N985AT

Part: NONE — NONE (NONE) · airframe 57,414 hrs · 41,492 cycles

TRACKING FOR ACCOMPLISHMENT OF ER/A 615647-14AD. ACCOMPLISHMENT OF ER/A 615647-14A (1377242)

Part: SKIN — DAMAGED (ZONE 300) · airframe 57,414 hrs · 41,492 cycles

ERA 630089-14, SECTION I, ISSUED FOR BIRD STRIKE DAMAGE TO RT HORIZONTAL STAB LEADING EDGE INBD STRUCTURE. REPAIRED IAW ER/A 630089-14. (1269533)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 56,997 hrs · 41,135 cycles

CREW REPORT EXIT SIGN F/C INOP (EMERRGENCY LIGHT). FOUND BATTERY PACK B5-259 INOP, REPLACED BATTERY PACK. OPS CHEC K GOOD, IAW B717AMM 33-51. (7585679)

Part: DOOR — OPEN (ZONE 700) · airframe 56,900 hrs · 41,048 cycles

ATB- PERFORMED AN AIR TURN BACK DUE TO A NOSE GEAR AREA VIBRATION. MAINTENANCE CLOSED THE NOSE GEAR DOORS, CONFIRMED THE SECURITY AND CONDITION OF THE DOORS AND SURROUNDING AREA AND RETURNED TO SERVICE.(7585642)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,957 hrs · 40,179 cycles

EMERGENCY LIGHTS OVERWING EXIT AND CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE FOUND B5-230 BATTERY PACK NOT WORKING. THE BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7173480)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 55,888 hrs · 40,112 cycles

THE OVERHEAD CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 24-28. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY B5-231 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7173431)

Part: CONTROLLER — FAULTED (ZONE 100) · airframe 55,537 hrs · 39,789 cycles

SHIP 9585 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO A "TAIL ANTI-ICE MANIFOLD FAIL" MESSAGE ILLUMINATING ABOUT 20 MINUTES FROM LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PODS CONTROLLER PER B717 AMM 36-23. RTS TEST WAS GOOD. FOUND CORROSION ON WIRE SOCKET ON D1-1023. REPLACED SENSOR D1-1023 PER B717 AMM 36-23. PERFORMED DUCT LEAK CHECKS PER B717 AMM 30-10. NO LEAKS NOTED. TAIL IP RESISTANCE READS 15 OHMS TOTAL. (LP #6507512)

Part: A/C PACK — SMOKE (ZONE 100) · airframe 55,453 hrs · 39,704 cycles

SHIP 9585 -ATB/SMKE/DE- THE CREW RETURNED THE FLIGHT BACK TO SDF DUE TO VISIBLE SMOKE AND ODOR IN THE MAIN CABIN. CORRECTIVE ACTION: MAINTENANCE ISOLATED THE SOURCE TO THE LEFT PACK SYSTEM WITH APU OR ENGINE AIR. PLACED LEFT PACK ON MEL. (LP #6779456)

Part: A/C PACK — ODOR (ZONE 100) · airframe 55,453 hrs · 39,704 cycles

SHIP 9585 -ATB/SMKE/DE- THE FLIGHT CREW AND CABIN CREW BOTH REPORTED SMOKE IN COCKPIT AND CABIN SOON AFTER TAKEOFF. AN EMERGENCY WAS DECLARED WITH ATC AND THE AIRCRAFT RETURNED TO ATL. CORRECTIVE ACTION: MAINTENANCE FOUND ODOR FROM PACKS WHEN RUNNING OFF APU BLEED AIR. REPLACED COALESCER BAGS AND PERFORMED DUCT BURN WITH APU AIR. NO ODOR DETECTED USING SNIFFER. RTS. (LP #6779448)

Part: BULKHEAD — MECHANIC ERROR (ZONE 100) · airframe 54,946 hrs · 39,262 cycles

-AD- ACCOMPLISH ER/A 551838-14AD REV A SECTION II FUSELAGE / BULKHEADS / CANTED STA 1178 FRAME / MISDRILLED HOLES. ACCOMPLISH ER/A 551838-14AD REV A SECTION II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-551838 ADDED FOR AC 9585. ACCOMPLISH ER/A 551838-14AD REV A SECTION II ALTERNATIVE INSPECTION FOR AD 2024-20-02. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 22NOV24 AND LOG COMMENTS. (LP #0650688)

Part: ACTUATOR — LEAKING (NLG) · airframe 54,526 hrs · 38,900 cycles

SHIP 9585 -DIV/FUME/DE- ENROUTE TO MDT THE FLIGHT WAS DIVERTED TO IAD FOLLOWING STRONG SULFUR FUMES THROUGHOUT THE COCKPIT AND CABIN. MAINTENANCE FOUND THE NOSE LANDING GEAR RETRACT ACTUATOR LEAKING HYDRAULIC FLUID. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (LP #6003184)

Part: SPAR — CRACKED (LT WING) · airframe 53,379 hrs · 37,902 cycles

CRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 61543-14 REV ORIG SECTION I AND II ACCOMPLISHED ON NRC 628 IN TOMX. NEEDS SECTION III ACCOMPLISHED. SUMMARY OF NRC 001-0002:0500-2000/001 00001: ACCOMPLISHED PERMANENT REPAIR PER ERA 615453-14 SECTION III PER ERA 615647-14 REV ORIG REF NRC 35. XFRD FROM LP #5518464. (LP #0240017)

Part: SKIN — CRACKED (LT WING) · airframe 53,379 hrs · 37,902 cycles

INSPECTION OF LOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (4 EA) COMMON TO LOWER WING SKIN DOUBLER AT XRS 164. 1 EACH IS OUTBOARD OF XRS 164, 3 EACH ARE INBOARD OF XRS 164. MARKED. COMPLIED WITH LH WING / REAR SPAR LOWER CAP / XRS=159 / CRACK ERA 615647-14AD REV ORIG SECTION I: PERMANENT REPAIR INSTRUCTIONS. ASSOCIATED ERA 41-746516 ADDED FOR AC 9585. (LP #0238101)

