N937AT

Part: HINGE FITTING — CORRODED (ZONE 600 FLAP) · airframe 55,478 hrs · 40,379 cycles

CORROSION FOUND ON BOLT SETTLEMENT AREA (INBRD SIDE) AT RT WING FLAP FWD HINGE NR 3. RT FLAP FWD HINGE WAS REPAIRED IAW PRI 631116-14 REV 2, AND ER/A 631116-14 (1361088)

Part: STRAP — CRACKED (ZONE 200) · airframe 55,478 hrs · 40,379 cycles

CRACKED ANGLE STRAP BTW CANTED BS 1178, L2R AT ROOT OF VERTICAL STABILIZER. REPAIRED IAW SRM 53-30-01-2R -1. (1358667)

Part: NOT REPORTED — NOT REPORTED · airframe 55,514 hrs · 40,411 cycles

DTA ER/A 631116-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-631116 (1359292)

Part: LANYARD — FRAYED (ZONE 800) · airframe 55,478 hrs · 40,379 cycles

FRAYED LANDYARD CABLE FROM L1 SLIDE DOOR. LANYARD CABLE FROM L1 SLIDE DOOR WAS REPLACED AND PART NUMBER WAS VERIFIED PER AIPC 25-61-01 AND INSTALLATION IS ACCOMPLISHED UNDER AMDS 5211-4002. (1354881)

Part: SPAR — CRACKED (ZONE 500) · airframe 53,991 hrs · 38,995 cycles

-AD- CRACK FOUND IN LWR AFT LEG OF LWR REAR SPAR JUST OB OF FLAP FITTING @ XRS170 DURING LT WING REAR SPAR INSP AMDS #5720-01103-01A. COMPLIED WITH PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7. COMPARED PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7 WITH ERA 623680-14AD REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 623680-14AD REV ORIG. ALL RII ITEMS C/W. ASSOCIATED ER/A 14-623680 ADDED FOR AC 9586. (LP #6976008)

Part: STRUCTURE — CRACKED (NOT REPORTED) · airframe 53,997 hrs · 38,999 cycles

-AD- COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 623843-14AD DUE TO CRACK INDICATION FOUND DURING INSP. COMPLIED WITH PRI 623843-14AD REV 0,1,2, & 3. COMPARED PRI 623843-14AD REV 0,1,2, & 3 WITH ERA 623843-14AD REV ORIG AND ALL ITEMS MATCH. ALL RII ITEMS CW. ASSOCIATED ER/A 14-623843 ADDED FOR AC 9586. (LP #6976015)

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 52,614 hrs · 37,789 cycles

SHIP 9586 -ATB/HYD/DE- THE CREW RETURNED THE AIRCRAFT BACK TO MSP AND DECLARED AN EMERGENCY WITH ATC DURING THE APPROACH DUE TO THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY. THE LANDING GEAR WAS EXTENDED USING THE ALTERNATE GEAR EXTENSION PROCEDURES. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN GEAR DOORS CONTACTING THE RUNWAY. CORRECTIVE ACTION: MAINTENANCE FOUND A B-NUT ON THE TRANSFER LINE TO BE LOOSE AND TIGHTENED IT. ALL OF THE HYDRAULIC PUMPS USED WITHOUT ENOUGH FLUID WERE REPLACED. THE MAIN GEAR DOORS WERE REPAIRED. (LP #5939976)

Part: JACKSCREW — CORRODED · corrosion level 2 · airframe 52,613 hrs · 37,788 cycles

-AD- FOUND CORROSION ON LOWER JACKSCREW THREADS APPROX 6"ABOVE LOWER STOP. SUMMARY SEE NRC 006-0001:2740-01114-05 /002 00007: REPLACED JACK SCREW PER AMDS 2740-01114-05. CLOSING REQUIREMENTS RII: INSPECTOR 00260220. (LP #0373180)

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 52,420 hrs · 37,611 cycles

THE TAIL EXIT LIGHT STAYS FLASHING WITH THE EMERGENCY POWER SWITCH ARMED. MAINTENANCE REPLACED THE BATTERY PACK AND CRADLE ASSEMBLY B5-260 PER B717 AMM 33-51. NOW OPERATES NORMALLY. (LP #5832652)

Part: GENERATOR — FAILED (RIGHT) · airframe 52,288 hrs · 37,487 cycles

SHIP 9586 -DIV- THE FLIGHT WAS DIVERTED TO MCO FOLLOWING THE FAILURE OF THE RIGHT GENERATOR AFTER TAKEOFF, WHILE THE APU GENERATOR WAS ON MEL. THE CAPTAIN DECLARED AN EMERGENCY WITH ATC. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL REQUIRED RTS TESTS. (LP #5453940)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

IMPROPERLY INSTALLATION OF LATCH AND MANUAL DEPLOYMENT HANDLE OF TAIL CONE SLIDE. 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 00756: LATCH AND MANUAL DEPLOYMENT HANDLE OF TAIL CONE SLIDE WAS RE-INSTALLED CORRECTLY PER AMDS 5352-4002 STEP 13.C. (LP #0123947)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACKED PLATE ON EMERGENCY DOOR INTERNAL STRUCTURE (MIDDLE SECTION) Y=1053 X=10 AT PAX CABIN. SUMMARY OF NRC 00097: PLATE (WEB) ON EMERGENCY DOOR INTERNAL STRUCTURE (MIDDLE SECTION) Y=1053 X=10 AT PAX CABIN WAS REPAIRED PER B717 AMM 52-12-03 000-801, 52-12-03 400-801, 52-12-03 800-801, 52-70-01 820-803, CMM 52-63-1, SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, 51-41-06-0G, AND DWG 9915565 REV BD. (LP #0122334)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT WAS REPAIRED PER ERA 598923-14 REV. A AND PRI 598923-14 REV 3. ASSOCIATED ER/A 14-598923 ADDED FOR AC 9586. (LP #0108347)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON PREVIOUS REPAIR SPLICES ON DOOR JAMB STA Y=954 BTW STRINGER 26-27RH. SUMMARY OF NRC 00698: CORROSION LEVEL 2. PREVIOUS REPAIR SPLICES ON DOOR JAMB STA Y=954 BTW STRINGER 26-27RH SPLICES (2 EA) WERE FABRICATED AND INSTALLED PER B717 SRM 53-20-15-2R REPAIR 7. (LP #0106823)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON LONGERON SPLICE L30 BETWEEN Y=889 AND Y=908, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. SPLICE ON L30 BETWEEN Y=889 AND Y=908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G PAR 10 AND 51-41-01-0G. (LP #0105920)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK ON FLOOR BEAM AND BEAM-WEB ATTACHED TO LH FRAME Y=674, X=57 AT PASSENGER CABIN. SUMMARY OF NRC 228: FLOOR BEAM WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. BEAM-WEB ATTACHED TO LH FRAME Y=674, X=57 AT PASSENGER CABIN WAS REPAIRED PER ER/A 613385-14 REV ORIG, SECTION I AND PRI 613385 REV 0, REV 1. (LP #0104605)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CORROSION ON RH TRACK ABOVE R=28 BTW STA Y=427+13, Y=446+6 AT LOWER FWD CARGO COMPARTMENT. SUMMARY OF NRC 00068: CORROSION LEVEL 2. RH TRACK ABOVE R=28 BTW STA Y=427+13, Y=446+6 AT LOWER FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 4 REPAIR 4. (LP #0104646)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON CUSP ANGLE BTW STA Y 208 TO STA Y 164 SERVICE DOOR (R1) AT PAX CABIN. SUMMARY OF NRC 284: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y 208 TO STA Y 164 SERVICE DOOR (R1) AT PAX CABIN WAS REPAIRED PER ERA 613317-14 REV ORIG AND PRI 613317-14 REV 2. ASSOCIATED ERA 14-613317 ADDED FOR AC 9586. (LP #0099014)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

