N960AT

Part: RELEASE CABLE — TORN (ZONE 300) · airframe 57,475 hrs · 40,594 cycles

INITIAL INSPECTION: TORN CABLE OF RELEASE MECHANISM OF TAIL CONE AT AFT ACCESORIES COMPARTMENT. CORRECTIVE ACTION: CABLE ASSY RELEASE HANLDE P/N: 3913359-545 OF RELEASE MECHANISM OF TAIL CONE WAS REPLACED PER B717-200 AMM 20-00-02 AND ADJUSTED WAS PERFORMED PER B717-200 AMM 53-52-01 AND UNDER AMDS 5352-4002 (1220435)

Part: VALVE — STIFF (NR 2 ENGINE) · airframe 56,266 hrs · 39,462 cycles

SHIP 9519 -ATB/FUME/DE- DURING CLIMB OUT AT ABOUT 10K FEET, THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO MEM DUE TO UNKNOWN ODOR THROUGHOUT THE CABIN. CORRECTIVE ACTION: MAINTENANCE DISCOVERED THAT THE BUFFER AIR VALVE ON THE #2 ENGINE WAS VERY STIFF IN IT'S OPERATION AND REPLACED IT. THE ODOR WAS REMOVED AND THE AIRCRAFT RETURNED TO SERVICE. (LP #7109314)

Part: ACCESS PANEL — MISSING (ZONE 500) · airframe 56,264 hrs · 39,459 cycles

LH WING LANDING LIGHT TOOLING ACCESS COVER MISSING. MAINTENANCE DEFERRED IT TO MONITOR PER ERA 607941-14TR REV ORIGINAL. C/W TEMP REPAIR PER SECTION I. ENGINEERING APPROVED REPAIR PER DAL P.S. 900-5-1, #04. REPETATIVE CHECK DUE EVERY 50 FLIGHT HOURS, TERMINATING ACTION DUE AT 500 FLIGHT HOURS. INSTALLED STOCK/SER NUMBER 09-3340-9-0007, 05148. ASSOCIATED ER/A 14-607941 ADDED FOR AC 9519. AS OF 03MAR25, LOG PAGE IS STILL ON DEFERRAL: 09 DFRD DTW 02MAR25 RII: N W (ETS WIP) MECHANIC: C/W REP CHECK PER ERA 607941-14TR. NO NEW DEFECTS NOTED. SPEED TAPE STILL ON AND IN GOOD CONDITION. OK TO CONTINUE ON MONITOR. (LP #6521340)

Part: CONTROL UNIT — FAILED (ANTI-SKID) · airframe 55,188 hrs · 38,516 cycles

SHIP 9519 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE WHEN TRANSITIONING FLAPS FROM 18 TO 40 WITH THE GEAR EXTENDED. THE CREW PERFORMED A GO-AROUND. ONCE STABLE, THE CREW COMPLIED WITH THE QRH AND REFERENCED THE ODM FOR LANDING PERFORMANCE DATA. THE CREW DID DECLARE AN EMERGENCY WITH ATC. CORRECTIVE ACTION: MAINTENANCE REPLACED THE BCU AND PERFORMED APPLICABLE RETURN TO SERVICE TESTS. ALL TESTS PASSED. (LP #6185580)

Part: NONE — NONE (NONE) · airframe 54,149 hrs · 37,605 cycles

ERA 612138-14 REV A. ACCOMPLISH SECTION III AT 50,000 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 00-612138 ADDED FOR AC 9519. ERA 612138-14 OK TO CLOSE, OPENED IN ERROR. TERMINATED LOG PAGE PER ENGINEERING COMMENTS ON LINE 3. CLOSED LOG AND REMOVED MONITOR INSP. (LP #0234418)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION TYPE EXFOLIATION ON PREVIOUS REPAIR BTW STA Y=960 TO Y=980, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. CORROSION TYPE EXFOLIATION ON PREVIOUS REPAIR BTW STA Y=960 TO Y=980, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 612138-14 REV ORIGINAL, SECTION I: TIME LIMITED REPAIR. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM TIME OF INSTALLATION ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION (DTE) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA ADVISORY CIRCULAR 120-93 UNDER LOG 0004872. ASSOCIATED ER/A 14-612138 ADDED FOR AC 9519. (LP #0010117)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON LOWER DOOR JAMB OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. LOWER DOOR JAMB OF AFT CARGO WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP #0009476)

Part: SKIN — DAMAGED (NR 2 CARGO DOOR) · airframe 53,935 hrs · 37,416 cycles

DTE, ERA 612138-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN REPAIR AT #2 CARGO DOOR OPENING / Y=954 - 994, L-28R IS PENDING DTE STAGE II & III APPROVAL PRIOR TO 12 MONTHS SERVICE FROM 06OCT23. DISCONTINUE REVENUE SERVICE ON OR BEFORE 06OCT24 PENDING STAGE III APPROVAL. ASSOCIATED ERA 00-612138 ADDED FOR AC 9519. **REDEFERRED LOG TO QC, ESTAB MON INSP **. OK TO CLOSE AT ERA 612138-14 REV A. TERMINATED PER LINE 04 LOG COMMENTS. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 07MAR24 AND LOG COMMENTS. (LP #0004872)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION WAS FOUND ON FRAME CLIP FROM STA 655 LOGERON 30, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00514: CORROSION LEVEL 2. FRAME CLIP FROM STA 655 LOGERON 30 WAS REPLACED AND INSTALLED PER B717-200 SRM 51-40-08-0G, 51-41-02-0G, AND 51-41-01-0G. (LP #0000105)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FRAME CLIP STA Y=1022 BTW LONGERON 26 RH TO LONGERON 26 LH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00499: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW LONGERON 26 RH TO LONGERON 26 LH WAS REPLACED AND INSTALLED PER DWG 9912243 TEM 383 REV JM AND B717-200 SRM 51-41-02-0G. (LP #2990225)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FRAMES STA 1022 BTW LONG 27R-29R AND AT STA 1037 BTW LONG 29R-29L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00622: CORROSION LEVEL 2. FRAMES STA 1022 BTW LONG 27R-29R AND AT STA 1037 BTW LONG 29R-29L AT AFT CARGO COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM INITIAL VISUAL INSPECTION AT 25000 CYCLES AND THEN REPETITIVE INSPECTIONS EVERY 6500 CYCLES PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 PARAGRAPH 6. (LP #2988933)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

