N953AT

Part: DOUBLER — DAMAGED (RT REFUEL PANEL) · airframe 61,262 hrs · 44,070 cycles

RT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 3 SHT 1. PERFORMED HFEC IAW B717 PER B717 SRM 57-40-01-2R PROCEDURE 3 AND NTSPM 06-10-01- 001. NO DEFECT NOTED. FABRICATED FILLERS AND DOUBLERS FOR BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 202 SHT 1. INSTALLED REPAIRED DOUBLERS PER B717 SRM 57-40-01-2R PROCEDURE 3. (LP #0382569)

Part: DOOR — BENT (FUEL SELECTOR) · airframe 61,256 hrs · 44,062 cycles

ON ARRIVAL FOUND FUEL SELECTOR PANEL DOOR BENT OPEN. DAMAGE TO THE SLAT SEAL, DAMAGE TO FUEL SELECTOR PANEL, AND DAMAGE TO THE GUARDED SWITCHES. ALL REFUEL ASSOCIATED LATCHES WERE FOUND OPEN / UNLATCHED. REPLACED GUARDED SWITCHES IAW B717 AMM 28-21-14. REPAIRED DOUBLERS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 202 SHEET 1 (ON LOG PAGE #0382569). REPLACED FUEL SELECTOR DOOR ON NR 2. REPLACED THE SLAT SEAL REF B717 SRM 51-40. (LP #5625018)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,306 hrs · 43,243 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EXIT LIGHT AND ISLE OVERWING EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED 2 EACH BATTERIES, AT ROWS 18 & 19, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL LIGHTS ILLUMINATE. AIRCRAFT IS OK FOR SERVICE. (LP #4581366)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,902 hrs · 42,063 cycles

AT CRUISE, MULTIPLE SPARKS ON CENTER WINDSHIELD AND CRACK FORMED. TURNED ANTI-ICE OFF PER QRH PROCEDURE. REMOVED CENTER WINDSHIELD IAW B717 AMM 56-11-01. REPLACED CENTER WINDOW HEAT CONTROLLER IAW AMM 30-41-01 A2-10. REPLACED THE CENTER WINDOW PER B717 AMM 56-11-01. OPERATIONAL CHECK OF THE WINDOW HEAT CONTROLLER COMPLIED WITH PER B717 AMM 30-41-01. (LP #9734886)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,575 hrs · 41,782 cycles

SHIP 9512 -HYD/DE- THE RIGHT HYDRAULIC SYSTEM EXPERIENCED A COMPLETE LOSS OF FLUID WHILE ON APPROACH FOR LANDING. THE CREW DECLARED AN EMERGENCY WITH ATC AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE COMPLIED WITH. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE GEAR DOORS CONTACTING THE RUNWAY AND THE #2 ENGINE THRUST REVERSER NOT DEPLOYING WITH ONLY ACCUMULATOR PRESSURE. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE AUXILIARY HYDRAULIC PUMP RELIEF VALVE FITTING FAILED RIGHT AT THE PUMP. THE HYDRAULIC ELECTRIC AUXILIARY PUMP WAS REPLACED. (LP #4629080)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,362 hrs · 41,594 cycles

SHIP 9512 - MISC/HYD - DECLARED EMERGENCY FOR THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. CORRECTIVE ACTION: FOUND RUDDER LIMITER ACTUATOR LINE LEAKING. FOUND LEAK ON PIPE ASSY CONNECTED TO RUDDER LIMITER CONTROL. PIPE WAS CHAFING AGAINST WORN ADEL CLAMP (915046) CUT TUBE TO BE REMANUFACTURED AND PERMA SWEGED (897744) CUT HYDRAULIC TUBE PER B71 AMM 20-10-01. D390 MFG TUBE PERMASWEGED PER B717 AMM 20-10-01. LEAK CK GOOD. (LP 9098444)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,490 hrs · 41,700 cycles

SHIP 9512 -HYD/MISC- THE FLIGHT CREW DECLARED AN EMERGENCY FOLLOWING THE ILLUMINATION OF THE "RIGHT HYD LO" MESSAGE AND THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. THE QRH WAS COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT A LOOSE B-NUT AT THE RUDDER ACTUATOR WAS LEAKING. THE LINE WAS SECURED, THE SYSTEM WAS SERVICED AND BLED, AND THE LEAK CHECK WAS GOOD PER B717 AMM 29-00-00. THE AIRCRAFT RETURNED TO SERVICE. (LP #9098442)

Part: NONE — NONE · airframe 58,193 hrs · 41,460 cycles

SHIP 9512 -ATB/GEAR/DE- DURING CLIMB OUT AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR "UNSAFE" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED ANOTHER RETRACTION. WHEN IT WAS DETERMINED THAT THE RIGHT LANDING GEAR WOULD NOT INDICATE A PROPER RETRACTION THE CREW DECLARED AN EMERGENCY AND RETURNED TO ATL. THE LANDING GEAR EXTENDED WITHOUT ISSUE AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR DOOR UP AND LATCHED SENSOR TARGET LOOSE. THE SENSOR WAS SECURED, A GOOD INDUCTANCE CHECK ACCOMPLISHED, GEAR WAS SWUNG, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #8263438)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 58,030 hrs · 41,322 cycles

DURING PRESSURE SEAL REMOVAL, CRACK WAS FOUND ON PASSENGER DOOR FWD UPPER CORNER. PASSENGER DOOR FWD WAS REPLACED FOR THE SERVICIABLE DOOR AND A NEW BRACKET WAS REPLACED PER AMM 52-11-01.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,030 hrs · 41,322 cycles

CRACK ON FWD SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR (PTAS). SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 604439-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.

