N981AT

Part: SEALANT — NOT REPORTED · airframe 59,924 hrs · 42,798 cycles

WORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717 51-24-00 & DWG'S. C/W STEP 19 OF ERA 629612-14AD (1239562)

Part: SKIN — LEAKING (ZONE 600) · airframe 59,924 hrs · 42,798 cycles

WORKING PRI 629612-14, RH WING LOWER SKIN XRS 164 FUEL SEEP. C/W SECTION I LEAK EVALUATION OF ERA 629612-14AD (1231435)

Part: COVER — MISSING (ZONE 500) · airframe 59,894 hrs · 42,775 cycles

LEFT WING HAS ONE LOWER SLAT TRACK COVER MISSING. FWD TO CDL 57-47-03. PLAC. INSTALLED. (7709014)

Part: PIN — OUT OF POSITION (TAIL CONE) · airframe 58,199 hrs · 41,263 cycles

TAIL CONE EXIT RELEASE CAM PIN IS NOT 34.5 TO 38.5 DEGREES FROM THE CENTERLINE OF THE BASE AT 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 00899: RELEASE CAM PIN WAS INSTALLED CORRECTLY PER B717 AMM 53-52-03 AND AMDS 5352-2001 FIGURE 11. (LP #0751691)

Part: ROD END — DAMAGED (ZONE 600 SPOILER) · airframe 58,199 hrs · 41,263 cycles

DAMAGED DURING ADJUSTMENT OF RH INBD SPOILER PANEL. THE HOLDDOWN ACTUATOR ROD-END INADVERTENTLY EXTENDED CAUSING A PUNCTURE ON RH INBD GUIDE VANE. SUMMARY OF NRC 00886: THE RH INBD GUIDE VANE WAS REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND IN REFERENCE TO B717 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0749918)

Part: ANGLE — CRACKED (ZONE 100) · airframe 58,199 hrs · 41,263 cycles

UPPER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED WAS REMOVED. LOWER ANGLE COMMON TO REMOVED ANGLE WAS FOUND CRACKED. SUMMARY OF NRC 00820: LOWER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED WAS REPAIRED PER ER/A 623100-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623100-14 REV 4. ASSOCIATED ER/A 14-623100 ADDED FOR AC 9548. (LP #0748728)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE DOOR JAMB AT CPAX. SUMMARY OF NRC 00506: CORROSION LEVEL 2. CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE DOOR JAMB WAS REPAIRED PER ER/A 622312-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND 621922-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-621922 ADDED FOR AC 9548. (LP #0727220)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00609: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. (LP #0717763)

Part: RETAINER — CRACKED (WINDOW FRAME) · airframe 58,199 hrs · 41,263 cycles

CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00782: CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED PER ER/A 622289-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 622289-14 REV 6. MAINTENANCE REQUIREMENTS WERE VERIFIED AND NO FURTHER ACTION ARE REQUIRED ER/A 622289-14 REV ORIGINAL. ASSOCIATED ER/A 14-622289 ADDED FOR AC 9548. (LP #0713389)

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON LONGERON 29L UPPER/LOWER SURFACE BTW STA Y=900-946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LONGERON 29L BTW STA Y= 898 TO 964 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND PER B717-200 SRM 51-41-01-0G. (LP #0708287)

Part: PAN — GOUGED (ZONE 100) · airframe 58,199 hrs · 41,263 cycles

GOUGE ON INNER PAN AFT EDGE, 2 INCHES BELLOW BEAM #1 AFT EDGE, ON AFT CARGO DOOR (C2). SUMMARY OF NRC 00321: INNER PAN ON AFT LOWER CORNER CLOSE TO BEAM #1 AT AFT CARGO DOOR (C2) WAS REPAIRED PER ER/A 621854-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 621854-14 REV 3. ASSOCIATED ER/A 14-621854 ADDED FOR AC 9548. (LP #0708609)

Part: SKIN — DENTED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

DAMAGE T: ELONGATE HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R. SUMMARY OF NRC 00627: ELONGATED HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R WERE REPAIRED PER PRI 622118-14 REV 3 AND ER/A 622118-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 8,000 FLIGHT CYCLES AFTER SECTION I (02DEC24) PER ER/A 622118-14 REV ORIG SEC II. FOLLOW UP UNDER LOG #0694789. ASSOCIATED ER/A 14-622118 ADDED FOR AC 9548. (LP #0707052)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION OUT OF LIMITS ON FLOOR SUPPORTS ON STA Y=157-200 AND X=45 (1 EA) PER B717-200 SRM 53-00-00-1A PROCEDURE, ALLOWABLE DAMAGE GENERAL, PAR 4.C, FIG 103. SUMMARY OF NRC 00821: CORROSION LEVEL 2. FLOOR SUPPORT ON STA Y=157-200 AND X=45 WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8. (LP #0705866)

Part: LUG — WORN (ZONE 500) · airframe 58,199 hrs · 41,263 cycles

WEAR ON HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING. SUMMARY OF NRC 00803: HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING WERE REPAIRED PER PRI 622848-14 REV 0 & ER/A 622848-14 REV ORIG. ASSOCIATED ER/A 14-622848 ADDED FOR AC 9548. (LP #0703921)

Part: HINGE FITTING — CORRODED (ZONE 500 FLAPS) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING. ALSO WEAR ON INNER CAVITY (4 EA) SUPPORT AT LH WING. CORROSION ON ACTUATOR SUPPORT LUGS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING. SUMMARY OF NRC 00713: CORROSION LEVEL 2. CORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING WERE REPAIRED WITH NRC 00738. THE INNER CAVITY (4 EA) SUPPORT AT LH WING. CORROSION ON ACTUATOR SUPPORT LUGS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING WERE REPAIRED PER PRI 622484-14 REV 2 & ER/A 622484-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-622484 ADDED FOR AC 9548. REPAIR INFORMATION IS ON LOG PAGE #0707323. UPDATE SUMMARY OF NRC 00713: LEVEL CORROSION 2. INNER CAVITY (4 EA) SUPPORT AT L H WING (ATACH FITTINGS/TRAILING EDGE FWD FLAP HINGE/BRACE FITTING XRS 164) WAS REPAIRED PER PRI 622484-14 REV 0, 1, 2 & ERA 622484-14 REV ORIG SECTION I: PERMANENT REPAIR. (LP #0703983)