BROKEN FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-300 AND LONG L 11R. SUMMARY OF NRC 00578: FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-300 AND LONG L 11R WAS REPAIRED PER PRI 611539-14 REV 3 AND ERA 611539-14AD REV ORIGINAL, SECTION I PERMANENT REPAIR. ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS WITHIN EVERY 8,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR UNDER LOG PAGE #2979015 REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL FLIGHT CYCLES. AMOC APPROVAL FOR AD 2017-01-03 IS REQUIRED FOR FLIGHT BEYOND THIS LIMIT UNDER LOG PAGE #2979024. ASSOCIATED ER/A 14-611539 ADDED FOR AC 9519. (LP #2979831)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACK ON PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB (RH EDGE) ON STA Y=1053 BTW LONG PROJECTION 14R AND 16R AT AFT CPAX. SUMMARY OF NRC 00285: PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB (RH EDGE) ON STA Y=1053 BTW LONG PROJECTION 14R AND 16R AT AFT CPAX WAS REPAIRED PER PRI 611330-14 REV 1 AND ERA 611330-14 REV ORIGINAL, SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-611330 ADDED FOR AC 9519. (LP #2979700)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON MEMBRANES BTW STA 1053 AND L-28L TO L-23R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00573: CORROSION LEVEL 2. MEMBRANES BTW STA 1053 AND L-28L TO L-23R AT AFT CARGO COMPARTMENT WERE REPAIRED PER B-717-200 SRM 51-70-10-2R REP 1 PAR 4 FIG 201. (LP #2971101)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON INNER DOUBLER UNDER FITTING OF CENTER BULKHEAD POST STA Y=1053 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INNER DOUBLER UNDER FITTING OF CENTER BULKHEAD POST STA Y=1053 AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-02 -0G. (LP #2968765)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION OUT OF LIMITS ON AN INTERCOASTAL AT STA 1037 LONG 30 RH CARGO COMPARTMENT (C2). SUMMARY OF NRC 00643: CORROSION LEVEL 2. INTERCOASTAL AT STA 1037 LONG 30 RH WAS REPLACED PER DWG 9936718-41 REV N AND INSTALLED PER B717-200 SRM 51-41-02-0G. (LP #2966569)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON LONG L 22R/23RH BTW STA Y=1002/1053 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00192: CORROSION LEVEL 2. LONG L 22R/23RH BTW STA Y=1002/1053 AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER DWG S2777922-5 REV B AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2955469)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON RH CUSP WEB STA Y=273-275, Y=370-389, Y=636-655, Y=832-851, Y=889-908, Y=908-927, Y=927-946, AND X=-56 IS OUT OF LIMIT AT PASSENGER CABIN IN REF NRC 00377. SUMMARY OF NRC 00626: CORROSION LEVEL 2. RH CUSP WEB STA Y=273-275, Y=370-389, Y=636-655, Y=832-851, Y=889-908, Y=908-927, Y=927-946, AND X=-56 WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #2955491)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION FOUND. THE LH OUTBD SEAT TRACK BTW STA 318-320 WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.100 IN. THE REMAINING THICKNESS IS 0.032 IN. THEREFORE THE REWORKED AREAS IS OUT OF LIMITS PER B717-200 SRM 53 -20-52-1A ALLOWABLE DAMAGE 1 PARAGRAPH 4 FIGURE 101 AND DC-MD/ BOEING NDT SPM PART. 4 FIG 9. SUMMARY OF NRC 00642: CORROSION LEVEL 2. LH OUTBD SEAT TRACK BTW STA 318-320 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #2955482)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON PRODUCTION DOUBLER LONGERON 18 RH BTW STA Y 889 AND 908 AT PAX CABIN. SUMMARY OF NRC 00653: CORROSION LEVEL 2. PRODUCTION DOUBLER LONGERON 18 RH BTW STA Y 889 AND 908 AT PAX CABIN WAS REPLACED PER DWG 9910151 REV CH. (LP #2952799)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACKS ON WEB BTW STA X=44/60 AND BTW STA Y=218/237 AT PAX CABIN (W1). SUMMARY OF NRC 00327: CRACKS ON WEB BTW STA X=44/60 AND BTW STA Y=218/237 AT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #2952841)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR SUPPORTS STA X=-56 BTW STA Y=200/216 AT PAX CABIN (W1). SUMMARY OF NRC 00317: CORROSION LEVEL 2. FLOOR SUPPORTS STA X=-56 BTW STA Y=200/216 AT PAX CABIN WAS REPLACED PER DWG 5952262 REV L. (LP #2952844)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR SUPPORTS (2 EA) STA X=56 BTW STA Y=196/200 AND STA Y=200/215 AT PAX CABIN (W1). SUMMARY OF NRC 00321: CORROSION LEVEL 2. FLOOR SUPPORTS STA X=56 BTW STA Y=196/200 AND STA Y=200/215 AT PAX CABIN WERE REPLACED AND INSTALLED PER B717-200 SRM 53-10-51-0I-2, 51-41-08-0G, AND 51-41-05-0G. (LP #2950338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACK LH CUSP WEB STA Y 889 AND STA 946 AT PASSENGER CABIN. SUMMARY OF NRC 00599: LH CUSP WEB STA Y 889 AND STA 946 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 