N920AT

Part: RELEASE MECH — OUT OF ADJUST (ZONE 100) · airframe 53,871 hrs · 38,431 cycles

FOUND TAIL CONE RELEASE MECHANISM CAM CLOCKED WRONG. TAILCONE RELEASE MECHANISM CAM REF B717 AMM 53-52-03 (1362721)

Part: NONE — NONE · airframe 53,871 hrs · 38,431 cycles

ERA 631006-14. : DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA ADVISORY CIRCULAR 120-93. ASSOCIATED ER/A 00-631006 (1359454)

Part: SKIN — DAMAGED (ZONE 600) · airframe 53,844 hrs · 38,413 cycles

FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN STA 164. REPAIRED PER ERA 629782-14AD (1346873)

Part: SPAR — DAMAGED (ZONE 600) · airframe 53,844 hrs · 38,413 cycles

ER/A 629782-14AD REV ORIGINAL. REPAIR TO RH WING REAR SPAR AT XRS 164. REPAIRED PER ER/A 14-629782. (1345195)

Part: SPAR — DAMAGED (ZONE 600) · airframe 53,844 hrs · 38,413 cycles

ER/A 629782-14. REPAIR AT RH REAR SPAR AT XRS 164. C/W WITH ER/A 629782-14. (1345202)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,844 hrs · 38,413 cycles

AFT CARGO CORROSION - INTERNAL DOUBLER STR 23R STA 1022 CORRODED. REPAIRED COMPLIED WITH ER/A 630153-14 REV. ORIG. (1335432)

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 53,844 hrs · 38,413 cycles

AFT CARGO SCUFF PLATE CRACKED. REPLACED JAMB PAN ON NR 408 IAW LOG 1325090. (1327367)

Part: NONE — NONE (NONE) · airframe 53,844 hrs · 38,413 cycles

REPETITIVE INSP PER SECT II. OF ERA 630153-14 REV ORIGINAL. C/W ER/A630153-14 REV ORIGINAL. (1324948)

Part: PAN — CORRODED (ZONE 100) · airframe 53,844 hrs · 38,413 cycles

AFT CARGO: C-2 DOOR THRESHOLD PAN CORRODED. REPLACED REPAIR AFT CARGO DOOR LOWER JAMB PAN IAW SRM 53-20-15-2R, PROCEDURE 7, REPAIR 7. AFT CARGO DOOR LOWER JAMB PAN CORROSION SPLICE REPAIR. (1325090)

Part: STRINGER FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,844 hrs · 38,413 cycles

AFT CARGO P/R: STRINGER END FITTING MARKED FS1053 28R IS CORRODED. REPLACED AFT END FITTING LONGERON 28R PER B717 DWG 5910228 (1310506)

Part: LONGERON SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,844 hrs · 38,413 cycles

AFT CARGO BAY BS 1002 L25R END SPLICE CORRODED. REPLACED LONGERON 25R AND FWD END FITTING REF: DACDWG 5919707-521 (1310504)

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,844 hrs · 38,413 cycles

C1 DOOR THRESHOLD: LIGHT SURFACE CORROSION IN DOOR SILL AREA. REPLACED REPAIRED FORWARD CARGO DOOR LOWER JAMB PAN REF: B717-200 SRM 53-20-15-2R (1300666).

Part: ACCESS PANEL — MECHANIC ERROR (ZONE 500) · airframe 53,666 hrs · 38,247 cycles

LEFT WING OUTER, LOWER SURFACE, ACCESS COVER SETTLEMENT AREA, XRS=383-414, MISDRILLED HOLE. ACCOMPLISH ER/A 611899-14 (1178468)

Part: LENS — MISSING (ZONE 200) · airframe 52,709 hrs · 37,348 cycles

THE OVERHEAD EMERGENCY LIGHT LENS AT 24L IS MISSING. MAINTENANCE REPLACED LENS IAW B717 AMM 33-51-08. (LP #6963274)