BEND AND CRACK ON CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE. SUMMARY OF NRC 00126: CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE WAS REPAIRED PER B717 SRM 53-10-15 2R, REPAIR 4 FIGURE 201. MAINTENANCE REQUIREMENTS WERE VERIFIED ON FOLLOWING ACTIONS ARE NEEDED: DO ETHF (HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND THE DOUBLER EDGES) REF 51-10-09, GENERAL: INITIAL 28,000 LANDINGS DO ETHF (HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND THE DOUBLER EDGES) REF 51-10-09, GENERAL: LANDINGS, REPETITIVE: 20,000 LANDINGS. (LP #0098776)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-01-0G, AND 53-20-52-2R REPAIR 5. (LP #0096562)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON RH CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CABIN. SUMMARY OF NRC 00509: CORROSION LEVEL 2. CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0095789)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON RH SEAT TRACK X=-44 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 0495: CORROSION LEVEL 2. SEAT TRACK X=-44 BTW STA Y=199-256 WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-05-0G, AND PER DWG 5930547 REV CW. (LP #0095908)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON LOWER SURFACE OF CUSP WEB STA Y 705 OVER X49 AND STA Y 676 AND X58 LH SIDE AT CPAX. SUMMARY OF NRC 00307: CORROSION LEVEL 2. CUSP WEB STA Y 655 TO 715 X58 LH SIDE AT CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G AND REPAIR PER B717-200 SRM 53-00-55-2R-4. (LP #0093036)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK ON EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L. SUMMARY OF NRC 00368: EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L WAS REPAIRED PER ER/A 613350-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME OF ACCOMPLISHMENT ACCOMPLISH SECTION II: THRESHOLD INSPECTION 28,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I, REPETITIVE INSPECTION AT INTERVAL 15,000 CYCLES. LOG PAGE #0090915 AND ACCOMPLISH SECTION III: PERMANENT REPAIR 52,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I: TEMPORARY REPAIR LOG PAGE #0090944. (LP #0091593)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON LH SEAT TRACK X=22 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK X=22 BTW Y=199-265 WAS REPLACED PER DWG 5930547 REV CZ AND B717-200 SRM 51-41-01-0G. (LP #0092293)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK ON CUSP WEP STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX. SUMMARY OF NRC 0293: SECTION CUSP WEB STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0089035)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON SLIDE LATCHES AT SERVICE DOOR (R1) IN PAX CABIN. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LATCHES FOR SLIDE AT SERVICE DOOR (R1) IN PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0084409)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON INTERCOSTAL BTW STA Y=1022 TO STAY=1037, LONGERON 30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00543: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=1022 TO STAY=1037, LONGERON 30 AT AFT CARGO COMPARTMENT WAS FABRICATED PER DWG 9936718 REV N AND REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0084414)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGER IN REF NRC 284. SUMMARY OF NRC 00518: CORROSION LEVEL 2. NEW ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGER WAS FABRICATED AND REPLACED PER DWG 590085-19 REV DJ. (LP #0081789)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN. SUMMARY OF NRC 00230: CORROSION LEVEL 2. VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #0080112)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK ON CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX. SUMMARY OF NRC 00305: CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIGURE 220. (LP #0077736)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK AT STA 1086.5 AND LONGERON 13RH APROX ON EXTERIOR FUSELAGE. SUMMARY OF NRC 00014: CRACK AT STA 1086.5 AND LONGERON 13RH APROX WAS REPAIRED PER PRI 613146-14 REV 2 AND ER/A 613146-14 REV ORIGINAL, SECTION I. PERMANENT REPAIR.ACCOMPLISH SECTION II. REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I. PERMANENT REPAIR PER ER/A 613146-14 REV ORIGINAL. THIS INSPECTION MONITORED UNDER LOGPAGE 0074253. ASSOCIATED ER/A 14-613146 ADDED FOR AC 9586. (LP #0075860)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK UPPER CAP ON STA Y=1022 AND LONGERON 7 LH SIDE AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00188: UPPER CAP ON STA Y=1022 AND LONGERON 7LH SIDE AT PASSENGER CABIN WAS REPAIRED PER PRI 613311-14 REV 1 AND ERA 613311-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613311 ADDED FOR AC 9586. (LP #0063427)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 51,741 hrs · 37,034 cycles

CORROSION ON PREVIOUS REPAIR ON CUSP WEB RH SIDE ON STA Y 332 AND -X56 AT CPAX. SUMMARY OF NRC 00240: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB RH SIDE ON STA Y 332 AND -X56 AT CPAX WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0057493)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

CRACK ON BEAMS (3 EA) OVER BEAM #1 AFT EDGE AND BEAM #2 AFT/FWD EDGE AT FWD PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00128: CRACK ON BEAMS OVER BEAM #1 AFT EDGE WAS FOUND REPAIRED IN REFERENCE TO LOG 2214723 AND CRACKED BEAM #2 AFT/FWD EDGE AT FWD PASSENGER ENTRANCE DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (LP #0048825)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,108 hrs · 36,496 cycles

