N935AT

Part: HOUSING — DIRTY (ZONE 100) · airframe 57,264 hrs · 41,984 cycles

ATB, CREW REPORTED CABIN ODOR IN AFT CABIN ON TAKEOFF CLIMB. BORESCOPE BOTH ENGINES, NO DEFECTS NOTED. INSPECTED THE BOTH PACKS COALESCER BAGS AND FOUND THE HOUSING DIRTY. PERFORMED HIGH POWER RUNS WITH SNIFFER, NTF.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,255 hrs · 41,974 cycles

RETURNED TO STL DUE TO BURNT OIL SMELL AT 300FT AFTER GEAR RETRACTION. UNABLE TO DUPLICATE ODOR AT GATE RUNNING APU OR ENGINES. GATHERING PARTS AND P-TRACK FROM CARGO TO BEGIN FURTHER EVALUATION. FOUND GLYCOL IN RAM AIR INLET. REPLACED COALESCER BAGS AND DUCT BURN OUT. NO SMELL NOTED.(7585196)

Part: LENS — WRONG PART · airframe 53,457 hrs · 38,616 cycles

PASSENGER EXIT SIGN IS MISSING THE WORD "EXIT". MISSING FROM LIGHT NEAREST CLOSET. MAINTENANCE FOUND THAT THE SIGN HAD BEEN INSTALLED BACKWARDS. ADJUSTED FWD CABIN EXIT SIGN PER B717 AMM 33-51. (LP #4601783)

Part: CUSP WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON RH CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN WAS REPAIRED PER ER/A 616043-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-616043 ADDED FOR AC 9564. (LP #0262253)

Part: SKIN — DEBONDED (LT TE FLAP VANE) · airframe 53,450 hrs · 38,610 cycles

TWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH .X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND 28.000 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE. (IN REFERENCE JOB# 020-0001) SUMMARY OF NRC 00653: AFT MOVABLE FLAP VANE LEFT WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #0260170)

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4 WAS REPAIRED PER B717 SRM 53-20-07-2R-3, 51-41-02-0G, AND 51-41-05-0G. PERFORM AN INITIAL VISUAL INSPECTION AT 25,000 CYCLES THEN EVERY 6,500 CYCLES PER B717-200 SRM 53-20-07-2R PROCEDURE 3 STEP 6, TABLE 205. (LP #0259309)

Part: SKIN — CRACKED (BS 370 L20-22) · airframe 53,450 hrs · 38,610 cycles

CRACK ON SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00227: SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER PRI 616337-14 REV 0 AND ERA 616337-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616337 ADDED FOR AC 9564. (LP #0258877)

Part: RIB — WORN (LT WING LE) · airframe 53,450 hrs · 38,610 cycles

WEAR ON RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING. SUMMARY OF NRC 00621: RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING WERE REPAIRED PER ERA 616112-14 REV ORIG SECTION 1 PERMANENT REPAIR. ASSOCIATED ERA 14-616112 ADDED FOR AC 9564. (LP #0256915)

Part: WEB — DAMAGED (BS 360-370) · airframe 53,621 hrs · 38,756 cycles

ELONGATED HOLES ON WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD). SUMMARY OF NRC 00131: WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 FIGURE 201 AND 53-00-00-2R PROCEDURE 2. (LP #0256328)

Part: DIAPHRAGM — CORRODED (BS 200-218) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA. SUMMARY OF NRC 00697: CORROSION LEVEL 2. RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA WAS REPLACED PER DWG 9936535 REV CS, PER B717-200 SRM 51-40-03-0G, 51-41- 08-0G, AND 51-41-02-0G. (LP #0254777)

Part: GUIDE VANE — PUNCTURED (RT WING TE FLAP) · airframe 53,450 hrs · 38,610 cycles

PUNCTURE ON AFT MOVABLE GUIDE VANE AT RH WING. SUMMARY OF NRC 00042: AFT MOVABLE GUIDE VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #0254635)

Part: SKIN — CRACKED (BS 1076-1087) · airframe 53,450 hrs · 38,610 cycles

CRACKS ON FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH. FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH WAS REPAIRED PER ERA 616042-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. ASSOCIATED ERA 14-616042 ADDED FOR AC 9564. (LP #0254610)

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN. SUMMARY OF NRC 00493: CORROSION LEVEL 2. RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5. (LP #0256135)

Part: DIAPHRAGM — CRACKED (BS 257) · airframe 53,450 hrs · 38,610 cycles

CRACK AND PUNCTURE ON DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00707: DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 AND 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 B FIG 102. (LP #0248230)

Part: FLOOR SUPPORT — CORRODED (FRM 160-200) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON CABIN FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44.5 TO -55; AND X=-12 STA Y=210. SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44.5 TO -55; AND X=-12 STA Y=210 WERE REPLACED PER DWG 9956534 REV BW AND PER B717 SRM 51-41-02-0G PAR 4 AND 51-41-05-0G PAR 8. (LP #0245537)

Part: WEB — CORRODED (BS 156) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN. SUMMARY OF NRC 00488: CORROSION LEVEL 2. DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0243883)

Part: FRAME — CRACKED (FRM 64) · airframe 53,450 hrs · 38,610 cycles

CRACK ON FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W. SUMMARY OF NRC 00705: FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1. (LP #0245021)

Part: TEE ANGLE — CORRODED (BS 1053 L30) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00559: CORROSION LEVEL 2. ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0242409)

Part: PAN — CRACKED (BS 427) · airframe 53,450 hrs · 38,610 cycles

CRACK ON PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00226: PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0242328)

Part: FRAME — CRACKED (BS 1200 L17-18L) · airframe 53,450 hrs · 38,610 cycles

CRACK ON CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE. SUMMARY OF NRC 00232: CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #0241299)

Part: SEAT TRACK — CORRODED (BS 636) · airframe 53,450 hrs · 38,610 cycles

CORROSION ON LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX. SUMMARY OF NRC 00605: LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5. (LP #0235072)

Part: LONGERON — CORRODED (BS 1050 L28R) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON LONGERON END STA Y=1050, LONG 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00654: CORROSION LEVEL 2. LONGERON END STA Y=1050, LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0234611)

Part: CUSP WEB — CORRODED (BS 489-494) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON RH CUSP WEB UPPER AND LOWER SUARFACE FROM STA Y=489 TO STA Y=494 COORDINATES X=-44 TO COORDINATES X=-60 (CAB PAX). SUMMARY OF NRC 00668: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER SURFACE FROM STA Y=489 TO STA Y=494 COORDINATES X=-44 TO COORDINATES X=-60 (CAB PAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0233255)

Part: INTERCOSTAL — CRACKED (BS 184) · airframe 53,450 hrs · 38,610 cycles

CRACK INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 AND 5 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00144: INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 AND 5 AT PASSENGER DOOR 1L WAS FABRICATED PER DOUGLAS DWG 9955763 REV K AND REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-01-0G, AND 51-41- 05-0G. (LP #0231534)

Part: CUSP WEB — CRACKED (BS 595) · airframe 53,450 hrs · 38,610 cycles

CRACK ON LH CUSP WEB LOCATED ON OUTB SEAT TRACK SPLICE AREA STA 595 AT PASSENGER CABIN. SUMMARY OF NRC 00639: LH CUSP WEB STA 595 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0229779)

Part: DOUBLER — CORRODED (BS 1053 L30) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00562: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND 51-41-02-0G AND PER B717-200 DWG 5930760 REV DL. (LP #0228593)

