N965AT

Part: SEAL — DIRTY (TAILCONE DOOR) · airframe 61,848 hrs · 44,242 cycles

TAILCONE DOOR NOT FULLY SEATING AND SEALING ON UPPER RT SIDE OF THE DOOR. NOISE OBSERVED FROM THE UNSEATED PORTION OF THE DOOR. CLEANED SEAL, CYCLED DOOR AND PRESSURIZED ACFT. DOOR OPS AND LEAK CKS GOOD IAW AMM 52-12. (7287760)

Part: LOCK LINK ASSY — DAMAGED (THRUST REVERSER) · airframe 60,659 hrs · 43,113 cycles

SHIP 9524 -IFSD/DE- THE CREW RECEIVED A "LEFT REVERSER UNLOCK" MESSAGE. THE QRH WAS COMPLIED WITH, WHICH INCLUDED SHUTTING DOWN THE LEFT ENGINE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE OUTBOARD UPPER AND LOWER LOCK LINK ASSEMBLY. THEY ALSO REPLACED THE #1 ENGINE INBOARD LOWER LOCK LINK ASSEMBLY. (LP #6792940)

Part: SKIN — CRACKED (ZONE 100) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL WAS REPAIRED PER ER/A 618958-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-618958 ADDED FOR AC 9524. (LP #0502350)

Part: STATIC WICK — DAMAGED (LT ELEVATOR) · airframe 59,557 hrs · 42,153 cycles

DURING LIGHTRING STRIKE INSPECTION FOUND LH ELEVATOR O/B STATIC DISCHARGER CONDUCTIVE DOUBLER DAMAGED. COMPLETED TEMP REPAIR PER ENGINEEREING CONCURRENCE EMAIL TOPP 40-60-05 PAR X.B.2 LH ELEVATOR O/B STATIC DISCHANGER CONDUCTIVE REPAIR BY ERA 618920-14 REV ORIG SECTION UNDER LP 0495234. (LP #5577970)

Part: SKIN — CRACKED (ZONE 100) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL WAS REPAIRED PER ER/A 618958-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-618958 ADDED FOR AC 9524. (LP #0502354)

Part: SKIN — CRACKED (ZONE 100) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL WAS REPAIRED PER ER/A 618744-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-618744 ADDED FOR AC 9524. (LP #0501808)

Part: HINGE — DAMAGED (ZONE 100) · airframe 59,557 hrs · 42,153 cycles

ELONGATED HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT). (PTAS). SUMMARY OF NRC 00106: HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT) WERE REPAIRED PER ERA 559577-14MA REV ORIGINAL, PER PRI 618954-14 REV 4, AND ER/A 618954-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-618954 ADDED FOR AC 9524. (LP #0496609)

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 59,557 hrs · 42,153 cycles

CRACKS WERE FOUND ON UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH. SUMMARY OF NRC 00701: UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH WAS REPAIRED PER ER/A 618920-14 REV ORIGINAL SECTION I: PERMANENT REPAIR ACCOMPLISH SECTION II REPETITIVE INSPECTION INSTRUCTIONS WITHIN EVERY 3,000 FLIGHT CYCLES INTERVALS FROM DATE OF THIS ERA (15,424 TOTAL COMPONENT FLIGHT CYCLES). LOG PAGE #0488017 PER ERA 618920-14 REV ORIGINAL. ASSOCIATED ER/A 14-618920 ADDED FOR AC 9524. (LP #0495234)

Part: SKIN — DENTED (ZONE 100) · airframe 59,557 hrs · 42,153 cycles

DENTS (2EA) ON FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH. SUMMARY OF NRC 00669: FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH WAS REPAIRED PER ER/A 619313-14 REV ORIG SECTION I PERMANENT REPAIR. ACCOMPLISHED REPETITIVE INSPECTIONS WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHEMENT OF SECTION I: PERMANENT REPAIR SECTION II, PER E/RA 619313-14 REV ORIGINAL, UNDER LOG PAGE #0489948. ASSOCIATED ER/A 14-619313 ADDED FOR AC 9524. (LP #0490368)

Part: PAN — CRACKED (ZONE 100) · airframe 59,557 hrs · 42,153 cycles

CRACK ON PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00402: PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER PRI 618569-14 REV 7 AND ERA 618569-14 REV ORIGINAL. SECTION I PERMANENT REPAIR. (LP #0489565)

Part: SKIN — CRACKED (ZONE 200) · airframe 59,557 hrs · 42,153 cycles

CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW CUTOUT AREA WAS FOUND. SUMMARY OF NRC 00628: INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 PARAGRAPH 5 FIGURE 201. (LP #0488328)

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

SEVERAL SPOTS OF CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00346: CORROSION LEVEL 2. WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 WAS REPAIRED PER ER/A 618642-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 618642-14 REV 6. ASSOCIATED ER/A 14-618642 ADDED FOR AC 9524. (LP #0467343)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,557 hrs · 42,153 cycles

CRACK WAS FOUND ON LH CUSP WEB STA 588 AT PAX CABIN. SUMMARY OF NRC 00798: LH CUSP WEB STA 588 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4. (LP #0454524)

Part: LONGERON — CORRODED (AFT CARGO COMPAR) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON END LONGERONS 25R AND 26R STA Y=1004 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00783: CORROSION LEVEL 2. END LONGERONS 25R AND 26R STA Y=1004 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0451371)

Part: SKIN — WORN (L1 DOOR AREA) · airframe 59,557 hrs · 42,153 cycles

WEAR ON EDGE SKIN AROUND HOOK AT L1 DOOR. SUMMARY OF NRC 00111: EDGE SKIN AROUND HOOK AT L1 DOOR WAS REPAIRED PER PRI 619136-14 REV 1 AND ERA 619136-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-619136 ADDED FOR AC 9524. (LP #0451426)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,557 hrs · 42,153 cycles

