N925AT

Part: CONTACT — SHORTED (ZONE 200) · airframe 57,400 hrs · 42,061 cycles

SHIP 9574 -SMKE- AFTER LIGHT TEST, WE NOTICED THAT THE RIGHT APU BUS LIGHT WAS INOPERATIVE. WE TRIED RESETTING THE LIGHT BUT THE BULB AND SOCKET BRIEFLY EMITS SMOKE. MAINTENANCE FOUND THAT THE KORRY SWITCH BRACKET FOR THE APU LIGHT MADE CONTACT AND BURNT UP THE CONTACT POINT. THE RIGHT APU BUS LIGHT KORRY ASSEMBLY WAS REPLACED IAW B717 AMM 33-13 AND B717 IPC 24-21-14-01. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5146176)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,032 hrs · 40,828 cycles

DURING 1L DOOR (LT) SLIDE CHANGE, MAINTENANCE FOUND CONTAINER LANYARD ASSEMBLY CABLE FRAYED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A NEW LANYARD, PER AMDS CARD 2561-9004. RII COMPLIED WITH. (LP #0124553)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,730 hrs · 40,585 cycles

THE EMERGENCY EXIT SIGN AT THE TAILCONE, FELL OFF. MAINTENANCE RESECURED THE LIGHT COVER AS REQUIRED. OK FOR SERVICE. (LP #4279682)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,864 hrs · 39,843 cycles

EXIT SIGN AT FRONT OF CABIN IS BROKEN OFF FROM THE CEILING AND IS HANGING BY THE WIRES. MAINTENANCE REPLACED THE FWD CABIN SIGN PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #9962890)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,384 hrs · 39,410 cycles

SHIP 9574-ATB-DE/ENVIROMENTAL. PERFORMED AN AIR RETURN DUE TO A BIRD STRIKE TO THE RADOME AND LOSS OF WEATHER RADAR. CORRECTIVE ACTION: MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION, REPLACED THE RADOME AND THE WEATHER RADAR DRIVE UNIT ASSEMBLY. (LP 4043168,4043169,4043171)

Part: UNKNOWN — UNKNOWN · airframe 54,323 hrs · 39,352 cycles

SHIP 9574 -ATB- THE FLIGHT CREW ACCOMPLISHED AN AIR TURN BACK AFTER THE CONTROL TOWER INFORMED THEM OF SOMETHING OBSERVED TRAILING THE AIRCRAFT. THE CREW CONFIRMED A 2000# FUEL IMBALANCE BETWEEN THE LEFT AND THE RIGHT WING TANK QUANTITIES. THE LANDING WAS UNEVENTFUL, AND NO FUEL WAS LEAKING ONCE THE AIRCRAFT WAS ON THE GROUND. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE RIGHT OVER-WING FUEL CAP WAS MISSING AND ALLOWING THE FUEL TO VENT OUT OF THE RIGHT WING TANK. THE FUEL CAP WAS REPLACED AND NO OTHER LEAKS WERE NOTED. THE AIRCRAFT RETURNED TO SERVICE. (LP #4043130)

Part: NONE — NONE · corrosion level 2 · airframe 52,004 hrs · 37,247 cycles

CORROSION ON UPPER AND LOWER SURFACE AT SEAT TRACK RH RBL=54 BTW STA=715 TO STA=737 AT CPAX REF NRC 202. SUMMARY OF NRC 00292: CORROSION LEVEL 2, SEAT TRACK RH RBL=54 BTW STA=715 TO STA=737 WAS REPAIRED PER B717-200 SRM. 53-20-52 -2R REPAIR 5 FIGURE 201. (LP #2140625)

Part: NONE — NONE · airframe 52,004 hrs · 37,247 cycles

THE FORWARD RETAINER CLIP, ON THE COVER ASSEMBLY AT THE TAILCONE SLIDE, WAS FOUND BROKEN DURING STEP 13 OF JIC 5352-4002. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00286: A NEW CLIP RETAINER WAS INSTALLED ON FWD COVER ASSEMBLY AT THE TAILCONE SLIDE PER AMDS 5352-4002. (LP #2140562)

