N986AT

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,771 hrs · 42,442 cycles

EMERGENCEY LIGHTS ROW 20-21 EXIT LIGHTS INOP. R & R BATTERY PACK B5-119 AND BATTERY POWER SUPPLY PER B717 AMM 33 -51. (7556762)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,771 hrs · 42,442 cycles

EMERGENCEY PATH LIGHTS ROW 1-13 INOP. R & R BATTERY PACK P5-227 PER B717 AMM 33-51 (7556761)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 58,685 hrs · 42,353 cycles

LEFT WING REAR SPAR LOWER CAP AFT FLANGE CRACKED NEAR XRS = 164. ACCOMPLISH ER/A 627199-14AD REV D (1156482)

Part: FUEL SYS — LEAKING (ZONE 600) · airframe 58,384 hrs · 42,092 cycles

SHIP 9584 C/W ERA 621136-14AD REV A - RH WING / REAR SPAR LOWER CAP / FUEL LEAK. CORRECTIVE ACTION: C/W ERA 621136-14AD REV A (1058308)

Part: FUEL SYS — LEAKING (ZONE 600) · airframe 58,347 hrs · 42,054 cycles

SHIP 9584 PER ERA 621136-14AD WORKING CARD 5720-01103-01B. FUEL LEAK FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: COMPLIED WITH PRI 621136-14AD REV A REV 0 (7125286)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 58,327 hrs · 42,031 cycles

SHIP 9584 CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP AFT LEG. CORRECTIVE ACTION: COMPLIED WITH 627199-14 REV A LH WING REAR SPAR LOWER CAP CRACK REPAIR. (1045285)

Part: NONE — NONE (NONE) · airframe 58,327 hrs · 42,031 cycles

ER/A 627199-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: C/W ERA 627199.

Part: REPAIR — NOT REPORTED (ZONE 600) · airframe 58,327 hrs · 42,031 cycles

SHIP 9584 EXISTING REPAIRS FOUND ON RH AFT REAR SPAR FC 5720-01103. REPAIRED PER ER/A 621136-14AD (7125256)

Part: REPAIR — NOT REPORTED · airframe 58,152 hrs · 41,873 cycles

-AD- EXISTING REPAIR FOUND, CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHUR FLIGHT REF. FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FOR PERFORMED REPAIR. (LP #6990539)

Part: NONE — NONE (NONE) · airframe 57,622 hrs · 41,376 cycles

-AD- EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHER FLIGHT REF FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FOR PERFORMED REPAIR. (LP #0790531)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,564 hrs · 41,324 cycles

THE EMERGENCY LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6384488)

Part: LENS — DETACHED (ZONE 200) · airframe 57,564 hrs · 41,324 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. THE EXIT SIGN COVER FELL OFF. MAINTENANCE RESECURRED THE LENS COVER. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #776098)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 57,137 hrs · 40,930 cycles

THE AFT OVER WING EXIT DOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY (B5-230) AND THE LIGHT OPERATIONALLY CHECKED GOOD IAW B717 AMM 33-51. (LP #6413923)

Part: FUEL CELL — LEAKING (ZONE 600) · airframe 57,118 hrs · 40,914 cycles

-AD- FOUND FUEL SEEPING FROM FWD FLAP CARRIAGE MOUNT AND DOUBLER ON RT WING INBOARD FLAP AT XRS 164. (FC 5720-01103) PERFORMED ALL REPAIRS PER PRI 621136-14, REV 13. LEAK CHECK WAS GOOD. REPAIRS COMPLETED IAW ER/A 621136-14AD, REV O, SECTION 1. A/C OK FOR SERVICE. ALL CDCCL AND SFAR 88 REQUIREMENTS HAVE BEEN MET. RII + NDT C/W PER ERA 621136-14AD, (QC5158). (LP #0652085)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,118 hrs · 40,914 cycles

-AD- EXISTING REPAIRS FOUND. PERFORMED ALL REPAIRS PER PRI 621136-14, REV 13. REPAIR LEAK CHECK WAS GOOD. REPAIRS COMPLETED IAW ER/A 621136-14AD, REV O, SECTION 1. A/C OK FOR SERVICE. ALL CDCCL AND SFAR 88 REQUIREMENTS HAVE BEEN MET. RII + NDT C/W PER ERA 621136-14AD. (LP #0652092)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 56,941 hrs · 40,754 cycles

BOTH EMERGENCY LIGHTS IN CABIN ABOVE AFT OVERWING EXITS ARE INOP. CORRECTIVE ACTION: REPLACED BATTERY AT STA 426.

