N957AT

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,491 hrs · 40,620 cycles

SHIP 9516 FRAME AND FASTENERS DAMAGED AT 6 O'CLOCK POSITION ON CANTED. CORECTIVE ACTION: COMPLIED WITH ER/A 627973-14 (1130003)

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,472 hrs · 40,599 cycles

SEVERAL AREAS OF CORROSION AROUND FASTENES. REPLACED FORWARD CARGO DOOR LOWER JAMB PAN IAW B717-200 SRM 53- 20-15-2R (1108952)

Part: PIN — COCKED (TAIL CONE) · airframe 57,472 hrs · 40,599 cycles

TAIL CONE RELEASE CAM PIN CLOCKED INCORRECTLY. ADDED WASHERS AND SHIMS WHICH WAS MISSING FROM THE TAIL CONE RELEASE CAM PIN TO CORRECT EXCESSIVE FORWARD AND AFT PLAY IN TAIL MECHANISM RELEASE CAM ASSEMBLY REF B717 AMM 53-52-03.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 57,310 hrs · 40,450 cycles

SHIP 9516 - DIV - DIVERSION TO ORD DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND SEVERAL HPC BLADES DAMAGED. REPLACED NBR 1 ENGINE. (LP 7264142)

Part: PCDU — FAULTED (ZONE 200) · airframe 56,687 hrs · 39,877 cycles

SHIP 9516 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING A "RIGHT DC BUS FAILURE" INDICATION. THE RESULT OF THAT WAS A NO FLAP, NO SLAT LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT PCDU AND THE LEFT POWER CONTACTOR RELAY. PERFORMED ALL RTS TESTS. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #7235652)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,939 hrs · 39,197 cycles

THE OVERWING EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT LIGHT BATTERY PACK PER B717 AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE. (LP #6703153)

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 55,404 hrs · 38,725 cycles

DURING SERVICE CHECK, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE FROM THE FLIGHT ATTENDANT PANEL. MAINTENANCE FOUND THAT THE CABIN EMERGENCY LIGHTS WOULD WORK WITH COCKPIT SWITCH ARMED AND FLIGHT ATTENDANT SWITCH SET TO "ON" ONLY, BUT NOT FROM FLIGHT ATTENDANT PANEL ALONE. CHECKED VOLTAGE GOING TO THE FLIGHT ATTENDANT SWITCH S1-387, ALL TERNMINAL SHOWING 28 VDC. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK ASSY B5-125 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5718809)

Part: CIRCUIT BREAKER — TRIPPED · airframe 55,318 hrs · 38,649 cycles

SHIP 9516 -MISC/DE- THE "DC R BUS OFF" WARNING ILLUMINATED IN CRUISE FLIGHT, ALONG WITH MANY OTHER ASSOCIATED MESSAGES. THE FLIGHT CREW DECLARED AN EMERGENCY INTO MKE DUE TO LOSS OF RIGHT DC BUS, BUT LANDED UNEVENTFULLY. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE RIGHT PCDU CB3 CIRCUIT BREAKER HAD TRIPPED. THE RIGHT PCDU WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD. (LP #5997362)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,649 hrs · 38,063 cycles

TAIL CONE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWERPACK REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275902)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,642 hrs · 38,057 cycles

ON SERVICE CHECK, FOUND AFT OVERWUNG EXIT SIGNS ABOVE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY CASE CRACKED. INSTALLED NEW BATTERY IAW B717 AMM 33-51-04. REPLACED POWER PACK ASSY PER B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275763)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,095 hrs · 37,591 cycles

GOUGES FOUND AT FUSELAGE BELLY SKIN FOR #1 RAD ALT TRANS ANTENNA. SUMMARY NRC 003-0001:0514-2001/001 00011: C/W ERA 614660-14 REV ORIG REPAIR INSTRUCTIONS. CHECKED TO ENSURE ALL PRI'S MATCH ERA 614660-14 REV ORIG. REPAIRED SKIN PER ERA 614660-14 REV ORIG. (LP #0128522)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,043 hrs · 37,555 cycles

AFT OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5513464)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK ON DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00141: DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #2911591)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

OUTER EMERGENCY TAILCONE HANDLE IS ARMED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00731: EMERGENCY TAILCONE HANDLE WAS REINSTALLED CORRECTLY PER B717-200 AMM 53-52-01-400-801. (LP #2909467)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON INTERCOSTAL (2 EA) BTW LONGERON 22 AND 21 LH FROM FRAME 1037 TO 1058 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00201: CORROSION LEVEL 2. INTERCOSTALS (2 EA) BTW LONGERON 22 AND 21 LH FROM FRAME 1037 TO 1058 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2906420)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION DAMAGE TO INTERNAL SKIN BETWEEN LONGERON 21-22L, FRAMES Y1037- Y1058 AT AFT CARGO COMPARTMENT, DAMAGE IS ESTIMATED TO EXCEED THE ALLOWABLE LIMITS. SUMMARY OF NRC 00656: CORROSION LEVEL 2. INTERNAL SKIN BETWEEN LONGERON 21-22L BTW FRAMES STA Y=1037 - Y=1058 AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 610195-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2906095)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

