N922AT

Part: ENGINE — FAULTED (NR 2) · airframe 45,317 hrs · 31,702 cycles

SHIP 9558 - RTO - CREW REPORTED WITH AUTO-THROTTLE ENGAGED AT 60KNTS RIGHT THROTTLE RETARDED. P30 FAULT, INSPECTED FOR LEAKS/BLOCKAGE WITH NO FINDINGS. REPLACED RIGHT ENGINE EEC, NO HELP. REPLACED #2 ENGINE.

Part: PUSHROD — NOT REPORTED (FLAPS SYS) · airframe 45,215 hrs · 31,604 cycles

ATB, RETURNED TO ATL DUE TO A FLAP INDICATION ISSUE. REPLACED DAMAGED FLAP CONTROL PUSHROD.

Part: HANDLE — DAMAGED (ZONE 800) · airframe 44,916 hrs · 31,341 cycles

THE CABIN CREW REPORTS THAT THE 1L DOOR INTERIOR HANDLE ROTATES FREELY WITHOUT OPENING THE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THAT THE HANDLE BOLT HAD SHEARED. REMOVED SHEARED SHAFT AND INSTALLED NEW BOLT/PIN REF B717 IPC 58-11-45 & AMM 52-11-01. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #7237308)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 44,007 hrs · 30,539 cycles

BOTH OVER-WING EMERGENCY EXIT LIGHTS ARE OUT. ALL OTHER EMERGENCY LIGHTS ARE GOOD. MAINTENANCE REPLACED THE OVER-WING EMERGENCY LIGHT BATTERY PER B717 AMM 31-51-06-401. BOTH OVER-WING EMERGENCY LIGHTS NOW ILLUMINATE PROPERLY. (LP #6931002)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 43,283 hrs · 29,867 cycles

FORWARD SMALLER EMERGENCY LIGHTS ARE INOPERATIVE AT DOORS 1LT & 1RT. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT LOCATION B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #9569211)

Part: PANEL — DAMAGED (THRUST REVERSER) · airframe 43,209 hrs · 29,793 cycles

DURING PILOT PRE-FLT WALKAROUND, NOTICED DAMAGE TO THE #2 ENGINGE UPPER THRUST REVERSER PANEL. 6-8 FOOT SECTION OF PANEL WAS MISSING. MAINTENANCE REPLACED THE #2 ENG THRUST REVERSER ASSEMBLY IAW B717 AMM 78-30. OPERATIONAL CHECK WAS GOOD. (LP #6193668)

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 42,756 hrs · 29,381 cycles

EXIT LIGHT OVER 1R DOOR AND EXIT LIGHT IN FRIST CLASS CABIN INTERMITIELY FLASHING. REPLACE THE EMERGENCY BATTERY & POWER SUPPLY UNIT LOCTION AT 247L PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #5824217)

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 42,856 hrs · 29,467 cycles

SHIP 9558 -MISC/DE- FLIGHT TEST. EXPERIMENTAL TEST FLIGHT FOR FLAP 25 LANDINGS. FLIGHT PLANNED FOR ATL-HSV-ATL. BOEING TEST ENGR/PILOT IN LEFT SEAT AND DELTA LLCP IN RIGHT SEAT AT INITIAL TIME OF EVENT. CREW EXECUTED SIX APPROACHES AND THREE TOUCH AND GOES IN HSV. AT INITIAL CLIMB OUT AFTER LAST TOUCH AND GO, THE JUMP SEAT PILOT NOTICED FLAP ASYMMETRY ON INDICATOR. NO REAL ROLL FORCE NOTICED. AT LEVEL SAFE ALT, HOLDING REQUESTED, LEFT SEAT WAS TRANSFERRED TO SECOND DELTA LLCP (TWO DELTA LLCP IN BOTH CONTROL SEATS). QRH 9.5 FLAP DISAGREE/ASYMMETRY RUN BY RIGHT SEAT AND DISP/MTC CONSULTED VIA ATL RADIO. BOEING PILOT/ENG OBSERVED NO ACTUAL NOTICEABLE FLAP ASYMMETRY FROM CABIN VIEW. AN EMERGENCY WAS DECLARED WITH ATC. AN UNEVENTFUL LANDING ON 26R IN ATL, WITH A NORMAL ROLL OUT AND RUNWAY EXIT WAS ACCOMPLISHED. ATL FIRE RESCUE WAS CALLED OFF. CORRECTIVE ACTION: UPON BOEING AND ATL MAINTENANCE DEBRIEF A FAULTY INDICATOR WAS BEING INVESTIGATED. ALL STANDARD DEBRIEF ITEMS WERE COMPLETED AND THE CREW WAS CLEARED TO CONTINUE. (LP #5824200)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