Part: FRAME — CRACKED · airframe 58,030 hrs · 41,322 cycles

CRACK ON FRAME STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00332: FRAMES ON STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2573068)

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CPAX)(W1). SUMMARY OF NRC 00334: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 WAS REPLACED PER DWG 9936534 REV. BW AND B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-02-0G. (LP #2572323)

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,030 hrs · 41,322 cycles

CRACK ON FRAME BS 674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00331: FRAMES ON STA Y=674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11 -2R, REPAIR 1. (LP #2571796)

Part: WEB — CORRODED (BS 946-954) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON WEB AT LWR SILL AREA BTW STA Y=946-954 PROJECTION LONG 28R-29R OF AFT CARGO COMPARTMENT. CORROSION LEVEL 2. WEB AT LWR SILL AREA BTW STA 946 TO STA 1002 PROJECTION LONG 28R-29R OF AFT CARGO WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-02-0G PAR 4, SRM 51-41-04-0G PAR 9, SRM 51-41-05-0G PAR 8, AND SRM 51-41-08-0G PAR. 7.

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 53-20-15- 2R REPAIR 7, SRM 51-40-02-0G, SRM 51-41-05-0G, AND SRM 51-41-01- 0G.

Part: SEAT TRACK — CRACKED (BS 218-342) · airframe 58,030 hrs · 41,322 cycles

AFTER REMOVAL RH SEAT TRACK SECTION X=-44 BTW STA Y= 218 TO Y=342 A CRACK WAS FOUND IN THE CUSP WEB AT STA Y=294 TO Y=300. SUMMARY OF NRC 00516: CUSP WEB STA Y=294 TO Y=300 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 222. (LP #2558235)

Part: SEAT TRACK — CORRODED (BS 920-922) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

IN REF TO NRC 00325: SEAT TRACK SECTION X=-56 BTW STA=920 TO STA=922 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK SECTION X=- 56 BTW STA=920 TO STA=922 WAS REPAIRED PER ER/A 604805-14 SECTION I PERMANENT REPAIR REV ORIGINAL. ASSOCIATED ER/A 14-604805 ADDED FOR AC 9512. (LP #2558078)

Part: SEAT TRACK — CORRODED (BS 479) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

SEAT TRACK SECTION X=-56 BTW STA=479 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK SECTION X=-56 BTW STA=479 WAS REPAIRED IAW SRM 53-20-52-2R REP. 1 FIG. 201.

Part: SEAT TRACK — CORRODED (BS 210-275) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

RIGHT SEAT TRACK SECTION X=-44 BTW STA Y=210 TO Y=275 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00503: CORROSION LEVEL 2. RH SEAT TRACK SECTION X =-44 BTW STA Y=218 TO Y=342 WAS REPAIRED PER B717-200 SRM 53-20 -52-2R PROCEDURE 5.

Part: LONGERON — CRACKED (BS 1144 L2L) · airframe 58,030 hrs · 41,322 cycles

CRACK ON LOGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00469: LONGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2.

Part: PAN — WORN (AFT CARGO DOOR) · airframe 58,030 hrs · 41,322 cycles

WEAR ON SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00061: SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8. FIG. 206.

Part: WEB — CORRODED (BS 256) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON WEB BS 256, X=49. THE WEB WAS REPAIRED IAW SRM 53-00-55-2R-4R.

Part: CUSP WEB — CRACKED (BS 898) · airframe 58,030 hrs · 41,322 cycles

CRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.

Part: CUSP WEB — CRACKED (BS 617-636) · airframe 58,030 hrs · 41,322 cycles

CRACK IN RT CUSP WEB BTW BS 617-636, X=-53 TO X=-59 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 200-266) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

SEAT TRACK X=-22 BTW BS 200-266 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK REPLACED IAW SRM 51-41-01-0G & SRM 51-41-05-0G.

Part: ANGLE — CORRODED (BS 829-912) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORRODED OUT OF LIMITS AT CLIPS STA Y=829, Y=875, Y=912. ORIGINAL THICKNESS IS 0.032 IN AND MINIMUM REMAINING THICKNESS IS 0.10 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00376 AT PAX CABIN. CLIPS STA Y=829, Y=875, Y=912 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-02-0G AND DWG 5913698 REV. K.