WEAR ON FWD/AFT LATCH FITTINGS AT AFT CARGO DOOR. SUMARY OF NRC 00135: THE LATCH FITTINGS AT AFT/FWD AT AFT CARGO DOOR WERE REPLACED PER BOEING CMM 52-30-2. (LP #2901739)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FRAME STA 1037 BETWEEN LONGERON 24 TO LONGERON 21 LH AT AFT CARGO COMPARTMENT IS OUT LIMITS WITH 0.040 IN PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PAR. 4. C. FIGURE 103. SUMMARY OF NRC 00660: CORROSION LEVEL 2. FRAME STA 1037 BTW LONG 24 LH TO LONG 21 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3. (LP #2898728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00667: CORROSION LEVEL 2. STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PER B-717-200 SRM 51-41-05-0G, 51- 41-01-0G PAR 6, AND 51-41-02-0G. (LP #2897903)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON LONGERONS END (28 Y 27) LH AND LONGERONS END (23 Y 26) LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00641: CORROSION LEVEL 2. LONGERONS END (28,27,26,23) LH AT AFT CARGO COMPARTMENT WERE REPLACED PER B-717-200 SRM 51-41-05-0G PAR 8.B . (LP #2896107)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON ANGLE OF FRAME BTW LON 27R TO LON 28L STA 908 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: CORROSION LEVEL 2. ANGLE OF FRAME BTW LONG 26L TO LONG 26R STA 908 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 9975524 REV P AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2893490)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 908 BTW L29-L AND L29 -R. SUMMARY OF NRC 00561: CORROSION LEVEL 2. REPAIR SPLICE AT FRAME STA 908 BTW LONGERON 27R TO LONGERON 28L WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. REPAIR SPLICE (4 EA) STA Y=908 BTW L-25 LH TO L-25 RH WERE INSTALLED UNDER NRC 00161. (LP #2893598)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON LON-30, LON-28L, AND LON-29L BTW STA 905 TO STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00158: CORROSION LEVEL 2. LON-30, LON-28LH, AND LON-29LH BTW STA 905 TO STA 1053 WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6, 51-41-02-0G PAR 4, AND 51-41-05-0G PAR 8. (LP #2894305)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R. SUMMARY OF NRC 00560: CORROSION LEVEL 2. FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 PAR 5, 51- 41-02-0G, 51-41-05-0G AND PER 53-20-07-2R PROCEDURE 3 PAR. 6, THE REPAIR'S SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 25,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 6,500 CYCLES. (LP #2891710)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION WAS FOUND ON LONGERON 22LH END FORWARD SECTION AT STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00679: CORROSION LEVEL 2. LONGERON END 22LH WAS FABRICATED AND REPLACED PER DWG 4914954 REV A. (LP #2891485)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00233: CORROSION LEVEL 2. ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 995814-39 REV CC AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2891445)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

DISBOND ON RUDDER TAB LH SIDE OF 1.7000IN LENGTH X 0.500IN WIDTH AT DENT #2, (9" ABOVE #2 HINGE 3"AFT L/E RUDDER TAB) IN REF MON JOB 029-0001, LOG 1488874. SUMMARY OF NRC 00564: DENT #2 AT RUDDER TAB LH SIDE WAS REPAIRED PER ER/A 609491-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 609491-14 REV 2. ASSOCIATED ER/A 14-609491 ADDED FOR AC 9516. (LP #2888271)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FRAME CLIP BTW LONGERON 26LH TO 26 RH STA Y=1022 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00710: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STR 26RH TO STR 26LH WAS FABRICATED AND REPLACED PER DWG 9912243 REV JS AND PER B717-200 SRM 51-41-02-0G. (LP #2886149)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON LOWER CUTOUT BTW FRAME 990 TO 950 AFT DOOR CARGO. SUMMARY OF NRC 00240: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4 AND 51-41-05-0G PAR 8. (LP #2879720)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR PANELS 222XF, 222NF, 223EF, 221SF, 221XF, 222HF, 222MF, 223AF, 222AQF, 222AWF, 222AJF, 222ASF, 222ZF, 222ALF, AND 222EF AT PASSENGER CABIN. SUMMARY OF NRC 00503: FLOOR PANELS 222XF, 222NF, 221XF, 222HF, 222MF, 223AF, 222AWF, 222ALF WERE REPAIRED PER B717-200 SRM 53- 00-00-2R, REPAIR 2. FLOOR PANELS 221SF AND 222ASF WERE FABRICATED AND REPLACED PER DRAWING 9956336 REV G AND DRAWING 9952521 REV BB. FLOOR PANELS 222AJF, 222AQF, 222EF, 222ZF, AND 223EF WERE REPAIRED PER ERA 610204-14 REV ORIG. AND PRI 610204-14 REV 1. ASSOCIATED ERA 14-610204 ADDED FOR AC 9516. (LP #2876212)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON TRACK BTW FRAME 950 TO 884 RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00242: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 950 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (LP #2874605)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON TRACKS RBL16 AND LBL16 BTW STA 810 TO STA 895 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: CORROSION LEVEL 2. TIE TRACKS RBL16 AND LBL16 BTW STA 810 TO STA 895 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2874607)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON ANGLE OF FRAME STA 927 BTW L29R TO L27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00166: CORROSION LEVEL 2. ANGLE OF FRAME STA 927 BTW L29R TO L27L WAS FABRICATED PER DWG 9915524 REV M. NEW ANGLE OF FRAME STA 927, STRAP STA 908 STR 28RH AND 29RH, STRAP STA 927 STR 29RH, SPLICE LH STA 927 BTW STR 26-27, SPLICE RH STA 927 BTW STR 26-27, INTERCOSTAL STR 28 RH BTW STA 908-927 AND INTERCOSTAL STR 29 RH BTW STA 908-927 MUST BE INSTALLED UNDER NRC 00560. (LP #2874273)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON TRACK BTW FRAME 1022 TO 884 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 1022LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2874544)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00563: CORROSION LEVEL 2. AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT WAS FABRICATED PER B717-200 SRM 53-20-15-2R PROC 7 AND INSTALLED PER NRC 00240. (LP #2874456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON SPLICE (4 EA) BTW FRAME 990 TO 950 FROM LONGERON 30 AND 27 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00227: CORROSION LEVEL 2. SPLICE (4 EA) L-28 LH AND L-27 BTW STA Y=974 TO STA Y=994 AND SPLICE L-29 BTW STA Y=954 TO Y=974 LH WERE REPLACED PER DWG 3913557 REV "D" AND DWG 3913291 REV "F". SPLICE BTW STA=954 TO STA=974 L-30 WAS FABRICATED PER B717-200 SRM 51-40-08-0G DWG: 3914677 REV: "D". (LP #2873029)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON GIRT BAR FITTINGS AT R1 DOOR. SUMMARY OF NRC 00691: CORROSION LEVEL 2. GIRT BAR FITTINGS (2 EA) WERE REPLACED PER B717 SRM 51-40-08-0G. (LP #2865125)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

