N996AT

Part: BATTERY — MALFUNCTIONED (ZONE 200) · airframe 58,159 hrs · 41,058 cycles

EMERGENCY EXIT LIGHT ON TOP OF TAILCONE IS INTERMITTENTLY FLASHING. MAINTENANCE REPLACED THE BATTERY AND BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6449074)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 57,622 hrs · 40,575 cycles

INTERIOR OVERWING EMERGENCY LIGHT LEFT & RIGHT LOWER LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY PER B717 AMM 33-51 AT LOCATION B5-119. OPERATIONAL CHECK OK. (LP #6208055)

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 57,151 hrs · 40,163 cycles

SHIP 9542 -HYD/DE- LOSS OF RIGHT HYDRAULIC SYSTEM ON APPROACH REQUIRING A MANUAL GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE HYDRAULIC REVERSABLE PUMP (PTU) WAS LEAKING INTERNALLY AND REPLACED IT ALONG WITH THE RIGHT SYSTEM RESERVOIR. (LP #5549470)

Part: NOT REPORTED — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

-AD- CORRORION WAS FOUND ON LH HORIZ STAB BARREL NUT HOLE #26. SUMMARY OF NRC 00719: CORROSION LEVEL 2. LH HORIZ STAB BARREL NUT HOLE #26 WAS REPAIRED PER ER/A 616773-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616773-14 REV 1. ASSOCIATED ER/A 14-616773 ADDED FOR AC 9542. (LP #0306775)

Part: SKIN — DAMAGED (BS 1133 L1-3L) · airframe 57,066 hrs · 40,091 cycles

-AD- CRACK ON SKIN DRILL FOUND. SUMMARY OF NRC 00852: FUSELAGE SKIN STA 1133 BTW L1-L3LH WAS REPAIRED PER ER/A 617266-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617266-14 REV 5. ASSOCIATED ER/A 14-617266 ADDED FOR AC 9542. (LP #0305492)

Part: UNKNOWN — CRACKED (HORIZONTAL STAB) · airframe 57,066 hrs · 40,091 cycles

CRACK ON LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 AT RH ELEVATOR. SUMMARY OF NRC 00385: LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 OF RH ELEVATOR WAS REPAIRED PER ER/A 616815-14 REV ORIGINAL SECTION I: PERMANENT REPAIR ACCOMPLISH SECTION II REPETITIVE INSPECTIONS WITHIN EVERY 3,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF ER/A 616815-14, REV ORIGINAL, SECTION I: PERMANENT REPAIR. REFER TO LP #0297057. ASSOCIATED ER/A 14-616815 ADDED FOR AC 9542. (LP #0304615)

Part: SPAR CAP — DAMAGED (RT WING TE) · airframe 57,066 hrs · 40,091 cycles

PERFORM PERMANENT REPAIR ON RH WING TRAILING EDGE LOWER SPAR CAP DUE TO MISDRILLED HOLES WITH TIME LIMITED REPAIR. SUMMARY OF NRC 00856: RH WING TRAILING EDGE LOWER SPAR CAP WAS REPAIRED PER PRI 608531-14 REV 1 AND ERA #608531-14 REV C. SECTION II: TIME LIMITED REPAIR. ASSOCIATED ER/A 14-608531 ADDED FOR AC 9542. (LP #0302344)

Part: VANE — DEBONDED (LT TE FLAP) · airframe 57,066 hrs · 40,091 cycles

SEVEN DISBONDS WERE FOUND ON LH AFT MOVABLE VANE LOWER SKIN, 1) LENGTH 1.550IN AND WIDTH 1.125IN, 2) LENGTH 1.000IN AND WIDTH 0.850IN, 3) LENGTH 1.250IN AND WIDTH 0.850IN, 4) LENGTH 1.250IN AND WIDTH 1.250IN, 5) LENGTH 1.250IN AND WIDTH 1.250IN, 6) LENGTH 1.375IN AND WIDTH 1.125IN, AND 7) LENGTH 1.000IN AND WIDTH 1.000IN (IN REFERENCE MON/9542/0131674 JOB # 006-0001). SUMMARY OF NRC 00412: LH AFT MOVABLE VANE WAS REPAIRED PER PRI 616844-14 REV 1 AND ER/A 616844-14 REV ORIGINAL. ASSOCIATED ER/A 14-616844 ADDED FOR AC 9542. (LP #0295849)

Part: GUIDE VANE — DAMAGED (RT TE FLAP) · airframe 57,066 hrs · 40,091 cycles

DAMAGE T DURING TEST OF FLIGHT SPOILER ACTUATOR. FLAPS WAS RETRACTED AND RH FLAP GUIDE VANE WAS DENTED WITH INDB FLAP INGE SUPPORT BRACKET (HINGE FAIRING REMOVAL). SUMMARY OF NRC 00077: RH FLAP GUIDE VANE WAS REPAIRED PER PRI 616775-14 REV 2 AND ER/A 616775-14 REV ORIGINAL. ASSOCIATED ER/A 14-616775 ADDED FOR AC 9542. (LP #0295551)

Part: BEAM — CRACKED (FWD CARGO) · airframe 57,066 hrs · 40,091 cycles

CRACK ON BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00221: BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1 WAS REPAIRED PER PRI 616929-14 REV 1 AND ERA 616929-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-616929 ADDED FOR AC 9542. (LP #0292261)

Part: ANGLE — CORRODED (BS 748) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION WAS FOUND IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0. SUMMARY OF NRC 00803: CORROSION LEVEL 2. CORROSION IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0 WAS REPAIRED PER PRI 616932-14 REV 4 AND ER/A 616932-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-616932 ADDED FOR AC 9542. (LP #0291161)

Part: FRAME — DAMAGED (BS 994 L26-27R) · airframe 57,066 hrs · 40,091 cycles

ELONGATE HOLES AND WRONG DRILLED ON FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00674: FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMEN WAS REPAIRED PER PRI 616818-14 REV 2 AND ERA 616818-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616818 ADDED FOR AC 9542. (LP #0290409)

Part: PAN — CORRODED (AFT CARGO) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON LOWER PAN AREA AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 0070: CORROSION LEVEL 2. LOWER PAN AREA AT AFT CARGO DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G AND WAS REPAIRED PER B717-200 SRM 53-00-15-2R PROCEDURE 1. (LP #0289228)

Part: DOUBLER — CORRODED (AFT CARGO) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0273: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PER PRI 616616-14 REV 2 AND ER/A 616616-14 REV ORIG SECTION I. SEC II ACCOMPLISH A REPETITIVE GENERAL VISUAL INSPECTION WITHIN EVERY 8,000 CYCLES AFTER SECTION I ACCOMPLISHMENT. UNDER LOGPAGE # 0283249. ASSOCIATED ER/A 14-616616 ADDED FOR AC 9542. (LP #0288688)

Part: SKIN — CRACKED (BS 1022 S8-9L) · airframe 57,066 hrs · 40,091 cycles

CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L WAS REPAIRED PER PRI 616777-14 REV 1 AND ERA 616777-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.