Part: AUTOPILOT SYS — FAILED · airframe 52,391 hrs · 37,039 cycles

SHIP 9578 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO JAX (VFR) DUE TO LOSS OF AUTOPILOT AND LATERAL ROLL MODE GUIDANCE ON APPROACH FOR LANDING AT ATL (IMC). CORRECTIVE ACTION: MAINTENANCE REPLACED THE GLARE SHIELD CONTROL PANEL AND THE #2 FCC. ALL RTS TESTS PASSED. (LP #6922360)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,570 hrs · 34,594 cycles

ON WALK AROUND DURING THE SERVICE CHECK, MAINTENANCE FOUND THAT THE AFT RIGHT HAND EXTERIOR EMERGENCY LIGHT STAYS ON AT ALL TIMES. MAINTENANCE REPLACED RELAY R2-273 PER B717 SWPM CHAPTER 20-25 AND REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PACK AND CHARGER (B5-125) PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OKAY FOR SERVICE. (LP #6886188)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

DENTS ON INB SURFACE AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00098: INBOARD SURFACE OF AFT MOVABLE FLAP VANE (LH WING) WAS REPAIRED PER ER/A 612278-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612278 ADDED FOR AC 9578. (LP #0021458)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON INTERCOSTAL BTW STA 1022-1037 AND LONGERON 30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00708: CORROSION LEVEL 2. INTERCOSTAL BTW STA 1022-1037 AND LONGERON 30, AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0016675)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

IN REF AMDS: 2040-0009: OPEN LEFT WING, FUEL TANK ZONE 520, DURING REMOVED ACCESS PLATE NBR 520 MB; CUT OUT SKIN OF FUEL ACCESS PLATE 520MB WAS DRILLED AT LH WING. SUMMARY OF NRC 00104: CUT OUT SKIN OF FUEL ACCESS PLATE 520MB WAS REPAIRED PER SECTION I: TIME LIMITED REPAIR OF ER/A NO. 611899-14 REV. ORIGINAL AND PRI 611899-14 REV 1. TIME OF ACCOMPLISHMENT SEC DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON CHORD ANGLE AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 27LH-27RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00230: CORROSION LEVEL 2. CHORD ANGLE AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0012455)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON PAN OF PASSENGER DOOR JAMB (EXTERNAL/INTERNAL SURFACE) BTW STA Y=200 AND PROJECT LONG 18L AT PAX CABIN. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PAN OF PASSENGER DOOR JAMB (EXTERNAL/INTERNAL SURFACE) BTW STA Y=200 AND PROJECT LONG 18L AT PAX CABIN WAS REPAIRED PER PRI 612312-14 REV 1 AND ER/A 612664-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612664 ADDED FOR AC 9578. (LP #0012693)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON L30 BTW STA 908 TO STA 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00578: CORROSION LEVEL 2. LONGERON SECTION OF L30 BTW STA 908 TO STA 950 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0009610)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ALONG OF TIE TRACK STA 954 TO 1022 LONGERON 28LH AT AFT CARGO IN REF NRC 213. SUMMARY OF NRC 00625: CORROSION LEVEL 2. TIE TRACK STA 954 TO 1022 LONGERON 28LH AT AFT CARGO WAS REPLACED PER DWG 5936663 REV Y AND PER B717-200 SRM 51-41-01-0G. (LP #0007688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON INTERCOSTAL STA 1223 CANT 12 O'CLOCK POSITION AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00251: RUDDER STOP SPRING RH (1 EA) WAS REMOVED AND INSTALLED PER B717-200 AMM 27-26-03 AND ANGLE BRACKET AND INTERCOSTAL WERE REPLACED PER B717 SRM 51-41-02-0G. (LP #0006477)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR (L1). SUMMARY OF NRC 00296: BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0002773)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON SEAT TRACK X 56 ON STA: Y=332 TO Y=333 ORIGINAL T. SUMMARY OF NRC 00428: CORROSION LEVEL 2. SEAT TRACK X=56R BTW STA Y=218 AND STA Y=334 WAS REPLACED PER DWG 5930547 AND PER B-717 SRM 51-41-01-0G. (LP #0003244)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON FWD REPAIR DOUBLER SPLICE ON AFT CARGO DOOR JAMB. CORROSION LEVEL 2. REPAIR DOUBLER SPLICES (2 EA) WERE REPLACED PER SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0001412)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON LONGERON END 24RH AND STA 1011 AT AFT CARGO. SUMMARY OF NRC 00650: CORROSION LEVEL 2. LONGERON END 24RH AND STA 1011 AT AFT CARGO WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2998688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN. SUMMARY OF NRC 00441: FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #2999578)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ANGLE INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00156: ANGLE (INTERCOSTAL) INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT PASSENGER DOOR (L1) WAS FABRICATED AND REPLACED PER B717-200 SRM 51-40-02-0G AND DWG 9955763 REV K. (LP #2998235)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON LONGERON END (1 EA) STA Y:1053 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00652: CORROSION LEVEL 2. LONGERON END AT STA Y:1053 LONGERON 27RH WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2996387)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACKS (2 EA) ON FWD AND AFT PANS UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00151: FWD PAN UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. NO CRACKS WERE FOUND AT AFT PAN PER B717 DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #2996862)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN. SUMMARY OF NRC 00442: FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4, REPAIR 4. (LP #2994735)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