Part: WEB — CRACKED · airframe 58,030 hrs · 41,322 cycles

CRACK ON LH CUSP WEB EDGE AT STA Y=717 AND X =56. SUMMARY OF NRC 00373: LH CUSP WEB EDGE AT STA Y=717 AND X=56 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 203. (LP #2548917)

Part: ANGLE — CRACKED (FWD CARGO DOOR) · airframe 58,030 hrs · 41,322 cycles

AFTER SEAL RETAINER REMOVAL, CRACKED INTERNAL ANGLE WAS FOUND ON APROX STA Y=390 AT FWD CARGO DOOR. INTERNAL ANGLE ON AFT LOWER EDGE APROX STA Y=390 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER DWG 9957664 REV N, B717-200 SRM 51-30-07-0G, SRM 51-41-05-0G, AND SRM 51-41-02-0G.

Part: FITTING — CRACKED (FWD CARGO DOOR) · airframe 58,030 hrs · 41,322 cycles

AFTER SEAL RETAINER REMOVAL, CRACK WAS FOUND ON FITTING. FITTING ON AFT LOWER EDGE AT FWD CARGO DOOR WAS REPLACED IAW SRM 51-41-01-0G AND SRM 51-41-02-0G.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CPAX)(W1). SUMMARY OF NRC 00335: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS FABRICATED AND REPLACED PER DWNG 936534 REV BW AND B717-200 SRM 51-41-02-0G. (LP #2547431)

Part: ANGLE — CRACKED · airframe 58,030 hrs · 41,322 cycles

CRACK ON INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00048: INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02 -2R PROCEDURE 1 REPAIR 1. (LP #2548249)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON FLOOR SUPPORT STA Y=218 - X=0 (CPAX)(W1). SUMMARY OF NRC 00363: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=218 - X=0 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2547442)

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 (CPAX)(W1). SUMMARY OF NRC 00361: CORROSION LEVEL 2. GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 WERE REPLACED PER B717-200 SRM 51-41-02- 0G. (LP #2547311)

Part: WEB — PUNCTURED · airframe 58,030 hrs · 41,322 cycles

PUNCTURE ON WEB STA Y=217 - X=-11 WAS FOUND DURING REMOVAL OF GALLEY SUPPORT ON NRC 00361. (CPAX)( W1). SUMMARY OF NRC 00456: WEB STA Y=217 - X=-11 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. PAR 4 FIG. 201. (LP #2545920)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

SECONDARY NRC, IN REF NRC 00364: AFTER REMOVAL PARTS TO ATTEND DISCREPANCY, CORROSION ON FLOOR SUPPORT STA Y=200 AND X=-55 WAS FOUND AT PASSENGER CABIN FLOOR AREA. SUMMARY OF NRC 00462: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 AND X=-55 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2545792)

Part: FLOOR SUPPORT — CORRODED (BS 180) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-42. CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G AND B717-200 SRM 51-41-05-0G.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1). SUMMARY OF NRC 00338: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1) WAS FABRICATED AND REPLACED PER DWG 9936534 -71 AND B717-200 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #2542969)

Part: FLOOR SUPPORT — CORRODED (BS 160-195) · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=160-195. ORIGINAL THICKNESS IS 0.071 IN AND MINIMUM REMAINING THICKNESS IS 0.025 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00352 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-195 AT PAX CABIN WAS FABRICATED AND REPLACED PER DWG 9936534-7 REV: VW AND B717-200 SRM 51-41-05-0G PAR 8. (LP #2541732)

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 58,030 hrs · 41,322 cycles

CORROSION ON RH REPAIR DOUBLER BTWN STA 908 TO STA 927 AND FROM X=44 TO X=59 OF PASSENGER CABIN FLOOR. SUMMARY OF NRC 00333: CORROSION LEVEL 2. PREVIOS REPAIR DOUBLER BTW STA 908 TO STA 927 AND FROM X=-44 TO X=-59 OF FLOOR CABIN PASSENGER WAS REPLACED PER B-717-200 SRM 53-00-55-2R-4 AND SRM 51-40-02-0G. (LP #2541486)

Part: NONE — NONE · airframe 57,418 hrs · 40,748 cycles

THE EMERGENCY LIGHTS OVER THE EMERGENCY EXIT WINDOWS AND ALL OF THE CEILING LIGHTS AFT OF THE OVER WING EMERGENCY EXITS CAME ON IN FLIGHT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE SYSTEM WAS RESET AND THE OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51-00 710-801. (LP #9129018)

Part: NONE — NONE · airframe 57,371 hrs · 40,701 cycles

SHIP 9512 -HYD/GEAR- AN EMERGENCY WAS DECLARED FOR THE APPROACH AND LANDING IN BTR FOLLOWING THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE NECESSARY AND UTILIZED. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE NOSE GEAR STEERING RIGHT HAND ACTUATOR WAS THE SOURCE OF THE LEAK AND REPLACED IT. (LP #9000174)