Part: CUSP WEB — DENTED (BS 355) · airframe 53,450 hrs · 38,610 cycles

DENT ON RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN. SUMMARY OF NRC 00400: RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIGURE 213. (LP #0227465)

Part: CUSP WEB — CORRODED (BS 636) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON LH CUSP WEB STA Y 636 AT PASSENGER CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. LH CUSP WEB STA Y 636 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2 PAR 4. (LP #0227124)

Part: BEAM — CRACKED (L1 DOOR) · airframe 53,450 hrs · 38,610 cycles

CRACK ON BEAM #1 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00138: BEAM #1 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7, FIGURE 201. (LP #0225315)

Part: WEB — CORRODED (BS 1053 L30) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON WEB (2 EA) OF STA Y=1053 LONGERON 30 AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00638: CORROSION LEVEL 2. SECTIONS OF THE WEB (PREVIOUSLY REPAIRED) WERE REPLACED PER B717-200 SRM 51-41-02-0G STEP 8 A, 51-41-05-0G STEP 8, AND 51-70-10-2R. (LP #0225822)

Part: FRAME — CRACKED (BS 1037 L17R) · airframe 53,450 hrs · 38,610 cycles

CRACK ON FRAME STA Y1037 OVER LONG 17 RH AT CPAX. SUMMARY OF NRC 00409: FRAME STA 1037 OVER LONG 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0221351)

Part: BEAM — CRACKED (BS 197) · airframe 53,450 hrs · 38,610 cycles

CRACK ON BEAM #2 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00139: BEAM #2 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0218077)

Part: CUSP WEB — CRACKED (BS 716) · airframe 53,450 hrs · 38,610 cycles

CRACK ON LH CUSP WEB STA 716 AND X44/60 AT CAB PAX. SUMMARY OF NRC 00399: CUSP WEB STA 716 AND X44/60 AT CAB PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 (FIG.221). (LP #0216965)

Part: SEAT TRACK — CORRODED (BS 215-256) · corrosion level 2 · airframe 53,450 hrs · 38,610 cycles

CORROSION ON SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN WAS REPAIRED PER B717-200 53-20-52-2R PROCEDURE 5. (LP #0215602)

Part: FRAME — CRACKED (BS 1037 L17L) · airframe 53,450 hrs · 38,610 cycles

CRACK ON FRAME STA Y1037 OVER LONG 17 LH AT CPAX. SUMMARY OF NRC 00408: FRAME STA Y1037 OVER LONG 17 LH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. PERFORM AN GVI ON FRAME STA Y=1037 OVER LONG 17 LH AT CPAX EVERY "C" CHECK PER B717 SRM 53-20-07-2R PROCEDURE 4. (LP #0212580)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,593 hrs · 37,915 cycles

THE FORWARD OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-121 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #4094980)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,468 hrs · 37,811 cycles

THE OVERHEAD LIGHT FIXTURE IN THE FWD GALLEY AT R1 DOOR WITH BUILT-IN EMERGENCY LIGHTING IS MISSING LENS COVER. MAINTENANCE INSTALLED THE MISSING OVERHEAD LIGHT FIXTURE LENS IN FWD GALLEY ABOVE R1 DOOR IN REF WITH B717 AMM 33-23. THIS ACTION ALSO CLEARS NEF 33-27-06 ON LOG PAGE 2904087. OK FOR SERVICE. (LP #4094901)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,424 hrs · 37,772 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT AFT CABIN. MAINTENANCE RESECURED LENS COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2902779)

Part: NONE — NONE · airframe 51,299 hrs · 36,809 cycles

THE F/O SIDE EXIT SIGN AT THE EMERGENCY ROW FELL OFF DURING TURBULENCE. MAINTENANCE RESECURED THE EXIT SIGN LENSE COVER AT THE EMERGENCY EXIT ROW CROWN. (LP #8566510)

Part: SPLICE — CRACKED (VERTICAL STAB) · airframe 51,128 hrs · 36,669 cycles

NOTED CRACK ON RT SIDE 2ND SCREW HOLE BELOW SPLICE 4NE 52.267. AFTER ACCOMPLISHMENT OF SEPARATION OF LAYERS, PERFORMED BHEC IAW STEP 14 OF AA5530-01048-02 AD 2618-10-08 & NOTED CRACK APPEARED TO BE IN SPAR RUNNING TOWARD 7 O'CLOCK. REMOVED VERTICAL STAB LEADING EDGE UP TO STEP E (1). IAW AMM 55-32-01. INSTALLED VERTICAL STAB LEADING EDGE IAW 55-32-01 UP TO RTS FOR MMR 34-32-03. PERFORMED MMR 1&2 TESTED IAW AMM 34-35-01. REMOVED VERT STAB LEADING EDGE IAW AMM 55-32-01. COMPLIED WITH 605326-14 PRI AD REV. O. C/W 605326-14 AD REV 1. C/W ERA 605326-14 REV. ORIG. ALL STEPS PRI REV. 0-1 MATCH ERA 605326-14 REV ORIG. INSTALLED VERT STAB LEADING EDGE IAW AMM 55-32-01. RTS MMR TESTED GOOD IAW AMM 34-35-01.

Part: NONE — NONE · airframe 50,449 hrs · 36,054 cycles

THE OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE FOUND A FAULTY POWER SUPPLY. THE POWER SUPPLY B5-125 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9062743)

Part: NONE — NONE · airframe 50,215 hrs · 35,833 cycles

AIRCRAFT 9564, BOTH OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHTS OVERWING BATTERY. LP 9128322

Part: BATTERY — INOPERATIVE · airframe 49,707 hrs · 35,388 cycles

THE EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY AND REPLACED THE BATTERY REF B717 AMM 33-51-01. (LP #9247536)

Part: NONE — NONE · airframe 49,524 hrs · 35,213 cycles

DURING THE SERVICE CHECK, SEVEN EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED SEVEN EMERGENCY LIGHT BATTERIES IN THE CABIN. OPERATIONAL CHECK WAS NORMAL. (LP #8635234)

Part: NONE — NONE · corrosion level 2 · airframe 49,153 hrs · 34,883 cycles

FOUND CORROSION ON INTERCOSTAL AFT CARGO BILGE AREA, AFT OF STA 1022, L29R. REPLACED PER BOEING DRAWING 9936718. CORROSION LEVEL 2. (LP #2154330)

Part: NONE — NONE · corrosion level 2 · airframe 49,146 hrs · 34,878 cycles

FOUND LIGHT CORROSION BILGE AREA AFT CARGO, STA 1022, FWD AND AFT OF STRINGER, L29 R. "M". SUMMARY SEE NRC 045-0008:5331-2001/001 00357: REPLACED LONGERON AT BILGE AREA AFT CARGO, STA 1022, STRINGER, L30 PER B712 DRAWING #5911425. CORROSION LEVEL:2 . (LP #2153238)

Part: NONE — NONE · airframe 49,146 hrs · 34,878 cycles

TAILCONE SLIDE DATA TAG STATES SLIDE IS OUT OF DATE. OVERHAUL WAS DUE IN DECEMBER 2020. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0261:2000-1002/021 00462: MAINTENANCE REPLACED THE TAILCONE SLIDE ASSEMBLY REF AMDS 2561-9006 AND B717 AMM 25-61-02. (LP #2151933)