Part: NONE — NONE · corrosion level 2 · airframe 52,004 hrs · 37,247 cycles

CORROSION ON JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00030: CORROSION LEVEL 2, JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2) WAS REPAIRED PER B717 SRM 53-20-15-2R, REPAIR 7. (LP #2132801)

Part: NONE — NONE · corrosion level 2 · airframe 52,004 hrs · 37,247 cycles

CORROSION ON JAM BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00075: CORROSION LEVEL 2, JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15 -2R. (LP #2132980)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,857 hrs · 35,449 cycles

ON THE SERVICE CHECK, MAINTENANCE FOUND THE OVER WING WALL EXIT LIGHT TO BE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED THE POWER SUPPLY LOCATED AT B5-119. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY REF B717 AMM 33-51. (LP 7596098)

Part: SLIDE — NO TEST (L1 DOOR) · airframe 49,779 hrs · 35,389 cycles

THE L1 DOOR SLIDE FAILED THE DEPLOYMENT TEST FORECAST #95-0525-0111 DUE TO THE LANYARD NOT ATTACHED TO GIRT BAR. PN- D29982-225 SN-2678 MFR DATE- 11/09. MAINTENANCE REPLACED THE SLIDE PER W/C 2561-9001. (LP #1728645)

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 47,967 hrs · 33,762 cycles

AFT CARGO DOOR JAMB INTERNAL FACTORY ALUMINUM DOUBLER IS CORRODED FOR APPROXIMATELY 6 INCHES FWD AND AFT OF CENTERLINE. NRC 001-0304:5231-2002/002 00218: COMPILED WITH ER/A 585336-14 ORIGINAL. (LP #1494200)

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 47,967 hrs · 33,762 cycles

AFT CARGO DOOR JAMB HAS CORROSION. NRC 001-0304:5231-2002/001 00013: REPAIRED REF B717 SRM 53-20-15-2R PROC 7. (LP #1493931)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,863 hrs · 32,203 cycles

THE EMERGENCY LIGHTS IN ROW 5, 6, & 7 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-55. ALL CHECKS ARE GOOD. (LP #5531007)

Part: FRAME — CRACKED (BS 1162) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME BS 1162, BETWEEN LONGERONS 1L AND 2L. REPAIRED IAW ETI-17-18-061, REV 1, AND ER/A 567141-14, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FRAME BS 1022, BETWEEN LONGERONS 20R - 22R. REPAIRED IAW SRM 53-20-07-2R, REPAIR 3.

Part: ANGLE — CRACKED (BS 1162) · airframe 43,285 hrs · 30,350 cycles

CRACKED ANGLE BS 1162 LONGERON 2L. REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.

Part: SHEAR TIE — CORRODED (BS 1022) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE FRAME SHEAR TIE BS 1022 BETWEEN LONGERONS 29L - 29R. THE FRAME SHEAR TIE WAS REPLACED IAW DWG 9958214, REV BW, SRM 51-41-02, AND 51-41-05.

Part: INTERCOSTAL — CORRODED (BS 1022-1037) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION THE ON THE INTERCOSTAL, LONGERON 30 BETWEEN BS 1022 - 1037. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05.

Part: HINGE FITTING — WORN (LT WING FLAP) · airframe 43,285 hrs · 30,350 cycles

FREE PLAY AT THE LT WING OTBD FLAP HINGE FITTING. OTBD FLAP HINGE WAS REPAIRED IAW ETI-17-18-056, REV 3, AND ER/A 566913-14, REV ORIGINAL.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FLOOR PANEL 221NF. THE FLOOR PANEL WAS REPLACED IAW AMM 53-21-01.