-AD- CRACK OF 1.00 IN LENGTH APPROX ON UPPER RADIUS OF THE LH OVERWING FRAME TAB STA Y=715.00 (IN REF. CARD 5310-01436-01B STEP 7). SUMMARY OF NRC 000333: THE LH OVERWING FRAME TAB STA Y=715.00 WAS REPLACED AMDS 5310-01436-03A JOB 165-0001. (LP #0444425)

Part: PAN — CRACKED (FWD CARGO) · airframe 59,557 hrs · 42,153 cycles

CRACK ON INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR. (PTAS) SUMMARY OF NRC 00099: INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR WAS REPAIRED PER PRI 618453-14 REV 1 AND ERA 618453-14 REV ORIGINAL SECTION I PERMANENT REPAIR. (LP #0439934)

Part: DOUBLER — CORRODED (BS 199-218) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00766: CORROSION LEVEL2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R AT E/E COMPARTMENT WAS FABRICATED AND INSTALLED PER DWG 9923686 REV J AND INSTALLED PER B717-200 SRM 51-41-02-0G. (LP #0437583)

Part: FRAME — CRACKED (BS 696) · airframe 59,557 hrs · 42,153 cycles

CRACK ON FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00499: FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROC 1 REPAIR 1. (LP #0438169)

Part: CUSP WEB — CORRODED (BS 397-406) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON CUSP WEB STA 397-406 AND X=-59. ORIGINAL THICKNESS 0.020" AND MINIMUM REMAINING THICKNESS 0.003", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1. SUMMARY OF NRC 00690: CORROSION LEVEL 2. CUSP WEB STA 397-406 AND X=-59 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0436126)

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 59,557 hrs · 42,153 cycles

CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 200-218) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

AIRCRAFT 9524, CORROSION ON INB SEAT TRACK X22 STA Y=200 TO STA Y= 218 AT PAX CABIN (W1). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK WERE REPAIRED ON X= 22 STA Y= 200 TO STA Y= 294 PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5. (LP 0428722)

Part: CUSP WEB — CORRODED (BS 568-577) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION ON PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN (CPAX). CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN(CPAX) WERE REPLACED PER B717-200 SRM 53-00-55-2R-4, FIG. 204.SRM 51-41-02-0G AND SRM 51-41-05-0G.

Part: SEAT TRACK — CORRODED (BS 898) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

AIRCRAFT 9524, CORROSION ON SEAT TRACK AT STA Y=898 X=44.5 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK SECTION BTW STA Y=898 TO STA Y= 935 X=44.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R REPAIR 5. (LP 0418906)

Part: PAN — CORRODED (BS 954-994) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

AIRCRAFT 9524, CORROSION ON PAN DOOR JAMB STA Y=994 TO Y= 954 BTW LONG 24 AND 28 RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2, PAN DOOR JAMB STA Y=994 TO Y=954 BTW LONG 24 AND 28 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP 0416972)

Part: FITTING — CORRODED (BS 560 L18L) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

AIRCRAFT 9524, CORROSION ON MAIN FRAME FITTING STAY=560 L18L AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. MAIN FRAME FITTING STAY= 560 L18L AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP 0414381)

Part: WEB — NICKED (BS 172-173) · airframe 59,557 hrs · 42,153 cycles

NICK ON MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX. SUMMARY OF NRC 00434: MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 REPAIR 2. (LP #0411983)

Part: CUSP WEB — CORRODED (BS 739-745) · corrosion level 2 · airframe 59,557 hrs · 42,153 cycles

CORROSION OUT OF LIMITS ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN. SUMMARY OF NRC 00744: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 PAR 5 FIGURE 216. (LP #0411977)

Part: BEAM — CRACKED (L1 DOOR AREA) · airframe 59,557 hrs · 42,153 cycles

CRACK ON BEAM #2 STA Y=196 APROX IN PASSANGER DOOR (L1) AT CABIN PAX. SUMMARY OF NRC 00090: AREA ON BEAM #2 STA Y=196 IN PASSANGER DOOR L1 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0406350)

Part: FRAME — CRACKED (BS 1037 L17L/R) · airframe 59,557 hrs · 42,153 cycles

CRACK ON MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN. SUMMARY OF NRC 00441: MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4, PAR 5A. (LP #0402943)

Part: HINGE FITTING — WORN (TE FLAPS) · airframe 59,387 hrs · 42,022 cycles

CORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541841-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSES ONLY. ASSOCIATED ER/A 00-541841 ADDED FOR AC 9524. ** REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTION; ** ER/A 541841-14 REV A IS CURRENT. DTA RESTRICTION MODIFIED FROM 365 DAYS TO 60,000 CYCLES. DTI STAGE III RESTRICTION. (LP #2246647)

Part: HINGE FITTING — WORN (TE FLAPS) · airframe 59,387 hrs · 42,022 cycles

CORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541845-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541845-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSES ONLY. ASSOCIATED ER/A 00-541845 ADDED FOR AC 9524. REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTION; ER/A 541845-14 REV A IS CURRENT. MONITOR CHANGED FROM 365 DAYS TO 60,000 TOTAL AIRCRAFT CYCLES. DTI STAGE III RESTRICTION. (LP #2246644)

Part: PSEU — FAILED (MLG) · airframe 59,261 hrs · 41,918 cycles

SHIP 9524 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC APPROACHING ATL DUE TO THE LEFT AND RIGHT "GEAR UNSAFE" INDICATIONS WITH THE GEAR HANDLE UP. THE AIRCRAFT ALSO HAD A LOSS OF FLAP/SLAT INDICATION ON APPROACH. CORRECTIVE ACTION: MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND THE PSEU FAILED THE RETURN TO SERVICE TESTS. SEE LOG PAGE #0237343 FOR COMPLETE REPAIR. (LP #5459026)