AFT F/A READY LIGHT COVER MISSING. RESECURED AFT F/A EMERGENCY LIGHT LENS COVER PER B717 AMM 33-51. A/C OK FOR SVC. (LP #4984108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,690 hrs · 36,116 cycles

SEVERAL CABIN EMERGENCY LIGHTS AND THE MID-CABIN EXIT IDENFIER LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD AND MID-CABIN BATTERY PACKS IAW B717 AMM 33-55. EMERGENCY LIGHT OPERATIONAL CHECK WAS NORMAL. (LP #9957867)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,665 hrs · 36,096 cycles

THE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THREE EMERGENCY LIGHT BATTERY PACKS PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #9957841)

Part: NONE — NONE · airframe 49,222 hrs · 34,841 cycles

ON INTERIOR WALK-THROUGH, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED ONE BATTERY PACK ABOVER ROW 19, FOR THE OVERWING EMERGENCY EXIT LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL EMERGENCY LIGHTS NOW OPERATE CORRECTLY. AIRCRAFT OKAY FOR SERVICE. (LP #8964900)

Part: NONE — NONE · airframe 48,725 hrs · 34,407 cycles

MAINTENANCE FOUND THAT THE EMERGENCY LIGHT OVER THE AFT EMERGENCY EXIT WAS NOT WORKING, WHEN PREFORMING LIGHTS TEST. THE POWER SUPPLY ASSOCIATED WITH THE LIGHT WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #7301237)

Part: SKIN — CORRODED · corrosion level 2 · airframe 48,407 hrs · 34,122 cycles

PROTUBERANCE PROVOKED BY CORROSION ON EXTERNAL FUSELAGE SKIN STA 650-655 BTW LONG 28LH TO 29LH. SUMMARY OF NRC 00226: LEVEL CORROSION 2, EXTERNAL FUSELAGE SKIN STA 650-655 BTW LONG 28LH TO 29LH WAS REPAIRED PER PRI 598923-14 REV. 2 AND ER/A 598923-14 SECTION I PERMANENT REPAIR, REV ORIGINAL. PERFORM A GENERAL VISUAL INSPECTION PER NDTSPM PART 9, 09-00-06 TO ENSURE NO ADDITIONAL DAMAGE EXISTS. ACCOMPLISH SECTION II: REPETITIVE GENERAL VISUAL INSPECTION AT 8,000 CYCLES FROM 27 APRIL, 2022 AND THEN REPETITIVELY AT EVERY 8,000 CYCLES PER ERA 598923-14 REV ORIGINAL SECTION II. ASSOCIATED ER/A 00-598923 ADDED FOR AC 9586. PLEASE CHANGE TO LEVEL CORROSION 2 EXTERNAL FUSELAGE SKIN STA 650-655 BTW LOIN G 28LH TT 29LH WAS REPAIRED PER PRI 598923-14V REV 2 AND ERA 598923-14 SECTION 1 PERMANENT REPAIR. (LP #2216170)

Part: NONE — NONE · airframe 48,404 hrs · 34,121 cycles

CRACK ON BEAM #1 STA Y=200 ON THE EDGE AT L1 DOOR. SUMMARY OF NRC 00159: BEAM #1 STA Y=200 ON THE EDGE AT L1 DOOR WAS REPAIRED PER B-717 SRM 52-10-02-2R-7 FIGURE 201. (LP #2214723)

Part: NONE — NONE · corrosion level 2 · airframe 48,470 hrs · 34,177 cycles

FUSELAGE SKIN AND INTERNAL DOUBLER STA 630 TO 655, L-28R TO L-29L CORROSION & CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. REVISED REPAIR LOCATION DESCRIPTION TO MATCH ER/A AS FOLLOWS; FUSELAGE SKIN AND INTERNAL DOUBLER STA 626 TO 661, L-28R TO L-28L CORROSION & CRACKS. (LP #2214966)

Part: VANE — DENTED · airframe 48,404 hrs · 34,121 cycles

DENTS #2, #3, AND #11 WERE IDENTIFIED AND EVALUATED PER B717 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. AT AFT MOVABLE VANE RH WING, TO ACCOMPLISH MON/ 9586/1712741, REF NRC S/N 00256 (AD). SUMMARY OF NRC 00259: MOVABLE VANE RH WING WAS REPAIRED PER B717 SRM 57-53-01-2R-1. (LP #2212342)

Part: STAY — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON FRAME CLIP STA Y=927 BTW LONG 28 LH TO LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00123: CORROSION LEVEL 2, FRAME CLIP STA Y=927 BTW LONG 28 LH TO LONG 30 WAS REPLACED PER B717 SRM 51-41-02 PAR 4 AND 51-41-05 PAR 8 AND DWG 9915524 REV P. (LP #2212679)

Part: FLAP — DENTED · airframe 48,404 hrs · 34,121 cycles

DENTS ON AFT MOVABLE VANE, LOWER SKIN LH FLAP. SUMMARY OF NRC 00044: MOVABLE VANE LOWER SKIN LH FLAP WAS REPAIRED PER B 717 SRM 57-53-01-2R PROCEDURE 1. (LP #2212347)

Part: FRAME — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON FRAME CLIP STA Y=974 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2, FRAME CLIP STA Y=974 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R FIG. 201. (LP #2211458)

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON DOUBLER STA APROX 974 AFTER REMOTION OF LOWER PAN OF AFTER CARGO DOOR JAMB STA 954 TO 990 IN ORDER TO PERFORM NRC 052 (C2). SUMMARY OF NRC 00242: CORROSION LEVEL 2, DOUBLER STA APROX 974 WAS REPAIRED PER ER/A 598922-14 REV ORIGINAL/PRI 598922-14 REV.0 . SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-598922 ADDED FOR AC 9586. (LP #2208833)

Part: STAY — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON FRAME CLIP STA Y=954 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2, FRAME CLIP STA Y=954 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R FIG. 201. (LP #2208838)

Part: STAY — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON FRAME CLIP STA Y=946 BTW LOGS 29 LH - 29 RH, AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00255: CORROSION LEVEL 2, FRAME CLIP STA Y=946 BTW LOGS 29 LH - 29 RH, AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R. (LP #2208952)

Part: STAY — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON FRAME CLIP STA Y=908 BTW LONG 28 LH TO LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00122: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26 LH TO LONG 26 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND DWG 9915524 REV P. (LP #2208665)

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB (C2). SUMMARY OF NRC 0052: CORROSION LEVEL 2, PREVIOUS REPAIR AND LOWER DOOR JAMB ON AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #2208730)