216. (LP #2950979)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON RH CUSP WEB IS OUT OF LIMITS STA Y=957-946, Y=908-889, AND X=-47 AT PASSENGER CABIN CPAX. SUMMARY OF NRC 00627: CORROSION LEVEL 2. WEB STA Y=957-946 WAS REPAIRED PER B717-200 SRM 51-41-02-0G AND 53-00-55-2R PROCEDURE 4. AND STA 889-908 MUST BE REPLACED PER DWG 991051-123 REV CH UNDER NRC 00626. (LP #2951333)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR SUPPORTS STA Y=200 (1 EA) BTW STA X=-46-56 AND STA X=55 (1 EA) BTW STA Y=160/196 AT PAX CABIN (W1). SUMMARY OF NRC 00316: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=200 (1 EA) BTW STA X=-46-56 AND STA X=55 (1 EA) BTW STA Y=160/196 AT PAX CABIN WERE REPLACED AND INSTALLED PER DWG 5930540 REV BF AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2948782)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON SEAT TRACK BTW Y=200 TO 246 AND X=-44 AT PAX CABIN STRUCTURE. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO 246 AND X= -44 AT PAX CABIN STRUCTURE WAS REPLACED AND INSTALLED PER DWG 5930547 REV CZ AND B717-200 SRM 51-41-05-0G. (LP #2948776)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR SUPPORTS STA Y=218 (1 EA) BTW STA X=-10/13, STA Y=200 (3 EA) BTW STA X=-9/-46, X=-5/5, X= 9/13, STA Y=196 (1 EA) BTW STA X=16/43, STA Y=180 (2 EA) BTW STA X=13/38, X=-9/-44, STA X=-45 (1 EA) BTW STA Y=160/200, STA X= 15 (2 EA) BTW STA Y=197/200, Y=200/256, STA X=44 (1 EA) BTW STA Y=161/204 AT PAX CABIN (W1). SUMMARY OF NRC 00315: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=218 BTW STA X=-10/13, STA Y=200 BTW STA X=-9/-46, X=-5 /5, X=9/13, STA Y=196 BTW STA X=16/43, STA Y=180 BTW STA X=13/38, X=-9/-44, STA X=-45 BTW STA Y=160/200, STA X=15 BTW STA Y=197/200, Y=200/256, STA X=44 BTW STA Y=161/204 AT PAX CABIN WERE REPLACED AND INSTALLED PER DWG 9936534 REV BW, B717-200 SRM 51-41-05-0G, AND 51-41- 02-0G. (LP #2948937)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR FITTING STA X=-11 BTW STA Y=200/218 AT PAX CABIN (W1). SUMMARY OF NRC 00319: CORROSION LEVEL 2. FLOOR FITTING STA X=-11 BTW STA Y=200/218 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG 5968021 REV AND B717 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #2948761)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON WEBS BTW STA X=55/-55 AND BTW STA Y=160/218 AT PAX CABIN (W1). SUMMARY OF NRC 00323: CORROSION LEVEL 2. WEBS BTW STA X=55/-55 AND BTW STA Y=160/218 AT PAX CABIN WERE REPLACED AND INSTALLED PER DWG 9936534-5 REV BW AND B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #2948102)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR CHANNELS (2 EA) STA X=-7 AND STA X=7 BTW STA Y=160/200 AT PAX CABIN (W1). SUMMARY OF NRC 00320: CORROSION LEVEL 2. FLOOR CHANNELS (2 EA) STA X=-7 AND STA X=7 BTW STA Y=160/200 AT PAX CABIN WERE REPLACED PER DWG 9936534-73 REV BW. (LP #2943607)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACK ON INTERNAL SKIN AT FWD CARGO DOOR BTW STA 402 TO STA 415 APROX AND Y=0. SUMMARY OF NRC 00103: INTERNAL SKIN (LOWER OUTER PAN) AT FWD CARGO DOOR BTW STA 402 TO STA 415 APROX WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2938777)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON DOUBLER OF AFT PRESSURE BULKHEAD FWD FACE BTW STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00306: CORROSION LEVEL 2. DOUBLER OF AFT PRESSURE BULKHEAD FWD FACE BTW STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2937018)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CORROSION WAS FOUND ON THE LEFTHAND CUSP WEB. MEASUREMENT THICKNESS WAS ACCOMPLISHED. ORIGINAL WIDTH THICKNESS IS 0.032 IN ON LH CUSP WEB (REPAIR PART) BTW STA Y=715-696. REMAINING THICKNESS IS 0.010IN, THEREFORE THESE ARE OUT LIMITS. SUMMARY OF NRC 00589: CORROSION LEVEL 2. LH CUSP WEB BTW STA Y=715-696 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #2931284)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON SPLICE STA Y=694 AND X=-49 AT PASSENGER CABIN (CPAX). SUMMRY OF NRC 00375: SPLICE WAS REPLACED PER B717 SRM 53-00-55- 2R. (LP #2929400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACKS ON CUSP WEB LOWER SIDE (2 EA) STA Y=718 LH/RH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00374: CRACKS ON CUSP WEB LOWER SIDE STA Y=718 LH/RH PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2929297)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR SUPPORT STA X=-54 AND BTW STA Y=1022/1055 AT PAX CABIN (W2). SUMMARY OF NRC 00380: CORROSION LEVEL 2. FLOOR SUPPORT STA X=-54 AND BTW STA Y=1022/1055 AT PAX CABIN WAS REPLACED PER DWG 9981474 REV K AND R B717-200 SRM 51-40-08-0G. (LP #2927770)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,024 hrs · 36,655 cycles