Part: NONE — NONE · airframe 49,146 hrs · 34,878 cycles

RT WING UPPER TRAILING EDGE PANEL DAMAGED FWD OF THE OUTBRD SPOILER OUTBRD HINGE. REMOVED DAMAGED "T" AND WEB ASSY FROM AFT WING SPAR. REPLACED THE "T" AND WEB ASSY PER LONG BEACH DWG 9957465, 975008, AND 57-51-09 BOEING 717 SRM. RIB INSTALLATION INSP: QC5312. (LP #7110857)

Part: LIGHT — DISCONNECTED (CABIN) · airframe 48,146 hrs · 34,112 cycles

ROW 20D CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY DISCONNECTED. ONCE THE LIGHT WAS RECONNECTED THE OPERATION CHECKED GOOD REF B717 WDM 33-51 AND THE AIRCRAFT RETURNED TO SERVICE. (LP #6370942)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,834 hrs · 33,141 cycles

EMERGENCY LIGHTS OVER THE AFT OVERWING EXIT IS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK, B5-230, TO BE BAD. BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5041741)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,636 hrs · 33,013 cycles

THE EMERGENCY LIGHTS ARE NOT WORKING AT THE OVERWING EXIT ON ROW 20 AND THE OVERHEAD EXIT ON ROW 20/21. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK B5-230. OPERATIONAL CHECKS ARE GOOD IAW AMM 33-51. OK FOR SERVICE. (LP #5824949)

Part: LANYARD — DISCONNECTED (TAILCONE) · airframe 46,134 hrs · 32,641 cycles

TAILCONE DEPLOYMENT SYSTEM LANYARD DISCONNECTED FROM DEPLOYMENT HANDLE ON BOX. NRC 001-0209:2000-1002/014 00195: COMPLIED WITH ON JOB 001-0106:5352-4002. (LANYARD CONNECTED). (LP #0898975)

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,134 hrs · 32,641 cycles

STA 715 LT FRAME CRACKED GREATER THAN 1/4" SEE CONDITION 3 STEP 13, REF NRC 51: REPLACED FRAME REF WORK CARD 5310-01436-03A. (LP #0900033)

Part: HINGE — OUT OF POSITION (EVAC SLIDE) · airframe 46,134 hrs · 32,641 cycles

TAILCONE SLIDE BOX COVER HALF HINGES NOT ENGAGED. NRC 001-0209:2000-1002/011 00192: COMPLY WITH ON JOB 001-0106:5352-4002. (ENGAGED HINGES). (LP #0898973)

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,134 hrs · 32,641 cycles

STA Y=696.00 OVERWING FRAME HAS CRACK AT UPPER RADIUS OF THE FRAME TAB GREATER THAN .250 (CONDITION 3) PER STEP 10 OF 5310-01436-04D. REF NRC 49: REPLACED FRAME REF WORK CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9564. (LP #0900044)

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 46,134 hrs · 32,641 cycles

NEW DAMAGE AT PREVIOUS MONITOR PLACARD LH FUSELAGE STA 237 AT CUSP LINE (MKD). NRC 001-0242:5300-2018/010 00016: PRI 574366-14 REV O-2 MATCHES ER/A 574366-14 REV O STEPS 1-8. (LP #0899736)

Part: SIGN — MISSING (CABIN) · airframe 45,296 hrs · 32,059 cycles

EXIT SIGN MISSING ONE SIDE MID-PLANE. FOUND & RE-SECURED FWD FACING EMERGENCY EXIT SIGN AS REQUIRED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,938 hrs · 31,795 cycles

ON WALKAROUND FOUND AFT LAV PANEL SKIN CORRODED AND BULGING. REPAIRED ON N/R 1, REF ERA 569907-14.

Part: SKIN — DELAMINATED (RT WING SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK, THE RT OTBD SPOILER WAS FOUND DELAMINATED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,050 hrs · 29,054 cycles

UPPER CABIN RIGHT CUSP WEB IS CORRODED AT STA 598-620 RBL 59, AT REPAIR BETWEEN STA 655-674 RBL 59, AND IS CRACKED AT STA 674 RBL 47. REPLACED CUSP WEB FROM STA 655 TO 674 IAW SRM 51-41-02, 51-41-03. BLENDED CUSP FROM 598 TO 620 IAW SRM 53-00-00 FIG 103. .019 REMAINING OF .020. FOUND TO BE IN LIMITS IAW SRM 53-00-00 FIG 103.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,050 hrs · 29,054 cycles

LONGERON 29R CORRODED STA 927-946. REMOVED .027 WAS REMOVED IAW SRM 53-00-00 FIG 103. LONGERON REPLACED WITH NEW LONGERON IAW SRM 51-41-02 06 ER/A 551819-14MA.

Part: LONGERON — CORRODED (BS 927-946) · corrosion level 2 · airframe 41,061 hrs · 29,061 cycles

LONGERON 29R CORRODED BS 927 - 946. THE LONGERON WAS BLENDED, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 51-41-02-06, AND ER/A 551819-14MA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 41,050 hrs · 29,054 cycles

R1 SRVC DOOR HAS A CRACKED BEAM INSIDE THE CAVITY AT THE DOOR HOLD OPEN RELEASE HANDLE. REPLACED R1 SERVICE DOOR FRAME INSIDE THE CAVITY AT THE DOOR HOLD OPEN RELEASE HANDLE IAW DRAWING 9911580 AND SRM 51-41-01-OG, 51-41-02 FIG 13, AND 51-41-05 FIG 2.

Part: SKIN — CRACKED (BS 1022) · airframe 41,044 hrs · 29,050 cycles

FUSELAGE SKIN CRACKED BS 1022, LONGERON 14L. HFEC VERIFIED IAW NDT SPM ETHF PROCEDURE 1, 06-10-01.001. REPAIRED THE SKIN IAW ER/A 553662-14 REV 0. ASSOCIATED ER/A 00-553662 ADDED FOR AC 9564.

Part: PANEL — DAMAGED (LT NACELLE) · airframe 41,044 hrs · 29,050 cycles

SEVERAL FASTENERS PULLED THROUGH THE LEFT PYLON FAIRING, LOWER FWD EDGE. REPAIRED THE PANEL IAW 54-00-00 REP 2. FIG 201.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 41,044 hrs · 29,050 cycles

LEFT VERTICAL STAB L/E AT SPLICE VSS 52.267, UPPER TWO ROWS HAVE 26 LOOSE SCREWS & 22 OVERSIZED HOLES. INSTALLED A REPAIR IAW BSG 95550001 AND W/C 5530-01048-03.

Part: CUSP WEB — CRACKED (BS 655) · airframe 41,044 hrs · 29,050 cycles

FOUND A CRACK IN THE CUSP WEB BS 655. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,078 hrs · 29,073 cycles

CORROSION FLC L30 STA 600. L30 STA 600 CORRODED, BLENDED CORROSION AS REQUIRED, IAW B717 SRM 53-00-00 FIG 103. ORIGINAL THICKNESS .170 REMOVED .040. FOUND TO BE OUT OF LIMITS. REPLACED.

Part: CUSP WEB — CORRODED (BS 908-946) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

UPPER CABIN RT SIDE CUSP WEB BETWEEN BS 908 - 946 HAS CORROSION ON UPPER AND LOWER SURFACES. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4 FIG 209.

Part: WEB — DAMAGED · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

FLOOR WEB BELOW PANEL 221EF IS CORRODED WITH A HOLE THROUGH IT. REPAIRED THE WEB IAW ER/A 551819-14MA REV OR.