Part: LONGERON — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON LONGERON 29 LH FROM STA 928 TO 931 AFT CARGO COMPARTIMENT IN ORDER TO PERFORM NRC 139. SUMMARY OF NRC 00251: CORROSION LEVEL 2, LONGERON 29 LH FROM STA 928 TO 931 AFT CARGO COMPARTIMENT IN ORDER TO PERFORM NRC 139 WAS REPAIRED PER B-717 SRM 53-00-05-2R REPAIR 3 FIG.201. (LP #2205368)

Part: LONGERON — CRACKED · airframe 48,404 hrs · 34,121 cycles

CRACK LONG 2RH AT STA 1133 AT AFT ACCESORIES COMPARTMENT. SUMMARY 0F NRC 00203: LONG 2RH AT STA 1133 AT AFT ACCESORIES COMPARTMENT.WAS REPAIRED PER B717 SRM 53-00-05-2R-2. (LP #2205959)

Part: LONGERON — CRACKED · airframe 48,404 hrs · 34,121 cycles

CRACK LONG 2LH STA 1133 AT AFT ACCESORIES COMPARTMENT. SUMMARY 0F NRC 00204: LONG 2LH AT STA 1133 AT AFT ACCESORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2. (LP #2205975)

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 48,404 hrs · 34,121 cycles

CORROSION ON DOUBLER ATTACH AFT PRESSURE BULKHEAD STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: LEVEL CORROSION 2, DOUBLER ATTACH AFT PRESSURE BULKHEAD STA Y=1053 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G PAR. 8.B. (LP #2205907)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,741 hrs · 37,034 cycles

MAIN ENTRANCE DOOR, (L-1), HOLD OPEN HOOK CAVITY IS GOUGED ON THE AFT SIDE. REPAIRED FUSELAGE SKIN AT L-1 DOOR HOLD OPEN HOOK CAVITY IAW B717 SRM 53-10-01-2R-7. INSPECTION REQ AT 8000 F.C. FROM DATE OF REPAIR INSTALL & REPEAT EVERY 8000 F.C. THERE AFTER INSP REQ VISUAL ONLY PER TABLE 203. (LP #0792109)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,796 hrs · 32,122 cycles

COCKPIT EMERGENCY FLOODLIGHT INOP. RELAMPED PER AMM 33-51 NO HELP. R&R EMERGENCY BATTERY PACK B5-123 PER AMM 33-51 OPS CHECK NORMAL OK FOR SERVICE. (LP5528324)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 44,781 hrs · 31,393 cycles

LEFT OUTBOARD MAIN CABIN METAL FLOOR PANEL AT STA 720 HAS A SMALL HOLE IN CENTER OF PANEL. CUT OUT DAMAGED AREA DIM 700"X700" AT LEFT O/B MAIN CABIN METAL FLOOR PANEL AT STA 720 IAW B717 SRM 51-70-10. FABRICATED AND INSTALLED DOUBLER FROM 7075 T6 .032 DIM 4 1/2 X 3 3/8 IAW B717 SRM 51-41-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,411 hrs · 36,743 cycles

PUSHBACK TOWBAR BROKE, AIRCRAFT MADE CONTACT WITH TUG. FOUND 3 DENTS AND 3 GOUGES AFT OF STA 37 12.5 INCHES BELOW THE PRESSURE BOUNDRY. LIGHTLY BLENDED GOUGE AREA & ACCOMPLISHED UT THICKNESS MEASUREMENT, REF B717 NDT SPM 04-00-03, MIN REMAINING THICKNESS IS .058, .063 ORIGINAL THICKNESS. ASSOCIATED ER/A 14-570847 ADDED FOR AC 9586. HFEC INSPECTION REF B717 NDT SPM 06-00-03 REVEALED NO CRACKS. C/W ERA 570847-14 RETREATED AND PRIMED PER SRM 51-10-04 / 51-22-01. REPETITIVE INSP DAILY TERMINATING AT C CHECK. C/W REPETITIVE CHECK OF DAMAGE ERA 570847-14 REV ORIG SECTION 2. NO FURTHER DAMAGE NOTED. REPAIRED THE RIGHT HAND FUSELAGE SKIN STA 37-47 BELOW HORIZONTAL PRESSURE PANEL IAW ERA 570847-14 REV A SECTION 3. PERMANENT REPAIR ACCOMPLISHED. GENERAL VISUAL INSPECTION REQUIRED EVERY 8000 CYCLES. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 24OCT18 AND LOG COMMENTS. REFERENCE LOG PAGE 0797377 FOR FOLLOW ON INSPECTIONS. (LP #0768519)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,154 hrs · 30,951 cycles

THE AFT DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-03. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 41,505 hrs · 29,123 cycles

AFT EMERGENCY EXIT LIGHT FLICKERING / INTERMITTENT. REPLACED AFT OVERHEAD POWER SUPPLY AND BATTERY PACKS. OPS CHECKED GOOD IAW AMM 33-54.

Part: PAN — CRACKED (BS 832) · airframe 39,959 hrs · 27,925 cycles

CRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.

Part: SKIN — CRACKED (BS 1076) · airframe 39,861 hrs · 27,854 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BS 1076 LONGERON 14L REPAIRED IAW ETI-17-16-154 REV.4 AND ER/A 551747-14 REV. A .

Part: SKIN — CRACKED (RT WING) · airframe 39,861 hrs · 27,854 cycles

CRACKED INBD BUTTE DOOR INBD SKIN AT RT WING. REPAIRED IAW ETI-17-16-171 REV. 1 AND ER/A 551772-14 REV. ORIG.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 39,857 hrs · 27,852 cycles

CRACK ON FUEL ACCESS PLATE 620MB. ACCESS PLATE 620MB WAS REPLACED PER AMM 28-00-00 AND IPC 57-23-01-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION ON DOUBLER, STA Y=954 AND PROTECTION BTW LONG 26R TO 27R DOOR JAMB, AT AFTER CARGO COMPARTMENT. DOUBLER WAS REMOVED PER SRM 51-41-05 PAR 10 AND 51-41-07 PAR 10, DOUBLERS WERE MANUFACTURED PER SRM 51-20-09 AND 53-20-15 REPAIR 7 AND DOUBLER WAS INSTALLED PER SRM 51-41-05 AND 51-41-07.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACK ON INTERNAL FUSELAGE SKIN STA Y=1021 BTW LONG 13L-14L AT PAX CABIN. CRACKS ON FUSELAGE/SKIN AND DOUBLER/STA 1022 & L-13-L14 WERE REPAIRED WITH ETI-17-16-149 REV 3 AND ER/A 551741-14 REV ORIGINAL. PERFORM GVI ON EXTERNAL SURFACE, EVERY 3000 FLIGHT CYCLES UNDER LOG 2773773 PER ER/A 551741-14 SEC II.

