N995AT

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,906 hrs · 42,438 cycles

CRACK ON CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX. SUMMARY OF NRC 00467: CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 221 AND 51-41-02-0G. (LP #0736473)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,906 hrs · 42,438 cycles

CORROSION ON FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR. SUMMARY OF NRC 00459: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR WERE REPLACED DUE TO CORROSION OUT OF LIMITS PER B717-200 SRM 51-41-01-0G, 51-41-05-0G, AND DWG 5940155 REV J. (LP #0736586)

Part: PAN — CRACKED (ZONE 100) · airframe 58,906 hrs · 42,438 cycles

CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 WAS FOUND AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00405: CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0734792)

Part: PAN — CRACKED (ZONE 100) · airframe 58,906 hrs · 42,438 cycles

CRACK ON PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5. SUMMARY OF NRC-00143: PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0730599)

Part: VANE — DENTED (ZONE 500 FLAP) · airframe 58,906 hrs · 42,438 cycles

SEVERAL DENTS ON LOWER SKIN LH AFT MOVEABLE FLAP VANE. SUMMARY OF NRC 00250: DENTS (8 EA) ON LOWER SKIN LH AFT MOVABLE FLAP VANE WERE EVALUATED AND DENTS #1 TO #7 ARE OUT OF LIMITS PER B717-200 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. A. AND WERE REPAIRED PER B717-200 SRM 51-40-02-0G PROCEDURE GENERAL; 51-41-02-0G PROCEDURE GENERAL; 57-53-01-2R PROCEDURE 1 REPAIR 1; AND 51-70-02-0G PROCEDURE GENERAL. DENT #8, XF=102.500", DAE=5.250", W=0.500", Y=0.015", W/Y=33 IS WITHIN LIMITS PER B717-200 SRM 57-53-01-1A PROCEDURE 1 ALLOABLE DAMAGE 1 PAR 3. A. PERFORM A DETAILED VISUAL INSPECTION AND TAP TEST FOR POSSIBLE DISBOND AT EVERY C-CHECK OR 3,000 CYCLES PER B717 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 2 (B). (LP #0732310)

Part: BEAM — CRACKED (ZONE 800) · airframe 58,906 hrs · 42,438 cycles

CRACK ON BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00255: BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0726863)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,906 hrs · 42,438 cycles

CORROSION ON LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX. SUMMARY OF NRC 00482: CORROSION LEVEL 2. CORROSION AT LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0726955)

Part: COVER — BROKEN (TAILCONE RELEASE) · airframe 58,906 hrs · 42,438 cycles

BROKEN PLASTIC COVER OF TAIL CONE EXTENSION PULL LEVER AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC: 00326 PLASTIC COVER OF TAIL CONE EXTENSION PULL LEVER AFT ACCESORIES COMPARTMENT WAS REPLACED PER B717-200 AMM 20-50-01. (LP #6556652)

Part: PAN — CRACKED (ZONE 100) · airframe 58,906 hrs · 42,438 cycles

CRACK ON INNER PAN AT FWD EDGE BTW BEAM 1 AND 2 WAS FOUND ON AFT CARGO DOOR. SUMMARY OF NRC 00442: OUTER PAN FWD EDGE BTW BEAM 1 AND 2 WAS BLENDED OUT AND MEASURED AS FOLLOW: MINIOR DAMAGED TO SKIN EDGE NO MORE THAN 0.380" DEEP: BLEND OUT IS 0.125". REWORK AREA NO LONGER THAN 1.250": REWORK IS 1.000". THEREFORE, IS WITHIN LIMITS PER B717-200 SRM 51-70-01-2R REPAIR 2. INNER PAN AT FWD EDGE BTW BEAM 1 AND 2 AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0719118)

Part: STRINGER — CORRODED (BS 1053 S26) · corrosion level 2 · airframe 57,819 hrs · 41,432 cycles