Part: LENS — MISSING (ZONE 200) · airframe 56,948 hrs · 40,761 cycles

AIRCRAFT 9584, EMERGENCY LENS COVER AT 26CDE IS MISSING. CEILING EMERGENCY LIGHT. CORRECTIVE ACTION: INSTALLED EMERGENCY CEILING LENS COVER PER B717 AMM 33-51. (LP 5719964)

Part: BATTERY — NO TEST (ZONE 200) · airframe 56,780 hrs · 40,616 cycles

FOUND OVERWING EMERGENCY EXIT LIGHTS OVERHEAD EXIT LIGHTS IN ROW 20 TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY FOR ROW 20 LIGHT PER B717 AMM 33-51. OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD. OK FOR SERVICE. (LP #6008052)

Part: CYLINDER — FAULTED (LT MLG DR LATCH) · airframe 55,980 hrs · 39,901 cycles

SHIP 9584 -ATB/GEAR/DE- FOLLOWING TAKEOFF AND LANDING GEAR RETRACTION, THE CREW RECEIVED A "LEFT MAIN GEAR UNSAFE" MESSAGE. AN EMERGENCY WAS DECLARED, AND THE CREW RETURNED THE AIRCRAFT TO ATL AND LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR LATCH CYLINDER IN REF B717 AMM 32-34. OPERATIONAL AND LEAK CHECKS WERE GOOD. GEAR FUNCTIONAL CHECK WAS GOOD. (LP #5296266)

Part: PAN — CRACKED (AFT CARGO) · airframe 55,749 hrs · 39,702 cycles

CRACK ON INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR. SUMMARY OF NRC 00087: INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR WAS REPAIRED PER ERA 615204-14 REV ORIGINAL SECTION I: REPAIR AND PRI 615204-14 REV 2. ASSOCIATED ERA 14-615204 ADDED FOR AC 9584. (LP #0180594)

Part: SKIN — CORRODED (AIRSTAIR DOOR) · corrosion level 2 · airframe 55,749 hrs · 39,702 cycles

CORROSION ON INNER SKIN NEXT TO HINGE AT FORWARD AIR STAIRWELL DOOR. SUMMARY OF NRC 00127: STAIRWELL DOOR WAS REPLACED PER BOEING 717-200 AMM 52-63-01. (LP #0177811)

Part: DOUBLER — CORRODED (BS 908 L29L/R) · corrosion level 2 · airframe 55,749 hrs · 39,702 cycles

CORROSION ON DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT. SUMMARY OF NRC 00535: CORROSION LEVEL 2. DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 FIG 201 AND 51-41-05-0G. (LP #0175829)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 55,749 hrs · 39,702 cycles

CRACK ON INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00069: INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. (LP #0171673)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,749 hrs · 39,702 cycles

CRACK INTERCOSTAL AT X=0, BTWEEN STA Y=1002 TO Y=1022, CABIN FLOOR SUPPORT STRUCTURE. SUMMARY OF NRC 00511: TRIMMED OUT INTERCOSTAL AT X=0, BT STA Y=1002 TO STA Y =1022 WAS REPAIRED PER B717-200 SRM-51-70-11-2R PROCEDURE 1 REPAIR. (LP #0156032)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,749 hrs · 39,702 cycles

SCRATCH ON WEB BTW APROX STA Y199/Y197 AND -X54 AT PAX CABIN. SUMMARY OF NRC 00327: SCRATCH ON WEB BTW APROX STA Y199/Y197 AND -X54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (LP #0149851)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,749 hrs · 39,702 cycles

CRACKS ON LOWER SURFACE OF CUSP WEB MEMBRANE RH ON STA Y=655, 674, 890, 694, AND 697 AT CPAX. SUMMARY OF NRC 00316: CRACKS ON LOWER SURFACE OF CUSP WEB MEMBRANE RH ON STA Y=655, 674, 694, AND 697 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 AND (ET) HFEC INSPECTION WAS ACCOMPLISHED ON LOWER SURFACE OF CUSP WEB MEMBRANE RH ON STA Y=890 AT CPAX, NO CRACKS WERE FOUND PER DC-MD /BOEING NDTSPM PART 6, 06-10-01.001.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,749 hrs · 39,702 cycles

CORROSION OUT OF LIMITS ON RH CUP WEB MEMBRANE ON STA Y=527 AND STA Y=608 PER B717-200 SRM 53-00-55-1A PROCEDURE 1. AD. 1 PAR 4. FIG 101. SUMMARY OF NRC 00457: CORROSION LEVEL 2. RH CUSP WEB MEMBRANE ON STA Y=527 WAS REPAIRED PER B717-200 SRM 51-70-01-2R PROCEDURE 2 REPAIR 2 AND RH CUSP WEB MEMBRANE ON STAY=608 MUST BE ATTENDED UNDER NRC 316. (LP #0137363)

Part: CUSP WEB — UNKNOWN (UNKNOWN) · airframe 55,749 hrs · 39,702 cycles

CRACK ON CUSP WEB LH SIDE BTW STA Y=655 X=49, Y=653 X=57.5, Y=675 X=46, AND Y=717 X=46 AT PAX CABIN. SUMMARY OF NRC 00366: CUSP WEB LH SIDE BTW STA Y=655 X=49, Y=653 X=57.5, Y=675 X=46, AND Y=717 X=46 AT PAX CABIN WAS REPAIRED PER B717-200 SRM-53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0137553)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,749 hrs · 39,702 cycles