Part: SPAR CAP — CRACKED (LT WING) · airframe 53,379 hrs · 37,902 cycles

ERA 615647-14AD REV ORIG - LH WING REAR SPAR LOWER CAP AT XRS=159 IS CRACKED. COMPLIED WITH ERA 615647-14AD REV ORIG PRI "0", "1", "2", "3, "4", "5", "6", "7", "8", "9, "10", "11", AND "12" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ERA 615647-14AD REV ORIG PRI "0", "1", "2", "3", "4", "5", "6", "7", "8", "9", "10", "11", AND "12" INSTRUCTIONAL STEPS ARE COMPLETE AND MATCH FINAL LH WING REAR SPAR LOWER CAP AT XRS=159 CRACK ERA 615647-14AD REV ORIG SECTION I: PERMANENT REPAIR INSTRUCTIONS. ASSOCIATED ERA 41-746516 ADDED FOR AC 9585. (LP #0238111)

Part: SKIN — CRACKED (LT WING) · airframe 53,379 hrs · 37,902 cycles

LOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (3 EA) COMMON TO LOWER WING SKIN DOUBLER BELOW XRS164, ALONG INBOARD EDGE. MARKED. COMPLIED WITH LH WING / REAR SPAR LOWER CAP / XRS=159 / CRACK ERA 615647-14AD REV ORIG SECTION I: PERMANENT REPAIR INSTRUCTIONS. ASSOCIATED ERA 41-746516 ADDED FOR AC 9585. (LP #0238103)

Part: SPAR — CRACKED (LT WING) · airframe 53,379 hrs · 37,902 cycles

CRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 615453-14 AD REV ORIG SECTION I AND SECTION II ACCOMPLISHED ON NRC 7628 IN TOMX. NEEDS SECTION III ACCOMPLISHED XFRD TO NR #1 ATG WO PO51540620240205. (LP #5518464)

Part: INTERCOSTAL — CORRODED (BS 927-946) · corrosion level 2 · airframe 53,376 hrs · 37,901 cycles

CORROSION ON INTERCOSTAL OVER STRG 29R AND 28R BTW STA Y=927 TO 946 AT AFT CARGO CPMPARMENT. SUMMARY OF NRC 00271: CORROSION LEVEL 2. INTERCOSTALS OVER STRG 29R AND 28R BTW STA Y=927 TO 946 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0175803)

Part: FINGER DOUBLER — CORRODED (BS 944-1004) · corrosion level 2 · airframe 53,376 hrs · 37,901 cycles

CORROSION ON FINGER DOUBLER STA 944, 972, 1001, AND 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00194: CORROSION LEVEL 2. FINGER DOUBLER BTW STA 944 AND STA 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. PAR 8 FIG 23. (LP #0170531)

Part: WEB — CRACKED (BS 674) · airframe 53,376 hrs · 37,901 cycles

CRACK ON WEB STA Y=674 X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00311: WEB STA Y=674 X=55 AT PASSENGER CABIN WAS REPAIRED PER ERA 614715-14 REV ORIGINAL SECTION I PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24-MONTHS FROM 14JAN24 ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ERA) 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. UNDER LOG PAGE 0159095. ASSOCIATED ERA 14-614715 ADDED FOR AC 9585. (LP #0161195)

Part: WEB — CORRODED (BS 200-205) · corrosion level 2 · airframe 53,376 hrs · 37,901 cycles

CORROSION ON WEB BTW STA Y=200/205 AND L 18L AND L 17L AT DOOR JAMB L1. SUMMARY OF NRC 00304: CORROSION LEVEL 2. CORROSION ON WEB BTW STA Y=200/205 AND L 18L AND L 17L AT DOOR JAMB L1 WAS REPAIRED PER ERA 614628-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ERA 14-614628 ADDED FOR AC 9585. (LP #0162663)

Part: CUSP WEB — CORRODED (BS 579-756) · corrosion level 2 · airframe 53,376 hrs · 37,901 cycles

CORROSION ON CUSP WEB (UPPER AREA) BTW STA 579-598, 609-617, 658-678, AND 720-756 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00560: CORROSION LEVEL 2. CORROSION ON CUSP WEB (UPPER AREA) BTW STA 579-598, 609-617, 658-678, AND 720-756 AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 215 AND FIG 216. (LP #0161040)

Part: WEB — CRACKED (BS 182) · airframe 53,376 hrs · 37,901 cycles

CRACK WAS FOUND ON WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT. SUMMARY OF NRC 00607: WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP #0158141)

Part: WEB — CRACKED (BS 1200) · airframe 53,376 hrs · 37,901 cycles

CRACKS ON WEBS AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT. SUMMARY OF NRC 00238: WEB AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT WAS REPAIRED PER ERA 537343-14MA REV B, SECTION I, PERMANENT REPAIR. ASSOCIATED ERA 14-537343 ADDED FOR AC 9585. (LP #0158180)

Part: BEAM — CRACKED (NR 1) · airframe 53,376 hrs · 37,901 cycles

CRACKS ON BEAM #1, STA Y=200 AT PAX CABIN DOOR L1. SUMMARY OF NRC 00595: BEAM #1, STA Y=200 AT PAX CABIN DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7, FIGURE 201. (LP #0158063)

Part: WEB — CRACKED (UNKNOWN) · airframe 53,376 hrs · 37,901 cycles

CRACK ON WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00312: WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0155891)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,376 hrs · 37,901 cycles

CRACK ON CUSP WEB IN STA Y=713 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: CUSP WEB IN STA Y=713 AND X=55 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0152363)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,376 hrs · 37,901 cycles

CUSP WEB AT STA Y=928, BTW STA Y=920 TO STA Y=935, WAS FOUND CRACKED. SUMMARY OF NRC 00581: CUSP WEB AT STA Y=928 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIG 215. (LP #0151475)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,376 hrs · 37,901 cycles

CRACKS ON BEAM #1, STA Y=160 AND Y=200 AT PAX CABIN DOOR L1. SUMMARY OF NRC 00199: BEAM #1, STA Y=160 AT PAX CABIN DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7, PARAGRAPH 5, A TABLE 201, AND PARAGRAPH 6 B FIGURE 202. (CRACK TYPE A). (LP #0151416)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,376 hrs · 37,901 cycles