Part: CUSP WEB — CORRODED (BS 370-389) · airframe 41,044 hrs · 29,050 cycles

LEFT CUSP WEB CORRODED AND HAS HOLE PUNCH THROUGH IT AT BS 370-389. BLENDED AREAS IAW SRM 53-00-00, FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS WAS .080 REMOVED .007 REPAIRED IAW 53-00-55. . FABRICATED DOUBLER IAW SRM 53-00-55.

Part: CUSP WEB — CORRODED (BS 366) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

RIGHT CUSP WEB IS CORRODED AT BS 366 RBL 59. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: CUSP WEB — CORRODED (BS 655-756) · airframe 41,044 hrs · 29,050 cycles

LEFT CUSP WEB BS 655-756 HAS CORROSION WITH CORROSION BETWEEN LBL 44-56. BLENDED AND A CRACK WAS FOUND AT STA 665 LBL 58. DAMAGE WAS REMOVED DOUBLER AND RING. DOUBLER AND FILLER ALODINE & PRIMED PARTS AND INSTALLED IAW SRM 51-10-04, 53-00-55 REPAIR 4 FIG 207.

Part: SHEAR TIE — CORRODED (BS 974) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

SHEAR TIE BS 974 BETWEEN STRINGERS 25-26L IS CORRODED. BLENDED IAW SRM 53-00-00 FIG 103 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-00-06 REPAIR 2.

Part: ATTACH BRACKET — CRACKED (BS 715 FLOORBEAM) · airframe 41,044 hrs · 29,050 cycles

FLOORBEAM SUPPORT STRUT ATTACH BRACKET IS CRACKED IN SEVERAL PLACES AT BS 715 LBL 44. REPLACED ATTACH BRACKET IAW SRM 51-41-05 STEP 8.

Part: CUSP WEB — CORRODED (BS 922-933) · airframe 41,044 hrs · 29,050 cycles

CUSP WEB BETWEEN BS 922-933 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS . INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4. FIGURE 216.

Part: CUSP WEB — CORRODED (BS 337) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

CUSP WEB IS CORRODED AT BS 337 RBL 59. REPAIRED IAW SRM 53-00-55-2R-4.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

FWD LOWER CARGO 121MF METAL FLOOR PANEL MOUNT HOLES HAVE SIGNS OF CORROSION. BLENDED THE PANEL IAW SRM 53-00-00. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-50 2R-1.

Part: CUSP WEB — CORRODED (BS 865) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

BS 865 CUSP WEB CORRODED. REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG 213.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,044 hrs · 29,050 cycles

UPPER CABIN RIGHT CUSP WEB IS CORRODED AT STA 825-830 RBL 59. MARKED. BLENDED CORROSION ON CUSP WEB AT STA 825-830 RBL 59. NOMINAL=.020 REMAINING=.014 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55 FIG 101. REPAIRED DAMAGED AREA ON CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,044 hrs · 29,050 cycles

INTERCOSTAL AT STA 636 BL0 CRACKED. REPAIRED CRACKED ANGLE ON INTERCOSTAL STA 636 BL0 IAW SRM 53-00-00 REPAIR 1.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 41,044 hrs · 29,050 cycles

FWD SERVICE DOOR LOWER HORIZONTAL BEAM JUST UNDER LOWER DOOR HINGE CRACKED. REPLACED LOWER HORIZONTAL BEAM ON FWD SERVICE DOOR IAW SRM 51-41-01-0G, 51-41-02 FIG 13, AND 51-41-05 FIG 2.

Part: FRAME — CORRODED (BS 927) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

FRAME BS 927 HAS CORROSION BETWEEN LONGERON 28L AND 29R ON BOTH SIDES. REPAIRED SRM 53-00-00, FIG 103, AND 51-70-11, FIG 201, REPAIR NR 1.

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

AFT CARGO DOOR ENTRY LOWER JAMB HAS CORROSION. REPARIED IAW SRM 53-20-15, REPAIR 7 AND DWG J060288.

Part: LANYARD — BROKEN (R1 DOOR SLIDE) · airframe 38,035 hrs · 26,695 cycles

RIGHT FWD DOOR 1 SLIDE PACK: LOWER PARACHUTE PIN LANYARD STRING IS BROKEN. REPLACED EVACUATION SLIDE NR 1 RT SERVICE DOOR IAW AMDS 2561-9005.

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

FWD CARGO ENTRY LOWER FRAME HAS CORROSION. REPLACED LOWER CARGO DOOR PAN IAW DWG J060228.

Part: LONGERON — CORRODED (BS 946-1002) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

LONGERON 30L HAS SIGNS OF CORROSION BETWEEN FRAME BS 946-1002. REPAIRED IAW ER/A 538313-14.

Part: DOUBLER — CORRODED (BS 965-986) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

AFT CARGO BILGE, CELL PHONE ANTENNA DOUBLER CORRODED, BS 965-986. REMOVED CORROSION IAW SRM 53-00-00, FIG 103, FABRICATED AND INSTALLED NEW INTERNAL DOUBLER IAW DWG P13110-05105.

Part: SHEAR TIE — CORRODED (BS 946) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

BS 946 FRAME SHEAR TIE HAS SIGNS OF CORROSION BETWEEN STRINGERS 29R & 29L. INSTALLED SHEAR TIE REPAIR AND REINSTALLED INTERCOSTAL BETWEEN FRAME 946 AND 954, TO THE RT OF L30 IAW SRM 53-00-00, AND SRM 53-00-06, REPAIR NR 2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

FUSELAGE SKIN CORRODED AROUND OPENING OF LAV VACUUM MOTOR EXHAUST PORT. FOUND INTERNAL BRACKET CORRODED BEYOND SRM LIMITS. R & R BRACKET IAW DWG 5936667.

Part: FRAME — CORRODED (BS 908) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

FRAME BS 908 HAS CORROSION BETWEEN LONGERONS 28L-28R. REPAIRED IAW SRM 53-00-06, FIG 201.

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 38,035 hrs · 26,695 cycles

FRAME BS 1022 HAS CORROSION BETWEEN LONGERON 29L-29R. SPLICED IN A NEW SECTION OF FRAME IAW SRM 53-00-06. REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 1002) · airframe 38,035 hrs · 26,695 cycles

SHEAR TIE BETWEEN 29 - 30L HAS CORROSION AT BS 1002. REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: BULKHEAD WEB — CRACKED (BS 1103) · airframe 38,035 hrs · 26,695 cycles

AFT BULKHEAD WEB HAS A 2.5 INCH CRACK NEAR INBD EDGE AT HORIZONTAL STIFFNER. REPAIRED IAW SRM 53-30-08, REPAIR 4.

Part: CUSP WEB — PUNCTURED (BS 696-715) · airframe 38,035 hrs · 26,695 cycles

DURING OVERWING FRAME REPLACEMENT, FOUND CUSP WEB PUNCTURED BETWEEN BS 696 AND BS 715 ON LT SIDE. REPAIRED IAW SRM 53-00-00, FIG 201.