Part: CUSP WEB — CRACKED (LH CUSP WEB) · airframe 58,199 hrs · 41,263 cycles

CRACKS ON LH CUSP WEB (3 EA) STA Y=657 & X=56 AND STA Y=716 & X=44.5 AND Y=888 & X=56 AT PASSENGER CABIN. SUMMARY OF NRC 00426: FABRICATED WEB STA Y-655 TO Y-715 PER B717-200 SRM 53-20-51-01 PROCEDURE 2. REPAIRED CUSP WEB STA 888 & X 56 PER B717-200 SRM 53-00-55-2R-4 FIG 211, CUSP WEB STA Y=716 TO Y=756 X=45 TO X=60 WERE FABRICATED PER NRC 00766 AND WERE INSTALLED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0683130)

Part: RIB — ELONGATED (RIGHT ELEVATOR) · airframe 58,199 hrs · 41,263 cycles

ELONGATED HOLE ON RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217. SUMMARY OF NRC 00410: RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217 WAS REPAIRED PER B717 SRM 55-00-00-2R REPAIR 2 PAR 4. THIS REPAIR IS PERMANENT IN ACCORDING WITH B717 SRM 55-00-00-2R PROCEDURE 2 REPAIR 2 PARAGRAPH 2 CATEGORY A. (LP #0681136)

Part: SKIN — MECHANIC ERROR (ZONE 100) · airframe 58,199 hrs · 41,263 cycles

EXTERNAL SURFACE OF FUSELAGE SKIN COMMON TO VHF ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L IN REF NRC 12. SUMMARY OF NRC 00169: FUSELAGE SKIN COMMON TO ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L WAS REPAIRED PER PRI 621891-14 REV 1 AND ER/A 621891-14 REV ORIGINAL SECTION I PERMANENT REPAIR. TIME OF ACCOMPLISHMENT SEC II ACCOMPLISH INSPECTION WITHIN EVERY 8,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR LOG PAGE # 0671385. ASSOCIATED ER/A 14-621891 ADDED FOR AC 9548. (LP #0680200)

Part: SKIN — DAMAGED (ZONE 200) · airframe 58,220 hrs · 41,282 cycles

LIGHTNING STRIKE ON THE FUSELAGE AT THE RH WINDOW PANEL, STA 484 TO 503. ACCOMPLISH ER/A 622755-14 SECTION II INSPECTION WITHIN EVERY 24 MONTHS UNTIL ACCOMPLISHMENT OF SECTION III PERMANENT REPAIR NO LATER THAN 48,400 TOTAL CYCLES. ASSOCIATED ER/A 00-622755 ADDED FOR AC 9548. 17DEC24 LOG WAS REDEFFERED TO QC, ESTABLISHED MONITOR INSP. (LP #0715690)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

CRACKS ON LH CUSP WEB (2 EA) STA Y=595 & X=56 AND STA Y=907 & X=56 BELOW SEAT TRACK SPLICE IN PASSENGER CABIN. SUMMARY OF NRC 00425: CUSP WEBS BTW STA Y 579-598 AND X=54 TO X=60 AND BTW STA Y 889-908 AND X=54 TO X=60 WERE REPLACED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 226, 51-41-02-0G, AND 51-41-05-0G. (LP #0673527)

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON DOOR JAMB FWD/AFT AT REPAIR SPLICES AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00806: CORROSION LEVEL 2. AFT CARGO DOOR JAMB FWD/AFT REPAIR SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0674286)

Part: SEAT TRACK — MECHANIC ERROR (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

MISDRILLED SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN. SUMMARY OF NRC 00751: SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP 30-10-70 PAR I PAGE 14 AND PER B717 SRM 53-20-52-2R REP 5 STEP 5 MAINTENANCE REQUIREMENTS. (LP #0668615)

Part: TRIPLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON PREVIOUS REPAIR TRIPLER ON FUSELAGE UNDER FILLET FAIRINGS AREA STA Y=843-860 LONG 28L-28R. SUMMARY OF NRC 00467: CORROSION LEVEL 2. PREVIOUS REPAIR TRIPLER WAS REPLACED PER B717 SRM 53-20-70-2R REP 1. PERFORM EXTERNAL VISUAL INSPECTION EVERY 8,000 CYCLES PER B717 SRM 53-20-70-2R PROCEDURE 1 REPAIR 1 PAR 7 A TABLE 201. (LP #0668323)

Part: LONGERON SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON UPPER AND LOWER SURFACE OF LONGERON AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LONGERON L29 R/H STA Y=157 TO Y=237 AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0666333)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

CRACKED FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT. SUMMARY OF NRC 00054: FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT WAS REPAIRED PER ER/A 621690-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 621690-14 REV 1. TIME CONTROLLED ITEMS: SEC II. ACCOMPLISH INSPECTION WITHIN EVERY 8,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. MONITORING UNDER LOGPAGE 0655266. ASSOCIATED ER/A 14-621690 ADDED FOR AC 9548. (LP #0660791)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN. SUMMARY OF NRC 730: CORROSION LEVEL 2. RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 (ET) HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER CUT OUT PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #0660337)

Part: DIAPHRAGM — CRACKED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON DIAPHRAGM BTW STA Y=200/218 AND X-54/X-22 AT CABIN PAX. SUMMARY OF NRC 00632: CORROSION LEVEL 2. DIAPHRAGM BTW STA Y=200 /218 AND X-54/X-22 WAS REPLACED PER DRAWING 9936535 REV CS. (LP #0658856)

