N988AT

Part: BOLT — SHEARED (ZONE 700) · airframe 58,500 hrs · 41,064 cycles

SHIP 9521 -ATB/GEAR/DE- THE FLIGHT CREW PERFORMED AN AIR TURN BACK TO CLT DUE TO A "RIGHT MAIN LANDING GEAR UNSAFE" MESSAGE WITH AN ASSOCIATED "RIGHT GEAR DOOR OPEN" MESSAGE. THE ALTERNATE GEAR EXTENSION LEVER WAS PULLED. AN EMERGENCY WAS DECLARED WITH ATC. CORRECTIVE ACTION: MAINTENANCE FOUND THE RT MLG DOOR ACTUATOR EYE-BOLT NUT LOCKING TAB SHEARED CAUSING THE PISTON ROD TO BACK OFF THE EYEBOLT. INSTALLED A SERVICEABLE LOCKING TAB AND RIGGED THE RT MLG DOOR PER B717 AMM 32-34-03. (LP #6746516)

Part: FUEL TANK — CORRODED (BS 747) · airframe 57,383 hrs · 40,076 cycles

-AD- CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-32 AT LH MLG WHEEL WELL (AREA UNDER MLG CABLE FITTING). SUMMARY OF NRC 00775: CORROSION LEVEL 1. CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-32 AT LH MLG WHEEL WELL (AREA UNDER MLG CABLE FITTING) WAS REPAIRED PER ER/A 618122-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 618122-14 REV 2. ASSOCIATED ER/A 14-618122 ADDED FOR AC 9521. (LP #0351865)

Part: SKIN — CORRODED (BS 870-896 L27R) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDURE 1. PERFORM AN EXTERNAL VISUAL INSPECTION INITIAL AT 8,000 CYCLES AND REPETITIVE EVERY 8,000 CYCLES PER B717 SRM 53-20-70-2R REPAIR 1 PAR 7. (LP #0320030)

Part: FRAME — CORRODED (BS 869 S29L-29R) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION AT FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00298: CORROSION LEVEL 2. FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3. PERFORM VISUAL INSPECTION INITIAL 25,000 CYCLES, REPETITIVE 6,500 CYCLES PER B717 SRM 53-20-07-2R PROCEDURE 3. (LP #0312583)

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00525: CORROSION LEVEL 2. RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215. (LP #0309257)

Part: FLOOR SUPPORT — CORRODED (BS 177-200) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00626: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE WERE FABRICATED PER B717 DWG 9936534 AND REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0310692)

Part: WINDOW FRAME — CRACKED (COCKPIT RIGHT) · airframe 57,383 hrs · 40,076 cycles

CRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION EVERY C CHECK PER B717 SRM 56-10-02-2R-1 PROCEDURE 1 - REPAIR, STEP 6.A TABLE 203. **REDEFERRED LOG TO QC, ESTAB MON INSP **00-0556-8-6608 S/N 09521 REP. (LP #0310423)

Part: WINDOW FRAME — CRACKED (COCKPIT RIGHT) · airframe 57,383 hrs · 40,076 cycles

CRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION EVERY C CHECK PER B717 SRM 56-10-02-2R-1 PROCEDURE 1 - REPAIR, STEP 6.A TABLE 203. (LP #0310272)

Part: FRAME — CRACKED (BS 969) · airframe 57,383 hrs · 40,076 cycles

-A.D.- CRACK OF 0.250IN LENGTH WAS FOUND ON UPPER RADIUS OF THE FRAME TAB ON THE LH OVERWING FRAME STA Y=696, IN REF CARD 5310-01436-04B JOB #063-0002 STEP: 10. SUMMARY OF NRC 00522: FRAME TAB ON THE LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND SRD SR95530013. ASSOCIATED AA 5310-01436 ADDED FOR AC 9521. (LP #0306723)

Part: CUSP WEB — CRACKED (BS 610) · airframe 57,383 hrs · 40,076 cycles

CRACK ON RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-PROCEDURE 4. REPAIR 4. (LP #0306797)

Part: LONGERON — CRACKED (BS 1133 L2L) · airframe 57,383 hrs · 40,076 cycles

CRACK ON LONGERON 2LH FROM STA 1133 OF AFTER ACCESSORIES. SUMMARY OF NRC 00389: LONGERON 2LH STA 1121 TO STA 1136 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2 REPAIR 2. (LP #0307355)

Part: PAN — CRACKED (L1 DOORWAY) · airframe 57,383 hrs · 40,076 cycles

CRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200. SUMMARY OF NRC 00193: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0305238)

Part: PAN — CRACKED (L1 DOORWAY) · airframe 57,383 hrs · 40,076 cycles

CRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160. SUMMARY OF NRC 00191: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDER 3 REPAIR 3. (LP #0305244)

Part: BEAM — CRACKED (L1 DOOR BS 200) · airframe 57,383 hrs · 40,076 cycles

CRACK ON BEAM #1 OF L1 DOOR STA Y=200. SUMMARY OF NRC 00194: BEAM #1 OF L1 DOOR STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0302430)