Part: UPLOCK SENSOR — FAULTED (LT MLG) · airframe 59,252 hrs · 41,910 cycles

SHIP 9524 -GEAR/DE- AFTER TAKEOFF AND LANDING GEAR SELECTED TO RETRACT, THE CREW RECEIVED A "LEFT GEAR UNSAFE" INDICATION AFTER RETRACTION. THE QRH WAS COMPLIED WITH AND THE GEAR WAS EXTENDED WITHOUT ANY PROBLEMS, UNTIL THE "PSEU FAIL" MESSAGE. THE QRH WAS COMPLIED WITH FOR THAT AND AN EMERGENCY WAS DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL. MAINTENANCE RAN BITE WHICH DID CONFIRM GEAR FAULT CODE 326084. THE LEFT MAIN LANDING GEAR UP AND LATCHED SENSOR WAS REPLACED. ALL OPERATIONAL CHECKS WERE GOOD; INCLUDING GEAR SWINGS. THE PSEU WAS REPLACED AS A PRECAUTIONARY. (LP #5459016).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,926 hrs · 41,616 cycles

SHIP 9524 -GEAR/DE- THE NOSE GEAR DID NOT EXTEND NORMALLY WHEN HANDLE WAS MOVED TO THE DOWN POSITION DURING APPROACH FOR LANDING AT HSV. THE TOWER DECLARED AN EMERGENCY. THE CREW UTILIZE THE MANUAL GEAR EXTENSION PROCEDURES PER THE QRH AND LANDED UNEVENTFULLY. THE AIRCRAFT TAXIED TO THE GATE. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH RESTRICTORS IN THE NOSE GEAR EXTEND/RETRACT CIRCUIT. ALSO FOUND THAT THE NLG LOCK LINK WAS OUT OF RIG. THE NLG LOCK LINK WAS ADJUSTED AND THE GEAR WAS CYCLED TWENTY TIMES WITHOUT ANY FAULTS. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5090160)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,905 hrs · 41,602 cycles

SHIP 9524 -GEAR/DE- THE NOSE LANDING GEAR FAILED TO EXTEND NORMALLY AFTER TWO ATTEMPTS. THE FLIGHT CREW ACCOMPLISHED A GO-AROUND, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES PER THE QRH. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THE NOSE LANDING GEAR BUNGEE CYLINDER INOPERATIVE, REPLACED IT, PERFORMED A FUNCTIONAL CHECK, AND RETURNED THE AIRCRAFT TO SERVICE. (LP #5090138)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,703 hrs · 41,439 cycles

MULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN AND TAIL. MAINTENANCE REPLACED THE BATTERY PACKS B5-118, B5-260, B5116, & B5-231. OPERATIONAL CHECK WAS GOOD. (LP #5508918)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,703 hrs · 41,439 cycles

THE COCKPIT EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (B5-123). OPERATIONAL CHECK WAS GOOD. (LP #5508919)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,504 hrs · 41,275 cycles

THE AISLE EXIT SIGN IS HANGING FREE. *** CONTRACT MAINTENANCE EVENT - OCM: 271717 *** COMPLIED WITH ERA 613272- 14 REV ORIG. TIME LIMITED REPAIR SECT I. DEFERED TO MONITOR FOR 1 FLT CYCLE. DTW MAINTENANCE REPLACED THE FORWARD CEILING MOUNTED EXIT LIGHT ASSEMBLY IAW ERA 613272-14 SECTION II REV ORIG. PERMANENT REPAIR COMPLETED. OK TO CLOSE MONITOR. AIRCRAFT IS OK FOR SERVICE. (LP #4735490)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,134 hrs · 40,116 cycles

FUSELAGE EDGE SKIN DAMAGE. LOWER FORWARD CORNER OF AFT CARGO DOOR CUT OUT. COMPLIED WITH PRI 607567-14-AD- REV 0 AND REV 1. (LP #2700709)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,134 hrs · 40,116 cycles

FOWARD L/H MOUNT FOR G-7 GALLEY CORRODED. FOUND AFTER GALLEY DISPLACEMENT. SUMMARY SEE NRC 089-0001:0591-2001/002 00355: REPLACED FWD L/H MOUNT AT G-7 GALLEY PER B717 AMM 25-31-70. (LP #2698677)

Part: DISC — CRACKED (AIR SEAL) · airframe 57,045 hrs · 40,029 cycles

1 AXIAL CRACK IN AIR SEAL F AREA (ABOVE DIA 15-2) MEASURING ~0.340 INCH 1 CIRCUMFERENTIAL CRACK IN AIR SEAL F AREA (BELOW DIA 15-2) MEASURING ~0.100 INCH

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,883 hrs · 38,109 cycles

FOUND WING EMERGENCY EXIT DOOR LOWER LIGHTS INOPERATIVE. MAINTEANACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY AT ROW 22 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #8751621)

Part: NONE — NONE · airframe 54,836 hrs · 38,072 cycles

LIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150535)

Part: NONE — NONE · airframe 54,849 hrs · 38,081 cycles

LIGHTNING STRIKE F.S. 60 BETWEEN 2ND AND 3RD FRAME FWD OF POWER RECEPTECLE L/H. REPAIRED REF B717 SRM 53-01-01-01A-2. (LP #2150411)

Part: NONE — NONE · airframe 54,836 hrs · 38,072 cycles

LIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150523)

Part: NONE — NONE · airframe 54,836 hrs · 38,072 cycles

LIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150520)