AFTER LONGERON 26 LH BTW STA Y=900 TO STA Y=1053 REMOVAL, CORROSION WAS FOUND AT FUSELAGE SKIN BTW STA 1000 TO STA 1006 L-26 LH. SUMMARY OF NRC 00688: CORROSION LEVEL 2. FINGER DOUBLER AT STA 946 TO 1006 LONGERON 26 LH WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2864406)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200. SUMMARY OF NRC 00472: CORROSION LEVEL 2. TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200 WERE REPLACED PER B717 SRM 51-40-08-0G AND DWG 957828 REV AB. (LP #2863315)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON WEBS BTW STA Y=148/218 AND BTW STA X=-60/60 AT PAX CABIN (W1). SUMMARY OF NRC 00373: CORROSION LEVEL 2. WEB STA Y=158/200 AND BTW X=-3.5/-60 AND Y=158/200 AND BTW X 48/60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #2861223)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 AT PAX CABIN (W1). SUMMARY OF NRC 00413: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 WAS REPAIRED PER ER/A 609285-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 609285 REV 1. ASSOCIATED ER/A 14-609285 ADDED FOR AC 9516. (LP #2855756)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK ON FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00291: FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2853009)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=200 AND BTW RBL=44/54 AT PAX CABIN WERE FOUND OUT OF LIMITS (W1). SUMMARY OF NRC 00676: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=200 AND BTW RBL=44/54 WERE REPLACED PER B717-200 SRM 51-40-02-0G. (LP #2850734)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR SUPPORTS STA Y=197 AND BTW LBL=15/43 WAS FOUND OUT LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=197 BTW LBL=15/43 WAS FABRICATED AND REPLACED PER DWG 99365534 REV BW AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2850635)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

FLOOR SUPPORT STA Y=200 LBL=6 WAS FOUND CORRODED OUT OF LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00678: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 LBL=6 TO RBL=6 WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2849660)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON LONGERON END 24 RH BTW FRAME 1022 TO 1002 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00212: CORROSION LEVEL 2. LONGERON END 24 RH BTW STA Y=1022-Y=1002 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2846590)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR SUPPORTS BTW STA Y=158/200 AND RBL=44, STA Y=179 AND BTW RBL=8/43, STA Y=200 AND BTW RBL=8/44. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) WERE REPLACED PER B717-200 SRM 51-40-02-0G AND 51-41-05-0G PAR 8.A. (LP #2846527)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON SEAT TRACK -X=22.0 BTW STA Y=200 TO STA Y=270. SUMMARY OF NRC 00603: CORROSION LEVEL 2. SEAT TRACK SECTION X=-22.0 BTW STA Y=200 TO STA Y=270 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2842925)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

SEVERAL CRACKS ON CUSP WEB LH SIDE LOWER SIDE STA Y=586 BTW X=+60 AT PAX CAB. SUMMARY OF NRC 00520: CUSP WEB LH STA 579 TO STA 598 WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 AND DWG: 9910151 REV CH AND REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2841783)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON CUSP WEB BTW STA Y=218/220 AND BTW STA X=-44/-54 AT PAX CABIN (W1). SUMMARY OF NRC 00377: CORROSION LEVEL 2. CUSP WEB BTW STA Y=218/220 WAS REPLACED B717-200 SRM 51-41-02 PAR 4 AND 51 -41-05-0G. (LP #2839683)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR SUPPORT STA Y=370 BTW STRG 29R AND STRG 29L AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00190: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=370 BTW STRG 29R AND STRG 29L AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2839189)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK FOUND ON CUSP WEB AFTER REMOVAL ANGLE ON FLOOR STRUCTURE RH SIDE BTW STA 636 AND STA 655 PAX CABIN. SUMMARY OF NRC 00607: CUSP WEB RH SIDE BTW STA 636 AND STA 655 PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R4. (LP #2836798)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK ON FRAME STA Y=1037 OVER SRT 17 RH AT CPAX. SUMMARY OF NRC 00424: FRAME STA Y=1037 OVER SRT 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2836625)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK WAS FOUND ON FWD PAN OF AFT CARGO DOOR. (PTAS). SUMMARY OF NRC 00599: FWD PAN AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8. (LP #2836314)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON CUSP WEB Y=313, Y=389, Y=636, AND X=-50 (APROX) AT PASSENGER CABIN. SUMMARY OF NRC 00515; CUSP WEB Y=313, Y=389, Y=636, AND X =-50 AT PASSENGER CABIN WERE REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2833071)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON DIAPHRAGM STA Y=217 AND X=-41 APROX AT PAX CABIN (W1). SUMMARY OF NRC 00428: CORROSION LEVEL 2. (WEB) DIAPHRAGM STA Y=217 AND X=-41 APROX AT PAX CABIN WAS FABRICATED PER DWG 9936535 AND INSTALL IS ACCOMPLISHED UNDER NRC 00413 AND B717-200 SRM 51-41-02-0G. (LP #2829562)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

DRILL HOLES, ADITTIONAL FOUND ON CUSP WEB AFTER REMOVAL ANGLE ON FLOOR STRUCTURE LH SIDE BTW STA 294 AND STA 313 PAX CABIN. SUMMARY OF NRC 00608: CUSP WEB LH SIDE BTW STA 294 AND STA 313 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PAR 4. (LP #2829937)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