Part: CARGO TRACK — CORRODED (BS 813-1022) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORRODED LT CARGO TRACK BETWEEN BS 813 - 1022. THE CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 (SHEET 1 AND 2) AND FOUND WITHIN LIMITS AT BS 813 TO 896 IAW SRM 53-20-52. FIG 101 (SHEET 1 OF 3). THE CARGO TRACK WAS REPLACED AT BS 896 - 1022 IAW SRM 51-40-08 AND DWG 5936663 REV. Y.

Part: HINGE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION AT HORIZONTAL STABILIZER CENTER SECTION HINGE BORE AT STRINGER 7 RT SIDE. THE REPAIR WAS ACCOMPLISHED PER ETI-17-16-155 REV 2 AND ER/A 551748-14 REV ORIG.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION AND DISBONDED VOR ANTENNA PANELS UPPER AND LOWER (4EA). VOR ANTENNA PANELS UPPER AND LOWER (4EA) WERE REMOVED PER AMM 34-32-03. VOR ANTENNAS (4 EA) WERE REPLACED PER AMM 34-32-03. FUNCTIONAL TEST WAS PERFORMED PER AMM 34-51-00. TEST OK.

Part: PAN — DAMAGED (CARGO DOOR) · airframe 39,857 hrs · 27,852 cycles

ELONGATED HOLE ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) (S/N 00554). REPAIR ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) WAS PERFORMED PER ETI-17-16-166 REV 1 AND ER/A 551752-14 REV ORIGINAL, AMM 52-31-03-000 802 AND SRM 51-41-02, 51-41-04 PARAGRAPH 9.

Part: RETAINER — WORN (DOOR BARRIER) · airframe 39,857 hrs · 27,852 cycles

WORN LOWER RETAINER AT FWD DOOR BARRIER. LOWER RETAINER WAS REPAIRED IAW ETI -17-16-168 REV. ORG. AND ER/A 551759-14 REV ORG.

Part: BEAM — CRACKED (NLG DOOR FRAME) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CRACKED LT NLG DOOR FRAME BEAM BS 48. AREA DAMAGE WAS REPAIRED IAW SRM 53-10-14 FIG. 201 REP. 2, ETI-17-16-158 REV. 1 AND ER/A 551751-14 REV. ORIG.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION ON FUEL ACCESS PANEL ON SETTLEMENT AREA AND COUNTERSINK 520 CT AT RT WING. THE ACCESS PANEL REPLACED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION ON FUEL ACCESS PANEL ON COUNTERSINK 520DT ON LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION ON FUEL ACCESS PANEL COUNTERSINK ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.

Part: CUSP WEB — CRACKED (BS 1002-1020) · airframe 39,857 hrs · 27,852 cycles

CRACKED CUSP WEB BETWEEN BS 1002 AND 1020, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG. 216. AND 51-41-05.

Part: BEAM — CRACKED (PAX DOOR) · airframe 39,857 hrs · 27,852 cycles

CRACK AT BEAM NR 6 ON FWD PASSENGER DOOR L1. BEAM NR 6 ON FWD PASSENGER DOOR WAS REPAIRED PER ER/A 551749-14 REV ORIGINAL AND ETI-17-16-156 REV ORIGINAL.

Part: CHANNEL — CRACKED (BS 764) · airframe 39,857 hrs · 27,852 cycles

CRACKED FWD CHANNEL OF THE LT MLG DOOR CUTOUT BS 764 AT LT WW AREA. THE CHANNEL WAS REMOVED PER B-717 SRM 51-41-02. A NEW CHANNEL WAS DRILLING IAW SRM 51-40-08. THE CHANNEL WAS TREATED AND PAINTED IAW SRM B717 51-10-04 PART 15 & 21. THE CHANNEL WAS INSTALLED IAW SRM 51-41-02 AN 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

DURING CORROSION REMOVAL CRACK WAS FOUND AT CUSP WEB STA Y=660 X=60. IN REF CARD 00278. (S/N 00525). CUSP WEB WAS REPAIRED PER SRM 53-00-55 FIG 126 HFEC WAS ACCOMPLISHED AND NO CRACKS WAS FOUND AFTER CUT OUT PER NDT SPM 06-10-01.001.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACK ON ANGLES 2EAS AT AFT PASSENGER EMERGENCY EXIT DOOR JAMB LT SIDE LOWER AND MIDDLE STOP AREA. (S/N 00506) FITTINGS WERE REPLACED PER SRM 51-41-02 AND 51-41-01.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 39,857 hrs · 27,852 cycles

CRACKED FITTING AT LT AFT OVERWING EMERGENCY EXIT DOOR BEAM 1 FWD EDGE. CLIP WAS REPLACED AND INSTALLED PER SRM 51-41-02, 51-41-05, AND DRAWING 9957735 REV G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACKED TEE AND CLIP AT FWD CARGO DOOR LOWER ANGLE BEAM INTERNAL STRUCTURE STA Y=410 APPROX. TEE AND CLIP WERE REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DPS 4.710-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACKED CLIPS AT Z=41.375 STA 196.8 AND STA 172.5 ON FWD GALLEY DOOR. CLIPS WERE REPLACED PER SRM 51-41-02, 51-41-05, AND DRAWING 9911581 REV U.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 39,857 hrs · 27,852 cycles

CRACKED CHANNEL ON FLOOR PANEL 222AFF AND 222AF, ALSO CRACKED WEB ON FLOOR PANEL 222XF AND CRACK ON STRAP ON FLOOR PANEL 223EF (S/N 00242). CRACKS ON FLOOR PANELS 222AFF, 222AF, 222XF AND 223EF WERE REPAIRED PER SRM 53-20-50 REPAIR 5, 53-00-00 REPAIR 1, AND 51-20-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACKED FRAMES STA 680, 696, 715 BTW LONG 28/25 LT AT KEEL BEAM AREA. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE REMOVED DAMAGE FRAME Y=696 LT PER NDT SPM 06-10-01.001.

Part: FRAME — CRACKED (BS 680) · airframe 39,857 hrs · 27,852 cycles

CRACKED FRAMES BS 680 BETWEEN LONGERON 25-28R. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37.