Part: NONE — NONE · airframe 56,816 hrs · 40,170 cycles

THE AFT LOWER OVERWING EMERGENCY EXIT LIGHTS WERE DISCOVERED AS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8505194)

Part: NONE — NONE · airframe 56,816 hrs · 40,170 cycles

THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. THE BATTERY POWER SUPPLY WAS REPLACED BY MAINTENANCE PER B717 AMM 33-51. OPERATIONAL WAS CHECK GOOD. (LP #8505193)

Part: NONE — NONE · airframe 56,816 hrs · 40,170 cycles

THE AFT BULKHEAD EMERGENCY EXIT LIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8505192)

Part: NONE — NONE · airframe 55,896 hrs · 39,319 cycles

TAIL CONE EXTERNAL RELEASE CLAMP OUT OF RIG LEFT AND RIGHT CLAMPS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0113:5352-4002/003 00423: RIGGED CLAMPS PER B717 AMM 53-52-01. OPERATIONAL CHECK WAS GOOD. (LP #2033419)

Part: NONE — NONE · airframe 55,896 hrs · 39,319 cycles

THE AFT CABIN EMERGENCY EXIT DOOR FRAME HAS TWO LARGE CRACKS. RIGHT HAND MID AREA. -M- SUMMARY SEE NRC 001-0308:5212-2001/001 00084: REPAIRED DAMAGE TO AFT CABIN EMERGENCY EXIT DOOR FRAME IAW PRI 595460-14 REV 0 THROUGH REV 4, AND ER/A 595460-14 REV ORIGINAL. REFERENCE LOG PAGE 2028230 FOR TIME LIMITED MONITOR. ASSOCIATED ER/A 00-595460 ADDED FOR AC 9512. (LP #2029477)

Part: NONE — NONE · airframe 55,896 hrs · 39,319 cycles

THE LEFT HAND FORWARD ENTRY DOOR SLIDE HAS THE PARACHUTE PIN ROUTED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0025:5211-4002/002 00405: THE LEFT HAND FORWARD ENTRY DOOR SLIDE WAS REPLACED IN REF B717 AMDS 2561-9004. (LP #2028225)

Part: NONE — NONE · airframe 55,896 hrs · 39,319 cycles

THE TAIL CONE SLIDE IS MISSING THE CABLE GUIDES. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED THE CLIP REF B717 AMM 25-61-02. (LP #2020658)

Part: NONE — NONE · airframe 55,896 hrs · 39,319 cycles

THE PROTECTIVE WRAP IS TORN ON CANNON PLUG RECEPTACLE R5-1150, ABOVE ACCUMULATOR IN RIGHT GEAR WELL. SUMMARY SEE NRC 001-0241:5300-2003/001 00268: WRAPPED PER B717 AMM 20-30-02 912-801. (LP #2020181)

Part: FRAME — CORRODED (BS 927) · airframe 53,144 hrs · 37,020 cycles

CORROSION WAS FOUND ON AFT SIDE OF STA 927. NRC 031-0008:5331-2001/003 00208; CORROSION LEVEL 1, MAINTENANCE SPLICED IN A NEW FRAME SECTION REF B717 SRM 53-20-07-2R-3. (LP #1354370)

Part: SKIN — DELAMINATED (SPOILER) · airframe 18,741 hrs · 12,969 cycles

INBOARD SPOILER ASSEMBLY PN# 5940974-502 WAS FOUND DURING ROUTINE WALKAROUND BY AIRCRAFT MAINTENANCE TO BE DELAMINATED AT BOTH THE UPPER AND LOWER SKINS. FURTHER INSPECTION AT FAA-145 SHOP LEVEL DETERMINED ENTIRE SPOILER TO BE DELAMINATED AT BOTH THE UPPER AND LOWER SKIN LOCATIONS.

Part: COALESCER BAG — ODOR (COCKPIT TEMP) · airframe 50,665 hrs · 35,293 cycles

WHEN COCKPIT TEMP CONTROL IS SET ABOVE CURRENT TEMP AC BLOWS WARM AIR THROUGH COCKPIT DUCT SYSTEM WARM AIR HAS HEAVY OILY SMELL. PERFORMED B717 FIM 21-22-00-810-808, REPLACED COALESCE BAGS B717 AMM 21-54. INSPECTED LEFT AND RIGHT PACK DUCT BETWEEN TEMP CONTROL VALVES AND HEAT EXCHANGERS. NO OIL CONTAMINATION FOUND, INSPECTED BUFFER AIR VALVE REF AMM 75-22-01 NO DEFECTS. C/W B717 AMM 21-54-00-100-801, NO SMELL NOTED AT THIS TIME. C/W AMDS CARD 0550-2001. OK FOR SERVICE. (LP5063540)

Part: LIGHT — DEPARTED (NLG) · airframe 50,352 hrs · 35,065 cycles

ON ARRIVAL ORD FOUND RT NOSE LANDING/TAXI LIGHT DEPARTED A/C. REPLACED NOSE TAXI LIGHT AND CLAMP. (LP4939010)

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 49,494 hrs · 34,455 cycles

THE L1 DOOR SLIDE BOTTLE PRESSURE WAS FOUND TO BE IN THE RED ARC. MAINTENANCE REPLACED THE L1 DOOR SLIDE IAW AMDS CARD 2561-9004.