TOOL MARKS ON CUSP WEB STA Y=255 AND LBL=46 APROX AT PAX CABIN (W1). SUMMARY OF NRC 00430: CUSP WEB STA Y=255 AND LBL=46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.219. (LP #2825205)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

PUNTURES (2 EA) ON WEB STA Y=211 APROX AND BTW STA X= 44/54 AT PAX CABIN (W1). SUMMARY OF NRC 00383: WEB STA Y=211 AND BTW STA X=44/54 WAS REPAIRED PER B-717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #2821676)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,296 hrs · 36,926 cycles

CORROSION ON FLOOR FITTING STA Y=217 AND RBL=11 AT PAX CABIN (W1). SUMMARY OF NRC 00396: CORROSION LEVEL 2. FLOOR FITTING WAS REPLACED PER B-717-200 SRM 51-41-05-0G. (LP #2818599)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK ON INSIDE JAMB STA Y=160 ON TOP OF PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00143: CRACKED INSIDE JAMB ON TOP OF PASSENGER ENTRANCE DOOR L1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2818186)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,296 hrs · 36,926 cycles

CRACK ON DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00140: DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #2809935)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,718 hrs · 35,693 cycles

EMERGENCY LIGHTS #L2-873, L2-845, L2-846, L2-848, AND L2-847 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 BATTERY PACK AND CHARGER PER AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #4621054)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,501 hrs · 35,534 cycles

THE AFT BULKHEAD DOOR EXIT MARKER SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-260 PER B717 AMM 33-50. THE AFT BULKHEAD DOOR EXIT SIGN NOW OPERATES NORMALLY. (LP #5359820)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,570 hrs · 33,494 cycles

THE LT AND RT VERTICAL STABILIZER EDGE STRUCTURE SPLICE BAND, HAD DEFORMED HOLES ON THE THIRD ROW OF FASTENERS. REAMED AND INSTALLED BUSHINGS IAW DRAWING SG95550001, REV B. INSTALLED AN EXTERNAL DOUBLER IAW DRAWING SG95550001, REV B.

Part: LONGERON — CRACKED (BS 1132) · airframe 48,570 hrs · 33,494 cycles

AFT ACCESSORY EMPENNAGE LONGERON 2L, BS 1132 WAS FOUND CRACKED ON THE AFT SIDE. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-05, REPAIR 2.

Part: LONGERON — CRACKED (BS 1132) · airframe 48,570 hrs · 33,494 cycles

AFT ACCY EMPENNAGE LONGERON 2R, BS 1132 FOUND CRACKED ON THE AFT SIDE. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-05, REPAIR 2.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 47,775 hrs · 32,935 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING FROM CEILING EXIT LIGHT AT ROW 1. MAINTENANCE LOCATED THE EMERGENCY EXIT COVER AND SECURED IAW AMM 33-51. OK FOR SERVICE.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 46,449 hrs · 32,038 cycles

EMERGENCY EXIT LIGHT COVER UNSECURE AT ROW 1. INSTALLED THE LIGHT COVER.

Part: SOCKET — SHORTED (EMERGENCY LIGHTS) · airframe 44,151 hrs · 30,359 cycles

MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR BOTH THE LEFT AND RIGHT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE FOUND THAT THE SOCKET FOR THE LIGHT ASSEMBLY WAS SHORTED AND REPLACED IT. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED FOLLOWING REPLACEMENT. (LP #8591026)

Part: CUSP WEB — CORRODED (BS 446) · airframe 43,629 hrs · 29,925 cycles

AT BS 446 RT CUSP WEB CORRODED ON BOTTOM SIDE. REMOVED CUSP WEB, RT WEB OUT OF LIMITS MATERIAL IS 100 PERCENT IN SEVERAL LOCATIONS, REMOVED CUSP TEE AT BS 446-484, CUSP TEE IS OUT OF LIMITS 100 PERCENT MATERIAL LOSS AT SEVERAL LOCATIONS, FABRICATED REPAIR PIECES IAW SRM 53-00-55, R1, FIG. 201, INSTALLED REPAIR PIECES AND NEW CUSP WEB, IAW SRM 53-00-55, R-1, FIG 201, SRM 57-40-02.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 43,629 hrs · 29,925 cycles

L1 DOOR SLIDE LOWER INFLATION CABLE PIN FOUND UNSECURED. INSTALLED PASSENGER ENTRY DOOR SLIDE.

Part: WEB — CORRODED (BS 190) · corrosion level 2 · airframe 44,665 hrs · 30,739 cycles

VERTICAL WEB AFT OF L1 DOOR FRAME IS CORRODED ABOVE FLOOR BS 190. COMPLIED WITH ERA 54677-14 REV ORIGINAL.

Part: CUSP WEB — CRACKED (BS 670) · airframe 43,629 hrs · 29,925 cycles

CUSP WEB CRACKED AT APPROXIMATELY BS 670 RT. R & R RT CUSP WEB AT BS 670 IAW DWG 9910151, REV CH.

Part: SKIN — CRACKED (BS 1022) · airframe 43,629 hrs · 29,925 cycles

BS 1022 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. REPAIRED THE SKIN IAW ERA NR 545671-14.

Part: INTERCOSTAL — CORRODED (BS 1028-1037) · airframe 43,629 hrs · 29,925 cycles

LOWER FUSELAGE, AFT CARGO BILGE, BETWEEN BS 1028-1037-L30, CORROSION. REMOVED INTERCOSTAL REINSTALLED INTERCOSTAL IAW SRM 51-40-2. REMOVED STR, FABRICATED NEW STR 717, SRM 52-20-05. INSTALLED STR IAW 717 SRM 51-40-2.