Part: FRAME ANGLE — CORRODED (BS 954) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FRAME ANGLE BS 954 BETWEEN LONGERON 27L TO 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06-2R, REPAIR 2, AND DWG 9958214, REV BW.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION TYPE EXFOLIATION AT RT CUSP ANGLE STA 200. CORROSION LEVEL 2, RT CUSP ANGLE STA 200 WAS REPAIRED PER ETI-17-18-045 REV 1 AND ER/A 566866-14 REV ORIGINAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,285 hrs · 30,350 cycles

CRACK ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870. FRAME CLIP WAS REPAIRED PER SRM 53-00-06-2R REPAIR 2. HFEC INSPECTION WAS ACCOMPLISHED ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870 AFTER TRIM OUT. NO CRACKS WERE FOUND PER NDT SPM PART 6, 06-10-01.001.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 43,285 hrs · 30,350 cycles

CRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROTECTION LONG 7R AT PAX CABIN. GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R WAS REPAIRED PER ETI-17-18-043 REV 1 AND ER/A 566865-14 REV ORIGINAL.

Part: LONGERON — CORRODED (BS 934-1002) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION OUT OF LIMITS ON LONGERON 30, BS 934 TO 1002. CORROSION OUT OF LIMITS. THE LONGERON WAS REPLACED IAW SRM 53-20-05-01-3, FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,285 hrs · 30,350 cycles

DELAMINATION ON FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF AT PAX CAB (CPAX). NRC 00560: FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3 PAR 2. FLOOR PANEL WERE INSTALLED WITH CARD JIC 2040-0024. (LP #0469629)

Part: LONGERON — CORRODED (BS 990-1022) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON LONGERON 27L BETWEEN BS 990 TO 1022. THE LONGERON SECTION WAS REPLACED SRM 53-20-05-01-3, FIG 1, AND 51-40-08.

Part: LONGERON — CORRODED (BS 1022-1037) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON LONGERON 30 BETWEEN BS 1022 - 1037. THE LONGERON SECTION WAS REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 43,285 hrs · 30,350 cycles

BROKEN CHANNEL ON GEN FLOOR PANELS #221GF, 222AJF, AND 222EF. NRC 00536: GEN FLOOR PANELS #221GF, 222AJF, AND 222EF WERE REPAIRED PER B717 SRM 53-20-50-2R REPAIR 5 FIG. 202. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON GEN FLOOR PANELS #222AJF AND 222EF AFTER STOP DRILL AND NO CRACKS WERE FOUND PER DC-MD/BOEING NDT SPM 06-10-01.001 EQUIPMENT: NORTEC 500S C/N: 1881 EXP. DATE: 28JUL18. (LP #0468954)

Part: SKIN SPLICE — CORRODED (BS 898) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON SKIN SPLICE BS 898, BETWEEN LONGERONS 26L TO 30L. THE SKIN SPLICE WAS REPLACED IAW SRM 53-20-01-0I-3, FIG 1. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND OUT LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE PAR 4, FIG 103.

Part: FLOORBEAM — CRACKED (BS 645) · airframe 43,285 hrs · 30,350 cycles

CRACKED FLOORBEAM BS 645. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 5971111, REV F.

Part: STRAP — CORRODED (BS 1002-1022) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON STRAP AT LONGERON 25L BETWEEN BS 1002 TO 1022. THE STRAP WAS REPLACED IAW SRM 51-41-05, AND DWG 5936021, REV EG.

Part: LONGERON SPLICE — CORRODED (BS 973-994) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON LONGERON SPLICE 27L BETWEEN BS 973 TO 994 IN THE AFT CARGO BAY. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.

Part: LONGERON SPLICE — CORRODED (BS 927-946) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE LONGERON 30 SPLICE BETWEEN BS 927 TO 946. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.