Part: SCREW — DAMAGED (HORIZONTAL STAB) · airframe 57,066 hrs · 40,091 cycles

AD - BURRS WERE FOUND ON THE THREADS OF THE ACME SCREW AT THE HORIZONTAL STABILIZER. SUMMARY NRC 00437: HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS REPLACED UNDER AMDS 2740-01114-05. (LP #0282538)

Part: SKIN — DENTED (BS 588 L30) · airframe 57,066 hrs · 40,091 cycles

DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE. SUMMARY OF NRC 00338: DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE WAS REPAIRED PER PRI 616805-14 REV 1 AND ER/A 616805-14 REV ORIG. SECTION I. ACCOMPLISH SECTION II REPETITIVE INSPECTIONS WITHIN EVERY 8,000 CYCLES AFTER SECTION I IS ACCOMPLISHED PER ER/A 616805-14 REV ORIGINAL AND UNDER LOG PAGE 0277348. (LP #0277864)

Part: WEB — CORRODED (L1 DOOR FRAME) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH. SUMMARY OF NRC 00651: CORROSION LEVEL 2. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH WAS REPAIRED PER PRI 616779-14 REV 1 AND ER/A 616779-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. MAINTENANCE REQUIREMENTS WERE VERIFIED AND NO FURTHER ACTION ARE REQUIRED. ASSOCIATED ER/A 14-616779 ADDED FOR AC 9542. (LP #0276562)

Part: LONGERON — CORRODED (BS 1017-1049) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION WAS FOUND ON LONGERON 22LH FROM STA 1017/STA 1049 AND LONGERON ENDS 22LH AND 24 LH STA 1053. ALSO CORROSION ON SHIMS OF LONGERONS 22LH, 23LH, AND 24LH BTW STA 1037-1042 AND FILLERS AT STA 1053 AND STR 21LH/STR 23LH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00661: CORROSION LEVEL 2. LONGERON 22LH FROM STA 1017/STA 1049 WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2, 51-41-01-0G, AND 51-41-05-0G. END LONG 22LH AND 24 LH STA Y=1053 WERE REPLACED AND INSTALLED PER NRC 00819 AND 00010. ALSO SHIMS OF LONGERONS 22LH, 23LH, AND 24LH BTW STA 1037-1042 WERE FABRICATED PER DWG 543604 REV EG. AND INSTALLED ON NRC 00010. FILLER STA 1053 BTW STR 21LH TO 23LH WAS FABRICATED PER DWG 9918572 REV AA AND INSTALLED ON NRC 00010. (LP #0269752)

Part: LONGERON — OUT OF LIMITS (BS 944 L23L) · airframe 57,066 hrs · 40,091 cycles

THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.080 IN. REMAINING THICKNESS IS 0.043 IN. THEREFORE, IT IS OUT OF LIMITS. SUMMARY OF NRC 829: ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 3 REPAIR 3 PAR 4 A (1) FIG 201 (SHEET 2) DETAIL A-A AND PER B717 SRM 51-41-05-0G. (LP #0267200)

Part: TAB — CORRODED (RUDDER) · corrosion level 2 · airframe 60,513 hrs · 43,152 cycles

CORROSION ON SKIN LT & RT SIDE AT RUDDER TAB. REPLACED BY SERVICIABLE RUDDER CONTROL TAB (0266679).

Part: FLOOR SUPPORT — CORRODED (BS 200-214) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON RH FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN (W1). SUMMARY OF NRC 00464: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-08-0G AND 51-41-01-0G. (LP #0267742)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1). SUMMARY OF NRC 00468: CORROSION LEVEL 2. L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1) WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0264025)

Part: PAN — CRACKED (FWD CARGO) · airframe 57,066 hrs · 40,091 cycles

CRACKS ON PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00222: DAMAGED SECTIONS OF PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1 WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0264188)

Part: WINDOW FRAME — CRACKED (SLIDING WINDOW) · airframe 57,066 hrs · 40,091 cycles

CRACK WAS FOUND ON FRAME ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00802: UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIG 201 OPTION 2 FLAG NOTE E AND F. (LP #0262080)

Part: FRAME — CORRODED (BS 927 L29L-R) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION WAS FOUND ON PREVIOUS REPAIR SPLICES AND FRAME, STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT. SUMMARY OF NRC S/N 00339: CORROSION LEVEL 2. FRAME STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT CORROSION WAS REMOVED PER B717-200 51-10-04-0G PAR 26 C (1), (UT) THICKNESS MEASUREMENT INSPECTION ON FRAME STA Y=927 LONGERON 29LH TO 29RH. ORIGINAL THICKNESS IS 0.071" REMAINING THICKNESS IS 0.063" THEREFORE IT'S WITH IN LIMITS PER B717-200 SRM 53-00-01-1A AND ALLOWABLE DAMAGE GENERAL FIG 103 AND DC-MD/BOEING NDTSPM PART 4 04-00-06 PAR 4, AND REPAIR PARTS, NEW ANGLE AND NEW PLATE TO PREVIOUS REPAIR AT FRAME STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT WERE REPLACED PER B717-200 SRM 51-41-05-9G AND 53-20-07-2R REPAIR 3. (LP #0256138)

Part: CUSP WEB — CRACKED (BS 1012) · airframe 57,066 hrs · 40,091 cycles

CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN. SUMMARY OF NRC 00514: RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R. (LP #0255600)

Part: BEAM — CRACKED (AFT PRESS BLKHD) · airframe 57,066 hrs · 40,091 cycles

CRACK ON BEAM 1 LH EDGE AT AFT CABIN PRESSURE BULKHEAD. SUMMARY OF NRC 00097: WEB WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND DWG 9915565 REV BD. (LP #0256085)

Part: LONGERON — CRACKED (BS 1022 L17R) · airframe 57,066 hrs · 40,091 cycles

CRACKED LONGERON 17RH STA 1022 PAX CABIN. SUMMARY OF NRC 00353: LONGERON 17RH STA 1022 PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #0254033)