CORROSION AT APPROX STATION 1053 ON STRINGER 26. RIVETS POPPED WITH SKIN PROTRUDING. REMOVED STR END FITTING AT STR 26 STA 1053 FOUND TO BE 100% LOSS. OUT OF LIMITS. INSPECTED AREA AFTER END FITTING REMOVAL, NO ADDITIONAL CORROSION FOUND. LOCATED, DRILLED, ALODINED, AND PRIMED NEW STR END FITTING PER B717 SRM 51-40-02 AND 51-22-01. PAINTED IAW B717 SRM 51-22-01. INSTALLED THE NEW STR END FITTING IAW B717 SRM 51-40-02 AND BAC DRAWING 5919707. (LP #0379453)

Part: BEARING — FAULTED (L1 DOOR) · airframe 57,570 hrs · 41,220 cycles

THE GATE AGENT REPORTS THAT THE 1L DOOR WAS HARD TO OPEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED 1L DOOR LINER, FOUND ROLLER BEARING NOT FALLING INTO DOOR HANDLE DETENT. MAINTENANCE ADJUSTED FWD ENTRY DOOR MECHANISM IAW B717 AMM 52-11-01. OPERATIONAL & LEAK CHECKS WERE GOOD. THE DOOR LINER WAS INSTALLED, THE SLIDE WAS REINSTALLED PER AMDS 2561-9004. RII OF SLIDE INSTALLATION WAS ACCOMPLISHED PER QC5219. JOB COMPLETE. DOOR OK FOR SERVICE. (LP #5442186)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,195 hrs · 40,887 cycles

THE TAIL CONE AREA EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY ASSEMBLY B5-260 BAD. BATTERY ASSEMBLY B5-260 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #5412733)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,108 hrs · 40,025 cycles

EXIT SIGN (RIGHT) AT ROW 19 KNOCKED DOWN. MAINTENANCE FOUND THE EMERGENCY SIGN COVERS KNOCKED OFF, RESECURED THEM AS REQUIRED. THE AIRCRAFT IS OK FOR SERVICE. (LP #4391072)

Part: NOT REPORTED — NOT REPORTED · airframe 52,871 hrs · 37,119 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING ABOVE SEAT 01B IN THE CABIN. MAINTENANCE RE-SECURED THE EMERGENCY "EXIT" LENS AT 01B AS REQUIRED. THE AIRCRAFT IS OK FOR SERVICE. (LP #2161790)

Part: NONE — NONE · airframe 51,937 hrs · 36,312 cycles

VAULT DOOR TAILCONE RELEASE PUSH-PULL CABLE TEFLON SHEATHING TORN AT RELEASE BLOCK STA 1212 AND AT THE 8 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE DEPLOYMENT RELEASE CABLE ASSEMBLY REF B717 AMM 53-52-01. THE AIRCRAFT IS OK FOR SERVICE. (LP #1994846)

Part: NONE — NONE · airframe 51,930 hrs · 36,308 cycles

RIGHT HAND SIDE PASSENGER WINDOW #30 IS FADED. SUMMARY SEE NRC 001-0308:5620-2001/004 00008: REPLACED WINDOW PER B717 AMM 56-20-01. (LP #1994391)

Part: NONE — NONE · airframe 51,930 hrs · 36,308 cycles

RIGHT SIDE AFT COCKPIT WINDOW HAS HEAVY SCRATCHES ON EXTERIOR. SUMMARY SEE NRC 001-0305:5610-2001/002 00062: REPLACED RT SIDE AFT COCKPIT WINDOW PER B717 AMM 56-13-01. (LP #1994394)

Part: NONE — NONE · corrosion level 2 · airframe 51,930 hrs · 36,308 cycles

FWD CARGO DOOR JAMB AREA HAS AREAS OF CHIPPED PAINT, LIGHT CORROSION, AND NO GRAY PAINT AS PER SRM 53-00-15 REPAIR 1 FROM HALFWAY UP JAMB FWD AND AFT SIDES AND LOWER JAMB AREA. SUMMARY SEE NRC 065-0009:5300-2007/001 00348: REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 6. (LP #1994673)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,985 hrs · 35,456 cycles

THE MAIN CABIN MAIN DOOR TOP EMR LIGHT OUT. R & R THE BATTERY PACK B5-123 PER AMM 33-51. OPS CHECK GOOD.