Part: CUSP WEB — CORRODED (BS 530-578) · airframe 57,383 hrs · 40,076 cycles

CORROSION ON LH CUSP WEB, OUT OF LIMITS PER B717 SRM 53-00-55-1A-1 ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00701: CORROSION LEVEL 2. RING DOUBLER ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND REPLACED PER B717-200 SRM 53-00-55-2R-4. FIG 207. (LP #0301173)

Part: DOOR FRAME — CORRODED (BS 201-203) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00700: CORROSION LEVEL 2. DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0300920)

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 57,383 hrs · 40,076 cycles

CRACK (3 EA) ON LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX. SUMMARY OF NRC 00717: LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 205. (LP #0300923)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00070: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0300206)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 57,383 hrs · 40,076 cycles

CRACK ON PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00320: PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0298813)

Part: CUSP WEB — CRACKED (BS 813) · airframe 57,383 hrs · 40,076 cycles

CRACK ON RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00526: RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 1. (LP #0292417)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,383 hrs · 40,076 cycles

CORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00072: CORROSION LEVEL 2. FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 FIG 201. (LP #0290334)

Part: CUSP WEB — CORRODED (BS 655-715) · airframe 57,383 hrs · 40,076 cycles

CRACK ON LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0289323)

Part: WEB — CRACKED (BS 218-223) · airframe 57,383 hrs · 40,076 cycles

CRACKED WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00580: WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0290917)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,873 hrs · 39,647 cycles

AT L1 DOOR CLOSURE PRIOR TO PUSH-BACK, GATE AGENT NOTICED DAMAGE TO BOTTOM FWD EDGE OF L1 DOOR. DAMAGE IS APROX 5" LONG. EDGE ROLLED BACK APROX 3/8". REMOVED DAMAGE PER SRM 52-10-01-2R-1. PERFORMED HFFC PER B717 NDT SPM PART 6-10-01.001. NO CRACKS FOUND QC 2099. INSTALLED REPAIR FILLER AND DOUBLER PER B717 SRM 59-10-01-2R-1 C. FINISH RESTORED, DOOR LINER REINSTALLED REF. B717 AMM 52-11-03. PRESSURIZATION CHECK L1 DOOR OK. A/C OK FOR SERVICE. (LP #5006794)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,765 hrs · 38,694 cycles

RAMP REPORTED DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE TO PREVIOUS REPAIR SPLICE ONLY. REMOVED SPLICE TO PREPARE FOR REPLACEMENT. NO OPEN HOLE REQUIRED. INSTALLED REPAIR PER B717 SRM 53-20-15-2R PROC 4 PERMENANT REPAIR. (LP #4798350)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,512 hrs · 38,464 cycles

SHIP 9521 -ATB/GEAR- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT TO DTW FOLLOWING THE FAILURE OF THE NOSE LANDING GEAR TO RETRACT. CORRECTIVE ACTION: MAINTENANCE ADJUSTED NOSE LANDING GEAR RETRACT ACTUATOR. (LP #4110406)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,467 hrs · 38,427 cycles

FOUND TWO FORWARD UPPER RIGHT OVERWING CABIN EXIT LIGHTS AND ONE CEILING AISLE LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED TWO EMERGENCY LIGHT POWER SUPPLY BATTERIES PER B717 AMM 33-51-03 PAGEBLOCK 401. OPERATIONAL CHECK WAS GOOD. (LP #9428982)

Part: NONE — NONE · airframe 55,074 hrs · 38,084 cycles

"FAA APPROVAL PENDING" FOR ERA 605849-14 REV ORIG. FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE SECTION I PERMANENT REPAIR INSTRUCTIONS. SUMMARY SEE NRC 003-0001:0514-2001/005 00005: COMPLIED WITH ER/A PRI 605849-14 REV A PRI REV 0 REPAIR INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 605849-14 REV A. WITH FINAL FAA APPROVAL FOR FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE MATCH WITH COMPLETED INSTRUCTIONAL STEPS COMPLETED ON ER/A PRI 605849-14 REV A PRI 0. ALL STEPS MATCH. CLOSING REQUIREMENTS RII: INSPECTOR 00390989. (LP #2628797)

Part: UNKNOWN — UNKNOWN · airframe 55,043 hrs · 38,050 cycles

C/W ERA 605849-14 REV ORIG, FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L26. SUMMARY NRC 003-0001:0514-2001/001 00001: COMPLIED WITH ER/A PRI 605849-14 REV "0","1","2","3". ALL REPAIR INSTRUCTION STEPS, ENSURE FINALE ER/A 605849-14 REV. ORIG. SECTION I PERMANENT REPAIR INSTRUCTIONS FOR FUSELAGE SKIN / STA 1002 - STA 1022 / L-24-L-26. GROUND DAMAGE MATCH WITH COMPLETED INSTRUCTIONAL STEPS COMPLETED ON ER/A PRI 605849-14 REV "0","1","2","3". (LP #2625566)