Part: FRAME — CRACKED (BS 1037 L17L) · airframe 57,066 hrs · 40,091 cycles

CRACKED LH FRAME STA 1037 AT LONG 17LH PAX CABIN. SUMMARY OF NRC 00449: LH FRAME STA 1037 AT LONG 17LH PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 4. (LP #0254275)

Part: DOUBLER — CORRODED (CARGO DOOR AREA) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 0069: CORROSION LEVEL 2. FWD AND AFT DOUBLERS OF FWD CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 PAR. 5. (LP #0253957)

Part: LONGERON — CRACKED (BS 1022 L17L) · airframe 57,066 hrs · 40,091 cycles

CRACKED LONGERON 17LH STA 1022 PAX CABIN. SUMMARY OF NRC 00352: LONGERON 17LH STA 1022 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #0254278)

Part: PAN — CRACKED (CARGO DOOR AREA) · airframe 57,066 hrs · 40,091 cycles

CRACK ON SPLICE AND PAN NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00219: SPLICE (REPAIR DOUBLER) NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1 WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON PREVIOUS REPAIR AT PAN NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1. NO CRACKS WERE FOUND PER DC-MD/BOEING NDTSPM PART 6, 06-10- 01.001.

Part: SKIN — DENTED (LT TE FLAP VANE) · airframe 57,066 hrs · 40,091 cycles

DENTS OUT LIMITS WERE FOUND ON REVALUATION DENTS OF LOWER SKIN FWR MOVABLE VANE FLAP AT LH WING. SUMMARY OF NRC 00659: PERMANENT REPAIR WAS PERFORMED ON FWD MOVABLE FLAP VANE (LOWER SKIN) OF LH WING PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #0248612)

Part: CUSP WEB — CRACKED (BS 636-655) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CRACK ON RH CUSP WEB STA X=-56 AND Y=636-655 ALSO CORROSION AND MISSING FASTENERS AT PASSENGER CABIN. SUMMARY OF NRC 00512: CORROSION LEVEL 2. RH CUSP WEB STA X=-56 AND Y=636-655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 215. (LP #0246400)

Part: CUSP WEB — CRACKED (BS 660) · airframe 57,066 hrs · 40,091 cycles

CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN. SUMMARY OF NRC 00513: RH SECTION CUSP WEB WAS FABRICATED AND REPAIRED ON STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 223. (LP #0246679)

Part: CUSP WEB — CORRODED (BS 568) · corrosion level 2 · airframe 57,066 hrs · 40,091 cycles

CORROSION ON RH CUSP WEB BTW STA X=-56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN. SUMMARY OF NRC 00749: CORROSION LEVEL 2. RH CUSP WEB BTW STA X=- 56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 215. (LP #0246687)

Part: RELEASE CABLE — OUT OF LIMITS (TAIL CONE) · airframe 57,066 hrs · 40,091 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN BEYOND ALLOWABLE LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-4002 TAILCONE SERVICE. (LP #0230140)

Part: NONE — NONE · airframe 54,154 hrs · 37,583 cycles

ON THE SERVICE CHECK, FOUND AFT F/A JUMPSEAT CEILING EMERGENCY LIGHT OUT AND EXIT SIGN NEAR FLOOR WITH LAMPS OUT. MAINTENANCE RELAMPED THE CEILING EMERGENCY LIGHT AT AFT F/A JUMPSEAT AND EXIT SIGN AT SAME LOCATION NEAR FLOOR PER B717 AMM 33-51. OPERATIONAL TEST OK. (LP #9705711)

Part: NONE — NONE · airframe 54,154 hrs · 37,583 cycles

ON SERVICE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS WITH MULTIPLE LAMPS OUT. MAINTENANCE RELAMPED BOTH OF THE OVER WING EMERGENCY EXIT LOWER SIGNS PER B717 AMM 33- 51. OPERATIONAL TEST OK. (LP #9705710)

Part: NONE — NONE · airframe 53,846 hrs · 37,301 cycles

DURING SERVICE CHECK THE RIGHT HAND EMERGENCY LIGHTS IN THE FIRST CLASS ROWS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY AND POWER SUPPLY (STA 39A) PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #8965525)

Part: LENS — MISSING · airframe 53,140 hrs · 36,651 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT ROW 29. MAINTENANCE REPLACED THE MISSING AFT COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2258245)

Part: PSEU — FAULT MESSAGE · airframe 53,140 hrs · 36,651 cycles

SHIP 9542 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING APPROACH DUE TO A PSEU FAILURE MESSAGE. A GO-AROUND WAS PERFORMED, THE QRH WAS COMPLIED WITH, AND THE SUBSEQUENT LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU. (LP #8812192)

Part: NONE — NONE · airframe 53,060 hrs · 36,573 cycles

THE FLIGHT ATTENDANT NOTICED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS MISSING AT THE TAILCONE AFT EMERGENCY CEILING LIGHT. MAINTENANCE INSTALLED THE AFT EMERGENCY EXIT CEILING LIGHT COVER PER B717 AMM 33 -51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #2241003)

Part: NONE — NONE · airframe 52,545 hrs · 36,109 cycles

SHIP 9542 - BOTH THE FLIGHT CREW AND THE CABIN CREW REPORTED SMOKE IN THE COCKPIT AND THE FORWARD CABIN AREA. "EMERGENCY POWER ON" MESSAGE SHOWED ON ELECTRIC PAGE, WITH SWITCH IN ARM POSITION. MAINTENANCE COMPLIED WITH THE NO-GO ODI PROCEDURES AND REPLACED THE GLARESHIELD CONTROL PANEL AS A PRECAUTION PER B717 AMM 31-11-01. GCP OPERATIONAL CHECK AND RTS TESTS PASS PER B717 AMM 31-11-01. WHEN NO C PHASE VOLTAGE WAS EVIDENT, MAINTENANCE DISCOVERED PIN C PUSHED BACK AND THE LOCK COLLAR DAMAGED AT P1-618. T HE CONNECTOR P1-618, WAS REPLACED ON LP #8059578. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #8059576)

Part: NONE — NONE · airframe 52,428 hrs · 36,009 cycles

SHIP 9542 - THE AIRCRAFT WAS RETURNED TO QRO AFTER TAKEOFF DUE TO A RIGHT MAIN LANDING GEAR DISAGREE MESSAGE. THE CAPTAIN DID DECLARE AN EMERGENCY TO HAVE ARFF AT THE RUNWAY FOR THE LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED AND ADJUSTED THE RIGHT MAIN GEAR UP LATCH PROXIMITY SENSOR. A FUNCTIONAL CHECK OF THE GEAR EXTENSION AND RETRACTION SYSTEMS WAS ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #8059550)