CRACK ON INTERCOSTAL (CEILING AREA) BTW SAT 851 AND X=0 AT AFT CARGO. SUMMARY OF NRC 00137: INTERCOSTAL (CEILING AREA) BTW SAT 851 AND X=0 AT AFT CARGO WAS REPAIRED PER B717-200 SRM 51-70-11-2R, PROCEDURE 1. (LP #0134029)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,620 hrs · 38,770 cycles

THE EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERIES PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. THE AIRCRAFT RETURNED TO SERVICE. (LP #9834970)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,576 hrs · 38,736 cycles

THREE EA HOLES WITH CRACK INDICATION IN SKIN LAYER, IB EDGE OF LOWER WING SKIN DOUBLER IB OF XRS 164.00. MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 27. (LP #2790416)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,576 hrs · 38,736 cycles

FLAP HINGE ATTACH FITTING INSIDE WING AT XRS 164.00 BOTTOM LUG HORIZONTAL FASTENER HOLES, 3 EA OUTBOARD SIDE - MARKED. COMPLIED WITH ON ERA 6071561-14 AD STEP 38 AND FIGURE 10. (LP #2790427)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,576 hrs · 38,736 cycles

3 EA HOLES MISDRILLED IN SKIN BELOW XRS 140.00 - MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 23. (LP #2790419)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 54,510 hrs · 38,680 cycles

CORROSION AT LWR FLAP FITTING ATTACH POINTS ON FWD INBD DRIVE FITTING ASSY RH SIDE. REMOVED HINGE FLAP FITTING NONROUTINE CARDS #09 & 01. REMOVED DAMAGE AT HOLE #12 BORE AND #13 BORE AND SPOT FACE WITHIN LIMITS PER B717 OHM 27-50-5 FIG 602. PERFORMED MPI INSPECTION OF BORES & SPOT FACE OF HOLE 13 & BORE OF HOLE #12 PER OHM 27-50-5 FIG 604. NO INDICATIONS (QC4051). FABRICATED BUSHINGS PER B717 OHM 27-50-5. MPI C/W PER OHM 27-50-5 PG 604 STEP I. (7) (QC5261). ROTO-PEEN AREA PER OHM 27-50-5. CAD PLATED AREA AND INSTALLED BUSHINGS PER OHM 27-50-5. (LP #2627878)

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 54,394 hrs · 38,580 cycles

DENT AFT CARGO DOOR, QTY 2. 1) 12" FROM TOP EDGE, 18" FROM T/E. 2) FWD EDGE IAW B717 SRM 53-01-01 AD 3 COND 1B DENT ORIGINALLY DOCUMENED, INSPECTED, MEASURED BY AIRTRAN/SWA, DECAL CONDITION MONITOR REPAIRED AT C-CHECK INTERVALS. AFT CARGO DOOR HAS BEEN REPLACED REF LOG 6701428. OK TO CLOSE MON LOG-PAGE. DOOR SKIN WAS REPLACED ON FTN 4G3097 PER LOG 0121425.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 54,394 hrs · 38,580 cycles

THE AFT CARGO DOOR HAS SKIN DAMAGED ALONG AFT EDGE OF DOOR. MARKED. REF NRC 74: MAINTENANCE REPLACED THE CARGO DOOR PER B717 AMM 52-31-01. (LP #2577273)

Part: FLOOR SUPPORT — CORRODED (BS 194-200) · corrosion level 2 · airframe 54,393 hrs · 38,578 cycles

CORROSION ON FLOOR SUPPORT AT RBL 7 STA 194-200 (C-CHECK N/R CARD 343). REPLACED FLOOR SUPPORT REF B717 DWG 9936534. (LP #2573682)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 54,393 hrs · 38,578 cycles

FWD GALLEY FLOOR AREA HAS LIGHT CORROSION UPPER SURFACE OF FLOOR SUPPORT STA 160 TO STA 200 X=4300. REPLACED FLOOR SUPPORT REF BAC DWG 9936534. SUBSTITUTED FASTENERS AS NECESSARY REF B717SRM 51-40-03. (LP #2572973)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 54,393 hrs · 38,578 cycles

AFT CARGO DOOR JAMB HAS CORROSION ON LOWER DOOR FRAME PAN ALL LONG LOWER END OF SCUFFPLATE. MARKED. REPAIRED DOOR PAN REF B717 SRM 53-20-15-2R PROCEDURE 7. (LP #2566110)

Part: FLOOR SUPPORT — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 54,393 hrs · 38,578 cycles

CORROSION FOUND ON FWD GALLEY AREA FLOOR SUPPORT STA 180 X7000 TO X4300. SUMMARY SEE NRC 001-0010:2500-2647/031 00377: REPLACED FLOOR SUPPORT REF BAC DWG 9936534, SUBSTITUTE FASTENERS AS NECESSARY REF B717 SRM 51-40-03. (LP #2565908)

Part: SLIDE — DISLODGED (TAILCONE) · airframe 51,083 hrs · 35,614 cycles

THE TAILCONE SLIDE IS OUT OF THE COVER. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAIL CONE SLIDE WAS REPLACED PER W/C 2561-9006. (LP #7804688)