Part: NONE — NONE · airframe 55,047 hrs · 38,053 cycles

COMPLY WITH FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L-26 PER ER/A 605849-14 REV ORIG. C/W ER/A 605849-14 REV ORIG. PERMANENT REPAIR AND ER/A 605849-14 REV A. RII C/W. ASSOCIATED ER/A 14-605849 ADDED FOR AC 9521. (LP #4025639)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 55,043 hrs · 38,050 cycles

LONGERON 24R CORRODED FROM STA 1000-1035. SUMMARY NRC 003-0001:0514-2001/002 00002: REPLACED LONGERON REF DAC DWG 5911424. (LP #2625262)

Part: LENS — MISSING · airframe 54,927 hrs · 37,949 cycles

THE 1R DOOR EXIT SIGN LENSE WAS MISSING ON PREFLIGHT. MAINTENANCE INSTALLED THE 1R DOOR EXIT SIGN LENSE REF B717 IPC 33-51. (LP #9884344)

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 ENGINE) · airframe 54,875 hrs · 37,907 cycles

SHIP 9521 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO BNA FOLLOWING A "FIRE" WARNING INDICATION ON THE #2 ENGINE WITH ANTI-ICE ON. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED WITH ATC, AND THE SUBSEQUENT OVERWEIGHT LANDING WAS UNEVENTFUL. CFR DID MEET THE AIRCRAFT ON THE RUNWAY AND CONFIRMED THAT NO FIRE EXISTED. CORRECT ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE FDCU, BOTH VIA, AND PERFORMED ABOVE IDLE PNEUMATIC LEAK CHECKS. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9884314)

Part: TRANSMITTER — FAULTED (FLAP SYSTEM) · airframe 54,669 hrs · 37,714 cycles

DECLARED EMERGENCY DUE TO AN INTERMITTENT FLAP DISAGREE INDICATION. STARTING AT 12000 FT, PFD SPORADICALLY SHOWED FLAPS 0 & PICTURE OF UNDERWING ON CONFIG PAGE. CREW REPORTED NO ADVERSE FEEL. CONTINUED THROUGH 25000 FT UNTIL THE FLAPS DISAG ON EICAS WITH SPLIT FLAPS INDICATIONS 0/25 ACCOMPANIED WITH A STICK SHAKER. AIRCRAFT STAYED LEVEL AT 25K FT, EVENTUALLY ALL INDICATIONS RETURNED TO NORMAL, AND FLIGHT CONTINUED TO DESTINATION. APPROACH & LANDED WITHOUT FURTHER INCIDENT.. , THE RIGHT FLAP POSITION TRANSMITTER WAS REPLACED IAW AMM 27-54. ALL ADJUSTMENTS WERE COMPLIED WITH IAW AMM 27-54. FUNCTIONAL TESTED GOOD IAW AMM 27-54. ALL RETURN TO SERVICE TESTS OF FLAP SYSTEM CHECKED GOOD IAW AMM 22-00.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 54,619 hrs · 37,672 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01 AND AMDS CARD 5352-4002. (LP #2497968)

Part: NONE — NONE · airframe 54,300 hrs · 37,383 cycles

CAPTAIN WINDSHIELD ARCING ON DESCENT. MCC FCP DEFERRED. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED AT CHA PER MEL 30-41-01B. REPLACED CAPTAIN WINDSHIELD PER B717 AMM 56-11. MEL AND PLACARD REMOVED. (LP #2402013)

Part: NONE — NONE · airframe 54,260 hrs · 37,341 cycles

AIRCRAFT 9521, DURING SVC CHK FOUND BATTERY 7 (685R) FOR EMERGENCY LIGHTS DRAINED. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY ASSEMBLY AT LOCATION 7 (685R). (LP9115548)

Part: TAILPIPE — PLUGGED · airframe 53,310 hrs · 36,481 cycles

SHIP 9521 - THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO ATL AND LANDED WITHOUT FURTHER INCIDENT AFTER THE #2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING CLIMB OUT. AT FL230, A LOUD REPORT WAS HEARD, FOLLOWED BY STRONG VIBRATIONS (9.9 UNITS) FROM THE ENGINE, THEN THE OIL PRESSURE DROPPED BELOW RED-LINE, AND THE CREW SHUT DOWN THE #2 ENGINE. THE CABIN CREW REPORTED THAT THERE WAS SMOKE ACCUMULATING IN THE CABIN DURING THIS ENGINE FAILURE EVENT. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN THE #2 ENGINE TAIL PIPE AND REPLACED THE ENGINE. (LP #8831952)

Part: LANYARD — OUT OF POSITION · airframe 53,302 hrs · 36,472 cycles

GIRT BAR LANYARD WAS FOUND TO BE NOT ATTACHED TO PASSENGER DOOR. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE LANYARD WAS NOT LOOPED AROUND THE GIRT BAR. PLACED THE GIRT BAR THRU LANYARD AND ARMED THE DOOR. NO OTHER ISSUES. OPERATIONAL CHECK WAS GOOD PER B717 AMM 25- 61. (LP #8831930)