BROKEN INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL=0 AT AFT CARGO. SUMMARY OF NRC 00214: INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL= 0 AT AFT CARGO WAS REPAIRED B717-200 SRM 51-70-11-2R-1 REPAIR 1. (LP #2991792)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00231: CORROSION LEVEL 2. INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 53-20-08-01, 51-41-02-0G PAR 4, AND 51-41- 05-0G PAR 8. (LP #2991938)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON BEAM 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00152: BEAM NBR 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2990273)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON FLOOR SUPPORT Y=180 FROM X=-10 TO X=-43, FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX IN REF NRC 00541. SUMMARY OF NRC 00610: CORROSION LEVEL 2. FLOOR SUPPORTS Y=180 FROM X=-10 TO X=-43 AND FLOOR SUPPORT FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX WERE FABRICATED AND REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2987467)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN IN REF NRC 00538. SUMMARY OF NRC 00614: CORROSION LEVEL 2. CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 PAR 4 FIG 201 SHEET 1. (LP #2988783)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX. SUMMARY OF NRC 00324: CORROSION LEVEL 2. FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2984541)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON FRAME STA Y=275 BTW STRG 15L/14L AT CPAX. SUMMARY OF NRC 00286: FRAME STA Y=275 BTW STRG 15L/14L AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 1. (LP #2984454)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT CPAX. SUMMARY OF NRC 00437: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT CPAX WERE REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-05-0G PAR 8. (LP #2979640)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON WEB ON STA Y=579 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00389: WEB ON STA Y=579 AND X=-44 AT PAX CABIN WAS REPAIRED PER B 717-200 SRM 53-00-55-2R REPAIR 4. (LP #2979222)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,516 hrs · 34,548 cycles

CRACK ON WEB STA Y 190, LBL44 AT CPAX. SUMMARY OF NRC 00436: WEB STA Y 190, LBL44 WAS REPAIRED PER B 717-200 SRM 51-70-10-2R REP 1 FIG 201. (LP #2976349)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

REWORKED CORRODED AREA RH CUSP WEB BTW STA Y=465 AND STA=484. ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS OF 0.014 IN. REWORKED AREA IS OUT LIMITS. SUMMARY OF NRC 00569: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=465 AND STA=484 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIG 215. (LP #2974299)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION ON SHIELD X=56R AND X=44.5R BTW STA Y=1022 TO Y=1053 AND WEB X=56R STA Y=1042 AT PAX CABIN. SUMMARY OF NRC 00233: CORROSION LEVEL 2. SUPPORT X=56R AND X=44.5R BTW STA Y=1022 TO Y=1053 WAS FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM 51-41-05-0G AND DAMAGE IN ZONE WEB X=56R STA Y=1042 AT PAX CABIN WILL BE ATTEND WITH NRC 604. (LP #2971444)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,516 hrs · 34,548 cycles