Part: LAMP — WRONG PART (EMERGENCY LIGHT) · airframe 49,994 hrs · 34,668 cycles

BOTH AFT OVERWING EXIT SIGNS ARE INOPERATIVE. MAINTENANCE FOUND THE WRONG LAMPS INSTALLED. COMPLETED RE-LAMP AND OPERATIONAL CHECK WAS GOOD, PER B717 AMM 33-51. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,308 hrs · 32,483 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. EXIT LIGHTS FLASHING. T/S AS PER FIM 33-50; ALLOW SUFFICIENT TIME FOR BATTERY PACKS TO RE-CHARGE OPS CHECK NORMAL OK FOR SERVICE. (LP1157653)

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 44,393 hrs · 30,462 cycles

THE CREW ABORTED THE TAKE-OFF AT 120 KNOTS AFTER THE "STAB TRIM" AURAL WARNING SOUNDED. THE STAB TRIM WAS SET WITHIN THE GREEN BOX AT 4.4 PRIOR TO THE TAKE-OFF ROLL. THE AIRCRAFT TAXIED BACK TO THE GATE. CORRECTIVE ACTION: MAINTENANCE HAS REPLACED THE FCC PER AMM 22-01. ALSO INSTALLED VIA 1 PER AMM 31-34.

Part: SKIN — CRACKED (RT BUTE DOOR) · airframe 43,261 hrs · 29,662 cycles

CRACK ON INBOARD RT WING BUTE DOOR. INNER SKIN WAS REPLACED PER DWG 5919571 REV BG AND SRM 51-41-02.

Part: SKIN — DAMAGED (TE FLAP) · airframe 43,261 hrs · 29,662 cycles

ELONGATED SCREW HOLES AT LOWER SKIN. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-41-01, AND DWG 5919571, REV BG.

Part: CUSP WEB — CRACKED (BS 650-655) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE RT CUSP WEB BETWEEN BS 650 - 655, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW ER/A 562407-14, REV ORIGINAL AND ETI 17-17-243, REV 2.

Part: DOUBLER — CORRODED (BS 965-979) · airframe 43,261 hrs · 29,662 cycles

CORROSION ON THE AFT CARGO BAY PRODUCTION DOUBLER IN THE JAMB AREA BETWEEN BS 965 - 979, LONGERONS 27 - 28R.

Part: CARGO TRACK — CORRODED (BS 813-1022) · airframe 43,261 hrs · 29,662 cycles

CORROSION ON CARGO TRACK BS 813 TO 1022 LT SIDE IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.

Part: CARGO TRACK — CORRODED (BS 994-1022) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON THE CARGO TRACK BS 994 TO 1022, IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,261 hrs · 29,662 cycles

CRACK ON VERTICAL STABILIZER SKIN. THE SKIN WAS REPLACED IAW SRM 51-41-02 0G, 51-40-05 0G, AND DWG 5936143, REV AS.

Part: CARGO TRACK — CORRODED (BS 892-954) · airframe 43,261 hrs · 29,662 cycles

CORROSION ON THE CARGO TRACK BS 892 TO 954 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 , 51-41-05, AND 51-41-02.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 43,261 hrs · 29,662 cycles

CRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.

Part: DOOR FRAME — CORRODED (BS 954-994) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON DOOR FRAME BS 954 TO 994 IN THE AFT CARGO BAY. THE DOOR FRAME WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-05.

Part: SKIN — WORN (RT WING SLAT) · airframe 43,261 hrs · 29,662 cycles

WEAR ON INTERNAL FACE OF SLAT SKIN SS 119, RT WING NR 1 SLAT. REPAIRED IAW ETI-17-17-240, REVISION 2, AND ER/A 562401-14, REVISION ORIGINAL.