CORROSION ON PREVIOUS REPAIR CUSP WEB LH SIDE STA Y=542. SUMMARY OF NRC 00363: CORROSION LEVEL 2. PREVIOUS REPAIR CUSP WEB LH SIDE STA Y=542 WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 FIG 207 AND 51-41-02-0G. (LP #0140410)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,376 hrs · 37,901 cycles

MAINTENANCE FOUND THE KEVLAR CABLE FOR THE RELEASE MECHANISM INSIDE TAILCONE TO BE TORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00061: CABLE ASSEMBLY WAS REPLACED PER B717-200 AIPC 53-52-30-01 AND WAS INSTALLED PER AMDS 5352-2001. (LP #0124484)

Part: UNKNOWN — UNKNOWN · airframe 51,677 hrs · 36,355 cycles

THE AFT 3 CENTER AISLE CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY LIGHT BATTERY PACK ROW 24-29 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9989192)

Part: OIL SYSTEM — LEAKING (APU) · airframe 51,390 hrs · 36,095 cycles

SHIP 9585 -SMKE- DURING BOARDING WITH APU RUNNING PACKS, SMOKE AND ODOR FILLED THE CABIN. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE APU HAD FAILED AND DUMPED ALL ITS OIL ON THE GROUND. THE APU WAS REPLACED. THE COALESCER BAGS WERE THEN REPLACED AND A DUCT BURN WAS ACCOMPLISHED. MAINTENANCE ALSO HAND CLEANED THE DUCTING FROM THE WATER SEPARATOR. NO FURTHER ISSUES WERE FOUND, AND THE AIRCRAFT RETURNED TO SERVICE. (LP #4048900)

Part: UNKNOWN — UNKNOWN · airframe 50,455 hrs · 35,266 cycles

AIRCRAFT 9585, EMERGENCY LIGHT ABOVE FWD F/A SEAT INOP. CORRECTIVE ACTION: REPLACED BATTERY POWER SUPPLY PER B717 AMM 33-51, OPERATIONAL CHECK GOOD. ( LP 9051790)

Part: THERMOSWITCH — MISALIGNED · airframe 49,901 hrs · 34,737 cycles

SPARKS EMITTED FROM CA WINDSHIELD WHEN ANTI-FOG SWITCH TURNED ON. FWD TO B717 MEL 30-41-01A. 'M' PROC C/W. MEL/PLAC INSTALLED. OK FOR SVC. *********************MCC TECHNICIAN UPDATE********************** CA WINDSHIELD MPN 5912290-508 REF B717 IPC 56-11-01-01 ITEM 140. STK# 92-5610-4-0001 REF B717 AMM 56-11-02 FOR REMOVE/INSTALL. **************************************************************** AFTER CONSULTING WITH PREVIOUS MTC IT WAS DISCOVERED THE CAPTS WINDOW THERMOSWITCH S1-220 HAD BECOME DISLODGED FROM THE SPRING RETAINER, RESULTING IN WIRE TERMINAL COMING INTO CONTACT WITH THE SPRING RETAINER. CONFIRMED PROPER INSTALLATION OF THERMOSWITCH S1-220 PER B717 AMM 30-42-01-000-801. CAPTS WINDSHIELD ANTI-FOG OPS CHK GOOD PER B717 AMM 30-42-01-710-801. MEL CLEARED, PLACARD REMOVED, NO "M" PROCEDURES. LOG-PAGE UPDATED @ 07JUN22 0851 UTC ******************************************************************************* (LP #8640656)

Part: COMPRESSOR — STALLED · airframe 49,677 hrs · 34,527 cycles

SHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 103 KNOTS FOLLOWING THE #2 ENGINE COMPRESSOR STALL AFTER INGESTING A MYLAR BALLOON FLOATING OVER THE RUNWAY. CORRECTIVE ACTION: MAINTENANCE FOUND BALLOON DEBRIS IN THE TAIL PIPE. INSPECTION PERFORMED BORESCOPE PER AMM NO RESTRICTIVE DAMAGE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (LP #7195794)

Part: NONE — NONE · airframe 49,573 hrs · 34,425 cycles

SHIP 9585 - THE FLIGHT CREW SAFELY ABORTED THE TAKEOFF ROLL AT 100 KTS. DUE TO A "STAB TRIM" MESSAGE WITH AN AURAL WARNING. CORRECTIVE ACTION: MAINTENANCE FOUND VALUES MISSING FROM FLIGHT PLAN AND THE CMU NOT PROPERLY STORING DATA. THE CMU WAS REPLACED AND THE FUNCTIONAL TEST OF THE CMU PASSED. (LP #7195710)

Part: DOOR — CRACKED · airframe 49,542 hrs · 34,397 cycles

FOUND FWD CARGO DOOR CRACKED/ DAMAGED DURING PRESSURIZATION CHECK. SUMMARY SEE NRC 001-0051:5230-2004/004 00500: REPLACED CARGO DOOR PER B717 AMM 52-31-01. REMOVED AND REINSTALLED CARGO BARRIER PER B717 AMM 25-54-01. (LP #2179455)

Part: STRINGER — CRACKED · corrosion level 2 · airframe 49,542 hrs · 34,397 cycles

AFT CARGO COMPARTMENT, STRINGER 28L CORRODED FROM STATION 1010 - 1022. WORK WITH NRC 357: CORROSION LEVEL 2, REPLACED STRINGER 28L, SPLICE (1) AND CLIP (1) FROM STA. 898.500 TO STA. 1053 IAW B717 SRM 53-20-05-01 AND 53-00-05-2R PROCEDURE 2. REFER TO NR 434 AND NR357 ITEMS 1 TO 17. (LP #2177859)

Part: STIFFENER — CORRODED · corrosion level 2 · airframe 49,542 hrs · 34,397 cycles