CORROSION ON FLOOR TRACK STA X=-44 AND BTW STA Y=1022/1059 AT PAX CABIN (W2). SUMMARY OF NRC 00379: CORROSION LEVEL 2. NEW FLOOR TRACK WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2927774)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,024 hrs · 36,655 cycles

CRACK ON FRAME STA Y=1037 ABOVE LONG 17L AT PAX CABIN. SUMMARY OF NRC 00236: FRAME STA Y=1037 ABOVE LONG 17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #2925535)

Part: HINGE — LOOSE (EVAC SLIDE) · airframe 52,949 hrs · 36,595 cycles

THE TAIL CONE SLIDE COVER HAS LOOSE HINGES. MAINTENANCE REPLACED THE TAIL CONE SLIDE CONTAINER IAW B717 AMM 25-61-02. INSTALLED SLIDE ON NEW SLIDE CONTAINER AND COMPLIED WITH ALL REQUIRED RII INSPECTIONS ON TAIL CONE SLIDE AND CONTAINER INSTALLATIONS. VERIFIED SAFETY PIN REMOVED AND STORED IN POUCH. VERIFIED ACTIVATION OF SLIDE PER AMDS 5352-4002. (LP #1521636)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,162 hrs · 35,981 cycles

THE AFT BULKHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY, MPN 803925-1, AND THE OPERATIONAL CHECK WAS GOOD. (LP #6321010)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,336 hrs · 35,404 cycles

CORROSION ON INTERCOSTAL BETWEEN STA 1002 AND STA 1022, FWD END. NRC 005-0001:21-0553-8-0817/022 00026: REPLACED INTERCOSTAL REF DWG #9958233. (LP #1151894)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,336 hrs · 35,404 cycles

STA 927-908 STRINGER 29L CORRODED. NRC 005-0001:21-0553-8-0817/014 00016: SPLICED IN NEW SECTION OF STRINGER REF DWG #5919707. (LP #1151743)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,336 hrs · 35,404 cycles

DUE TO CORROSION DAMAGE, SPLICE IN NEW SECTION OF STRINGER 30 FROM STA 900-1012. NRC 005-0001 21-0553-8-0817/025 00029: NEW SECTION OF STRINGER WAS SPLICED IN, IN REF SRM 53-20-05-2R. (LP #1151745)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,336 hrs · 35,404 cycles

INTERCOSTAL CORRODED BETWEEN STA 944 AND 954 JUST O/B OF S30 (M). NRC 005-0001:21-0553-8-0817/011 00013: REPLACED INTERCOSTAL REF DWG #9915578. (LP #1149950)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,336 hrs · 35,404 cycles

CLIP CORRODED ON AFT SIDE OF STA 944 BETWEEN S30 AND S29R. NRC 005-0001:21-0553-8-0817/005 00007: SPLICED IN NEW SECTION OF SHEAR CLIP REF SRM 53-00-06-2R-2 FIG 201. (LP #1150830)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,021 hrs · 36,654 cycles

THIS ER/A 527176-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV A. AT OR PRIOR TO 35,500 TOTAL AIRCRAFT FLIGHT CYCLES, AND REPETITIVELY THEREAFTER EVERY 4,000 FLIGHT CYCLES, ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. ASSOCIATED ER/A 00-527176 ADDED FOR AC 9519. PERFORMED DVI OF THE REPAIR EXTERNALLY AND INTERNALLY AS SHOWN IN FIG 2 AND 3 OF ERA 527176-14 REV A. QC 5123. HFEC INSPECTED PER ERA 527176-14 REV A SECTION II STEP 5, NO ITEMS NOTED. QC 4034. LFEC INSPECTED PER ERA 527176-14 REV A SECTION II STEPS 3 AND 4, NO ITEMS NOTED. QC 4034. C/W ERA 527176-14 REV A SECTION II. (LP #1128740)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,808 hrs · 34,988 cycles

BOTH AFT OVERWING EMERGENCY EXIT LIGHT VERTICAL STRIPS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY PACK IAW B717 AMM 33-51. EMERGENCY LIGHTS OP NORMAL. (LP #5836814)

Part: LIGHT — MISSING (SEAT 1B) · airframe 49,899 hrs · 34,375 cycles

EMERGENCY PATH LIGHT STRIP ON FLOOR BY SEAT 1B IS MISSING. REPLACED EMERGENCY PATH LIGHT STRIP PER B717 AMM 33-51. (LP4717872)

Part: COVER — MISSING (EXIT SIGN) · airframe 49,580 hrs · 34,129 cycles

EXIT COVER LIGHT MISSING AT FIRST CLASS LAVATORY. MAINTENANCE REPLACED THE EXIT SIGN LIGHT COVER AT FIRST CLASS LAVATORY PER AMM 33-51. OK FOR SERVICE. (LP 5130810)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 49,206 hrs · 33,886 cycles

THE INTERIOR EMERGENCY EXIT LENS WAS DAMAGED. MAINTENANCE INSTALLED A NEW LENS. AIRCRAFT RETURNED TO SERVICE.

Part: COWLING — CRACKED (NR 1 ENGINE) · airframe 48,817 hrs · 33,618 cycles

CRACKS ON INLET COWL BULLNOSE AROUND FASTENERS IN INTERIOR MARKED. REPLACED NR 1 ENGINE INLET COWL REF AMM 71-11-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,817 hrs · 33,618 cycles

CRACK INDICATION ON O/W EXIT FRAME RT SIDE STA 715. REPLACE OVERWING FRAME AT STA 715 RT REF CARD 5310-01436-03B.