Part: HANDLE — MALFUNCTIONED (TAILCONE) · airframe 52,777 hrs · 36,291 cycles

SHIP 9524 - THE CREW RETURNED THE AIRCRAFT BACK TO ATL FOLLOWING THE "TAILCONE UNLOCK" INDICATION ILLUMINATING. CORRECTIVE ACTION: MAINTENANCE FOUND THE AFT INSIDE RELEASE HANDLE LOWER BALL OUT OF THE SWITCH. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE RELEASE HANDLE LOWER BALL WAS REINSTALLED PER B717 AMM 53-52-01. THE LIGHT REMAINED EXTINGUISHED AND THE TAILCONE SECURED. THE RII WAS ACCOMPLISHED AND SIGNED OFF ON LP #7576592. AIRCRAFT RETURNED TO SERVICE. (LP #7576588)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,777 hrs · 36,291 cycles

BOTH THE LEFT AND RIGHT OVER-WING EMERGENCY EXIT LIGHT ARE INOPERATIVE. MAINTENANCE REPLACED THE OVER-WING EMERGENCY EXIT LIGHT BATTERY REF B717 AMM 33-51-06. (LP #1778268)

Part: STRINGER — CORRODED (BS 908-974) · corrosion level 2 · airframe 52,773 hrs · 36,287 cycles

AFT CARGO COMPARTMENT, STRINGER #30 CORRODED FROM STA 908 TO 974. NRC 057-0022:5310-2014/007 00211: MAINTENANCE REPLACED LONGERON 30 FROM STATION 906 TO 1012 PER DWG #5919707 AND INSTALLED REPAIR SPLICE AT STA 964 PER B717 SRM 53-20-05-2R PROCEDURE 1 REPAIR 1. (LP #1778272)

Part: RETAINER — MISSING (TAIL SLIDE) · airframe 52,773 hrs · 36,287 cycles

THE RETAINING CLIP IS MISSING FROM THE COVER OF THE TAIL SLIDE REF STEP 9A AND FIG 4 SHEET 13. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 000-0002:2561-9006/002 00310: MAINTENANCE REPLACED THE CLIP. (LP #1775199)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,102 hrs · 33,505 cycles

THE OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVER WING EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-54. OPERATIONAL CHECK WAS GOOD. (LP #4842898)

Part: SKIN — CORRODED (BS 629) · corrosion level 2 · airframe 44,738 hrs · 30,351 cycles

CORROSION SKIN BS 629, LONGERON 28L - 30L. REPAIRED IAW SRM 51-40-08, 51-44-02 PARA 4, AND 51-41-05 PARA 8.

Part: SEAT TRACK — CORRODED (BS 587-656) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

SEAT TRACK AT BS 587 TO 656, LBL 17 HAS CORROSION IN SCREW HOLES. MECHANICALLY BLENDED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED WITH NEW.

Part: SKIN — CRACKED (BS 1037) · airframe 44,719 hrs · 30,334 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 1037, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 555611-14, REV OR.

Part: SKIN — CRACKED (BS 1087) · airframe 44,719 hrs · 30,334 cycles

RIGHT FUSELAGE SKIN CRACKED, BS 1087, ABOVE LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557984-14, REV OR.

Part: CUSP WEB — CRACKED (COCKPIT) · airframe 44,719 hrs · 30,334 cycles

ON REMOVAL OF THE FIRST OFFICER`S OTBD SEAT TRACK, FOUND A CRACKED CUSP WEB FROM ATTACH FASTENER HOLE. REPAIRED THE CUSP WEB IAW SRM 53-00-00-2R, EX B, AND 51-41-02.

Part: DOOR FRAME — DAMAGED (BS 408) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

FWD LOWER FUSELAGE, FWD CARGO DOOR FRAME, BS 408 TO 434.5, LONGERON 18R, UPPER SILL, LOWER CUSP WEB PANEL. REPAIRED IAW SRM 53-00-55-2R-4 .

Part: SKIN — CRACKED (BS 1076) · airframe 44,719 hrs · 30,334 cycles

RIGHT FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557983-14, REV OR.

Part: FRAME — CORRODED (BS 974) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CORROSION AT BS 974 FRAME FWD SIDE LONGERON 29L - 29R. PERFORMED FRAME REPAIR IAW SRM 53-20-07-2R-2.

Part: SKIN — CRACKED (BS 1022) · airframe 44,719 hrs · 30,334 cycles

LEFT FUSELAGE SKIN CRACKED, BS 1022, LONGERON 14L. REPAIRED SKIN IAW ER/A 555612-14, REV O.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

RT STA 434 CUSP WEB HAS CORROSION ON TOP AND BOTTOM. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREATED, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-055-2R-4, AND AMM 51-10-00 370-803.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

RT STA 389 UNDERSIDE OF CUSP WEB HAS CORROSION. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREAT, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-00-55-2R-4, AND AMM 51-10-00-370-803.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

THE RT CUSP WEB AT STA 737-756, RBL 55 HAS CORROSION AROUND THE UNDERSIDE OF LIGHTENING HOLE(S). BLENDED CUSP WEB AT STA 737-756 ORIGINAL THICKNESS .040 REMAINING THICKNESS .028. FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW SRM 53-00-55 REPAIR 4.

Part: LONGERON — CORRODED (BS 931) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CORROSION AT BS 954 - 908, L30. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS AT STA 931. REPAIR THE AREA. TREATED, PRIMED, TOP COATED, INSTALLED FASTENERS, IAW SRM 51-41-02, 53-00-00, FIG 103, 53-00-05-2R-3, AND AMM 51-10-00-370-803.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

RIGHT INBOARD SEAT TRACK RBL 22, BS 200 - 256, HAS AREAS OF CORROSION. BLENDED THE SEAT TRACK, AND FOUND AREAS OUT OF LIMITS. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-20-52-2R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

AFT WET AREA STA 1022-1053, LBL 46 FLOOR SUPPORT HAS CORROSION IN MULTIPLE AREAS INCLUDING OUTBD FLANGE. REMOVED CORROSION BY BLENDING ON FLOOR SUPPORT AT LBL46 STA 1041 .025" MATERIAL REMOVED .055" REMAINING .080" ORIGINAL THICKNESS OUT OF LIMITS IAW SRM 53-00-00-1A FIG 103. FABRICATED NEW FLOOR SUPPORT IAW B717 SRM 51-30-08-OG FIG 2 AND DWG 9981474 REV L. REPLACED FLOOR SUPPORT P/N 9981474-81 IAW SRM 51-41-05-OG PG 3 PARA 8 AND DWG 9981474 REV L.