AFT CARGO COMPARTMENT STA 1053, VERTICAL STIFFENER, AFT SIDE OF BULKHEAD AT STRINGER 29L CORRODED AT LOWER TIP. MARKED. CORROSION LEVEL 2, REPLACED STIFFENER PER DOUGLAS LONG BEACH B717 DWG 9915561 AND B717 SRM 51-41-00. REF NR 365. (LP #2177980)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT, STA 927 SHEAR TIE, OUTBOARD OF STRINGER 29L CORRODED ON LOWER LEG. MARKED. SUMMARY SEE NRC 046-0008:5331-2001/004 00348: CORROSION LEVEL 2, REPAIRED SHEAR TIE AFT CARGO COMPARTMENT, STA 927, OUTBOARD OF STRINGER 29L IAW B717SRM 53-00-06-2R PROCEDURE 2. (LP #2177063)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT, SHEAR TIE, LOWER LEG AT STA 1002 CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/014 00358: CORROSION LEVEL 2, INSTALLED REPAIR SHEAR TIE PER B717 SRM 53-00-06-2R PROCEDURE 2. (LP #2177318)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO STA 1002, OUTBAORD OF STRINGER 28L, INTERCOSTAL CORRODED NEAR SKIN. SUMMARY SEE NRC 046-0008:5331-2001/037 00435: CORROSION LEVEL 2, REPLACED INTERCOSTAL PER B717 SRM 51-41-00. (LP #2177265)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT SHEAR TIE CLIP AT STA 974 BETWEEN STRINGER 30 AND 29R CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/010 00354: CORROSION LEVEL 2, REPAIRED PER B717 SRM 53- 00-06-2R PROCEDURE 2. (LP #2177068)

Part: SPLICE — CORRODED · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO STATION 895.500 SPLICE STRAP CORRODED ON BOTH SIDES OF STRINGER 30. MARKED. SUMMARY SEE NRC 001-0374:5231-2002/006 00344: COMPLIED WITH ER/A 598215-14 REV. ORIGINAL, CORROSION LEVEL 2, REPAIRED PER PRI 598215-14 REV O AND REV. 1 AND ER/A 598215-14 REV. ORIGINAL. (LP #2177166)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT, SHEAR TIE AT STA 1022 (AFT BULKHEAD) CORRODED BETWEEN STRINGERS 29R - 29L. SUMMARY SEE NRC 046-0008:5331-2001/016 00360: CORROSION LEVEL 2, INSTALLED REPAIR PARTS PER B717 SRM 53-00-06-2R PROCEDURE 2. (LP #2177210)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT, STRINGER 28L CORRODED FROM STATION 994-1010. SUMMARY SEE NRC 046-0008:5331-2001/013 00357: CORROSION LEVEL 2, REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2177188)

Part: NONE — NONE · airframe 49,538 hrs · 34,395 cycles

ROBBED PASSENGER ROW 21, R WINDOW PANE INNER AND OUTER SERVICEABLE. SUMMARY SEE NRC 001-0311:5620-2001/003 00006: REPLACED WINDOW PANE PER B717 AMM 56-20-01. PERFORMED LEAK CHECK PER AMM 56-20-01, NO LEAKS FOUND. (LP #2176984)

Part: RETAINER — CRACKED · airframe 49,538 hrs · 34,395 cycles

FOUND RETAINING CLIP CRACKED ON TAILCONE EXTERNAL RELEASE HANDLE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 038-0001:5352-2001/002 00485: REPLACED RETAINING CLIP REF B717 AMM 53-52-01. FUNCTIONAL TEST WILL BE COMPLETED ON AMDS 5352-2001. (LP #2176928)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO STA 1022 AFT SIDE OF FRAME CORRODED BETWEEN 29RT AND 29LT. SUMMARY SEE NRC 046-0008:5331-2001/027 00424: INSTALLED REPAIR PARTS PER B717 SRM 53-20-07-2R, PROCEDURE 3. (LP #2177194)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO COMPARTMENT, 3 EACH SKIN SPLICE PLATES BETWEEN STATIONS 1015 - 1037 BETWEEN STRINGERS 29R - 29L CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/015 00359: CORROSION LEVEL 2, REPLACED SKIN SPLICES PER B717 SRM 53-03-01 REPAIR 1. (LP #2177215)

Part: NONE — NONE · corrosion level 2 · airframe 49,538 hrs · 34,395 cycles

AFT CARGO STRINGER 30 BETWEEN STATIONS 1022-1037 CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/017 00363: CORROSION LEVEL 2, REPLACED INTERCOSTAL AT STA 1022-1037 PER B717 SRM 51-41-00. (LP #2177262)

Part: NONE — NONE · airframe 49,538 hrs · 34,395 cycles

RH MOVEABLE FLAP VANE HAS POSSIBLE DELAMINATION AT PREVIOUS DENT LOCATION. SUMMARY SEE NRC 019-0001:00-0557-8- 9290/001 00211: REPLACED RH FWD MOVEABLE VANE PER AMDS 2750-4010. ALL RII'S COMPLIED WITH ON AMDS 2750-4010. (LP #2175616)

Part: NONE — NONE · airframe 49,538 hrs · 34,395 cycles

RIGHT FLAP MOVEABLE VANE FOUND DAMAGE ON THE UNDERSIDE. "M". SUMMARY SEE NRC 001-0364:2753-2003/002 00332: REPLACED RH WING FLAP AFT VANE PER B717 AMDS 2750-4008. ALL RII'S COMPLIED WITH ON AMDS 2750-4008. (LP #2175615)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 49,542 hrs · 34,397 cycles

AFT CARGO COMPARTMENT STA 908 SHEAR TIE AT STRINGER 29R - 29L CORRODED. MARKED. SUMMARY SEE NRC 046-0008:5331-2001/001 00345: CORROSION LEVEL 2, REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2. (LP #2174601)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 49,542 hrs · 34,397 cycles

AFT CARGO COMPARTMENT STRINGER 30 BETWEEN STA 908 AND 974 CORRODED. MARKED. SUMMARY SEE NRC 046-0008:5331-2001/002 00346: CORROSION LEVEL 2, REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #2174608)

Part: SKIN — BUCKLED · airframe 49,542 hrs · 34,397 cycles

BUCKLED FUSELAGE SKIN AT POTABLE WATER DRAIN LOWER FUSELAGE STA 274-294. SUMMARY SEE NRC 047-0019:5310-2006/001 00210: REPAIRED PER B717 SRM 53-03-01-2R-1. (LP #2167669)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,286 hrs · 33,435 cycles