Part: VANE — GOUGED (TE FLAP) · airframe 48,817 hrs · 33,618 cycles

LEFT WING OUTBD END OF FWD FLAP FIXED VANE L/E HAS DAMAGE (GOUGED). INSTALLED SAME O/B FIXED VANE AFTER SHOP VISIT PER AMM TASK 27-50-02.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 45,375 hrs · 31,233 cycles

DURING L1 DOOR SLIDE CHANGE, FOUND CONTAINER LANYARD BROKEN. REPLACED THE LANYARD IAW MM 25-61. OK FOR SERVICE.

Part: PAN — CHAFED (CABIN DOOR) · airframe 43,787 hrs · 30,063 cycles

AFT CABIN DOOR LOWER INTERIOR HAS CHAFE DAMAGE TO DOOR PAN & FRAMEWORK 8" FROM BOTTOM OF DOOR OPPOSITE HINGES. REPAIRED CHAFE DAMAGE TO DOOR PAN & FRAME WORK ON AFT CABIN EXIT DOOR IAW SRM 52-10-02, REPAIR 15.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

3 FORMERS ON LT SIDE OF FUSELAGE IN CANTED KEEL AREA AT FS 679, FS 694, AND FS 715 ARE CRACKED, MARKED. REPAIRED FORMERS AT FS 679, FS 694, AND FS 715 IAW ER/A 545683-14MA ORIGINAL REVISION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

RIGHT FUSELAGE EXTERIOR SKIN CRACKED AROUND FASTENER HEAD STA 1095 JUST ABOVE LONGERON 14R. REPAIRED RT FUSELAGE EXTERIOR SKIN AT STA 1095 AND LONGERON 14R IAW ER/A 547486-14, ORIGINAL REV ASSOCIATED ER/A 00-547486.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

CUSP WEB ANGLE CORRODED IN BOTH FWD AND AFT CORNERS ON RT GALLEY SERVICE DOOR. REPAIRED CUSP WEB ANGLE IAW SRM 53-00-55, REP 3.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

STA 1002, HORIZONTAL CLOSEOUT WEB CORRODED NEAR PANEL ATTACH STRUCTURE. BLENDED NOTED AREA IAW SRM 51-10-02, PAR 26, ORIG .040, .026. REMAINING FOUND TO BE OUT OF LIMITS, REPAIRED AREA IAW PRI 547489-14, TAG 6785 AND ER/A 547489-14, TAG 1482284 IAW PRI 547789-14. ASSOCIATED ER/A 54-748914, ADDED FOR AC 9519.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,484 hrs · 30,605 cycles

CUSP MEMBRANE AT STA 160-200 RBL 55 HAS CORROSION OUT OF LIMITS. REPAIRED CUSP MEMBRANE AT STA 160-200 IAW ER/A 547490-14 REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

DURING REMOVAL OF L17R FOUND CRACK ON FRAME AT STA 1037, L17R. REPAIRED CRACKED FRAME AT STA 1037 L-17R IAW SRM 53-20-07, REPAIR 4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

RIGHT FUSELAGE, STA 1022, BULKHEAD SHEAR TIE CRACKED IN UPPER RADIUS JUST BELOW LONGERON 16R. REMOVED SHEAR TIE, FABRICATED ATTACH ANGLE, INSTALLED ATTACH ANGLE AND NEW SHEAR TIE IAW SRM 51-41-02 AND PRI 547496-14, REV 0 AND ER/A 547496-14.

Part: CUSP WEB — CRACKED (BS 245) · airframe 43,787 hrs · 30,063 cycles

FOUND CUSP WEB CRACKED FROM EOP TRAVELING INBOARD TO LIGHTNING HOLE AT BS 245. CUT OUT THE DAMAGE & REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,484 hrs · 30,605 cycles

FO'S AFT O/B SEAT TRACK IS CORRODED. REPLACED FO'S AFT O/B SEAT TRACK IAW ER/A 547488-14 REV O.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,484 hrs · 30,605 cycles

CUSP WEB CORRODED FROM STA 200-STA 218. FABRICATED NEW CUSP WEB MEMBRANE AT FS 200-218 RBL 25-56 IAW SRM 53-10-51 FIG 1 AND 51-40-08 AND PER SAMPLE INSTALLATION OF WEB WILL BE INSTALLED ON NRC 200-0049.

Part: PAN — CRACKED (GALLEY DOOR) · airframe 43,787 hrs · 30,063 cycles

GALLEY SERVICE DOOR INTERNAL PAN TO WEB IS CRACKED. REPAIRED THE PAN IAW SRM 52-00-00 REP 3.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,787 hrs · 30,063 cycles

DURING REMOVAL OF SHEAR TIE AT BS 1022, FOUND LONGERON 16R CRACKED. REPAIRED THE LONGERON .

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

CORROSION ON AFT SIDE OF FRAME 446 AT LONGERON 30. ALSO, TOOLING MARKS ON AFT SIDE OF FRAME 446 FROM LONG 27, LT TO 27 RT. CORROSION ON FRAME AT STA 446, L30. REMOVED AND BLENDED IAW SRM 53-00-00, FIG 103, TOOL MARKS AT STA 446 L27, LT TO 27 RT BLENDED IAW SRM 53-00-00, FIG 103. ORIGINAL MATERIAL THICKNESS 0.050" IAW SRM 53-20-07, ID 1, 0.002" MATERIAL THICKNESS REMOVED. 0.048" MATERIAL REMAINING WITHIN LIMITS. FORMER AT STA 446, L30 FOUND TO BE CRACKED, REPAIRED IAW SRM 53-00-06, REPAIR 3 AND FABRICATED IAW DWG 9912454. HEAT TREATED TO T-6. CLIP AT STA 446, L30 REQUIRED FABRICATION DUE TO DOUBLER. FABRICATED IAW DWG 2913743.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

