N943AT

Part: WINDSHIELD — ARCED (ZONE 200) · airframe 67,452 hrs · 48,744 cycles

WHEN TURNING ON THE WINDSHIELD ANTI ICE SWITCH SENSOR ON F/O'S FWD WINDOW STARTED ARCHING. REMOVED AND REPLACED CENTER WINDSHIELD REF B717 AMM 56-11. (7791708)

Part: SWITCH — FAULTED (ZONE 200) · airframe 67,415 hrs · 48,716 cycles

ATB, CREW REPORTED SMOKE IN THE COCKPIT WITH ASSOCIATED ELECTRICAL SMELL. FOUND ELECTRICAL ODOR TO BE EMITTING FROM THE FIRST OFFICERS MASTER CAUTION PUSH BUTTON SWITCH AND WARM TO TOUCH. REPLACED SWITCH.(7791702)

Part: TIRE — FAILED (ZONE 700) · airframe 66,732 hrs · 48,056 cycles

TIRE- #1 MLG TIRE FAILURE AFTER LANDING WITH LEFT ANTISKID FAIL MESSAGE. REPLACED #1 ANTISKID TRANSDUCER, ANTISKID CONTROLLER AND #1-#2 MLG WHEEL ASSEMBLIES. OPS CHECKS GOOD.(7436618)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,281 hrs · 47,655 cycles

AIRCRAFT 9503, FWD GALLEY AREA CORROSION: RH O/B SEAT TRACK CORRODED AT FWD END. CORRECTIVE ACTION: REPAIRED SEAT TRACK PER B717 SRM 53-20-52-2R-5. (LP 1001907)

Part: WEB — CRACKED (ZONE 200) · airframe 66,281 hrs · 47,655 cycles

SHIP 9503 CUSP MEMBRANE DAMAGE (CRACKED) RIGHT SIDE STA STA 200. CORRECTIVE ACTION: REPAIRED PER B717-200SRM 53-00-55-2R PROCEDURE 4. (0999891)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 65,570 hrs · 47,033 cycles

THE FWD EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK AT THE FWD OVERHEAD EQUIPMENT F5-259 COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6858025)

Part: SKIN — DAMAGED (ZONE 100) · airframe 65,382 hrs · 46,868 cycles

SKIN AT FWD LOWER CORNER OF LAV WASTE DUMP CUT OUT PUSHED OUT APPROX .75" FWD LAV WASTE BOX. CREASE IN SKIN APPROX 4" LONG. MAX DEEP IN GAP BETWEEN SKIN AND WASTE BOX APPROX 1". PERFORMED EXTERNAL DOUBLER AND TRIPLER REPAIR IAW ER/A 622994-14 REV O. FOLLOW ON INSPECTIONS WILL BE PERFORMED ON LOG PAGE 0738200 AT 8,000 FLIGHT CYCLE INTERVALS. A/C OK FOR SERVICE. REQUIRED INSPECTION ITEM COMPLETED. (LP #6621482)

Part: WIRE — SHORTED (ZONE 200) · airframe 65,377 hrs · 46,864 cycles

THE FWD EXIT SIGN OVER FWD F/A SEAT IS INOPERATIVE. ALSO, 4 EXIT LIGHTS ON AFT CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY EXIT SIGN (L2-790). ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-260 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51. PAX CABIN EEPL CHECK OK. AFT ACCESSORY COMPARTMENT EEPL REMAIN INOPERATIVE. FOUND NO POWER COMING FROM PLUG P1-260 PIN 9 TO TERMINAL BLOCK S3-559 STUD 1. FOUND WIRE SHORT ON WIRE E9405-519-16 BETWEEN PLUG P1-6028 AND SPLICE P1-3803. REPAIRED WIRE C9302-255-16 PER B717 SWPM 20-10. REPLACED EMERGENCY POWER SUPPLY PER B717 AMM 33-51. REPLACED CATWALK LIGHT L2-845 AND CONNECTORS. REPLACED CONNECTORS P1/R5-3804, P1/R5-3803, P1/R5-3805, AND P1/R5-3806 AS WELL PER B717 WDM 33-51-14. ALL EEPL CHECK GOOD. (LP #6621480)

Part: ANGLE — CRACKED (ZONE 200) · airframe 64,847 hrs · 46,400 cycles

ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L CRACKED. REPLACED ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L IAW B717 SRM 51-40-02 AND B DRAWING 5420838. INSTALLED LT & RT LOUVER PANELS. COMPLIED WITH INSP PER B717 W/C 5312-01194-01.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 63,987 hrs · 45,725 cycles

DURING THE SERVICE CHECK, THE EMERGENCY LIGHTS AT THE CATWALK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-237 PER B717 AMM 33-51-03. (LP #5853294)

Part: RUDDER — DAMAGED (ZONE 300) · airframe 61,596 hrs · 43,620 cycles

RUDDER RH SKIN PANEL DAMAGED ON UPPER SIDE NEAR STA ZR165.3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,202 hrs · 44,234 cycles

THE TAILCONE COMPARTMENT EMERGENCY LIGHTING IS INOPERATIVE. MAINTENANCE TROUBLE SHOT PER B717 FIM 33-50-00-810-801, WDM 33-51-13, AND 33-51-14. FOUND B5-116 BATTERY ASSEMBLY DISCONNECTED FROM CRADLE SOCKET. ALSO FOUND THE BATTERY BASE FOR B5-260 WAS BAD. THE BATTERY ASSEMBLY WAS RECONNECTED AND THE BASE WAS REPLACED PER AMM 33-51-03. OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT IS OKAY FOR SERVICE. (LP #4950649)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,108 hrs · 44,155 cycles

THE TAIL CONE RELEASE CAM IS CLOCKED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED THE RELEASE CAM REF AMDS WORKCARD 5352-2001. (LP #2859456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,270 hrs · 44,297 cycles

AFT CARGO DOOR JAMB CORROSION ON SKIN TO LONGERON ADJACENT TO REAR CARGO DOOR FRAME AT STA 1000. REPAIRED PER ER/A 610079-14 REV. ORIGINAL. (LP #2846315)

Part: PANEL — CORRODED (LEFT) · corrosion level 2 · airframe 63,556 hrs · 45,347 cycles

AREA OF CORROSION NOTED DIRECTLY FWD OF LEFT SLANT PANEL (MARKED). COMPLIED WITH ERA 610004-14 REV ORIG. PRI 610004-14 REV 0 MATCHES ERA 610004-14 REV ORIG. ASSOCIATED ERA 14-610004 ADDED FOR AC 9503. (LP #2846122)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,107 hrs · 44,153 cycles