Part: FRAME — CRACKED (BS 674) · airframe 48,436 hrs · 33,768 cycles

CRACK IN UPPER RADIUS OF FRAME BS 674 . REPLACED THE FRAME IAW 5310-01436-03A.

Part: TAIL CONE — OUT OF RIG (FUSELAGE) · airframe 48,427 hrs · 33,760 cycles

THE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY DURING USE OF THE EXTERNAL TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK WITHIN LIMITS.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,427 hrs · 33,760 cycles

FLOOR SUPPORT BRACKET CRACKED AT STA 715 LBL 38. REPLACED BRACKET REF DWG 9923417.

Part: TAIL CONE — OUT OF RIG (FUSELAGE) · airframe 48,427 hrs · 33,760 cycles

REQUIRED TO RELEASE THE COMPLETELY RIGGED TAILCONE IS 30+/- 5LBS. THE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY USING THE INSIDE TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK IS NOW WITHIN LIMITS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,529 hrs · 33,187 cycles

CABIN CEILING MOUNTED EMERGENCY LIGHT MISSING THE LENS AT ROW 25CDE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,780 hrs · 32,631 cycles

AFT OVERWING EMER EXIT DOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY B5-230 REF AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 46,621 hrs · 32,511 cycles

AFT EMERGENCY LIGHT LENS MISSING ABOVE AFT LAVATORY DOOR. INSTALLED A NEW LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,548 hrs · 31,755 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT LEFT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. REPLACED THE LAMP AND THE OPERATIONAL CHECKED GOOD.

Part: VANE — LOOSE (RT WING TE FLAP)

DURING UNSCHEDULED NON-ROUTINE CHECK, INBD FLAP FORWARD MOVABLE VANE HAS PLAY AT TORQUE TUBE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,523 hrs · 30,203 cycles

DURING THE TURNAROUND CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR BOTH THE MAIN CABIN DOOR AND THE GALLEY DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LANYARD — BROKEN (ESCAPE SLIDE) · airframe 43,542 hrs · 30,216 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD A BROKEN DEPLOYMENT LANYARD. THIS BROKEN LANYARD, WHICH ATTACHES THE SLIDE ASSY TO THE TAIL CONE, WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYSTEM AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAILCONE DEPLOYMENT SYS WAS REPLACED AND AN RII WAS COMPLETED SATISFACTORILY.

Part: SEAL — LOOSE (L1 DOOR) · airframe 43,506 hrs · 30,190 cycles

L1 DOOR PRESSURE SEAL MID AFT AREA ADJACENT TO BAYONET HAS LOOSE RETAINER SCREWS. REF: ORNRC 63165-0800-0005. INSTALLED REPAIR IAW ER/A 542358-14, REV ORIGINAL AT L1 DOOR PRESSURE SEAL MID AFT AREA.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 43,506 hrs · 30,190 cycles

DOOR JAMB HAS MULTIPLE AREAS OF CORROSION. BLENDED CORRODED AREAS AND FOUND TO BE OUT OF LIMITS. REMOVED DOOR JAMB AND INSTALLED REPAIR PARTS AND SURROUNDING STRUCTURE IAW SRM 53-20-15, REPAIR 6.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,506 hrs · 30,190 cycles

R1 DOOR FAN AREA CORROSION AT FWD AND AFT CUSP WEB POCKETS AND FLOOR PANEL SUPPORT EXTRUSION MARKED IN RED. REPLACED UPPER CUSP ANGLE AT R1 DOOR FAN AREA, FWD AND AFT CUSP WEB POCKETS AND FLOOR SUPPORT EXTENSION IAW SRM 53-00-55, REPAIR 3.

Part: BRACE — CORRODED (R1 DOOR) · airframe 43,506 hrs · 30,190 cycles

FWD WEB BRACE FOR R1 DOOR. CORROSION BLENDED BEYOND 20 PERCENT LIMIT MARKED. PART ON R1 REPAIR PARTS RACK. REF ORNCR 63165-0200-0275, FABRICATED NEW ANGLE IAW DWG 5910085. ANGLE HEAT TREATED TO T42 CONDITION. INSTALLED NEW ANGLE IAW SRM 51-41-05, PG 1.

Part: WEB — CORRODED (R1 DOOR FRAME) · airframe 43,506 hrs · 30,190 cycles

WEB NR 1 FWD LOWER FOR R1 DOOR CORROSION AND ELONGATED FASTENER HOLES MARKED PART ON R1 DOOR PARTS RACK, REF 63165-0200-0276. REPLACED WEB NR 1 FWD LOWER, OUT R1 DOOR IAW SRM 51-41-02, PG 1-4, 51-41-04, FIF 4 AND 51-41-05, PG 1.