DURING REMOVAL OF SHEAR TIE AT STA 1022, FOUND LONGERON 17R CRACKED. REPAIRED DAMAGE BY REMOVING DAMAGE SECTION OF LONGERON 17R AT FS 1016- 1053 AND REPLACING WITH SECTION OF LONGERON EXTRUSION AND SPLICE ANGLE IAW SRM 53-00-05, REPAIR 2, FIG 201. APPLIED LOG DECAL IAW DPS 900-5-1, NR 4. SPLICE ANGLE WHERE HEAT TREATED ON WO 96008-0006.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

RIGHT SEAT TRACK CORRODED BEYOND LIMITS AT STA 896-902, RBL 22. REPLACED RT SEAT TRACK AT STA 898-1022, RBL 22 IAW SRM 51-41-05, PG 17, STEP 8 AND SRM 51-41-01, STEP 6.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

FLOOR SUPPORT AT STA 160, RBL 46-52 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 AND SRM 51-40 08, BEYOND LIMIT IAW SRM 53-00-00, PG 105, FIG 103. FLOOR SUPPORTS WILL BE INSTALLED ON 69007-0200-0089. JOB COMPLETE.

Part: SHEAR TIE — CORRODED (BS 1002) · airframe 43,787 hrs · 30,063 cycles

SHEAR TIE CORRODED BS 1002 BETWEEN LONGERON 29-30L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

FLOOR SUPPORT AT STA 200, RBL 10-43 IS CORRODED AT MARKED LOCATIONS IN SIDE CHANNEL. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-08 & DWG 9936534. PART BEYOND LIMIT IAW SRM 53-00-00, PG 105 FIG 103. FLOOR SUPPORTS TO BE INSTALLED ON NON-ROUTINE 69007-200-0049. JOB COMPLETE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

FLOOR SUPPORT AT STA 160-200, RBL 43 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 & SRM 51-40-08, BEYOND LIMITS IAW SRM 53-00-00, PG 105, FIG 103. JOB COMPLETE. FLOOR SUPPORTS TO BE INSTALLED ON 69007-0200-0049.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,787 hrs · 30,063 cycles

FLOOR SUPPORT AT STA 180, RBL 43 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 AND SRM 51-40-08, BEYOND LIMITS IAW SRM 53-00-00, PG 105, FIG 103. FLOOR SUPPORTS TO BE INSTALLED ON NON-ROUTINE 69007-200-0049.

Part: CUSP WEB — CRACKED (BS 661) · airframe 43,787 hrs · 30,063 cycles

CUSP WEB CRACKED FROM LIGHTING HOLE OTBD SEAT TRACK BS 661. REMOVED AND REPLACED THE CUSP WEB IAW SRM 53-00-55.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

CRACKED SHEAR TIE AT BULKHEAD STA 1022 BETWEEN LONGERON 13LT AND 14LT. REPLACED CRACKED FORMER, SHEAR TIE AT FS 1022 BETWEEN LONGERON 13L AND 14L WITH FORMER, SHEAR TIE IAW SRM 51-41-05 AND 51-41-02. APPLIED LOG DECAL IAW DPS 900-5-1, NR 04.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

LEFT CUSP WEB CRACKED AROUND 3 RIVETS, STA 589, LBL 44.5, VIEWED FROM TOP WITH MIRRIOR. REPAIRED CRACKS AROUND 3 RIVETS AT STA 589, LBL 44.5 IAW SRM 53-00-55, REPAIR 4, FROM 7075-T6 .032 AND 7075-T6 .020 FILLER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,787 hrs · 30,063 cycles

FORWARD CARGO FUSELAGE STA 636, BL0 AFT ANGLE ON INTERCOSTAL IS CRACKED, MARKED. REMOVED CRACKED END OF INTERCOSTAL AT STA 636, BLO. FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW DWG 9936580, REV B2 AND SRM 51-70-11, REP 1, FIG 201.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 1 NACELLE) · airframe 42,527 hrs · 29,088 cycles

THE CREW DIVERTED THE AIRCRAFT TO CHS AFTER THE NR 1 ENGINE SHOWED A MOMENTARY FIRE INDICATION, WHICH EXTINGUISHED ON IT'S OWN. THE THROTTLE WAS BROUGHT TO IDLE AND NO EXTINGUISHING AGENT BOTTLES WERE DISCHARGED. MAINTENANCE PERFORMED A TEST OF THE FIRE WARNING SYSTEM AND ALL CHECKS WERE GOOD. ALL FIRE WARNING LOOP RESISTANCES ARE WITHIN MM LIMITS. AN ENGINE RUN-UP WAS PERFORMED AND ALL PNEUMATIC DUCTS WERE CHECKED, NO TROUBLE FOUND. THE FDCU WAS REPLACED AND THE FINAL FIRE WARNING TEST WAS SATISFACTORY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,922 hrs · 28,629 cycles

DURING LINE CHECK, EMERGENCY EXIT SIGN ON CEILING AFT OF FWD GALLEY L2-791 DID NOT ILLUMINATE WHEN TESTED. REPLACED EMERGENCY LIGHT BATTERY PACK B5-259 IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,045 hrs · 27,886 cycles

EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY IN POWER SUPPLY ABOVE ROW 25 RT IAW AMM 33-51.

Part: SHEAR TIE — DAMAGED (BS 120) · airframe 41,044 hrs · 27,885 cycles

DURING CHECK IN MSP SHEAR TIE DAMAGED AT STA 120 ABOVE LONGERON 20. REPAIRED IAW SRM 53-00-06.

Part: SHEAR TIE — DAMAGED (BS 148) · airframe 41,044 hrs · 27,885 cycles

DURING CHECK, FOUND SHEAR TIE DAMAGED AT BS 148.55 ABOVE LONGERON 20. INSTALLED REPAIR IAW SRM 53-00-06 AND SRM 53-00-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,017 hrs · 27,867 cycles

OVERWING SLIDE DOORS, LT AND RT FWD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FWD OVERWING EXIT DOOR LIGHTS, LT AND RT SIDES IAW AMM 33-51. OPS CHECK NORMAL. LP 6980176.

