N930AT

Part: SLIDE — DISLODGED (ZONE 800) · airframe 57,540 hrs · 41,447 cycles

OPS REPORTS R1 DOOR SLIDE DISLODGED. DOOR SLIDE IAW AMM 25-61. ACFT OK FOR SERVICE. (8406508)

Part: CABLE — OUT OF ADJUST (ZONE 700) · airframe 57,285 hrs · 41,230 cycles

ATB- RETURNED TO ATL DUE TO AIR/GROUND FAULTS. ADJUSTED GROUND SHIFT CABLE. OPS NORMAL.(7834142)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 56,397 hrs · 40,388 cycles

AIRCRAFT 9567, ON SVC CK FOUND AFT L/R OVER WING DOOR EMERGENCY BOTTOM LIGHT INOP. CORRECTIVE ACTION: REPLACED EMERGENGY BATT POWER SUPPLY IAW B717 AMM 33-51-03 OPS CK GOOD. (LP 6812167)

Part: LIGHT — UNKNOWN (ZONE 200) · airframe 55,625 hrs · 39,734 cycles

THE F/A REPORTED THAT THE EXIT ROW EMERGENCY LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE PERFORMED A TEST OF THE EMERGENCY LIGHT SYSTEM AND NO FAULTS WERE FOUND. ALSO, THERE IS NOT ANY HISTORY OF EMERGENCY LIGHTS MALFUNCTIONING IN THE LAST 30 DAYS. ALL CHECKS ARE GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6759907)

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 55,408 hrs · 39,545 cycles

FOUND ROW 21 EMERGENCY EXIT LIGHT B5-230/P9 TO BE INOPERATIVE. MAINTENANCE TRIED A NEW EMERGENCY LIGHT BATTERY. NO HELP, REINSTALLED ORIGINAL. REPLACED POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733147)

Part: LIGHT — INTERMITTENT (ZONE 200) · airframe 54,688 hrs · 38,975 cycles

WITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. MAINTENANCE TROUBLESHOT PER B717 FIM 33-50-00 810-801 AND FAULT WAS INTERMITANT. NO 60 DAY HISTORY. AIRCRAFT OK FOR SERVICE. (LP #5899894)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

CORROSION ON CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 AT PASSENGER CABIN. SUMMARY OF NRC 541: CORROSION LEVEL 2. CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 WAS REPAIRED PER PRI 618606-14 REV 5 AND ER/A 618606-14 REV ORIG. SECTION I. PERMANENT REPAIR. ASSOCIATED ER/A 14-618606 ADDED FOR AC 9567. (LP #0448174)

Part: PAN — CRACKED (FWD CARGO) · airframe 54,485 hrs · 38,792 cycles

CRACKS (3 EA) WERE FOUND ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00573: CRACKS (3 EA) ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR WERE REPAIRED PER ER/A 618437-14 REV ORIGINAL. ASSOCIATED ER/A 14-618437 ADDED FOR AC 9567. (LP #0446314)

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,485 hrs · 38,792 cycles

CRACK ON EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK ON OPEN POSITION. ALSO FWD PREVIOUSLY REWORK DOES NOT MEET WITH RADII. SUMMARY OF NRC 175: EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK WAS REPAIRED PER PRI 618669-14 REV 1 AND ERA 618643-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCOMPLISHED REPETITIVE INSPECTIONS WITHIN EVERY 8,000 CYCLES PER ER/A 618643-14 REV ORIGINAL SEC II UNDER LOG 0413016. ASSOCIATED ER/A 14-618643 ADDED FOR AC 9567. (LP #0443952)

Part: SKIN — CRACKED (BS 1087 L14R) · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT Y=1087 AND L-14R. AN EXISTING SKIN SPLICE REPAIR IS ADJACENT TO THE DAMAGE REPORTED. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FAVICATED SKIN REPAIR FILLER, DOUBLER REPAIR AND CONICAL SPACERS AND INSTALLED. FUS SKIN STA Y=1087 BTW L13R AND L14R AT AFT FUSELAGE AREA WAS REPAIRED PER PRI 618385-14 REV. 1 AND ERA 618385-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR DTE. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 17-JUN-24. (LP 0423719)

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5. (LP 0417885)