CORROSION IN LIGHTENING HOLE AREA ON RH CUSP WEB BTW STA Y=434 TO STA=446. REWORKED AREA IS OUT OF LIMITS. SUMMARY OF NRC 00570: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=434 TO STA=446 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REP 4. (LP #2968541)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,377 hrs · 33,675 cycles

THE OVERHEAD EMERGENCY LIGHT LENS COVER WAS FOUND MISSING DURING THE SERVICE CHECK. MAINTENANCE REPLACED THE LENS COVER. THE SYSTEM IS NOW OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,360 hrs · 33,664 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 102. MAINTENANCE REPLACED THE AFT LIGHT LENS. (LP #1295863)

Part: STRAKE — DAMAGED (LT WING) · airframe 45,134 hrs · 31,432 cycles

COMPOSITE DAMAGED/MISSING. LT WING STRAKE. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0275:0593-2011/009 00096 C/W TASK CARD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,614 hrs · 29,736 cycles

LOWER LT & RT AFT OVERWING EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,416 hrs · 29,586 cycles

AFT EMERGENCY EXIT DOOR OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS OK IAW AMM 33-51.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,263 hrs · 29,458 cycles

EMERGENCY EXIT SIGNS AT THE AFT OVER WING EXITS INOPERATIVE. REPLACED BATTERY CHARGER PB5-230. CHECKS GOOD REF AMM 33-51.

Part: SPOILER — DELAMINATED (RT WING)

DURING UNSCHEDULED MAINTENANCE CHECK RT OTBD SPOILER, FOUND DELAMINATED.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING NON ROUTINE CHECK, LT OTBD SPOILER FOUND DELAMINATED.

Part: SEAT TRACK — WORN (COCKPIT) · corrosion level 2 · airframe 40,861 hrs · 28,446 cycles

CAPTAIN`S AND FIRST OFFICER'S SEAT TRACKS ARE WORN ON EDGES AND LOWER SURFACE OF T FLANGE. REMOVED WORN AREA FROM CAPTAIN`S SEAT TRACK AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00. FOUND FO SEAT TRACK TO BE CORRODED BEYOND LIMITS AND REPLACED IAW SRM 51-41-01 PG 2 AND PG 17.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

SERVICE DOOR CUTOUT CUSP ANGLE IS CORRODED. REPLACED CUSP ANGLE AT SERVICE DOOR CUTOUT IAW SRM 53-00-55, REPAIR 3. FABRICATED REPAIR DOUBLER.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

CUSP MEMBRANE CORRODED AT STA 160-STA 200 AND CRACKED AT STA 133-STA 138 ON RT SIDE. REPAIRED CORRODED CUSP MEMBRANE AT STA 160-STA 200 AND DOUBLER. REPAIRED CRACKED CUSP MEMBRANE AT STA 133-STA 138 IAW ER/A 547484-14 ALSO PRI REV 2, 547484. ASSOCIATED ER/A 00-547484 ADDED FOR AC 9578.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,049 hrs · 27,797 cycles

LEFT FUSELAGE SKIN CRACKED APPROXIMATELY .125" AROUND FASTENER HEAD AT STA 1095 JUST ABOVE LONGERON 14L. VERIFIED BY EDDY CURRENT. REPAIR 4H FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,049 hrs · 27,797 cycles

RIGHT FUSELAGE SKIN CRACKED AT FASTENER HEAD AND BETWEEN 2 FASTENERS, STA 1095 JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

FRAME CORRODED STA 832 AT LONGERON 30. FRAME AT STA 832, L30, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS IAW SRM 53-20-07, REPAIR 3. HEAT TREAT REPAIR PARTS 7075-T6 IAW CWO 68433-0018. INSTALLED REPAIR IAW SRM 53-20-07, REPAIR 3, FIG 201.

Part: FRAME — CORRODED (BS 870) · corrosion level 2 · airframe 40,861 hrs · 28,446 cycles

FRAME CORRODED BS 870 AT LONGERON 30. BLENDED IAW SRM 53-00-00 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-07 REPAIR 3.