Part: PAN — CRACKED (CARGO BAY) · airframe 43,285 hrs · 30,350 cycles

CRACK FOUND ON THE FWD EDGE OUTER PAN BELOW THE NR 2 STOP FITTING AT THE FWD CARGO DOOR. REPAIRED IAW ETI-17-18-055, REV 1, AND ER/A 566780-14, REV ORIG.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME ANGLE, FWD FACE BS 1022, BETWEEN LONGERONS 7L - 8L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05 AND DWG 9912243, REV JS. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01.001.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON MEMBRANE STA Y=200 X=-54 5300-2010. CORROSION LEVEL 2, MEMBRANE WAS REPAIRED PER SRM 51-70-10-2R. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=200 X=-54, NO CRACKS WERE FOUND AFTER CUT OUT PER NDTSPM 06-10-01.001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 REF AMDS 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 WERE REPLACED PER SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 REF 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 WERE REPLACED PER SRM 51-41-02.

Part: CUSP WEB — CORRODED (BS 902-904) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE CUSP WEB, BS 902 TO 904, LBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.

Part: SEAT TRACK — CORRODED (BS 240-247) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE SEAT TRACK LBL 54, BETWEEN BS 240 TO 247. THE SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R-5.

Part: CUSP WEB — CRACKED (BS 647) · airframe 43,285 hrs · 30,350 cycles

CRACK ON THE RT CUSP WEB, BS 674, RBL 46: THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R-2. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS FOUND IAW NDT SPM PART 6, 06-10-01.001,

Part: NONE — NONE · airframe 43,285 hrs · 30,350 cycles

EXCESSIVE CORROSION ON FUEL ACCSESS PLATE #620CT, 520CT, AND 520DT AT SETTLEMENT AND COUNTERSINK AREA RH/LH WING IN REFERENCE NRCS 00549, 00553, AND 00554. NRC 00603: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR IS NOT PERMITTED PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III; ALSO DUE TO EXCESSIVE CORROSION ON COUNTERSINK AREAS, FUEL ACCESS PLATE #520DT WAS REPLACED PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II (A AND B). (LP #0461796)

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORRODED FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED, AND REPLACED IAW DWG 9957828, REV AB.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 43,285 hrs · 30,350 cycles

CRACKED ANGLE AT THE RT FWD EMERGENCY EXIT DOOR UPPER BEAM FWD EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957735, REV G.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,285 hrs · 30,350 cycles

CRACKED DOOR FRAME AT THE NLG LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 43,285 hrs · 30,350 cycles

CRACKS ON FLOOR PANELS #221EF, 211ANF, AND 223GF AT PAX CAB (CPAX). NRC 00556: FLOOR PANELS #221EF, 211ANF, AND 223GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50. FLOOR PANELS WERE INTALLED WITH JIC CARD 2040-0024. (LP #0460121)

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,285 hrs · 30,350 cycles

CRACKED NLG DOOR FRAME, RT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.

Part: FLOOR SUPPORT — CORRODED (BS 120-148) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE FLOOR SUPPORT BETWEEN BS 120 TO 148, RBL 50 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 43,285 hrs · 30,350 cycles

CRACKED ANGLE AT THE FWD CARGO DOOR BETWEEN THE UPPER EDGE AND BEAM 1 AND NEXT TO AFT HINGE. THE ANGLE WAS REPLACED SRM 51-41-02, 51-41-05, AND DWG 9957664, REV N.

Part: WEB — CRACKED (BS 208) · airframe 43,285 hrs · 30,350 cycles

CRACKED WEB BS 208, LONGERON 15L. THE WEB WAS REPAIRED IAW SRM 53-10-15-2R, PR 4. HFEC INSPECTION PERFORMED AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM 06-10-01.001.

Part: CUSP WEB — CRACKED (BS 219) · airframe 43,285 hrs · 30,350 cycles

CRACKED CUSP WEB BS 219, LBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R. HFEC INSPECTION WAS PERFORMED AT THE TRIMMED OUT AREA. NO CRACKS WERE FOUND IAW NDT SPM PART 6 06-10-01.001.