DURING THE INSPECTION OF EXTERIOR LIGHTS, DISCOVERED THAT THE EXTERIOR EMERGENCY LIGHTS DO NOT TURN ON. SUMMARY OF NRC 00593: EMERGENCY LIGHTING PROBLEM FAULT ISOLATION WAS PERFORMED PER B717 FRM FIM 33-50-00 810-801. THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY B5-125 WAS REPLACED PER B717 AMM 33-51-06. TEST OK. (LP #2941244)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON PAN FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00063: PAN OF FWD UPPER CORNER AT PASSENGER DOOR L1 WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-40-04-0G. (LP #2936954)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON INTERNAL STRUCTURE AT AFT CARGO DOOR. SUMMARY OF NRC 00072: INTERNAL STRUCTURE AT AFT CARGO DOOR WAS REPAIRED PER ERA 610790-14 REV ORIGINAL. SECTION I: PERMANENT REPAIR AND PRI REV. 2. (LP #2931572)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

DENT #9 OUT OF LIMITS ON LOWER SURFACE OF AFT MOVABLE FLAP VANE AT RH WING. SEPARATE ITEMS ON NRC 00101. SUMMARY OF NRC 563: DENT #9 ON LOWER SURFACE OF AFT MOVABLE FLAP VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R REPAIR 1. (LP #2925376)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON DOUBLER AND FILLER DOOR JAMB AT FWD CARGO DOOR. SUMMARY OF NRC 00084: REPAIR DOUBLER ON AFT INNER PAN SECTION DOOR JAMB AT FWD CARGO DOOR WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. AND REPAIR FILLER DOES NOT EXIST BECAUSE THE REPAIR WAS PERFORMED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. (LP #2907992)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON CUSP WEB BTW STA 715 AND STA 737 LH SIDE (CPAX). SUMMARY OF NRC 00271: CUSP WEB BTW STA 715 AND STA 737 LH SIDE (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R-PROCEDURE 4. (LP #2907552)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON CUSP WEB BTW STA 696 AND STA 715 LH SIDE (CPAX). SUMMARY OF NRC 00272: CUSP WEB BTW STA 696 AND STA 715 LH SIDE (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #2901920)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACKS ON UPPER AFT CORNERS STA Y=636, Y=696 , Y=832 AND LOWER AFT CORNER STA Y=870 OF RH RING PANS AT INNER STRUCTURE OF PAX CABIN. SUMMARY OF NRC 00309: REPAIR ON UPPER AFT CORNERS STA Y=636, Y=696, Y=832 AND LOWER AFT CORNER STA Y=870 OF RH RING PANS AT INNER STRUCTURE OF PAX CABIN WAS PERFORMED PER B717-200 SRM 56- 20-02-2R-1 REPAIR 1 PAR 5 B. (LP #2901924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACKS ON UPPER FWD CORNER STA Y=756, LOWER FWD CORNERS STA Y=794, Y=851, Y=908, AND UPPER AFT CORNERS STA Y=832, Y=870, Y=889 OF LH RING PANS AT INNER STRUCTURE OF PAX CABIN. SUMMARY OF NRC 00311: REPAIR ON UPPER FWD CORNER STA Y=756, LOWER FWD CORNERS STA Y=794, Y=851, Y=908, AND UPPER AFT CORNERS STA Y=832, Y=870, Y=889 OF LH RING PANS AT INNER STRUCTURE OF PAX CABIN WAS PERFORMED PER B717-200 SRM 56-20-02-2R-1 REPAIR 1 PAR 5 B. (LP #2901929)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,299 hrs · 28,175 cycles

CORROSION ON CHANNEL AT GENERATION FLOOR 221SF OF PAX CABIN. SUMMARY OF NRC 00350: CHANNEL (PANEL) OF GENERATION FLOOR 221SF AT PAX CABIN WAS FABRICATED AND REPLACED PER DWG 9952521 REV. AH, DAL P.S. 900-7-1-1 NO. 03 PAR 4E AND B717-200 SRM 51-20-05-0G PAR 4. (LP #2903093)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,299 hrs · 28,175 cycles