Part: FITTING — CRACKED (BS 661) · airframe 43,261 hrs · 29,662 cycles

CRACK ON FITTING, LONGERON 22R, BS 661. REPAIRED IAW ETI-17-17-236, REV 2, AND ER/A 562397-14, REV ORIGINAL.

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON BARREL NUTS WAS FOUND. THE BARREL NUT HOLES WERE REPAIRED IAW ETI-17-17-231, REV 5, AND ER/A 562391-14, REV ORIG. BOLTS AND NUTS WERE REPLACED IAW AMM 20-20-22.

Part: TORQUE TUBE — CORRODED (RUDDER) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION WAS FOUND ON THE RUDDER TORQUE TUBE ASSY. THE RUDDER TORQUE TUBE WAS REPAIRED IAW ER/A 562416-14, REV ORIGINAL.

Part: GUSSET — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED GUSSET AT LONGERON 7R AT BULKHEAD BS 1022. THE GUSSET WAS REPAIRED IAW ER/A 562380-14, REV ORIGINAL, AND ETI-17-17-226, REV ORIGINAL.

Part: SKIN — CORRODED (BS 737-756) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON UPPER SURFACE OF THE SKIN BETWEEN BS 737 & 756, RBL 44 - 60. CORROSION OUT OF LIMITS AND WAS REPAIRED IAW ER/A 562387-14 REV. ORIGINAL. AND ETI-17-17-228 REV 1.

Part: FRAME ANGLE — CRACKED (BS 408) · airframe 43,261 hrs · 29,662 cycles

CRACKED FRAME ANGLE BS 408 AT FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-01-0G AND 51-41-05-0G.

Part: FRAME — CRACKED (BS 674) · airframe 43,261 hrs · 29,662 cycles

CRACK ON RT OVERWING FRAME AT BS 674, BETWEEN LONGERONS 9R TO 19R. THE FRAME WAS REPLACED IAW DWG SR95530013, REV A, & SRM 51-41-05.

Part: CUSP WEB — CRACKED (BS 725) · airframe 43,261 hrs · 29,662 cycles

SEVERAL CRACKS IN THE RT CUSP WEB BS 725. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG.215.

Part: CUSP WEB — CRACKED (BS 674-725) · airframe 43,261 hrs · 29,662 cycles

SEVERAL CRACKS IN THE RT CUSP WEB BS 674 - 725. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 226 AND FIG 223.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED LONGERON 4R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: CUSP WEB — CRACKED (BS 715-737) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE CUSP WEB BETWEEN BS 715 - 737, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED LONGERON 5R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: CUSP WEB — CRACKED (BS 807) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE LEFT CUSP WEB BS 807, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4 CONFIGURATION 7037.

Part: CUSP WEB — CRACKED (BS 657) · airframe 43,261 hrs · 29,662 cycles

CRACKED CUSP WEB BS 657, LBL 5. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 209.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: FRAME ANGLE — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED FRAME ANGLE BS 1022 BETWEEN LONGERONS 6R TO 7R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, SRM 51-41-05, AND DWG 9912243, REV. HF.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACK ON LONGERON 6L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: PAN — CRACKED (CARGO DOOR) · airframe 43,261 hrs · 29,662 cycles

CRACK ON LOWER EDGE INNER PAN, BELOW PRESSURE SEAL OF THE FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R, REPAIR 1, FIG 201.

Part: INTERCOSTAL — CRACKED (BS 380) · airframe 43,261 hrs · 29,662 cycles

CRACKED INTERCOSTAL UPPER EDGE BS 380 AT THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 43,261 hrs · 29,662 cycles

CRACKED ANGLE ON THE LOWER EDGE BS 408 AT FWD CARGO DOOR. THE CARGO DOOR TEE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 43,261 hrs · 29,662 cycles

CRACKED INTERCOSTAL AND ANGLE BETWEEN LOWER EDGE AND BEAM 1 BS 408 AT THE FWD CARGO DOOR. THE INTERCOSTAL AND ANGLE WERE REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 43,261 hrs · 29,662 cycles

CORROSION ON FLOOR PANEL 211AMF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, FIG 201, SHEET 2.