AFT CARGO DOOR LOWER PAN HAS CORROSION IN SEVERAL LOCATIONS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/003 00024: EDGED SEALED AFT CARGO DOOR LOWER PAN REF REPAIRED CARGO DOOR FRAME LOWER PAN REF B717-200 SRM 53-20-15-2R REPAIR 7 AFT CARGO LOWER JAMB PAN CORROSION SPLICE REPAIR AND REAPPLIED CARGO COMPARTMENT DOOR LOWER JAMB CORRSION PROTECTION REF B717-200 SRM 53-00-15-2R REPAIR 1. (LP #2844392)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,107 hrs · 44,153 cycles

FWD CARGO DOOR FRAME LOWER PAN HAS CORROSION IN AT LEAST 2 LOCATIONS NEAR STOP FITTINGS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/001 00018: REPAIRED CARGO DOOR FRAME LOWER PAN REF B717-200 SRM 53-20-15-2R REPAIR 6. FORWARD CARGO LOWER JAMB PAN CORROSION SPLICE REPAIR AND REAPPLIED CARGO COMPARTMENT DOOR LOWER JAMB CORROSION PROTECTION REF B717-200 SRM 53-00-15-2R REPAIR 1. (LP #2836273)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,039 hrs · 44,094 cycles

FOUND THAT THE EMERGENCY LIGHT IN ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #9964533)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,204 hrs · 43,384 cycles

THE AFT WALKWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE AFT BATTERY CHARGER ASSEMBLY PER B717 AMM 33-51-01. (LP #4048883)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,023 hrs · 43,228 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND THE SIDE EXIT LIGHTS INOPERATIVE ON L1, R1 DOORS & FWD OVERWING L&R DOORS. THE EMERGENCY LIGHT BATTERY B5-118 WAS REPLACED IAW B717 AMM 33-51-03 000-082. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE · airframe 60,754 hrs · 42,988 cycles

THE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 10. MAINTENANCE FOUND SPLICE FOR EMERGENCY LIGHT TO BE BROKEN. AFTER RESPLICE, THE LIGHT OPERATIONAL CHECK FAILED. RELAMPING BOTH EMERGENCY LIGHTS DID NOT CORRECT THE PROBLEM. THE EEP LIGHTS WERE DEFERRED PER MEL 33-51-01A AND PLACARDS WERE INSTALLED. ON 21NOV22 IN MCI, THE CABIN EMERGENCY POWER SUPPLY AT ROW 10 WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE MEL AND PLACARD WAS REMOVED. (LP #9419827)

Part: NONE — NONE · airframe 60,664 hrs · 42,902 cycles

THE EMERGENCY EXIT LIGHT OVER THE AFT CABIN BULKHEAD DOOR AND THE TAIL COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-116 PER B717 AMM 33-51. (LP #9639470)

Part: NONE — NONE · airframe 59,875 hrs · 42,178 cycles

THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20B. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20B PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #2320352)

Part: NONE — NONE · airframe 59,875 hrs · 42,178 cycles

THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20A. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20A PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #2320351)

Part: NONE — NONE · airframe 59,139 hrs · 41,520 cycles

THE EMERGENCY EXIT LOCATOR (SIGN) AT L2-791 BY SEAT ROW IA, ON THE CEILING IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE POWER SUPPLY B5-259. THE EMERGENCY EXIT LOCATOR L2-791 NOW CHECKS GOOD REF B717 AMM 33-51. (LP #8550478)

Part: NONE — NONE · airframe 60,297 hrs · 42,576 cycles

ESTABLISHING DTE RESTRICTION FOR ER/A 594509-14. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM THE APPROVAL DATE. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONT SERVICE BEYOND THIS LIMIT. REPAIR IS APPLIED TO RUDDER SN 55010 INSTALLED. ASSOCIATED ER/A 00-594509 ADDED FOR AC 9503. ERA IS NOW AT REVISION LEVEL 'A', THIS LP MAY BE CLOSED. ALL FOLLOW ON ACTION IS PROVIDED VIA LP 1969671. TERMINATED LOG PAGE PER ENGINEERING COMMENTS ON LINE 4. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 13SEP22 AND LOG COMMENTS. (LP #1969666)

Part: NONE — NONE · airframe 60,297 hrs · 42,576 cycles

REPEAT INSPECTION PER ER/A 594509-14 REQUIRED EVERY 3000FC AFTER REPAIR INSTALLATION. REPAIR IS APPLIED TO RUDDER SN 55010 INSTALLED. ASSOCIATED ER/A 00-594509 ADDED FOR AC 9503. REDEFERRED LOG TO QC, ESTABLISHED MONITOR INSP. ERA 594509-14 REV A IS NOW CURRENT. NEW FOLLOW ON ACTION IS REQUIRED. CONTINUE TO ACCOMPLISH SECTION II REPEAT INSPECTIONS EVERY 3000 CYCLES AFTER SECTION I, UNTIL COMPLETION OF SECTION III. A CCOMPLISH SECTION III AT NEXT C-CHK, NTE 02OCT2023. (LP #1969671)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,580 hrs · 40,144 cycles

THE EMERGENCY EXIT SIGN ABOVE THE AFT CABIN DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7569558)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,375 hrs · 39,989 cycles

THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT SIGN LIGHTS AT THE GALLEY SERVICE DOOR AND CABIN ENTRANCE DOOR, THE LOWER EXIT SIGN LIGHTS AT RT & LT FWD OVER WING EXIT DOORS, AND THE TAIL COMPT ESCAPE PATH LIGHTING WERE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES B5-118, B-119, AND B5-260 PER B717 AMM 33-51. OPERATIONAL TEST OF EMERGENCY LIGHTS SYSTEM CHECKED GOOD. (LP #7297451)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,845 hrs · 39,573 cycles

THE TAIL CONE SECTION EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 AND B5 -116 BATTERY PACKS AND THE OPERATIONAL CHECKS WERE GOOD, PER B717 AMM 33-51.

Part: DRIVE ASSY — DAMAGED (SLAT SYSTEM) · airframe 56,246 hrs · 39,053 cycles

THE CREW DIVERTED THE AIRCRAFT INTO IAH FOLLOWING A "SLAT DISAGREE" UPON SLAT EXTENSION. IAH HAS A LONGER RUNWAY THAN HOU. CORRECTIVE ACTION: MAINTENANCE FOUND THE NR 1 RIGHT HAND SLAT DRIVE MECHANISM DAMAGED. REPLACED THE RIGHT WING SLAT DRIVE AND ACTUATOR ASSEMBLY, PER B717 AMM 27-81.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,235 hrs · 39,045 cycles

EMERGENCY LIGHT LENS AT 29L IS MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 55,649 hrs · 38,521 cycles

THE R1 DOOR SLIDE LANYARD WAS FOUND TO BE INSTALLED IMPROPERLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REINSTALLED THE R1 DOOR SLIDE LANYARD CORRECTLY PER B717 AMM 25-61. (LP #6535579)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,856 hrs · 37,902 cycles