AFTER CORROSION REMOVAL AT FLOOR SUPPORTS RH SIDE: #1 FROM STA Y=148 TO STA Y=200 AND - X7, #4 FROM STA Y=180 AND -X26, AND #6 FROM STA Y=160 TO STA Y=200 AND -X53 AT PAX CABIN WERE FOUND OUT OF LIMITS. SUMMARY OF NRC 00437: CORROSION LEVEL 2. FLOOR SUPPORTS RH SIDE: #1 FROM STA Y=148 TO STA Y=200 AND -X7, #4 FROM STA Y=180 AND -X26, AND #6 FROM STA Y=160 TO STA Y=200 AND -X53 AT PAX CABIN WERE REPLACED PER DRAWING 9936534 REV BW AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 10. (LP #2903456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACK ON ATTACH ANGLE APPROX STA 1178 CANT BTW LONGERON 1LH AND LONGERON 3LH AT EMPENNAGE AREA. SUMMARY OF NRC 00035: REPAIR ON ATTACH ANGLE APPROX STA 1178 CANT BTW LONGERON 1LH AND LONGERON 3LH AT EMPENNAGE AREA WAS PERFORMED PER 717-200 SRM 53-30-01-2R REP 1 STEP 6 A. (LP #2902099)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,299 hrs · 28,175 cycles

CORROSION ON FLOORS SUPPORTS (9 EA) LH SIDE: #1 FROM STA Y=160 TO STA Y=197 AND +X=55, #2 FROM STA Y=200 AND +X 55, #3 FROM STA Y=186 TO STA Y=195 AND +X=52, #4 FROM STA Y=160 TO STA Y=197 AND +X44, #5 FROM STA Y=180 AND +X=25, #6 FROM STA Y=195 TO STA Y=200 AND +X=14, #7 FROM STA Y=200 AND +X=11, #8 FROM STA Y=148 TO STA Y=200 AND +X=7, AND #9 FROM STA Y=200 AND X=0 AT PAX CABIN. SUMMARY OF NRC 00167: CORROSION LEVEL 2. FLOORS SUPPORTS (9 EA) LH SIDE: #1 FROM STA Y=160 TO STA Y=197 AND +X=55, #2 FROM STA Y=200 AND +X 55, #3 FROM STA Y=186 TO STA Y=195 AND +X=52, #4 FROM STA Y=160 TO STA Y=197 AND +X44, #5 FROM STA Y=180 AND +X=25, #6 FROM STA Y=195 TO STA Y=200 AND +X=14, #7 FROM STA Y=200 AND + X=11, #8 FROM STA Y=148 TO STA Y=200 AND +X=7, AND #9 FROM STA Y=200 AND X=0 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2900148)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,299 hrs · 28,175 cycles

CORROSION OUT OF LIMITS ON STA=994 TO STA=1053. ORIGINAL THICKNESS OF 0.052 IN. AND MINIMUM REMAINING THICKNESS IS 0.009 IN ON SIDE PARTS, THEREFORE AREAS ARE OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 PAR 4 FIG 101 AND PER DC-MD/BOEING NDT SPM PAR 4 FIG 9. SUMMARY OF NRC 00472: CORROSION LEVEL 2. RH TIE TRACK BTW STA=994 TO STA=1053 WAS REPLACED PER B717-200 SRM 51-40-04-0G. (LP #2901609)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

HOLE AT UPPER SKIN AND PROTUBERANCE AT LOWER SKIN OF RH ELEVATOR BETWEEN XHS 122.241 AND XHS 104.000 (ER/A RELATED 610064-14). SUMMARY OF NRC 00460: UPPER SKIN AND PROTUBERANCE AT LOWER SKIN OF RH ELEVATOR BETWEEN XHS 122.241 AND XHS 104.000 WAS REPAIRED PER B717-200 SRM 51-70-13-2R PROCEDURE 1 REPAIR 1. (LP #2900356)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

DENT ON LOWER SURFACE OF AFT MOVABLE VANE AT LH FLAP. SUMMARY OF THE NRC 00359: AFT MOVABLE VANE AT LH FLAP WAS REMOVED PER B717 AMM 27-50-03 AND DENT REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND SRM 57-53-01 FIG 201. REFER TO AMDS 2750-4007 FOR COMPLETION OF THE AFT MOVABLE VANE INSTALLATION AT LH FLAP. (LP #2895218)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

CRACKS ON STRINGERS 6LH, 8LH AND 6RH STA Y=1022 AT INTERNAL FUSELAGE (PAX CABIN). SUMMARY OF NRC 00153: REPAIR ON STRINGERS 6LH, 8LH AND 6RH STA Y = 1022 AT INTERNAL FUSELAGE WAS PERFORMED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 PAR 5 FIG 201. (LP #2891854)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,299 hrs · 28,175 cycles