Part: FRAME — CRACKED (BS 1037) · airframe 43,261 hrs · 29,662 cycles

CRACKED FRAME BS BS 1037, LONGERON 17L. HFEC INSPECTION WAS ACCOMPLISHED ON THE FRAME. NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW SRM 53-20-07-2R, PROCEDURE 4, PARA. 5.A.(2), AND NDT SPM 06-10-01.001. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R.

Part: FRAME — CRACKED (BS 1037) · airframe 43,261 hrs · 29,662 cycles

CRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R. HFEC INSPECTION WAS ACCOMPLISHED ON THE FRAME, NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW SRM 53-20-07-2R, PROCEDURE 4, PARA. 5.A.(2). AND NDT SPM 06-10-01.001.

Part: ACCESS PANEL — CRACKED (WING) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE RT ACCESS PANEL 620KB. THE ACCESS PANEL WAS REPLACED IAW SRM 51-41-01, AND SERVICEABLE MAGNETIC DRIPLESS FUEL MEASURING HOUSING WAS INSTALLED ON THE NEW ACCESS PANEL IAW AMM 28-42-01.

Part: PAN — CRACKED (BS 889-908) · airframe 43,261 hrs · 29,662 cycles

CRACKED PAN UPPER FWD CORNER BS 908 - 889. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 202.

Part: PAN — CRACKED (BS 813-870) · airframe 43,261 hrs · 29,662 cycles

CRACKED LEFT PAN UPPER AFT CORNER BS 851 - 870 AND 813-832. REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 202.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,261 hrs · 29,662 cycles

CRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: SEAT TRACK — CORRODED (BS 110-140) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

EXCESSIVE CORROSION ON SEAT TRACK SUPPORT BS 110 TO 140, RBL 22. A NEW SEAT TRACK SUPPORT WAS INSTALLED IAW SRM 51-41-01.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON FLOORBEAM BS 200 BETWEEN RBL 8 TO LBL 8. THE CORROSION WAS REMOVED IAW SRM 51-10-04, PAR 26. ACCOMPLISHED NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE FIG 103. REMOVED AND REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.

Part: CUSP WEB — CRACKED (BS 413-419) · airframe 43,261 hrs · 29,662 cycles

CRACKED CUSP WEB BS 413 & 419, RBL 56. THE CRACKS WERE FOUND WHEN CORROSION WAS REMOVE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 207. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW NDT SPM 06-10-01-01.001.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

EXCESSIVE CORROSION ON THE FLOORBEAM BS 200, LBL 8 TO LBL 14. REMOVED AND REPLACED IAW SRM 51-41-02.

Part: FLOOR PANEL — BROKEN (COCKPIT) · airframe 43,261 hrs · 29,662 cycles

BROKEN FLIGHT DECK FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED, AND REPLACED IAW 2040-0024.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 43,261 hrs · 29,662 cycles

DISBOND OF 2.300" X 3.500" AT 9.00" FROM OUTBOARD EDGE AND 9.00" FROM AFT EDGE ON THE RT AFT MOVABLE FLAP VANE, REPAIRED IAW SRM 57-53-01-2R-1.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 43,261 hrs · 29,662 cycles

BROKEN FLOOR PANEL 221LF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R, REP 3.

Part: FLOOR SUPPORT — CORRODED (BS 140) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

EXCESSIVE CORROSION ON THE FLOOR SUPPORT BS 140, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05-0G AND 51-41-08-0G.

Part: FRAME — CRACKED (BS 851) · airframe 43,261 hrs · 29,662 cycles

CRACK FOUND ON THE BS 851 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.