Part: LONGERON SPLICE — CORRODED (BS 891-906) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CORROSION AT BS 891 - 906, LONGERON 30 SPLICE FITTING. REMOVED AND REPLACED THE DAMAGED LONGERON SPLICE IAW SRM 51-41-01, 51-41-05, AND DRAWING 5924878.

Part: BULKHEAD — GOUGED · airframe 44,719 hrs · 30,334 cycles

AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR INTERNAL STRUCTURE IS GOUGED IN SEVERAL AREAS AT LOWER RT SECTION WHERE FLIGHT ATTNANTS SEAT IS MOUNTED. REPAIRED IAW SRM 52-10-02-2R, OPTION 2.

Part: CUSP WEB — CRACKED (BS 716) · airframe 44,719 hrs · 30,334 cycles

CRACKS AROUND RIVET HEADS ON LT SIDE CUSP WEB BS 716, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R4, REPAIR 4.

Part: CUSP WEB — CORRODED (BS 737-756) · airframe 44,719 hrs · 30,334 cycles

CORROSION ON TOP AND BOTTOM SIDE OF LEFT CUSP WEB BETWEEN BS 737-756, LBL 60. REPAIRED THE CUSP WEB IAW SRM 53-00-55-4R-2, REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,719 hrs · 30,334 cycles

FWD LT STA 1022 FRAME FORMER CRACKED BETWEEN LONGERON 5L-6L. REPAIRED FWD LT STA 1022 FRAME FORMER BETWEEN 5L-6L IAW SRM 53-00-06-2R REPAIR 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CUSP WEB LT AT STA 427-446 CORRODED. REPAIRED LT CUSP WEB AT STA 427-446 IAW SRM 53-00-55-2R-4. BLENDED CORROSION ON WEB. NOMINAL .020 REMOVED .005 REMAINING .015. OUT OF LIMITS IAW SRM 53-00-55-1A-1.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CORROSION ON THE F/O'S OTBD SEAT TRACK. CORROSION ON SEAT TRACK FOUND TO BE BEYOND DWG TOLERANCE OF .015 WITH 50% MATERIAL LOSS IAW BOEING DWG 5971207. REPLACED THE SEAT TRACK IAW AMM 53-22-01.

Part: CARGO TRACK — CORRODED (BS 995-1022) · corrosion level 2 · airframe 44,719 hrs · 30,334 cycles

CORROSION BS 995 - 1022, RT CARGO TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, FIG 103. REPLACED THE CARGO TRACK IAW SRM 51-41-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 44,719 hrs · 30,334 cycles

RT I/B SEAT TRACK GOUGED STA 890. GOUGED AREA ON SEAT TRACK WAS OUT OF LIMITS ORIG 0.115" REMAINING 0.090" IAW SRM 53-20-52-1A. REPLACED RT IB SEAT TRACK FROM STA 822 TO 897 IAW SRM 53-20-52-2R-5 FIG 201.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 44,719 hrs · 30,334 cycles

FWD CARGO DOOR SKIN CRACKED AT FWD LWR CORNER UNDER DOOR LATCH HOOK. FWD CARGO DOOR FOUND TO BE OUT OF LIMITS. REMOVED UNSERVICEABLE. SERVICEABLE DOOR TO BE INSTALLED ON JOB CARD 5231-4003.

Part: CUSP WEB — CORRODED (BS 408-465) · airframe 44,719 hrs · 30,334 cycles

LEFT CABIN FLOOR CUSP WEB IS CORRODED AROUND SEVERAL FASTENERS FROM BS 408 - 465. COMPLETED A CUSP WEB REPAIR IAW SRM 53-00-55-2R-4, REPAIR 4, FIGURE 204.

Part: CUSP WEB — CORRODED (BS 532) · airframe 44,719 hrs · 30,334 cycles

THE RT CUSP WEB AT BS 532, RBL 55 HAS CORROSION AROUND THE UNDERSIDE OF LIGHTENING HOLES. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 44,719 hrs · 30,334 cycles

CUSP WEB AT BS 446 - 465 CORRODED. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R, REPAIR 4, FIGURE 205.

Part: SKIN — DAMAGED (RUDDER) · airframe 44,719 hrs · 30,334 cycles

LOWER LEFT EDGE OF RUDDER IS DAMAGED. REMOVED DAMAGED SECTION OF THE RUDDER SKIN. FABRICATED & INSTALLED A REPAIR DOUBLER & FILLER IAW SRM 51-70-13-2R-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,719 hrs · 30,334 cycles

LT CABIN FLOOR CUSP WEB IS CORRODED AROUND SEVERAL FASTENERS FROM STATION 541 TO 617. BLENDED AREAS LT CABIN FLOOR CUSP THAT WAS CORRODED BETWEEN STA 541-617, ALL AREAS WERE FOUND TO BE WITHIN ALLOWABLE LIMITS; EXCEPT STA 580. TREATED, PRIMED ALL AFFECTED AREAS, INSTALLED REPAIR DOUBLER IAW SRM 53-00-55-1A, 51-10-04, 51-10-02, 51-41-08 PG 7-9, AND 53-00-55-2R-4.

