 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0489872)

Part: HUB CAP — MISSING (ZONE 700) · airframe 59,201 hrs · 42,207 cycles

SHIP 9527 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 65 KTS DUE TO RIGHT "ANTI-SKID FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THE #4 MAIN GEAR HUBCAP AND CLAMP MISSING. THE HUBCAP AND CLAMP WERE REPLACED AND ALL ANTI-SKID RETURN TO SERVICE TESTS WERE COMPLETED. CASS FOR PDA ON TOP/6059-24 SUBMITTED ON 29JUL24. (LP #4305828)

Part: SPRING — BROKEN (UPLOCK SENSOR) · airframe 59,129 hrs · 42,143 cycles

SHIP 9527 -ATB/GEAR/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO A RIGHT MAIN LANDING GEAR "DOOR UP AND LATCHED UNSAFE" INDICATION. ATC DECLARED AN EMERGENCY FOR THIS EVENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR UP AND LATCHED SENSOR SPRING BROKEN AND THE PROXIMITY SENSOR CLAMP BROKEN. REPLACED SAME AND PERFORMED SUCCESSFUL GEAR SWINGS. PSEU RTS PASSED. (LP #5958880)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,348 hrs · 40,711 cycles

THE CIRCUIT BEAKER Z26 WAS DISCOVERED OUT. FLIGHT CREW RESET IT ON DIRECTION OF MAINTENANCE. BREAKER VISIBLY SPARKED. BREAKER IS OUT AGAIN. MAINTENANCE FOUND WIRES CROSSED AT F/O SLIDING WINDOW. RETERMINATED WIRES AT SPLICE. BREAKER NOW OPERATES NORMALLY. WINDOW FOG SYSTEM REMAINS ON MEL. REF SWPM CHAP 20. (LP #4620400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

CRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE. SUMMARY OF NRC 00077: CRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE WAS REPAIRED PER PRI 612145-14 REV 5 AND ER/A 612142-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR TIME CONTROLLED ITEMS SEC. AMOC: CONTROLLED WITH LOG PAGE 2988651 AND SEC II: CONTROLLED WITH LOG PAGE 2988657. (LP #2990123)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

CRACK ON LH CUSP WEB STA Y=696 X=54 AT PAX CABIN. SUMMARY OF NRC 00135: CUSP WEB FROM STA Y=655 TO STA Y=715 X=54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2988642)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

CRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME. (WINGBOX AREA). SUMMARY OF NRC 00118: CRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME WAS REPAIRED PER PRI 612213-14 REV 2 AND ER/A 612213-14 REV ORIGINAL SECTION I: PERMANENT REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 25SEP23 (729 DAYS FROM 26SEP23). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A) REVISION IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93 PER LOG PAGE 2988074. ASSOCIATED ER/A 14-612213 ADDED FOR AC 9527. (LP #2988778)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,183 hrs · 40,555 cycles

CORROSION FOUND ON AFT CARGO LOWER DOOR JAMB BTW STA Y-954 TO Y-994 AND LONGERONS 27R AND 28R. SUMMARY OF NRC 0163: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-20-15-2R-7 REPAIR 7. (LP #2987631)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14. SUMMARY OF NRC 00024: CRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14 WAS REPAIRED PER ER/A 612108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612108-14 REV 2. REPETITIVE INSPECTION MONITORING UNDER LP #2986418 PER ERA 612108-14 REV ORIGINAL. ASSOCIATED ER/A 14-612108 ADDED FOR AC 9527. (LP #2986780)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

A.D. CRACK WAS FOUND ON RH UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME STA Y=674.000 IN REFERENCE CARD 5310-01436-01D JOB #044-0004 STEP 7. SUMMARY OF NRC 00112: RH FRAME OF THE OVERWING FRAME STA Y=674.000 WAS REPLACED UNDER AMDS 5310-01436-03B. (LP #2980821)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,183 hrs · 40,555 cycles

CRACK ON RH CUSP WEB STA Y=655 AND Y=715 AND X=54. SUMMARY OF NRC 00145: RH CUSP WEB BETWEEN STA Y=655 AND Y=715 AND BETWEEN X=40 AND X=54 WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 REPAIR 4. (LP #2979411)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,378 hrs · 39,862 cycles

SHIP 9527 -GEAR/DE- UPON LANDING GEAR EXTENSION DURING FINAL APPROACH, THE LEFT GEAR RED "UNSAFE" INDICATION REMAINED ON. THE CREW COMPLIED WITH THE QRH, PERFORMED ALTERNATE GEAR EXTENSION PROCEDURES, AND THE LANDING WAS UNEVENTFUL. THE MAIN GEAR DOORS DID SCRAPE THE RUNWAY ON TOUCHDOWN. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE LEFT MAIN GEAR DOOR UP-LATCH LOCK WAS SHEARED. THE L/H MLG RETRACT ACTUATOR AND THE L/H ACTUATOR UPPER SUPPORT FITTING WERE REPLACED ON LP #2761101. ALSO THE L/H MLG DOOR WAS REPLACED ON LP #4681717. (LP #4681714)

Part: SUPPORT — CRACKED (RT WS 146) · airframe 55,454 hrs · 39,091 cycles

WING SUPPORT STRUCTURE AT RH WING STATION 146.421 IS CRACKED. SUMMARY SEE NRC 001-0030:2040-0048/002 00010: REPLACED L/E RIB (SUPPORT) REF BOEING DWG 5919110 AND 9919398. (LP #2536609)