Part: FRAME — CRACKED (BS 696) · airframe 38,035 hrs · 26,695 cycles

LEFT OVERWING FUSELAGE FRAME AT BS 696 IS CRACKED. REPLACED LT OVERWING FRAME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 38,017 hrs · 26,676 cycles

EMERGENCY LIGHTS IN AFT CAT WALK ARE DIM. REPLACED BATTERY B5-116.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,184 hrs · 25,977 cycles

DURING LINE CHECK, NOTED AFT EXIT LIGHTS AT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51. LP 6571031.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 36,505 hrs · 25,458 cycles

DURING SERVICE CHECK, FOUND L1 DOOR SLIDE PIN PULLED. REPLACED L1 DOOR SLIDE IAW WORK CARD 2561-9004.

Part: SENSOR — MALFUNCTIONED (SLATS) · airframe 35,945 hrs · 25,057 cycles

ACFT DIVERTED WHILE ENROUTE DUE TO A PSEU FAIL MESSAGE ILLUMINATING MULTIPLE TIMES ENROUTE; PARTICULARLY DURING TURBULENCE. PSEU FAIL ILLUMINATED WITH SLAT DOWN ARROW ON APPROACH. THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED BECAUSE THE QRH REQUIRES A ZERO FLAPS LANDING AND A LONGER RUNWAY. THE FAULT EXTINGUISHED ENROUTE AND THE FLIGHT CREW WAS ABLE TO MAKE A NORMAL FLAPS 40 LANDING. TROUBLESHOT IAW FIM 27-80. FOUND RT SLAT SENSOR D1-66 AT FAULT. REPLACED RT SLAT B SENSOR IAW AMM 27-84. PERFORMED GOOD OPS TEST IAW AMM 27-84. THE ACFT HAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,720 hrs · 24,872 cycles

DURING LINE CHECK, NOTED THE EMERGENCY LIGHTS WERE INOPERATIVE AT EXIT ROW 19 AND IN CEILING ABOVE ROW 17-19. MAINTENANCE REPLACED BATTERY PACK CHARGER AND BATTERY B5-120 AND B5-121 IAW WDM 33-51. OPS CKS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,099 hrs · 24,337 cycles

FLIGHT ATTENDANT REPORTED EMERGENCY EXIT SIGN LENS WAS MISSING AT DOOR 1R. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,584 hrs · 23,859 cycles

DURING SERVICE CHECK, STEP 7, CEILING EMERGENCY LIGHTS ROW 13 AND FORWARD FAILED TO ILLUMINATE IN ANY OF THE THREE TEST MODES. REPLACED BATTERY PACK IAW AMM 33-51.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 34,013 hrs · 23,389 cycles

DURING LINE CHECK, R1 DOOR EMERGENCY EXIT SIGN WAS REPORTED TO BE INOPERATIVE. THE EMERGENCY EXIT SIGN COVER WAS REPLACED.

Part: WIRE — LOOSE (CABIN) · airframe 33,018 hrs · 22,752 cycles

TAIL COMPARTMENT EMERGENCY EXIT LIGHT WIRES LOOSE AT CONNECTOR. SECURED PIN AT THE CONNECTOR IAW SWPM & MM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 33,018 hrs · 22,752 cycles

LOWER FORWARD CUTOUT FRAME CORNER ATTACH BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,018 hrs · 22,752 cycles

FLOOR PANEL 222YF OVER CENTER TANK S/M CRACKED. R&R PANEL IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 33,018 hrs · 22,752 cycles

RT VENT BOX, UPPER INBD LOWER ATTACH PANEL UPPER AFT CORNER DOUBLER REPAIR PANEL CRACKED. R&R PANEL IAW DRAWING.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 33,018 hrs · 22,752 cycles

RT HEAT EXCHANGER EXHAUST FWD TOP CORNER CRACKED IN THE RADIUS & FASTENER HOLES OF THE ATTACH ANGLE. R&R ANGLE IAW DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,018 hrs · 22,760 cycles

SEAT TRACK BRACKET CRACKED AT STATION 736, BL 44.5. R&R BRACKET IAW SRM.

Part: BRACKET — CRACKED (LE SLAT) · airframe 33,018 hrs · 22,760 cycles

LT WING NR 5 LE SLAT OTBD SEAL RETAINING BRACKET CRACKED FROM RIVET HOLE TO EDGE OF BRACKET. R&R BRACKET IAW SRM.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 33,018 hrs · 22,760 cycles

LEFT FWD EMERGENCY EXIT DOOR UPPER INSIDE FRAME CORRODED. REPAIRED FRAME IAW SRM.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 33,018 hrs · 22,760 cycles

LEFT AFT EMERGENCY EXIT DOOR INNER FRAME UPPER SECTION CORRODED. REPAIRED FRAME IAW SRM.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 33,018 hrs · 22,760 cycles

R2 EMERGENCY EXIT DOOR INNER FRAME CORRODED. REPAIRED FRAME IAW SRM.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 33,018 hrs · 22,760 cycles

R1 EMERGENCY EXIT DOOR INNER UPPER FRAME UPPER SECTION CORRODED. REPAIRED FRAME IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 33,077 hrs · 22,794 cycles

FORWARD BULL NOSE EXIT SIGN FELL OFF. REPLACED EXIT SIGN LENS, REF AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,750 hrs · 21,944 cycles

EEPLS BULBS INOP. RELAMPED BULBS PER MM.

Part: LATCH — OUT OF ADJUST (RT MLG) · airframe 30,747 hrs · 21,283 cycles

RIGHT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR PER QRH. ADJUSTED LATCH ASSY PER MM.

Part: ACTUATOR — MALFUNCTIONED (RT MLG DOOR)

AFTER GEAR EXTENSION GEAR DOOR OPEN ILLUMINATED. AFTER 15 SECONDS ALERT EXTINGUISHED. REMOVED AND REPLACED RT MLG DOOR ACTUATOR IAW B717 MM 32-34. OP'S AND LEAK CK'D GOOD.

Part: FLOOR PANEL — CORRODED (CARGO BAY)

FWD CARGO COMPARTMENT FLOOR PANEL, CORROSION. ACCOMPLISHED FLOOR PANEL REPLACEMENT PER B717 SRM 53-20-01, 51-10-01.

Part: FRAME — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT FRAME, STA 484, LONG 29L TO 29R, CORROSION. ACCOMPLISHED FRAME DOUBLER REPAIR PER B717 SRM 53-20-07.

Part: PAN — CORRODED (CARGO DOORWAY)

AFT CARGO DOOR JAMB FLOOR PAN, CORRODED. ACCOMPLISHED DOOR PAN REPLACEMENT PER SRM 53-20-15, 51-10-04 AND 51-40-08.

Part: PAN — CORRODED (CARGO DOORWAY)

FWD CARGO DOOR JAMB FLOOR PAN, CORRODED. ACCOMPLISHED DOOR PAN REPLACEMENT PER SRM 53-20-15, 51-10-04 AND 51-40-08.

Part: LENS — MISSING (CABIN)

EPL CLEAR LENSES MISSING- 2 POSITIONS. INSTALLED LENSES AS REQD REF 33-51.

Part: LENS — MISSING (CABIN)

EMERGENCY PATCH LIGHT MISSING LENS AT ROW 19 AND 30. REPLACED MISSING LENS IAW MM 33-50. GOOD FOR CONT'D SVC.

Part: FASTENER — MISSING (CABIN)

E-PATH LIGHT SOCKET AT ROW 22DEF, LOOSE, AND MISSING MOUNTING HARDWARE. INSTALLED MISSING HARDWARE AND TIGHTENED LOOSE HARDWARE IAW AMM 33-51-04. OPS CHECK NORMAL IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 10D EGRESS LIGHT INOP AND LENS MISSING. RELAMPED AND REPLACED MISSING LENS REF MM 33-51.