Part: NONE — NONE · airframe 52,425 hrs · 36,008 cycles

CRACK ON FRAME STA 1133 AND LONG 2RH AT AFT ACCESORIES COMPARTMENT (CAT). SUMMARY OF NRC 00157: FRAME STA 1133 WAS REPAIRED PER ER/A 596793 -14 REV. A AND ETI-17-22-006 REV. 3. ASSOCIATED ER/A 14-596793 ADDED FOR AC 9542. (LP #2110523)

Part: NONE — NONE · airframe 52,425 hrs · 36,006 cycles

AD HFEC INSPECTION WAS PERFORMED AND A CRACK WAS FOUND ON THE UPPER RADIUS OF THE LH OVERWING FRAME AT STA. Y=674.00, APPROX LENGTH 0.120 IN, IN REF. CARD 5310-01436-01B STEP 7. SUMMARY OF NRC 00203: LH OVERWING FRAME AT STA. Y=674.00 WAS REPLACED WITH AMDS 5310-01436-03A JOB 096-0001. ASSOCIATED AA 5310-01436 ADDED FOR AC 9542. (LP #2108412)

Part: NONE — NONE · airframe 52,425 hrs · 36,006 cycles

CRACK ON LONG 2RH STA 1133 AT AFT ACCESORIES COMPARTMENT (CAT). SUMMARY OF NRC 00156: LONG 2RH (STA 1120 TO STA 1135) WAS REPAIRED PER B717 SRM 53-00-05-2R-2. (LP #2104522)

Part: NONE — NONE · corrosion level 2 · airframe 52,425 hrs · 36,006 cycles

CORROSION ON FWD AND AFT REPAIR SPLICES OF DOUBLERS AT AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00010: FWD AND AFT REPAIRS SPLICE DOUBLERS WERE REPLACED PER B717 SRM 53-20- 15-2R REP.7. (LP #2101904)

Part: NONE — NONE · airframe 52,630 hrs · 36,177 cycles

SEVERAL DENTS ON LH HORIZONTAL STABILIZER LEADING EDGE SKIN INBOARD SECTION. SUMMARY OF NRC 00070: DENTS WERE MEASURED AND FOUND TO BE OUT LIMITS PER B717 SRM 55-10-01-1A PROCEDURE 1 PARAGRAPH 4. A. AND FIGURE 102. DENT FILLER REPAIR WAS PERFORMED PER B717 SRM 55- 10-01-2R PROCEDURE 2. PERFORM GENERAL VISUAL INSPECTION INITIAL 24 MONTHS AND REPETITIVE 24 MONTHS PER B 717 SRM 55-10-01-2R PROCEDURE 2. PAR 5. (LP #2099819)

Part: NONE — NONE · airframe 52,425 hrs · 36,006 cycles

DURING THE DOUBLER REMOVAL PROCESS A WEB WAS FOUND DAMAGE ON THE RIGHT HAND SIDE, LOCATED ON INTERSECTION STA 696 AND STGR 18RH. SUMMARY OF NRC 00205: WEB ON RIGHT HAND SIDE, LOCATED ON INTERSECTION STA 696 AND STGR 18RH WAS REPAIRED PER B717 SRM 53- 00-55-2R PROCEDURE 4. (LP #2099034)

Part: SLIDE — NO TEST (TAILCONE) · airframe 50,539 hrs · 34,351 cycles

THE TAIL CONE SLIDE FAILED THE DEPLOYMENT TEST. THE TAIL CONE SLIDE WAS DEPLOYED FOR SAMPLING. THE SLIDE DEPLOYMENT FAILED. MAINTENANCE REPLACED THE SLIDE ON W/C 2561-9006. (LP 1739712)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,968 hrs · 33,884 cycles

THE EMERGENCY LIGHTS AT THE AFT OVERWING EXIT MARKERS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK (B5-230) AND THE SYSTEM TESTED OK, PER B717 AMM 33-51-03/401. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,911 hrs · 32,941 cycles

THE FORWARD UPPER LEFT OVERWING EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT CHARGER REF B717 AMM 33-51. OPERATION CHECK WAS GOOD. OK FOR SERVICE. (LP #6934282)

Part: STRUCTURE — GOUGED · airframe 48,766 hrs · 32,819 cycles

DAMAGE TO STRUCTURE JUST TO THE RIGHT OF THE RIGHT STEERING ACTUATOR WAS FOUND. (NOSE LANDING GEAR SUPPORT WEB.) MAINTENANCE BLENDED THE GOUGE PER B717 SRM 53-10-14-2R PROC 3 AND PERFORMED U.T. THICKNESS MEASUREMENT PER B717 NDT PART 4. NO DEFECTS NOTED. INSTALLED REPAIR FASTENERS PER B717 SRM 53-10-14 PROCEDURE 3 REPAIR 3 FIG 201. ALL RII C/W & COMPLETE QC1322 416561 INSTALLED DAMAGE STICKER ON REPAIR. REQUIRES REPETITIVE INSPECTION EVERY 3000 CYCLES REF TABLE 203 B717 SRM 53-10-14-2R -3. REFER TO LOG PAGE #6896386 FOR MONITOR. (LP #6896380)

Part: CABLE — FRAYED (TAILCONE) · airframe 48,652 hrs · 32,739 cycles

THE TAIL CONE KEVLAR CABLE WAS DISCOVERED FRAYED. MAINTENANCE REPLACED THE KEVLAR CABLE IAW AMM 53-52-01.