Part: ANGLE — CRACKED (BS 210-212 L18R) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE. W1. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER PRI 618846-14 REV 3 AND ER/A 618846-14 REV.ORIGINAL SECTION I: PERMANENT REPAIR. (LP 0415431)

Part: LONGERON — CRACKED (BS 1133 L2R) · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, INITIAL INSPECTION: CRACK ON LONGERON END L2R AND STA 1133 ALSO BRACKET SUPPORT LOWER SECTION CANTED BULKHEAD 1103 RH SIDE AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CRACK ON LONGERON END L2R AND STA 1133 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 AND BRACKET SUPPORT WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR.8. (LP 0416149)

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, CORROSION ON CENTER SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2. SECTION CENTER SEAT TRACK BTW STA= 200 TO STA= 256 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 53-20-52-2R REPAIR 5.

Part: SKIN — CRACKED (LT PAX DOOR) · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, CRACK ON DOOR SKIN ADJACENT TO EXTERNAL DOOR HANDLE HOUSING AT LEFT PASSENGER ENTRANCE DOOR. SUMMARY OF NRC SERIAL 00370: DUE TO SEVERAL DAMAGE ON FWD PASSENGER DOOR (L1) WILL BE REPLACED WITH SERVICEABLE DOOR; PER TRACKING PURPOSE ONLY; FWD PASSENGER DOOR ASSY WAS REPLACED WITH SERVICEABLE DOOR ASSY AND PART NUMBER WAS VERIFIED PER B717 IPC 52-11-30-01. (LP #412960)

Part: SKIN — DAMAGED (L1 DOOR AREA) · airframe 54,485 hrs · 38,792 cycles

AIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. (LP 0413016)

Part: LONGERON — CORRODED (BS 1002 L26R) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

CORROSION OUT OF LIMIT ON LONGERON END STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT. C2. SUMMARYOF NRC 00857: CORROSION LEVEL 2. LONGERON END ON STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8. (LP #0411089)

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 54,485 hrs · 38,792 cycles

CRACKS WERE FOUND ON MEMBRANE OF PASSENGER CABIN AT CUSP WEB BTW STA 218/237 AND BTW STA X=-56/-22. SUMMARY OF NRC 00678: CUSP WEB BTW STA 218/237 AND BTW STA X=-56 /-22 WAS REPAIRED PER B717 53-00-55-2R-4 CONFIGURATION 7015 FIG 210 PAR 40 AND 51-41-02-0G. (LP #0407549)

Part: FRAME — CRACKED (BS 715) · airframe 54,485 hrs · 38,792 cycles

A.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF NRC 00508: OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B AND B717-200 SRM 51-41-05-0G PAR 8. ASSOCIATED AA 5310-01436 ADDED FOR AC 9567. (LP #0405638)

Part: INTERCOSTAL — CRACKED (BS 686) · airframe 54,485 hrs · 38,792 cycles

CRACK ON INTERCOSTAL WAS FOUND ON STA Y=636 X=0 AT PAX CABIN. SUMMARY OF NRC 00838: CRACK ON INTERCOSTAL ON STA Y=636 X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #0403676)

Part: BEAM — CRACKED (FWD CARGO DOOR) · airframe 54,485 hrs · 38,792 cycles

CRACK ON INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00685: INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER B717-200 SRM 52-30- 02-2R PROCEDURE 1 REPAIR 1. (LP #0402498)

Part: SKIN — CRACKED (BS 992 S25R) · airframe 54,485 hrs · 38,792 cycles

CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS REPAIRED PER B717-200 SRM 53-20-15- 2R PROCEDURE 12. PERFORM AN EXTERNAL GVI EVERY 8000 CYCLES TO THE REPAIR PERFORMED IAW SRM 53-20-15-2R PROCEDURE 12 REPAIR 12 PAR 7.A TABLE 202. (LP #0398928)

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

CORROSION ON FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE. IN REFERENCE NRC 00604. SUMMARY OF NRC 00789: CORROSION LEVEL 2. FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 9936534 REV BW AND B717-200 SRM 51-40-01-0G. (LP #0394294)

Part: CUSP WEB — CRACKED (BS 476-670) · airframe 54,485 hrs · 38,792 cycles

CRACKS CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00610: CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN WERE REPAIRED PER B717- 200 SRM 53-00-55-2R-4. (LP #0393751)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 54,485 hrs · 38,792 cycles