THE EMERGENCY EXIT LIGHTS ABOVE THE AFT DOOR AND IN THE AFT ACCESSORY COMPARTMENT ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

OUT OF LIMITS- CORROSION IN ACCESS 620 CB, 620AT AND 620 DT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). ACCES PANEL 620CB WAS REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-23-01-01 (SHEET 6) (ITEM 465J) AND ACCES PANNEL 620AT AND 620DT WERE REPLACED AND PART NUMBER WAS VERIFIED PER IPC 57-22-01-01 (SHEET 2) (ITEM 20). (LP1157914)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

OUT OF LIMITS - CORROSION IN ACCESS 520FT, 520GB, 520DT, 520CT, 520CB AND CENTER FUEL TANK UPPER ACCES PANNEL, SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AI). ALL PANELS WERE REPLACED. (LP1157907)

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 53,836 hrs · 37,114 cycles

AWR, HIDDEN CORROSION (IN REF NRC S/N 00283): CORROSION WAS FOUND ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 2. CORROSION ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 225 (EHV) WAS REPAIRED PER ETI-17-19-102 REV. 5 STEP 14 AND ER/A 579399-14 REV. ORIG. (LP1156942)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

INITIAL INSPECTION: SEVERAL CORROSION ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 CORROSION ON LONGERON 30 BTW STA Y=894-1076 WAS REMOVED PER SRM 51-10-04-0G PAR 26 (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR.5 FIG 3(SHEET 1 AND 2). ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARTMENT ORIGINAL THICKNESS IS (0.080") THEREFORE ITS OUT OF LIMITS PER SRM 53-00-00-1A ALLOWABLE DAMAGE PAR 4 FIG 103. (LONGERON 30 BTW STA Y=895-1076 WAS REPLACED PER SRM 53-20-05-01-3 FIG 1 ITEM 8,51-41-05-0G AND 51-41-02-0G)(INTERCOSTAL AT LONG 30 STA = 1022-1040 WAS REPLACED WITH NRC 00210)(SPLICES 4EAS ON LONGERON 30 BTW STA 889 NTO STA 1053 WERE REPLACED WITH NRC 00190)(FRAME CLIP STA 974 LONG 29R TO 24L WAS REPLACED WITH NRC 00152)(ELONGATED FASTENER HOLE WAS REPAIRED WITH NRC 00496). (LP1156530)

Part: FASTENER — DAMAGED (TAILCONE) · airframe 53,836 hrs · 37,114 cycles

INITIAL INSPECTION: DAMAGED INTERNAL HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE CUTOUT. NEW HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE WERE INSTALLED PER AMM TAILCONE ADJUSTED WAS PERFORMED AND TEST OK PER AMM 53-52-01-830-802. (LP1155413)

Part: SKIN — DENTED (AILERON TAB) · airframe 53,836 hrs · 37,114 cycles

SEVERAL DENTS ( 7 EAS ) ON RH WING AILERON CONTROL TAP UPPER SKIN BTW STATION XAC=3.5 TO XAC=48.2. RT AILERON CONTROL TAB UPPER SKIN DENT 7 WAS REPAIRED PER SRM 51-70-02-2R PROCEDURE 6 REPAIR 6. TAP TEST INSPECTION WAS PERFORMED AFTER REPAIR AND NO DISBONDS WERE FOUND PER SRM 51-70-02-0G, PAR 16 AND NDT SPM PART 5,05-10-02.001. RT AILERON CONTROL TAB BALANCE WAS PERFORMED PER SRM 51-60-01-0G PAR. 10 TO 14 WEIGHT TABLE 9 IS 9.58 LB, WEIGHT TABLE 12 IS 0.52 IT IS WITHIN LIMITS. RT WING AILERON CONTROL TAB WAS INSTALLED PER AMM 27-10-02-401.AND TOOL USED TORQUE P/N QD1R50 S/N 0115802894 D/D 18-DEC-19 TORQUE P/N QD2R1000 S/N 111650395 ADJUSTMENT OF THE AILERON CONTROL TAB AND FUNTIONAL TEST OF THE AILERON AND TAB SYSTEM WERE PERFORMED PER AMM 27-10-00- 730-801 AND AMM 27-10-00-720-803, DETAILED DIMENSIONAL INSPECTION OF THE AILERON CONTROL TAB WAS PERFORMED PER AMM 27-10-02-220-801. TOOL USED PROTACTOR P/N 950-317 S/N 17060779. SEE LOG SHEET FOR MORE INFO. (LP1155402)

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,836 hrs · 37,114 cycles

INITIAL INSPECTION: CRACKED FUSELAGE SKIN STA Y=97 ON NLG DOOR CUT OUT LT AFT HINGE DOOR. SUMMARY IN REF OF NRC 00039 AREA WAS REPAIRED PER SRM 53-10-01-2R-11, SRM 51-41-02-0G AND 51-41-05-0G. (LP1153816)

Part: HANDLE — OUT OF ADJUST (TAILCONE) · airframe 53,836 hrs · 37,114 cycles

AWR: DURING CHECK OF THE TAILCONE RELEASE SYSTEM, TAILCONE WAS NO RELEASED WITH "EMERGENCY OPERATING HANDLE" OF THE PASSENGER AFT ENTRANCE DOOR PER 5352-2001, STEP 2. NRC 00534 EMERGENCY OPERATING HANDLE OF THE PASSENGER AFT ENTRANCE DOOR WAS ADJUSTED AND TEST OK PER AMM 53-52-01-830-802. (LP1153332)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

INITIAL INSPECTION: CORROSION ON FUSELAGE SKIN BTW STA Y= 1022 - 1035 AND LONG 23L - 26L. CORROSION LEVEL 2 IN REF OF NRC 00063 AREA WAS REPAIRED PER ER/A 578990-14 REV ORIGINAL AND ETI-17-19-085 REV 3. TIME CONTROLLED ITEMS: ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY 8,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR, AND FOLLOWED UNDER LOG PAGE 1150080. ASSOCIATED ER/A 14-578990 ADDED FOR AC 9503. (LP1153204)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON FRAME AFT AND FWD SURFACE AT STA 1022 BTW L28R TO L28L AT AFT CARGO COMPARMENT (C2 ). NRC 00156: CORROSION LEVEL 2, CORROSION ON FRAME AFT AND FWD SURFACE AT STA 1022 BTW L29R TO L29L WAS REMOVED PER SRM 51-10-04-0G PAR. 26. (LP #1150161)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON FRAME OF STA 974 FROM L29R TO L28L AT AFT CARGO COMPARMENT (C2). NRC 00152: CORROSION LEVEL 2, CORROSION WAS REMOVED PER SRM 51-10-04-0G PAR 26. (LP #1150270)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 AFT CARGO COMPARMENT (C2). NRC 160: CORROSION LEVEL 2, CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 WAS REMOVED PER SRM 51-10-04-0G PAR 26. (LP #1149264)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,836 hrs · 37,114 cycles