Part: NONE — NONE · airframe 53,292 hrs · 37,119 cycles

FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. REMOVED EXSITING RIVETS AND CUT OUT DAMAGE FOR REPAIR PER B717 SRM 53-20-15-2R PRC. 11. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53- 20-15-2R PROC 11 OPTION 2 AND INSTALLED CONICAL SEALS. RII COMPLED WITH DELTA QC 5289. PLACING ON MON FOR REPETIVE VISUAL CK AT 3000 CYCLES AND PERMAMENT REPAIR AT 8000 CYCLES PER B717 SRM 53-20-15-2R PROCEDURE 11 OPTION 2. (LP #2075974)

Part: NONE — NONE · airframe 53,072 hrs · 36,928 cycles

THE CABIN OVERWING EXIT LIGHT WAS MISSING THE LENS COVER. LOCATION CABIN CENTER CEILING ROW 20. MAINTENANCE INSTALLED THE OVERWING EMERGENCY EXIT LIGHT COVER. (LP #2033883)

Part: NONE — NONE · airframe 52,879 hrs · 36,749 cycles

THE CIRCUIT BREAKER A10, CABIN STANDBY LIGHTS, TRIPS AFTER RESET MAINTENANCE PERFORMED A WIRING CHECK PER B717 WDM 33-52-02. WIRING CHECKS GOOD. PERFORMED OPERATIONAL TEST OF CABIN STANDBY LIGHTING PER B717 AMM 33-52 . OPERATIONAL CHECK WAS GOOD. NO 30 DAY HISTORY. AIRCRAFT IS OK FOR SERVICE. (LP #7336583)

Part: NONE — NONE · airframe 52,836 hrs · 36,708 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT BOTH OF THE OFF WING EMERGENCY LIGHTS WERE INOPERATIVE. FOUND A PULLED WIRE GOING TO THE BATTERY PACK. THE BATTERY PACK IN THE AFT CARGO COMPARTMENT WAS REPLACED. THE BATTERY PACK WAS CHARGED AND THE LEFT WING LIGHT WAS RELAMPED. BOTH OFF WING EMERGENCY LIGHTS NOW CHECK GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #7336525)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

FLOOR SUPPORT HAS CORROSION STA 200 LBL 6 - RBL 6. SUMMARY SEE NRC 058-0023:5310-2005/043 00471: REPLACED PER BAC DWG 9936534. ASSOCIATED ER/A 00-594165 ADDED FOR AC 9527. (LP #1972892)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

CORROSION R1 DOOR LOWER AFT CORNER. ONE FRAME AFT. MARKED. SUMMARY SEE NRC 058-0023:5310-2005/011 00351: REPLACED UPPER CUSP ANGLE REF BOEING DWG #9923667 AND SPLICED PER ERA 594104-14 REV ORIG. (LP #1972983)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

R1 DOOR THRESHOLD BENT UP IN MANY PLACES AND HAS CORROSION ON BOTTOM SIDE. MARKED. SUMMARY SEE NRC 058-0023:5310-2005/033 00433: REPLACED PER BOEING DWG 9936534. (LP #1968043)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

CORROSION FOUND ON SEAT TRACK AT FS 200 RBL 44. SUMMARY SEE NRC 058-0023:5310-2005/024 00421: REPAIRED PER B717 SRM 53-20-52-2R. (LP #1967693)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

CORROSION ON SUB FLOOR WEB STA 199 RBL 49. SUMMARY SEE NRC 058-0023:5310-2005/026 00423: REPAIRED PER ERA 594165-14 REV. O. (LP #1968423)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

R-1 DOOR AREA CORROSION: FWD GIRT BAR FITTING MOUNT PLATE CORRODED (MKD). SUMMARY SEE NRC 058-0023:5310-2005/005 00329: REPLACED FITTING PER DWG 9936534. (LP #1967900)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

R-1 DOOR AREA CORROSION: AFT GIRT BAR FITTING MOUNT PLATE CORRODED (MKD). SUMMARY SEE NRC 058-0023:5310-2005/004 00328: REPLACED FITTING PER DWG 9936534. (LP #1967899)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

R-1 DOOR AREA CORROSION: O/B FLOOR SUPPORT THRESHOLD PLATE CORRODED (MKD). SUMMARY SEE NRC 058-0023:5310-2005/008 00332: REPLACED FLOOR SUPPORT PER DWG 9936534. (LP #1967903)

Part: NONE — NONE · airframe 52,796 hrs · 36,672 cycles

R1 DOOR AREA, SEAT TRACK AT STA 220-260, RBL 54 REQUIRES CUT AND SPLICE TO FOM REF NR 351. SUMMARY SEE NRC 058-0023:5310-2005/034 00434: COMPLETED INSTALLATION OF RBL 54 SEAT TRACK REF BAC DRWG 5930547 AND B717 SRM 53-20-52-2R REP. 5 ASSOCIATED ER/A 00-594104 ADDED FOR AC 9527. (LP #1967351)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

RIGHT SIDE CUSP WEB MEMBRANE DAMAGED - APPROX. STA 218" TO STA 240" - RBL 44.50" TO RBL 54.00". SUMMARY SEE NRC 058-0023:5310-2005/058 00551: REPLACED CUSP WEB MEMBRANE REF BAC DWG 9910140. (LP #1967305)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

CORROSION ON SUB FLOOR WEB STA 202 RBL 44. SUMMARY SEE NRC 058-0023:5310-2005/025 00422: REPLACED DAMAGED SUB FLOOR REF BOEING DRAWING #9936534. (LP #1967378)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

FLOOR SUPORT FOR R2 THRESHOLD BETWEEN STA 180 AND 200 HAS SERVAL DEEP GOUGES (PART IS PREVIOUSLY BLENDED MARKED WITH BLUE). SUMMARY SEE NRC 058-0023:5310-2005/029 00429: REPLACED PER DAC DRWG 9936534. (LP #1961929)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