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 58,199 hrs · 41,263 cycles

CRACKED INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 WAS REPAIRED PER B717 SRM 51-70-11-2R REP. 1. (LP #0658130)

Part: SEAT TRACK — MISINSTALLED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

WRONG INSTALLED FASTENERS ON SEAT TRACK AND CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN. SUMMARY OF NRC 00427: CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0655354)

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION AT CHANNEL BETWEEN STA 827 AND 832 L22R EXTERNAL FUSELAGE. SUMMARY OF NRC 407: CORROSION LEVEL 2. CHANNEL BTW STA Y=827 AND Y=832 L22R EXTERNAL FUSELAGE WAS FABRICATED PER DWG 5924872 REV BT AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0654013)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

CRACKED FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER. SUMMARY OF NRC 00052: FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER WAS REPAIRED PER ER/A 621691-14 REV ORIGINAL SECTION I PERMANENT REPAIR ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS, WITHIN EVERY 24 MONTHS AFTER NOV 05, 2024. LOG PAGE #0649328 PER ER/A 621691-14 REV ORIGINAL ASSOCIATED ER/A 14-621691 ADDED FOR AC 9548. (LP #0652226)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

CRACK ON LONGERON #8RH STA Y1022 AT PAX CABIN. SUMMARY OF NRC 00501: LONGERON #8RH STA Y1022 AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-05-2R-2. (LP #0650326)

Part: VANE — DENTED (ZONE 600 FLAP) · airframe 58,199 hrs · 41,263 cycles

DENTS (2 EA) ON UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=91 AT RH WING. SUMMARY OF NRC 00143: UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=76 OF RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0648769)

Part: LONGERON — CRACKED (ZONE 200) · airframe 58,199 hrs · 41,263 cycles

CRACK ON LONGERON 6LH STA Y=1022 AT PAX CABIN. SUMMARY OF NRC 00499: LONGERON 6LH STA Y=1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0647976)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,199 hrs · 41,263 cycles

CORROSION ON FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 AT PASSENGER CABIN. SUMMARY OF NRC 00475: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0645647)

Part: PAN — CRACKED (ZONE 100) · airframe 58,199 hrs · 41,263 cycles

CRACK ON INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPRTMENT. SUMMARY OF NRC 00112: INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0638113)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,491 hrs · 40,650 cycles

EXIT SIGNS ABOVE LT & RT OVERWING FWD EXIT DOORS DO NOT ILLUMINATE. T/S PER B717 FIM 33-50-00-201. R&R B5-121 BATTERY ASSEMBLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #5891885)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,926 hrs · 40,181 cycles

THE EMERGENCY OVERHEAD EXIT SIGN AT ROW 19 IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-120 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5441945)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,479 hrs · 39,796 cycles

THE EXIT MARKER AT THE AFT OVERWING EXIT AT STA 726L/726R IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE OVERHEAD BIN 10R, SEAT ROW 22R IAW B717 AMM 33-51. EXIT LIGHT OPERATIONALLY CHECKS GOOD. (LP #5150193)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,479 hrs · 39,796 cycles

THE CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE AT ROW 19. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT OVERHEAD BIN 8, ROW 17R IAW B717 AMM 33-51. LIGHT OPERATION CHECKS GOOD. (LP #5150194)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,001 hrs · 39,394 cycles

SHIP 9548 -ATB/DE- THE FLIGHT WAS RETURNED TO ATL DUE TO THE LOSS OF THE PRIMARY STABILIZER TRIM. ON DEPARTURE CLIMB OUT, THE CAPT NOTICED THAT THERE WAS NOT ANY DOWN TRIM AVAILABLE. UP TRIM WORKED FINE. ALTERNATE TRIM WAS USED SUCCESSFULLY TO CORRECT PITCH DOWN. AN EMERGENCY WAS DECLARED WITH ATC AND THE F/A WERE BRIEFED ON YELLOW EMERGENCY. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED MULTIPLE RELAYS AND THE STABILIZER TRIM MOTOR. OPERATIONAL CHECKS WERE ALL GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4825460)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,919 hrs · 39,337 cycles

SHIP 9548 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO A "STICK SHAKER PUSHER FAIL", FOLLOWED BY THE "SLAT DISAGREE" MESSAGE, AND AN AMBER X ON THE RIGHT WING CONFIG PAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE FLAP/SLAT HANDLE TRANSMITTERS WENT BAD. THE TRANSMITTERS WERE REPLACED PER B717 AMM 27-51-01 ON LOG PAGE 0013015. RETURN TO SERVICE TESTS ALL PASSED. THE AIRCRAFT IS OK FOR SERVICE. (LP #4825414)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 56,716 hrs · 39,997 cycles

CORROSION IN I/B SEAT TRACK UNDER G-7 GALLEY- MARKED. REPAIRED SEAT TRACK REF B717-200 SRM 53-20-52-2R REPAIR 5. (LP #2967622)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 55,882 hrs · 39,308 cycles

CORROSION WAS FOUND AT FLOOR SUPPORT IN GALLEY. MARKED. SUMMARY SEE NRC 001-0010:2500-2647/095 00253: REPLACED FLOOR SUPPORT REF DAC DWG 9936534. (LP #2964169)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,311 hrs · 38,826 cycles

THE EMERGENCY BATTERY PACK B5-120 DIES. MAINTENANCE REPLACED THE B5-120 EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. (LP #4688714)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,235 hrs · 38,758 cycles

THE CABIN CREW NOTICED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS MISSING AT LOCATION 300. MAINTENANCE REPLACED THE MISSING EXIT COVER AT LOC 300. (LP #2778074)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,147 hrs · 38,682 cycles