THE FORWARD GALLEY EMERGENCY LIGHTS AND THE FORWARD OVERWING EXIT IDENTIFIER EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-118 AND B5-235 IAW AMM 33-51. OPERATIONAL CHECK WA GOOD. (LP #6074402)

Part: TRAY — DIRTY (COMPUTER) · airframe 47,799 hrs · 33,113 cycles

SHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 110 KNOTS FOR A "TAKEOFF CONFIGURATION" WARNING DUE TO STAB TRIM. ALSO THE ENGINE DISPLAY BLANKED FOR 4 SECONDS. CORRECTIVE ACTION: MAINTENANCE FOUND DUST IN BOTH OF THE VIA COMPUTER TRAYS. THE TRAYS WERE CLEANED AND BOTH VIA COMPUTERS WERE REPLACED. (LP #5973322)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,752 hrs · 33,081 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHT FROM ROW 23-29 IN OP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER AMM 33-51 AND OPS CHECK GOOD. A/C OK FOR SERVICE. (LP5973324)

Part: SMOKE DETECTOR — NO TEST · airframe 46,295 hrs · 32,022 cycles

LH SMOKE DETECTOR FAILED TEST ON AMDS CARD 2614-2001. REMOVED AND REPLACED SMOKE DETECTOR REF B717 AMM 26-14-01. (LP0841369)

Part: UNKNOWN — UNKNOWN (EMEGENCY LIGHT) · airframe 45,030 hrs · 31,134 cycles

THE OVERHEAD EMERGENCY LIGHTS AT ROW 3, 12, 15, 18, 22, 26, AND AFT LAVATORY AREA WERE INOPERATIVE. OPS TESTED NORMAL AMM 33-51. AIRCRAFT OKAY FOR SERVICE.

Part: ENGINE — SEIZED (NR 1) · airframe 44,715 hrs · 30,873 cycles

THE CREW SAFELY ABORTED TAKEOFF AT 120 KNOTS, FOLLOWING A NR 1 ENGINE COMPRESSOR STALL. MAINTENANCE FOUND THE NR 1 ENGINE SEIZED AND METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,750 hrs · 29,507 cycles

MID CABIN EXIT SIGN LENS MISSING. REPLACED EXIT SIGN LENS. CHECKED GOOD.

Part: LONGERON — DAMAGED (BS 351) · airframe 41,630 hrs · 28,708 cycles

FOUR HOLES OUT OF ROUND IN LONGERON 30, FWD OF BS 351 COMMON TO ANTENNA DOUBLER. REPAIRED IAW ER/A 554839-14 REV 0.

Part: LONGERON — DAMAGED (BS 994) · airframe 41,630 hrs · 28,708 cycles

TWO HOLES OUT OF ROUND IN LONGERON 30, FWD OF BS 994 COMMON TO ANTENNA DOUBLER. REPAIRED IAW ER/A 554839-14.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

AFT CARGO DOOR CUTOUT CORRODED ON LOWER SIDE UNDER LOWER SCUFF PLATE. CLEAN UP CORROSION ON AFT CARGO DOOR CUTOUT ON INTERNAL DOUBLER IAW SRM 53-00-00 FIG 103 ORIGINAL THICKNESS .071 REMAINING .023, BEYOND ALLOWABLE LIMITS. REPAIRED BLENDED AREA OF INTERNAL DOUBLER IAW ER/A 551833-14 REPETITIVE INSP DUE EVERY 8,000 CYCLES REPAIR COMPLETED AT 28,474 CYCLES.

Part: SUPPORT ANGLE — CRACKED (SERVICE DOOR) · airframe 41,307 hrs · 28,474 cycles

RT SERVICE DOOR CRACKED ON LOWER DOOR HINGE SUPPORT ANGLE. REPLACED LOWER RT SERVICE DOOR HINGE SUPPORT ANGLE IAW SRM 51-41-02.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 41,307 hrs · 28,474 cycles

AFT UPPER ATTACH ANGLE BRACKET FOR LT AFT ACCESSORY BAY VENT CRACKED AT FASTENER. REPLACED AFT UPPER ATTACH ANGLE BRACKET FOR LT AFT ACCESSORY BAY VENT IAW SRM 51-41-02.

Part: DOOR FRAME — DAMAGED (AFT CARGO) · airframe 41,307 hrs · 28,474 cycles

AFT CARGO DOOR FRAME PAN DAMAGED. REPLACED IAW SRM 53-20-15 (FIG 201) REPAIR 7, 51-41-02, 51-41-05.

Part: SHEAR TIE — CRACKED (BS 1152) · airframe 41,307 hrs · 28,474 cycles

SHEAR TIE CRACKED AT VERT STAB MOUNTS BS 1152 LT AND RT SIDE. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-02 & 51-41-05 PAGE 1-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,307 hrs · 28,474 cycles

CUSP WEB BETWEEN STA 215-230 IS CRACKED AT RBL 44. REPAIRED CRACKED CUSP WEB AT STA 215-230 RBL 44 IAW SRM 53-00-55 REPAIR 4.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

R1 SERVICE DOOR HAS CORROSION FROM STA 160-200 ON CUSP ANGLE. REPAIRED SERVICE DOOR CUSP ANGLE STA 160-200 IAW SRM 53-00-55 REPAIR 3, 51-41-05 PG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,307 hrs · 28,474 cycles

NR 3 AFT LAV FLOOR PANEL HAS DELAMINATED CORNER AND EDGE SEAL MISSING. REPAIRED LAV FLOOR PANEL IAW SRM 52-20-50 REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

LEFT OUTBD SEAT TRACK LBL 56 HAS CORROSION DISCREPANCIES FROM FUSELAGE STATION 982-986. REPAIRED LEFT OUTBD SEAT TRACK LBL56 FUSELAGE STATION 982-986 IAW SRM 53-20-52 REPAIR 1.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 41,307 hrs · 28,474 cycles

AFT CARGO DOOR CRACKED AT UPPER FWD AND AFT DOOR STOPS. FABBED DOUBLERS FROM 2024-0-.050, HEAT TREATED TO 2024-T42, AND INSTALLED DOUBLERS AT UPPER FWD AND AFT STOPS IAW SRM 52-30-02 REPAIR 6 ON AFT CARGO DOOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