Part: STIFFENER — CRACKED · airframe 43,629 hrs · 29,925 cycles

AFT ACCY RT SIDE FRAMES 1178.225 & 1200 HAVE 2 EA SUPPORT STIFFENERS CRACKED. CAN BE SEEN INSIDE RT VENT BOX. R & R CRACKED STIFFENERS IAW SRM 51-41-02, SECTION 4.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 43,629 hrs · 29,924 cycles

BS 1022, BELOW LONGERON 14R FOUND SHEAR TIE CRACKED DURING INSPECTION WITH ORN 66647-200-0049. REPLACED SHEAR TIE IAW SRM 51-41-05, PARA 2.

Part: CUSP WEB — CRACKED (BS 813) · airframe 43,629 hrs · 29,924 cycles

CUSP WEB CRACKED AT BS 813. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4, FIG 216.

Part: SKIN — CRACKED (BS 1037) · airframe 43,629 hrs · 29,924 cycles

BS 1037, ABOVE LONGERON 14L EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.

Part: SKIN — CRACKED (BS 1037) · airframe 43,629 hrs · 29,924 cycles

STA 1037 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.

Part: FORMER — CRACKED (BS 674) · airframe 43,629 hrs · 29,924 cycles

LOWER FUSELAGE, LT FILLET, BS 674-L27L, CRACKED STR IN BOX. MARKED ON OUTSIDE. REPAIRED FORMER BS 674, L27L IAW ER/A 545672-14, REV 0. ASSOCIATED ER/A 54-567214 ADDED FOR AC 9516.

Part: STRUCTURE — CRACKED (BS 696) · airframe 43,629 hrs · 29,925 cycles

LOWER FUSELAGE, RT FILLET, BS 696 STRINGER 27R, CRACKED STRINGER END. REPAIRED DAMAGED FORMER AT BS 696-L27R IAW ERA 545672-14.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 43,629 hrs · 29,924 cycles

F/O'S AFT OTBD SEAT TRACK IS CORRODED IN SEVERAL PLACES. REPLACED F/O AFT SEAT TRACK IAW SRM 51-41-01, PARA 2 DUE TO PART BEING CORRODED OUT OF LIMITS.

Part: CUSP WEB — CORRODED (BS 446-927) · corrosion level 2 · airframe 43,629 hrs · 29,924 cycles

LEFT CUSP WEB CORRODED AT BS 446 - 927. BLENDED CORRODED AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-55, FIG 101.

Part: SKIN — CRACKED (BS 1095) · airframe 43,629 hrs · 29,924 cycles

SKIN CRACKED AT APPROXIMATELY FS 1095 AND APPROX 6" ABOVE RT PYLON-M. REPAIRED SKIN CRACK AT FS 1095 IAW ER/A 54669-14. SRM 51-40-05, PG 1 IDENTIFY REPAIRED IAW ER/A 54669-14. ASSOCIATED ER/A 54-566914 ADDED FOR AC 9516.

Part: CUSP WEB — CRACKED (BS 813) · airframe 43,629 hrs · 29,924 cycles

CUSP WEB CRACKED AT BS 813 RIGHT. REPAIRED CUSP WEB AT FS 813 BY REMOVING DAMAGE AND INSTALLING A DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.

Part: INTERCOSTAL — CRACKED (BS 636) · airframe 43,629 hrs · 29,924 cycles

INTERCOSTAL CRACKED IN FWD CARGO CEILING AT BL 0, BS 636. REPAIRED DAMAGED INTERCOSTAL AT BS 636, BL-0 IAW SRM 53-00-00, REPAIR 1.

Part: CUSP WEB — CORRODED (BS 370) · corrosion level 2 · airframe 43,629 hrs · 29,924 cycles

AT BS 370 RT CORRODED CUSP WEB. CORROSION CUT-OUT AND REPAIRED IAW SRM 53-00-55, REPAIR 4, FIG 216 & 223. CORROSION AT FASTENER HOLE REMOVED, BLEND OUT, & WITHIN ALLOWABLE LIMITS, REMOVED .001 ALLOWED REMOVING .002 IAW SRM 53-00-55. ALLOWABLE DAMAGE 1, PARA 4.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 43,629 hrs · 29,924 cycles

VERTICAL STABILIZER SKIN RT GOUGED UNDER PANEL 360AT. REPLACED NEW VERTICAL STABILIZER SKIN RT IAW DWG 5936143 AND 51-41-02, PARA 4 AND 51-41-05, PARA 2.

Part: SEAT TRACK — CORRODED (BS 995-1021) · airframe 43,629 hrs · 29,924 cycles

LOWER FUSELAGE, AFT CARGO, RT SEAT TRACK FOR BS 995-1021, FASTENER HOLES CORRODED. FABRICATED NEW AFT CARGO RT SEAT TRACK F/S 995-1021 IAW SRM 51-40-08, TABLE 1. NEW SEAT TRACK TO BE INSTALLED ON NR 66647-0100-077, PARTIAL 4.

Part: CUSP WEB — CORRODED (BS 585) · corrosion level 2 · airframe 43,629 hrs · 29,924 cycles

CUSB WEB AT BS 585 RT CORRODED. REPLACED LOWER CUSP TEE SPLICE CORRODED OUT OF LIMITS 50 PERCENT. REPLACED UPPER CUSP TEE SPLICE AND DAMAGED CUSP WEB AT BS 575 TO 595 IAW SRM 53-00-00, FIG 103, SRM 51-41-05, SRM 51-41-02.

Part: FLOOR SUPPORT — DAMAGED (BS 1022-1053) · airframe 43,629 hrs · 29,924 cycles

MULTIPLE DISCREPANCIES NOTED ON THE FORE TO AFT FLOORBEAMS BS 1022-1053. REPLACED FORE TO AFT FLOORBEAMS BS 1022-1053 RT AND LT BL 445 IAW SRM 51-41-05, PG 17, PARA 8, ER/A 545674-14. COMPLIED WITH ASSOCIATED ER/A 54-567414 ADDED FOR AC 9516.