Part: DOOR FRAME — DENTED (FWD CARGO) · airframe 45,738 hrs · 30,727 cycles

FWD CARGO DOOR CUTOUT AREA - DENT. ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS AT 8,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR AND EVERY 8,000 FLIGHT CYCLES THEREAFTER. ASSOCIATED ER/A 00-573730 ADDED FOR AC 9542. (LP #0860614 )

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,521 hrs · 30,577 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 15-20. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT SEAT 18 PER B717 AMM 33-51. EMERGENCY LIGHTS NOW ILLUMINATE NORMALLY. OPERATIONAL CHECK IS GOOD. (LP #0811746)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,352 hrs · 29,737 cycles

DELAMINATED PASSENGER CABIN FLOOR PANELS #222ARF, 222VF, 221KF, 221AF. NRC 00454: FLOOR PANELS #222ARF, 222VF, 221KF, AND 221AF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3 AND WERE INSTALLED WITH CARD JIC 2040-0023. (LP #0410341)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 43,371 hrs · 29,015 cycles

EMERGENCY EXIT SIGN ON FWD BULKHEAD ABOVE F/A JUMPSEATS AT DOOR 1L IS IN DIM MODE AT ALL TIMES, EVEN IF SWITCH IS OFF AND ALL OTHER EMERGENCY EXIT SIGNS ARE OFF. WHEN EMERGENCY EXIT SIGNS TURNED ON, ALL THE OTHERS COME ON BRIGHT EXCEPT FOR THIS LIGHT, WHICH FLASHES BRIGHT AND THEN GOES DIM IMMEDIATELY. MAINTENANCE FOUND THE BATTERY CHARGE TO BE LOW AND REPLACED THE BATTERY IAW SCM 33-51-0, CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 45,524 hrs · 30,579 cycles

DENT AND GOUGE DAMAGE AT STA 227 ABOVE L-20L. ER/A 563130-14 REV A IS CURRENT.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 45,807 hrs · 30,781 cycles

DAMAGE FOUND AFT OF L1 DOOR LOWER EDGE AT STATION 227 AND 1 INCH ABOVE L-20 STRINGER. COMPLIED WITH REPAIR INSTRUCTIONS IAW ER/A 563130-14 REV ORIG. WILL REQUIRE REPEATED INSPECTION EVERY 20 DAYS AND A PERMANENT REPAIR AT OR BEFORE NEXT C-CHECK. NO CRACK INDICATIONS NOTED ON INSPECTION QC4080 (358523). ASSOCIATED ER/A 14-563130 ADDED FOR AC 9542. PERFORMED DVI AND HFEC INSPECTION OF DAMAGE AREA IAW ER/A 563130-14 REV A DATED 31AUG18 SECTION II. NO CRACKS OR ADDITIONAL DAMAGE NOTED (LP #3605989)

Part: SIGN — MISSING (CABIN) · airframe 42,411 hrs · 28,417 cycles

EXIT SIGN MISSING. FOUND THE SIGN AND SECURED BACK IN PLACE. OK FOR SERVICE.

Part: DOOR — CORRODED (STAIRWELL) · corrosion level 2 · airframe 42,285 hrs · 28,329 cycles

CORROSION WAS FOUND ON THE FWD STAIRWELL DOOR. THE DOOR WAS REPAIRED IAW ETI-17-17-132, REV 2, AND ER/A 559570-14, REV ORIG.

Part: SKIN — DAMAGED (BS 1189-1195) · airframe 42,284 hrs · 28,328 cycles

DENTS AND SCRATCHES ON EXTERNAL FUSELAGE SKIN FROM BS 1189 TO 1195, BETWEEN 5 AND 6 HRS POSITION. THE DAMAGED AREA WAS REPAIRED IAW ETI 17-17-126, REV I, AND 559588-14 REV ORIGINAL.

Part: SKIN — CRACKED (BS 1037) · airframe 42,284 hrs · 28,328 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BS 1037, LONGERON 14L. DAMAGED AREA WAS REPAIRED IAW ETI-17-17-108, REV 6 AND ER/A 559552-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON COUNTERSINK AND ELONGATE HOLES ON FUEL TANK ACCES PLATE 141AR. ACCES PLATE WAS REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON STRAP (ABOVE LONG 26L) FROM Y=900 TO Y=943 AT AFT CARGO COMPARTMENT. STRAP WAS REPLACED PER SRM 51-41-02, 51-41-05, AND DWG S2912900 REV D.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON CUSP ANGLE BTW STA Y 598-617 BELOW RT CUSP WEB. CORROSION ON CUSP ANGLE BTW STA Y 598-617 BELOW RT CUSP WEB WAS REPAIRED PER ETI-17-17-114 REV 2 AND ER/A 559569-14 REV ORIG.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 42,284 hrs · 28,328 cycles

CRACK ON RT FWD SIDE LOWER FAIRING CUTOUT EDGE NEAR STA YV 157 AT VERTICAL STAB(EHV). CRACK ON RT FWD SIDE LOWER FAIRING CUTOUT EDGE NEAR STA YV 157 AT VERTICAL STAB WAS REPAIRED PER ETI-17-17-110 REV 3 AND ER/A 559560-14 REV ORIG.

Part: SKIN — CRACKED (LT WING) · airframe 42,284 hrs · 28,328 cycles

CRACK ON LT WING LOWER TRAILING EDGE AT STA XRS=126 APPROX. CRACK ON LT WING LOWER TRAILING EDGE AT STA XRS=126 APPROX WAS REPAIRED PER SRM 57-00-00-2R-1.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON LT TIE TRACK BTW STA 895-1022 AT AFT CARGO COMPARTMENT. LT TIE TRACK WAS REMOVED AND INSTALLED PER SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. NEW SECTION OF TIE TRACK WAS DRILLED AND ADJUSTED PER SRM 51-40-08-0G. NEW SECTION OF TIE TRACK WAS TREATED AND PAINTED PER SRM 51-10-04-0G PAR 21 AND 15.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON COUNTERSINK AND ELONGATE HOLES ON FUEL TANK ACCES PLATE 520PB AND 141AL. ACCESS PLATES 520PB AND 141AL WERE REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL TANK ACCESS PLATE 520DB, 530FT, AND 520CT. ACCESS PLATE 520CT WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION III AND DUE TO EXCESSIVE DAMAGE BY CORROSION ON COUNTERSINK AREAS, ACCESS PLATES 520DB AND 520FT ARE OUT OF LIMITS AND WERE REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.

Part: PAN — CORRODED (BS 370-427) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON FWD CARGO COMPARTMENT DOOR FRAME PAN BS 370 TO 427. REPLACED IAW SRM 53-20-15-2R-6, AND DWG 5910142, REV DJ.

Part: STRUCTURE — CRACKED (LT WING) · airframe 42,284 hrs · 28,328 cycles

CRACKS ON SPLICE AND STRUCTURE INBD LEADING EDGE XRS 277 AT LT WING. REPLACED IAW SRM 57-40-01-01, ITEM 32, SRM 51-41-02, SRM 51-41-05, AND DWG 9919326, REV E.

Part: SKIN — CRACKED (BS 1087) · airframe 42,284 hrs · 28,328 cycles

CRACK ON FUSELAGE SKIN BS 1087, LONGERONS 13 - 14R. REPAIRED IAW ETI-17-17-109, REV 2, AND ER/A 559556-14, REV ORIG.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 42,284 hrs · 28,328 cycles

CORROSION ON FLOOR PANEL.. REPAIRED IAW SRM 53-00-00-2R.