EMERGENCY LIGHTING IS OUT AT 17C AND 18C. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT OVERHEAD BIN 18CDE (B5-120) AS PER B717 AMM 33-51. ALL CHECKS ARE NORMAL. (LP #9495086)

Part: SKIN — DENTED (LT TE FLAP) · airframe 57,700 hrs · 40,820 cycles

DENT & 3/8" HOLE IN FLAP SKIN AFT OF LT MAIN LANDING GEAR. PER ERA 606778-14 REV ORIGINAL, SEC 1 ACCOMPLISHED DETAILED VISUAL INSPECTION, NO DAMAGE BEYOND PUNCTURE, NO LOOSE, MISSING, OR PULLED FASTNERS. COMPLIED WITH PERMANENT REPAIR OF FLAP OF ERA 606778-14 REV ORIGINAL REF B717 SRM 57-00-00-2R PROCEDURE 2. (LP #4135408)

Part: UNKNOWN — UNKNOWN · airframe 54,611 hrs · 38,235 cycles

REMOVED LT OUTER WING FIXED TRAILING EDGE REF ERA 604993-14 REV ORIG SECTION V. BLENDED DAMAGE AREA PER ERA 604993-14 REV A. PERFORMED HFEC OF CUTOUT PER STEP 5 OF ERA 604993-14 REV A SECTION 5. NO CRACK INDICATIONS NOTED. QC2013. FILLER & DOUBLER MADE, DRILLED, TREATED, & PRIMED PER REA 604993-14 REV A. NEW RIB INSTALLED. COMPLETED REPAIR PER ERA 604993-14 REV A. SECTION 5. OK FOR SVC. (LP #2621100)

Part: NONE — NONE · airframe 53,949 hrs · 37,670 cycles

THE INTERIOR EMERGENCY LIGHTING FOR THE LEFT AND RIGHT AFT LOWER OVERWING EXITS ARE NOT WORKING. MAINTENANCE REPLACED THE BATTERY PACK FOR THE INTERIOR AFT LOWER OVERWING LIGHTS PER B717 AMM 33-51-06. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #9192898)

Part: COVER — MISSING · airframe 52,782 hrs · 36,575 cycles

THE FORWARD EMERGENCY EXIT LIGHT COVER IS MISSING. THIS COULD PREVENT PROPER LOCATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED THE FORWARD EMERGENCY EXIT LIGHT COVER. THE AIRCRAFT IS OK FOR SERVICE. (LP #8828964)

Part: NONE — NONE · airframe 52,771 hrs · 36,564 cycles

THE INTERIOR EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8828951)

Part: NONE — NONE · corrosion level 2 · airframe 51,611 hrs · 35,561 cycles

CORROSION ON PAN BTW STA Y954 TO Y994 AT AFT CARGO COMPARTMENT JAMB. SUMMARY OF NRC 00158: CORROSION LEVEL 2. PAN BTW STA Y954 TO Y994 AT AFT CARGO COMPARTMENT JAMB WAS REPAIRED PER ER/A 594290-14 REV. ORIGINAL AND ETI-17-21-007 REV. ORIGINAL. ACCOMPLISH SECTION II: PERMANENT REPAIR WITHIN 24 MONTHS FROM 19-SEP-21 AND LOG PAGE #1959913. ASSOCIATED ER/A 14-594290 ADDED FOR AC 9548. (LP #1960671)

Part: NONE — NONE · corrosion level 2 · airframe 51,601 hrs · 35,551 cycles

CORROSION ON SPLICE ON AFT PRESSURE BULKHEAD STA 1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00136: CORROSION LEVEL 2, SPLICE ON AFT PRESSURE BULKHEAD STA 1053 BTW LONG 29LH-29RH WAS REPLACED PER B717 SRM 53-20-08-0I, SRM 51-41-02-0G PAR 4, AND SRM 51-41-05-0G PAR 8. (LP #1961195)

Part: NONE — NONE · airframe 51,601 hrs · 35,551 cycles

CRACKED CHANNEL AT LH MLG INBOARD DOOR INTERNAL SKIN, BETWEEN STA 790 TO 793. (PTAS). SUMMARY OF NRC 00266: FORWARD Z CHANNEL AT LH MLG DOOR WAS REPAIRED PER ER/A 594279-14 REV. ORIGINAL, SECTION I - PERMANENT REPAIR AND ETI-17-21-004 REV. 1 ASSOCIATED ER/A 14-594279 ADDED FOR AC 9548. (LP #1961264)

Part: NONE — NONE · corrosion level 2 · airframe 51,598 hrs · 35,550 cycles

CORROSION ON JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT JAMB AREA. SUMMARY OF NRC 00216: CORROSION LEVEL 2, SECTION OF JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R-6. (LP #1953156)

Part: WEB — CORRODED (BS 190-195) · corrosion level 2 · airframe 51,598 hrs · 35,550 cycles

CORROSION ON MEMBRANE BTW STA Y=190 TO STA Y=195 AND X=53 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00191: CORROSION LEVEL 2. MEMBRANE BTW STA Y=190 TO STA Y=195 AND X=53 AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 53-00-55-1A-1- PAR.4 FIG.101 ( SHEET 1). (LP #1947909)

Part: CUSP WEB — CRACKED (BS 715) · airframe 51,598 hrs · 35,550 cycles

CRACK ON CUSP MEMBRANE STA Y=715 X=54 AT CPAX IN REF AMDS 5310-01436-01A. SUMMARY OF NRC 00174: CUSP MEMBRANE STA Y=715 X=54 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG. 212. (LP #1943839)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,375 hrs · 33,674 cycles

DURING SERVICE CHECK, THE EMERGENCY EXIT LIGHT AT ROW 19 EDC WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-121 IAW B717 AMM 33-55. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMEGENCY LIGHTS) · airframe 49,257 hrs · 33,566 cycles

AFT CABIN OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENCE REPLACED THE BATTERY CHARGER PER B717 AMM 33-51-03.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,995 hrs · 33,334 cycles

THE CENTER AISLE EMERGENCY ESCAPE LIGHTS AT ROW 15 - 18 AND THE EMERGENCY EXIT DOOR LIGHT ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-120 IAW AMM 33-51-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE.