Part: ANGLE — CRACKED (BS 636) · airframe 44,719 hrs · 30,334 cycles

FORWARD CARGO BS 636, BL 0 AFT SIDE OF INTERCOSTAL ANGLE IS CRACKED IN CEILING. REPAIRED THE ANGLE IAW SRM 51-70-11-2R-1. CRACK FOUND TO BE 2 INCHES IN LENGTH.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 43,610 hrs · 29,499 cycles

2 EA 3/16TH DOUBLER ATTACHMENT FASTENER HOLES DAMAGED. COMPLIED WITH PRI 552498-14 REV 0 IAW ER/A 552498-14 REV ORG.

Part: SKIN — DELAMINATED (SPOILER)

DURING NON ROUTINE LINE CHECK, R/H I/B SPOILER FOUND DELAMINATED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,424 hrs · 27,812 cycles

MAINTENACE FOUND THE MID CABIN OVERHEAD EMERGENCY EXIT SIGNS INOPERATIVE. THE BP120 BATTERY PACK WAS REPLACED. THE EMERGENCY EXIT SIGNS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,995 hrs · 27,505 cycles

DURING SERVICE CHECK, CEILING EMERGENCY LIGHTS ROW 22-29 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES AND CHECKS OK.

Part: CONTROL UNIT — FAULTED (AILERON TRIM) · airframe 40,632 hrs · 27,314 cycles

ON T/O THE ACFT ROLLED LEFT BUT WAS CONTROLLABLE. AT 2,000FT ACFT NORMAL WITH RIGHT STEERING , BUT TO THE LEFT WAS VERY STIFF, LIKE SOMETHING WAS BINDING. RETURNED TO DEPARTURE. COMPLIED WITH FIM 27-10-00-810-803. AILERON RTS CHECKS GOOD ON BOTH FCCS. LUBRICATED BOTH AILERONS AND TABS IAW AMM 12-24. AILERON RIG CHECKS OK IAW AMM 27-10. BOTH CONTROL WHEELS OPERATE SMOOTHLY, NO BINDING OR RATCHETING. FWD BAG BIN CEILING CHECKS OK WITH NO EVIDENCE OF OVERLOADING. FOUND ATCU FAULT ON AILERON TRIM CONTROL UNIT. REPLACED CONTROL UNIT IAW AMM 27-10. PERFORMED SUCCESSFUL VERIFICATION FLIGHT. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,793 hrs · 26,628 cycles

AFT LT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CORRODED (FUEL TANK) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN CTR WING TANK UPPER SKIN CORRODED BETWEEN BS 715 - 737, BETWEEN LBL 44 & LBL 54. R & R SKIN IAW SRM & EA.

Part: SKIN — CORRODED (FUEL TANK) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN CTR WING TANK SKIN CORRODED BETWEEN BS 737 - 746, BETWEEN LBL 44 & LBL 54. R & R SKIN IAW SRM & EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 38,379 hrs · 25,658 cycles

CABIN TOP OF FWD CORNER OF R1 DOOR INTERIOR WEB SKIN CRACKED AT BS 161. REPAIRED SKIN IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 636 - 655. R & R CUSP WEB IAW DWG & EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOOR MEMBRANE DOUBLER CRACKED AT BS 200, RBL 46. REPAIRED DOUBLER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 200 - 238, LBL 14.5. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 - 236, RBL 44.5. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN SEAT TRACK CRACKED AT BS 205, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 9 - 41. R & R SUPPORT IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

RIGHT FRAME CRACKED AT BS 696, UPPER RADIUS OF THE TAB. R & R FRAME IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

INTERCOSTAL SUPPORT CRACKED AT BS 715, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: TAB — DELAMINATED (LT WING) · airframe 38,379 hrs · 25,658 cycles

LEFT WING INBD CONTROL TAB DELAMINATED ON UPPER SURFACE. R & R TAB IAW TC.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 715 - 655. REPAIRED CUSP WEB IAW SRM & DWG.

Part: HINGE BRACKET — CRACKED (LT AILERON) · airframe 38,379 hrs · 25,658 cycles

LEFT WING AILERON OTBD HINGE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOORBOARD 222AGF DELAMINATED. R & R FLOORBOARD IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOORBOARD 222GF DELAMINATED. R & R FLOORBOARD IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,379 hrs · 25,658 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 655 - 715. R & R CUSP WEB IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOORBOARD 222WF DELAMINATED. R & R FLOORBOARD IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOORBOARD 223DF DELAMINATED. R & R FLOORBOARD IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

MAIN CABIN FLOORBOARD 222AHF DELAMINATED. REPAIRED FLOORBOARD IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 38,379 hrs · 25,658 cycles

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

Part: SUPPORT — CRACKED (RT MLG DOOR) · airframe 38,379 hrs · 25,658 cycles

RIGHT WW DOOR CROSS BAR LOWER SUPPORT CRACKED. R & R CROSS BAR IAW SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 38,379 hrs · 25,658 cycles

RIGHT WW INBD SIDE OF INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: COVER — CRACKED (R1 DOOR) · airframe 38,379 hrs · 25,658 cycles

R1 DOOR EMER EVAC SLIDE COVER EXTERIOR HOLDER PLASTIC CRACKED. R & R COVER IAW SRM.

Part: TAB — DELAMINATED (LT WING) · airframe 39,435 hrs · 26,384 cycles

LEFT WING INBD CONTROL TAB DELAMINATED ON UPPER SURFACE. REPAIRED TAB IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 39,545 hrs · 26,459 cycles

EXIT LIGHT LENS LOOSE AT 24 DEF. R & R LIGHT LENS IAW MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 39,320 hrs · 26,304 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR SLIDE LOOSE. SECURED GIRT BAR IAW AMM.