BENT ON AFT COMPARMENT CARGO DOOR JAMB STA 992 BTW L25R TO L24R (FUS). NRC 00089: A CRACK OF 0.500" IN LENGTH, WAS FOUND AFTER FORMING. CRACK ON AFT COMPARMENT CARGO DOOR JAMB STA 992 BTW L25R TO L24R WAS REPAIRED PER SRM 53-20-15-2R-4 PAR. 4. (LP #1148784)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON INTERCOSTAL AT LONG 30 STA=1022-1040 AT AFT CARGO COMPARMENT (REF NRC SN 146) (C2). NRC 00210: CORROSION LEVEL 2, INTERCOSTAL AT LONG 30 STA=1022-1040 WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #1149302)

Part: HINGE — CORRODED (APU DOOR) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON LT APU DOOR UPPER SECTION HINGE (FUS). NRC 0064: CORROSION LEVEL 2, CORROSION IN UPPER HINGE ON LT APU DOOR WAS REMOVED PER SRM 51-10-04-0G PAR. 26. HINGE ON LT APU DOOR WAS REPLACED PER AMM 52-45-01-400-801. (LP #1149074)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,836 hrs · 37,114 cycles

CRACKED ON CUT OUT FRAME AT STA 47 X=11, X=-11 LH NOSE LANDING GEAR. NRC 00159: AREA WAS REPAIRED PER SRM 53-10-14-2R-2 FIG 201. (LP #1146437)

Part: VANE — WORN (TE FLAP) · airframe 53,836 hrs · 37,114 cycles

WEAR ON TRAILING EDGE OF AFT MOVABLE FLAP VANE AT LT WING. NRC 00241: TRAILING EDGE TIP OF AFT MOVABLE FLAP VANE AT LT WING WAS REPLACED PER DWG. #5910040 REV. BN AND SRM 51-41-02. (LP #1146810)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,836 hrs · 37,114 cycles

CRACKED ON CUT OUT FRAME AT STA 47 X=11, X=-11 RH NOSE LANDING GEAR. NRC 00161: AREA WAS REPAIRED PER SRM 53- 10-14-2R-2 FIG 201. (LP #1146419)

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROCION SPLICES (4 EA) ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARMENT (REF NRC SN 146)(C2). NRC 00497: CORROSION LEVEL 2, CORROSION ON SPLICES (4EAS) ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARMENT WERE REMOVED PER SRM 51-10-04 PAR. 26 PAR. D. (LP #1146131)

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON INTERNAL FINGER DOUBLER BTW STA Y=927 TO Y=954 AND LONG 30 TO 29L AT AFT CARGO COMPARTMENT. (C2). NRC 00497: CORROSION LEVEL 2, INTERNAL FINGER DOUBLER BTW STA Y=927 TO Y=954 AND LONG 30 TO 29L AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-41-02-0G AND 51-40-08-0G. (LP #1146042)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON CUSP MEMBRANE (WEB) FROM Y= 965 TO Y=986 RT SIDE (PAX CAB). NRC 00510: CORROSION LEVEL 2, CORROSION WAS REMOVED ON STA Y=979 TO Y=981 PER SRM 51-10-04-0G PAR 26, A10X MAGNIFIED INSPECTION WAS PERFORMED AND A CRACK OF 0.380" LENGTH WAS FOUND AND REPAIRED PER SRM 53-00-00-2R -2. (LP #1145878)

Part: FLOOR PANEL — PUNCTURED (PAX CABIN) · airframe 53,836 hrs · 37,114 cycles

PUNCTURE AT PAX CABIN FLOOR PANEL #223EF. (CPAX). NRC 00488: PUNCTURE IN FLOOR PANEL #223EF WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #1142188)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION IN ACCESS 620CT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). NRC 00502: CORROSION LEVEL 2, THE UPPER WING ACCESS DOOR 620CT WAS REPLACED PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION 3. (LP #1142552)

Part: FLOOR PANEL — DEBONDED (COCKPIT) · airframe 53,836 hrs · 37,114 cycles

DISBONDED FLOOR PANEL #211ANF COCKPIT (CPIL). NRC 00401: FLOOR PANEL #211ANF WAS REPLACED AND IDENTIFIED BY A FABRICATED PANEL PER B-717-200 SRM 53-20-50-2R-3. (LP #1143068)

Part: CUSP WEB — CRACKED (BS 560-579) · airframe 53,836 hrs · 37,114 cycles

CRACKED CUSP WEB BS 560 - 579 RT SIDE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G PAR 8.

Part: CUSP WEB — CRACKED (BS 813) · airframe 53,836 hrs · 37,114 cycles

CRACK ON CUSP MEMBRANE (WEB) AT Y=813 RH SIDE. AREA WAS CLEANED PER PS 900-1-2-1NO. GVI WAS PERFORMED AND NO CORROSION WAS FOUND PER B717-200 AMM 05-21-02-210-802. CRACK WAS REPAIRED PER B717-200 SRM 53-00-00-2R AND 51-41-02-0G.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON REPAIR OF CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE (PAX CAB). NRC 00308: CORROSION LEVEL 2, MAINTENANCE FOUND CORROSION ON THE EXISITING REPAIR OF THE CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE: SO THIS REPAIR WAS REPLACED PER B717-200 SRM 53-00-55-2R-4. (LP #1137597)

Part: FLOOR SUPPORT — CORRODED (BS 1022-1076) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=20 AT CABIN PAX. (CPAX). NRC 00351: CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. MINIMUM REMAINING THICKNESS IS 0.028 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE PAR. 4 FIG. 103. FLOOR SUPPORT WAS REPLACED PER B717-200 DWG #9936656 REV AM, SRM 51-40-08-0G, 51-20-09-0G, 51-20-09-0G, 51- 41-02-0G, AND 51-41-01-0G. (LP #1137177)

Part: FLOOR SUPPORT — CORRODED (BS 1022-1076) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=-20 AT CABIN PAX. CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. REMAINING THICKNESS IS ONLY 0.025 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE PAR. 4 FIG. 103. FLOOR SUPPORT WAS REPLACED PER B717-200 DWG #9936656 REV: AM, SRM 51-40-08-0G, AND 51-20-09-0G.

Part: BEAM — CRACKED (PAX DOOR) · airframe 53,836 hrs · 37,114 cycles

CRACKED BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE (L1) (PTAS). NRC 00080: BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE WERE REPAIRED PER B717-200 SRM 52-10-02-2R-13, 52-10-02-2R-8, AND 52-10-02-2R-7.

Part: CHANNEL — CRACKED (PAX DOOR) · airframe 53,836 hrs · 37,114 cycles

CRACKED CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE. (L1) (PTAS). CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE WAS REPAIRED IAW SRM 52-10-02- 2R REPAIR 3.