Part: PANEL — DETACHED (NR 1 NACELLE) · airframe 48,498 hrs · 32,916 cycles

GROUND AGENT FOUND A PANEL HAD FALLEN FROM AREA OF NUMBER 1 ENGINE. PANEL WAS HOT TO TOUCH. DETERMINED TO BE THE LEFT PACK FAN BYPASS CHECK VALVE FLAPPER DOOR. (LP #7215891)

Part: WIRE — PINCHED (AILERON SERVO) · airframe 46,984 hrs · 31,733 cycles

ON TAXI OUT WHEN CHECKING CONTROLS THE WHEEL BECAME STUCK FULL RIGHT. FOUND WIRING INTERNAL ON DUAL AILERON SERVO PINCHED AND WIRING EXSPOSED. DUAL AILERON SERVO WAS REPLACED PER B717 AMM 22-12. FAILED AILERON RTS TEST. REPLACED THE SERVO A SECOND TIME PER B717 AMM 22- 12 AND FUNCTIONAL CHECK WAS GOOD. DISCREPANCY NOTED WAS DETERMINED TO BE CAUSED BY A JAMB OF THE RHEOSTAT TO AIL SERVO DRUM & HOUSING ASSY ATTACH SCREW. SAFETY CRIMP MOVED & GOT JAMMED BETWEEN SCREW HEAD & DRUM ASSEMBLY. A NEW DRUM AND HOUSING ASSY WAS INSTALLED PER B717 AMM 22-12-02 000-801. RII COMPLETE PER MCC R&R FCC 1/2 PER B717 AMM 22-01-03. (LP #5813820)

Part: FRAME — CRACKED (BS 1022) · airframe 42,719 hrs · 28,768 cycles

CRACK ON FRAME ANGLE BS 1022, LONGERON 7R. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.

Part: FRAME — CRACKED (BS 1022) · airframe 42,719 hrs · 28,768 cycles

CRACK ON FRAME ANGLE BS 1022, LONGERON 6R. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.

Part: FRAME — CRACKED (BS 1022) · airframe 42,719 hrs · 28,768 cycles

CRACK ON FRAME ANGLE BS 1022, LONGERON 7L. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.

Part: PIN — OUT OF POSITION (L1 DOOR SLIDE) · airframe 42,719 hrs · 28,768 cycles

OUT OF POSITION SAFETY PIN HOLE AND PIN AT L1 DOOR SLIDE. REPLACED THE SLIDE.

Part: FRAME ANGLE — CORRODED (BS 908) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON FRAME ANGLE BS 908, BETWEEN LONGERONS 25R TO 26L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND DWG 9912243, REV JS.

Part: FRAME ANGLE — CRACKED (BS 1053) · airframe 42,719 hrs · 28,768 cycles

CRACK ON FRAME ANGLE, BS 1053 BETWEEN LONGERONS 17 - 18L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG S2912293S, REV DL.

Part: SKIN — CRACKED (BS 1022) · airframe 42,719 hrs · 28,768 cycles

SKIN CRACKED BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 590959-14, REV ORIGINAL, AND ETI-17-17-182, REV 1.

Part: SKIN — CRACKED (BS 1076) · airframe 42,719 hrs · 28,768 cycles

SKIN BS 1076, BETWEEN LONGERONS 13 - 14R CRACKED. THE SKIN WAS REPAIRED IAW ETI 17-17-184, REV 1, AND ER/A 560957-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1022) · airframe 42,719 hrs · 28,768 cycles

CRACKED LONGERON 7R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.

Part: SKIN — CORRODED (BS 849-856) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

EXCESSIVE CORROSION ON THE FUSELAGE SKIN, UNDER FILLET FAIRINGS BETWEEN BS 849 - 856, LONGERONS 29R TO 28L. THE SKIN WAS REPAIRED IAW SRM 53-20-70-2R.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 42,719 hrs · 28,768 cycles

CRACKED FLOORBEAM BS 737, LBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05, AND 51-41-02.

Part: STRUCTURE — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

AFTER A CORRODED NUT WAS REMOVED, CORROSION AND SCRATCHES AT BORES WERE FOUND. BORE OF BARREL NUT NR 27 WAS REPAIRED IAW ETI-17-17-190, REV 1, AND ER/A 562336-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (BS 617-636) · airframe 42,719 hrs · 28,768 cycles

CRACK ON THE INTERCOSTAL BETWEEN BS 617 - 636, BL 0 (CEILING AREA) IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1, 51-41-02, AND 51-41-05.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 42,719 hrs · 28,768 cycles

CRACK ON THE FLOOR PANEL 221SF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG 201.

Part: FRAME — CRACKED (BS 1037) · airframe 42,719 hrs · 28,768 cycles

CRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, PRCEDURE 4. ET, HFEC ACCOMPLISHED IAW NDT SPM 06-10-01.001 NO CRACKS FOUND AFTER DAMAGED WAS REMOVED.

Part: WEB — CORRODED (BS 201) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON THE WEB AT BS 201, LBL 54 OF THE L1 DOOR FRAME. THE WEB WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, 51-41-05, 51-41-08, AND 53-10-15-01-2, FIG.1.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 42,719 hrs · 28,768 cycles

CRACK ON UPPER SURFACE OF FLOOR PANEL 222AQF. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-41-02, AND SRM 53-00-00-2R-1, FIG 201.