Part: FRAME — CRACKED (BS 617) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE BS 617 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.

Part: FRAME — CRACKED (BS 756) · airframe 43,261 hrs · 29,662 cycles

CRACK ON THE BS 756 FRAME UPPER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.

Part: RUB STRIP — CORRODED (RT WING) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON THE RT WING ACCESS PANEL RUBSTRIP 620D. THE RUBSTRIP #620DT WAS REPLACED IAW SRM 57-10-01, REP 3.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,261 hrs · 29,662 cycles

CRACK ON NLG RT DOOR FRAME AT BS 46. CRACK ON NLG RH DOOR JAMB AT STA 46 APPROX WAS REPAIRED IAW SRM 53-10-14-2R. NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,261 hrs · 29,662 cycles

CRACK ON NLG LT DOOR FRAME AT BS 46. REPAIRED IAW SRM 53-10-14-2R. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.001.

Part: TAB — DELAMINATED (RUDDER TRIM) · airframe 43,261 hrs · 29,662 cycles

DELAMINATED RUDDER TRIM TAB. THE TRIM TAB WAS REPAIRED IAW SRM 51-70-02-2R, PROCEDURE 7, PARAGRAPH 4 B.

Part: RETAINER — CORRODED (R1 DOOR) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION ON THE R1 DOOR SEAL RETAINER. THE RETAINER WAS REPLACED IAW SRM 51-41-01 AND DWG 5910084, REV EP.

Part: RUB STRIP — CORRODED (RT WING) · corrosion level 2 · airframe 43,261 hrs · 29,662 cycles

CORROSION POINTS ON THE RIGHT WING FUEL ACCESS PANEL RUB STRIP 620CT. THE RUBSTRIP WAS REPLACED IAW SRM 57-10-01, REP 3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,055 hrs · 28,806 cycles

EMERG ESCAPE LIGHT INOP BY C1 DOOR. REPLACED BATTERY PACK B5-235 REF AMM 33-51. OPS CHECK GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 42,589 hrs · 29,217 cycles

DURING C CHECK, MAINTENANCE REPORTED DAMAGE TO THE UPPER EDGE OF THE LOWER FIXED LEADING EDGE PANEL COMMON TO THE ZFS=52 SPLICE STRAP. ON THE PANEL, ALL FASTENER LOCATIONS WERE BADLY OVERSIZED AND SKIN WASHERS HAD WORN INTO THE SURFACE ON THE LT UPPER AND LOWER ROW, AND MOST OF THE RT UPPER AND LOWER ROW. TRIMMED OFF ALL UPPER AND LOWER ROW HOLES, INSTALLED A NEW BONDED FINGER DOUBLER, FILLERS AND AN EXTERNAL DOUBLER.SECTION II. NSTALLED A DOUBLER ONTO THE UPPER REMOVABLE LE SKIN TO FACILITATE AN EXTERNAL SPLICE, AND INSTALLED A REPAIR BUSHING AT ONE HOLE ON THE UPPER REMOVEABLE LE SKIN.

Part: FITTING — NOT REPORTED (FUSELAGE) · corrosion level 2 · airframe 40,589 hrs · 27,723 cycles

GIRT BAR FITTING MOUNT. SEE NR FOR ADDITIONAL INFORMATION 027-0015:5310-2005/004 00112. REPLACED FITTINGS PER DWG 3936190.

Part: WEB — CORRODED · corrosion level 2 · airframe 38,596 hrs · 26,214 cycles

R1 DOOR LWR AFT CORNER AT FLOOR, WEB THAT GOES BEHIND GALLEY AGAINST FUSELAGE IS CORRODED AT FWD END. REPLACED PART IAW SRM 51-70-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,229 hrs · 25,921 cycles

EMERGENCY LIGHTS BATTERY PACK, BP-119, INOPERATIVE. REPLACED THE BATTERY PACK.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 36,534 hrs · 24,530 cycles

DURING SERVICE CHECK, NOTED RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE RT OVERWING EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51 AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,657 hrs · 23,839 cycles

DURING SERVICE CHECK, FOUND BOTH EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE OVERWING BATTERY WAS REPLACED AND OPS NORMAL.