AD RELATED. FERRY FLIGHT ER/A 610173-14 REMOVES ALL PAX SEATS FROM A/C AND TRACKS ACCOMPLISHEMENT OF PERMANENT REPAIR. ASSOCIATED ER/A 14-610173 ADDED FOR AC 9558. COMPLIED WITH ERA 610173-14 REVISION ORIGINAL SEC I STEPS 1, 2, 3, 4, AND 5. IN REFERENCE TO ER/A 610173-14AD REV.ORIGINAL, SECTION II PERMANENT REPAIR WAS ACCOMPLISHED. (LP #2842819)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,927 hrs · 27,120 cycles

THE AFT EMERGENCY LIGHT ABOVE AFT F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY B5-116 PER AMM 33- 51 AND RELAMPED AS NEEDED. OPERATIONAL CHECK GOOD. (LP #6140482)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,927 hrs · 27,120 cycles

THE THREE (3) AFT ACCESSORY SIDEWALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY B5-116 PER AMM 33- 51 AND RELAMPED AS NEEDED. OPERATIONAL CHECK WAS GOOD. (LP #6140483)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,610 hrs · 26,877 cycles

THE EMERGENCY EXIT SIGNS ABOVE 1L DOOR, 1L F/A SEAT, 1R DOOR, AND CENTER AISLE 1 ABCD ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS AT B5-259 AND B5-235 PER AMM 33-51. OPERATIONAL CHECKS ARE NOW GOOD. (LP #5929639)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 39,241 hrs · 26,612 cycles

THRESHOLD LIGHT LENS COVER DAMAGED ABOVE AFTJUMPSEAT. FORWARD TO MEL 33-52-01. PLACARDS INSTALLED. R&R LENS COVER IAW B717 AMM 33-25. OK FOR SERVICE. MCO/PLAC REMOVED. (LP #1099186)

Part: CLAMP — DISCONNECTED (DRAIN LINE) · airframe 39,107 hrs · 26,517 cycles

THE AFT EMERGENCY EXIT LIGHT SPONTANEOUSLY COMES ON AND OFF. IT WAS ALSO NOTED THAT THERE IS WATER IN THAT AREA OF THE CEILING. MAINTENANCE FOUND A DRAIN LINE HOSE CLAMP DISCONNECTED, RESECURED IT AS REQUIRED. LEAK NO LONGER OCCURS. THE NR 4 EMERGENCY BATTERY PACK WAS REPLACED PER AMM 33-51. THE EMERGENCY LIGHTS NOW OPERATE PROPERLY. THE AIRCRAFT IS OK FOR SERVICE. (LP #1074674)

Part: LENS — MISSING (CABIN) · airframe 38,231 hrs · 25,904 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING AT 604 INTERIOR. RE-INSTALLED DIFFUSER LENS AT ROW 20. (LP #0911582)

Part: NOT REPORTED — MALFUNCTIONED (LT MLG) · airframe 38,119 hrs · 25,822 cycles

ON TAKEOFF WE RECEIVED A "GEAR DOOR OPEN" ALERT WITH GEAR HANDLE IN THE UP POSITION. ALSO A "LEFT GEAR UNSAFE" RED LIGHT WAS ILLUMINATED. NO SOUNDS OR VIBRATIONS NOTED FROM THE COCKPIT OR CABIN CREW. CHECKLIST 14.7 & 14.8 WERE RUN WHILE TALKING TO MAINTENANCE AND FLIGHT OPERATIONS. ALTERNATE LANDING GEAR EXTENTION PROCEDURES WERE NOT UTILIZED. DURING THE LANDING, SPARKS WERE NOTICED ON RUNWAY SO THE AIRCRAFT WAS TOWED BACK. MAINTENANCE REPLACED THE LEFT MLG DOOR PER AMM 32-14. JACKED AC PER AMM 07-11 AND A GEAR SWING WAS PERFORMED PER AMM 32-30. ALL GEAR OPERATIONS ARE NORMAL AT THIS TIME. (LP #4845186)

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,096 hrs · 25,807 cycles

IN FLIGHT AFT EXIT SIGN FLASHING. ON GROUND LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED AFT EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PER B717 AMM 33-51. TEST WAS GOOD. (LP #4845162)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,048 hrs · 25,779 cycles

THE AFT EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4845153)