Part: SPLICE — CRACKED (LT WING LE) · airframe 42,719 hrs · 28,768 cycles

CRACKED SPLICE ON LEADING EDGE XRS 267, LT WING . THE SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 57-40-01-01, FIG 1, SRM 51-41-02, AND SRM 51-41-05.

Part: BEAM — CRACKED (NLG DOOR FRAME) · airframe 42,719 hrs · 28,768 cycles

CRACK ON THE LT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, ET, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.

Part: BEAM — CRACKED (BS 48) · airframe 42,719 hrs · 28,768 cycles

CRACK ON THE RT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.

Part: WEB — CORRODED (BS 200) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION AT FLOOR WEB BS 200 BETWEEN LBL 8 - RBL 8. THE WEB WAS REPAIRED IAW SRM 51-70-10-2R, FIG 2.

Part: SUPPORT — CORRODED (BS 148) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON PANEL SUPPORT BS 148 RBL 54. THE SUPPORT WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-08.

Part: CUSP WEB — CORRODED (BS 628) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON THE LOWER & UPPER SURFACES OF THE CUSP WEB AT BS 628. THE CORROSION WAS REMOVED. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS FOUND AFTER TRIM OUT IAW NDTSPM 06-10-01.001. A REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55-2R-4, FIG 215.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 42,719 hrs · 28,768 cycles

PUNCTURE IN THE LOWER SKIN ON THE AFT MOVABLE VANE OF THE RT WING TE FLAP. THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, PAR 4.

Part: PAN — CRACKED (BS 757) · airframe 42,719 hrs · 28,768 cycles

CRACK ON RT RING PAN BS 757. REPAIRED PER B-717 SRM 56-20-02-2R-1, FIG 202.

Part: CUSP WEB — CORRODED (BS 489) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON THE LOWER & UPPER SURFACES OF THE CUSP WEB BS 489. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON THE SEAT TRACK RBL 22 AND SETTLEMENT AREA FROM BS 200 - 256. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-01-0G.

Part: CUSP WEB — CORRODED (BS 517) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

EXCESIVE CORROSION ON THE CUSP WEB RT LOWER & UPPER SURFACES BS 517, RBL 54 TO 60. REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON THE FLOORBEAM BS 200 BETWEEN RBL 9 - 44, THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-01-2, 51-40-08, 51-10-04, PAR 15, 21, 51-41-02, AND 51-41-05.

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION OUT OF LIMITS BS 541 - 560, LBL 44.5 AND LBL 60 ON THE CUSP WEB. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01.001.

Part: FLOOR SUPPORT — CORRODED (BS 1025-1060) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON FLOOR SUPPORT FROM BS 1025 - 1060, RBL 16. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9936656-67, REV AM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,719 hrs · 28,768 cycles

CORROSION ON FLOOR SUPPORT BS 167, RBL 11. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05, AND SRM 51-40-08.

Part: PAN — CRACKED (L1 DOOR) · airframe 42,719 hrs · 28,768 cycles

CRACK ON INNER PAN BETWEEN THE NR 1 BEAM AND FWD UPPER CORNER AT L1 DOOR. THE PAN WAS REPAIRED IAW SRM 52-10-02-2R-3 FIG.201.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,719 hrs · 28,768 cycles

CRACK ON THE NR 1 BEAM AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, FIG 20.

Part: ANGLE — CRACKED (R1 DOOR BEAM) · airframe 42,719 hrs · 28,768 cycles

CRACK ON ANGLE BELOW THE NR 1 BEAM, AFT EDGE. R1 DOOR. THE ANGLE WAS REPLACED IAW DWG 9911579, REV L, SRM 51-41-01, AND 51-41-05.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 41,840 hrs · 28,118 cycles

L1 DOOR EXIT SIGN LENS DETACHED. SECURED THE LENS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,357 hrs · 27,792 cycles

CABIN CEILING EMERGENCY LIGHTS OF BS 569, 626, 680, 626, AND 706 EXIT SIGN INOPERATIVE. REPLACED THE B5-120 POWER SUPPLY, OPS CHECKED NORMAL IAW AMM 33-51.

Part: STRINGER — CORRODED (BS 974) · corrosion level 2 · airframe 40,388 hrs · 27,126 cycles

CORROSION ON STRINGER 29L JUST AFT OF BS 974. REPAIRED IAW SRM 53-00-05, REP 3.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,978 hrs · 25,370 cycles

AFT CARGO, LOWER ENTEY JAMB CORRODED. BLENDED OUT CORROSION ON LOWER JAMB ENTRY. REMOVED SCUFF PLATE AND SILL. REMOVED LOWER JAMB PAN. REPLACED FWD AND AFT SIDE SPLICES. INSTALLED NEW LOWER JAMB PAN. REINSTALLED SCUFF PLATE AND SILL SRM 53-20-15, REPAIR NR 7, AND PRI 541202-14, REV 1. ER/A 541202-14, REV ORIGINAL RECEIVED ON 13NOV15.

Part: LONGERON — CRACKED (BS 1133) · airframe 37,966 hrs · 25,361 cycles

TAIL INTERIOR, LONGERON 2R IS CRACKED AT AFT SIDE OF FRAME AT BS 1133. REPAIRED IAW SRM 53-00-05, REPAIR 2.