Part: HOLDER — DIRTY (GIRT BAR) · airframe 38,882 hrs · 25,998 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER SECURING CLIP DIRTY. CLEANED HOLDER IAW MM.

Part: TAB — DELAMINATED (LT AILERON TAB) · airframe 37,332 hrs · 25,006 cycles

LT WING INBD AILERON TAB DELAMINATED ON UPPER SURFACE. R & R TAB ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,660 hrs · 24,592 cycles

RT EMERGENCY EVAC LIGHT LOOSE AT ROW 3. SECURED LIGHT ASSEMBLY IAW AMM.

Part: ROD END — FAULTY (ELEVATOR TAB) · airframe 36,209 hrs · 24,303 cycles

AIR TURNBACK AFTER TAKEOFF, FELT VIBRATION IN YOKE & FLOOR. R&R ELEVATOR GEARED TAB CONTROL ROD ENDS IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 35,627 hrs · 23,951 cycles

OVERHEAD CEILING EMERGENCY EXIT SIGN CRACKED AT ROW 1. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: CONTROL VALVE — FAULTY (HYDRAULIC SYS) · airframe 35,440 hrs · 23,840 cycles

HYD QUANTITY LOW ALERT ALTERNATE EXTENSION GEAR DOORS OPEN ON LANDING. REMOVED AND REPLACED HYD TRANSFER PUMP FLOW CONTROL VALVE PER MM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 34,488 hrs · 23,236 cycles

LEFT WING FIXED L/E - AT 58.500 - BONDING STRAP CRACKED. REMOVED & REPLACED STRAP PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

LIGHT CUSP WEB CORRODED AT BS 560 TO BS 579. REPAIRED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

RIGHT CUSP WEB CORRODED AT STA 541 TO STA 560. REPAIRED WEB PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

RIGHT CUSP WEB CORRODED AT STA 560 TO STA 579. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

TAIL COMPARTMENT LEFT SIDE CRACKED WEB AT FS 1200, LONGERON 3L. REPAIRED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

WING CENTER SECTION, RBL 45 SEAT TRACK VERTICAL SUPPORT FITTING CRACKED AT STA 737. REMOVED AND REPLACED FITTING PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 34,488 hrs · 23,236 cycles

WING CENTER SECTION FRONT SPAR, VERTICAL STIFFENER UNDER RBL 24 CRACKED AT STA 661. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CORRODED (LT WING) · airframe 34,488 hrs · 23,236 cycles

LEFT WING AFT FAIRING - FRAME 832 AT L26L TO L30L CORRODED. REMOVED AND REPLACED FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (NR 2 PYLON) · airframe 34,488 hrs · 23,236 cycles

NR 2 PYLON INSIDE ACCESS PANEL 440JB VERTICAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

LONGERON 2L CRACKED AT STA 1133. REPAIRED LONGERON PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

AFT CARGO COMPMENT FRAME CORRODED AT BS 946, BETWEEN L-28L TO L-27L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

FUSELAGE FRAME CRACKED AT STA 1022 BETWEEN LONGERONS 13L & 13L. REPAIRED FRAME PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

CABIN SEAT TRACK SECTION CORRODED BETWEEN BS 342 TO BS 588, RBL 44. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

LONGERON 2R CRACKED AT STA 1133. REPAIRED LONGERON PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

CABIN FLOORBOARD SUPPORT CORRODED AT BS 1044, RBL 20. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

LEFT AFT OVERWING EXIT HATCH FRAME FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM.

Part: SPRING — BROKEN (EMERGENCY EXIT) · airframe 34,488 hrs · 23,236 cycles

AFT PRESSURE BULKHEAD EMERGENCY EXIT DOOR SEAT RIGHT SPRING BROKEN. REMOVED AND REPLACED SPRING IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,488 hrs · 23,236 cycles

MAIN CABIN FLOOR PANEL 221 UF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM AND AMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

FORWARD CARGO RIGHT TRACK SUPPORT ATTACH CLIP CRACKED AT STA 434. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,488 hrs · 23,236 cycles

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

Part: SEAL — LOOSE (R1 DOOR) · airframe 34,488 hrs · 23,236 cycles

R1 DOOR SLIDE COVER SEAL LOOSE AT LWR FWD CORNER. RE-SECURED SEAL IAW AMM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

FWD CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 362 TO BS 434. REMOVED AND REPLACED PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,488 hrs · 23,236 cycles

AFT CARGO DOOR LOWER JAMB PAN CORRODED BETWEEN BS 954 TO BS 994. REMOVED AND REPLACED PAN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,527 hrs · 23,259 cycles

AFT EMERGENCY FLASHLIGHT INOP. REPLACED AFT FLASHLIGHT BATTERY IAW AMM.

Part: INDICATION SYS — FAULTY (LT MLG) · airframe 34,419 hrs · 23,193 cycles

DIVERSION -- LEFT MAIN LANDING GEAR LIGHT STAYED RED WITH GEAR HANDLE UP. CYCLED PER QRH 3 GREEN WHEN DOWN ALL GEAR DOORS APPEAR UP NO EXTRA GEAR NOISE OR DRAG. LEFT MLG GEAR FAULTY INDICATION, COMPLIED WITH MM & EA.

Part: STRUCTURE — CORRODED (GALLEY)

GALLEY COFFEEMAKER COMPARTMENTS 102, 103 AND 106 LOWER SURFACE, CORROSION. ACCOMPLISHED LOWER SURFACE PANEL REPLACEMENT PER EA 17-25-03110IR.