Part: HOUSING — CORRODED (RUDDER) · corrosion level 2 · airframe 53,836 hrs · 37,114 cycles

CORROSION ON RUDDER YOKE BEARING SUPPORT HOUSING (AMDS 2720-2004). NRC 00379: CORROSION LEVEL 2, BEARING SUPPORT HOUSING WAS REPLACED PER SRM 51-41-02-0G AND 51-41-01- 0G. (LP #1132426)

Part: FLOOR PANEL — DEBONDED (PAX CABIN) · airframe 53,836 hrs · 37,114 cycles

DEBONDED FLOOR PANEL #221LF PAX CABIN (CPAX). NRC 00403: FLOOR PANEL #221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1131537)

Part: FRAME — CRACKED (BS 889) · airframe 53,836 hrs · 37,114 cycles

CRACK ON RH WINDOW RING PAN STA Y=889 AT PAX CABIN. NRC 00197: CRACK ON RH WINDOW RING PAN STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.

Part: WEB — CRACKED (BS 161) · airframe 53,836 hrs · 37,114 cycles

CRACK ON WEB FROM STA 161 BTW X=-42 TO X=-44 (FUS). NRC 0366: WEB FROM STA 161 BTW X=-42 TO X=-44 WAS REPAIRED PER B717 SRM 53-00-00-2R-1 FIG. 201. (LP #1126059)

Part: SPOILER — DEBONDED (RT WING)

LARGE DISBOND.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,120 hrs · 36,600 cycles

B5-235 BATTERY WILL NOT ILLUMINATE THE EXIT SIGN OVER FWD FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACED THE BATTERY ASSEMBLY. CHECK WAS NORMAL REF B717 AMM 33-51. (LP #5513762)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,598 hrs · 36,239 cycles

ON THE SERVICE CHECK, MAINTENANCE FOUND THAT THE AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE DETERMINED THAT THE EMERGENCY LIGHT BATTERY PACK, B5-230, WAS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #4287978)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,326 hrs · 35,360 cycles

DURING A SERVICE CHECK, FOUND THE LOWER WING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE DISCOVERED A BAD POWER SUPPLY B5-119 AND REPLACED IT. OPS CHECKED GOOD IAW AMM 33-51-03, AND WDM 33-51-12.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 50,679 hrs · 34,851 cycles

SEAT TRACK CORRODED. SPLICED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-20-52-2R, PRO 5.

Part: ATTACH FITTING — CORRODED (AFT GIRT BAR) · corrosion level 2 · airframe 50,679 hrs · 34,851 cycles

THE AFT GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE IAW DWG 3936190.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 50,679 hrs · 34,851 cycles

THE FWD GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE FITTING DWG 3936190.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,315 hrs · 33,982 cycles

SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE ON AFT CATWALK. MAINTENANCE REPLACED THE LAMPS IAW AMM 33-52. OPS CHECKED GOOD.

Part: ANTENNA — ERODED (TCAS) · airframe 48,932 hrs · 33,699 cycles

L/E OF FWD TCAS ANTENNA ERODED. REPLACED THE TCAS ANTENNA IAW AMM 34-46-03.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 48,929 hrs · 33,698 cycles

FOUND NUMEROUS LOOSE FASTENERS ON VERTICAL STABILIZER REMOVABLE LEADING EDGE AT STA ZFS 52. REPAIRED REF PRI 560042-14 REV 0 AND ER/A 560042-14 REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,929 hrs · 33,698 cycles

2 SKIN CRACKS AT FASTENERS AT STA 1095, 4" ABOVE L14R ABOVE LT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,929 hrs · 33,698 cycles

SKIN CRACK AT FASTENER AT STA 1095, 4" ABOVE L14R ABOVE RT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 48,929 hrs · 33,698 cycles

VERTICAL STAB LEADING EDGE LOWER FASTENERS ARE LOOSE AT STA ZFS 52. COMPLIED WITH PRI 560026-14 REV 0 AND REV 1. REPAIRED REF ER/A 560026-14 REV ORIG.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,929 hrs · 33,698 cycles

CORROSION ALONG THRESHOLD SILL FROM STA 370 TO 427. REPAIRED PER SRM 53-20-15-2R PROCEDURE 6.

Part: SKIN — DAMAGED (BS 813-898) · airframe 48,406 hrs · 33,285 cycles

SKIN DAMAGED BS 813 - 898. LONGERON 15 - 18L. REMOVED, FABRICATED, AND REPLACED THE SKIN PANEL IAW ER/A 557708-14, AND SRM 51-41-02 / 51-41-05.

Part: SKIN — DAMAGED (BS 813-899) · airframe 48,406 hrs · 33,285 cycles

SKIN WRINKLED BETWEEN BS 813 AND 899 LT SIDE ABOVE WING AND BELOW WINDOW.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,220 hrs · 32,412 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS DAMAGED. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 47,070 hrs · 32,319 cycles

DURING LINE CHECK, THE PILOT FOUND HE COULD NOT CONTROL THE EMERGENCY LIGHTS IN THE CABIN AT THE L1 DOOR, IT WOULD REACT WHEN CONTROLLING CABIN LIGHTING. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,070 hrs · 32,319 cycles

DURING LINE CHECK, THE PILOT FOUND HE COULD NOT CONTROL THE EMERGENCY LIGHTS IN THE CABIN AT THE L1 DOOR. IT WOULD REACT WHEN CONTROLLING CABIN LIGHTING. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,280 hrs · 31,671 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,108 hrs · 31,526 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,948 hrs · 31,379 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,535 hrs · 31,047 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES AND AT THE AFT CABIN DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (BS 210) · airframe 50,257 hrs · 34,586 cycles

SKIN DAMAGED AT BS 210, STRINGER 25R. REPAIRED THE SKIN IAW PRI 544069-14, REV 0, 1, & 2.