Part: PAN — CRACKED (R1 DOOR) · airframe 39,857 hrs · 27,852 cycles

CRACK ON PAN AT BS 170 AND Z 11.063 ON FWD R1 SERVICE DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK OF 0.312" WAS FOUND IAW NDTSPM 06-10-01. THE CRACK WAS STOP DRILL IAW SRM 52-00-00 FIG. 202. NO CRACKS FOUND AFTER STOP DRILL, IAW NDTSPM 06-10-01 .001. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-00-00 FIG. 202 AND INSTALLED IAW SRM 52-00-00 FIG. 202 REPAIR. 3.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 39,857 hrs · 27,852 cycles

DAMAGED FLOOR PANEL. FLOOR PANEL REPLACED IAW DWG 9936639 REV: P.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,857 hrs · 27,852 cycles

CRACKED CLIP STA Y=1022 BTW LONG 16 AND 17 LT SIDE AT PAX CABIN. DAMAGED CLIP WAS REPLACED PER DWG 9912243 REV JS AND SRM 51-20-09.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION ON FLOOR SUPPORT X=0 STA AND Y= 218 AT W1 AREA (S/N 00489). NEW SUPPORT FLOOR PANEL WAS INSTALLED PER SRM 51-41-02.

Part: WINDOW — CRACKED (BS 427-446) · airframe 39,857 hrs · 27,852 cycles

CRACKED UPPER FWD CORNER WINDOW BETWEEN BS 427 AND 446. REPAIRED IAW SRM 56-20-02 REPAIR 1 TYPE C FIG 203. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01. 001. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 56-20-02 REPAIR 1 TYPE C FIG 203.

Part: FLOOR SUPPORT — CORRODED (BS 200-256) · corrosion level 2 · airframe 39,857 hrs · 27,852 cycles

CORROSION AND ENLONGATED HOLES ON FLOOR SUPPORT FROM BS 200 TO 256, X 15, W1. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-01 AND 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 541 TO 560, RBL 56. R & R CUSP WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

AFT PIT FWD BULKHEAD INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 258 LBL 44. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

RIGHT CUSP WEB RING STIFFENER CRACKED AT BS 655. R & R CUSP WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

INTERCOSTAL CRACKED AT LT MLG DOOR AT BS 750.2729. R & R INTERCOSTAL IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB MEMBRANE CRACKED AT BS 200.5 RBL 18. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN RT CUSP WEB CRACKED AT STATION 398. REPAIRED WEB IAW SRM & EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN RT CUSP WEB CRACKED AT STATION 541. REPAIRED WEB IAW SRM & EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 487.5 RBL 59. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN RT CUSP WEB CRACKED AT STATION 446. REPAIRED WEB IAW SRM & EA.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

AFT CARGO COMPARTMENT CARGO TRACK SUPPORT FITTING CORRODED AT BS 946 BETWEEN STRINGER 28R TO 27R. R & R FITTING IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

AFT CARGO COMPARTMENT RT INTERCOSTAL CORRODED STRINGER 28R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 34,353 hrs · 23,409 cycles

RIGHT ELEVATOR CONTROL TAB TE UPPER SURFACE DELAMINATED. REPAIRED TAB IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FLOOR PANEL 222 AQF CRACKED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FLOOR PANEL 222 MF CORRODED. REPAIRED PANEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200 BETWEEN LBL 6 TO RBL 6. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FLOOR PANEL 221 GF CORRODED. R & R PANEL IAW SRM.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK MOUNT FITTING CORRODED BETWEEN BS 195 TO 200 LBL 22. R & R FITTING IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN LT CUSP WEB CRACKED AT STATION 579 TO 598. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 736 TO 756. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

LT CUSP WEB CORRODED BETWEEN BS 229 TO 313. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

LEFT CUSP WEB CORRODED AT BS 223 LBL 54. REPAIRED CUSP WEB IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 34,353 hrs · 23,409 cycles

RIGHT FWD OVERWING EMER EXIT IDENTIFIER SIGN LIGHT HOUSING CRACKED. R & R SIGN IAW AMM.

Part: HOUSING — CRACKED (CABIN) · airframe 34,353 hrs · 23,409 cycles

L1 DOOR EMER EXIT IDENTIFIER LIGHT ASSEMBLY HOUSING CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBEAM UPPER DECK FITTING CORRODED AT BS 218 RBL 54. R & R FITTING IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 34,353 hrs · 23,409 cycles

R1 DOOR EMER EXIT IDENTIFIER LIGHT HOUSING LENS CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED AT BS 229 RBL 44. R & R SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN RT CUSP WEB CORRODED AT STATION 889 TO 908. REPAIRED WEB IAW SRM & EA.

Part: LENS — CRACKED (EXIT SIGN) · airframe 34,353 hrs · 23,409 cycles

RIGHT FWD OVERWING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 34,353 hrs · 23,409 cycles

R1 DOOR UPPER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 34,353 hrs · 23,409 cycles

L1 DOOR UPPER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 34,353 hrs · 23,409 cycles

LEFT AFT OVERWING EMER EXIT IDENTIFIER LIGHT HOUSING CHIP BOARD LOCK CLIP BROKEN. R & R LIGHT IAW AMM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOOR BOARD PANEL 211ARF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOOR BOARD 211 ASF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,353 hrs · 23,409 cycles

AFT CARGO COMP RT CARGO TRACK CORRODED BETWEEN BS 994 TO 1022. REPAIRED TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 626 TO 655. REPAIRED WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 598 TO 626. REPAIRED CUSP WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

C2 DOOR AFT CUT OUT PANEL WEB CORRODED BETWEEN BS 990 TO 996 BETWEEN LONGERON 28R TO 24R. REPAIRED WEB IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL 221 KF DELAMINATED. REPAIRED PANEL IAW MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL 211 ALF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOOR PANEL 221 SF CORRODED AT FWD CORNERS. R & R PANEL IAW AMM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL DELAMINATED AT FLOOR 221DF. REPAIRED PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL DELAMINATED AT FLOOR 221CF. REMOVED PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL 222AEF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 34,353 hrs · 23,409 cycles

MARKED CARGO COMPARTMENT FLOOR PANEL 181DF CORRODED. R &R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOORBOARD PANEL 224UF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

AFT SIDE OF FORMER ON FRAME CORRODED AT BS 1022 BETWEEN LONGERON 30L TO 29L. REPAIRED FORMER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB CORRODED AT STATION 218 RBL 54. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB CORRODED AT STATION 217 RBL 54. REPAIRED WEB IAW SRM.