Part: DOUBLER — CORRODED (CUSP WEB) · airframe 42,284 hrs · 28,328 cycles

CORROSION OUT OF LIMITS ON RT DOUBLER PRODUCTION LOWER SURFACE OF CUSP WEB BS 579 TO 598, RBL 54 TO 60. THE DOUBLER WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 446-503) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON RT CUSP WEB UPPER/LOWER SURFACE BS 446 TO 503, RBL 54 TO 60. CORROSION AND FASTENERS WERE REMOVED IAW SRM. FOUND TO BE OUT OF LIMITS. A REPAIR FABRICATED IAW SRM. REPAIR INSTALLED.

Part: CUSP WEB — PUNCTURED (BS 712) · airframe 42,284 hrs · 28,328 cycles

PUNCTURE ON RT CUSP WEB BS 712, RBL 54 TO 60. THE DAMAGE WAS REPAIRED IAW SRM.

Part: FORMER — CRACKED (BS 679) · airframe 42,284 hrs · 28,328 cycles

CRACK ON RT FORMER BS 679 AT UNDERWING BARREL CANTED KEEL BEAM AREA. THE DAMAGE WAS REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 899-901) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 899 TO 901, RBL 54 TO 60. THE DAMAGE WAS REPAIRED SRM.

Part: FLOORBEAM — CRACKED (BS 737) · airframe 42,284 hrs · 28,328 cycles

CRACKED FLOORBEAM BS 737 BETWEEN LBL 56 TO 60. THE FLOORBEAM WAS REPLACED IAW SRM.

Part: SUPPORT — WORN · airframe 42,284 hrs · 28,328 cycles

WEAR ON SUPPORT , RT SIDE ATTENDANT SEAT SETTLEMENT AT AFT CABIN BULKHEAD DOOR. THE SUPPORT WAS REPAIRED IAW SRM.

Part: FRAME — CRACKED (BS 679) · airframe 42,284 hrs · 28,328 cycles

CRACK ON LT FRAME BS 679 AT UNDERWING BARREL CANTED KEEL BEAM AREA. DAMAGE AREAS WERE REPAIRED SRM.

Part: SEAT TRACK — DAMAGED (BS 281-400) · airframe 42,284 hrs · 28,328 cycles

OUT OF LIMITS SEAT TRACK RBL 44.5 FROM BS 281 TO 283, BS 323 TO 324 AND BS 399 TO 400. DAMAGE AREA WAS REPAIRED IAW SRM.

Part: PAN — WORN (CARGO DOORWAY) · airframe 42,284 hrs · 28,328 cycles

CRACK ON FWD CARGO DOOR FRAME PAN BS 427 BETWEEN BEAM 4 AND UPPER EDGE. THE PAN WAS REPAIRED IAW SRM.

Part: PAN — WORN · airframe 42,284 hrs · 28,328 cycles

WEAR ON PAN , LT SIDE. ATTENDANT SEAT SETTLEMENT, AT AFT CABIN BULKHEAD DOOR. THE PAN WAS REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 544-555) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 544 TO 555, RBL 54 TO 60. DAMAGE WAS REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 868-870) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON SEAT TRACK LBL 44 FROM BS 868 TO 870. DAMAGE AREA WAS REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 750-752) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON LT SEAT TRACK LBL 44 FROM BS 750 - 752. AREA OUT OF LIMITS. TRMIMED AREA AND NEW HOLES WERE TREATED AND PAINTED. A REPAIR PLUG AND CHANNEL WERE INSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON THE FLOOR SUPPORT BS 160 - 200 LBL 44 IN THE CABIN. THE FLOOR SUPPORT WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 706-712) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON THE LEFT CUSP WEB BS 706 - 712. THE DAMAGED AREA WAS REPAIRED.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 42,284 hrs · 28,328 cycles

DAMAGED FLOOR PANEL 211ANF. THE FLOOR PANEL WAS REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 42,284 hrs · 28,328 cycles

CORROSION ON THE FLOOR SUPPORT BS 160 - 200, RBL 44 IN THE CABIN. THE FLOOR SUPPORT WAS REPLACED.

Part: FRAME — CRACKED (BS 1037) · airframe 42,284 hrs · 28,328 cycles

CRACK ON FRAME BS 1037, LONGERON 17R. NO CRACKS WERE FOUND AFTER TRIM OUT. DAMAGE AREA WAS REAPIRED IAW SRM 53-20-07-2R-4.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 42,284 hrs · 28,328 cycles

DAMAGE FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50 2R.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 42,284 hrs · 28,328 cycles

CRACK INNER PAN AT BS 994, NEAR BEAM NR 5 IN THE AFT CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-6.

Part: CUSP WEB — CRACKED (BS 218) · airframe 42,284 hrs · 28,328 cycles

CRACK ON THE RT CUSP WEB BS 218 RBL 44. REPAIRED IAW SRM 53-00-55-2R.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,284 hrs · 28,328 cycles

CRACKED NR 1 BEAM AFT EDGE AT L1 DOOR. THE BEAM WAS REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,500 hrs · 27,721 cycles

FUSELAGE SKIN STA 235, ABOVE L-18L "FOUR CORNERS" AREA DENT AND GOUGE. PERMANENT REPAIR RESTRICTION. ER/A 539814-14 REV B IS CURRENT. REMOVED TIME LIMITED REPAIR AT STA 235 LONGERON 18LT AND ACCOMPLISHED A CLASS 1 PERMANENT REPAIR IAW SRM 53-10-01 REPAIR 10 FIG 202.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,211 hrs · 27,508 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS AT BOTH L1 AND R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,905 hrs · 27,296 cycles

DURING LINE CHECK, MAINTENANCE NOTED THAT THE OVERHEAD EMERGENCY LIGHTS FOR BOTH THE AFT OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE APPLICABLE BATTERY PACK AND THE OPERATION OF THE LIGHTS CHECKED GOOD. (LP #9446654)

Part: HANDLE — DAMAGED (TAILCONE RELEASE) · airframe 40,400 hrs · 26,932 cycles

EXTERNAL TAIL CONE JETTISON HANDLE ANGLE MISSING ALONG WITH INSTALL HARDWARE. REPLACED THE MISSING ANGLE AND HARDWARE IAW AMM 53-50. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,643 hrs · 26,368 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 38,694 hrs · 25,561 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE EXTERIOR OVERWING EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (BS 229) · airframe 37,754 hrs · 24,864 cycles

DURING CHECK, NOTED SKIN DAMAGED AT BS 229, LONGERON 18L. REPAIRED IAW ER/A 539814-14.