FLOOR SUPPORT HAS CORROSION STA 170-200 LBL 7. SUMMARY SEE NRC 058-0023:5310-2005/042 00470: REPLACED FLOOR SUPPORT REF BAC DWG #9936534. (LP #1961930)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

FLOOR SUPPORT IS CORRODED. SUMMARY SEE NRC 058-0023:5310-2005/046 00500: REPLACED SUPPORT REF DAC 9936534. (LP #1961931)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

R-1 DOOR AREA CORROSION. INBOARD FLOOR SUPPORT FOR PNL 221EF HAS CORROSION AT NUTPLATE HOLES TOP AND BOTTOM (MKD). SUMMARY SEE NRC 058-0023:5310-2005/006 00330: REPLACED FLOOR SUPPORT PER DWG #9936534. (LP #1961898)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

FLOOR SUPPORT CORRODED. SUMMARY SEE NRC 058-0023:5310-2005/047 00501: REPLACED SUPPORT REF DAC #9936534. (LP #1961928)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

LONGERON 30 HAS CORROSION AT FRAME 994 (PREVIOUS BLENDED MARKED WITH BLUE). SUMMARY SEE NRC 059-0008:5331-2001/006 00319: REPLACED DAMAGED LONGERON PER B717 SRM 53-20-05-2R. (LP #1955060)

Part: NONE — NONE · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

AFT CARGO LONGERON 30 FROM SPLICE AT F.S. 946-F.S. 984. MARKED. SUMMARY SEE NRC 001-0292:2550-2003/002 00262: REPLACED DAMAGED LONGERON PER B717 SRM 53-20-05-2R. (LP #1955059)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 52,796 hrs · 36,672 cycles

THE L-1 DOOR AREA HAS CORROSION: I/B FLOOR SUPPORT FOR 221AF CORRODED AND MANY MISDRILLED FASTENER HOLES. REPLACED SUPPORT REF BAC DWG 9936534. (LP #1943991)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,905 hrs · 35,922 cycles

THE AFT COMPARTMENT EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE AFT EQUIPMENT BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #7296477)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 50,932 hrs · 35,115 cycles

WORKING PRI 588486-14. THE FIRST BOLT HOLE ABOVE SKIN SPLICE AT STATION 2FS=52.267, HAS CRACK INDICATION IN VERT STAB LEADING EDGE LT SIDE. MAINTENANCE COMPLETED PRI 588486-14 REV 1. PERMANENT REPAIR PERFORMED, PER ERA 588486-14AD REV "O".

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 50,932 hrs · 35,115 cycles

THE FIRST BOLT HOLE ABOVE SKIN SPLICE AT STATION 2FS=52.267, HAS CRACK INDICATION IN VERT STAB LEADING EDGE LT SIDE, MARKED, REF AA 5530-01048 AND AD 2018-10-08. CRACK REPAIRED PER ERA 588486-14AD REV O (REF PRI 599486-14 REV 1) SEC 1. PERMANENT REPAIR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,228 hrs · 34,458 cycles

THE FOLLOWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING A SERVICE CHECK: - L1 & R1 EMERGENCY EXIT SIGNS, FAP PANEL EMERGENCY EXIT SIGN, AND THE CABIN OVERHEAD LIGHTS BETWEEN ROWS 24 THROUGH 29. MAINTENANCE REPLACED THE BATTERY PACKS B5-231, B5-118, AND B5-235 PER B717 AMM 33-51. OPERATIONAL CHECKS ARE NOW GOOD. (LP #7110689)

Part: SKIN — DEBONDED (LT SPOILER)

UPPER SURFACE DISBONDED.

Part: HOUSING — LOOSE (FUEL FILTER) · airframe 48,619 hrs · 33,232 cycles

THE CREW DIVERTED THE FLIGHT DUE TO THE AIRCRAFT DEVELOPING A FUEL LEAK WHILE ENROUTE. MAINTENANCE FOUND THE FUEL FILTER HOUSING COVER ATTACHMENT LOOSE DUE TO A MIGRATED INSERT. THE FUEL FILTER HOUSING WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PACKING — DAMAGED (FUEL FILTER) · airframe 48,612 hrs · 33,228 cycles

APPROX 40 MINUTES AFTER TAKEOFF, THE LAT FUEL UNBAL MESSAGE ANNUNCIATED. REBALANCED FUEL TRANSFER AND DIAGNOSED LEFT FUEL SYSTEM WAS LOSING FUEL. MAINTENANCE FOUND FUEL LEAKING FROM LOW PRESS FUEL FILTER CAP AND FROM BYPASS VENT VALVE ON THE NR 1 ENGINE. REPLACED DAMAGED PACKING ON FILTER CAP. REPLACED FUEL BYPASS VENT VALVE IAW AMM 73-13. REPLACED COELESTER BAGS AND CW DUCT BURNOUT. NO LEAKS ON ENGINE. OK FOR SERVICE.

Part: SKIN — DEBONDED (SPOILER)

UPPER SURFACE IS DISBONDED.