CRACK ON INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE. SUMMARY OF NRC 00686: INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0393395)

Part: CUSP WEB — CORRODED (BS 936-940) · corrosion level 2 · airframe 54,485 hrs · 38,792 cycles

CORROSION ON LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00791: CORROSION LEVEL 2, LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 216. (LP #0391165)

Part: FRAME — DAMAGED (BS 737 L18R) · airframe 54,485 hrs · 38,792 cycles

TOOL MARKS ON OVERWING FRAME STA737 L-18R AT WING BOX. SUMMARY OF NRC 00533: OVERWING FRAME STA737 L-18R AT WING BOX WAS REPAIRED PER PRI 618675-14 REV.0 AND ERA 618675-14 REV. ORIGINAL ASSOCIATED ER/A 14-618675 ADDED FOR AC 9567. (LP #0392376)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,050 hrs · 37,597 cycles

THE EMERGENCY LIGHTS IN ROWS 15-19 ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-120 TO BE INOPERATIVE AND REPLACED THE BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4952903)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,442 hrs · 37,060 cycles

SHIP 9567 -HYD/DE- THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID INDICATION WITH THE LEFT SYSTEM. THE QRH WAS COMPLIED WITH AND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP WAS SHUTDOWN. AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF THE LEFT SYSTEM HYDRAULICS WHILE ON APPROACH. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP, THE LEFT CASE DRAIN, PRESSURE, AND RETURN FILTERS. ALSO REPLACED THE LEFT INBOARD SPOILER ACTUATOR STRAINER PACKING. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9415054)

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,403 hrs · 36,153 cycles

THE EXIT LENS COVER AT ROW 19 IS MISSING. MAINTENANCE REPLACED THE MISSING LENS COVER AT ROW 19. (LP #2513959)

Part: FRAME SPLICE — CORRODED (BS 1022 L26-30L) · corrosion level 2 · airframe 49,871 hrs · 34,786 cycles

CORROSION ON REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: (CORROSION LEVEL 2) REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 53-20-07-2R. REPAIR 3. (LP #2169817)

Part: LONGERON — DAMAGED (BS 900-968) · corrosion level 2 · airframe 49,873 hrs · 34,787 cycles

SECOND DAMAGE AFTER CORROSION REMOVAL ON L29 LH BTW STA 900 TO STA 968 REMAINING THICKNESS IS OUT OF LIMITS. IN REFERENCE NRC 184. SUMMARY OF NRC 00252: CORROSION LEVEL 2, LONGERON 29LH BTW STA 900 TO STA 968 WAS REPAIRED PER B717-200 SRM 53-20-05-2R REPAIR 1, FIG 201, PAR 4. (LP #2170171)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 49,871 hrs · 34,786 cycles

CORROSION ON SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00196: CORROSION LEVEL 2, SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-00-05-2R, REPAIR 2. (LP #2168169)

Part: NOT REPORTED — NOT REPORTED · airframe 49,871 hrs · 34,786 cycles

SECONDARY DAMAGE AREAS WERE FOUND AT DENTS #8 & #10 ON INNER FACE OF REAR MOVABLE VANE AT LH WING. AREAS WERE FOUND DEBONDED (IN REF NRC 00060). SUMMARY OF NRC 00238: INNER FACE OF REAR MOVABLE VANE AT LH WING WAS REPAIRED PER B717 SRM 51-70-02-0G AND IN REFERENCE TO B717 SRM 57-53-01-2R-1. (LP #2165037)

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 49,871 hrs · 34,786 cycles

CORROSION ON DOOR JAMB BTW STA 950 TO 1000 OF AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB OF AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R, REP. 7. (LP #2164034)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,330 hrs · 32,744 cycles

THE FORWARD FACING LENS FROM THE CENTER AISLE EMERGENCY EXIT SIGN AT THE OVERWING EXIT IS MISSING. MAINTENANCE INSTALLED THE CENTER AISLE FORWARD FACING LENS AT THE OVERWING EXITS PER B717 AMM 33-51. (LP #6167025)