Part: SKIN — DENTED (AILERON TAB) · airframe 53,845 hrs · 37,120 cycles

DENT INSPECTION RT AILERON CONTROL TAB, LOWER SKIN - QTY 3, 1) 6" FROM I/B, 5.5" FROM T/E, 2) 7" FROM I/B, 5" FROM T/E, 3) APPROX 8" FROM I/B, 4" FROM T/E. AREA TO DENTS ON RT AILERON CONTROL TAB LOWER SKIN WERE REPAIRED PER SRM 51-70-02-2R PROCEDURE 6 REPAIR 6. AND WEIGHT AND BALANCE WAS PERFORMED WITH NRC 00491 LP 1155402. (LP2118123)

Part: MOUNT BRACKET — CRACKED (CABIN) · airframe 44,392 hrs · 30,232 cycles

OVERHEAD EMER EXIT LIGHT MOUNT BRACKET CRACKED AT ROW 1. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,392 hrs · 30,232 cycles

AFT OTBD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 44,392 hrs · 30,232 cycles

R2 DOOR EMER EXIT SIGN COVER LOOSE. R & R COVER IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,930 hrs · 29,228 cycles

R1 LOWER EMER EXIT IDENTIFIERS INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,930 hrs · 29,228 cycles

L1 LOWER EMER EXIT IDENTIFIERS INOPERATIVE. R & R BATTERY IAW AMM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FORMER CRACKED AT BS 674, LONGERON 25R. REPAIRED FORMER IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FORMER CRACKED AT BS 696, LONGERON 26R. R & R FORMER IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CANTED KEEL AREA FORMER CRACKED AT BS 694, LONGERON 26L. R & R FORMER IAW DWG & EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CANTED KEEL AREA FORMER CRACKED AT BS 715, LONGERON 27L. R & R FORMER IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FORMER CRACKED AT BS 674, LONGERON 25L. R & R FORMER IAW EA.

Part: LENS — DIRTY (CABIN) · airframe 42,930 hrs · 29,228 cycles

RIGHT EMER LIGHT LENS DIRTY IN AFT ACCESSORY INBD OF AIR BOX. CLEANED LENS IAW AMM.

Part: SUPPORT BRACKET — CRACKED (TE FLAP) · airframe 42,930 hrs · 29,228 cycles

LEFT WING FLAP MOVEABLE VANE CARRIAGE SUPPORT BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT BS 1116, LONGERON 14L. R & R FORMER IAW DWG.

Part: STRAP — BROKEN (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD LINER, LOWER ATTACH STRAP BROKEN AT BS 813. R & R STRAP IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN AFT PRESS BULKHEAD DOOR JAMB LT SIDE TIE FITTING CRACKED 19TH FROM FLOOR. R & R FITTING IAW DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 42,930 hrs · 29,228 cycles

LEFT WING LE SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

AFT PRESS BULKHEAD DOOR JAMB RT SIDE TIE FITTING CRACKED 17" FROM FLOOR. R & R FITTING IAW DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER LINER ATTACH STRAP CRACKED AT BS 813. R & R STRAP IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN AFT PRESS BULKHEAD DOOR JAMB RT SIDE TIE FITTING CRACKED 37" FROM FLOOR. R & R FITTING IAW DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 44,392 hrs · 30,232 cycles

FUSELAGE SKIN DOUBLER CORRODED BETWEEN BS 927 TO 946, BETWEEN LONGERON 29R TO 30R. R & R DOUBLER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

KEEL BEAM AREA FITTING CRACKED AT BS 737, LONGERON 30. R & R FITTING IAW DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

WEB MEMBRANE CORRODED AT BS 217, RBL 11. REPAIRED WEB IAW SRM.

Part: DOOR — CRACKED (RT WING) · airframe 42,930 hrs · 29,228 cycles

RIGHT WING FIXED LE DOOR CRACKED. R & R DOOR IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

LEFT WW FWD DOOR CUT OUT INBD FITTING CRACKED. R & R FITTING IAW DWG.

Part: TEE FITTING — CRACKED (RT MLG WW) · airframe 42,930 hrs · 29,228 cycles

RIGHT WW FWD DOOR CUT OUT INBD FITTING CRACKED. R & R TEE FITTING IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

SEAT TRACK CORRODED BETWEEN BS 1022 TO BS 1053, LBL 44.5. R & R SEAT TRACK IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FRAME STRAP DOUBLER ANGLE CORRODED AT BS 1022, BETWEEN LBL 12 TO RBL 12. R & R ANGLE IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FORWARD FACE OF PRESS BULKHEAD WEB T ANGLE CORRODED AT BS 1022, BL 0. R & R T ANGLE IAW DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

AFT PRESS BULKHEAD DOUBLER CORRODED LOWER SIDE BL 0. R & R DOUBLER IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

SEAT TRACK CORRODED BETWEEN BS 908 TO 986, RBL 44.5. R & R SEAT TRACK IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CABIN FLOOR WEB CRACKED BETWEEN BS 165 TO BS 170, BETWEEN LBL 8 TO RBL 7. REPAIRED WEB IAW SRM & DWG.

Part: SLAT TRACK — CRACKED (RT WING) · airframe 42,930 hrs · 29,228 cycles

RIGHT WING INBD SIDE OF THE NR 12 SLAT TRACK ON SLAT SIDE ANGLE CRACKED. R & R NR 12 SLAT TRACK IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

R1 DOOR GIRT BAR FLOOR ATTACH FITTING FWD & AFT ARE CORRODED BETWEEN BS 160 TO BS 200. R & R FITTING IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO RBL 22. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 148.55 TO 200, RBL 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 133. 425, BETWEEN RBL 34 TO RBL 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 133 TO 200, RBL 7. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 7 TO RBL 8. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 14 TO LBL 28. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, LBL 9. R & R SUPPORT IAW DWG.

Part: LENS — CRACKED (CABIN) · airframe 42,930 hrs · 29,228 cycles

OVERWING EMER LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 238, BL 0. R & R SUPPORT IAW DWG.

Part: LENS — CRACKED (CABIN) · airframe 42,930 hrs · 29,228 cycles

L1 EMER LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, LBL 13. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

R1 DOOR FWD CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO BS 200. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

L1 DOOR FLOOR SUPPORT CORRODED BETWEEN BS 160 TO BS 200, LBL 51. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

INTERCOSTAL WEB CORRODED AT BS 219, BETWEEN RBL 50 TO RBL 55. R & R WEB IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 160, BETWEEN LBL 7 TO RBL 8. R & R SUPPORT IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

GALLEY FLOOR MOUNTING FITTING CORRODED AT BS 217, RBL 11. R & R FITTING IAW DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR ATTACH PAN CORRODED BETWEEN BS 148 TO BS 160. R & R PAN IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 160 TO 200, LBL 7. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 133.425, RBL 34. R & R SUPPORT IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 42,930 hrs · 29,228 cycles

R1 EMER LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 7 TO RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, RBL 55. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

SEAT TRACK CORRODED AT BS 200, RBL 44. REPAIRED SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 44 TO RBL 54. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 542 TO BS 554, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (BS 218) · airframe 42,930 hrs · 29,228 cycles

RIGHT CUSP WEB CRACKED AT BS 218. REPAIRED THE CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (BS 969) · airframe 42,930 hrs · 29,228 cycles

LEFT CUSP WEB CRACKED AT BS 696. REPAIRED THE CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CORRODED BETWEEN BS 579 TO 598. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CRACKED AT BS 800, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CORRODED AT BS 723, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 423, RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CRACKED AT BS 715, LBL 55. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CORRODED BETWEEN BS 409 TO 410, LBL 58. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 636 - 655. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 626, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 655 TO 715, RBL 58. REPAIRED CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CORRODED AT BS 460, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CORRODED BETWEEN BS 535 TO 541, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

CUSP WEB CRACKED AT BS 655, LBL 50. REPAIRED CUSP WEB IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,930 hrs · 29,228 cycles

EMERGENCY LIGHT BATTERY CHARGER B5-118 INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,930 hrs · 29,228 cycles

EMERGENCY LIGHT BATTERY CHARGER B5-227 INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,930 hrs · 29,228 cycles

MAIN CABIN FRAME CRACKED AT BS 696, RT SIDE. R & R FRAME IAW SR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,392 hrs · 30,232 cycles

MAIN CABIN FRAME CRACKED AT BS 696, RT SIDE. R & R FRAME IAW SRM.