Part: NONE — NONE · airframe 52,554 hrs · 35,818 cycles

SHIP 9521 - THE CREW DECLARED AN EMERGENCY DURING THE APPROACH FOR LANDING IN ATL DUE TO THE LOSS OF LEFT HYDRAULIC SYSTEM FLUID QUANTITY. CORRECTIVE ACTION: MAINTENANCE FOUND THE SOURCE OF THE LEAK AND REPLACED THE DAMAGED SECTION OF A HYDRAULIC LINE NEAR THE LEFT THRUST REVERSER CONTROL VALVE. THE LEAK CHECK AND OPERATIONAL CHECK WERE GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #8186722)

Part: NONE — NONE · airframe 52,310 hrs · 35,589 cycles

R1 DOOR SLIDE PINS PULLED OUT WHEN DOOR WAS OPENED FROM THE OUTSIDE. THE SLIDE DID NOT DEPLOY AS DESIGNED. THIS IS A FAILURE OF PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE R-1 DOOR SLIDE BOTTLE PIN WAS INSTALLED AND THE SLIDE WAS REMOVED FROM THE DOOR. A NEW SLIDE WAS INSTALLED AT R-1 IAW AMDS WORK CARD 2561-9005. (LP #8920201)

Part: COVER — MISSING (LT WING TE FLAP) · airframe 51,019 hrs · 34,443 cycles

A FLAP COVER ON LEFT WING (CIRCLER 2" DIAMETER COVER) ON UNDER SIDE IS MISSING LOCATED NEAR FUSELAGE BY GEAR BAY. MAINTENANCE INSTALLED A NEW COVER. (LP #7576961)

Part: NUT PLATE — CORRODED (THRESHOLD) · airframe 50,721 hrs · 34,218 cycles

CORROSION AT C2 CARGO DOOR THRESHOLD ATTACH POINTS. BLIND NUT LOCATIONS. SEE NR 048-0008:5331-2001/003 00169: REPAIRED REF B717 SRM 53-20-15-2R PROCEDURE 7. (LP #1719805)

Part: HINGE — WORN (LT WING TE FLAP) · airframe 50,721 hrs · 34,218 cycles

LEFT WING. SEALANT MISSING/CRACKED WITH ATTACH HARDWARE RUSTY. OUTBOARD WING FLAP HINGE CONNECTION POINT. -MARKED- REPAIRED WORN FLAP HINGE PER PRI 589529-14 REV 1 AND PER ER/A 589529-14. (LP #1720421 )

Part: STRUCTURE — CORRODED (CARGO DOORWAY) · airframe 50,721 hrs · 34,218 cycles

CORROSION INSIDE LIGHTENING HOLE AT C2 DOOR OPENING STA 960. SEE NR 048-0008:5331-2001/006 00172: REPAIRED REF ER/A 589573-14 REV O. PRI AND ER/A MATCH CLOSING REQUIREMENTS RII: INSPECTOR 00466532. (LP #1720023)

Part: SPAR CAP — CRACKED (VERT STABILIZER) · airframe 50,721 hrs · 34,218 cycles

ONE EACH FASTENER HOLE WITH A BHEC CRACK INDICATION ON RT VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP FORWARD FLANGE. CRACK IS IN FIRST FASTENER HOLE BELOW ZFS=52.267, MARKED. REFERENCE: AA 5530-01048, AD 2018-10-08 STEP 16B. COMPLIED WITH PRI 589482-14AD REV O-2, PRI 589482-14AD REV O-2 MATCHES ER/A 589482-14AD REV O, REPAIR PER ER/A 589482-14AD REV O.

Part: SHEAR TIE — CORRODED (BS 1002) · corrosion level 2 · airframe 50,721 hrs · 34,218 cycles

CORROSION ON FUSELAGE FRAME AND SKIN CLIP AT STA 1002 LONGERON 28L. REPAIRED FRAME AND SKIN CLIP AT STA 1002, PER B717 SRM 53-20-07-2R ON NRC 186.

Part: STRUCTURE — CORRODED (BS 1022) · corrosion level 2 · airframe 50,721 hrs · 34,218 cycles

THE AFT CARGO BIN SHOWS EVIDENCE OF SURFACE CORROSION AT J FRAME AT STA 1022, BETWEEN STR 29L-29R. LOCATED JUST FORWARD OF LAV TANK VENT MOTOR, MARKED. COMPLETED REPAIR AT J FRAME AT STATION 1022 BETWEEN STR 29L-29R, REF B717 SRM 53-20-07-2R. ALL WORK COMPLETED ON NRC 139.