Part: SKIN — CRACKED (VERTICAL STAB LE) · airframe 37,693 hrs · 25,541 cycles

THE VERTICAL STAB LEADING EDGE SKIN COMMON TO THE RHS FRONT SPAR IS CRACKED COMMON TO THE 2ND FASTENER HOLE AS SEEN IN FIG 1. AN EXISTING EXTERNAL REPAIR IS INSTALLED ON THE LEADING EDGE SKIN IMMEDIATELY BELOW ZFS=52.267, INSTALLED IN 2016 PER SG95550001 AND AA WORK CARD 5530-01048-03 DOC VIA LOG PAGE 2760104. THIS ER/A REVISION REMOVES THE LIMITED AND PREVIOUS REPAIR DOUBLER AND INSTALLS A SINGLE DOUBLER. COMPLIED WITH ER/A 569539-14AD REV A. (LP #0814729)

Part: FRAME — CRACKED (BS 674) · airframe 37,693 hrs · 25,541 cycles

OVERWING FRAME AT STA Y=674.0 RH SHOWS CRACK GREATER THAN 0.125 DURING GVI. NRC 040-0003:5310-01436-01C/001 00021 FRAME REPLACEMENT ON AMDS CARD 5310-01436-03B HAS BEEN COMPLIED WITH. (LP #0814612)

Part: LONGERON — NONE (BS 668) · airframe 37,693 hrs · 25,541 cycles

CUT LONGERON 11RT AT APPROX. STA 668 FOR FRAME REMOVAL. NRC 040-0003:5310-01436-01C/002 00153: REPAIRED REF ER/A 530437-14MA REV O. (LP #0810425)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,785 hrs · 24,914 cycles

THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHTS BATTERY PACK AND CHARGER IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 36,519 hrs · 24,727 cycles

THE OUTSIDE WING EMERGENCY LIGHTS REMAIN ILLUMINATED AFTER TESTING. MAINTENANCE REPLACED THE THE OVERWING LIGHTS POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD. AIRCRAFT IS OK FOR SERVICE.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 36,330 hrs · 24,586 cycles

THE UPPER EMERGENCY LIGHTS AT 20DC AND 20B WERE FOUND TO BE INOPERATIVE. MAINTENANCE CYCLED THE EMERGENCY SWITCH AND ALL OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,179 hrs · 24,470 cycles

THE EMERGENCY EXIT SIGN ABOVE L1 F/A SEAT IS INOPERATIVE. MAINTENANCE TROUBLESHOT IAW ASM 33-51-0 AND REPLACED THE B5-235 BATTERY PACK IAW AMM 33-51. SYSTEM CHECKED OK.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 35,984 hrs · 24,328 cycles

THE TAIL CONE EMERGENCY EXIT LIGHT ILLUMINATED ON THE GROUND UNCOMMANDED. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY EXIT LIGHT POWER SUPPLY PER AMM 33-51. THE LIGHT CHECKS GOOD AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,261 hrs · 23,819 cycles

AFT ACCESSORY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-260 IAW AMM 33-51. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 33,848 hrs · 22,788 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 19C. FLOOR MOUNTED LIGHTING ALL OK. OVERHEAD EMERGENCY LIGHT AT ROW 19 MISSING LENS, INSTALLED LENS.

Part: SKIN — DELAMINATED (SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK L/H O/B SPOILER FOUND DELAMINATED.

Part: LENS — BROKEN (EXIT SIGN) · airframe 32,759 hrs · 21,973 cycles

THE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS BROKEN. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,718 hrs · 21,942 cycles

CRACK IN SKIN AT TOP FASTENER AT STA 1152 JUST BELOW DORSAL FIN ON LEFT SIDE. REPAIRED SKIN CRACK AT STA 1152 L/H IAW ERA 549634-14 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,718 hrs · 21,942 cycles

CRACK IN SKIN AT TOP FASTENER AT STA 1152 JUST BELOW DORSAL FIN ON RIGHT SIDE. REPAIRED SKIN CRACK AT STA 1152 RT IAW ER/A 549635-14 REV 0.

Part: SKIN — BENT (CARGO DOOR) · airframe 32,716 hrs · 21,940 cycles

FWD LOWER CORNER OF DOOR SKIN BENT. CUT OUT DAMAGED AREA IAW SRM 52-00-01 FIG 202, FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SRM 52-00-01 REPAIR 8 AND INSTALLED IAW SRM 52-00-01 REPAIR 8.

Part: SHEAR TIE — CRACKED (BS 1152) · airframe 32,716 hrs · 21,940 cycles

FRAME SHEAR TIE CRACKED BS 1152 STRINGERS 2R AND 2L. REPLACED THE SHEAR TIE IAW SRM 51-41-05.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

RIGHT INBOARD SEAT TRACK IS CORRODED ON TOP FORWARD END. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 32,716 hrs · 21,940 cycles

SEVERAL FASTENER HOLES OF THE VERTICAL STABILIZER LEADING EDGE STRUCTURE EXHIBIT EVIDENCE OF DISTRESS AT SPLICE STATION ZFS-52.267 IAW JC 5530-01048-01. REPAIRED IAW DRAWING SG95550001 AND WORK CARD 5530-01048-03.