AFT CARGO L30 IS CORRODED BETWEEN STA 920 - STA 994. BLENDED CORROSION ON STR 30 FROM STA 920 TO 965 IAW SRM 51-10-04 SECTION 26. .115 REMAINING OF .125 FOUND TO BE IN LIMITS IAW SRM 53-00-60 FIG 103. BLENDED STR 30 FROM STA 975 TO 994 IAW SRM 51-10-04 SECTION 26. .065 REMAINING OF .125 FOUND TO BE OUT OF LIMITS AT STA 987 (APPROX), IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-00-05 REPAIR 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

SHEAR TIE CORRODED IN AFT BAG BIN STA 908 BETWEEN LONGERON 29L-30. SHEAR TIE FOUND TO BE CORRODED THROUGH. 100% MATERIAL LOSS. REPAIRED CORRODED SHEAR TIE SECTION IAW SRM 53-20-06 REPAIR 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,458 hrs · 28,586 cycles

RT CUSP WEB HAS MULTIPLE AREAS OF CORROSION STA 157, 198, 218, 222 RBL 56 AND STA 222 RBL 44.5. REPLACED RT CUSP WEB STA 157-222 RBL56-RBL 44.5 IAW ER/A 551819-14 MA.

Part: STIFFENER — CRACKED (FLOOR PANEL) · airframe 41,307 hrs · 28,474 cycles

UPPER CABIN FLOOR PANEL 222 AJF HAS A CRACKED STIFFENER AND DISBONDED STIFFENER END. REPAIRED CRACKED STIFFENER IAW SRM 53-20-50 REPAIR 5 FIG 202. REPAIRED DISBONDED STIFFENER IAW SRM 51-20-05 REPAIR SEALING.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 41,307 hrs · 28,474 cycles

FLOOR PANEL 222AFF HAT CHANNEL IS CRACKED. FABRICATED HAT CHANNEL REPAIR SECTION IAW SRM 53-20-50 REPAIR NR 5 FIG 202, HEAT TREATED TO T-6 CONDITION IAW DPS 900-4-1 NR 1 PAGES 16 AND 18. INSTALLED REPAIR IAW SRM 53-20-50 REPAIR NR 5 FIG 202.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,307 hrs · 28,474 cycles

UPPER FUSELAGE, PASSENGER CABIN, STA 1022 L12R TO L14R, CRACKS. STA 1022 L12R TO L14R CRACKED SHEAR TIE. REMOVED CRACKED SHEAR TIE AND INSTALLED REPLACEMENT IAW SRM 51-41-05 AND 51-41-05.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

FLOOR PAN IS CORRODED AT STA 200 BL0. REPLACED FLOOR PANS AT STA 200 IAW SRM 51-41-05 PG 1 DWG 9936535 REV CS REISSUE FRAME 6.

Part: SHEAR TIE — CORRODED (BS 1002) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

AFT CARGO SHEAR TIE AND FRAME IS CORRODED AT BS 1002 BETWEEN LONGERSONS 29 - 30L. REPLACED THE SHEAR TIE IAW DWG 9957739, SRM 53-00-00 FIG 103 & SRM IN 51-41-05 PGS 1-5.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 41,307 hrs · 28,474 cycles

FWD CARGO DOOR EXTERNAL SKIN EDGE AT THE AFT LOWER CORNER AREA HAS TWO DENTS. REMOVED AND REPLACED THE SKIN.

Part: ATTACH FITTING — WORN (TAILCONE) · airframe 41,307 hrs · 28,474 cycles

INSPECTION OF THE TAILCONE LOCKING MECHANISM CABLE DISCOVERED A WORN CABLE SLIDE ATTACHMENT WHICH MAY PREVENT THE SLIDE FROM DEPLOYING. THE ATTACHMENT WAS REPLACED, THE SYSTEM WAS RETURNED OPERATIONAL STATUS, AND THE RII WAS COMPLETED.

Part: CUSP WEB — CRACKED (BS 218) · airframe 41,307 hrs · 28,474 cycles

RIGHT CUSP WEB CRACKED AT BS 218. REPLACED THE CUSP WEB IAW SRM 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

AFT CARGO INTERNAL DOUBLER IS CORRODED AT STA 1025, BETWEEN L29L-L30. REPLACED INTERNAL DOUBLER IAW SRM 53-02-01 REPAIR 1 2024-T3 -.025.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 41,307 hrs · 28,474 cycles

RIGHT FLAP INBD LOWER WEDGE HAS A HOLE. REMOVED DAMAGED AREA IAW SRM 51-70-13 REPAIR 1 FIG 202. FABRICATED A REPAIR IAW SRM 51-70-13 REPAIR 1 AND INSTALLED IAW SRM 51-70-13 REPAIR 1 FIG 202.

Part: SEAT TRACK — DAMAGED (BS 956-1022) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

UPPER CABIN RT INBD SEAT TRACK RBL 22 CORRODED & GOUGED AT BS 956-1022. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. TRIMMED OUT SEAT TRACK IAW SRM 53-20-52 REPAIR 1.

Part: FLOOR PANEL — DAMAGED (LAVATORY) · airframe 41,307 hrs · 28,474 cycles

AFT LAV WASTE DRAIN FLOOR PANEL HAS A MISSING INSERT AND DISBONDED HONEYCOMB CORE. REPAIRED IAW SRM 53-20-50 REPAIR 4.

Part: CUSP WEB — CRACKED (BS 1002-1022) · airframe 41,307 hrs · 28,474 cycles

LEFT CUSP WEB IS CRACKED BETWEEN BS 1002 AND 1022 LBL 44-55. CUT OUT THE DAMAGED SECTION OF CUSP WEB. FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED RING DOUBLER, AND FABRICATED AND INSTALLED FILLER REF B717 SRM 53-00-55 REPAIR 4.

Part: FLOOR PANEL — CRACKED · airframe 41,307 hrs · 28,474 cycles

FLOOR PANEL 211JF IS CRACKED. REPAIRED THE FLOOR PANEL IAW SRM 51-70-11, REPAIR 1 FIG 201. FABRICATED A REPAIR DOUBLER. APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 AND 3.