Part: THRESHOLD — CORRODED (AFT CARGO DOOR) · airframe 48,168 hrs · 32,898 cycles

CORROSION FOUND AT AFT CARGO DOOR THRESHOLD. REPAIRED REF B717 SRM 53-20-15-2R-7-REPAIR 7. (LP #1100474)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,927 hrs · 32,714 cycles

DOOR 1L & 1R EMERGENCY EXIT IDENTIFIERS DO NOT LIGHT UP DURING TEST. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER (B5-118) FOR THE LEFT & RIGHT FWD DOOR EXIT SIGNS PER B717 AMM 33-51-03. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM PER B717 AMM 33-51-00 710-801, FWD DOOR EXIT SIGNS CHECK GOOD AT THIS TIME.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 45,172 hrs · 30,777 cycles

THE EMERGENCY EXIT SIGN AT THE R1 DOOR AND THE EMERGENCY EXIT SIGN ABEAM FIRST CLASS LAVATORY ARE FLICKERING WHILE IN FLIGHT. MAINTENANCE REPLACED THE AFT BATTERY CHARGER UNDER THE FWD FOLD DOWN PANEL. OPS CHECKED GOOD IAW AMM 33-51. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,979 hrs · 30,636 cycles

EMERGENCY EXIT SIGN AT DOOR AND 1ST CLASS FLICKERS (ON AND OFF). MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT BATTERY PACK AND BATTERY OPERATION IS NOW NORMAL PER AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,801 hrs · 30,505 cycles

EMERGENCY LIGHTS AT THE MAIN CABIN AND SERVICE DOORS ARE INOPERATIVE. MAINTENANCE TROUBLESHOT IAW WDM 33-51 AND REPLACED THE BATTERY PACK AND POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD.

Part: TERMINAL BLOCK — SMOKE (WINDOW) · airframe 44,466 hrs · 30,292 cycles

DURING PRE FLIGHT, THE CREW NOTICED AN ODOR IN THE COCKPIT, THEN HAD SMALL AMOUNT OF SMOKE COMING FROM THE FIRST OFFICER`S WINDSHIELD TERMINAL BLOCK. MAINTENANCE REPLACED THE WINDOW AND TERMINAL BLOCK.

Part: SKIN — DELAMINATED (RT WING SPOILER)

DURING AN UNSHEDULED, NON ROUTINE CHECK, FOUND DELAMINATION ON UPPER SURFACE SKIN OF THE RIGHT SPOILER.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 43,763 hrs · 29,838 cycles

CRACKED FITTING ON THE LT FLAP INTERNAL STRUCTURE XCW 65. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AMM 20-00-02, AND AMM 20-50-01.

Part: FRAME — CRACKED (BS 1225) · airframe 43,763 hrs · 29,838 cycles

CRACK ON FRAME BS 1225, 7 HRS POSITION. THE FRAME WAS REPAIRED IAW ETI17-17-165, REV ORIGINAL. AND ER/A 590926-14, REV ORIGINAL.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 43,763 hrs · 29,838 cycles

CRACKS FOUND ON THE AFT CARGO DOOR INNER PAN AND OUTER PAN AROUND UPPER STOP. REPAIRED IAW ER/A 560875-14, REV ORIGINAL, AND ETI-17-17-140, REV 4.

Part: INTERCOSTAL — CRACKED (LT WING TE FLAP) · airframe 43,763 hrs · 29,838 cycles

CRACKED INTERCOSTAL ON LT FLAP, XCW 65. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05-0G, SRM 51-41-02-0G, AND DWG 9958001, REV U.

Part: LONGERON — CORRODED (BS 927-946) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON LONGERON 30, BS 927 TO 946 FOUND TO BE OUT OF LIMITS. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,763 hrs · 29,838 cycles

DAMAGE PAX CABIN FLOOR PANELS #220F, 221AF, 221CF, 221DF, 221EF, 221FF, 221KF, 221LF, 221QF, 222ABF, 222ACF, 222QF, 210F, 211AMF, 211ANF, 211ASF, AND 211ATF. (CPAX). NRC 00418: FLOOR PANEL #220F AND 210F DO NOT EXIST. THESE ARE IN ERROR IN TEXT DESCRIPTION. FLOOR PANEL #211AMF WAS ATTENDED WHITH NRC 00473 AND FLOOR PANEL #221LF, 221CF, 221DF, 221KF, 222ACF, 221QF, AND 221QF FERRULES WERE REPLACED PER B-717 SRM 53-20-2R PROCEDURE 3 AND FLOOR PANEL #211ASF, 222ABF, 221ATF, 221AF, 221EF, 211ANF, AND 221FF WERE FABRICATED, REPLACED, AND IDENTIFICATED PER B-717 SRM 53-20-2R PROCEDURE 3 AND FLOOR PANELWERE INSTALLED PER CARD 2040-0024 CREW 01 JOB #001-0061. (LP #0210264)

Part: ACCESS PANEL — CRACKED (NOT REPORTED) · airframe 43,763 hrs · 29,838 cycles

CRACK ON ACCESS PANEL 211GR. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-70-11-2R, FIG 201.

Part: SKIN — DEBONDED (LT WING SPOILER) · airframe 43,763 hrs · 29,838 cycles

DISBONDED UPPER SKIN OF INBD SPOILER PANEL XRS 220, LT WING. THE SPOILER PANEL WAS REPAIRED IAW ETI-17-17-154, REV ORIGINAL, ER/A 560897-14, REV ORIGINAL, AND JIC CARD 2000-8149-01.

Part: RUB STRIP — CORRODED (FUSELAGE PANELS) · corrosion level 2 · airframe 43,763 hrs · 29,838 cycles

CORROSION AND DISBONDED LT RUB STRIP ON SETTLEMENT AREA AF FILLET FUSELAGE PANELS. THE RUB STRIP WAS REPLACED IAW SRM 53-20-70-01 AND SRM 51-20-05.