Part: FITTING — NOT REPORTED (FUSELAGE) · corrosion level 2 · airframe 40,373 hrs · 27,116 cycles

FWD GIRT LATCH ATTACH LUG SEEN UNDER FLOOR PANEL 221EF, AT 1R DOOR. REPLACED FITTING PER DWG 9936534.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,856 hrs · 25,301 cycles

DURING SERVICE CHECK, FOUND AFT LOWER OVER WING EXIT SIGN LIGHTS INOPERATIVE ON THE LT AND RT SIDES. REPLACED BATTERY PACK B5-230 AND CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,819 hrs · 25,277 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,613 hrs · 22,626 cycles

DURING LINE CHECK, EMERGENCY LIGHTS IN TAIL COMPARTMENT WERE INOPERATIVE. BATTERY CHARGER WAS FOUND INOPERATIVE AND THE POWER SUPPLY WAS REPLACED IAW AMM 33-51. OPS NORMAL.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 33,729 hrs · 21,824 cycles

EMERGENCY EXIT LIGHT SIGN AT CEILING ROW 1 FELL OFF DURING TAKE-OFF. REPLACED EMERGENCY LIGHT LENS.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 33,464 hrs · 21,628 cycles

EMERGENCY LIGHT BATTERY PACK AT BS 59 INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 33,464 hrs · 21,628 cycles

RT WING UPPER SURFACE TE FLAP DAMAGED APPROXIMATELY XRS 89.000, 17" FWD OF TE, JUST AFT OF INBD SPOILER AT CTR. REPAIRED DOUBLER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

RT CUSP WEB CORRODED BETWEEN STATION 927 TO STATION 946. REPAIRED CUSP WEB IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

LT WING TO BODY FORMER CORRODED AT BS 851 BETWEEN LONGERON 25L & LONGERON 28L. R&R STRAP IAW SRM & DRAWING.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

RT MAIN CABIN CUSP WEB SKIN DAMAGED AT STATION 674, RBL 52. R&R WEB IAW SRM.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 33,464 hrs · 21,628 cycles

PAX CABIN FLOOR BOARD CORRODED AT STATION 825, BETWEEN RBL 44 TO RBL 56. REPAIRED BOARD IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

FWD CARGO CUSP WEB SKIN CORRODED AT BS 589, LONGERON 18R. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN UPPER AFT WINDOW FRAME ANGLE BETWEEN BS 870L & BS 889L CRACKED. REPAIRED ANGLE IAW SR.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

LT SIDE TIE DOWN TRACK SUPPORT CLIP CRACKED AT STATION 994. R & R IAW CLIP SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

EE COMPARTMENT VERTICAL STRAP CRACKED AT STATION 110, BL 0. R & R STRAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

FRAME CRACKED AT BS 696, BETWEEN LONGERON 9R TO LONGERON 18R. R & R FRAME IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

FRAME CRACKED AT BS 715, BETWEEN LONGERON 9R TO LONGERON 18R. R &R FRAME IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,464 hrs · 21,628 cycles

L1 DOOR CLIP CRACKED INSIDE HANDLE BOX. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: PANEL — CRACKED (RT MLG WW) · airframe 33,464 hrs · 21,628 cycles

RT MLG WW AFT DOOR CUT OUT AREA CRACKED ON ATTACH SHIELD PANEL. REPAIRED DOUBLER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

CABIN FLOOR BOARD VERTICAL SUPPORT CRACKED AT STATION 737 LBL 44. R & R SUPPORT IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

AFT ACCESSORY COMPARTMENT RT LOUVER AT CANT FRAME 1200 UPPER AFT REPAIR DOUBLER CRACKED. R & R PANEL IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

CENTER TANK FWD BULKHEAD VERTICAL SUPPORT CRACKED AT BS 655, LBL 22. R & R STIFFENER IAW SRM & DRAWING.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

AFT ACCESSORY LOWER LT LOUVER SUPPORT BRACKET CRACKED AT CANT FRAME 1189. R & R CLIP IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

SHEAR TIE CRACKED AT STATION 1144 STRINGER 2R. R & R TIE CLIP IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

SHEAR TIE CRACKED AT STATION 1152 STRINGER 2R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

STRINGER CRACKED AT STATION 1113, STRINGER 2L. REPAIRED STRINGER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 ACF DELAMINATED. R & R PANEL IAW SRM & AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 AFT DELAMINATED. R & R PANEL IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

FS SKIN CORRODED AT STATION 579, STRINGER 20L. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222AEF DELAMINATED. R & R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 JF DELAMINATED. R &R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 AVF DELAMINATED. R & R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 221 WF DELAMINATED. R & R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 RF DELAMINATED. R & R PANEL IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 AGF DELAMINATED. R & R PANEL IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 FF DELAMINATED. R & R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 BF DELAMINATED. R & R PANEL IAW SRM & AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 PF DELAMINATED. R & R PANEL IAW SRM & MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222 LF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,464 hrs · 21,628 cycles

MAIN CABIN FLOOR PANEL 222AMF DELAMINATED. R & R PANEL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,464 hrs · 21,628 cycles

LT INTERCOSTAL CRACKED AT STATION 817 AFT PIT BULKHEAD AREA 12" LBL. R&R INTERCOSTAL IAW SRM.

Part: COVER — LOOSE (R1 DOOR) · airframe 32,807 hrs · 21,229 cycles

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

Part: LENS — UNSECURE (CABIN) · airframe 32,514 hrs · 21,056 cycles

FWD EMERGENCY EXIT LIGHT COVER FELL OFF. REINSTALLED AND SECURED LENS PER AMM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 29,909 hrs · 19,389 cycles

DURING OPERATIONAL CHECK OF TAIL CONE EMERGENCY RELEASE, UNSAFE LIGHT INDICATOR INOP. REMOVED AND REPLACED LIGHT INDICATION CONTROL SWITCH PER MM.

Part: FITTING — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT SHEAR CLIP, STA 927, LONG 29L TO 30, CORROSION. ACCOMPLISHED SHEAR CLIP REPLACEMENT PER B717 SRM 51-41-02, 51-41-05 AND 53-00-00.

Part: FITTING — CORRODED (FUSELAGE)

CABIN FLOOR FITTING, STA 218, RBL 55, CORROSION. ACCOMPLISHED FLOOR FITTING REPLACEMENT PER B717 SRM 53-00-00, 51-41-01 AND 51-41-05.

Part: FITTING — CORRODED (GIRT BAR)

MAIN CABIN R1 DOOR GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-01.