Part: CUSP WEB — CRACKED (BS 916-980) · corrosion level 2 · airframe 41,307 hrs · 28,474 cycles

RIGHT CUSP WEB HAS MULTIPLE AREAS OF CORROSION BS 916, 930, 943, 955, 980, RBL 61. CLEANED CORROSION IAW SRM 53-00-55 FIG 101, REPAIRED IAW SRM 53-00-55 REPAIR 4.

Part: FLOOR SUPPORT — CRACKED (BS 617-636) · airframe 41,307 hrs · 28,474 cycles

FLOOR SUPPORT AT BS 617 - 636 BL 0 CRACKED. REPAIRED IAW SRM 53-00-00 REPAIR 1 FIG 201, AND DWG 9936580.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,139 hrs · 27,592 cycles

DURING SERVICE CHECK, FOUND AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. R & R CABIN EMERGENCY POWER SUPPLY BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,743 hrs · 27,258 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 1-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: DAMPENER — MALFUNCTIONED (ELEVATORS) · airframe 38,877 hrs · 26,619 cycles

ACFT RETURNED TO DEPARTURE DUE TO ELEVATOR VIBRATION. MAINTENANCE REPLACED THE LT AND RT ELEVATOR DAMPERS AND LUBRICATED THE ELEVATOR. VERIFICATION FLIGHT WAS SUCCESSFUL.

Part: HOOK — DIRTY (L1 DOOR) · airframe 36,502 hrs · 24,831 cycles

L1 DOOR GIRT BAR HOOK DIRTY. CLEANED HOOK IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 34,606 hrs · 23,565 cycles

EMERGENCY EXIT LIGHT BROKEN AT ROW 18 DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

FUSELAGE SKIN CORRODED BETWEEN STA 1022 TO 1023, LONGERON 30L. REPAIRED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,212 hrs · 22,674 cycles

FUSELAGE SKIN CORRODED AT STA 1022, LONGERON 30L. REPAIRED SKIN IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

VERTICAL SUPPORT CRACKED ABOVE CENTER WING STA 715, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: STRAP — CRACKED (CARGO BAY) · airframe 32,466 hrs · 22,212 cycles

AFT CARGO FWD GILLINER SUPPORTS CRACKED AT FWD BULKHEAD. R & R STRAPS IAW SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 32,466 hrs · 22,212 cycles

LEFT ELEVATOR AT INBD TAB CARBON FIBER DELAMINATED. R & R CONTROL TAB IAW AMM.

Part: RETAINER — MISSING (EVAC SLIDE) · airframe 32,466 hrs · 22,212 cycles

AFT ACCESSORY COMPARTMENT PLASTIC CABLE RETAINER MISSING FROM EVACUATION SLIDE COVER. INSTALLED RETAINER IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

VERTICAL FLOORBEAM SUPPORT CRACKED AT STA 737, LBL 44. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

ANGLE SUPPORT OVER FWD SIDE OF CENTER WING TANK CRACKED AT STA 655, LBL 20. R & R SUPPORT IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

RIGHT SEAT TRACK SECTION CORRODED BETWEEN STA 898 TO STA 1022, RBL 54. R & R SEAT TRACK IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

CUSP WEB CRACKED AT STA 674, LBL 44. REPAIRED DOUBLER IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 32,466 hrs · 22,212 cycles

LEFT WING INBD FLAP FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

VERTICAL FLOORBEAM SUPPORT CRACKED AT STA 737, RBL 44. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 32,466 hrs · 22,212 cycles

LEFT ELEVATOR AT OTBD GEARED TAB DELAMINATED. RR GEARED TAB IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LEFT SEAT TRACK SECTION CORRODED BETWEEN STA 256 TO STA 579, LBL 54. R & R SEAT TRACK IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LONGERON CRACKED AT STA 1133, LONG 2L. R & R LONGERON IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 589 TO STA 880, RBL 54. R & R SEAT TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

FRAME CORRODED AT STA 974, BETWEEN LONGERON 30L TO LONGERON 29L. R & R FRAME IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 655 TO STA 674. REPAIRED CUSP WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LEFT SEAT TRACK SECTION CORRODED BETWEEN STA 256 TO STA 587, LBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

RIGHT CUSP WEB CORRODED AT STA 710. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (AC BAY) · airframe 32,466 hrs · 22,212 cycles

AFT ACCESSORY COMPT EXIT SIGN LOWER BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LEFT CUSP WEB CORRODED STA 550. R & R CUSP WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LEFT SEAT TRACK SECTION CORRODED BETWEEN STA 587 TO STA 880, LBL 54. REPAIRED SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

LEFT CUSP WEB CORRODED BETWEEN STA 900 TO STA 908. R & R CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

AFT ACCESSORY COMPARTMENT AT CANT FRAME 1212, RT SIDE LOWER RAIL SUPPORT, CRACKED. R & R BRACKET IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

RIGHT SEAT TRACK SECTION CORRODED BETWEEN STA 265 TO STA 579, RBL 54. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

RIGHT SEAT TRACK SECTION CORRODED BETWEEN STA 265 TO STA 579, RBL 22. R & R SEAT TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,212 hrs · 22,674 cycles

FRAME CORRODED AT STA 974, BETWEEN LONG 30L TO LONG 29L. REPAIRED FRAME IAW SRM.