Part: COVER — DETACHED (SLIDE) · airframe 50,713 hrs · 35,315 cycles

DURING OTHER MAINTENANCE IN THE TAIL OF THE AIRCRAFT, THE SLIDE COVER WAS FOUND TO BE OFF ITS HINGES. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RESEATED SLIDE COVER PER B717 AMM 25-61. PER RII LIST, COVER REINSTALL IS NOT RII PER NOTES. (LP #7409858)

Part: COVER — DISLODGED (TAIL SLIDE) · airframe 50,690 hrs · 35,294 cycles

THE TAILCONE SLIDE COVER DISLODGED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RESECURED THE TAILCONE SLIDE COVER AS REQUIRED. CONTACTED MCC AND VERIFIED RII NOT REQUIRED FOR RESECURING COVER. (LP #7409851)

Part: FRAME — CORRODED (AFT CARGO) · airframe 50,528 hrs · 35,173 cycles

CORROSION ON AFT SIDE OF FRAME AT AFT CARGO BIN AFT BULKHEAD STA 1022. MARKED. NRC 037-0022:5310-2014/002 00282 REPAIRED REF B717 SRM 53-20-07-2R. (LP #1748759)

Part: DOOR — DENTED (AFT CARGO) · airframe 55,749 hrs · 39,702 cycles

DENT AFT CARGO DOOR (X2), ONE OF WHICH IS 12" FROM TOP EDGE, 18" FROM TRAILING EDGE. THE OTHER IS ON THE FWD EDGE. FWD EDGE IAW B717 SRM 53-01-01 AD 3 COND 1B DENT ORIGINALLY DOCUMENED, INSPECTED, MEASURED BY AIRTRAN/SWA. DECAL CONDITION MONITOR REPAIRED AT C-CHECK INTERVALS. ERA WAS VERIFIED AND DECAL WAS FOUND IN GOOD CONDITION. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP 30-10-70 PAR I, PG 14. THE AFT CARGO DOOR WAS REPLACED ON 05DEC19 PER LOG #6701428. OK TO CLOSE MONITOR. (LP #2052559)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,067 hrs · 34,799 cycles

THE FORWARD EMERGENCY EXIT SIGN FLASHES ON, THEN OFF. MAINTENANCE FOUND THE BATTERY PACK, B5-235, CHARGE TO BE LOW. THE BATTERY PACK WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD. (LP #6536600)

Part: LENS — MISSING (EXIT SIGN) · airframe 48,383 hrs · 33,507 cycles

EXIT SIGN AT THE FRONT OF FIRST CLASS IS MISSING. MAINTENANCE SECURED THE LENS. OKAY FOR SERVICE. (LP #5502216)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,963 hrs · 32,458 cycles

THE FORWARD ENTRYWAY AND COCKPIT DOOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD AREA/COCKPIT DOOR EMERGENCY LIGHT BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 46,541 hrs · 32,147 cycles

THE L1 DOOR GIRT BAR WAS NOT POSITIONED THROUGH SLIDE WIRE LOOP. MAINTENANCE RE-POSITIONED THE L1 DOOR GIRT BAR THROUGH WIRE LOOP LANYARD. CHECKS NORMAL PER AMM 25-61-13.

Part: FUEL FILTER — LEAKING (NR 1 ENGINE) · airframe 46,025 hrs · 31,814 cycles

DISCOVERED FUEL LEAK FROM NR 1 ENGINE WHILE AIRBORNE. FOUND FUEL LEAKING FROM LEFT ENGINE LOW PRESSURE FUEL FILTER. HELICOIL HAD BACKED OUT OF FILTER HOUSING AND O-RING DEFORMED AND LEAKED. R&I LEFT ENGINE LOW PRESSURE FUEL FILTER HOUSING PER AMM 73-11-01. R&I FUEL FILTER PER AMM 73-11-01. PERFORMED ENGINE RUN AND LEAK CHECK PER AMM 71-00-11 710-801 TEST 2A. NO FURTHER LEAKS. OK FOR SERVICE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 43,327 hrs · 29,982 cycles

FIRST CLASS EXIT SIGN BROKEN. REPAIRED THE SIGN. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,877 hrs · 29,649 cycles

FLT ATTENDANT FOUND FRONT CENTER EXIT SIGN LENS MISSING. MAINTENANCE REPLACED THE SIGN LENS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 42,811 hrs · 29,612 cycles

DURING SERVICE CK FOUND EXIT SIGNS AT ROW 19A NEED RELAMPED. RELAMPED EXIT SIGNALS AS REQUIRED. OK FOR SERVICE.