Part: SKIN — DAMAGED (TE FLAP) · airframe 45,794 hrs · 31,685 cycles

THE LEFT HAND INBOARD FLAP LEADING EDGE WAS FOUND DAMAGED. NRC 010-0001:0514-2001/001 00011: REMOVED AFT VANE PER AMM 27-50-03. REMOVED NOSE ASSY AND ROUTED TO SHOP 383 FOR REPAIR WHICH WAS ACCOMPLISHED ON SHOP ORDER PA4968/ WORK ORDER 19567 AND INSTALLED ORIGINAL REWORKED NOSE ASSY REF CMM 27-50-1 AND DWG 5913601. REINSTALLED AFT VANE PER AMM 27-50-03. (LP #0889823)

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 45,442 hrs · 31,484 cycles

THE FIRST EMERGENCY LIGHT IN THE AFT ACCESSORY COMPARTMENT IS MISSING THE LENS COVER. MAINTENANCE HAS RE-INSTALLED THE COVER. LIGHT OPERATIONAL CHECK IS GOOD. (LP #5101298)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,011 hrs · 31,196 cycles

ON A SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERHEAD CEILING EMERGENCY LIGHTS TURNING ON AND THEN OFF. MAINTENANCE REPLACED THE FORWARD TWO EMERGENCY LIGHT POWER SUPPLIES PER AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-51. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,908 hrs · 29,698 cycles

AFT EXIT DOOR CEILING LIGHT MISSING THE LENS. MAINTENANCE INSTALLED A NEW LENS.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.

Part: FLOOR PANEL — CRACKED · airframe 41,513 hrs · 28,752 cycles

CABIN FLOOR PANEL 223AF IS CORRODED IN SEVERAL AREAS AND CRACKED AT CORNER. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-20-50-01. STOP DRILLED THE CRACK IAW SRM 53-00-00-2R-1. INSTALLED REPAIR DOUBLER IAW SRM 53-00-00-2R-1 FIG 201.

Part: PAN — CORRODED (DOOR) · corrosion level 2 · airframe 41,513 hrs · 28,752 cycles

CORROSION ON DOOR JAMB PAN AT LOWER CENTER DOOR STOP. BLENDED CORROSION ON ALC DOOR JAMB PAN AT LOWER CENTER DOOR STOP, REMOVED .020" OUT OF .050" ORIGINAL THICKNESS (MAX ALLOWABLE .010"), FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 TOOL TAG #2737, REPLACED ALC DOOR JAMB PAN IAW B717 SRM 51-41-02, 51-41-05, 53-20-15-2R-7- FIG 201. (LP #2989323)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,513 hrs · 28,752 cycles

RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND UPPER AND LOWER SURFACES OF LIGHTENING HOLES. REPAIRED CUSP WEB AT STA 446 TO 465 IAW SRM 53-00-55-2R-4 SHEET 4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,513 hrs · 28,752 cycles

RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND AROUND LOWER SURFACE OF LIGHTENING HOLES AT STA 484 TO 503. BLENDED CORROSION ON CUSP WEB AT FS 484-503R OT .020 REMAINING .010 OUT OF LIMITS IAW SRM 53-00-55. REPAIRED CUSP WEB IAW SRM 53-00-55-2R-4 FIG 215 CONFIG 7025 AND SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,513 hrs · 28,752 cycles

UPPER CABIN FLOOR SUPPORTS BETWEEN STA 178 - 202 AT RBL 30-44 ARE CORRODED IN SEVERAL AREAS. REPLACE FLOOR SUPPORT RBL 30.00-44 PER SRM 51-41-02 & DRAWING 9936534.

Part: CUSP WEB — CORRODED (BS 876) · corrosion level 2 · airframe 41,513 hrs · 28,752 cycles

LOWER EDGE OF LIGHTENING HOLE AT BS 876 ON LEFT OTBD CUSP WEB CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55, CUT OUT DAMAGE AND REPAIRED CUSP WEB IAW SRM 53-00-55, FIG 215, AND 51-41-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,860 hrs · 26,120 cycles

DURING LINE CHECK, MAINTENANCE NOTED FORWARD DOORS AND FWD OVERWING EXIT DOORS EMERGENCY EXIT MARKER LIGHTS WERE INOPERATIVE. REPLACED BATTERIES B5-118 AND B5-119.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