Part: PAN — WORN (CABIN DOOR) · airframe 43,763 hrs · 29,838 cycles

WORN PAN ON ATTENDANT`S SEAT AREA AT AFT CABIN DOOR. THE PAN WAS REPAIRED SRM 52-10-02-2R-15 AND THE ANGLE WAS REPAIRED IAW ER/A 560896-14, REV ORIGINAL AND ETI-17-17-153 REV ORIGINAL.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 43,763 hrs · 29,838 cycles

ELONGATED HOLES ON FWD CARGO DOOR. REPAIRED IAW ETI-17-17-157, REV 2, AND ER/A 560915-14, REV ORIGINAL

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,763 hrs · 29,838 cycles

SCRATCHES ON THE SKIN AROUND THE LT ALTERNATE STATIC PORT. THE SKIN WAS REPAIRED IAW ETI-17-17-163, REV ORIG, AND ER/A 560924-14, REV ORIG.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 43,763 hrs · 29,838 cycles

CRACKED PASSENGER CABIN FLOOR PANEL 222XF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.

Part: SKIN — CRACKED (BS 1076) · airframe 43,763 hrs · 29,838 cycles

CRACKED FUSELAGE SKIN BETWEEN BS 1076 AND LONGERON 14R ABOVE THE RT PYLON. REPAIRED IAW ER/A 560871-14, REV ORIGINAL.

Part: RUB STRIP — CRACKED (FLOOR PANEL) · airframe 43,763 hrs · 29,838 cycles

CRACK AND MISSING PLASTIC RUBSTRIP ON FLOOR PANEL #211AKF AND 211AMF (CPIL). NRC 00473: CRACK ON FLOOR PANEL #211AKF AND 211AMF WAS REPAIRED PER B717 SRM 53-00-00-2R-1 FIG. 201 (SHEET 2) AND MISSING PLASTIC RUBSTRIP WAS INSTALLED PER B717 SRM 51-41-02-0G. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FLOOR PANEL #211AMF AFTER STOP DRILL AND NO CRACKS WERE FOUND PER DC-MD/BOEING NDT SPM 06-10-01.001 EQUIPMENT: NORTEC 600 C/N: 1601 S/N: 60002161027 EXP. DATE: 01MAR18. (LP #0203444)

Part: FRAME — CRACKED (BS 1022) · airframe 43,763 hrs · 29,838 cycles

CRACK ON FRAME CAP BS 1022 OVER LONGERON 7L. THE FRAME CAP WAS REPAIRED IAW ETI-17-17-145, REV 2, AND ER/A 560883-14, REV ORIG.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 43,763 hrs · 29,838 cycles

ELONGATED HOLES IN RH FUEL ACCESS #620DT, 620FT, 620LB, AND 620HB. (REF CARD 001-0434:2000-1002/016.) (AD). NRC 00466: HOLE OF THE ACCESS PLATE #620DT, 620FT, 620LB, AND 620HB WERE REWORKED, MEASURED, AND FOUND TO BE WITHIN LIMITS OF REPAIR PER B-717 SRM 57-10-01-2R-2- PAR. 5 B CONDITION II. BUSHINGS WERE FABRICATED AND INSTALLED IN #620DT, 620FT, 620LB, AND 620HB PER B-717 SRM 57-10-01 2R-2-PAR.5 B CONDITION II. (LP #0201670)

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 43,763 hrs · 29,838 cycles

ELONGATED HOLES ON RH FUEL ACCESS #520JB AND 520MB. (REF CARD 001-0434:2000-1002/017.) (AI). NRC 0468: HOLES (4EAS) ON ACCESS PLATE #520MB WERE REWORKED PER B-717 SRM 57-10-01-2R-2-PAR 5B CONDITION II AND WERE FOUND TO BE WITHIN LIMITS OF REPAIR PER B-717 SRM 57-10-01-2R-2 PAR. 5B CONDITION II. AREA WAS TREATED PER B-717 SRM 51-10-04-0G PAR. 21 AND BUSHINGS WERE INSTALLED PER B-717 SRM 57-10-01. HOLE ON ACCESS PLATE #520JB WAS REWORKED PER B-717 SRM 57-10-01-2R-2- PAR. 5 B CONDITION II AND FOUND TO BE WITHIN LIMITS OF REPAIR PER B-717 SRM 57-10-01-2R-2- PAR. 5B CONDITION II. BUSHING OF FUEL ACCESS PLATE #520JB WAS FABRICATED PER B-717 SRM 57-10-01 2R-PAR. 5B CONDITION II. AREA WAS TREATED PER B-717 SRM 51-10-04-0G PAR. 21 AND BUSHING WAS INSTALLED PER B-717 SRM 57-10-01. TOOL USED: DIGITAL CALIPER N/P: 500-196-30 N/S: B16188252 DUE DATE: 27OCT2017 CHAMFER GAGE N/P:1127 N/S: 60553 DUE DATE: 02FEB2018. (LP #0201731)

Part: VANE — PUNCTURED (LT WING TE FLAP) · airframe 43,763 hrs · 29,838 cycles

PUNCTURE ON INBD FACE AT AFT MOVABLE FLAP VANE, LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01-2R-1.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON THE CABIN FLOOR PANEL 120G. THE FLOOR PANEL WAS REPLACED IAW DWG 9957828, REV AB.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 43,763 hrs · 29,838 cycles

CRACK AND DENT ON THE LT AFT MOVABLE FLAP VANE LOWER SURFACE APROX 24.75 INCHS FROM INBD SIDE AND 3.25 INCHS FROM THE LE. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01-2R-1.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,763 hrs · 29,838 cycles