Part: SKIN — DAMAGED (VERTICAL STAB LE) · airframe 54,501 hrs · 37,567 cycles

AIRCRAFT 9521, WHILE IN ATL FOR C-CHECK, MAINTENANCE WAS PERFORMING INSPECTIONS PER WORKCARD 5530-01048-02 AND FAA AD 2018-10-08 ON THE VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. DURING WORKCARD ACCOMPLISHMENT, MTC REPORTED CRACK INDICATIONS AT ONE EXISTING FASTENER HOLES IN THE RH FRONT SPAR CAP LAYER FORWARD FLANGE BELOW ZFS=52.267. UPON LAYER SEPARATION, NO INDICATION WAS NOTED IN EITHER LAYER HOWEVER THE HOLE COMMON TO THE SKIN WAS NOTED TO BE ELONGATED. CORRECTIVE ACTION: THIS ER/A 589482-14 PROVIDES INSTRUCTIONS TO OVERSIZE THE HOLE IN SKIN LAYER ONLY AND ACCOMPLISH A BUSHING REPAIR PER BAC DWG SG95550001. LP 1712123

Part: HINGE FITTING — DAMAGED (LT WING TE FLAP) · airframe 54,619 hrs · 37,672 cycles

WHILE IN ATL FOR SCHEDULED MAINTENANCE, THE #4 OUTBOARD FLAP HINGE FITTING (LH WING) COMMON TO THE IDLER HINGE FITTING WAS FOUND TO BE ELONGATED. THIS ER/A AUTHORIZED MAINTENANCE TO REPAIR THE ELONGATED HOLE BY CLEANING THE HOLE, FABRICATE AND INSTALLING A NEW BUSHINGS. ERA 589529-14 PROVIDES INSTRUCTIONS FOR REPAIR ACCOMPLISHMENT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA ADVISORY CIRCULAR 120-93. PER ER/A 589529-14 REV A, SECOND STAGE DTE COMPLETE. ALL FOLLOW ON ACTIONS TO BE TRACKED VIA LOGPAGE 2458752. 24MO LIMIT IS REMOVED. OK TO CLOSE THIS LOG. ASSOCIATED ER/A 00-589529 ADDED FOR AC 9521. (LP #1710065)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,634 hrs · 34,139 cycles

THE EMERGENCY PATH LIGHTS FROM SEAT ROW 24 THROUGH 29 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK B5-231, PER B717 AMM 33-51. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,634 hrs · 34,139 cycles

THE EMERGENCY PATH LIGHTS FROM SEAT ROW 15 THROUGH 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK B5-120, PER B717 AMM 33-51. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,771 hrs · 32,739 cycles

EMERGENCY EXIT MARKERS @ L1, L2, AND OVERWING EXIT DOORS INOP. R/R BATTERIES PER AMM 33-51. OP'S CHECK GOOD. (LP5742980)

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 48,270 hrs · 32,373 cycles

RIGHT DOOR EXIT SIGN IS BROKEN. MAINTENANCE REPLACED THE R1 DOOR EMERGENCY LIGHT LENS ASSY PER B717 AMM 33-50. THE AIRCRAFT IS OK FOR SERVICE. (LP #5837084)

Part: LIGHT — DISCONNECTED (CABIN) · airframe 47,927 hrs · 32,142 cycles

FOUND EMERGENCY EXIT LIGHT OUT AT L1 DOOR. REMOVED & REINSTALLED FWD ATTEDENT SEAT TO FOM PER AMM 25-23. RECONNECTED EMER LIGHT. OPS CHECK GOOD. (LP #5545005)

Part: SIGN — MISSING (CSABIN) · airframe 47,927 hrs · 32,142 cycles

THE 1R DOOR EXIT SIGN IS MISSING. MAINTENANCE REINSTALLED THE LENS. (LP #5548399)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,736 hrs · 32,000 cycles

DURING SERVICE CHECK, MAINTENANCE NOTED THAT ONE FLOOR LEVEL EMERGENCY LIGHT WAS INOPERATIVE ON THE CATWALK. LIGHT L2-847. MAINTENANCE THEN FOUND A WIRE BROKEN AT THE CONNECTOR P1-3038. THE WIRE WAS REPAIRED PER SWPM 20-31. OPERATIONAL CHECK WAS GOOD. (LP #4327098)

Part: DOOR FRAME — CRACKED (RT OVERWING EXIT) · airframe 47,698 hrs · 31,969 cycles

AMDS 5310-01436-01C RIGHT OVER WING EXIT FRAME CRACKED AT STA 715. CONDITION 3 EXITS. REPLACED FRAME ON AMDS WORK CARD 5310-01436-03B. (LP #0928476)

Part: CAM — EXCESS PLAY (TAILCONE) · airframe 47,698 hrs · 31,969 cycles

TAIL CONE CAM ASSEMBLY HAS EXCESSIVE PLAY, REF NRC 186. MAINTENANCE REPLACED THE CAM ASSEMBLY REF B717 AMM 53-52-03. SEE NRC 186 FOR DETAILS. (LP #0926185)

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 47,698 hrs · 31,969 cycles

FORWARD CARGO COMPARTMENT: CORROSION AT FWD CARGO DOOR CUT OUT THRESHOLD. (MKD). NRC 001-0229:0593-2007/002 00031 REPLACED DOOR JAMB SECTION REF B717 SRM 53-20-15-2R REPAIR 6. (LP #0926097)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,056 hrs · 31,541 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 20C. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN LENS COVER. OK FOR SERVICE. (LP 0799210)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 46,146 hrs · 30,892 cycles