Part: ATTACH ANGLE — CRACKED (BS 1022) · airframe 43,629 hrs · 29,924 cycles

PYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS, LONGERON 7R. REPAIRED ATTACH ANGLE AT 1022 L7R IAW SRM 51-70-11, REPAIR 1, FIG 201.

Part: ATTACH ANGLE — CRACKED (BS 1022) · airframe 43,629 hrs · 29,924 cycles

PYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS LONGERON 7L. REPAIRED ATTACH ANGLE AT 1022 L7L IAW SRM 51-70-11, REPAIR 1, FIG 201.

Part: BRACKET — CRACKED (INTERCOSTAL) · airframe 43,629 hrs · 29,924 cycles

INTERCOSTAL BRACKETS ARE CRACKED, VERIFIED WITH HFEC ON THE FWD SIDE OF FRAME AT BS 237. JUST OTBD OF LONGERON 28L ABD OTBD OF LONG .28R LOCATED UNDER CARGO TIE-DOWN TRACKS. REMOVED CRACKED INTERCOSTAL BRACKETS AT BS 237, STR 28R AND 28L. FABRICATED ANGLES 9815554-7 & 11. HEAT TREATED ANGLES TO T6 CONDITION. TREATED, PRIMED, PAINTED, INSTALLED, AND APPLIED CIC TO ANGLES 9815554-7 AND 11 IAW DWG 9915554, REV U AND DPS 900-4-1, NR 1.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 42,730 hrs · 29,260 cycles

DURING THE TURN-AROUND CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE AFT OVERWING HATCHES ON BOTH SIDES WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,275 hrs · 28,957 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE MID-CABIN EMERGENCY LIGHTING WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 696) · airframe 40,779 hrs · 27,745 cycles

DURING AD MANDATED INSPECTION, FOUND LT OVERWING FRAME AT STATION 696 CRACKED BELOW L18. REPLACED IAW DWG SR95530013, REV A, SRM 51-40-2 AND 51-40-05.

Part: FLOORBEAM — MECHANIC ERROR (BS 737) · airframe 40,779 hrs · 27,745 cycles

DURING SCHEDULED INSPECTION/REPAIR FLOOR STRUCTURE AND OVERWING FRAME INSPECTION, MIS-DRILLED HOLE AT FLOORBEAM STA 737, LBL 54, IN MAIN CABIN. REPLACED FLOORBEAM IAW SRM 51-41-05, DWG 9919645, REV D.

Part: SUPPORT — CRACKED · airframe 40,774 hrs · 27,741 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN STA 737, RBL 44, VERTICAL SUPPORT CRACKED. REPLACED VERTICAL SUPPORT FROM PN 3925812U2 AT STA 737, RBL 44 IAW SRM 51-40-08, 51-10-04, 51-41-05 AND 51-41-02.

Part: FLOOR SUPPORT — CRACKED · airframe 40,774 hrs · 27,741 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN STA 737, RBL 56 FLOOR SUPPORT CRACKED. REPLACED FLOORBEAM SUPPORT, PN 9915527-506 IAW SRM 51-41-08, 51-41-05, 51-10-05, 51-10-04 AND DWG 5930561, REV AC.

Part: SUPPORT — CRACKED · airframe 40,774 hrs · 27,741 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN STA 737, LBL 44, VERTICAL SUPPORT CRACKED. REPLACED VERTICAL SUPPORT FROM PN 392581ZU1 AT STA 737, LBL 44 IAW SRM 51-40-08, 51-10-04, 51-41-05 AND 51-41-02.

Part: ANGLE — CRACKED (BS 715) · airframe 40,774 hrs · 27,741 cycles

DURING SPECIAL VISIT, FOUND MAIN CABIN STA 715, RBL 44, TEE ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-40-05 AND DWG 9923417, REV B.

Part: O-RING — LEAKING (ACCUMULATOR) · airframe 39,782 hrs · 26,972 cycles

ON APPROACH, LOST RT HYD SYS. PERFORMED ALT EXTEND AND DOORS WERE EXTENDED ON TOUCHDOWN. REPLACED O-RING ON RT THRUST REVERSER ACCUMULATOR. REPLACED NR 2 EDP AND SYS FILTERS. SERVICED RT HYD SYS AND CYCLED THE REVERSER SEVERAL TIMES WITH NO FURTHER LEAKAGE NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,997 hrs · 26,309 cycles

LOWER EMER LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 38,997 hrs · 26,309 cycles

LEFT FWD EMER EXIT DOOR SIGN BULB INOPERATIVE. RELAMPED SIGN ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 39,193 hrs · 26,445 cycles

COCKPIT EMER EXIT LIGHT OVERHEAD INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,491 hrs · 25,986 cycles

RIGHT FWD OVERWING EMER EXIT LIGHT CHARGER INOPERATIVE. R & R CHARGER IAW AMM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 38,491 hrs · 25,986 cycles

UPPER FUSELAGE TO VERTICAL STABILIZER LE RT & LT ACCESS PANEL MOUNT ANGLES CRACKED AT STATION 1126. R & R ANGLES IAW SRM & DWG.

Part: SPLICE — CRACKED (VERTICAL STAB) · airframe 38,491 hrs · 25,986 cycles

UPPER FUSELAGE AT VERTICAL STABILIZER LE AFT MOUNTING SPLICE CRACKED AT TRANSITION FAIRING ACCESS PANEL STATION 1126. R & R SPLICE IAW & DWG.