Part: WIRE — BROKEN (CABIN)

ROW 19 E-PATH LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT QUICK-DISCONNECT CONNECTOR IAW SWPM 20-31-31, SWPM 20-10-05. OPS CHECK OF EMERGENCY LIGHTING SYSTEM NORMAL IAW 33-51-00.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

R1 DOOR SLIDE LANYARD CAME DISCONNECTED. RE-ATTACHED SLIDE LANYARD TO R1 DOOR SLIDE IAW B717 AMM 25-61-03 PARA 3B.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 247, RBL 45, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F. SEE NR 5204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 256, LBL 22 TO RBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5206.

Part: RUB STRIP — CORRODED (RT WING)

RIGHT WING UPPER ACCESS PANEL 620FT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 620FT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F. SEE NR 5195.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 11, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5192.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 256, LBL 22 TO RBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5206.

Part: RUB STRIP — CORRODED (LT WING)

LEFT WING UPPER ACCESS PANEL 520DT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 520DT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01. SEE NR 1070.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN CUSP PANEL, STA 665, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP PANEL DOUBLER AND FILLER REPAIR PER BOEING DWG 09530003. SEE NR 5188.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 147 TO 200, RBL7, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01. SEE NR 5194.

Part: FITTING — CORRODED (CABIN)

RIGHT CABIN CUSP GRILL CLIP, STA 500, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5185.

Part: FITTING — CORRODED (CABIN)

RIGHT CABIN CUSP GRILL CLIP, STA 460, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5184.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN CUSP PANEL LIGHTENING HOLE, STA 490, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP PANEL LIGHTENING HOLE DOUBLER AND FILLER REPAIR PER BOEING DWG 09530003. SEE NR 5186.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01. SEE NR 5193.

Part: LONGERON — CRACKED (FUSELAGE)

LEFT LONGERON FINGER WEB, STA 200, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1. SEE NR 5180.

Part: FITTING — CORRODED (CABIN)

RIGHT CABIN CUSP GRILL CLIP, STA 610, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5187.

Part: ACTUATOR — CRACKED (RT MLG)

DURING TAKEOFF WHEN LANDING GEAR UP WAS SELECTED RIGHT MLG RETRACT CYLINDER HAD A STRUCTURAL FAILURE, RESULTING IN TOTAL LOSS OF HYDRAULIC SYSTEM RIGHT FLUID AND PRESSURE. THE BARREL ASSY CRACKED AND SEPARATED APPROX 2 INCHES ABOVE LOWER GLAND. REMOVED AND REPLACED RIGHT MLG RETRACT CYLINDER IAW AMM 32-33. NO LEAKS NOTED. SERVICED HYD SYSTEM REF AMM 12-13.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

OVERWING EMERGENCY EXIT LIGHTS ON WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED EMERGENCY BATTERY ASSY AMM 33-50, OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE)

COCKPIT ENTRANCE SUB FLOOR AREA HAS CORROSION. CUT OUT DAMAGED SECTION AND REPAIR. REF B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR CORRODED AT STA 187 LBL 12. REMOVED AND REPLACED FLOOR SUPPORT AT STA 187 LBL 12. REF B717 SRM 51-42-02 DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORRODED FROM STA 157-187 RBL 55. REMOVED AND REPLACED FLOOR SUPPORT. REF B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT CORRODED AT STA 187 LBL 12-16. REMOVED AND REPLACED FLOOR SUPPORT. REF B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR CORRODED BYL AT STA 200 RBL 48. REMOVED AND REPLACED FLOOR SUPPORT. REF B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT CORRODED FROM STA 157-180 RBL 44. FABRICATED NEW FLOOR SUPPORT AND INSTALLED. REF B717 SRM 51-41-02, DWG 9936534 AND EA 17-53-01535IR.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR LOWER PAN CORRODED STA 962.5 AND 989. REPLACED LOWER CARGO DOOR PAN REF EA 17-53-005-2561R, B717 SRM 53-20-15 REPAIR 7.

Part: STIFFENER — CORRODED (CARGO BAY)

AFT CARGO, FWD BULKHEAD VERTICAL STIFFENER LBL 34 LOWER SECTION CORRODED. INSTALLED REPAIR AT AFT CARGO COMPARTMENT LBL 34 FWD BULKHEAD VERTICAL STIFFENER.

Part: STRAP — CORRODED (FAIRING)

STRAP ON FAIRING SUPPORT STA 851 RT SIDE CORRODED. INSTALLED STRAP ON FAIRING SUPPORT STA 851 RT SIDE IAW B717 SRM 51-41-02. MATERIAL USED 7075-T6 100" SIZE 6'.3" X 2".

Part: FRAME — DAMAGED (FUSELAGE)

AFT CARGO COMPARTMENT AT STA 832 AND LONGERON 26 LEFT FRAME LOWER FLANGE IS DAMAGED. INSTALLED FRAME REPAIR SPLICE ON STA 832 AND LONGERON 26L IAW B717 SRM 53-20-07 F-201. MATERIAL USED .063, 7075-0, TREATED TO T6 SIZE 11 X 2.75 INCHES.

Part: STRINGER SPLICE — CORRODED (FUSELAGE)

STA 898.5 LONG 25L SPLICE CORRODED. INSTALLED SPLICE AT BS 898.5 LONGERON 25L IAW B717 SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (FUSELAGE)

STA 878.5 LONG 23L SPLICE CORRODED. INSTALLED NEW SPLICE AT BS 878.5 LONGERON 23L IAW B717 SRM 41-41-05.

Part: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT REAR LAVATORY DUMP DOUBLER CORROSION ON LT LOWER EDGE FROM STA 1022 TO 1037 AND BETWEEN LONGERON 23 TO LONGERON 25. INSTALLED REAR LAVATORY DUMP DOUBLER AT AFT CARGO COMPARTMENT STA 1022 TO 1037 AND BETWEEN LONGERON 23L AND LONGERON 25L AS PER B717 SRM 51-41-02 AND EA 17-53-00534 IR. MATERIAL USED 2024-T3 .090.

Part: STRAP — CORRODED (FUSELAGE)

INTERNAL TIE STRAP ON LONG 23L HAS CORROSION FROM STA 1002 - 1033. INSTALLED INTERNAL TIE STRAP ON LONGERON 23L FROM STA 1002 TO STA 1003 IAW B717 SRM 51-41-05.

Part: SKIN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT, INNER SURFACE OF SKIN HAS CORROSION BETWEEN STA 813 AND 898.5 AND L 26L TO 25L LAP SEAM AREA. INSTALLED DOUBLER AND TRIPLER REPAIR AT AFT CARGO COMPARTMENT, INNER SURFACE SKIN BETWEEN STA 813 AND 898.5 AND L-26L AND L-25L IAW BOEING MESSAGE NUMBER 1-383755005-4 DATED 20-JUN-2007 AND AIRTRAN EA 17-53-00541 IR. MATERIAL USED FOR DOUBLER AND TRIPLER 7075-T6 .080. SIZE 1.0 X 19.0 INCHES.

Part: STRAP — CORRODED (FUSELAGE)

INTERNAL TIE STRAP ON LONG 25L HAS CORROSION FROM STA 1002 - 1033. INSTALLED INTERNAL TIE STRAP ON LONGERON 25L FROM STA 1002 TO STA 1003 IAW B717 SRM 51-41-05.