Part: CUSP WEB — CORRODED (BS 389) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON THE RT CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R -2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ON TRIMMED OUT AREA IAW NDT SPM 06-10-01.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION OUT OF LIMITS ON ACCESS PANEL 620AT. THE ACCES PANEL WAS REPLACED IAW SRM 57-10-01-2R-2, PAR 5.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME ANGLE, FWD FACE BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, AND SRM 51-20-09.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 43,285 hrs · 30,350 cycles

CRACKED ANGLE AT THE RT AFT EMERGENCY EXIT DOOR UPPER BEAM AFT EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON RUBSTRIPS OF THE FUEL ACCESS PANELS 520GB AND 520MB ON THE LT WING THE RUBSTRIPS WERE REPLACED IAW SRM 57-10-01-2R, REP 3, PAR 6.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME ANGLE AFT FACE, BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DRAWING 9912243, REV JS.

Part: SKIN — PUNCTURED (LT MLG DOOR) · airframe 43,285 hrs · 30,350 cycles

PUNCTURE ON AFT EDGE INTERNAL SKIN OF LT MLG DOOR. THE DOOR SKIN WAS REPAIRED IAW SRM 52-82-02-2R-1, FIG 201, SHEET 5.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,285 hrs · 30,350 cycles

CRACKED LONGERON 8L AT BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REP 2.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 43,285 hrs · 30,350 cycles

CORROSION OUT OF LIMITS ON COUNTERSINK FUEL ACCESS PLATE #620CB, 620AT, AND 620DT AT RH WING IN REFERENCE NRC 00548. NRC 00600: COROSION LEVEL II, ACCESS PLATE #620CB AND 620DT WERE REWORKED PER B717 SRM 57-10-01-2R-2-PAR. 5 CONDITION II AND ACCESS PLATE #620AT WAS REPLACED ON NRC 00650. (LP #0457446)

Part: FRAME — CRACKED (BS 675) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.

Part: FRAME — CRACKED (BS 675) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.

Part: FRAME — CRACKED (BS 660) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 43,285 hrs · 30,350 cycles

CRACKED ANGLE AT UPPER BEAM AFT EDGE OF THE FWD LT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, & DWG 9957735, REV G.

Part: FRAME — CRACKED (BS 660) · airframe 43,285 hrs · 30,350 cycles

CRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.

Part: PAN — CRACKED (BS 522) · airframe 43,285 hrs · 30,350 cycles

CRACK ON THE RT RING PAN BS 522 LOWER AFT CORNER. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 889) · airframe 43,285 hrs · 30,350 cycles

CRACKED RT RING PAN BS 889, UPPER FWD CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 617) · airframe 43,285 hrs · 30,350 cycles

CRACKED LT RING PAN BS 617, LOWER FWD CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 870) · airframe 43,285 hrs · 30,350 cycles

CRACKED LT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 870) · airframe 43,285 hrs · 30,350 cycles

CRACKED RT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 636) · airframe 43,285 hrs · 30,350 cycles

CRACKED RT RING PAN BS 636 LOWER, FWD CORNER: THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: PAN — CRACKED (BS 636) · airframe 43,285 hrs · 30,350 cycles

CRACKED LT RING PAN BS 636 UPPER AND LOWER FWD CORNER. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,285 hrs · 30,350 cycles

CRACK ON CUSP WEB FROM STA Y=655 TO Y=674 BTW X-54 TO X-60 RT SIDE AT PAX CABIN. CUSP WEB WAS REPAIR ON FROM STA Y=655 TO Y=674 BTW X-54 TO X-60 RT SIDE AT PAX CABIN REPAIR PER SRM 53-00-55 REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,285 hrs · 30,350 cycles

CORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-44 TO X=-9 5300-2010 (W1). CORROSION LEVEL 2, FLOOR SUPPORT STA Y=180 BTW X=-44 TO X=-9 WAS REPLACED PER SRM 51-41-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,210 hrs · 30,293 cycles

DURING CHECK, FOUND THE AFT OVERWING INTERNAL UPPER EMERGENCY EXIT LIGHTS INOPERATIVE FOR BOTH SIDES. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.