Part: CUSP WEB — CRACKED (BS 579-700) · airframe 42,930 hrs · 29,228 cycles

RIGHT MAIN CABIN CUSP WEB BAFFLE CLIPS CRACKED BETWEEN BS 579 TO 700. REPAIRED CLIPS IAW SRM & DWG.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,970 hrs · 28,617 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,624 hrs · 28,392 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 40,370 hrs · 27,592 cycles

L1 DOOR INTERNAL STRUCTURE BETWEEN BEAM 4 & 5, AFT OF HANDLE INTERCOSTAL CRACKED. R&R INTERCOSTAL IAW SRM & DRAWING.

Part: PANEL — CRACKED (RT WING) · airframe 40,370 hrs · 27,592 cycles

RT WING PANEL FWD OF INBD BUTE DOOR STATION 111 CRACKED. R&R PANEL IAW SRM & DRAWING.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 40,370 hrs · 27,592 cycles

L1 DOOR INTERNAL STRUCTURE BEAM NR 6 CRACKED AROUND FASTENER. REPAIRED ANGLE IAW SRM & DRAWING.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 40,370 hrs · 27,592 cycles

EMPENNAGE CATWALK CEILING PANEL ATTACH BRACKET CRACKED AT 12 O'CLOCK POSITION. R&R ANGLE IAW SRM & DRAWING.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 40,370 hrs · 27,592 cycles

EMPENNAGE COMPARTMENT LT SIDE CANTED FRAME REPAIR CRACKED AT FS 1225 AT 11 O'CLOCK POSITION. R&R PANEL IAW SRM.

Part: PANEL — CRACKED (LT WING) · airframe 40,370 hrs · 27,592 cycles

LT WING FWD OF INBD BUTE DOOR PANEL CRACKED AT STATION 111. R&R PANEL IAW SRM & DRAWING.

Part: OUTLET — CRACKED (APU) · airframe 40,370 hrs · 27,592 cycles

LT SIDE OF FS LT ACM EXHAUST DUCT OUTLET CRACKED. REPAIRED OUTLET IAW SRM.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 41,417 hrs · 28,249 cycles

L1 DOOR SLIDE GIRT BAR LT SIDE HARD TO ATTACH. LUBRICATED GIRT BAR IAW MT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,367 hrs · 26,981 cycles

LOWER FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER AMM.

Part: LONGERON — DAMAGED (FUSELAGE)

LONGERON 30, STA 927 TO 946, HOLES ELONGATED. ACCOMPLISHED LONGERON 30 DOUBLER REPAIR PER B717 SRM 53-30-03, 53-03-01, 53-10-04 AND SPM 06-10-01-001.

Part: STRUCTURE — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER AREA, CORROSION. ACCOMPLISHED DOOR CUTOUT LOWER AREA SPLICE REPAIR PER B717 51-20-09, 51-41-02.

Part: STRUCTURE — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER AREA, CORROSION. ACCOMPLISHED DOOR CUTOUT LOWER AREA SPLICE REPAIR PER B717 53-20-15.

Part: STRUCTURE — CORRODED (FUSELAGE)

FWD CARGO DOOR CUTOUT LOWER AREA, CORROSION. ACCOMPLISHED DOOR CUTOUT LOWER AREA REPLACEMENT PER B717 SRM 51-20-09, 51-10-04, 51-41-02.

Part: STRINGER — CORRODED (FUSELAGE)

AFT CARGO BAY, STA 927 TO 947, LONG L30, CORROSION. ACCOMPLISHED L30 SPLICE REPAIR PER B717 SRM 51-41-02, 53-20-05 AND 51-10-04.

Part: STRINGER — CORRODED (FUSELAGE)

AFT CARGO BAY, STA 908 TO 927, LONG L30, CORROSION. ACCOMPLISHED L30 SPLICE REPAIR PER B717 SRM 53-20-05.

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: LIGHT — MALFUNCTIONED (CABIN)

OVER WING EMERGENCY EXIT LIGHTS REMAIN ON WHEN POWER REMOVED FROM AIRCRAFT. CYCLED SWITCH PER MAINTENANCE CONTROL REQUEST.

Part: COVER — MISSING (CABIN)

COVER MISSING ON EMERGENCY PATH LIGHTING AT ROW 3. INSTALLED EMERGENCY PATH LENS COVER AT ROW 3 IAW 33-51.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

INTERGRANULAR CORROSION FUSELAGE INTERNAL RIGHT SIDE INTERCOSTAL AT CUSP LINE BETWEEN STA 465 AND 484. CUT OUT DAMAGED SECTION BETWEEN STA 465 AND 484 RT CUSP LINE WEB AREA. FABRICATED DOUBLER REPAIR AND FILLER REPAIR FROM T7075T6, TREATED, PRIMED AND INSTALLED.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

INTERGRANULAR CORROSION FUSELAGE INTERNAL RIGHT SIDE INTERCOSTAL AT CUSP LINE BETWEEN STA 484 AND 503. CUT OUT DAMAGED SECTION BETWEEN STA 484 AND 503 RT CUSP LINE WEB AREA. FABRICATED DOUBLER REPAIR AND FILLER REPAIR FROM T7075T6, TREATED, PRIMED AND INSTALLED REF B717 DWG SG09530003.

Part: FASTENER — UNKNOWN (CARGO BAY)

TWELVE (12) BLIND HUCK BOLTS INSTALLED IN AFT UPPER CORNER OF C-1 DOOR CUTOUT. REMOVED FASTENERS AT FWD CARGO COMPARTMENT DOOR, COLD WORKED HOLES. ACCOMPLISHED HFEC, REINSTALLED FASTENERS PER EA 17-53-00764D REPAIR.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

INTERGRANULAR CORROSION FUSELAGE INTERNAL RIGHT SIDE INTERCOSTAL AT CUSP LINE BETWEEN STA 446 AND 465. CUT OUT DAMAGED SECTION BETWEEN STA 446 AND 465 RT CUSP LINE WEB AREA. FABRICATED DOUBLER REPAIR AND FILLER REPAIR FROM T7075T6, TREATED, PRIMED AND INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN FLOOR STA 200 TO STA 210, RBL 22 SEAT TRACK CORRODED. CUT OUT DAMAGED SECTION BETWEEN STA 200 AND 267, RBL 22. INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE PER AIRTRAN EA 17-53-01981IR AND DC9 SRM 53-05 FIG 4F.