Part: ENGINE — MAKING METAL (NR 2) · airframe 41,894 hrs · 28,952 cycles

THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL FOLLOWING THE FAILURE OF THE NR 2 ENGINE. MAINTENANCE FOUND METAL IN TAILPIPE UPON THE AIRCRAFT'S ARRIVAL AND REPLACED THE ENGINE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,758 hrs · 28,846 cycles

VERIFY REPAIR DIMENSIONS PER SRM 53-20-07 REP3 FOR CORROSION ON LOWER LIP OF FRAME AT STA 908 L30 RT SIDE. VERIFIED REPAIR DID NOT CONFORM TO SRM 53-20-07 REP 3 DUE TO SHORT EDGE DISTANCE ON -17 PLATE AND -19 FILLER. FABRICATED NEW-17 PLATE AND -19 FILTERS, REPAIRED FRAME AT STA 908 L30 IAW SRM 53-20-07 REPAIR 3 PER ER/A 551831-14.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,758 hrs · 28,846 cycles

RIGHT WALKWAY SUPPORT ANGLE ATTACHED TO BOTTOM STIFFENER / FRAME IN AFT ACCESSORY AT STA 1133 IS CORRODED. RT WALKWAY SUPPORT STRUT WAS CORRODED TO 100%. REPLACED WALKWAY STRUT IAW B717 SRM 51-41-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,753 hrs · 28,843 cycles

DENT DAMAGE TO FUSELAGE STA 579 BETWEEN L27L AND L28L REQUIRES SRM REPAIR. REPAIRED FUSELAGE SKIN STA 579 BETWEEN L27L AND L28L IAW ER/A 549357-14 REV A.

Part: STRINGER — CORRODED (BS 1002-1024) · corrosion level 2 · airframe 41,753 hrs · 28,843 cycles

CORROSION ON STRINGER 24R BS 1002-1024. THE STRINGER WAS FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-00-00. REPLACED THE STRINGER IAW SRM 51-41-02.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 41,753 hrs · 28,843 cycles

AFT CARGO DOOR FRAME HAS SEVERAL AREAS OF CORROSION. PAN SPLICE FOUND TO BE OUT OF LIMITS, MORE THAN 50% REMOVED. REPLACED LOWER PAN SPLICE IAW SRM 53-20-15 REPAIR 7.

Part: FRAME — DENTED (BS 579) · airframe 41,753 hrs · 28,843 cycles

DENT FOUND IN FRAME BS 579 BETWEEN LONGERONS 27 AND 28L. REPAIRED THE FRAME IAW SRM 53-00-06 REPAIR 3 PG 201-206.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 41,753 hrs · 28,843 cycles

FLOOR PANEL 222MF HAT CHANNEL IS CRACKED AT AFT END. REPAIRED AFT END OF HAT CHANNEL ON FLOOR PANEL 222MF IAW SRM 53-20-50 REPAIR 5. REPAIR DOUBLER FABBED FROM 6061-0=.032 HEAT TREATED TO 6061-T6. APPLIED ALODINE AND PRIMER TO DOUBLER IAW SRM 51-22-01 PAGES 2 AND 3.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 41,753 hrs · 28,843 cycles

FLOOR PANEL 222AJF HAT CHANNEL IS CRACKED AT AFT END AND SEPARATING FROM PANEL ON FORWARD END. REPAIRED CRACK ON AFT END OF HAT CHANNEL ON FLOOR PANEL 222AJF IAW B717 SRM 53-20-05 REPAIR 5. REPAIR DOUBLER FABBED FROM 6061-0-.032 HEAT TREATED TO 6061-T6 APPLIED ALODINE AND PRIME TO DOUBLER IAW SRM 51-22-01 PAGES 2 & 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,753 hrs · 28,843 cycles

FS 1087 LONGERON 14R EMPENNAGE SKIN HAS 3 EA CRACKS, MARKED. HFEC VERIFIED IAW NDTSPM ETHF PROCEDURE 1, 06-10-01.001. CUT OUT CRACKED AREA; FABRICATED AND INSTALL FILLER/EXTERNAL REPAIR DOUBLER IAW ER/A 551823-14 REV, ORIGINAL AT F/S 1087 LONGERON 14R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,753 hrs · 28,843 cycles

CRACK AROUND RIVET HEAD IN FUSELAGE SKIN AT L14 LT STA 1076 ABOVE NR 1 ENGINE PYLON, LOCATION MARKED. REPAIRED SKIN AT L14 LT STA 1076 IAW ER/A 551822-14 REV O.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 41,753 hrs · 28,843 cycles

FLOOR PANEL 221SF HAS CRACKED HAT CHANNEL ON FORWARD END. REPAIRED CRACKED HAT CHANNEL ON FWD END OF FLOOR PANEL 221SF IAW SRM 53-20-50 REPAIR 5 DOUBLER FABBED FROM 6061-0-.032 HEAT TREATED TO 6061-T6 APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 & 3.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 41,753 hrs · 28,843 cycles

PANEL 223EF FORWARD CORNER IS BENT AND SEPARATED FROM BACKUP STRIP. FURTHER INSPECTION REVEALED A CRACK IN THE NR 2 FASTENERS HOLE. REPAIRED CRACK IAW SRM 53-00-00 REPAIR 1 DOUBLER FABBED. CRACK REPAIR SATISFIED SEPARATION REPAIR.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,753 hrs · 28,843 cycles

SHEAR TIE AT STA 1020 BULKHEAD FWD SIDE IS CRACKED BETWEEN STRINGER 6LT& 7LT. VERIFIED WITH HFEC. REPLACED SHEAR TIE AT STA 1020 ON FWD SIDE OF BULKHEAD BETWEEN STRINGERS 6L AND 7L REF SRM 51-41-02 AND 51-41-05.