Part: BEAM — CRACKED (L1 DOOR) · airframe 39,824 hrs · 27,938 cycles

CRACKED NR 1 BEAM AT THE L1 DOOR INTERNAL STRUCTURE AFT EDGE. THE BEAM WAS REPAIRED IAW SRM 52-10-02 FIG. 201.

Part: SKIN — DENTED (BS 200-218) · airframe 39,824 hrs · 27,938 cycles

DENT ON FUSELAGE SKIN BS 200 - 218 LONGERONS 17-18R. FOUND TO BE WITHIN LIMITS IAW SRM 53-01-01 PAR 4 B. DETAILED 10X MAGNIFIED VISUAL INSPECTION WAS PERFORMED AND ADDITIONAL DAMAGE WAS NOT FOUND IAW SRM 53-01-01 PAR. 4 (1). HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01, SRM 53-01-01 PAR 4. .

Part: SPOILER — DENTED (RT WING)

DURING NON-ROUTINE CHECK, UNSCHEDULED INSPECTION, RT OTBD SPOILER FOUND DENTED.

Part: SKIN — DELAMINATED (LT WING SPOILER)

DURING ROUTINE MAINTENANCE LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 38,372 hrs · 26,825 cycles

VERTICAL STABILIZER L/E HAS MANY WORN FASTENER HOLES ALONG UPPER EDGE AND MANY OTHERS ON AFT EDGE UPPER END SHOW SIGNS OF LOOSENESS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0220:0593-2005/011 00068, REPAIRED ON PRI 544861-14, REV 0 AND C/W SECTION I OF ER/A 544861-14, REV ORIGINAL.

Part: SHEAR TIE — CORRODED (BS 927) · airframe 38,372 hrs · 26,825 cycles

SHEAR TIE CORRODED AT BS 927 BETWEEN L30 AND L29L. REPAIRED IAW ER/A 545187-14, REV ORIGINAL.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 38,372 hrs · 26,825 cycles

LT SIDE VERTICAL STABILIZER INNER SKATE ANGLE ATTACH ANGLE CRACKED. REPLACED ANGLE REF DWG NR 5912188 AND SRM 51-40-02.

Part: SKIN — CRACKED (BS 1311) · airframe 38,455 hrs · 26,892 cycles

CRACKED SKIN BS 1311 BETWEEN S2L AND S3L. FOLLOW ON ACTION IS REQUIRED. THIS IS A MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,823 hrs · 26,408 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT THE AFT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: SKIN — DENTED (BS 229) · airframe 37,703 hrs · 26,309 cycles

FUSELAGE DENT AT BS 229 BETWEEN STR 17L AND 18L CAUSED BY JETWAY IMPACT. REPAIRED DAMAGE IAW SRM 53-10-01, REPAIR 10, PAGE 206.

Part: GENERATOR — FAILED (RIGHT) · airframe 36,982 hrs · 25,828 cycles

ABOUT A 30 MINUTES PRIOR TO LANDING, THE CREW REPORTED THE LOSS OF THE RT GENERATOR. THE RT GENERATOR WAS SUCESSFULLY RESET, BUT SHORTLY THEREAFTER, BOTH GENERATORS FAILED AND RESETS WERE NOT SUCCESSFUL. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY USING EMERGENCY POWER. MAINTENANCE REPLACED THE EPCU FOR A HARD FAULT INDICATION AND REPLACED THE RT PCDU AND BOTH RT PCDU MOUNTED RELAYS. OPS CHECKS WERE PERFORMED AND WERE SUCCESSFUL. THE AC HAD A SUCCESSFUL VERIFICATION FLIGHT AND HAS BEEN RELEASED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 36,248 hrs · 25,231 cycles