Part: PAN — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 43,506 hrs · 30,190 cycles

ALC DOOR FRAME CORRODED AT LOWER END IN THRESHOLD AREA. REF ORNRC 63165-0800-0014. INSTALLED NEW DOOR PAN IAW SRM 53-20-15.

Part: CUSP WEB — CORRODED (BS 208-218) · airframe 43,506 hrs · 30,190 cycles

CORROSION ON CUSP WEB, BS 208-218, LBL 56 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0220, PERFORMED INSPECTION WEB REPAIR AT BS 208-218, LBL 56 IAW SRM 51-70-10, REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (BS 197-207) · airframe 43,506 hrs · 30,190 cycles

CORROSION ON FLOOR SUPPORT AT BS 197-207, LBL 58 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0217. REPLACED FLOOR SUPPORT AT BS 197-207, LBL SB JUST INSIDE L-1 DOOR IAW SRM 57-41-02, FIG 211.

Part: FLOOR SUPPORT — CORRODED (BS 218) · airframe 43,506 hrs · 30,190 cycles

CORROSION ON FLOOR SUPPORT BS 218, LBL 48 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0219. REPLACED FLOOR SUPPORT WITH NEW SUPPORT BS 218, LBL 48 IAW SRM 51-41-02, FIG 201.

Part: FUEL TANK — CORRODED (BS 696-737) · airframe 43,506 hrs · 30,190 cycles

THE UPPER LT EXTERNAL SURFACE OF THE CENTER WING FUEL TANK HAS AREAS OF CORROSION FROM BS 696 TO 737, LBL 30 TO FUSELAGE SKIN. AREAS MARKED. REF 63165-0100-0187. BLENDED AND REMOVED CORROSION ON UPPER SKIN IAW SRM 57-10-01. MATERIAL REMOVED .010 IN SKIN IS WITHIN LIMITS IAW 57-10-01, FIG 108.

Part: STRINGER SPLICE — CORRODED (BS 958-974) · corrosion level 2 · airframe 43,506 hrs · 30,190 cycles

BS 958-974 S30 SPLICE IS CORRODED. MARKED, REF ORNRC 63165-0100-0037, REPLACED SPLICE IAW SRM 51-41-05.

Part: STRINGER SPLICE — CORRODED (BS 927-946) · corrosion level 2 · airframe 43,506 hrs · 30,190 cycles

BS 927- 946, S30 & SPLICE IS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-41-05.

Part: CUSP WEB — CORRODED (BS 389-427) · airframe 43,506 hrs · 30,190 cycles

CORROSION ON RT SIDE CUSP WEB AND CLIPS BS 389 - 427. REMOVED CORROSION IAW SRM 53-00-55, PG 101. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW SRM 53-00-55, REPAIR NR 4.

Part: SKIN — CRACKED (BS 1076) · airframe 42,876 hrs · 29,736 cycles

DURING LINE CHECK, MAINTENANCE NOTED A SKIN CRACK ON THE RT FUSELAGE AT BS 1076, STR 14 RT. THE CRACK WAS APPROXIMATELY 1.4" IN LENGTH. REPAIRED IAW ER/A 539301-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,749 hrs · 29,618 cycles

DURING LINE CHECK, NOTED F/A EMERGENCY LIGHT SWITCH WAS INOPERATIVE. REPLACED AFT CARGO EMERGENCY POWER BATTERY PACK & BATTERY POWER SUPPLY UNIT IAW 33-51. ALL CHECKED NORMAL.

Part: DOOR FRAME — NOT REPORTED (BS 674 - 715) · airframe 41,164 hrs · 28,310 cycles

FUSELAGE OVERWING DOOR FRAME BS 674 - 715. REPLACED IAW AA 5310-01436, LOGS 1743028, 1744982, 1744986, 1750332.

Part: FRAME — CRACKED (BS 674) · airframe 41,170 hrs · 28,314 cycles

BS 674 RT OVERWING FRAME CRACKED JUST BELOW FLOOR. REPLACED THE FRAME IAW AMDS WC 5310-01436-03B.

Part: WEB — CRACKED (BS 655-674) · airframe 41,170 hrs · 28,314 cycles

FLOOR WEB IS CRACKED BETWEEN OVERWING FRAMES BS 655-674. REMOVED & FABRICATED NEW WEB IAW DWG 9910151-147.

Part: CUSP WEB — DAMAGED (BS 655) · airframe 41,170 hrs · 28,314 cycles

CUSP WEB DAMAGED AT BS 655. INSTALLED A REPAIR TO THE CUSP WEB IAW SRM 53-00-00, FIG 207.

Part: JACKSCREW — NOT REPORTED (HORIZONTAL STAB) · airframe 40,649 hrs · 27,912 cycles

HORIZONTAL STABILIZER JACKSCREW REPAIRED IAW AA 2740-01114.

Part: BOTTLE — DISCHARGED (L1 DOOR SLIDE) · airframe 40,301 hrs · 27,595 cycles

DURING A CABIN CHECK, FOUND L1 SLIDE PRESSURE GAUGE NEEDLE IN RED BAND. REPLACED L1 SLIDE AND COMPLIED WITH REQUIRED INSTALLATION INSPECTION.