Part: SKIN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT AREA FUSELAGE SKIN, EXTERNAL SURFACE HAS CORROSION BETWEEN STA 860 AND 880 AND L-29L TO 27L. INSTALLED DOUBLER REPAIR AT AFT CARGO COMPARTMENT BETWEEN STA 851 AND STA 874 AS PER AIRTRAN EA 1753-00542 IR. MATERIAL USED .063 7075T6, 7.0 X 17.0 INCHES AND .025 2024T3 FOR FINGER DOUBLER.

Part: INTERCOSTAL — CORRODED (BS 927-946)

BS 927 LONGERON 29R FUSELAGE FRAME HAS CORROSION. INSTALLED INTERCOSTAL AT STA 927 TO STA 946 STR 29R AS PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: INTERCOSTAL — CORRODED (BS 1002-1022)

INTERCOSTAL AT BS 1002 - 1022 AND BETWEEN LONG 26L AND 27L. INSTALLED INTERCOSTAL BETWEEN STA 1002 AND STA 1022 AND BETWEEN LONGERON 26L AND 27L IAW B717 SRM 51-41-02.

Part: STIFFENER — CORRODED (BULKHEAD)

AFT CARGO COMPARTMENT, FWD BULKHEAD, VERTICAL STIFFENER LBL 48, LWR SECTION IS CORRODED. INSTALLED EXTRUDED REPAIR ON VERTICAL STIFFENER AFT CARGO, FWD BULKHEAD LBL 48 LOWER SECTION PER SRM 51-70-11 FIG 201.

Part: RIB — CORRODED (BS 832)

LEFT FUS FAIRING SUPPORT RIB AT STA 832 IS CORRODED. INSTALLED NEW FAIRING SUPPORT RIB AT LEFT STA 832 IAW B717 SRM 51-41-02 AND SRM 51-41-056.

Part: RIB — CORRODED (STA 851)

LEFT FUSELAGE STA 851, FAIRING SUPPORT RIB HAS CORROSION ON LOWER END. INSTALLED NEW FAIRING SUPPORT RIB AT LT STA 851 IAW B717 SRM 51-41-02.

Part: STRUCTURE — CORRODED (BS 1053)

JACKPAD FITTING BARREL NUT HOLE IS CORRODED. INSTALLED NEW END TIE FITTING LONGERON 30 AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05.

Part: SKIN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FUSELAGE SKIN INNER SURFACE IS CORRODED FROM STA 1002 TO 1053 BETWEEN L-26L TO 21L. INSTALLED SKIN AND DOUBLER AT AFT CARGO COMPARTMENT FROM STA 895.5 TO STA 1053, LONGERON 21L TO LONGERON 26L AS PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (BS 898.5)

BS 898.5 LONGERON 30L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 30L ON BS 898.5 PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: BULKHEAD — CORRODED (BS 1053)

AFT PRESSURE BULKHEAD LOWER CHORD DOUBLER IS CORRODED STA 1053 BETWEEN L-29L TO 29R. INSTALLED LOWER CHORD ANGLE DOUBLER AT AFT PRESSURE BULKHEAD STA 1053 BETWEEN L-29L TO 29R AS PER B717 SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (BS 898.5)

BS 898.5 LONGERON 26L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE AT AFT CARGO COMPARTMEN AT STA 898.5 LONGERON 26L AS PER B717 SRM 51-41-05.

Part: LONGERON SPLICE — CORRODED (BS 1002-1022)

SPLICE ON L-22L BETWEEN STA 1002 AND 1022 IS CORRODED OUT OF LIMITS. INSTALLED SPLICE ON L-22L BETWEEN STA 1002 AND STA 1022 IAW B717 SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (BS 898.5)

BS 898.5 LONGERON 29L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 29L ON BS 898.5 PER B717 SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (BS 898.5)

BS 898.5 LONGERON 27L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 27L ON BS 898.5 PER B717 SRM 53-00-05.

Part: STRINGER SPLICE — CORRODED (BS 898.5)

BS 898.5 LONGERON 28L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 28L ON BS 898.5 PER B717 SRM 51-41-01 AND SRM 51-41-05.

Part: INTERCOSTAL — CORRODED (BS 946-954)

INTERCOSTAL BETWEEN STA 946 AND 954 AND BETWEEN STR 30R - 29R IS CORRODED AND CRACKED. INSTALLED NEW INTERCOSTAL BETWEEN STA 946 TO STA 954 AND STR 30R AND 29R IAW B717 SRM 54-41-02 AND SRM 51-41-05.

Part: DOUBLER — CORRODED (BS 1040)

CORROSION ON AFT CARGO COMPARTMENT DRAIN DOUBLER LOCATED BETWEEN LONGERON 30L AND LONGERON 29L AT BS 1040. INSTALLED NEW DOUBLER BETWEEN LONGERON 30L AND LONGERON 29L IAW B717 SRM 51-41-02. MATERIAL USED 0.063 7075T6; SIZE 3.0 X 4.25 INCHES.

Part: SPLICE — CORRODED (STA 898.5)

AFT CARGO COMP STA 898.5 INNER SPLICE CORRODED FROM LONG 26L AND 26R. REPLACED INNER SPLICE FROM LONGERON 26 LT TO 26 RT ON STA 898.5 IAW B717 SRM 51-41-05. MATERIAL USED 7075 T6 0.080" X 60." X 3.50".

Part: LONGERON — CORRODED (BS 813-832 L26L)

FS 813 - 832 L AND LONG 26L, EXTERNAL LONGERON HAS CORROSION AT FWD AND AFT ENDS. INSTALLED EXTERNAL LONGERON AT STA 813 TO 832 IAW B717 SRM 51-41-05.

Part: SKIN — CORRODED (BS 898.5-1053)

AFT CARGO COMPARTMENT REAR SKIN PANEL CORROSION ON LT EDGE FINGER DOULBER FROM BS 898.5 TO BS 1053. INSTALLED NEW FINGER DOUBLER FROM BS 898.5 TO BS 1053 LT PER B717 SRM 51-41-02.

Part: STRAP — CORRODED (BULKHEAD)

AFT PRESSURE DOME FWD FACE AT 6 O'CLOCK POSITION STRAP HAS CORROSION (9-010). INSTALLED WEB AND DOUBLER 2 EACH AT AFT PRESSURE BULKHEAD IAW B717 SRM 51-41-05 AND SRM 51-41-02. MATERIAL USED ON WEB 7075-T6 0.040 SIZE 33.5 X 9.25 INCHES AND 38 X 9.25 INCHES, DOUBLER 7075-T6 0.050 SIZES 9.3125 X 4.25 INCHES AND 10 X 4.25 INCHES.

Part: LONGERON — CORRODED (BS 1053)

CORROSION ON AFT CARGO WASTE TANK AREA AT LONG 30 END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 30 AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05.

Part: SHEAR TIE — CORRODED (BS 1002)

CORROSION ON AFT CARGO COMPARTMENT BS 1002 SHEAR TIE BETWEEN LONGERON 30 AND LONGERON 22L. INSTALLED NEW SHEAR TIE AT STA 1002 BETWEEN LONGERON 30L AND 22L PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: LONGERON — CORRODED (BS 1037-1053)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 23L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 23L AT AFT CARGO COMPARTMENT BETWEEN STA 1037 TO STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05.

Part: LONGERON — CORRODED (BS 1053 L28L)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 28L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 28L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 1037 ON FRAME BETWEEN LONGERON 29R AND LONG 21L. INSTALLED NEW FRAME SECTION STA STA 1037 FROM LONGERON 29R TO 18L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .063 AND 7075-T6 0.071.