FRAME FORMER HAS DAMAGE AT FS 889 BETWEEN STR 27R-28R. REMOVED DAMAGED FRAME FORMER AND FABRICATED REPAIR PARTS PER 53-00-06-2R PROCEDURE 2 REPAIR 2. INSTALLED REPLACEMENT PARTS PER SRM 53-00-06-2R PROCEDURE 2 REPAIR 2.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,508 hrs · 30,420 cycles

EXIT SIGN LENS WAS FOUND TO BE MISSING, OVER THE R1 DOOR. MAINTENANCE INSTALLED THE LENS ASSEMBLY. SYSTEM IS OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,246 hrs · 30,240 cycles

FOUND WALKWAY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING. THE BATTERY PACK WAS REPLACED AND NOW THE LIGHT OPERATE NORMALLY.

Part: COVER — MISSING (EXIT SIGN) · airframe 44,664 hrs · 29,884 cycles

THE EXIT SIGN IN THE FIRST CLASS AISLE IS MISSING THE COVER. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE.

Part: SKIN — DAMAGED (WING) · airframe 42,698 hrs · 28,437 cycles

ELONGATED HOLE IN AFT SIDE OF PANEL OPENING 520QB. REPAIRED ELONGATED HOLE IN AFT SIDE OF PANEL OPENING 520QB IAW ER/A 553683-14 REV 0.

Part: DOOR — GOUGED (CABIN) · airframe 42,698 hrs · 28,437 cycles

AFT CABIN BULKHEAD DOOR HAS GOUGE IN SEAT STORAGE AREA LOWER LEFT CORNER. REPAIRED AFT CABIN BULKHEAD DOOR IAW SRM 52-10-02 REPAIR 15 AND REMOVED, REINSTALLED APB DOOR IAW AMM 52-12-03 400-801, NO LEAKS NOTED.

Part: SKIN — CRACKED (BS 1022) · airframe 42,698 hrs · 28,437 cycles

FUSELAGE SKIN BS 1022 ABOVE LONGERON 14R CRACKED. REPAIRED THE SKIN IAW ER/A 553675-14 REV 0.

Part: FORMER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,698 hrs · 28,437 cycles

LT FILLET FORMER AT STA 851 HAS CORROSION AROUND SCREW HOLES AT LOWER END. REPLACED LT FILLET FORMER "ITEM-10 ANGLE" AT STA 851 THAT WAS CORRODED BEYOND LIMITS NOMINAL .050" LOSS=.023 REMAINING .027" IAW SRM 51-41-02 0G, 53-20-71 0I-1 AND DWG 5971058.

Part: SEAT TRACK — DAMAGED (BS 268-368) · corrosion level 2 · airframe 42,698 hrs · 28,437 cycles

LEFT INBD SEAT TRACK BS 268 - 368, LBL 22 HAS SCRATCHED, AND CORROSION. BLENDED THE SEAT TRACK, AND FOUND TO BE OUT OF LIMITS AND REPAIRED IAW SRM 53-20-52 2R-1.

Part: CUSP WEB — CORRODED (BS 910-920) · corrosion level 2 · airframe 42,698 hrs · 28,437 cycles

CORROSION ON LEFT CUSP WEB LBL 60, BS 910 - 920. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. REPAIRED IAW SRM 53-00-55 2R-4.

Part: SKIN — CRACKED (BS 1475) · airframe 39,410 hrs · 25,863 cycles

FUSELAGE SKIN BS 1475, L2R CRACKED.

Part: SKIN — CRACKED (BS 1494) · airframe 39,402 hrs · 25,856 cycles

SKIN AFT BS 1494 LONGERONS 2-3R FOUND CRACKED.

Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 37,809 hrs · 24,575 cycles

DURING TAKEOFF NOSE GEAR UNSAFE INDICATION AFTER RETRACTION. FOLLOWED GEAR UNSAFE PROCEDURE IN QRH, CYCLED GEAR. R & R B DOWNLOCK SENSOR IAW AMM.

Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 37,809 hrs · 24,575 cycles

DURING TAKEOFF NOSE GEAR UNSAFE INDICATION AFTER RETRACTION. FOLLOWED GEAR UNSAFE PROCEDURE IN QRH, CYCLED GEAR. R & R A DOWNLOCK SENSOR IAW AMM.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 37,388 hrs · 24,279 cycles

VERTICAL STABILIZER LE RAM AIR FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 36,940 hrs · 23,979 cycles

VERTICAL STABILIZER LE RAM AIR FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 36,453 hrs · 23,657 cycles

VERTICAL STABILIZER LE RAM AIR FAIRING PREVIOUS WELD REPAIR CRACKED. REPAIRED STABILIZER IAW SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,040 hrs · 23,393 cycles

FWD GALLEY FLASHLIGHT INOPERATIVE. RELAMPED FLASHLIGHT IAW AMM.

Part: COVER — BROKEN (L1 DOOR) · airframe 34,809 hrs · 22,620 cycles

L1 DOOR EMERGENCY EVAC SLIDE BROKEN. R&R COVER IAW AMM.