Part: STIFFENER — CRACKED (FUEL TANK) · airframe 41,753 hrs · 28,843 cycles

RT VERTICAL STIFFENER ON FWD FACE OF CENTER FUEL TANK IS CRACKED. VERIFIED WITH HFEC, MARKED. REMOVED CRACKED RT VERTICAL STIFFENER AND REPLACED WITH SERVICEABLE STIFFENER IAW SRM 51-41-05. LEAK CHECK WILL BE COMPLETED ON 72816-0100-0123.

Part: SEAT TRACK — CORRODED (BS 215) · airframe 41,753 hrs · 28,843 cycles

CORROSION ON RT OTBD SEAT TRACK BS 215. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPLACED THE SEAT TRACK IAW SRM 51-41-01.

Part: SPLICE — DAMAGED · corrosion level 2 · airframe 41,753 hrs · 28,843 cycles

AFT SILL SPLICE IS CORRODED AND BENT. REMOVED AND REPLACED THE SILL SPLICE IAW SRM 53-00-00 FIG 103 AND DWG 5910142 REV DJ.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,753 hrs · 28,843 cycles

CORROSION ON UPPER SURFACE OF LT CENTER SEAT TRACK, AROUND FASTENER HOLES AT STA 1026 AND STA 1057 LEFT AFT LAV AREA. CORROSION ON UPPER SURFACE LT CENTER SEAT TRACK STA 1026-1057 BLENDED IAW SRM 53-00-00 FIG 103 ORIGINAL THICKNESS 0.080, 0.030 FOUND REMAINING OUT OF LIMITS IAW SRM 53-00-00. SEAT TRACK REPLACED IAW SRM 51-41-05 NEW SEAT TRACK FABRICATED IAW DLG.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 41,753 hrs · 28,843 cycles

LT INBOARD SEAT TRACK HAS MULTIPLE AREAS OF GOUGES AND CORROSION FROM STA 856 TO STA 956 (AREAS MARKED IN RED). REMOVED CORROSION AND GOUGES FROM SEAT TRACK LT IB STA 856-956. ORIGINAL THICKNESS .115" REMOVED .025" REMAINING .090" SEAT TRACK OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-20-52-2R REPAIR 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,753 hrs · 28,843 cycles

CORROSION ON THE F/O O/B SEAT TRACK. SEAT TRACK FOUND TO BE BEYOND LIMITS. REPLACED WITH NEW SEAT TRACK. INSTALLED NEW SEAT TRACK IAW SRM 51-41-01.

Part: LENS — CRACKED (EXIT SIGN) · airframe 36,093 hrs · 24,508 cycles

R1 DOOR EMER EXIT SIGN LENS CRACKED. REPAIRED LENS IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 36,093 hrs · 24,508 cycles

LEFT SIDE END OF CATWALK TAIL CONE EMER EGRESS SIGN EXIT CRACKED. R & R SIGN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,093 hrs · 24,508 cycles

RIGHT NLG STRUT DOOR AFT HINGE SKIN CUT OUT CRACKED AT AFT HINGE UPPER CORNER. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 36,093 hrs · 24,508 cycles

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

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 36,093 hrs · 24,508 cycles

LEFT WW FWD DOOR CUT OUT INBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 36,093 hrs · 24,508 cycles

C2 DOOR CUT OUT SEAL DEPRESSOR SPLICE PLATE DAMAGED BOTTOM OF CUT OUT. R & R PLATE IAW SRM & DWG.

Part: CROSSMEMBER — CRACKED (RT MLG DOOR) · airframe 36,093 hrs · 24,508 cycles

RIGHT WW DOOR CROSS BAR CRACKED ON LOWER END. R & R CROSS BAR.

Part: WIRE — LOOSE (CABIN) · airframe 36,613 hrs · 24,858 cycles

RIGHT EEPLS WIRE LOOSE BETWEEN ROW 25 TO ROW 31. SECURED WIRE IAW MM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 35,587 hrs · 24,177 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP IAW SIP.

Part: CABLE — MISROUTED (R1 DOOR) · airframe 34,569 hrs · 23,508 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: LANYARD — DISCONNECTED (R1 DOOR) · airframe 33,650 hrs · 22,927 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DISCONNECTED. REINSTALLED GIRT BAR LANYARD IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

AFT ALLY CANTED FRAME CRACKED AT STA 1189. R & R FRAME IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

PANEL 370BR CRACKED. R & R PANEL IAW SRM & DWG.

Part: RUB STRIP — CORRODED (LT WING) · airframe 32,751 hrs · 22,360 cycles

LT WING FUEL PANEL 520FT CUTOUT CORRODED. R & R RUBSTRIP IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CRACKED AT STA 655, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: RUB STRIP — CORRODED (LT WING) · airframe 32,751 hrs · 22,360 cycles

LT WING FUEL PANEL 520CT CUTOUT CORRODED. R & R RUB STRIP IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 32,751 hrs · 22,360 cycles

RIGHT WING LANDING ON PANEL 620FT LIGHT CORRODED. R & R RUB STRIP IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 32,751 hrs · 22,360 cycles

RT WING PANEL 620DT CORRODED. R & R RUB STRIP IAW SRM.