Part: RETAINER — CRACKED (R1 DOOR) · airframe 34,353 hrs · 23,409 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR RETAINER CRACKED. R & R RETAINER IAW SRM & AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 946 TO 954 BETWEEN LONGERON 30R TO 29R. R & R INTERCOSTAL IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 218 RBL 46. R & R CUSP WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FLOOR WEB SKIN CORRODED AT BS 148, RBL 36. REPAIRED WEB IAW AMM, SRM & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589 TO 899 RBL 54. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 218 TO 589 RBL 54. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 TO 256 LBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 TO 256, LBL 44. R & R TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 216 TO 256 LBL 54. R & R SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200 BETWEEN LBL 9 TO LBL 13. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 34,353 hrs · 23,409 cycles

R1 DOOR EMER EVAC SLIDE FWD GIRT BAR FITTING CORRODED. R & R FITTING IAW SRM & AMM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 34,353 hrs · 23,409 cycles

R1 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING CORRODED. R & R FITTING IAW SRM & MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

L1 DOOR FLOOR SUPPORT CORRODED. REPAIRED SUPPORT IAW SRM & DWG.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FORWARD CARGO DOOR CUT OUT PAN AFT SECTION CRACKED. R & R PAN IAW SRM.

Part: PIN — CRACKED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FORWARD CARGO DOOR CUT OUT LOWER CHORD PIN CRACKED. R & R PIN IAW SRM.

Part: WIRE — LOOSE (CABIN) · airframe 34,353 hrs · 23,409 cycles

AFT FUSELAGE OVERHEAD LIGHT WIRE LOOSE BETWEEN BS 1116 TO 1133, STRINGER 3L. SECURED WIRE IAW AMM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,353 hrs · 23,409 cycles

FORWARD CARGO DOOR CUT OUT PAN LOWER SECTION CORRODED. REPAIRED PAN IAW SRM.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 34,353 hrs · 23,409 cycles

LEFT MLG DOOR FWD FACE CHANNEL CRACKED. R & R CHANNEL IAW SRM & DWG.

Part: ENGINE — FAILED (LEFT) · airframe 34,618 hrs · 23,593 cycles

INFLIGHT SHUTDOWN & DIVERSION. LT ENG COMPRESSOR STALL ALERT DURING CRUISE, LOUD BANG & CONTINUED EVEN WITH ENG AT IDLE & ALL ANTI-ICE ON. R & R NR 1 ENG IAW TC.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 31,800 hrs · 21,772 cycles

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

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

LEFT WING TO BODY PANEL 150 CC SUPPORT BRACKET CRACKED AT STA 674. REMOVED AND REPLACED BRACKET IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

WEB CRACKED AT BS 674, LBL 47. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 737, LBL 44. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 737, RBL 44.0. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 653, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

VERTICAL SUPPORT ANGLE CRACKED AT BS 665, RBL 20. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

RIGHT INTERCOSTAL CRACKED AT BS 715, LONGERON 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

SEAT TRACK SUPPORT FITTING CRACKED AT BS 715, RBL 54. REMOVED AND REPLACED FITTING IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

SEAT TRACK CORRODED BETWEEN STA 342 TO STA 589, RBL 54. REMOVED AND REPLACED SEAT TRACK IAW SRM AND MM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

FLOOR PANEL 221XF CORRODED. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

FLOOR PANEL 222EF CORRODED. REMOVED AND REPLACED FLOOR PANEL 223EF IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

FLOOR PANEL 222ADF CORRODED. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

RIGHT CUSP WEB CORROSION BETWEEN STA 484-465. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

WEB CRACKED AT BS 674, RBL 47. REPAIRED CUSP WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 31,103 hrs · 21,342 cycles

L1 DOOR INSIDE HANDLE AREA ANGLE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: STRAP — CRACKED (RT WING) · airframe 31,103 hrs · 21,342 cycles

RIGHT WING FIXED L/E - THE MOST I/B SIDE BONDING STRAP CRACKED. REMOVED AND REPLACED STRAPS IAW SRM.

Part: STRAP — CRACKED (CARGO BAY) · airframe 31,103 hrs · 21,342 cycles

AFT CARGO FWD BULKHEAD GILLINER SUPPORTS CRACKED. REMOVED AND REPLACED STRAPS IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

AFT CABIN EMERGENCY EXIT DOOR JAMS UPPER TRIM CRACKED. REPAIRED JAMB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

AFT ACCESS COMP ANGLE CRACKED AT BS 114, LONG 1L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

FRAME CRACKED AT BS 715, RIGHT ON FWD FLANGE. REMOVED AND REPLACED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,103 hrs · 21,342 cycles

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

Part: PANEL — CRACKED (RT WING) · airframe 31,103 hrs · 21,342 cycles

RIGHT WING TO BODY FAIRING CRACKED AT L/E, PANEL 160SR. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,103 hrs · 21,342 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,103 hrs · 21,342 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED. REMOVED AND REPLACED PANEL IAW B717 SRM.

Part: STIFFENER — CRACKED (FLOOR PANEL) · airframe 31,103 hrs · 21,342 cycles

MAIN CABIN FLOOR PANEL 222YF CRACKED STRIP. REMOVED AND REPLACED STIFFENERS IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 31,103 hrs · 21,342 cycles

MAIN CABIN FLOOR PANEL 222ADF CHANNEL CRACKED. REMOVED AND REPLACED STIFFENERS IAW SRM & AMM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

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

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,103 hrs · 21,342 cycles

NLG STRUT DOOR AFT HINGE CUTOUT CRACKED RIGHT SIDE. REPAIRED DOUBLER IAW SRM.

Part: WEB — CRACKED (CARGO DOOR) · airframe 31,103 hrs · 21,342 cycles

AFT CARGO DOOR LOWER CENTER RIB CRACKED AT STOP FITTING FWD & AFT SIDE. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 31,003 hrs · 21,283 cycles

DURING APPROACH GEAR WOULD NOT COME DOWN WHEN EXTENDING GEAR. BROUGHT HANDLE BACK UP RECYCLED GEAR AND THEN GEAR FINALLY CAME DOWN WITH 3 GREEN. FIRST ATTEMPT ALL RED INDICATION ON PANEL AND CONFIGURATION PAGE. REMOVED AND REPLACED PSEU AS PE

Part: LIGHT — MISSING (CABIN) · airframe 30,708 hrs · 21,101 cycles

SEAT 3D EMERGENCY LIGHT BULB AND LENS MISSING AT ONE SEAT POSITION. INSTALLED EPL BULB A 3D. REF AMM MDDR CLOSED DESK 2 DISPATCH 109892.