Part: FASTENER — SHEARED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

AFT ACCESSORY COMPARTMENT FASTENER SHEARED OFF AT BS 1144, LONGERON 1R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT BS 1144, LONGERON 1. REMOVED AND REPLACED FORMER IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

FLOOR SUPPORT ANGLE CRACKED AT STA 714, RBL 44. REMOVED AND REPLACED ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CRACKED AT STA 655. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 33,581 hrs · 21,851 cycles

LEFT WHEEL WELL - AFT SIDE OF KEEL BEAM - ATTACHED ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: PANEL — CRACKED (LT MLG WW) · airframe 33,581 hrs · 21,851 cycles

LEFT WHEEL WELL AFT DOOR CUTOUT BELOW HYD RESERVOIR PANEL CRACKED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CUSP WEB CORRODED AT STA 761. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222 AGF DELAMINATED BETWEEN STA 737 TO STA 813, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 33,581 hrs · 21,851 cycles

RIGHT WHEEL WELL AFT SIDE OF KEEL BEAM ATTACHED ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: PANEL — CRACKED (RT MLG WW) · airframe 33,581 hrs · 21,851 cycles

RIGHT WHEEL WELL - AFT DOOR CUTOUT - BELOW HYD RESERVOIR PANEL CRACKED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

CUSP WEB CORRODED AT BS 389, RBL 54. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB DAMAGED AT STA 672. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED AT STA 745. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 33,581 hrs · 21,851 cycles

RT WHEEL WELL FWD DOOR CUTOUT I/B SUPPORT BRACKET CRACKED. REMOVED & REPLACED BRACKET PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 645 TO STA 822, RBL 44. REMOVED AND REPLACED TRACK IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 33,581 hrs · 21,851 cycles

LEFT WHEEL WELL FWD DOOR CUTOUT I/B SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 822 TO STA 898, RBL 22. REMOVED AND REPLACED TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 898 TO 1015, RBL 24. REMOVED AND REPLACED TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 585 TO STA 898, RBL 54. REMOVED AND REPLACED TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

SEAT TRACK CORRODED BETWEEN STA 256 TO STA 585, RBL 54. REPAIRED TRACK IAW SRM.

Part: LONGERON CLIP — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LONGERON CLIP CORRODED AT STA 1002, LONG 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

SEAT TRACK CORRODED BETWEEN STA 256 TO STA 585, RBL 44. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 33,581 hrs · 21,851 cycles

NR 1 PYLON SKIRT FAIRING CRACKED AT LOWER ENGINE COWL AFT HINGE ATTACH POINT. REPAIRED FAIRING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED BETWEEN STA 560 TO STA 579. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED BETWEEN STA 484 TO STA 503. REMOVED AND REPLACED WEB IAW SRM.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 33,581 hrs · 21,851 cycles

VERTICAL STAB T/E ACCESS PANEL 374 CL CRACKED. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 408 TO BS 427. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED BETWEEN STA 389 TO STA 408. REMOVED AND REPLACED WEB IAW SRM.

Part: RUB STRIP — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RUB STRIP CORRODED BETWEEN BS 870 TO BS 917, BETWEEN LONGERON 26L TO 29L. REMOVED AND REPLACED RUB STRIP IAW M/M & SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED BETWEEN STA 541 TO STA 560. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LEFT CABIN CUSP WEB CORRODED AT STA 605. REMOVED AND REPLACED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STA 256 TO STA 585, LBL 44. REMOVED AND REPLACED TRACK PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 560 TO STA 579. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 541 TO STA 560. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 484 TO BS 503. REPAIRED WEB IAW SRM.

Part: SUPPORT — CRACKED (CENTER WING) · airframe 33,581 hrs · 21,851 cycles

CENTER WING VERTICAL SUPPORT CRACKED AT BS 737, RBL 44. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 446 TO BS 465. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 465 TO BS 484. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 655 TO STA 674. REMOVED AND REPLACED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 522 TO STA 541. REMOVED AND REPLACED WEB IAW SRM.

Part: SUPPORT — CRACKED (CENTER WING) · airframe 33,581 hrs · 21,851 cycles

CENTER WING AT BS 737 LBL 44 VERTICAL SUPPORT CRACKED BELOW SEAT TRACK. REMOVED & REPLACED SUPPORT IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222ATF DELAMINATED BETWEEN STA 889 TO STA 954, BETWEEN LBL 22 LBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED BETWEEN STA 813 TO STA 889, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222 AHF DELAMINATED BETWEEN STA 737 TO STA 813, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222LF DELAMINATED BETWEEN STA 465 TO STA 541, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED BETWEEN STA 696 ST STA 737, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222AHF DELAMINATED BETWEEN STA 813 TO STA 889, BETWEEN LBL 32 TO LBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 221WF DELAMINATED BETWEEN STA 313 TO STA 389, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222PF DELAMINATED BETWEEN STA 541 TO STA 617, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222BF DELAMINATED BETWEEN STA 389 TO STA 465, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW AMM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,581 hrs · 21,851 cycles