LEFT AFT UPPER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

LEFT FWD LOWER EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

RIGHT AFT LOWER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

AFT CABIN DOOR EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

LEFT AFT LOWER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,626 hrs · 25,164 cycles

LEFT FWD UPPER EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,040 hrs · 24,104 cycles

EMERGENCY BATTERY CHARGER IN FWD DROP CEILING INOPERATIVE B5-235. R & R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,040 hrs · 24,104 cycles

EMERGENCY BATTERY CHARGER B5-259 INOPERATIVE. R & R EMER BATTERY CHARGER IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 35,040 hrs · 24,104 cycles

OVERHEAD EMER EXIT SIGN BROKEN AT ROW 1. R & R SIGN IAW MM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CRACKED AT BS 598, LBL 54. REPAIRED CUSP WEB IAW SRM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 35,040 hrs · 24,104 cycles

LEFT WW FLAP CARRIAGE ASSEMBLY BRACKET CRACKED. REPAIRED BRACKET IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 822 - 899, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 589 - 646, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 1022 - 1002. R & R CUSP WEB IAW SRM & EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 737 - 756. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 446 - 696. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 986 - 1002. R & R CUSP WEB IAW SRM & EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 408 - 427. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 813 - 870. R & R CUSP WEB IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR WEB CORRODED BETWEEN BS 200 - 218, RBL 22. R & R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 696 - 715. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN RT CUSP WEB CORRODED BETWEEN BS 927 - 908. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 870 - 851. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 598 - 579. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 579 - 598. R & R CUSP WEB IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 756 - 737. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 655 - 674. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 484 - 503. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

FLOOR SUPPORT CORRODED AT BS 256, BETWEEN LBL 22 TO RBL 22. R & R SUPPORT IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SHEAR TIE CRACKED AT BS 1022, BETWEEN LONGERON 11L - 12L. R & R SHEAR TIE IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

AFT PIT FWD PRESS BULKHEAD SEVERAL LINER SUPPORT, STIFFENER, CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 889 - 1022, RBL 54. R & R SEAT TRACK IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR PANEL CORRODED BETWEEN BS 387 - 465, RBL 4. REMOVED FLOOR PANEL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK FITTING SUPPORT CRACKED AT BS 737, LBL 44. R & R FITTING IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK FITTING SUPPORT CRACKED AT BS 737, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR PANEL 222 AJF CORRODED AT RBL 47. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR PANEL CORRODED BETWEEN BS 946 - 1022, RBL 47. R & R FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR PANEL 222 ZF CORRODED AT RBL 47. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOOR PANEL CORRODED BETWEEN BS 813 - 889, RBL 47. REPAIRED PANEL IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

FORWARD PIT AFT PRESS BULKHEAD SEVERAL STIFFENERS CRACKED AT BS 663, RBL 22. R & R STIFFENER IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 490 - 579, RBL 22. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 590 - 896, LBL 54. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 794 - 851, RBL 54. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 640 - 832, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

SEAT TRACK CORRODED BETWEEN BS 275 - 589, LBL 54. R & R SEAT TRACK IAW DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 35,040 hrs · 24,104 cycles

LEFT WING NR 5 SLAT INBD SIDE OF TRACK NR 12 ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222AHF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

FLOOR SUPPORT CORRODED AT BS 1044, RBL 17. R & R SUPPORT IAW DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222 AVF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222FF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222AMF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222AAF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222APF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222 LF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222PF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222WF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

C2 CUT OUT FWD FRAME WEB CORRODED BETWEEN BS 946 TO BS 102, LONGERON 29R. REPAIRED WEB IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222UF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222AMF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222ATF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,040 hrs · 24,104 cycles

MAIN CABIN FLOORBOARD 222JF DELAMINATED. R & R FLOORBOARD IAW AMM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,040 hrs · 24,104 cycles

C2 CUT OUT AFT FRAME WEB CORRODED AT BS 986, BETWEEN LONGERON 25R - 27R. REPAIRED WEB IAW SRM & EA.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 35,316 hrs · 24,280 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR SYS DIRTY. CLEANED GIRT BAR IAW AMM.

Part: BRACKET — DIRTY (L1 DOOR) · airframe 35,291 hrs · 24,263 cycles

L1 DOOR EMER EVAC SLIDE GIRT BRACKET BAR DIRTY. CLEANED BRACKET IAW MMM.