Part: STRUCTURE — CORRODED (BS 160-200) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

CORROSION ON SUB FLOOR AT BS 160-200 AT RBL 50. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. PG 101 STEP 4. REPAIRED IAW ER/A 551819-14MA REV 0.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

FLOORBEAM AT BS 200, RBL 9 TO 43 HAS LIGHT CORROSION AROUND FASTENER HOLES. BLEND CORROSION IAW SRM 53-00-00 FIG 103. REPLACED THE FLOORBEAM IAW SRM 51-41-02, 51-41-05.

Part: STRUCTURE — CHAFED (NR 2 NACELLE) · airframe 32,716 hrs · 21,940 cycles

NR 2 PYLON APRON UPPER SIDE AT THE NR 4 UPPER COWL HINGE APRON HAS CHAFED FLANGE. BLENDED CHAFE DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-00 FIG 103. REPAIRED IAW SRM 54-50-02 REPAIR 2.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 32,716 hrs · 21,940 cycles

CRACK IN A SHEAR TIE AT BS 1022 FWD SIDE OF THE BULKHEAD AT LONGERON 14R. REPLACED THE SHEAR TIE IAW SRM 51-41-05 PARA 2.

Part: STRAP — CORRODED (BS 994) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

BS 994 LBL 15 FRAME STRAP CORRODED INBD SIDE OF LT SEAT TRACK. BLENDED THE FRAME STRAP IAW SRM 53-00-00 FIG 103. REPLACED THE STRAP IAW SRM 51-41-05.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 32,716 hrs · 21,940 cycles

CRACK IN A SHEAR TIE AT BS 1022 AFT SIDE OF THE BULKHEAD AT LONGERON 14R. REPLACED THE SHEAR TIE IAW SRM 51-41-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,716 hrs · 21,940 cycles

FORWARD CARGO STA 636, BL0 INTERCOSTAL AFT ANGLE CRACKED. REPAIRED AFT CRACKED ANGLE ON INTERCOSTAL AT STA 636 BL0 IAW SRM 53-00-00 REPAIR 1 AND DWG 9936580 REV BZ.

Part: FLOOR SUPPORT — CORRODED (BS 186) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

UPPER SURFACE OF FLOOR SUPPORT AT BS 186 HAS LIGHT CORROSION AROUND THE FLOOR PANEL FASTENER HOLES AND FOUND OUT OF LIMITS IAW SRM 53-00-00. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-41-05.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,718 hrs · 21,942 cycles

DOOR CUTOUT LWR SEAL SPLICE ANGLE CORRODED. SEAL SPLICE CORRODED THROUGH, 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. FABRICATED NEW SEAL SPLICE OUT OF 7075-0 TAG 1713722 IAW DWG 5910158. HEAT TREATED FROM 7075-0 TO 7075-T6 ON CWO 72689-0004. INSTALLED SEAL RETAINER IAW SRM 51-41-02 SEC 4.

Part: CUSP WEB — CRACKED (BS 219) · airframe 32,716 hrs · 21,940 cycles

CUSP WEB CRACKED AT BS 219 RBL 46. REPLACED THE CUSP WEB IAW DWG 9930538, SRM 51-41-02, AND 51-41-05.

Part: CUSP WEB — CRACKED (BS 717) · airframe 32,716 hrs · 21,940 cycles

BS 717 LBL 45 CUSP WEB CRACKED. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.

Part: CUSP WEB — CRACKED (BS 237) · airframe 32,716 hrs · 21,940 cycles

CUSP WEB CRACKED AT STA 237 AT RBL 50. TRIMMED OUT THE DAMAGE, AND INSTALLED A FILLER & DOUBLER REPAIR. REPAIR FABRICATED IAW SRM 53-00-55 REPAIR 4. FIG 203.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 32,716 hrs · 21,940 cycles

CRACK IN A SHEAR TIE AT BS 1022 FWD SIDE OF THE BULKHEAD AT LONGERON 14L. REPLACED THE SHEAR TIE IAW SRM 51-41-05.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

LEFT WING UPPER FUEL PANEL 520DT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00 00-410.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

LT WING UPPER FUEL PANEL 520CT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