Part: LONGERON — CORRODED (BS 1053 L22L)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 22L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 22L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 927 FRAME BETWEEN LONG 29R AND 22L. REPLACED FRAME BS 927 BETWEEN LONGERON 29R AND LONGERON 22L IAW SRM 51-41-02.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 974 FRAME BETWEEN LONG 29R AND 21L. REPLACED FRAME BS 974 BETWEEN LONGERON 29R AND LONGERON 21L IAW SRM 51-41-02.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 908 FRAME BETWEEN LONG 28R AND 22L. REPLACED FRAME BS 908 BETWEEN LONGERON 28R AND LONGERON 22L IAW SRM 51-41-02.

Part: LONGERON — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT LONG 26 LT BETWEEN BS 813 AND BS 1053. INSTALLED NEW LONGERON 26L AND SPLCE FROM STA 813 TO 1053 AND NEW FINGER DOUBLER AS PER B717 SRM 51-41-02 AND 51-41-05.

Part: LONGERON — CORRODED (BS 898.5-1053)

CORROSION ON AFT CARGO COMPARTMENT LONGERON 22L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 22L AT AFT CARGO COMPARTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02.

Part: LONGERON — CORRODED (BS 1053 L25L)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 25L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 25L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05.

Part: INTERCOSTAL — CORRODED (BS 1022-1043)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT INTERCOSTAL LONGERON 25L BETWEEN BS 1022 AND BS 1043. INSTALLED INTERCOSTAL AT AFT CARGO COMPARTMENT LONGERON 25L BETWEEN STA 1022 TO STA 1043.

Part: LONGERON — CORRODED (BS 898.5-1053)

CORROSION SPOTS ON AFT CARGO COMPARTMENT LONGERON 29L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 29L AT AFT CARGO COMPARTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02.

Part: LONGERON — CORRODED (BS 1037-1053)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 24LT END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 24L AT AFT CARGO COMPARTMENT STA 1037 TO STA IAW B717 SRM 51-41-02 AND SRM 51-41-05.

Part: LONGERON — CORRODED (BS 1053 L27L)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 27L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 27L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05.

Part: LONGERON — CORRODED (STA 898.5 - 1053)

CORROSION ON AFT CARGO COMPARTMENT LONGERON 30 BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 30L AT AFT CARGO COMPARTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 1022 SHEAR TIE. INSTALLED SHEAR TIE ON STA 1022 BETWEEN L 30 AND 26L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .050 AND 7075-T6 0.071.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 974 SHEAR TIE BETWEEN LONG 29R AND 21L. REPLACED SHEAR TIE BS 974 BETWEEN LONGERON 29R AND LONGERON 21L IAW SRM 51-41-02.

Part: FRAME — CORRODED (BS 1002)

CORROSION ON AFT CARGO COMPARTMENT BS 1002 FRAME BETWEEN LONGERON 30 AND LONGERON 22L. INSTALLED NEW FRAME AT STA 1002 BETWEEN LONGERON 30L AND 22L PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: LONGERON — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 26L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 26L AT AFT CARGO COMPARTMENT IAW B717 SRM 51-41-05.

Part: LONGERON — CORRODED (BS 1053 L29L)

CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 29L END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 29L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 908 STRINGER TIE BETWEEN LONG 28R AND 22L. REPLACED SHEAR TIE BS 908 BETWEEN LONGERON 28R AND LONGERON 22L IAW SRM 51-41-02.

Part: LONGERON — CORRODED (FUSELAGE)

SPOTS OF CORROSION ON AFT CARGO COMPARTMENT LONGERON 27L BETWEEN BODY STATION 889 AND BODY STATION 1053. INSTALLED LONGERON 27L AT AFT CARGO COMPARTMENT BETWEEN STA 889 AND STA 1053 AS PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 927 STRINGER TIE BETWEEN LONG 29R AND 22L. REPLACED SHEAR TIE BS 927 BETWEEN LONGERON 29R AND LONGERON 22L IAW SRM 51-41-02.

Part: LONGERON — CORRODED (BS 898.5-1053)

CORROSION ON AFT CARGO COMPARTMENT LONGERON 23L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 23L AT AFT CARGO COMPARTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT FRAME BETWEEN LONG 30 AND LONG 22L. INSTALLED FRAME SPLICE AT STA 1022 FROM LONGERON 25L TO 23L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .050 AND 7075-T6 0.071.

Part: SKIN — CORRODED (FUSELAGE)

CORROSION SPOTS ON AFT CARGO COMPARTMENT SKIN INNER SURFACE BETWEEN BS 898.5 AND BS 1053 AND FROM LONG 26 LT TO LONG 29 RT. INSTALLED LOWER SKIN BETWEEN STA 895.5 TO STA 1053 AND BETWEEN LONGERON 26L TO LONGERON 26R PER B717 SRM 51-41-02 SRM 51-41-05.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON AFT CARGO COMPARTMENT BS 1037 ON SHEAR TIE. INSTALLED SHEAR TIE ON STA 1037 BETWEEN LONGERON 25L TO 20L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .063 AND 7075-T6 0.071.

Part: LONGERON — CORRODED (BS 889-1053)

CORROSION SPOTS ON AFT CARGO COMPARTMENT ON LONGERON 28L BETWEEN BS 889 AND BS 1053. INSTALLED LONGERON 28L AT AFT CARGO COMPARTMENT BETWEEN STA 889 AND STA 1053 AS PER B717 SRM 51-41-02 AND SRM 51-41-05.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SECTION HAS SPOTS OF CORROSION. ROUT OUT DAMAGED AREAS AND INSTALLED (2 EA) DOUBLERS REPAIRS, FABRICATED FROM 7075-0 .063 AND HEAT TREATED TO T-6. DIMENSION 4.5 X 4.25 INCHES AND 4.5 X 4.5 INCHES AS PER MESSAGE 1-383694435-1 AND AIRTRAN EA 17-53-00526IR.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SECTION HAS SPOTS OF CORROSION. INSTALLED DOOR JAMB LOWER SECTION AT FWD CARGO COMPARTMENT DOOR CUTOUT AS PER B717 SRM 53-20-115.

Part: CONTROL UNIT — INOPERATIVE (APU FIRE DETECT)

APU FIRE ALERT FOLLOWED QRH ALERT REMAINED ILLUMINATED UNTIL LDG ROLLOUT APU WAS OFF AT THE TIME. INSPECTED APU COMPARTMENT FOUND NO EVIDENCE OF FIRE OR OVERHEATING CONDITIONS. OPS & LEAK CHECK OF APU GOOD, REF 717 M/M 49-10. REMOVED AND REPLACED APU FIRE DETECTOR CONTROL UNIT RE 26-12, NO FAULTS NOTED AT THIS TIME.

Part: LAMP — BROKEN (EMERGENCY LIGHT)

ROW 17 EMERGENCY LIGHT INOP. REMOVED & REPLACED EMERGENCY LIGHT BULBS REF AMM 33-51, OPS CHECK GOOD. P/N OFF/ON LP7265-001.

Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHT)

CABIN CEILING EMERGENCY LIGHTS FOR ROWS 1-15 DISCHARGE AND SHUT OFF AFTER APPROXIMATELY 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY R5-227 IAW AMM 33-51-03. OPS CHECK NORMAL IAW MM 33-51-00.