Part: SUPPORT BEAM — CRACKED (NLG WW) · airframe 38,491 hrs · 25,986 cycles

LEFT SIDE NOSE WW CLOSE OUT FRAME SUPPORT BEAM CRACKED AT STATION 40 UPPER FASTENER IN WEB. REPAIRED BEAM IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 38,491 hrs · 25,986 cycles

AFT LT LAVATORY EMER EXIT LIGHT CRACKED. R & R LIGHT IAW AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL MC 221KF DAMAGED. R & R PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 219, RBL 44. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 214, RBL 57. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 38,491 hrs · 25,986 cycles

LEFT WING FIXED TE INBD BUTTE DOOR CTR SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT — CRACKED (LT WING) · airframe 38,491 hrs · 25,986 cycles

LEFT WING NR 4 HINGE UPPER PANEL SUPPORT FOR AILERON CRACKED. R & R SUPPORT IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 38,491 hrs · 25,986 cycles

LEFT WING FLAP CTR HINGE AFT FAIRING CRACKED. REPAIRED FAIRING IAW SRM.

Part: ANGLE — CRACKED (FLAP CARRIAGE) · airframe 38,491 hrs · 25,986 cycles

RIGHT WW INBD SIDE OF INBD FLAP TRACK CARRIAGE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

R1 DOOR CUT OUT WET AREA FLOOR SUPPORT CORRODED BETWEEN BS 160 TO BS 200. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN ENTRY WET AREA FLOOR SUPPORT CORRODED AT BS 1160, BETWEEN RBL 46 TO RBL 55. R & R SUPPORT IAW DWG & SRM.

Part: SUPPORT FITTING — CORRODED (R1 DOOR) · airframe 38,491 hrs · 25,986 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FWD & AFT SUPPORT FITTINGS CORRODED. R & R FITTINGS IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR SUPPORT Z ANGLE CORRODED BETWEEN BS 200 TO BS 214, RBL 57. REPAIRED Z ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN ENTRY WET AREA FLOOR SUPPORT CORRODED BETWEEN BS 162 TO BS 198, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 TO BS 237, RBL 44. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

SEAT TRACK CORRODED BETWEEN BS 200 TO BS 266, RBL 22. R & R SEAT TRACK IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

AFT ACCESSORY COMPARTMENT AT CANT FRAME 1200 LT SIDE LOUVER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN ENTRY WET AREA FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO RBL 46. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 148 TO BS 200, RBL 7. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 222AHF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 222AVF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 221CF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 222ATF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 221EF DAMAGED. R & R PANEL IAW AMM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 222LF DAMAGED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR SUPPORT PANEL 221WF DAMAGED. REPAIRED PANEL IAW SRM & AMM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FLOOR PANEL 222APF DAMAGED. REPAIRED PANEL IAW SRM.

Part: MOUNT — CORRODED (CABIN) · airframe 38,491 hrs · 25,986 cycles

LEFT EMER ESCAPE LINE MOUNTING HARDWARE CORRODED. R & R MOUNTING ASSEMBLY IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 655, LBL 56. REPAIRED CUSP WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,491 hrs · 25,986 cycles

FRAME CORRODED AT BS 974. REPAIRED FRAME IAW SRM.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 39,061 hrs · 26,352 cycles

AIR TURN BACK, ON DEPARTURE LT ENG COMPRESSOR STALL 2 TIMES WITHIN 3 MINUTES BETWEEN COMPRESSOR STALLS. R & R NR 1 ENG IAW TASK CARD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,598 hrs · 23,513 cycles

RIGHT EEPLS CHARGER ASSY INOP AT ROW 24. REMOVED AND REPLACED CHARGER IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,371 hrs · 24,013 cycles

FRAME CORRODDED AT BS 974. REPAIRED FRAME PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP WEB CORRODED BETWEEN BS 503 TO BS 522, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP WEB CORRODED BETWEEN BS 465 TO BS 484, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP WEB CRACKED AT BS 660, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP WEB CORRODED AT BS 527, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP WEB CORRODED BETWEEN BS 541 TO BS 559, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

CUSP CORRODED AT BS 912, RBL 58. REPAIRED CUSP IAW SRM.

Part: LATCH — INOPERATIVE (R1 DOOR) · airframe 34,598 hrs · 23,513 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH ASSY INOP. REMOVED AND REPLACED LATCH ASSY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

LEFT SIDE AFT NLG STRUT DOOR AFT HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

RIGHT SIDE AFT NLG STRUT DOOR AFT HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

STRINGER CORRODED BETWEEN BS 927 TO BS 1012, STR 30L. REMOVED AND REPLACED STRINGER SECTION IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

FORWARD CARGO DOOR CUTOUT LOWER JAMB PAN CORRODED. REMOVED AND REPLACED PAN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

SHEAR TIE CORRODED AT BS 954, BETWEEN STR 30R TO STR 29R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 30L TO STR 29L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

FRAME CORRODED AT BS 908, BETWEEN STR 29R TO STR 29L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,598 hrs · 23,513 cycles

FRAME CORRODED AT BS 974, STR 30L. REMOVED AND REPLACED FRAME IAW SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 23,024 hrs · 23,146 cycles

R1 DOOR EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED BAR CLIP PER MM.

Part: SPRING — BROKEN (MLG DOOR LATCH)

AFTER TAKEOFF, ON GEAR REACTION RT MAIN GEAR INDICATED UNSAFE (RED) FOLLOWED ABNORMAL NON-ALERT P-15. SLOWED TO 210 KIAS. CYCLED GEAR, ALL GEAR INDICATED GREEN WHEN DOWN AND GEAR LIGHTS WENT DARK (SAFE). ON SECOND GEAR RETRACTION, DURING APPROACH ALL GEAR LIGHTS WERE GREEN. FOUND DOOR LATCH SPRING BROKEN. REPLACED SPRING AND ADJUSTED RT MLG LATCH, REF AMM 32-34-01. CHECKED DOOR PROXIMITY AND GEAR UPLATCHED PROXIMITY INDICATIONS, NORMAL PER REF AMM 32-61-00.