Part: SUPPORT FITTING — CHAFED (WING) · airframe 40,049 hrs · 27,797 cycles

SUPPORT FITTING FOR PANEL 630HB IS HEAVILY CHAFED IN 2 PLACES, MARKED. PART REMOVED ON JIB CARD 2040-0049. PART FOUND TO BE OUT OF LIMITS IAW SRM 57-00-00, FIG 103. MATCH DRILLED NEW PART IAW SRM 51-40-08 AND INSTALLED NUTPLATES IAW SRM 51-40-02, PAR 4. PART WILL BE RE-INSTALLED ON JOB CARD 2040-0050.

Part: REPAIR — CRACKED (NR 2 PYLON) · airframe 40,049 hrs · 27,797 cycles

NR 2 PYLON REPAIR CRACKED AND CHERRY LOCK BACKED OUT AT FORWARD LATCH, MARKED. REMOVED FWD LATCH ASSY FROM NR 2 PYLON APRON FOR FOM AND REMOVED CRACKED REPAIR. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER. RE-INSTALLED LATCH ASSY IAW SRM 51-41-05, PAR 6, SRM 54-50-02, REPAIR 1, FIG 202.

Part: PAN — CRACKED (LT BLG DOOR) · airframe 40,049 hrs · 27,797 cycles

LEFT MLG BODY DOOR CRACKED ON FWD SIDE APPROXIMATELY MIDWAY DOWN, MARKED. REMOVED AND REINSTALLED MLG DOOR IAW 32-14-00, INSTALLED NEW DOOR PAN IAW ERA 545687-14 AND DWG 5910782. ASSOCIATED ER/A 00-545687, ADDED FOR AC 9578.

Part: PAN — CRACKED (RT BLG DOOR) · airframe 40,049 hrs · 27,797 cycles

RIGHT MLG BODY DOOR CRACKED AT FORWARD DOOR PAN, MARKED. REMOVED AND REINSTALLED MLG DOOR IAW 32-14-01, INSTALLED NEW DOOR PAN IAW ER/A 545687-14 AND DWG NR 5910782. ASSOCIATED ER/A 54-568814, ADDED FOR AC 9578.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

FWD CARGO DOOR JAMB IS CORRODED IN SEVERAL PLACES, MARKED. REPLACED DOOR JAMB IAW SRM 51-41-02 AND 51-41-05 AND 51-41-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

UNDER FLOOR SUPPORT, CUSP WEB 219-237, RBL 44-RBL HAS CORROSION. REPLACED CUSP WEB AT FS 218 TO 237, RBL 44 TO 56 IAW SRM 51-41-02, 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,049 hrs · 27,797 cycles

RIGHT CUSP MEMBRANE IS CRACKED AT STA 384. REPAIRED RT CUSP MEMBRANE AT STA 384 IAW SRM 53-00-55, REPAIR 4, FIG 224.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,049 hrs · 27,797 cycles

RIGHT CUSP MEMBRANE CRACKED AT STA 943. REMOVED CRACK DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,049 hrs · 27,797 cycles

CORROSION ON RT CUSP WEB AT STA 655 TO 674 IS OUT OF LIMITS. INSTALLED REPAIR DOUBLER ON RT CUSP WEB AT STA 655-674 IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,049 hrs · 27,797 cycles

RIGHT CUSP MEMBRANE CRACKED AT BS 435. REPAIRED CRACKED MEMBRANE AT BS 434 RT IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CORRODED (BS 943) · airframe 40,049 hrs · 27,797 cycles

RT CUSP MEMBRANE AT BS 943 HAS CORROSION. REMOVED CRACK DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.