Part: ACTUATOR — BYPASSING (MLG) · airframe 39,721 hrs · 27,040 cycles

FLIGHT CREW PERFORMED AN AIR RETURN DUE TO A LT AND RT MLG UNSAFE INDICATION WITH ASSOCIATED GEAR DOOR OPEN LIGHTS AND THE GEAR HANDLE IN THE UP POSITION. ONCE THE GEAR HANDLE WAS PLACED IN THE GEAR DOWN POSITION THE CREW REPORTED THAT THEY HAD 3 DOWN AND LOCKED GEAR INDICATIONS. AN EMERGENCY WAS DECLARED IAW THE CREW REPORT. THE ACFT HAD A UNEVENTFUL LANDING. WHILE WAITING ON ACFT JACKS TO ARRIVE, MAINTENANCE REPLACED THE LANDING GEAR CONTROL VALVE. ONCE THE ACFT WAS JACKED AND THE GEAR WAS SWUNG, THE LT MLG RETRACT ACTUATOR WAS FOUND TO BE BYPASSING. THE LT MLG RETRACT ACTUATOR WAS REPLACED, THE GEAR SUCCESSFULLY OPERATED THROUGH FULL TRAVEL. THE ACFT WAS RETURNED TO SERVICE.

Part: GUIDE — OUT OF POSITION (TAILCONE SLIDE) · airframe 39,249 hrs · 26,604 cycles

DURING INSPECTION, NOTED TAILCONE SLIDE CABLE GUIDE (AFT) ON SLIDE RACK OUT OF POSITION. REPOSITIONED TAILCONE SLIDE CABLE GUIDE (AFT) IAW AMM 25-61-02-400.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 39,246 hrs · 26,601 cycles

LT FWD OVERWING DOOR EMERGENCY EXIT SIGN BULB LOOSE. SECURED BULB IAW MM.

Part: ACCESS PANEL — LOOSE (CABIN) · airframe 39,246 hrs · 26,601 cycles

RT EMERGENCY BATTERY ACCESS PANEL LOOSE AT ROW 17. SECURED PANEL IAW MM.

Part: TRACK — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

RT TRACK CORRODED BETWEEN STATION 160 TO STATION 218. R & R TRACK IAW SRM & DRAWING.

Part: TRACK — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

LT TRACK CORRODED BETWEEN STATION 160 TO STATION 218. R & R TRACK IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

CUSP WEB CORRODED BETWEEN STATION 152 TO STATION 160, BETWEEN LBL 6 TO RBL 6. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

RT CUSP WEB CORRODED BETWEEN STATION 927 TO STATION 946. R & R WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

SEAT TRACK CORRODED AT STATION 200, RBL 22. REPAIRED SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

LT CUSP WEB CORRODED BETWEEN STATION 541 TO STATION 560. REPAIRED DOUBLER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN STATION 493 TO STATION 588, RBL 44. REPAIRED SEAT TRACK IAW SRM.

Part: COVER — CRACKED (TE FLAP) · airframe 39,009 hrs · 26,451 cycles

RT WING FLAP BETWEEN INBD & OTBD FLAP VANE JOINT COVER CRACKED. R & R COVER IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

MAIN CABIN WEB CORRODED AT STATION 175 TO STATION 200, LBL 10 TO RBL 10. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 39,009 hrs · 26,451 cycles

LT CUSP WEB CRACKED AT STATION 674. R & R WEB IAW SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 38,595 hrs · 26,179 cycles

EXIT SIGN OVERHEAD AT ROW 1 FELL OFF. SECURED SIGN IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 36,930 hrs · 25,161 cycles

R-1 EXIT SIGN MISSING. INSTALLED MISSING LENS ON R-1 DOOR EXIT SIGN.

Part: FRAME — CRACKED (NLG WW) · airframe 36,501 hrs · 24,891 cycles

NOSE LANDING GEAR WHEEL WELL CUTOUT AT STA 106 RBL - 6, FRAME IS CRACKED. REMOVED AND REPLACED NLG WHEEL WELL CUTOUT FRAME AT STA 106, RBL 17 TO LBL 17 IAW B717 SRM 51-41-02, 51-40-08 AND MD DWG 5913421.