RT WING UPPER FUEL PANEL 620AT MATING SURFACE HAS CORROSION. REPLACED ACCESS PANEL IAW AMM 28-00-00 410.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 32,716 hrs · 21,940 cycles

RT WING UPPER FUEL PANEL 620DT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,051 hrs · 18,307 cycles

TAIL COMPARTMENT CATWALK MIDDLE EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,051 hrs · 18,307 cycles

TAIL COMPARTMENT AFT HANDRAIL EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 28,051 hrs · 18,307 cycles

TAIL COMPARTMENT AFT HANDRAIL EMER LIGHT LENS COVER CRACKED. R & R COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,263 hrs · 17,769 cycles

RIGHT OVERWING EMER EVACUATION LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

SEAT TRACK CORRODED BETWEEN FS 899 TO 1002 RBL 44. R & R SEAT TRACK IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222AHF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222QF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

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

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222 AGF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222UF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222TF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 221VF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 27,263 hrs · 17,769 cycles

MAIN CABIN FLOORBOARD PANEL 222JF DELAMINATED. R & R PANEL IAW SRM.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 27,263 hrs · 17,769 cycles

FORWARD ENTRY DOOR EXTERNAL SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: MOUNT BRACKET — LOOSE (R1 DOOR) · airframe 27,263 hrs · 17,769 cycles

R1 DOOR EMER EVAC SLIDE COVER LOWER MOUNTING BRACKET LOOSE AT DOOR LOWER FRAME. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 27,263 hrs · 17,769 cycles

FORWARD CARGO DOOR BARRIER INNER SKIN CRACKED AT CTR & REAR AREA 10 INCHES TO LOWER EDGE. REPAIRED SKIN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

FORWARD CARGO COMPARTMENT DOOR JAM LOWER SILL PAN CORRODED. REPAIRED PAN IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

CUSP WEB CRACKED BETWEEN BS 484 TO 503 RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

CUSP WEB CRACKED BETWEEN BS 541 TO 560 RBL 56. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

RIGHT CUSP WEB CORRODED AT STATION 503 TO 522 RBL 56. REPAIRED WEB IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

SPLICE CORRODED BETWEEN BS 579 TO 598 RBL 56. R & R SPLICE IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

CUSP WEB CORRODED BETWEEN BS 560 TO 579 RBL 56. R & R CUSP WEB IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 27,263 hrs · 17,769 cycles

R1 DOOR EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 522 TO 541. REPAIRED CUSP WEB IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

DOUBLER CORRODED BETWEEN BS 636 TO 655 LBL 56. R & R DOUBLER IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

CUSP WEB CORRODED BETWEEN BS 560 TO 579 LBL 56. REPAIRED CUSP WEB IAW SRM.

Part: COVER PLATE — CORRODED (R1 DOOR) · airframe 27,263 hrs · 17,769 cycles

R1 DOOR ENTRY COVER PLATE CORRODED BETWEEN BS 160 TO 200, RBL 54. R & R PLATE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,263 hrs · 17,769 cycles

WEB CORRODED AT BS 200 LBL 42. REPAIRED WEB IAW SRM.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 27,275 hrs · 17,778 cycles

R1 DOOR EMERGENCY EVAC SLIDE FOUND LOWER PARACHUTE PIN LOOSE. R & R SLIDE IAW AMM.

Part: COVER — UNSECURE (R1 DOOR) · airframe 27,275 hrs · 17,778 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK COVER INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED COVER IAW AMM.

Part: FIXTURE — DIRTY (GIRT BAR) · airframe 26,976 hrs · 17,586 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FIXTURE DIRTY. CLEANED FLOOR FIXTURE IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,392 hrs · 17,207 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 25,320 hrs · 16,513 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: LANYARD — LOOSE (L1 DOOR) · airframe 25,299 hrs · 16,500 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK LOOSE. LANYARD AT CENTER OF BAR LOOSE. SECURED LANYARD ASSEMBLY TO SLIDE DOOR CLIP IAW MM.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 25,140 hrs · 16,406 cycles

TAILCONE EMERGENCY EXIT O/H LIGHT FLICKERED. REMOVED AND REPLACED BATTERY PER AMM.