Part: BRACKET — CRACKED (LT WING) · airframe 40,049 hrs · 27,797 cycles

LEFT WING, L/E, STATION 164, CRACKED. REMOVED DAMAGED BRACKET, FABRICATED NEW BRACKET. TREAT AND PRIME BRACKET IAW SRM 51-22-01. INSTALLED FABRICATED BRACKET IAW SRM 51-40-02 AND 51-41-05 PARA 10,

Part: CUSP WEB — CRACKED (BS 675) · airframe 40,049 hrs · 27,797 cycles

RT CUSP MEMBRANE CRACKED AT BS 675. REPAIRED CRACKED CUSP MEMBRANE IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CRACKED (BS 218) · airframe 40,049 hrs · 27,797 cycles

LEFT CUSP WEB CRACKED AT BS 218. INSTALLED REPAIR DOUBLER ON LT CUSP WEB IAW SRM 53-00-55, REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,147 hrs · 23,963 cycles

RIGHT MLG WW CUT OUT FWD FRAME CRACKED UPPER INBD CORNER ABOVE SWITCH. REPAIRED FRAME IAW SRM.

Part: WIRE — LOOSE (CABIN) · airframe 35,147 hrs · 23,963 cycles

OVERHEAD EMER LIGHT WIRING LOOSE. SECURED WIRE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,147 hrs · 23,963 cycles

EMERGENCY LIGHT BULB AT THE END OF CAT WALK FWD OF SLIDE PACK INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FITTING — CRACKED (RT MLG WW) · airframe 35,147 hrs · 23,963 cycles

RIGHT MLG WW FRAME ATTACH ANGLE FITTING CRACKED AT FWD INBD END AT KEEL ATTACHMENT. R & R FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (LT MLG WW) · airframe 35,147 hrs · 23,963 cycles

LEFT MLG WW FRAME CRACKED AT FWD INBD END ATTACHED TO KEEL. R & R FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 34,503 hrs · 23,566 cycles

AFT CARGO DOOR BARRIER DOOR FWD UPPER MOUNT ANGLE CRACKED AT FASTENER HOLE. REPAIRED ANGLE IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,503 hrs · 23,566 cycles

MID CABIN BATTERY CHARGER INOPERATIVE. R & R BATTERIES IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,503 hrs · 23,566 cycles

FORWARD CABIN BATTERY CHARGER INOPERATIVE. R & R BATTERIES IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,503 hrs · 23,566 cycles

AFT CABIN BATTERY CHARGER INOPERATIVE. R & R BATTERIES IAW AMM.

Part: CAP — CRACKED (LE SLAT) · airframe 34,503 hrs · 23,566 cycles

RIGHT WING NR 5 SLAT OTBD END CAP CRACKED. R & R CAP IAW AMM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,503 hrs · 23,566 cycles

FLOOR SUPPORT CORRODED AT BS 199, LBL 55. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,503 hrs · 23,566 cycles

R1 DOORWAY LOWER SHIELD ANGLE CORRODED AT BS 201, RBL 50. R & R ANGLE IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (R1 DOOR) · airframe 34,503 hrs · 23,566 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNT FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: MOUNT FITTING — CORRODED (R1 DOOR) · airframe 34,503 hrs · 23,566 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,503 hrs · 23,566 cycles

EMPENNAGE LT SIDE VENT LOUVER INTERIOR SUPPORT STRUCTURE ATTACH ANGLE CRACKED AT AFT UPPER CORNER. R & R ANGLE IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 34,503 hrs · 23,566 cycles

EMPENNAGE LT SIDE VENT LOUVER INTERIOR SUPPORT STRUCTURE ATTACH CLIP CRACKED AT FWD UPPER CORNER. R & R CLIP IAW DWG & SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,503 hrs · 23,566 cycles

RIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. RE LAMPED LIGHT IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,160 hrs · 23,335 cycles

AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,506 hrs · 22,911 cycles

AFT F/A FLASHLIGHT INOP. R&R BATTERY IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 30,744 hrs · 21,195 cycles

EEPLS LAMPS MISSING. INSTALLED BULBS IAW AMM.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 30,744 hrs · 21,195 cycles

LEFT WING UPPER FUEL ACCESS PANEL HAS CORRODED & DAMAGED FASTENERS (520CT). REMOVED & REPLACED DOME NUTS AS REQ IAW B717 SRM 51-41-00.

Part: RUB STRIP — CORRODED (LT WING) · airframe 30,744 hrs · 21,195 cycles

LEFT WING UPPER FUEL PANEL CUTOUT 520CT RUB STRIP IS CORRODED 22-05. REMOVED AND REPLACED RUB STRIP AT PANEL 520CT IAW B717 SRM 51-10-01.