Part: SKIN — CRACKED (LT WING) · airframe 33,894 hrs · 23,364 cycles

LT WING INBD BUTTE DOOR HINGE ATTACH AREA SKIN PANEL CRACKED. R & R SKIN IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 33,894 hrs · 23,364 cycles

L1 DOOR UPPER AFT BEAM DOUBLER CRACKED. R & R DOUBLER IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,894 hrs · 23,364 cycles

L1 DOOR FWD CTR INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 34,378 hrs · 23,669 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESS GAUGE LOW. R & R SLIDE IAW AMM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 32,974 hrs · 22,758 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER CAME LOOSE FROM DOOR. SECURED HOLDER IAW SRM.

Part: RETAINING CLIP — DETACHED (R1 DOOR) · airframe 32,218 hrs · 22,299 cycles

R1 DOOR EMERGENCY EVAC SLIDE RETAINER CLIP FELL OFF. INSTALLED CLIP PER MM.

Part: COVER — MISSING (CABIN) · airframe 32,183 hrs · 22,280 cycles

RIGHT EMERGENCY EXT LIGHT COVERS MISSING BETWEEN ROW 2 TO ROW 10. REMOVED AND REPLACED COVERS IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 31,031 hrs · 21,586 cycles

L1 DOOR SLIDE FELL OUT. REMOVED AND REPLACED L1 DOOR SLIDE ASSY AT DOOR EVACUATION REF AMM 25-61-01 PARTS VER 44939.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,369 hrs · 21,152 cycles

EMERGENCY EXIT LIGHT INOP. RELAMPED COVER PER MM.

Part: STOP FITTING — CORRODED (CARGO BAY)

C-1 CARGO DOOR PRESSURE STOP FITTING FWD, CORROSION. ACCOMPLISHED PRESSURE STOP FITTING FWD REPLACEMENT PER B717 SRM 51-40-02. SEE NR 24231.

Part: SUPPORT — CORRODED (FUSELAGE)

VHF ANTENNA SUPPORT, CORROSION. ACCOMPLISHED ANTENNA SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-40-08. SEE NR 24224.

Part: FRAME — CORRODED (FUSELAGE)

FRAME LOWER FLANGE, STA 927, LONG L29L TO L30, CORROSION. ACCOMPLISHED LOWER FLANGE DOUBLER AND FILLER REPAIR PER B717 SRM 53-20-07. SEE NR 24126.

Part: LONGERON — CORRODED (FUSELAGE)

LONGERON FLANGE, STA 927, LONG 30, CORROSION. ACCOMPLISHED FLANGE SPLICE REPAIR PER B717 SRM 51-41-02 AND 53-00-05. SEE NR 24223.

Part: ATTACH FITTING — CORRODED (FUSELAGE)

LOWER FUSELAGE WING TO BODY FAIRING ATTACHMENT FRAME, STA 832, LBL 3 TO LBL 30, CORROSION. ACCOMPLISHED ATTACHMENT FRAME SPLICE REPAIR PER B717 SRM 51-70-11. SEE NR 24220.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FORWARD CARGO LOWER DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB SPLICE REPAIR PER B717 SRM 53-20-15, 51-41-02 AND 51-10-04. SEE NR 24122.

Part: FORMER — CORRODED (FUSELAGE)

FORMER, STA 908, LONG L28L TO L30, CORROSION. ACCOMPLISHED FORMER SPLICE REPAIR PER B717 SRM 53-00-06 AND 51-20-01. SEE NR 24131.

Part: ATTACH FITTING — CORRODED (FUSELAGE)

LOWER FUSELAGE WING TO BODY FAIRING ATTACHMENT FRAME, STA 832, RBL 0 TO RBL 30, CORROSION. ACCOMPLISHED ATTACHMENT FRAME SPLICE REPAIR PER B717 SRM 51-70-11. SEE NR 24221.

Part: ATTACH BRACKET — CORRODED (FUSELAGE)

WING TO BODY FAIRING BELLY ATTACH BRACKET, STA 825 TO 834, BL 0, CORROSION. ACCOMPLISHED BELLY ATTACH BRACKET REPLACEMENT PER B717 SRM 51-41-02 AND 51-40-08. SEE NR 24219.