Part: LIGHT — NOT SEATED (TAILCONE) · airframe 38,896 hrs · 26,135 cycles

TAIL COMPARTMENT AFT HANDRAIL EMER LIGHT INOPERATIVE. RESEATED LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF ADJUST (TAILCONE) · airframe 38,896 hrs · 26,135 cycles

TAIL CONE SLIDE PRESS INDICATOR NOT VISIBLE. R & R SLIDE ASSEMBLY IAW MM.

Part: MOUNT BRACKET — BROKEN (CABIN) · airframe 38,896 hrs · 26,135 cycles

FORWARD CTR AISLE EMER LIGHT MOUNT BRACKET BROKEN. SECURED LIGHT IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 38,895 hrs · 26,134 cycles

CEILING PANEL EMER LIGHT LENS CRACKED. R & R LENS IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 38,895 hrs · 26,134 cycles

AFT LT LAVATORY EXIT SIGN CRACKED. R & R SIGN IAW MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

RIGHT BELOW AFT EXIT DOOR FITTING CORRODED AT BS 1053, RBL 24. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, LBL 9. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO BS 200, LBL 8. R & R SUPPORT IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

C1 DOOR JAMB CORRODED. R & R JAMB IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 KF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: CLOSEOUT PANEL — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

FORWARD GALLEY SERVICE DOOR LOWER CUT OUT FWD CLOSE OUT PANEL CORRODED. REPAIRED PANEL IAW SRM & DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

DOUBLER CORRODED AT LONGERON 30 EACH SIDE OF VERTICAL STIFFENER. REPAIRED DOUBLER IAW SRM & DWG.

Part: SUPPORT — CORRODED (R1 DOOR) · airframe 38,895 hrs · 26,134 cycles

R1 DOOR LOWER JAMB AREA FWD GIRT BAR FITTING SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221ALF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221CF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 222DF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 222FF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221DF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 EF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 BF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 FF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 JF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,895 hrs · 26,134 cycles

MAIN CABIN FLOORBOARD 221 RF DELAMINATED. R & R FLOORBOARD IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,895 hrs · 26,134 cycles

FRAME CORRODED AT BS 908, LONGERON 30R. REPAIRED FRAME IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,170 hrs · 26,321 cycles

LEFT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BULB IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,170 hrs · 26,321 cycles

RIGHT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BULB IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 38,570 hrs · 25,930 cycles

FWD OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 37,860 hrs · 25,484 cycles

AFT FLASHLIGHT INOPERATIVE. R& R BATTERY IAW MM.

Part: LANYARD — DETACHED (R1 DOOR) · airframe 36,783 hrs · 24,797 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT NOT ATTACHED TO THE SLIDE. REATTACHED LANYARD IAW AMM.

Part: LATCH — LOOSE (R1 DOOR) · airframe 36,565 hrs · 24,655 cycles

R1 DOOR EMERGENCY EVAC SLIDE LATCH LOOSE. SECURED LATCH IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,423 hrs · 24,568 cycles

EMERGENCY EXIT SIGN IN BUSINESS CLASS LOOSE. SECURED LIGHT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,997 hrs · 24,312 cycles

FORWARD FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,240 hrs · 23,836 cycles

BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CUSP ANGLE CRACKED AT RIGHT SIDE BS 657. REMOVED AND REPLACED ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

RIGHT CUSP WEB CRACKED AT BS 653. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 674 TO BS 696. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FOUND CORROSION AT FWD CORNER CUSP WEB AT BS 462, RBL 59.0. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CUSP WEB CRACKED AT RIGHT BETWEEN STA 696 TO STA 675, L18. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

RIGHT CUSP WEB CRACKED AT BS 655, L18. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 35,240 hrs · 23,836 cycles

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

Part: RUB STRIP — CORRODED (RT WING) · airframe 35,240 hrs · 23,836 cycles

RIGHT WING UPPER CUTOUT FOR ACCESS PANEL 620FT, MATING SURFACE RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP PER SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 35,240 hrs · 23,836 cycles

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

Part: RUB STRIP — CORRODED (RT WING) · airframe 35,240 hrs · 23,836 cycles

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

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CRACK METAL FLOOR PANEL 222EE RBL 44.5 AROUND STA 450. REMOVED AND REPLACED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FUSELAGE SKIN CRACKED AT BS 899, LONGERON 28. REPAIRED SKIN PER SRM.

Part: STRIP — CRACKED (TE FLAP) · airframe 35,240 hrs · 23,836 cycles

RIGHT WING NR 3 FLAP AFT FAIRING IS CRACKED AT FWD INBD EDGE. REMOVED AND REPLACED STRIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FRAME CRACKED AT BS 696, RBL 54.5. REMOVED AND REPLACED FRAME IAW DWG AND SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CORROSION CUSP WEB BETWEEN STA 715 TO STA 696, LBL 59.0. REMOVED AND REPLACED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CORROSION CUSP WEB RIVET LINE STA 389-408 RBL 54.0. REMOVED AND REPLACED WEB IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CORROSION ON REPAIR DOUBLER AT CUSP WEB AND FUSELAGE SKIN STA 591, LBL 59.0. REMOVED AND REPLACED SPLICE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

CORROSION CUSP WEB BETWEEN STA 674 TO STA 655, LBL 59.0. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,979 hrs · 24,302 cycles

EXTERNAL FUSELAGE SKIN CORRODED AT STA 860, LONGERON 28 LT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FUSELAGE FRAME CRACKED AT STA 674, LBL 54.5. REMOVED AND REPLACED FRAME PER SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 35,240 hrs · 23,836 cycles

RIGHT WING BONDING STRAPS CRACKED AT BL 58.00. REMOVED AND REPLACED STRAPS IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FRAME CORRODED AT BS 927, BETWEEN LONGERON 30L TO 29L. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FRAME CORRODED AT BS 908, L30. REMOVED AND REPLACED FRAME IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 35,240 hrs · 23,836 cycles

FORWARD CARGO DOOR EXTERNAL SURROUND LOWER JAMB PAN CORRODED. REMOVED AND REPLACED PAN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,979 hrs · 24,302 cycles

FRAME CORRODED AT BS 908, LONG 30. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 35,665 hrs · 24,104 cycles

ONE BULB OUT OVERHEAD COCKPIT EMERGENCY LIGHTS. REMOVED AND REPLACED BULB REF AMM 33-51.