Part: RUB STRIP — CRACKED (RT WING) · airframe 30,744 hrs · 21,195 cycles

CRACK CHANGE STRIP RIGHT WING TO BODY STA 579 BETWEEN L18R TO L19R 88-47. REMOVED AND REPLACED RUB STRIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

ANGLE SUPPORT CRACKED AT BS 653, STR 20R. REMOVED AND REPLACED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

CHAFE STRIP ANGLE CRACKED AT BS 579, BETWEEN LBL 18 TO LBL 19. REPAIRED ANGLES IAW SRM.

Part: STRIP — CRACKED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

NUMEROUS LOCATIONS OF CRACKED RUB STRIPS LEFT FWD FILLET STA 560 TO STA 653 BETWEEN L18L-L27L. 88-52. REMOVED AND REPLACED LEFT WING TO BODY FAIRING RUB STRIP IAW B717 SRM 53-20-70.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

STRINGER CORRODED BETWEEN BS 1002 TO BS 851, STR 30R. REMOVED AND REPLACED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

FRAME CORRODED AT BS 870, BETWEEN STR 29L TO STR 29R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

STRINGER CORRODED BETWEEN BS 946 TO BS 908, LBL 29. REMOVED AND REPLACED STRINGER SECTION IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

FRAME CORRODED AT BS 889, BETWEEN STR 29L TO STR 29R. REPAIRED FRAME IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

CUSP MEMBRANE CRACKED AT BS 661, LBL 58. REPAIRED DOUBLER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

STRINGER CORRODED AT BS 908, BETWEEN STR 29L TO STR 30L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

FRAME CORRODED AT BS 974, BETWEEN STR 29R TO STR 30R. REPAIRED FRAME IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

AFT CARGO DOOR CUTOUT LOWER PAN CORRODED BETWEEN BS 954 TO BS 990, BETWEEN STR 27R TO STR 28R. REPAIRED PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 30,744 hrs · 21,195 cycles

FWD CARGO DOOR FUSELAGE JAMB LOWER PAN CORRODED BETWEEN BS 389 TO BS 409. REPAIRED ANGLES IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 31,656 hrs · 21,785 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 30,627 hrs · 21,119 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 30,569 hrs · 21,080 cycles

EEPLS LENS MISSING AT ROW 28 DEF. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 30,569 hrs · 21,080 cycles

EEPLS LENS MISSING AT ROW 14 DEF. INSTALLED LENS PER MM.

Part: WIRE — UNSECURE (CABIN)

EMERGENCY PATHWAY LIGHTING LAYING ON FLOOR UNDERNEATH 26F, 22F, 21F, 20F, 16F. SECURED EMERGENCY PATHWAY LIGHTING WIRING MM REF 33-51.

Part: LANYARD — DETACHED (EVAC SLIDE)

GALLEY DOOR SLIDE LANYARD DETACHED. (CONTRACT MX RESECURED) PERFORMED VISUAL INSPECTION OF R-1 DOOR SLIDE LANYARD ATTACHMENT. OK FOR SERVICE AMM 25-61.

Part: SIGN — CRACKED (CABIN)

EXIT SIGN OVER ROW 1 IS CRACKED. REMOVED AND REPLACED EXIT SIGN REF SWPM 20-10, OPS CHECK GOOD REF MM 33-50.

Part: SUPPORT BEAM — GOUGED (FUSELAGE)

FWD CARGO COMPARTMENT, DOOR BUMPER AREA CEILING SUPPORT BEAM, STA 389, RBL 1, GOUGED. ACCOMPLISHED CEILING SUPPORT BEAM BLENDING AND REWORK PER 17-5320-2663 AND EA 17-53-02913IR.