Part: LANYARD — MISINSTALLED (TAILCONE SLIDE) · airframe 34,135 hrs · 22,448 cycles

TAILCONE SLIDE LANYARD HAS THE INCORRECT SHRINK TUBING INSTALLED. COMPLIED WITH ER/A 522284-14 AND INSTALLED CORRECT TUBING.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 34,002 hrs · 22,358 cycles

RT EMERGENCY EXIT LIGHT BATTERY PACK CONNECTOR P1-119 OUT OF POSITION AT ROW 23. R & R BATTERY PACK IAW SWFM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LONGERON CRACKED AT STATION 1133, LONGERON 2L. REPAIRED LONGERON IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

CUSP WEB CRACKED AT STATION 674, LBL 44.5. REPAIRED CUSP WEB IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

AFT CARGO COMPARTMENT LONGERON CORRODED BETWEEN STATION 927 TO STATION 954 +7, LONGERON 30. R & R LONGERON IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

AFT CARGO COMPARTMENT FRAME SPLICE STRAP CORRODED AT STATION 954, LONGERON 28L. R & R SPLICE IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

AFT CARGO COMPARTMENT FIBERGLASS FLOOR PANEL SUPPORT ANGLE CRACKED STATION 994, LONGERON 29L. R & R ANGLE IAW SRM & DRAWING.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

EE COMPARTMENT CABIN FLOOR CORRODED AT STATION 160, BETWEEN RBL 2 TO RBL 7. R & R PANEL IAW SRM.

Part: BULKHEAD — CORRODED (LT MLG WW) · airframe 34,002 hrs · 22,358 cycles

LT MLG FWD BULKHEAD WEB STRUCTURE CORRODED AT STATION 749, LBL 17 TO LBL 48. REPAIRED WEB STRUCTURE IAW SRM & SWA EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

FWD CARGO DOOR CUT OUT LOWER SECTION JAMB CORRODED BETWEEN STATION 370 TO STATION 427. R & R JAMB IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

SEAT TRACK CORRODED BETWEEN BS 1018 TO BS 1021 RBL 22. R & R SEAT TRACK IAW SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 34,002 hrs · 22,358 cycles

L1 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNTED GIRT BAR LATCH, AFT LATCH ASSEMBLY LOOSE. R & R FITTING IAW SRM & MM.

Part: BRACKET — CRACKED (AC BAY) · airframe 34,002 hrs · 22,358 cycles

TAIL COMPARTMENT INTERPHONE LIGHT SWITCH BRACKET UPPER & LOWER FLANGE CRACKED AT STATION 1053, LBL 18. R & R BRACKET IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

RT CUSP WEB CORRODED BETWEEN STATION 598 TO 617, STRINGER 18L. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LT CUSP WEB CORRODED BETWEEN STATION 598 TO STATION 617. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

RT SEAT TRACK CORRODED BETWEEN STATION 900 TO STATION 986, 45 IN OTBD OF CENTERLINE. REPAIRED TRACK IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

FUSELAGE INTERIOR STATION Y889 - 908 LT WINDOW PAN FWD LOWER ATTACH POINT CRACKED. REPAIRED PAN IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LT CUSP WEB CORRODED BETWEEN STATION 579 TO STATION 598, BETWEEN LBL 45 TO LBL 60. REPAIRED WEB IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 34,002 hrs · 22,358 cycles

LT WING INBD LE, BS Y636, BRACKET CONNECTED TO WING BODY FAIRING SUPPORT CRACKED. R & R SUPPORT IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

RT WING TO BODY FILLET FAIRING HORN ASSEMBLY SUPPORT WEB CORRODED. R & R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LT CUSP WEB CORRODED AT STATION 403. R & R PANELS IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LT CUSP WEB CORRODED AT STATION 489. REPAIRED CUSP WEB IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 34,002 hrs · 22,358 cycles