Part: FRAME — CRACKED (FUSELAGE)

APU ENCLOSURE RIGHT FWD FRAME, CRACKED. ACCOMPLISHED FRAME REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PASSENGER ENTRANCE AREA FLOOR SUPPORT, STA 187, LBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 180, RBL 23 TO RBL 37, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FAIRING — CRACKED (HORIZ STAB)

LEFT LOWER HORIZONTAL STAB L/E FAIRING, CRACKED. ACCOMPLISHED FAIRING DOUBLER REPAIR PER B717 SRM 55-00-00 FIG 201 REPAIR 1.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR SUPPORT, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: DOUBLER — CRACKED (FUSELAGE)

CABIN LONGERON FINGER DOUBLER, STA 200, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER DOUBLER FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 160, RBL 4, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

L1 DOOR SCUFF PLATE SUPPORT ANGLE, CORROSION. ACCOMPLISHED SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, LBL 12 TO RBL 7, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 198 TO 256, RBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: APU — SHUTDOWN

APU SHUT DOWN ON ITS OWN AFTER LOUD BANG. APU WAS REMOVED AND SERVICEABLE APU ASSEMBLY INSTALLED ON LOG PAGE 1733519.

Part: BATTERY — DISCHARGED (CABIN)

FIVE FORWARD RIGHT SIDE A 3 FORWARD LEFT EMEREGENCY CEILING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY/BATTERY B5-227 IAW AMM 33-51-03 OPS/FUNCTIONAL CHECK NORMAL IAW AMM 33-51-00.

Part: CDU — MALFUNCTIONED (COCKPIT)

BUS DC R OFF BUS AC R OFF LOST DU 4, 5, 6 & NR 2 MCDU. PERFORMED FIM 24-30 TASK 805 & FOUND RPCDU GCU FAULT. REMOVED AND REPLACED RPCDU PER 717 AMM 24-21-04 & REMOVED AND REPLACED POWER RELAYS PER 717 AMM 24-21-06. RPCDU OPS CHECKS GOOD PER 717 AMM 24-21-04. OK FOR CONTINUED SERVICE.

Part: SLIDE — OUT OF POSITION (CABIN DOOR)

MAIN CABIN DOOR SLIDE PANEL FELL OUT OF DOOR LANYARD ASSEMBLY. REPLACED THE FORWARD ENTRANCE DOOR SLIDE. REF MM 25-61-03.

Part: SIGN — LOOSE (CABIN)

LIGHTED EXIT SIGN COVER OVERHEAD BUSINESS CLASS LOOSE. REPLACED EXIT SIGN.

Part: LIGHT — MISSING (CABIN)

EMERGENCY LIGHT MISSING ROW 1. INSTALLED EMERGENCY LIGHT.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: LINE — LEAKING (GALLEY)

SMOKE AND ACID SMELL IN COCKPIT. PUFF AND ELECTRICAL SMELL GALLEY AREA IE COFFEE POTS REPORTED BY A FLIGHT ATTENDANT. FOUND WATER LEAK IN GALLEY DRIPPING ON NR 3 COFFEEMAKER CONNECTOR CAUSING A SHORT AND SMALL AMOUNT OF SMOKE. REPLACED WATER SUPPLY LINE. REF M/M 38-10.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING POWER SUPPLY IAW M/M 33-51-06, OPS CHECK OK.

Part: VENT — CRACKED (FUSELAGE)

REPAIR OF AFT FUSELAGE RIGHT SIDE VENT. INSTALLED REPAIR AT AFT FUSELAGE RIGHT SIDE VENT BOX DRAIN PAN IAW AIRTRAN T/C 17-5320-23 FIGURE 1 AND FIGURE 2 MATERIAL USED 7075-T6.0.40 SIZE OF DOUBLER 5.5 X 4.19 X 4.06 INCHES PO 023152.

Part: SKIN — DENTED (BS 250)

FUSELAGE SKIN HAS DENT STA 250. INSTALLED FLUSH REPAIR AT STA 229 TO STA 263 AND BETWEEN LT LON. 16 AND 18. IAW 53-00-01 FIG 201. MATERIAL USED FILLER 2024-T3-050 SIZE 34.3750 INCH X 14 INCH PO NR 022199, DOUBLER 2024-T3.063 SIZE 45 INCHES X 4 INCHES AND FINGER DOUBLER 2024-T3.025 SIZE 50 INCHES X 6 INCHES PO NR 022287.

Part: ENGINE — FAILED (NR 2)

CLIMBING THROUGH 16,000 FEET RIGHT ENGINE ROLLED BACK TO IDLE POWER. ENGINE SURGE RIGHT LIGHT CAME ON WITH A MESSAGE TO INCREASE ENGINE BLEED. RPM LOW LIGHT ALSO CAME ON. THROTTLE WAS BROUGHT BACK TO IDLE AND ANTI-ICE WAS TURNED. THROTTLE WAS ADVANCED. ENGINE REMAINED IN IDLE (N1 21 PERCENT - N2 62 PERCENT) N1 VIBE WAS 99. ENGINE WAS SHUTDOWN AND RESTARTED, START WAS NORMAL BUT ENGINE REMAINED IN IDLE WHEN THROTTLE WAS ADVANCED. ENGINE WAS SHUTDOWN AGAIN AND AIRCRAFT LANDED IN BMI. REMOVED AND REPLACED THE NR 2 ENGINE.

Part: ENGINE — MAKING METAL (LEFT)

AT FLIGHT LEVEL 28,000 AND DESCENDING WHEN THE AUTO THROTTLES RETARDED, A LOUD POP OCCURRED, THE AUTO THROTTLES WENT TO GROUND IDLE, THE EXHAUST GAS TEMPERATURE STARTED TO CLIMB, AT EGT 928 DEGREES CELSIUS. CREW SHUTDOWN THE LEFT ENGINE MANUALLY. UPON ARRIVAL METAL WAS DISCOVERED IN THE TAIL SECTION. REMOVED AND REPLACED NR 1 ENGINE.