Part: LATCH — BROKEN (EMERGENCY EXIT) · airframe 35,948 hrs · 24,538 cycles

LEFT EMERGENCY EXIT LATCH BROKEN AT ROW 21. REMOVED AND REPLACED LATCHES PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 35,935 hrs · 24,529 cycles

RIGHT EEPLS INOP AT ROW 29. CONNECTED CONNECTOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,231 hrs · 24,068 cycles

EMERGENCY EXIT LIGHT BATTERY INOP AT BS 794. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 35,231 hrs · 24,068 cycles

EMERGENCY EXIT LIGHT BATTERY FAILED TO CHARGER AT BS 218. REMOVED AND REPLACED BATTERY PER MM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

CUSP WEB CORRODED AT BS 494, STR 18L. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

SHEAR TIE CORRODED AT BS 1022, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

SHEAR TIE CORRODED AT BS 927, BETWEEN STR 30 TO STR 29L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

CUSP WEB CORRODED AT BS 563, STR 18R. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

CUSP WEB CORRODED AT BS 923, STR 18R. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

FRAME CORRODED AT BS 832, BETWEEN STR 27L TO STR 29L. REMOVED AND REPLACED FRME IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

CUSP WEB CORRODED BETWEEN BS 449 TO BS 506, STR 18R. REPAIRED WEB IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

STRINGER CORRODED BETWEEN BS 996 TO BS 1012, BETWEEN STR 30L TO STR 30R. REMOVED AND REPLACED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

FRAME CORRODED AT BS 851, BETWEEN STR 29L TO STR 27L. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

FRAME CORRODED AT BS 832, BETWEEN STR 30R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,231 hrs · 24,068 cycles

FRAME CORRODED AT BS 851, BETWEEN STR 26L TO STR 30L. REMOVED AND REPLACED FRME IAW SRM.

Part: PIN — OUT OF ALIGNMENT (TAILCONE)

TAIL CONE DEPLOYMENT SYSTEM RELEASE MECHANISM CAM PIN NOT ALIGNED. ROTATED TAIL CONE RELEASE MECHANISM CAM PIN FULLY CLOCKWISE TO CORRECT POSITION WAS REQUIRED IAW BOEING 717 MM 53-52 NO ADJUSTMENTS MADE TO SYSTEM OR SETTINGS. OK FOR CONTINUED SERVICE.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L-1 DOOR SLIDE PACK BAYONET PIN OUT OF GROMMET AWI. REMOVED AND REPLACED L-1 DOOR SLIDE PACK IAW REF M/M 25-61 AWI.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN, STA 229 TO 250, LONG L16L TO L18L, DENT. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-01839A. SEE NR 3643 AND 1888.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 225 TO 247, RBL24, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02502IR. SEE NR 5487 AND 1889.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5473.

Part: LANYARD — BROKEN (GIRT BAR)

R-1 DOOR LANYARD BROKEN ON GIRT BAR. REMOVED AND REPLACED R-1 DOOR GIRT BAR LANYARD ASSY REF AMM 25-61.

Part: TERMINAL — BROKEN (AC BAY)

EMERGENCY LIGHT INOPERATIVE ON CATWALK PATH CEILING IN AFT ACCESSORY COMPARTMENT. REPAIRED WIRE TERMINAL ON AFT ACCESSORY CATWALK CEILING EMERGENCY LIGHT IAW B717 MM 33-51. REF B717 MM 20-30 FOR TERMINAL REPAIR. OPS CHECK GOOD.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY)

CORROSION ON AFT CARGO COMPARTMENT LOWER JAMB AREA. CUT OUT DAMAGED SECTION OF LOWER JAMB AREA, AND INSTALLED NEW SECTION P/N J060228-9 WITH 2EA SPLICES, INSTALLED ON FWD AND AFT SECTION, MATERIAL USED .040 T075-0, HEAT TREATED TO T-6 AND INSTALLED IAW B 717 SRM 53-20-15 FIG 201.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY)

CORROSION AT FWD CARGO COMPARTMENT LOWER JAMB. INSTALLED NEW LOWER JAMB PAN BETWEEN STA 370-00 AND 427.00 PER B717 SRM 53-20-15 FIG 201.

Part: HOUSING — LEAKING (RT ENGINE)

RIGHT FUEL LEAK. REPLACED LP FUEL FILTER HOUSING LEAK CHECK OK, GOOD FOR FURTHER SERVICE REF 73-11.

Part: SKIN — DENTED (FS 237)

FUSELAGE SKIN HAS DENT AT FUS STA 237 ABOVE LONG 18L. INSTALLED FLUSH REPAIR TO FUSELAGE SKIN AT FS 237 ABOVE LONGERON 18L DUE TO DENT. REPAIR 21 X 14 X 0.050 INCH, 2024 T3 INSTALLED PER B717 SRM 53-00-01 PG 208 FIG 201.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

EMERGENCY EXIT SIGN ABOVE FORWARD FLIGHT ATTENDANT SEAT COMES ON DIM WHEN ENTRY LIGHT SWITCH TURNED ON. SIGN OPS CHECK AS REQUIRED WITH EMERGENCY LIGHTS ON. ALSO LIGHT ABOVE L-1 DOOR AND 3 LIGHTS NEXT TO ENTRY LIGHTS. SECURED GROUND WIRE AT FORWARD ENTRY LIGHT ASSEMBLY, OPS CHECK FORWARD LIGHT AND EMERGENCY LIGHT NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT ABOVE SEAT ROW 16 INOPERATIVE. REPLACED EMERGENCY LIGHT CHARGER (POWER SUPPLY).

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-125 OPS CHECK GOOD.