Part: FORMER — CORRODED (FUSELAGE)

FORMER, STA 1002, LONG 28L TO 30, CORROSION. ACCOMPLISHED FORMER REPLACEMENT PER B717 SRM 51-41-02, 53-00-06, 51-40-08 AND 51-41-02. SEE NR 24136.

Part: STOP FITTING — CRACKED (FUSELAGE)

FWD CARGO DOOR FWD LWR STOP FITTING, CRACKED. ACCOMPLISHED FWD LWR STOP FITTING REPLACEMENT PER B717 SRM 51-41-01, 51-40-08.

Part: FRAME — CORRODED (FUSELAGE)

FRAME LOWER FLANGE, CORROSION. ACCOMPLISHED FLANGE DOUBLER AND FILLER REPAIR PER B717 SRM 53-20-07. SEE NR 24124.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 974, LONG L30, CORROSION. OPEN DEFECT. SEE NR 24128.

Part: STRUCTURE — CORRODED (FUSELAGE)

LOWER FLANGE, STA 889, LONG L29R TO L29L, CORROSION. ACCOMPLISHED LOWER FLANGE DOUBLER AND FILLER REPAIR PER B717 SRM 53-20-07, 51-10-04 AND 51-41-02. SEE NR 24125.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO LOWER DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB REPLACEMENT PER B717 SRM 51-20-09, 51-40-08,53-20-15 REP 7.

Part: FORMER — CORRODED (FUSELAGE)

AFT CARGO FORMER LOWER LEG, STA 927, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FORMER LOWER LEG SPLICE REPAIR PER B717 SRM 53-00-06.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ROW 12-20 EMERGENCY SEAT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AT STA 342R AND 804R OPS CHECK GOOD REF MM 33-51. REMOVED AND REPLACED BATT PACKS AT STA 342R AND 804R OPS CHECK GOOD REF MM 33-51.

Part: BATTERY — DISCHARGED (CABIN)

SEAT MOUNTED EMERGENCY FLOOR PATH LIGHTS INOP AT SEATS 11-19. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY, OPS CHECK GOOD. REF B717 AMM 33-51.

Part: PUMP — FAILED (HYDRAULIC SYS)

RIGHT HYDRAULIC SYSTEM FAIL. REMOVED AND REPLACED AUX PUMP IAW MM 29-21. P/N OFF 861555, S/N OFF MX596730.

Part: LENS — MISSING (CABIN)

EPL LENS MISSING AT SEAT 21D (RED). REPLACED EPL LENS AT SEAT 21D (RED).

Part: SLIDE — MISINSTALLED (R1 DOOR)

R1 SLIDE NOT INSTALLED CORRECTLY. REMOVED AND REPLACED R1 SLIDE PER AMM 25-61.

Part: SLIDE — DEFECTIVE (R1 DOOR)

R1 DOOR SLIDE PINS PULLED FROM ORIGINAL POSITION & VELCRO ON GIRT BAR NOT WORKING. REMOVED AND REPLACED R1 DOOR SLIDE AMM 26-61.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 936 TO 965, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION SPLICE REPAIR PER BOEING DWG SG09530000 AND B717 53-20-05.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 215, RBL 56, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-46-05.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237 TO 598, RBL 56, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52 FIG 201 AND B717 SRM 51-41-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT INTERCOSTAL SECTION, STA 1002, LONG L29R, CORROSION. ACCOMPLISHED INTERCOSTAL SECTION REPLACEMENT PER B717 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 598 TO 898, RBL 56, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52 AND B717 SRM 51-41-01.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME SECTION, STA 1022, LONG L28L TO L28R, CORROSION. ACCOMPLISHED FRAME SECTION SPLICE REPAIR PER B717 SRM 53-20-07 FIG 201.