Part: ANGLE — GOUGED (LT NACELLE)

LEFT ENGINE UPPER COWLING INNER FACE, GOUGED. ACCOMPLISHED COWLING INNER FACE FRAME ANGLE REPAIR PER B717 SRM 54-20-05 FIG 201 REPAIR 3.

Part: WEB — CRACKED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 237, RBL 44, CRACKED. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-00-07.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, LBL 18, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT INTERCOSTAL SECTION, STA 946 TO 954, LONG 28R TO 29R, CORROSION. ACCOMPLISHED INTERCOSTAL SECTION REPLACEMENT PER B717 SRM 53-00-00, 51-41-02, 53-20-51 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 7 TO LBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 237, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-20-52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP AT ROWS 1-10. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER AT ROW 10DEF IAW B717 MM 33-51. OPS CHECK GOOD.

Part: SKIN — DAMAGED (FUSELAGE)

RIGHT WINDOW BELT FUSELAGE SKIN, STA 389 TO 408, LONG L13R TO L15R, REQUIRES DOUBLER. ACCOMPLISHED FUSELAGE SKIN BELT DOUBLER REPAIR PER BOEING DWG SR09530053-9 CONFIG 7007 AND AIRTRAN TC 738-012.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 22 DEF AFT EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LAMP ASSY ROW 22 IAW B717 MM 33-51-04.

Part: BATTERY — DISCHARGED (CABIN)

F/A'S REPORT EMER LIGHTS WERE ON 10 TO 15 MIN DUE TO EXT PWR BEING PULLED. VERIFIED WITH RAMP PERSONNEL THAT EMERGENCY LIGHTS WERE ON FOR LESS THAN 5 MINUTES, CHARGED EMERGENCY LIGHT BATTERIES PER AMM 33-51.

Part: LIGHT — MISSING (CABIN)

EMERGENCY LIGHT AND COVER ARE MISSING. INSTALLED LIGHT BULB AND COVER REF MM 33 51. OPS CHECK NORMAL.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L-1 DOOR SLIDE LANYARD LOCK PIN WILL NOT STAY IN PLACE. REMOVED AND REPLACED L-1 DOOR SLIDE ASSY IAW MM 25-61; A/C OK FOR SERVICE.

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: FRAME — DAMAGED (FUSELAGE)

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

Part: PAN — CORRODED (FR 954-994)

CORROSION AT AFT CARGO SURROUNDING DOOR JAMB LOWER AREA. CUT OUT DAMAGED SECTION AND INSTALLED NEW LOWER SECTION PER REF SRM 53-20-15.

Part: BRACKET — CORRODED (FUSELAGE)

CABIN, FUSELAGE STA 160 AT CENTER AREA, FLOOR SUPPORT HAS SURFACE CORROSION. REPLACED FLOOR SUPPORT BRACKET FABRICATED PER REF DWG 9936534, MAT PO 1064860 & 3932140-2400. INSTALLED REF B717 SRM 51-41-01.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE)

CORROSION AT COCKPIT DOOR, SEC NR 1. REPLACED BRACKET SUPPORT ASSY FROM COCKPIT THRESHOLD AS REQUIRED. REF SRM 51-41-01 AND EA 17-53-02196IR.

Part: BATTERY — DISCHARGED (CABIN)

WHILE PERFORMING MAINTENANCE CHECK OF THE EMERGENCY ESCAPE LIGHTING SYSTEM, BOTH LT AND RT FUSELAGE LIGHTS JUST FORWARD OF ENGINES ARE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

BULB OUT IN EMERGENCY LIGHT IN COCKPIT. REMOVED AND REPLACED BATTERY SUPPLY AND BATTERY. OPS CHECK GOOD. REF MM 33-51.

Part: BATTERY — ACTIVATED (CABIN)

BUSINESS CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND CHARGER FOR BUSINESS CLASS.

Part: FRAME — CRACKED (BS 1178)

TWO CRACKS FOUND AT INT TAIL COMP LT SIDE CANTED FRAME STA 1178.225 BETWEEN LONG 13L AND 14L. INSTALLED FORMED CHANNEL REPAIR ON CANTED FRAME LT STA 1178.225 PER B717 SRM 51-70-11 FIG 201.

Part: FRAME — CRACKED (BS 1178)

CRACK AT TAIL COMPARTMENT, RIGHT CANTED FRAME 1178.225 BETWEEN LONG 13 AND 14 R. INSTALLED FORMED CHANNEL REPAIR ON RIGHT CANTED 1178.225 PER SRM 41-70-11 F 201.

Part: THRESHOLD — PUNCTURED (FWD CARGO BAY)

FWD PIT AFT THRESHOLD STRUCTURE IS PUNCTURED. DAMAGED AREA HAS BEEN ROUTED OUT AND DYE PEN INSPECTION REVEALED NO CRACKS. REPLACED LOWER SECTION OF THE FORWARD CARGO DOOR LOWER JAMB PAN IAW B717 SRM 53-20-15 REP 6.

Part: VENT — CRACKED (RIGHT)

RIGHT HAND VENT BOX CRACKED. INSTALLED DOUBLER REPAIR AT RIGHT HAND VENT BOX IAW AIRTRAN T/C 17-5320-2023 FIG 1 AND 2. MATERIAL USED 7075 T6-040 SIZE 4.06 X 5.12 INCHES.

Part: SKIN — DENTED (BS 251-256 S17L)

FUSELAGE LEFT FWD AREA HAS 4 EA DENTS LOCATED AT APPROX STA 251-256 LONGERON 17. CUT OUT DAMAGED AREA AS PER B-717 MM 53-00-02 REPAIR 6, INSPECT CUT OUT AREA PER B-717 NDT SPM 06-10-01 .001, NO CRACKS FOUND. INSTALLED REPAIR PER B-717 SRM 53-00-01 REPAIR 6.