Part: RUB STRIP — CORRODED (LT WING) · airframe 32,751 hrs · 22,360 cycles

LT WING FUEL PANEL 520DT CUTOUT CORRODED. R & R RUB STRIP IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CRACKED AT STA 1022, RBL 54.5. REPAIRED CUSP WEB IAW SRM.

Part: PANEL — CORRODED (RT WING) · airframe 32,751 hrs · 22,360 cycles

RIGHT WING PANEL 620AT CORRODED. R & R PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CRACKED AT STA 674, LBL 56. R & R CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

AFT ACCESSORY COMP AT FRAME 1212 RT LOWER SIDE ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

SKIN CRACKED AT STA 1022, LONGERON 16R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 32,751 hrs · 22,360 cycles

CRACKED RIB ANGLE INTERNAL PASSENGER DOOR ENTRY BEAM NR 1 AFT CORNER. R & R DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED AT STA 941, RBL 57. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED AT STA 570, RBL 57. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED BETWEEN STA 513 TO STA 518, RBL 57. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED AT STA 304, RBL 57. R & R CUSP WEB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

AFT ACCESSORY COMP FORMER CRACKED AT STA 1133, LONG 2R. R & R SHEAR TIE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED AT STA 551, RBL 57. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

VERTICAL SUPPORT ANGLE CRACKED AT STA 715, RBL 44.0. R & R ANGLE IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CENTER WING BOX MAIN CABIN BELOW PASSENGER FLOOR BOARD VERTICAL SUPPORT CRACKED AT STA 737, RBL 44. R & R STIFFENER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

CUSP WEB CORRODED AT STA 475, RBL 57.6. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

LEFT FRAME BRACKET CRACKED AT STA 1178. REMOVED & REPLACED BRACKET IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222 LF DELAMINATED. R & R PANEL IAW SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 32,751 hrs · 22,360 cycles

RIGHT WING INBD BULLNOSE TO WING TO BODY FAIRING ATTACH SUPPORT CRACKED AT STA 636, LONG 20R. R & R STRAP IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222 JF DELAMINATED. R & R PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

SEAT TRACK CORRODED BETWEEN STA 588 TO STA 865, RBL 54.5. R & R SEAT TRACK IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222 AMF DELAMINATED. R & R PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

SEAT TRACK CORRODED BETWEEN BS 908 TO BS 965, RBL 54.5. R & R SEAT TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

FRAME CRACKED AT BS 674, RT SIDE. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

FRAME CRACKED AT STA 674, LBL 56. R & R FRAME IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222 AVF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222AAF DISBONDED. R & R FLOOR PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222 PF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DEBONDED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222 ABF DISBONDED. R & R FLOORBOARD IAW AMM.

Part: STRAP — CRACKED (LT WING) · airframe 32,751 hrs · 22,360 cycles

LEFT WING INBD BULLNOSE WING TO BODY FAIRING ATTACH STRAP CRACKED AT STA 686, LONG 20L. R & R STRAPS IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222 FF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

FLOORBOARD 221 UF DELAMINATED BETWEEN STA 313 TO STA 389. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222 AHF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222 ACF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOOR PANEL 222 ATF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD PANEL 222RF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DEBONDED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 222AEF DISBONDED. R & R FLOORBOARD IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

FRAME FLOORBEAM CRACKED AT STA 696, LBL 56. R & R FRAME IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 32,751 hrs · 22,360 cycles

PASSENGER FLOORBOARD 221BF DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW SRM.

Part: PAN — CORRODED (CARGO DOOR) · airframe 32,751 hrs · 22,360 cycles

C1 DOOR PAN CORRODED BETWEEN STA 370 TO STA 427, BETWEEN LONG 28R TO LONG 27R. R & R PAN IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

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

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,751 hrs · 22,360 cycles

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

Part: LATCH — DIRTY (GIRT BAR) · airframe 32,664 hrs · 22,305 cycles

L1 DOOR SLIDE GIRT BAR IS VERY DIFFICULT TO ARM. CLEANED AND LUBED L1 GIRT BAR LATCHES, OPS GOOD IAW AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 32,178 hrs · 21,995 cycles

LT SLIDE GIRT BAR CLIP UNATTACHED. SECURED GIRT BAR CLIP ASSEMBLY ON LT SLIDE IAW AMM 25-61-01.

Part: LENS — MISSING (CABIN) · airframe 31,214 hrs · 21,372 cycles

EEPLS LENSES MISSING BETWEEN ROWS 11 TO ROW 21. INSTALLED LENSES PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 31,214 hrs · 21,372 cycles

EEPLS BULBS MISSING BETWEEN ROWS 11 TO ROW 21. INSTALLED BULBS PER MM.

Part: BAR — OUT OF ADJUST (L1 DOOR) · airframe 31,164 hrs · 21,342 cycles

L1 DOOR EMERGENCY EXIT UPPER LATCH BAR OUT OF ADJUST. ADJUSTED BAR ASSY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 30,963 hrs · 21,204 cycles

RIGHT EEPLS LENS MISSING AT ROW 24. INSTALLED LENS PER AMM.