DURING LINE CHECK , MAINTENANCE NOTED EMERGENCY EXIT SIGN WIRE SPLICES BROKEN AT ROW 19AB. REPLACED BROKEN WIRE CONNECTORS IAW WDM 33-51 AND CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,696 hrs · 24,777 cycles

AFT OVERHEAD EMERGENCY EXIT SIGN AND CATWALK LIGHTS INOPERATIVE. REPLACED AND TESTED AFT EMERGENCY LIGHT POWER SUPPLY AND BATTERY. CHECKED GOOD.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 35,226 hrs · 24,374 cycles

PERFORMED AN AIR RETURN, DUE TO RT ENGINE SHUTDOWN. CREW PERFORMED INFLIGHT RESTART AND ENGINE EXCEEDED EGT LIMIT. THE ACFT LANDED SAFELY. REPLACED RT, NR 2 ENGINE DUE TO EGT LIMITS EXCEEDED.

Part: WIRE — LOOSE (AC BAY) · airframe 33,821 hrs · 23,137 cycles

TAIL COMPARTMENT EMERGENCY EXIT LIGHT WIRES LOOSE. SECURED WIRES IAW SWPM.

Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 33,821 hrs · 23,137 cycles

FORWARD EMERGENCY EXIT LIGHT SWITCH LOOSE. SECURED SWITCH IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,149 hrs · 22,700 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN LAVATORY & G2 CLOSET. RELAMPED EMERGENCY LIGHT IAW MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,149 hrs · 22,700 cycles

R1 DOOR CUTOUT AFT GIRT BAR MOUNT FITTING CORRODED AT BS 200, RBL 53. R &R FITTING IAW SRM.

Part: SIGN — DAMAGED (CABIN) · airframe 33,149 hrs · 22,700 cycles

MID CEILING EMERGENCY EXIT SIGN DAMAGED. R & R SIGN IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,149 hrs · 22,700 cycles

EMPENNAGE CANTED FRAME 1225 WEB CRACKED AT LOCKPIN AT 3 O'CLOCK POSITION. REPAIRED WEB IAW EA.

Part: LENS — FADED (CABIN) · airframe 33,149 hrs · 22,700 cycles

FWD CABIN CEILING EMERGENCY LIGHT LENS COVER FADED. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 33,149 hrs · 22,700 cycles

FORWARD CABIN CEILING EMERGENCY EXIT SIGN LENS COVER CRACKED. R & R COVER IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 33,149 hrs · 22,700 cycles

MID CEILING EMERGENCY EXIT SIGN CRACKED. R & R SIGN IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 33,149 hrs · 22,700 cycles

L1 DOOR EXIT LIGHT LENS COVER CRACKED. R & R LIGHT LENS IAW MM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 32,949 hrs · 22,563 cycles

RT WING FIXED FLAP FAIRING CRACKED. R & R LUVER IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 32,917 hrs · 22,540 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 31,480 hrs · 21,631 cycles

EMERGENCY FLOOR LIGHTS BROKEN BETWEEN ROW 10 AND ROW 31. REMOVED AND REPLACED COVERS PER AMM.

Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 30,464 hrs · 20,987 cycles

COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT STA 160R IAW B717 AMM 33-51-03. OPS TEST GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

STRINGER CORRODED BETWEEN BS 898 TO BS 946. REPAIRED STRINGER IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

CUSP WEB CRACKED BETWEEEN BS 665 TO BS 674, LBL 57. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

SKIN DOUBLER CORRODED AT BS 813, LT & RT SIDE OF FUSELAGE BENEATH EXTERNAL STRINGERS. REPAIRED SKIN IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FLOORBEAM SUPPORT FITTING CRACKED AT BS 737, RBL 44. REMOVED AND REPLACED FITTING IAW SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