Part: STRAP — CORRODED (FUSELAGE)

LEFT AND RIGHT EXTERIOR WING TO BODY SUPPORT STRAPS, STA 851 TO 918, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAPS REPLACEMENT.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 160 TO 200, LBL 15 TO RBL 56, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER AND SPLICE REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 159, RBL 12, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 151 TO 159, RBL 30 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 256, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02271IR.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN, STA 851 TO 866, LONG L28L TO L28R, CORROSION. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-02270IR.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 159, RBL 45, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

GALLEY SUPPORT FITTING, STA 159, RBL 51, CORROSION. ACCOMPLISHED SUPPORT FITTING REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 161 TO 199, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 154 TO 159, RBL 11 TO RBL 16, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, RBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 159, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 179, RBL 10 TO RBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 148, RBL 32 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 10 TO LBL 13, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, RBL 11 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

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 51-41-02.

Part: PANEL — CORRODED (FUSELAGE)

FILLER PANEL, STA 160 TO 200, CORROSION. ACCOMPLISHED FILLER PANEL REPLACEMENT PER B717 SRM 51-41-01.

Part: SKIN PANEL — CRACKED (RT WING)

RIGHT WING T/E LOWER SKIN PANEL, STA XRS189, CRACKED. ACCOMPLISHED T/E LOWER SKIN PANEL DOUBLER REPAIR PER B717 SRM 51-41-01 AND B717 SRM 51-41-02.

Part: SUPPORT — CORRODED (FUSELAGE)

RIGHT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG L26R TO L29R, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: SUPPORT — CORRODED (FUSELAGE)

LEFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG L26L TO L29L, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT SEATS 25DEF THROUGH 31DEF ARE INOPERATIVE. PER FIM 33-50 TASK 801 STATION 804, REMOVED AND REPLACED BATTERY SUPPLY ASSEMBLY. OPS CHECK OF LIGHTS IS GOOD IAW AMM 33-51-00.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2976.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2986.

Part: DOUBLER — DENTED (FUSELAGE)

DENT FOUND AT STA 228 TO 237, LOCATED ON PREVIOUS REPAIR OF FUSELAGE SKIN. ACCOMPLISH FUSELAGE SKIN REPAIR STA 229 TO 244. REF B717 SRM 53-00-01 FIG 201 SHEET 4.

Part: WIRE — BROKEN (CABIN)

SEAT ROW 22DEF E-PATH LIGHTS INOP (BROKEN WIRE). RE-TERMINATED 1 EA PIN SOCKET ON THE FLOOR SIDE ELECTRICAL CONNECTOR PER SWPM 20-20, WDM 33-51-14, OPS CHECK GOOD IAW AMM 33-51-00 SEAT ROW 22DEF.

Part: WIRE — BROKEN (CABIN)

SEAT ROW 25DEF E PATH LIGHTS INOP (BROKEN WIRE). RE-TERMINATED 1 EA PIN SOCKET ON THE FLOOR SIDE ELECTRICAL CONNECTOR PER SWPM 20-20, WDM 33-51-14 OPS CHECK GOOD IAW AMM 33-51-00 SEAT ROW 25DEF.

Part: BATTERY PACK — DISCHARGED (CABIN)

LT AND RT EXTERIOR EMERGENCY LIGHTS WILL NOT EXTINGUISH. REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY PACK AND RELAY R2-273, ALL OPS CHECK OK PER MM 33-51.

Part: PAN — CORRODED (CARGO BAY)

FWD CARGO COMP LOWER PAN HAS CORROSION. INSTALLED LOWER PAN SPLICE REPAIR PER SRM 53-20-15 FIG 201.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY OVERWING LIGHTS ARE ILLUMINATED WITH EMERGENCY LIGHT SWITCH OFF. REMOVED AND REPLACED OVERWING EMERG LIGHTS PACK REF MM 33-51. EMERG LIGHTS OPS TEST NORMAL REF 33-51.

Part: ENGINE — UNSERVICEABLE (NR 1)

AT CRUISE, A GROWLING NOISE HEARD ALONG WITH ENGINE SURGE FOLLOWED BY TWO LOUD POPPING NOISES ACCOMPANIED BY A BRIEF SMELL OF SMOKE. SHUT ENGINE DOWN AND DIVERTED. REMOVED AND REPLACED NR 1 ENGINE.

Part: ENGINE — INOPERATIVE (LEFT)

ON CLIMBOUT ENGINE LEFT SURGE ALERT CAME ON. ALL ENGINE PARAMETERS NORMAL. AT ABOUT 13,000 LEFT ENGINE FAILED, SEVERE DAMAGE SUSPECTED. REPLACED ENGINE.