Part: ACTUATOR — MALFUNCTIONED (RT MLG DOOR)

MOMENTARY GEAR DOOR OPEN LEVEL 2 ALERT ON EXTENSION. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR, REF B717 AMM 32-34.

Part: LANYARD — BROKEN (GIRT BAR)

FWD SERVICE DOOR GIRT BAR LANYARD HAS SEVERAL BROKEN STRANDS. REPLACED GIRT BAR LANYARD IAW AMM 25-61.

Part: SKIN — DENTED (HORIZ STAB)

RIGHT HORIZONTAL STAB LEADING EDGE SKIN, DENTED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 55-10-01 FIG 201 AND EA 17-55-02825IR.

Part: FAIRING — CRACKED (FUSELAGE)

RIGHT FWD VERTICAL STAB TO FUSELAGE FAIRING, CRACKED. ACCOMPLISHED FAIRING DOUBLER REPAIR PER B717 SRM 53-00-00 FIG 201 REPAIR 1 AND B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 12 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 655, CRACKED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 53-20-15.

Part: SUPPORT — CORRODED (FUSELAGE)

CABIN SIDEWALL SUPPORT, STA 200, RBL 59, CORROSION. ACCOMPLISHED SIDEWALL SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 26, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: ANGLE — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR, O/B FWD CORNER BELOW LATCH "Z" ANGLE, CRACKED. ACCOMPLISHED "Z" ANGLE DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: PANEL — CORRODED (FUSELAGE)

GALLEY ENTRANCE DOOR JAMB GAP PANEL, STA 160 TO 200, CORROSION. ACCOMPLISHED DOOR JAMB GAP PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: SUPPORT FITTING — CRACKED (FUSELAGE)

PASSENGER ENTRANCE DOOR LINER SUPPORT FITTING, CRACKED. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, RBL 29 TO RBL 49, CORROSION. ACCOMPLISHED FLOOR WEB FILLER AND DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: WEB — CRACKED (FUSELAGE)

CABIN LONGERON FINGER WEB, STA 200, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB FILLER AND DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 199 TO 256, LBL 17, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: WEB — CRACKED (FUSELAGE)

CABIN FLOOR WEB, STA 217, RBL 46, CRACKED. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 13 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, LBL 26, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 12 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LIGHT — MISSING (CABIN)

ON SEAT 1D ONE WHITE EMERGENCY ESCAPE PATH LIGHT ASSY IS MISSING ITS LENS COVER AND ONE BULB IS MISSING. INSTALLED EPL COVER AND BULB. OPS CHECK OK REF MM CH 33-50.

Part: SIGN — BROKEN (CABIN)

EXIT SIGN BETWEEN BINS ABOVE ROW 1 BROKEN. SECURED EXIT SIGN LENS ABOVE ROW 1. REFER AMM 33-51.

Part: SIGN — MISSING (CABIN)

EXIT SIGN ABOVE R-1 DOOR MISSING. REPLACED LENS COVER REF 25-60.

Part: LIGHT — INOPERATIVE (CABIN)

THE 21D AFT EMERGENCY EXIT LIGHT ON SEAT INOP. REMOVED AND REPLACED E-PATH LIGHT ASSEMBLY AT SEAT 21D IAW AMM 33-51-04. OPS CHECK GOOD.

Part: ENGINE — SHUTDOWN (LEFT)

IN CRUISE, NR 1 ENGINE AUTO-SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE IAW AIRTRAN TASK CARD 603.

Part: SKIN — DAMAGED (FUSELAGE)

AFT BAG BIN THRESHOLD STRUCK BY BELT LOADER. FABRICATED DOUBLER REPAIR. MAT USED -071-2024-T3 X 34 " X 29". TRIPLER REPAIR .080-7075-T6 X 32 " X 33 1/2". QUADRUPLEX REPAIR .100-2024-T3 X 22" X 30 1/2" IAW EA 17-53-01078A SECTION 2.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 DOOR LANYARD SLIDE PIN OUT. REMOVED AND REPLACED L1 SLIDE REF M/M 26-61.

Part: FRAME — CRACKED (FUSELAGE)

FOUND CRACK AT LT AFT FUSELAGE CANTED FRAME AT FASTENER HOLE AT STA Y-1178.225 CANT, LONG 14-6. INSTALLED DOUBLER ANGLE REPAIR AT LT CANTED FRAME AT STA Y-1178.225 CANT L-14-L, IAW SRM 51-70-11. MATERIAL USED .080 7775-0 SIZE 2.5" X 9.5", HEAT TREATED DOUBLER TO T6 PER AVBORNE G-PS 98PMS.247PS-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

ROW 12 EMERGENCY AISLE LIGHT IS OUT. REPAIR LOOSE CONNECTOR, OPS CHECK GOOD IAW MM 33-51.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

BATTERY PACK AT B5-119 FOR EMERGENCY PATH LIGHTING WOULD NOT ILLUMINATE. REPLACED BATTERY ASSEMBLY, OPS CHECK GOOD. SUSPECT FUSE AT PIN 10 IS BLOWN.