Part: WIRE — MISROUTED (AC BAY) · airframe 37,420 hrs · 24,591 cycles

TAIL COMPARTMENT CATER OVERHEAD EMERGENCY LIGHT WIRE MISROUTED. REROUTED WIRE IAW SWPM.

Part: SIGN — BROKEN (CABIN) · airframe 37,420 hrs · 24,591 cycles

OVERHEAD EMERGENCY EXIT SIGN LIGHT MOUNT BROKEN AT ROW 1. R & R SIGN ASSEMBLY IAW AMM.

Part: COVER — LOOSE (L1 DOOR) · airframe 37,420 hrs · 24,591 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT EDGE TRIM LOOSE. REPAIRED COVER ASSEMBLY IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 35,934 hrs · 23,572 cycles

RIGHT AFT OVERWING DOOR EXIT SIGN CRACKED. R & R SIGN IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 35,934 hrs · 23,572 cycles

R1 DOOR LOWER AFT EMER EXIT SIGN CRACKED. R & R SIGN IAW MM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,934 hrs · 23,572 cycles

AFT RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 35,934 hrs · 23,572 cycles

AFT LT EMER LIGHT LENS CRACKED AFT ACCESSORY WORK PLATFORM. R & R LENS IAW AMM.

Part: SKIN — DELAMINATED (LT WING) · airframe 35,934 hrs · 23,572 cycles

LEFT WING INBD FIXED VANE SKIN DELAMINATED ON LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 35,934 hrs · 23,572 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR FITTINGS CORRODED. R & R FITTING IAW SRM.

Part: LANYARD — FRAYED (R1 DOOR) · airframe 35,934 hrs · 23,572 cycles

R1 DOOR GIRT BAR LANYARD FRAYED. R & R LANYARD IAW WO.

Part: ANGLE — CRACKED (TE FLAP) · airframe 35,934 hrs · 23,572 cycles

LEFT WING INBD FLAP TRACK INBD ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT MLG WW) · airframe 35,934 hrs · 23,572 cycles

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

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,934 hrs · 23,572 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 674 TO 715. R & R CUSP WEB IAW SRM.

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 35,934 hrs · 23,572 cycles

AFT CARGO LOWER PAN CORRODED. R & R PAN IAW SRM.

Part: HANDLE — CRACKED (TAILCONE) · airframe 35,934 hrs · 23,572 cycles

AFT ACCESSORY COMPARTMENT, INTERNAL TAIL CONE DEPLOYMENT HANDLE. EXIT SIGN, CRACKED. R & R HANDLE IAW SRM.

Part: BRAKE ASSY — FAULTY (RT MLG) · airframe 36,964 hrs · 24,275 cycles

DECLARED EMER NR 2 BRAKE HOT INDICATION. R & R NR 2 BRAKE ASSEMBLY IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,593 hrs · 24,023 cycles

AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW SIP.

Part: COVER — LOOSE (EXIT SIGN) · airframe 35,894 hrs · 23,545 cycles

FORWARD EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER IAW AMM.

Part: PROXIMITY SENSOR — FAULTY (RT MLG) · airframe 35,864 hrs · 23,523 cycles

AIR TURN BACK, RED RT MAIN GEAR UNSAFE LIGHT WITH GEAR HANDLE UP. R & R RT MAIN GEAR UP & LATCHED PROXIMITY SENSOR IAW AMM.

Part: COVER — LOOSE (L1 DOOR) · airframe 34,756 hrs · 22,804 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW MM.

Part: LATCH — DIRTY (GIRT BAR) · airframe 34,469 hrs · 22,611 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIRTY. CLEANED GIRT BAR LATCHES IAW MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

FRAME CLIP CRACKED AT BS 1053. R&R CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

MAIN CABIN AFT BULKHEAD DOOR CUT OUT FRAME LT SIDE TIE FITTING CRACKED AT STATION 426, LONGERON 13L. R&R FITTING IAW SRM & DRAWING.

Part: DOME NUT — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

DOME NUT CORRODED AT UPPER FS INTERNAL SKIN STATION 302 ATC ANTENNA. R&R DOME NUT IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,413 hrs · 21,949 cycles

CENTER WING TANK BULKHEAD FWD SIDE CRACKED AT VERTICAL STIFFENER, STATION 655, RBL 20. R&R STIFFENER IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

MAIN CABIN AFT BULKHEAD DOOR CUT OUT LT FRAME TIE FITTING CRACKED AT STATION 425, LONGERON 15L. R&R FITTING IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 737, LBL 44. R&R FITTING IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 737, RBL 44. R&R FITTING IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

RT CUSP WEB CORRODED AT STATION 670. R&R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

RT CUSP WEB CORRODED AT STATION 470. R&R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

LT CUSP WEB CORRODED BETWEEN STATION 503 TO STATION 522. R&R WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,413 hrs · 21,949 cycles

LT CUSP WEB CORRODED BETWEEN STATION 541 TO STATION 560. R&R WEB IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 33,413 hrs · 21,949 cycles

MAIN CABIN FLOOR PANEL 222APF DAMAGED. R&R PANEL IAW MM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

RT CUSP WEB CORRODED BETWEEN STATION 503 TO STATION 522. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

RT CUSP WEB CORRODED AT STATION 653. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,413 hrs · 21,949 cycles

RT CUSP WEB CORRODED AT STATION 954, UNDER FRAME FITTING. R&R WEB IAW SRM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 33,416 hrs · 21,963 cycles

R1 DOOR EMERGENCY DOORS FOUR EACH LOWER SIDE BRACKET FASTENERS LOOSE. SECURED FASTENERS IAW SRM.

Part: FASTENER — LOOSE (L2 DOOR) · airframe 33,416 hrs · 21,963 cycles

L2 DOOR EMERGENCY DOORS FOUR EACH LOWER SIDE BRACKET FASTENERS LOOSE. SECURED FASTENERS IAW SRM.