Part: SKIN — GOUGED (RT WING)

RIGHT WING FIXED LEADING EDGE O/B STA XW536.86 HAS DEEP GOUGE FROM SLAT END. REMOVED FIXED LEADING EDGE RIGHT WING O/B STA XW530.86 FROM SLAT END. WELDED RT WING TIP SUPPORT, VERIFIED THICKNESS RESTORED PER EA17-57-01982IR, TREATED, PRIMED, TOP COAT, RE-INSTALLED FIXED LEADING EDGE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO DOOR JAMB AREA HAS CORROSION FROM STA 370-427. CUT OUT DAMAGED LOWER SECTION AND INSTALLED NEW LOWER SECTION AND SPLICES, REPAIR PER REF B717 SRM 53-20-15 REPAIR 6.

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.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FUSELAGE INTERNAL RT SIDE INTERCOSTAL AT CUSP LINE BETWEEN STA 598 AND 617 HAS SPOTS OF SURFACE CORROSION. INSTALLED CUSP LINE REPAIR BETWEEN 598 AND 617 AS PER B717 DWG SG09530003 AND SRM 51-10-04.

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: STRUCTURE — CRACKED (AC BAY)

AFT ACCESSORY COMPARTMENT LEFT VENT BOX AFT I/B CORNER PREVIOUS REPAIR CRACK. FABRICATED NEW DOUBLER REPAIR AT AFT ACCESSORY COMPARTMENT LT VENT BOX AFT I/B CORNER, PER B717 SRM 51-20-09 / 51-41-02.

Part: CONTROL QUADRANT — BROKEN (COCKPIT)

CAPTAIN'S FOOT PEDAL ADJUSTMENT BROKE LOOSE AND PEDALS NOT AT FULL EXTENSION WITH NO ADJUSTMENT BACK AVAILABLE. REMOVED & REPLACED RUDDER PEDAL ADJUSTMENT QUADRANT ASSEMBLY. CHECKS GOOD IAW MM 27-21.

Part: SKIN — DENTED (BS 365-415)

ACFT DAMAGE FWD ABOVE CARGO DOOR FOUR FOOT SCRATCH, DENT DUE TO BAGGAGE CART. CUT OUT DAMAGED AREA IAW EA 17-53-010764B. PERFORMED HFEC AT ALL OPEN HOLES AND CUT OUT OF DAMAGE AREA IAW NT SRM 06-10-01. NO CRACKS NOTED. FAB REPAIR DOUBLERS, INSTALLED DOUBLERS AND 1 FELLE IAW EA 17-53-00764B.

Part: LANYARD — PULLED (EVAC SLIDE)

L1 DOOR SLIDE LANYARD IS PULLED. BOTH PINS ARE PULLED ON SLIDE PACK. REMOVED AND REPLACED L1 DOOR SLIDE PACK IAW B717 M/M 25-61.

Part: SKIN — DAMAGED (FWD CARGO DOOR)

BAG CART HIT FORWARD CARGO DOOR OPENING. CUT OUT DAMAGE AREA IN SKIN, DOUBLER AND TITANIUM DOUBLER IAW B717 SRM 53-20-15 FIG 201. INSTALLED DOUBLER IAW B717 SRM 53-20-150 FIG 201. REPAIRED SEAL DEPRESSOR IAW B717 SRM 53-20-15.

Part: SKIN — DENTED (BS 229-244)

FUSELAGE LT SIDE HAS 3EA DENTS AFT OF THE L1 DOOR. ALL THREE DENTS ARE BETWEEN LONGERONS 17L AND 18L. DENT (1) IS 35 INCHES FROM L1 DOOR AND IS 1.25" WIDE X .025" DEEP, DENT (2) IS 38.25 INCHES FROM L1 DOOR AND IS 1.75" WIDE X .025" DEEP WITH A .007" GOUGE, AND DENT (3) IS 40.5 INCHES FROM THE L1 DOOR AND IS 1.375" WIDE X .019" DEEP. THE SKIN IS ALSO CREASED AT STA 237 BY THIS DENT. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN RT BETWEEN STR 18L AND 16L IAW B717 SRM 53-00-01 FIG 201. SIZE OF INTERNAL DOUBLER 26 X 3.25 INCHES AND FINGER DOUBLER 17 X 6 INCHES.

Part: SKIN — DENTED (FS 408)

DENT LOCATED FS 408 AND RT L16 MEASURES A 1.5 INCH IN DIA BY .045 DEEP, PER SRM 53-00-01 COND 3 MUST BE REPAIRED WITHIN 4500 FLT HOURS. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN RT BETWEEN STA 414.5 TO 422 AND BETWEEN L-16R TO 18R IAW B717 SRM 53-00-01 FIG 201. SIZE OF REPAIR 7.5 X 8.0 INCHES.

Part: SCHRADER VALVE — UNSERVICEABLE (NLG)

AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE, ALL QRH PROCEDURES ACCOMPLISHED, LANDING WEIGHT WAS 99,000 IBS, SINK RATE AT TOUCHDOWN 100 FPM. FOUND NOSE STRUT FLAT (ZERO PRESSURE), JACKED NOSE GEAR AND CYCLED SEVERAL CYCLES PER B717 AMM 32-30, NOSE GEAR FUNCTION CHECK NORMAL. AS PRECAUTIONARY REPLACED SCHRADER VALVE.

Part: ODOR — DETECTED (CABIN)

LAVATORY SMOKE EAD ALERT. FLIGHT ATTENDANT COMPLAINED OF ABNORMAL A/C HEAT, FAINT A/C ODOR IN COCKPIT. ISOLATED OIL ODOR TO AUXILIARY POWER UNIT. PERFORMED B717 FIM 49-50 TASK 807. CHECKED LEFT AND RIGHT WATER SEPARATOR COALESCER BAGS FOR OIL CONTAMINATION. COALESCER BAGS OK. RAN LEFT AND RIGHT AIR CONDITIONING PACKS WITH APU AND ENGINES FOR EXTENDED PERIOD OF TIME REF B717 AMM 21-00-00. NO SMOKE OR ODOR NOTED. A/C OK FOR SERVICE.

Part: PSEU — FAILED (E/E BAY)

FOUND AFTER TAKEOFF AT 200-300FT PSEU FAIL ON EAD. AFTER GEAR EXTENSION, NO GREEN LIGHT ON LEFT MAIN GEAR, SECONDARY INDICATIONS ALL GREEN. REMOVED AND REPLACED PSEU IAW 717 MM 32-61-01 PAGE 401-405.