LT WING TOP SKIN STATION XFS 353 AFT OF FWD SPAR CORRODED. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

AFT UPPER FUSELAGE RT LOUVER VENT BOX ANGLE CLIP CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 34,002 hrs · 22,358 cycles

RT WING INBD LE INBD MOST FIXED LE RIB CLOSEST TO FUSELAGE STATION 636, SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,002 hrs · 22,358 cycles

LT VENT BOX UPPER AFT CORNER SHROUD ANGLE CRACKED AT STATION 1200. R & R PANEL IAW SRM & EA NO.

Part: LENS — MISSING (EXIT SIGN) · airframe 33,276 hrs · 21,920 cycles

MID CABIN EMERGENCY EXIT SIGN ALONG EXIT ROWS MISSING. INSTALLED LENS IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 33,157 hrs · 21,848 cycles

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

Part: SCREW — MISSING (EXIT SIGN) · airframe 32,115 hrs · 21,225 cycles

A/C LEFT ROW 21 EMERGENCY EXIT SIGN MISSING SCREWS. RE-SECURED SCREW AT ROW 21 REF AMM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 314,090 hrs · 20,785 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE LOOSE. SECURED LANYARD CLIP PER AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, LBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER 51-10-04, 53-00-00 AND 51-41-02.

Part: STRUCTURE — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER AREA, CORROSION. ACCOMPLISHED DOOR CUTOUT LOWER AREA SPLICE REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 53-20-15.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT SHEAR TIE, STA 908, LONG L30 TO L29L, CORROSION. ACCOMPLISHED SHEAR TIE REPLACEMENT PER B717 SRM 53-00-00 AND 53-00-06.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT SHEAR TIE, STA 927, LONG L30 TO L29L, CORROSION. ACCOMPLISHED SHEAR TIE REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 53-00-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN 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)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 7 TO LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CRACKED (FUSELAGE)

PASSENGER CABIN WEB, STA 208, LONG 15L, CRACKED. ACCOMPLISHED WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL 43, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 165, RBL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 REP 2, FIG 201.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 180, RBL 6, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10, 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-41-05.

Part: COWLING — CRACKED (RT ENGINE)

RIGHT ENGINE LOWER COWLING SECOND FROM FWD HINGE CUTOUT, CRACKED. OPEN DEFECT.

Part: COWLING — CRACKED (RT ENGINE)

RIGHT ENGINE UPPER COWLING SECOND FROM FWD HINGE CUTOUT, CRACKED. OPEN DEFECT.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L1 SLIDE COVER DAMAGED AND L1 SLIDE NEEDS REPLACEMENT. REMOVED AND REPLACED L1 SLIDE ASSEMBLY; REMOVED AND REPLACED SLIDE COVER IAW 25-61-03.

Part: LIGHT — MISSING (CABIN)

ROW 1DF EMERGENCY EPL LENS AND LIGHTS MISSING (2). INSTALLED LIGHT BULBS AND LENS COVERS (2). OPS CHECK OK IAW 717 33-52.

Part: FITTING — MISINSTALLED (EVAC SLIDE)

L1 DOOR SLIDE LANYARD CLIP NOT INSTALLED PROPERLY. REMOVED AND REPLACED L1 DOOR SLIDE AND INSTALLED LANYARD CLIP CORRECTLY PER 717 AMM 25-61.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-40-02 AND B717 SRM 51-41-01.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 908 TO 994, LONG L30, CORROSION. ACCOMPLISHED CARGO COMPARTMENT LONGERON SECTION BLENDING WITHIN LIMITS PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PASSENGER ENTRANCE AREA FLOOR SUPPORT BEAM, STA 256, LBL 12 TO RBL 23, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GALLEY AREA FLOOR SUPPORT BEAM, STA 218, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FRAME — DAMAGED (FUSELAGE)

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