Part: LENS — MISSING (CABIN)

TWO EPL CLEAR LENSES MISSING. INSTALLED LENSES AS REQUIRED.

Part: SLIDE — UNSECURE (L1 DOOR)

L1 SLIDE NOT SECURE. REMOVED AND REPLACED L1 DOOR SLIDE. REF 25-61.

Part: LENS — MISSING (CABIN)

RED EMERGENCY LENS COVER MISSING - 21D. INSTALLED NEW EPL LENS (RED) 21D REF GMM/8103.

Part: LENS — MISSING (CABIN)

WHITE EMERGENCY LIGHT COVER MISSING - 20D. INSTALLED NEW EPL LENS (RED) 20D REF GMM / 8103.

Part: LENS — MISSING (CABIN)

EMERGENCY PATH LIGHTING COVERS MISSING ON ROWS 18 & 19. REPLACED LENS, CHECK OK MM3351.

Part: COVER — MISSING (CABIN)

EMERGENCY LIGHT COVER ON SEAT 21D MISSING. INSTALLED NEW COVER ON SEAT 21D PER M/M 33-51.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22R TO RBL 44R, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

FORWARD ENTRY DOOR AFT FRAME, STA 210, LONG 15, CRACKED. ACCOMPLISHED DOOR AFT FRAME DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

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 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LANYARD — TORN (R1 DOOR)

R1 DOOR LANYARD TORN, AWI. REMOVED AND REPLACED R1-DOOR LANYARD REF AMM 25-61AWI.

Part: COVER — UNKNOWN (CABIN)

THE 21-D NEEDS RED COVER EMERGENCY EXIT. INSTALLED 21D EMERGENCY EXIT LIGHT COVER AS REQUIRED.

Part: COVER — CRACKED (EMERGENCY LIGHT)

FWD CABIN CEILING EMERGENCY LIGHT COVER CRACKED - SECURED. REPLACED LENS PER AMM 33-51.

Part: LENS — MISSING (CABIN)

ONE WHITE EMERGENCY PATH LIGHT ASSY IS INOP AND BOTH BULB ARE INOP ON 2D, LENS ASSY IS MISSING. RELAMPED SEAT 2D EPL AND INSTALLED NEW LENS COVER REF AMM 33-50.

Part: COVER — MISSING (EMERGENCY LIGHT)

MISSING LIGHT COVER ON SEAT 12. INSTALLED LENS CHECKS GOOD REF MM 33-51.

Part: LIGHT — MISSING (CABIN)

ROW 17, 18, 19 EPL LENSES AND BULBS MISSING. INSTALLED NEW BULBS AND LENSES AT ROW 17, 18, 19, OPS CHECK GOOD REF B717 AMM 33-51.

Part: FRAME — DAMAGED (FUSELAGE)

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

Part: FRAME — DAMAGED (FUSELAGE)

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

Part: BATTERY — DISCHARGED (CABIN)

SEAT ROWS 25 THUR 31 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY SUPPLY ASSY & BATTERY OP'S CHECK GOOD REF MM 33-51.

Part: GIRT BAR — OUT OF POSITION (SERVICE DOOR)

SERVICE DOOR PACK SLIDE FOLDS HANGING LOW. REPOSITIONED GIRT BAR AND REINSTALLED LANYARD ASSY REF MM 25-61.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LOWER PAN CORRODED BEYOND LIMITS. FABRICATED 4 EACH SPLICE 7075 0.040 HEAT TREATED TO 7075 T6 AND INSTALLED AFT CARGO DOOR JAMB LOWER PAN CORROSION REPAIR PER SRM 53-20-15.

Part: BATTERY PACK — DISCHARGED (CABIN)

EPLS ON SEATS 25-31 NOT COMING ON. REMOVED AND REPLACED BATTERY SUPPLY ASSY AT B5-119. OPS CHECK GOOD, REF AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEAT EMERGENCY LIGHTS INOP SEAT ROWS 25-31 FED. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY FOR SEAT ROWS 25-31 FED. PER AMM 33-51, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FIRST CLASS ROWS 1, 2 AND 3 EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT P-118 PER AMM CH 33-51, OP'S CHECKED GOOD.

Part: ENGINE — FAILED (NR 1)

ENGINE LEFT FAILURE AROUND 11,000 DURING CLIMB OUT. REMOVED AND REPLACED LT ENG PER TASK CARD 607 ON W/O 139090.

Part: SUPPORT ANGLE — CRACKED (RT VENT BOX)

RT VENT BOX AND ANGLE SUPPORT ARE CRACKED. STOP DRILL THE CRACK AT RT VENT BOX IAW SRM 51-00-07. PERFORMED A HFEC INSP OF THE STOP DRILLED HOLE. IAW NDTSPM 06-10-01.001, NO CRACK FOUND EXTENDING BEYOND STOP DRILLED HOLE INSTALLED REPAIR AS RT VENT BOX DRAIN PAN IAW T/C 17-5320-2023 REMOVED AND REPLACED ANGLES ON RT SIDE VENT BOX IAW SRM 51-41-05 MAT USED 7075 T6 .090 PN 017523.