Part: LENS — MISSING (CABIN) · airframe 30,708 hrs · 21,101 cycles

REF L/P 8478987, SEAT 3D CLEAR EMERGENCY LIGHT LENS MISSING AT ONE POSITION. INSTALLED PL LENS AT 3D. REF AMM MDDR CLOSED DESK 2 DISPATCH 109892.

Part: SCREW — LOOSE (EVAC SLIDE) · airframe 28,419 hrs · 19,591 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER SCREW LOOSE. REPAIRED SLIDE PER MM.

Part: LENS — MISSING (CABIN)

ESCAPE PATH LIGHT COVER MISSING 11D. INSTALLED ESCAPE PATH LIGHT LENS PER MM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN GALLEY INOP. PERFORMED FIM TASK 33-50 TASK 801 FOUND NO OUTPUT POWER AT PIN 9 OF BATTERY PACK B5-259. REMOVED AND REPLACED BATTERY POWER SUPPLY ASSY AT LOCATION B5-259 OPS CHECKED NORMAL - REF B717 AMM 33-51-03.

Part: LIGHT — MISSING (CABIN)

EMERGENCY ESCAPE LIGHT COVER 1D MISSING. INSTALLED LIGHT COVER AS REQ OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT AT SEAT 2D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 2D IAW B717 MM 33-51. OPS CHECK OK.

Part: TEE FITTING — CRACKED (LT PYLON)

LEFT ENGINE PYLON BRACKET "T" FITTING, CRACKED. ACCOMPLISHED PYLON BRACKET "T" FITTING REPLACEMENT PER B717 SRM 51-40-02 AND 51-10-04 AND EA 17-54-02521A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180 TO 240, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-10-04, 51-30-08, 51-22-01, 51-41-01, 51-41-02 AND BOEING DWG 9936534.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 237, RBL 20, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 51-10-04 AND 53-20-52.

Part: SEAT TRACK — GOUGED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 237, RBL 20, GOUGED. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 53-20-52, 51-41-02 AND BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, LBL 14 TO LBL 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, LBL 20 TO RBL 20, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02 AND BOEING DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 180, LBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 180, LBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02, 51-22-01, 51-41-05 AND BOEING DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR "T" SUPPORT, STA 180, LBL 22, CORROSION. ACCOMPLISHED FLOOR "T" SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 10 TO LBL 13, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02 AND BOEING DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, RBL 0 TO RBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 51-10-04, 51-40-08, AND 51-40-02 AND BOEING DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 180, RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-41-02, 51-40-08, 51-20-09, 51-10-4, AND 51-41-02 AND BOEING DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN LAVATORY FLOOR SUPPORT, STA 176 TO 180, LBL 21 AND 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-08, 51-10-04 AND 51-41-02.

Part: GIRT BAR — OBSTRUCTED (SERVICE DOOR)

SERVICE DOOR GIRT BAR WILL NOT STAY ENGAGED IN LOCKED POSITION. REMOVED DEBRIS FROM REAR GIRT BAR FITTING. OPS NORMAL.

Part: LENS — MISSING (CABIN)

ESCAPE PATH WHITE LIGHT AT ROW 22 MISSING. INSTALLED MISSING LENS AS REQUIRED, LIGHT OPS GOOD.

Part: COVER — MISSING (CABIN)

FPL COVER AT ROW 10 MISSING (WHITE). REPLACED COVER AND LAMPS. CHECKED OK, IAW AMM 33-51.

Part: WIRE — EXPOSED (CABIN)

SEAT 25D WIRE BUNDLE EXPOSED AT FLOOR TRIM ON WALL. SEAT 24 EMERGENCY LIGHTS INOP. RE-SECURED WIRE AT SEAT 25D IN REF TO B717 SWPM 20-10-03. SEAT 24 EMERGENCY LIGHT OPS CHECKS GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEAT ROWS 25 FED TO 31 FED EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY, OPS CHECK GOOD. REF MM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING TEST OF EMERGENCY LIGHT SYSTEM, ESCAPE PATH LIGHTING ASSOCIATED WITH STATION 804R WOULD NOT ILLUMINATE. REPLACED STATION 804R EMERGENCY BATTERY PACK/CHARGER IAW AMM 33-51.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

FOUND R-1 GIRT BAR INSTALLED IN TRACK ON FLOOR, BOTH PINS REMOVED (INFLATION SAFETY). REMOVED AND REPLACED R-1 DOOR SLIDE. OPS CHECK OK REF MM 25-61.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

CHECK R-1 DOOR GIRT BAR. FOUND R-1 DOOR GIRT BAR INSTALLED IN TRACK ON FLOOR. REMOVED AND REPLACED R-1 DOOR SLIDE. OPS CHECK OK REF MM 25-61.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR LOWER JAMB CORROSION OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO DOOR LOWER JAMB.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

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: SKIN — CRACKED (VERTICAL STAB)

VERTICAL STAB RT SKIN CRACKED JUST BELOW HORIZONTAL STAB CUTOUT. COMPLIED WITH EA 17-55-01183A. MAJOR REPAIR, FORM 337 SUBMITTED.

Part: FRAME — CRACKED (BS 1178 L16-18L)

CRACK ON CANTED FRAME STA 1178.225 BETWEEN LONGERON 16 LT AND 18 LT. INSTALLED ANGLE REPAIR 16 X 2 INCHES MAT USED 7075.0 0.80. HEAT TREATMENT TO 7075T6 GENERAL PROCESS SPECIFICATION 98 PMS 247.PS 01 AS PER SRM 51-70-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS AT ROWS 20 THROUGH 24 INOP (END BAYS). REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM CHAPT 33-51 OP'S CHECK GOOD.

Part: ENGINE — INOPERATIVE (NR 1)

LEFT ENGINE COMPRESSOR STALLS AND ROLL BACK AT FL310. REMOVED AND REPLACED LEFT ENGINE.

Part: BRACKET — BROKEN (RUDDER LIMITER) · airframe 1,669 hrs · 1,525 cycles

DURING ROUTINE INSPECTION OF THE TAIL COMPARTMENT, RUDDER LIMITER BRACKET ASSEMBLY, PN 5914138503 WAS FOUND BROKEN. THERE WAS NO INBOUND REPORT OF RUDDER LOAD FEEL OR HANDLING PROBLEMS ON THE FLIGHT. SUSPECT CONNECTING LINKAGE (ITEM NR 105) MOVED WITH RIGH PIN INSTALLED, CAUSING BRACKET (ITEM NR 85) TO BRAKE.