Part: SKIN — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR LOWER FWD CORNER SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: SKIN — CRACKED (LT MLG DOOR)

LEFT MLG DOOR LOWER FWD CORNER SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER TRA 17-52-TR00139.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL45 TO RBL 58, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: DOOR — GOUGED (THRUST REVERSER)

NR 2 ENGINE, 5 O'CLOCK POSITION, TR DEFLECTOR DOOR, GOUGED. ACCOMPLISHED TR DEFLECTOR DOOR DOUBLER REPAIR PER B717 SRM 54-30-01 FIG 201 REPAIR 3.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, LBL 14, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: LONGERON — CRACKED (FUSELAGE)

LEFT LONGERON FINGER WEB, STA 208, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: LANYARD — BROKEN (GIRT BAR)

L-1 GIRT BAR LANYARD BROKEN. REMOVED AND REPLACED GIRT BAR LANYARD AND VERIFIED PROPER CONFIGURATION OF L-1 DOOR SLIDE AS OUTLINED IN 717 MM 25-61.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: STRUCTURE — DAMAGED (FUSELAGE)

LOWER CARGO DOOR AREA BELOW SCUFF PLATE REPAIR. ACCOMPLISHED REPAIR.

Part: FRAME — DAMAGED (FUSELAGE)

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

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT DOOR JAMB CORRODED OUT OF LIMITS. CUT AND SPLICE PAN. REPAIRED IAW SRM 53-20-15 REPAIR 7.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY E-PATH LIGHTS NOT WORKING AT SEAT ROW 1DF, 2DF, 3DF AND 10DEF. FOUND IMPROPER E-PATH LAMPS INSTALLED AT SEAT 3DF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY B5-118 IAW 33-51-03. RELAMPED E-PATH LIGHTS AT SEAT ROW 3DEF. OPS CHECK GOOD PER AMM 33-51-00.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

UPON A/C ARRIVAL NOTICED PARACHUTE PINS PULLED OUT OF L-1 DOOR SLIDE PACK. REMOVED AND REPLACED L-1 DOOR SLIDE PACK IAW AMM 25-61.

Part: NUT — LOOSE (OIL SYSTEM)

RT ENGINE OIL QUANTITY DROPPED FROM 8 QTS TO 2 QTS IN FLIGHT. REMOVED AND REPLACED OIL TUBE AND OIL TUBE BUSHING. RETORQUED OIL SCAVENGE AND OIL VENT TUBE UNION NUTS. PER AMM 79-21, 70-50 AND TYPICAL REPAIR TRA NR 17-79-TR00026. OIL CONSUMPTION MEASUREMENT CHECKED GOOD, PER AMM 79-00-00.

Part: SKIN — DAMAGED (BS 256-275)

GROUND DAMAGE LT SIDE A/C AT BS 256 AND L17 AND BS 275 LONGERON. CUT OUT DAMAGED AREA, FABBED AND INSTALLED DOUBLER REPAIR PER SRM 53-00-01 REPAIR 1 NDT OF CUT OUT AREA PERFORMED PER NDT SPM 06-10-01-001, NO CRACKS NOTED AT AAR W/O 28385 N/R 3777 AND 3780.

Part: FRAME — CRACKED (FUSELAGE)

CRACK NOTICED AFT FUSELAGE INT LEFT CANTED FRAME AREA STA 1178.225 BELOW L16L AFT OF HYD S/O VALVE. INSTALLED ANGLE REPAIR AT LEFT CANTED FRAME STA 1178.225 BELOW L161L, AFT OF HYD S/O VALVE IAW B717 SRM 51-70-11 FIG 201 REPAIR 1. MATERIAL USED 7075-0 .080 SIZE 11" X 21.2". HEAT TREATED FROM 0 TO T6 IAW AVBORNE HEAVY MAINTENANCE, GENERAL PROCESS SPEC 98PMS.24PS-01.

Part: PIN — MISSING (EVAC SLIDE)

L1 SLIDE PACK MISSING A PIN. REMOVED AND REPLACED L1 DOOR SLIDE REF 25-61-01.

Part: CONTROL UNIT — INOPERATIVE (E/E BAY)

AT FL 330 LOST L AC BUSS, G/S A/C EMERGENCY POWER ON NUMEROUS FAULTS AND INDICATION ERRORS. REPLACED EPCU AND OPS CHECKED REF AMM 24-21.