CRACK ON LT BEAM CUT OUT STA Y=47 NLG WHEEL WELL (NLG). DAMAGE AREA WAS REPAIRED PER ER/A 560906-14 REV ORIGINAL. (ET)(HFEC) WAS ACCOMPLISHED PER NDTSPM 06-10-01.001 NO CRACKS WERE FOUND AFTER REMOVED DAMAGE ON LT BEAM CUT OUT STA Y=47 NLG WHEEL WELL.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,763 hrs · 29,838 cycles

CRACK ON RT BEAM CUT OUT STA Y=47 NLG WHEEL WELL (NLG). DAMAGE AREA WAS REPAIRED PER ER/A 560906-14 REV ORIGINAL. (ET)(HFEC) WAS ACCOMPLISHED PER NDTSPM 06-10-01.001 NO CRACKS WERE FOUND AFTER REMOVED DAMAGE ON RT BEAM CUT OUT STA Y=47 NLG WHEEL WELL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,763 hrs · 29,838 cycles

CORROCION ON FUEL ACCESS PLATE 620CT. THE ACCESS PANEL WAS REPLACED AND VERIFIED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON FUEL ACCESS PANEL 520CT. THE ACCESS PANEL WAS REPLACED AND VERIFIED.

Part: CUSP WEB — CORRODED (BS 465-558) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON CUSP WEB, RBL 54 AND 60, BS 465 TO 471 AND 541 TO 550, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG. 216.

Part: CUSP WEB — CORRODED (BS 269-285) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON CUSP WEB, RBL 44 AND 60, BS 269 TO 271 AND 283 TO 285, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG. 215

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 43,763 hrs · 29,838 cycles

CRACKS INTERCOSTAL BETWEEN BEAM 5 AND UPPER EDGE ON AFT CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957666, REV V.

Part: FLOOR SUPPORT — CORRODED (BS 200-214) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON FLOOR SUPPORT BS 200 TO 214, RBL 56 AT FWD WET AREA. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-11-2R-1.

Part: CUSP WEB — CORRODED (BS 418-421) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON THE LT CUSP WEB UPPER & LOWER SURFACES, LBL 54 AND 60 FROM BS 418 TO 421. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINE AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.

Part: WEB — CORRODED (BS 200-208) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON WEB FROM BS 200 TO 208, BETWEEN LONGERONS 17L AND 18L. THE WEB WAS REPAIRED IAW SRM 53-00-00 2R.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON THE FLOORBEAM BS 200, RBL 10 TO 46. REPLACED IAW SRM 51-40-08-0G, 51-41-02, AND 51-41-05.

Part: CUSP WEB — CRACKED (BS 219) · airframe 43,763 hrs · 29,838 cycles

CRACKED CUSP WEB BS 219 BELOW SEAT TRACK RBL 44 AT FWD WET AREA. THE CUSP WEB WAS REPLACED IAW SRM 53-20-51-01-1, AND DWG 9930538, REV CF.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,763 hrs · 29,838 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=160 TO Y=200 AND X=55 AT FWD WET AREA. FLOOR SUPPORT BTW STA Y=160 TO Y=200 AND X=55 AT FWD WET AREA WAS REPLACED PER SRM 51-40-08-0G AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,763 hrs · 29,838 cycles

CORROSION ON FLOOR SUPPORT IS OUT OF LIMITS, STA X=-7 FROM Y=148 TO Y=200 AT FWD WET AREA. FLOOR SUPPORT ON STA X=-7 FROM Y=148 TO Y=200 AT FWD WET AREA. WAS REPLACED PER SRM 51-41-01.

Part: FRAME — CRACKED (BS 1037) · airframe 43,763 hrs · 29,838 cycles

CRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R-4 REPAIR 4. HFEC WAS ACCOMPLISHED ON THE FRAME, NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM PART 6, 06-10-01.001.

Part: CUSP WEB — DAMAGED (BS 484-497) · corrosion level 2 · airframe 43,763 hrs · 29,838 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 484 - 497, RBL 54 - 60 ON THE CUSP WEB. THE CUSP WEB WAS REPLACED IAW SRM 53-00-55-2R-4, FIG 216.

Part: CUSP WEB — CRACKED (BS 674) · airframe 43,763 hrs · 29,838 cycles

CRACKED LT CUSP WEB BETWEEN BS 674, LBL 44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 220. HFEC INSPECTION WAS ACCOMPLISHED WITH NO CRACKS FOUND AFTER DAMAGE REMOVED IAW NDT SPM 06-10-01.001.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,763 hrs · 29,838 cycles

CRACK ON FWD CARGO DOOR INNER PAN BETWEEN BEAMS 1 AND 2, BS 427. CRACK WAS 0.487. REPAIRED IAW SRM 52-30-02-2R, FIG 201, SHEET 2.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,258 hrs · 29,425 cycles

FORWARD CABIN NR 2 POWER SUPPLY FOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51. AIRCRAFT IS OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,686 hrs · 29,013 cycles

DURING A SERVICE CHECK, FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE AT THE L1 DOOR AND FWD R1 DOOR. REPLACED THE POWER SUPPLY. OPS CHECKED NORMAL IAW AMM 33-51.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,390 hrs · 28,796 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE FORWARD MAIN CABIN DOORS L1 AND R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER FOR B1-118 AND THE LIGHT BASES FOR L2-832 & L2-833. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,371 hrs · 28,785 cycles

MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHTS AT BOTH L1 AND R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 42,327 hrs · 28,749 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER AT 01C WAS LOOSE. MAINTENANCE SECURED THE LENS AND OPS CHECKED GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 42,327 hrs · 28,749 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER AT 01C WAS LOOSE. MAINTENANCE SECURED THE LENS, AND OPS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 42,038 hrs · 28,520 cycles