LEFT KEEL BEAM FAIRING ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FRAME CORRODED AT BS 974, BETWEEN STR 29R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

LEFT FRAME ATTACH ANGLE CRACKED AT BS 1178. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FLOORBEAM SUPPORT FITTING CRACKED AT BS 757, LBL 44. REPAIRED FLOORBEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FRAME ANGLE CRACKED AT BS 1200, STR 4R. REMOVED AND REPLACED ANGLE IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

LEFT CUSP WEB CORRODED AT BS 549, LBL 57. REPAIRED CUSP WEB IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

STRINGER CRACKED AT BS 1133, STR 2L. REPAIRED STRINGER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

RIGHT CUSP WEB CORRODED AT BS 471, RBL 57. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

LEFT CUSP WEB CORRODED AT BS 527, LBL 57. REPAIRED CUSP WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FRAME CORRODED AT BS 946, STR 9L. REPAIRED FRAME IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

AFT CARGO DOOR JAMB LOWER SECTION CORRODED BETWEEN BS 954 TO BS 988. REPAIRED PAN SECTION IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 29,452 hrs · 20,305 cycles

FORWARD CARGO DOOR LOWER CUTOUT CORRODED BETWEEN BS 370 TO BS 427. REPAIRED JAMB PAN AND ANGLES IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,257 hrs · 20,845 cycles

FUSELAGE SKIN CRACKED AT BS 238, STR 17L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,809 hrs · 19,669 cycles

RT EEPLS INOP BETWEEN ROW 10 TO ROW 23. RELAMPED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN)

THE 10D ESCAPE PATH LIGHTING HAS COVER REMOVED AND LIGHT DAMAGE. RELAMPED AND INSTALLED COVER OPS CHECK GOOD. REF AMM 33-51.

Part: COFFEEMAKER — DEFECTIVE (GALLEY)

SMOKE/VAPOR NOTED NEAR CEILING AND AUDIBLE POP WATER LEAKING FROM COFFEEMAKERS. REMOVED AND REPLACED NR 102 COFFEEMAKER IAW B717 MM 25-33-0. NO LEAKS NOTED AT THIS TIME. OPS CHECK GOOD.

Part: LENS — MISSING (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT ASSY ON AISLE SIDE OF SEAT 3D IS MISSING A LENSE COVER. INSTALLED ONE ESCAPE LIGHT COVER REF 25-60.

Part: LANYARD — MISINSTALLED (EVAC SLIDE)

L1 DOOR SLIDE LANYARD CLIP INSTALLED INCORRECTLY, AWI. REMOVED AND RE-INSTALLED L1 DOOR SLIDE LANYARD IN THE PROPER POSITION IAW AMM 25-61 AWI.

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 160, BL 0, 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: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 238, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL40, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

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: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LANYARD — FRAYED (EVAC SLIDE)

R1 DOOR SLIDE LANYARD FRAYED. REPLACED SLIDE LANYARD ON R1 DOOR SLIDE IAW MM 25-61.

Part: COVER — MISSING (CABIN)

ROW 10 FED EPL CLEAR COVER MISSING. REPLACED COVER. CHECKED OK IAW AMM 33-51.

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: DOOR FRAME — DAMAGED (FUSELAGE)

INSTALLED AFT CARGO COMPARTMENT DOOR JAMB LOWER SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIGURE 201. SEE NR 3391, 3451 AND 5655.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS)

SEAT EXIT IDENTIFIERS INOP SEAT ROWS 11-19. RESET BATTERY PACK ON B5-118. OPS CHECK GOOD IAW B717 AMM 33-51.

Part: VENT — CRACKED (FUSELAGE)

AFT FUSELAGE RIGHT HAND VENT BOX CRACKED. INSTALLED DOUBLER REPAIR ON RIGHT HAND VENT BOX PER EO 17-5320-2023.