Part: LANYARD — DISCONNECTED (L1 DOOR) · airframe 24,617 hrs · 16,086 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD DISCONNECTED FROM DOOR. RECONNECTED LANYARD PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,605 hrs · 16,078 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

SKIN CORRODED AT BS 833, LONGERON 29R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

AFT CARGO FWD & AFT SPLICES ON DOOR CUTOUT PAN CORRODED. REMOVED AND REPLACED ANGLES IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

FRAME CORRODED AT STA 908, L30. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

FRAME CORRODED AT STA 889, L30. REMOVED AND REPLACED FRAME IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 24,009 hrs · 15,708 cycles

MAIN CABIN FLOOR PANEL 221KF DELAMINATED INSERT. REMOVED AND REPLACED PANEL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

FRAME CORRODED AT STA 927, BETWEEN L30R TO L29R. REMOVED AND REPLACED FRAME IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 24,009 hrs · 15,708 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS BOTH FWD & AFT CORRODED. REMOVED AND REPLACED FITTINGS IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

LONGERON CORRODED BETWEEN BS 948 TO BS 956, 29L. REMOVED AND REPLACED LONGERON IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 24,009 hrs · 15,708 cycles

NLG STRUT DOOR, RIGHT AFT CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER IAW SRM.

Part: DOOR — CRACKED (RT WING) · airframe 23,833 hrs · 15,599 cycles

2 SCREW ON ACCESS PANEL RT WING BETWEEN 2 INNER FLAP ACTUATOR CRACKED IN METAL DOOR. REMOVED AND REPLACED DOOR PER AMM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 23,416 hrs · 15,341 cycles

R-1 DOOR SLIDE PAC PARTIALLY DISLODGED. SECURED R-1 DOOR SLIDE PAC PER AMM. OK FOR SERVICE.

Part: RETAINER — BROKEN (R1 DOOR) · airframe 23,416 hrs · 15,341 cycles

R-1 GIRT BAR RETAINER BROKEN ON ONE SIDE. (INTERIM SECURED). REMOVED AND REPLACED SERVICE DOOR ESCAPE SLIDE DOOR COVER; OP'S CHECKS GOOD ON GIRT BAR.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 23,280 hrs · 15,250 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK LOOSE. REMOVED AND REPLACED SLIDE IAW MM.

Part: GUIDE — LOOSE (EVAC SLIDE) · airframe 22,568 hrs · 14,794 cycles

TAIL CONE SLIDE LANYARD AFT GUIDE LOOSE FROM SLIDE COVER. SECURED LANYARD GUIDE PER AMM.

Part: COVER — MISSING (CABIN) · airframe 21,976 hrs · 14,405 cycles

AFT EEPLS COVER MISSING. INSTALLED COVER IAW MM.

Part: COVER — MISSING (CABIN) · airframe 21,976 hrs · 14,405 cycles

FWD EEPLS COVER MISSING. INSTALLED COVER IAW MM.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 21,976 hrs · 14,405 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD CABLE ASSY FRAYED. REMOVED AND REPLACED LANYARD ASSY.

Part: COVER — MISSING (CABIN) · airframe 21,976 hrs · 14,405 cycles

MID EEPLS COVER MISSING. INSTALLED COVER IAW MM.

Part: LANYARD — DETACHED (EVAC SLIDE)

GALLEY DOOR SLIDE PIN CAME OFF. R-1 RE-ATTACH GALLEY DOOR SLIDE LANYARD IAW AMM 25-61-03. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT)

LIGHT LENS MISSING SEAT 1D. INSTALLED LIGHT LENS CHECKS GOOD REF MM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOTH OVERWING EMERGENCY LIGHTS STAY ON IN ARM POSITION. RELAMPED BOTH OVERWING EMERGENCY LIGHTS. REPLACED BATTERY PACK AND RELAY R2-273. OPS CHECK OK. REF MM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOTH OVERWING EMERGENCY LIGHTS STAY ON IN ARM POSITION. RELAMPED BOTH OVERWING EXIT LIGHTS. REPLACED BATTERY PACK AND RELAY R2-273. OPS CHECK OK REF MM 33-51.

Part: LIGHT — INTERMITTENT (CABIN)

OVERWING EXTERIOR EMERGENCY LIGHTS FLICKERING AT GATE. CYCLED EMERGENCY LIGHT SWITCH IN COCKPIT AND F/A STATION.

Part: FRAME — DAMAGED (BS 1178)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2989.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY OVERWING EXIT IDENTIFIER LIGHT FOUND INOPERATIVE WHILE PERFORMING SVC TASK CARD 601; B-5-119. REPLACED BATTERY SUPPLY ASSEMBLY AND BATTERY AT B-5-119 IAW B717 MM 33-51-03. OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT LOWER DOOR JAMB PAN HAS EVIDENCE OF CORROSION IN SEVERAL AREAS. INSTALLED AFT CARGO DOOR JAMB LOWER PAN CORROSION DAMAGE SPLICE REPAIR IAW B717 SRM 53-20-15 FIG 201 REPAIR 7.