Part: FASTENER — LOOSE (R2 DOOR) · airframe 33,416 hrs · 21,963 cycles

R2 DOOR EMERGENCY DOORS FOUR EACH LOWER SIDE BRACKET FASTENERS LOOSE. SECURED FASTENERS IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 33,416 hrs · 21,963 cycles

L1 DOOR 2ND LOWER AFT BEAM CRACKED IN CORNER. REPAIRED DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,413 hrs · 21,949 cycles

FRAME CRACKED AT STATION 715 RT. REPAIRED FRAME IAW SRM & DRAWING.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 33,416 hrs · 21,963 cycles

L1 DOOR EMERGENCY DOORS FOUR EACH LOWER SIDE BRACKET FASTENERS LOOSE. SECURED FASTENERS IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

AFT ACCESSORY COMPARTMENT. Y DUCT LOWER CLAMP SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

LT WING INBD WING TO BODY BONDING STRAP CRACKED. R&R STRAP IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (LT MLG WW) · airframe 33,413 hrs · 21,949 cycles

LT GEAR DOOR CUTOUT FRAME CRACKED BELOW DOOR SENSOR. REPAIRED DOUBLER IAW SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

AFT ACCESSORY COMPARTMENT CEILING PANEL ATTACH BRACKET CRACKED AT STATION 1146, STRINGER 3L. R&R BRACKET IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,416 hrs · 21,963 cycles

AFT CARGO DOOR PAN AFT LATCH AREA CRACKED. R&R ANGLE IAW SRM.

Part: STRAP — CRACKED (RT WING) · airframe 33,416 hrs · 21,963 cycles

RT WING BONDING STRIP CRACKED AT LOWER SIDE WING TO BODY. R&R STRAP IAW & DRAWING.

Part: HOLDER — OUT OF ADJUST (GIRT BAR) · airframe 34,269 hrs · 22,492 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED HOLDER IAW SIP.

Part: COVER — LOOSE (R1 DOOR) · airframe 33,667 hrs · 22,123 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW MM.

Part: LATCH — LOOSE (R1 DOOR) · airframe 33,358 hrs · 21,925 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR TRIANGULAR CONNECTION LOOSE. SECURED LATCH PER MM.

Part: FITTING — DIRTY (GIRT BAR) · airframe 30,382 hrs · 20,035 cycles

R1 DOOR EVAC SLIDE GIRT BAR ATTACH FITTINGS DIRTY. CLEANED ATTACH FITING PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 30,269 hrs · 19,959 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN PANEL — CRACKED (LT WING)

LT WING I/B BUTE DOOR FWD PANEL, CRACKED. ACCOMPLISHED FWD PANEL REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

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

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN, DENTED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 53-00-01 AND TRA 17-53-TR00109.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 56, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SKIN — CRACKED (LT WING)

LEFT WING I/B BUTE DOOR INNER UPPER SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 44 TO RBL 53, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 238, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-20-52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 180 TO 200, RBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 180 TO 200, RBL44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-30-07 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 6 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 1180, LBL25, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR WEB REPLACEMENT PER B717 SRM 53-00-00 AND 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 180, RBL 6 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL 32 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 53-10-51, 51-10-01 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01 AND 51-40-08.

Part: WEB — CRACKED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 160, RBL 8, CRACKED. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 238, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-20-52.

Part: STRINGER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON STRINGER AND BRACKET SUPPORT, STA 1037 TO 1053, LONG L22, CORROSION. OPEN DEFECT.

Part: FLOOR PANEL — CORRODED (CABIN)

R1 DOOR LWR JAM CUTOUT SILL FWD AFT FLOOR SUPPORT PANELS, CORROSION. ACCOMPLISHED FLOOR SUPPORT PANELS REPLACEMENT PER B717 SRM 51-41-01 AND 53-00-00.

Part: LENS — MISSING (CABIN)

ON SEAT 1D THE RED FWD LENS PATH LIGHTING ASSEMBLY LENS COVER IS MISSING. INSTALLED LENS OK FOR SERVICE REF 33-51.

Part: LANYARD — DETACHED (EVAC SLIDE)

R1 SLIDE GIRT BAR DETACHED. RE-ATTACHED LANYARD IN R-1 SLIDE AS OUTLINED IN 717 MM 25-61.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)

BULB BURNED OUT IN COCKPIT EMERGENCY LIGHT. RESET CIRCUIT BREAKER, OPS CHECKED GOOD.

Part: SCREW — MISSING (LIGHT SOCKET)

ROW 3 E-PATH LIGHT FWD SOCKET NOT MOUNTED, MISSING HARDWARE. INSTALLED TWO MISSING SCREWS.

Part: COVER — MISSING (CABIN)

CLEAR COVER ON ELS IS MISSING FROM ROW 3. REPLACED ROW 3 ELS LENS COVER.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2985.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB, STA 954 TO 994, CORROSION. ACCOMPLISHED CARGO DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201. SEE NR 3695 AND 2687.

Part: STRUCTURE — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT, STA 927, LONG L30 TO L29L, CORROSION. ACCOMPLISHED CARGO COMPARTMENT FILLER AND DOUBLER REPAIR PER B717 SRM 53-20-07 P204-214. SEE NR 3743 AND 2697.

Part: STRINGER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT, STA 974 TO 994, LONG L28L, CORROSION. ACCOMPLISHED CARGO COMPARTMENT STRINGER SECTION REPAIR PER B717 SRM 53-00-05 REPAIR 2. SEE NR 3742 AND 2683.

Part: DOOR FRAME — CORRODED (CARGO BAY)

FWD CARGO DOOR JAMB, STA 372 TO 425, CORROSION. ACCOMPLISHED CARGO DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 6 FIG 201. SEE NR 3694 AND 3767.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

THE R1 DOOR SLIDE IS PARTIALLY OUT OF POUCH. REMOVED AND REPLACED R1 DOOR SLIDE PER 25-61-03 DUE TO BOTH INFLATION CABLE PINS PULLED.

Part: SKIN — DAMAGED (BS 550 L21R)

BAG CART DAMAGE ON RT FUSELAGE APPROX STA 550 AT LONGERON 21 AFT OF FWD BB DOOR AND FWD OF RT WING TO BODY FAIRING HIDDEN DAMAGE INSPECTION REQUIRED REF: RFE 07-0665 / PEA 17- 53-00518IR. INSTALLED PERMANENT REPAIR AT SKIN DAMAGE AND LONGERON DAMAGED IAW B717 SRM 53-00-01 FIG 201 REPAIR 1 AND 5300-05 REPAIR 2 FIG 201.

Part: PCDU — MALFUNCTIONED (COCKPIT)

DURING T-OFF ROLL NR 1 AND 3 DU'S WENT BLANK AND SLATS CALL ALERT WAS HEARD TAKE OFF REJECTED. SUSPECT PWR INTERRUPTION NO PCDU FAULTS REPLACED LPCDU (PRECAUTIONARY) AND RELAYS RAN ENG TO T/O PWR ALL CKS OK.