LONGERON CRACKED AT STA 1133, LONGERON 2R. REPAIRED LONGERON IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222 ACF DELAMINATED BETWEEN STA 696 TO STA 737, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 221UF DELAMINATED BETWEEN STA 313 TO STA 389, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222FF DELAMINATED BETWEEN STA 408 TO STA 446, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222 AVF DELAMINATED BETWEEN STA 889 TO STA 954, RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED BETWEEN STA 674 TO STA 696, RBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222AAF DELAMINATED BETWEEN STA 674 TO STA 696, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222JF, DELAMINATED BETWEEN STA 465 TO STA 541, AT LBL 22. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

MAIN CABIN FLOOR PANEL 222RF DELAMINATED BETWEEN STA 541 TO STA 636, BETWEEN RBL 22 TO RBL 33. REMOVED AND REPLACED PANEL IAW MM DELAMINATED.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 33,581 hrs · 21,851 cycles

RIGHT EEPLS INOP AT ROW 23. RESEATED CONNECTOR IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 33,819 hrs · 21,997 cycles

R1 DOOR SLIDE PARK LOOSE. SECURED GIRT BAR PER AMM.

Part: SKATE ANGLE — CRACKED (NR 2 PYLON) · airframe 33,558 hrs · 21,836 cycles

NR 2 PYLON UPPER SKATE ANGLE CRACKED. TRIMMED OUT DAMAGED AREA PER BOEING DRAWING SG95530003.

Part: COVER — DAMAGED (R1 DOOR) · airframe 31,856 hrs · 20,734 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER DAMAGED. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — TORN (R1 DOOR SLIDE)

R1 DOOR SLIDE COVER TORN AWAY FROM HINGE, AWI. REMOVED SLIDE DOOR AND REPLACED REF AMM 20-60, REMOVED AND REPLACED SLIDE REF AMM 25-61, RE-INSTALLED SLIDE DOOR REF AMM 25-61, AWI.

Part: FUSE — BLOWN (CABIN)

TAIL CONE SLIDE EMERGENCY LIGHTS 2 EA, AND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT INOPERATIVE. FOUND BLOWN FUSE IN BATTERY PACK B5-116. REPLACED BATTERY PACK B5-116. REF AMM 33-51-03, OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN, STA 1022.091, LONG L13, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER EA 17-53-03221IR.

Part: DOUBLER — CORRODED (FUSELAGE)

LOWER AFT CARGO DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB DOUBLER REPAIR PER B717 SRM 53-20-15.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN, STA 218, LONG L15L TO L16L, DENTED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 53-00-01, 51-10-04 AND TRA 17-53-TR00109.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK, STA 212 TO 245, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B717 SRM 51-10-04, 53-20-52 AND BOEING DWG SR09530085.

Part: SKIN — CRACKED (LT NACELLE)

LEFT ENG APRON NR 2 COWL LATCH LOWER CUTOUT, CRACKED. ACCOMPLISHED LOWER CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: FINGER DOUBLER — CRACKED (FUSELAGE)

PASSENGER CABIN FINGER DOUBLER, STA 209, LONG L15L, CRACKED. ACCOMPLISHED FINGER DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 32, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 188 TO 200, RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: STRUCTURE — CORRODED (CABIN)

AIR GRILL SUPPORT, STA 208, RBL 56, CORROSION. ACCOMPLISHED AIR GRILL SUPPORT DOUBLER REPAIR PER B717 SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 225 TO 230, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY FLOODLIGHT FOR OVERHEAD PANEL LOCATED BEHIND CAPTAINS SEAT IS INOP. RELAMPED AND OP'S CHECK GOOD.

Part: COMPRESSOR — STALLED (LT ENGINE)

WHEN ADDING POWER FOR TAKEOFF EXPERIENCED COMPRESSOR STALL LEVEL 2 ALERT FOR LEFT ENGINE. ACCOMPANIED BY AUDIBLE POP, TGT EXCEEDANCE OF 974. OTHER AIRCRAFT REPORTED TAILPIPE FIRE. DID NOT FEEL SURGE. REMOVED AND REPLACED NR 1 ENGINE.

Part: BATTERY — UNSERVICEABLE (AFT CARGO BAY)

EXTERIOR EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN SWITCH IN COCKPIT WAS OFF. REMOVED & REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY LOCATED AT AFT CARGO BIN. LIGHTS OPERATED NORMAL WITH REPLACEMENT BATTERY ASSEMBLY.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2979.

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 — DENTED (FS 239)

FUSELAGE DENT AT FS 239L BETWEEN L17 AND L18 MEASURES 6 X 8 X .125 INCH DEEP. INSTALLED PERMANENT REPAIR AT BS 239 BETWEEN LONG 17L AND 18L AS REQUIRED IAW B717 SRM 53-00-01 FIG 201, MATERIAL USED 2024T3.050, 16.25 X 18.5 AND 2024T3.025, 33.5 X 5.75 DOUBLER 2024T3.063, 25 X 4 INCH.