Part: PANEL — CRACKED (RT MLG WW) · airframe 32,466 hrs · 22,212 cycles

RIGHT MLG W/W AT AFT FRAME METAL PANEL CRACKED. REPAIRED PANEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

FRAME CORRODED AT STA 1022, BETWEEN LONG 29L & LONG 29R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,212 hrs · 22,674 cycles

FRAME CORRODED AT STA 1022, BETWEEN LONG 29L TO LONG 29R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

FRAME FORMER SECTION CORRODED AT STA 1022, BETWEEN LONG 29L TO LONG 30L. REPAIRED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED BETWEEN STA 541 TO STA 636, BETWEEN RBL 22 TO RBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL NR 222 APF DELAMINATED BETWEEN STA 813 TO STA 889, BETWEEN RBL 22 TO RBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222LB DELAMINATED BETWEEN STA 465 TO STA 541, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED BETWEEN STA 737 TO STA 813, BETWEEN RBL 22 TO RBL 44. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222 AMF DELAMINATED BETWEEN STA 813 TO STA 889, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222 ATF DELAMINATED BETWEEN STA 889 TO STA 954, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222ACF DELAMINATED BETWEEN STA 696 TO STA 737, BETWEEN LBL 22 TO LBL 44. R & R PANEL IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 32,466 hrs · 22,212 cycles

LEFT WING L/E INSIDE FAIRING UPPER & LOWER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DWG AND SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL NR 222LF DELAMINATED BETWEEN STA 465 TO STA 541, BETWEEN RBL 22 TO RBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222WF DELAMINATED BETWEEN STA 313 TO STA 389, BETWEEN RBL 22 TO RBL 44. R & R FLOOR PANEL IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 32,466 hrs · 22,212 cycles

RIGHT WING L/E INSIDE FAIRING BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DWG AND SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 221UF DELAMINATED BETWEEN STA 313 TO STA 389, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL NR 222BF DELAMINATED BETWEEN STA 389 TO STA 465, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL 222PF DELAMINATED BETWEEN STA 541 TO STA 617, BETWEEN LBL 22 TO LBL 44. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,466 hrs · 22,212 cycles

MAIN CABIN FLOOR PANEL AAF222 DELAMINATED BETWEEN STA 674 TO STA 696, LBL 22. R & R PANEL IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

FWD CARGO DOOR FRAME CRACKED AT FWD LATCH AREA. R & R DOUBLER IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

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

Part: PAN — CORRODED (FUSELAGE) · airframe 32,466 hrs · 22,212 cycles

AFT CARGO DOOR PAN CORRODED. REPAIRED PAN IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 30,485 hrs · 20,948 cycles

EXIT SIGN COVER OVER BUSINESS CLASS LOOSE. SECURED COVER PER MM.

Part: SIGN — MALFUNCTIONED (CABIN)

EXIT SIGN BLINKING ON AND OFF ACFT LEFT AT TAIL CONE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, ALL LIGHTS OP'S CHECK'S NORMAL; NO FLICKERING NOTED IAW B717 AMM 33-51.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT ON SEAT 2D IS INOP (REFER TO F/A CBR). RELAMPED FORWARD EPL LIGHT AT 2D OP CHECK GOOD IAW AMM 33-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN AT L1 DOOR FLOOR SUPPORT, STA 168, LBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE STA 270, LONG 19R, DENTED. ACCOMPLISHED EXTERNAL DOUBLER AND FINGER DOUBLER REPAIR PER B717 SRM 53-03-01.

Part: FITTING — CORRODED (GIRT BAR)

FORWARD GALLEY SERVICE DOOR GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT, STA 200, RBL 10 TO RBL 20, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CRACKED (FUSELAGE)

LEFT SIDE CABIN INTERIOR WEB, STA 210, LONG 15L, CRACKED. ACCOMPLISHED INTERIOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FORWARD CABIN FLOOR SUPPORT, STA 200, RBL 57, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER BOEING DWG SR09530085.

Part: BATTERY — DISCHARGED (CABIN)

LT AND RT AFT EMERGENCY EXITS LOWER LIGHT INOP. REMOVED AND REPLACED BIN 24 RT EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY IAW B717 AMM 33-51, OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN)

EPL LIGHT LENS MISSING AT SEAT ROWS 12 AND 24. REPLACED CLEAR LENS AT SEAT ROWS 12, AND 24 IAW MM 33-51-00. OPS CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND THE LEFT AND RIGHT OVERWING EXIT IDENTIFIER LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY ON SEAT ROW 24R IAW MM 33-51. EMERGENCY LIGHTS OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 20 EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. RELAMPED EMERGENCY EXIT LIGHT ASSY AS REQUIRED MM 33-51.

Part: ENGINE — FAILED (LEFT)

DURING TAKEOFF AT APPROXIMATELY 300-900 FT AGL, LEFT ENGINE FAILED WITH A LOUD BANG. LAST SAW EGT CLIMBING THROUGH 965 DEGREES C. REMOVED AND REPLACED LEFT ENGINE. COMPLIED WITH ALL INSPECTIONS.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2976.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2987.

Part: ENTERTAIN SYS — SHORTED (ROW 12-14)

PAX IN ROW 12 AND 14 AC LEFT SAW SPARKS AND ODOR SMOKE. F/A CONFIRM ODOR BUT NOT NO SPARKS. CONFIRMED SPARK THAT WAS REPORTED BY PAX IN ROW 12 AC. FOUND C/B ZONE 5 POPPED FOR XM SYSTEM IN THE E&E. COLLARED C/B FOR ZONE 5. PULLED AND COLLARED XM SYSTEM C/B IN COCKPIT D3,4,5 AND E5.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR FRAME LOWER PAN, CORRODED BEYOND LIMITS. INSTALLED SPLICE REPAIR PER B717 SRM 51-41-05.

Part: BATTERY — DISCHARGED (CARGO BAY)

BOTH EXTERIOR EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY IAW 717 AMM 33-51.

Part: COMPRESSOR — STALLED (LT ENGINE)

INDICATIONS OF COMPRESSOR STALL FOLLOWED BY RED BOXED OIL PRESS LOW ON LEFT ENGINE. COMPLIED W/QRT AND SHUT DOWN LEFT ENGINE. REMOVED AND REPLACED LEFT ENGINE PER TASK CARD 603.

Part: LINE — UNSERVICEABLE (NR 2 ENGINE)

LOST RIGHT HYDRAULIC FLUID AFTER TAKEOFF, HYDRAULIC LOW QUANTITY ALERT ILLUMINATED, HYDRAULIC QUANTITY INDICATES ZERO. RTB PERFORMED, MANUAL GEAR EXTENSION, NORMAL LANDING AND ROLL OUT, TOWED TO GATE. REPLACED NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE IAW MM 29-10, LEAK CHECK. REMOVED AND REPLACED RIGHT AND LEFT MAIN LANDING GEAR DOORS FOR DAMAGE, PROVIDED CLEARANCE ON THE NEW DOORS. OPS CHECK GOOD MM 3200.