Part: UNKNOWN — UNKNOWN (CABIN)

SMOKE / MIST OR DUST CLOUD IN CABIN NOTICED WHILE DEPLANING. UPON ARRIVAL TO A/C AND INITIAL EVALUATION NO UNUSUAL SMELLS WERE NOTED, NO POPPED CB'S NOTED. INSPECTED CABIN, GALLEYS, LAVS, FLIGHT DECK, EE BAY, CARGO BINS, TAIL COMPARTMENT. OPERATED ENGINES WITH CREW OPERATED BOTH PACKS WITH GASPER FAN. OPERATED ALL CABIN LIGHTS. MOCS REVIEWED TRAX AND SHOWED NO HISTORY FOR LAST 30 DAYS NO EVIDENCE OF UNUSUAL SMELLS OR SMOKE WAS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: BATTERY — LOW (MAIN)

ARRIVED AT AIRCRAFT TO FIND IRU HORN BLOWING, BATT SW ON, EMER PWR OFF AND EMER EXIT LIGHTS ILLUMINATED NO IDEAA HOW LONG AIRCRAFT WAS IN THIS CONDITION. REMOVED AND REPLACED MAIN A/C BATTERIES, FUNCTIONAL CHECK GOOD REF AMM 24-24.

Part: LANYARD — DETACHED (EVAC SLIDE)

FWD SERVICE DOOR ESCAPE SLIDE LANYARD UNATTACHED. (AWI) RE-INSTALLED R-1 GIRT BAR LANYARD IAW AMM 25-61. (AWI)

Part: LENS — MISSING (CABIN)

ROW 10D MISSING 2 EA EMERGENCY LIGHT LENS. REPLACED 2 EA EMEGENCY LIGHT LENS.

Part: TIE CLIP — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT BULKHEAD SHEAR TIE CLIP, STA 1152, LONG L2R, CRACKED. ACCOMPLISHED SHEAR TIE CLIP REPLACEMENT PER B717 SRM 51-41-05 AND EA 17-53-02803IR.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FRAME — DAMAGED (FUSELAGE)

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 AIRTRAN TASK CARD 17-5310-2985.

Part: FRAME — DAMAGED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2979.

Part: STRUCTURE — CRACKED (PYLON)

RIGHT PYLON APRON LOWER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129 AND EA 17-54-02846IR.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 238, RBL 44, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: SKIN — GOUGED (RT MLG DOOR)

RIGHT MLG DOOR 6 INCHES UP FROM LOWER EDGE SKIN, GOUGED. ACCOMPLISHED SKIN COMPOSITE REPAIR PER B717 SRM 51-70-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL35 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, LBL 15 TO RBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LONGERON — CRACKED (FUSELAGE)

LEFT LONGERON FINGER WEB, STA 210, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

GIRT BAR LANYARD DISCONNECTED FROM L1 SLIDE PACK DOOR. REMOVED AND REPLACED SLIDE PACK ASSEMBLY.

Part: WIRE — PULLED (CABIN)

OVERHEAD EMERGENCY LIGHT AT ROW 21 HAS WIRE PULLED OUT OF CONNECTOR. REPLACED CONNECTOR AT SEAT ROW 21 PER SWPM 20-31. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT ROWS 1, 2 AND 3 INOP. REMOVED AND REPLACED ROW NR 3 BATTERY PACK ASSY IN REF TO B717 MM 33-51. OPS CHECK GOOD AT THIS TIME.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO COMP LOWER PAN CORRODED BEYOND LIMITS. REPAIR FWD CARGO COMP LOWER SECTION OF JAMB PAN IAW B717 53-20-15 REP 6.

Part: SKIN — DENTED (FUSELAGE)

DENT IN FUSELAGE BS 214L LONGERON 17. INSTALLED INTERNAL DOUBLER PER 717 SRM 51-10-02 AND 53-00-01.

Part: COFFEEMAKER — DEFECTIVE (NR 3)

BOTH CABIN AND FLIGHT CREW SMELLED VERY STRONG ODOR THAT MIGHT HAVE BEEN SMOKE, WITHIN 15 SEC OF NOTICING THE SMELL IT HAD DISSIPATED. CREW STATED, SAW EMERGENCY LIGHTS FLASH AND HEARD A POP OR CLICK BY L1 DOOR WHEN ODOR WAS SMELLED. REMOVED AND REPLACED GALLEY CONTROL RELAY AS PRECAUTION IAW B717 WDM 25-31. INSPECTED WIRES AND COMPONENTS BEHIND F/A SEAT IN GALLEY, REMOVED AND REPLACED COFFEEMAKER NR 3 OPS CHECK NORMAL NO C/B POPPED. PERFORMED ENG RUNS AND LOAD CHECK OF ELECTRICAL SYSTEM. ALL SYSTEMS CHECK GOOD. NO DEFECTS FOUND A/C OK FOR CONTINUED SERVICE. OPS CHECK OF EMERGENCY LIGHTS NORMAL.

Part: PSEU — MALFUNCTIONED (E&E BAY)

ON APPROACH WITH GEAR LOWERED GEAR UNSAFE WITH THREE RED LIGHTS WITH GEAR HANDLE DOWN CHECKLIST GEAR SHOWED SAFE LANDED STRAIGHT AHEAD. JACKED A/C REF B717 AMM 07-11, PERFORMED ADJUSTMENT TEST OF LANDING GEAR INDICATION PER 717 AMM 32-00, NO FAULTS OR DISCREPANCIES NOTED REMOVED AND REPLACED PSEU AS PRECAUTIONARY REF AMM 32-61, DOWNJACKED A/C RTS PASSED.

Part: DOOR FRAME — DAMAGED (FUSELAGE)

FWD CARGO DOOR JAMB DAMAGE. INSTALLED DOUBLER REPAIR ON FWD CARGO DOOR PAN AFT CORNER IAW BEACOM CQTCRL-03-00134H DATED MARCH 18, 2003 AND RES 03-0265. MATERIAL USED 2024-0 .063. HEAT TREATED TO 2024-T3, 5.5" X 5.5".