THE PILOT DISCOVERED THAT THE EMERGENCY EXIT LIGHTS AT THE GALLEY DOOR AND THE FRONT OF THE FIRST CLASS SECTION OF THE CABIN WERE INTERMITTENT IN OPERATION. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND SIGNED IT OFF AS NTF.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,936 hrs · 28,449 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT AND THE EXIT SIGN AT L1 DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LANYARD — DISCONNECTED (L1 DOOR SLIDE) · airframe 40,728 hrs · 27,563 cycles

F/A DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A DISCONNECTED LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. MAINTENANCE REINSTALLED THE DOOR SLIDE LANYARD IAW AMM 25-61.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,482 hrs · 27,356 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH THE L1 AND L2 MAIN CABIN DOORS, EMERGENCY LIGHT HANDLE ILLUMINATOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,220 hrs · 27,147 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE FORWARD MAIN CABIN DOORS, L1 & R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: LONGERON — CRACKED (BS 1133) · airframe 39,262 hrs · 26,429 cycles

TAIL COMPARTMENT, LONGERON 2L CRACKED AT BS 1133. PERFORMED LONGERON SPLICE REPAIR IAW SRM 53-00-05, REPAIR 2.

Part: LONGERON — CRACKED (BS 1133) · airframe 39,262 hrs · 26,429 cycles

TAIL COMPARTMENT, LONGERON 2 RT CRACKED AT BS 1133. SPLICED LONGERON IAW SRM 53-00-05, REPAIR 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,581 hrs · 25,123 cycles

DURING SERVICE CHECK, FOUND EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK B5-235 AND POWER SUPPLY, BATTERY PACK B5-118 IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,406 hrs · 23,170 cycles

MID EXIT LIGHTS ON L1 AND R1 DOOR INOPERATIVE. REPLACED EXIT POWER SUPPLY IAW AMM 33-55.

Part: BEARING — FAILED (NR 3 WHEEL) · airframe 35,327 hrs · 23,100 cycles

CREW REPORTED RT BRAKE CHATTERING ON TAXI OUT FOLLOWED BY A REPORT FROM OTHER ACFT THERE WAS VISIBLE SMOKE & FIRE ON THE RT MAIN GEAR. WHEN EMERGENCY EQUIPMENT ARRIVED, GEAR WAS SMOKING, BUT NO FLAMES WERE VISIBLE. ACFT WAS TOWED BACK TO THE GATE. MAINTENANCE JACKED THE RT MLG AND FOUND THE NR 3 MAIN WHEEL ASSY INNER BEARING FAILED AND THE SLEEVE DAMAGED. REPLACED THE NR 3 MAIN WHEEL ASSY NR 3 MLG BRAKE ASSY, AXLE SLEEVE, NR 3 ANTI-SKID TRANSDUCER, NR 4 MAIN WHEEL ASSEMBLY, AND INSPECTED THE NR 2 ENGINE FOR FOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 343,830 hrs · 22,397 cycles

OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM.

Part: WEB — CRACKED (LT HORIZ STAB) · airframe 343,830 hrs · 22,397 cycles

LT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AT RECESSED AREA STATION XFS 194 I40-1. R & R WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

SEAT TRACK CORRODED BETWEEN STATION 200 TO STATION 598, RBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

TAIL COMPARTMENT FRONT SPAR AFT FUSELAGE BULKHEAD LOOKING FWD STATION 1152 INBD SUPPORT CLIP CRACKED JUST ABOVE RAM AIR DUCT. R & R SHEAR CLIP IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 343,830 hrs · 22,397 cycles

OVER WING DOOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 343,830 hrs · 22,397 cycles

EMERGENCY LIGHT EXIT SIGN ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

AFT CARGO FWD PRESSURE BULKHEAD CENTER VERTICAL SUPPORT CRACKED AT LOWER END. R & R SUPPORT IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

FUSELAGE EXTERIOR CANTED KEEL LT SIDE INTERNAL AT FS 675 OTBD ANGLE CRACKED. REPAIRED DOUBLER IAW SRM.

Part: FITTING — DIRTY (L1 DOOR) · airframe 343,830 hrs · 22,397 cycles

L1 DOOR AFT GIRT BAR FITTING & FASTENER HOLES DIRTY. CLEANED FITTING IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

FUSELAGE EXTERIOR CANTED KEEL RT SIDE INTERIOR AT FS 715 OTBD UPPER ANGLE CRACKED. REPAIRED DOUBLER IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 343,830 hrs · 22,397 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING FASTENER HOLES CORRODED. REPAIRED FITTING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

CUSP WEB CORRODED BETWEEN STATION 486 TO STATION 490, LONGERON 18R. R & R CUSP WEB IAW SRM.

Part: COVER — CRACKED (L1 DOOR) · airframe 343,830 hrs · 22,397 cycles

L1 DOOR LINER ESCAPE SLIDE COVER CUTOUT CRACKED AT AFT EDGE. REPAIRED COVER IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

FS EXTERIOR CANTED KEEL LT SIDE INTERNAL AT FS 660 HAS OTBD UPPER ANGLE CRACKED. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

CUSP WEB CORRODED BETWEEN STATION 647 TO STATION 672, LONGERON 18R. R & R CUSP WEB IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

FUSELAGE EXTERIOR CANTED KEEL RT SIDE INTERNAL AT FS 660 OTBD UPPER ANGLE CRACKED. REPAIRED DOUBLER IAW EA & SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

AFT CARGO FWD PRESSURE BULKHEAD HORIZONTAL PANEL SUPPORTS CRACKED. R & R SUPPORTS IAW SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 343,830 hrs · 22,397 cycles

RT WING FRONT SPAR FWD FACE VERTICAL STIFFENER CRACK RT OF AIRCRAFT CENTER LINE FWD CARGO BAY AFT BULKHEAD. R & R STIFFENER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 343,830 hrs · 22,397 cycles

CUSP WEB CORRODED AT STATION 525, LONGERON 18R. REPAIRED CUSP WEB IAW SRM.

Part: SPAR — CRACKED (RT HORIZ STAB) · airframe 343,830 hrs · 22,397 cycles

RT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AT STATION FS 194 140-1. R & R WEB IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 343,830 hrs · 22,397 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING FASTENER HOLES CORRODED. REPAIRED FITTING IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,763 hrs · 22,003 cycles

L1 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 33,581 hrs · 21,890 cycles

EMERGENCY EXIT ROW, SIGN AT ROW 2 LOOSE. SECURED SIGN PER AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 32,453 hrs · 21,185 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK LOOSE. SECURED SLIDE PER AMM.

Part: LENS — MISSING (CABIN) · airframe 31,899 hrs · 20,822 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT AT WING MISSING LENS. INSTALLED LENS PER MM.

Part: FITTING — CRACKED (LE SLAT) · airframe 31,221 hrs · 20,370 cycles

RT WING NR 4 L/E SLAT O/B FITTING CRACKED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: PLACARD — UNSECURE (CABIN)

THE FWD AISLE EXIT PLACARD IN THE BUSINESS CLASS IS NOT SECURED. REMOVED AND REPLACED FWD EXIT SIGN PLASTIC COVER. REF MM 33 23.

Part: LENS — LOOSE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED EMERGENCY EXIT LENS, OPS CHECK OK. IAW 33-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 172 TO 192, LBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FRAME — CRACKED (BS 212 L15)

MAIN CABIN FRAME CLIP, STA 212, LONG L15, CRACKED. ACCOMPLISHED FRAME CLIP DOUBLER REPAIR PER SRM 51-70-10. SEE NR 713964.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 192 TO 200, RBL 55, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-41-02.

Part: FLOORBEAM — CORRODED (BS 200)

FLOORBEAM BS 200, RBL 9 TO RBL 45, CORRODED. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 195)

MAIN CABIN FLOOR SUPPORT, BS 195, LBL 24, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER 51-41-02.

Part: ATTACH FITTING — CORRODED (CABIN)

R1 DOOR AFT GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (BS 237)

FLOORBEAM, BS 237, LBL 15 TO RBL 15, CORRODED. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (BS 200)

MAIN CABIN FLOOR SUPPORT, BS 200, RBL 5 CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 200)

MAIN CABIN FLOORBEAM, BS 200, LBL 8-12, CORRODED. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 256, LBL15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL45 TO RBL52, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER .

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS FROM ROW 25 TO AFT ACCESSORY COMPT DID NOT ILLUMINATE WHEN TESTED. CHECKED BATTERY PACK AT ROW 25. NO DEFECTS NOTED. PERFORMED EMERGENCY LIGHTING OPERATIONAL TEST. EMERGENCY LIGHTS NOW ILLUMINATE. OPS CHECK GOOD REF B717 33-51.

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 — DAMAGED (CARGO DOOR)

REPAIR OF AFT CARGO DOOR LOWER JAMB. COMPLETED REPAIR OF DOOR LOWER JAMB.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORROSION REPAIR. COMPLETED FLOOR SUPPORT REPAIR FROM STA 200 TO STA 148.

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: WIRE — DAMAGED (LT WING)

DEPARTED TPA CLIMBING ABOVE 10,000 FEET ENGINE LEFT FUEL PRESSURE AND TANK LEFT PUMP LOW LIGHTS CAME ON. CONFIRMED LEFT TANK NOT FEEDING. OPENED CROSSFEED VALVE AND DIVERTED TO KMOC. REPAIRED DAMAGED WIRES TO LEFT FUEL BOOST PUMP IN LEFT WING IAW EA 17-28-1412A; ALL SYSTEMS OPS CHECK NORMAL IAW 28-20-01; LEAK CHECK GOOD FOR LEFT WING ANTI-ICE DUCT IAW 30-10-07. AIRCRAFT RETURNED TO NORMAL.

Part: SPRING — MISSING (TAIL CONE)

A 1EA TAIL CONE RELEASE MECHANISM TENSION SPRING MISSING. INSTALLED 1EA TAIL CONE MECHANISM TENSION SPRING PER EA 17-53-01195IR.

Part: SOCKET — MISSING (ROW 26 DEF)

EMERGENCY PATH LIGHT AT SEAT ROW 26 DEF DOES NOT ILLUMINATE. ELECTRICAL CONNECTOR AT BASE OF SEAT WAS TORN OFF/MISSING. FOUND DURING SERVICE CHECK. REPLACED AIRCRAFT SIDE ELECTRICAL CONNECTOR AT SEAT ROW 26 DEF PER SWPM 20-20, WDM 33-51-14. OPS CHECK GOOD PER AMM 33-51-00.

Part: BUNGEE CYLINDER — MALFUNCTIONED (NLG)

NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE STRUT LOW ON SERVICE. REMOVED AND REPLACED NOSE GEAR BUNGEE CYLINDER AND SERVICED NOSE STRUT. PERFORMED GEAR SWING AND ALL CHECKED GOOD.

Part: CYLINDER — MALFUNCTIONED (NLG)

NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF IN ATLANTA. REMOVED AND REPLACED NOSE LANDING GEAR RETRACT CYLINDER PER B717 AMM 32-35-01, NO LEAKS AT THIS TIME.