N944AT

Part: BOLT — MISSING (NLG LOCK LINK) · corrosion level 2 · airframe 64,038 hrs · 45,636 cycles

NLG LOCK LINK ASSY FOUND UPPER PIN RT I/B BOLT MISSING, LT I//B DAMAGED, AND PROTRUDING WITH EMANATING CORROSION ON UPPER LOCK LINK PIN REF B717 IPC 32-22-01-01. FOUND BOTH BOLTS REF B717 IPC 32-22-01-01 TO BE SHEARED AND PIN DAMAGED. FOUND NO SEALANT WITH TRACES OF CORROSION. NDT FOR REPLACEMENT LOCK LINK C/W ON AMDS W/C 3230-01132-01 JOB 000-0001 WORK PACKAGE 1367646. SEE NRC 003: A/C SIDE BUSHING REPLACED PER B717 AMM 32-22-01. (LP #0381995)

Part: ACTUATOR — FAULTED (NLG) · airframe 64,038 hrs · 45,636 cycles

SHIP 9504 -GEAR/DE- ON APPROACH FOR LANDING THE FLIGHT CREW RECEIVED AN "NLG UNSAFE" INDICATION AFTER SELECTING THE GEAR TO EXTEND. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED, AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE PERFORMED. THE NOSE LANDING GEAR DID EXTEND AT THAT TIME AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE NLG BUNGEE ACTUATOR, A MISSING UPPER PIN RIGHT INBOARD BOLT, A DAMAGED LEFT INBOARD BOLT, AND THE CORRODED UPPER LOCK LINK PIN (BOTH BOLTS). INVESTIGATION SHOWED THE BOLTS TO BE SHEARED AND THAT NO SEALANT WAS PRESENT. (LP #5625362)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,156 hrs · 44,874 cycles

ON SERVICE CHECK FOUND A FEW CEILING EMERGENCY LIGHTS OUT. MAINTENACE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT LOCATION B5-227 PER B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4369661)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,608 hrs · 44,432 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND THE L-1 DOOR FWD EXIT LIGHT AND THE R-1 DOOR AFT EXIT LIGHT EACH INOPERATIVE. THE POWER SUPPLY WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4547645)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,179 hrs · 44,053 cycles

WEB-CORRODED FS 1053 AFT SIDE AT STR 28 LH (P DOME AREA). SUMMARY NRC 096-0022:5310-2014/003 00258: CLEANED AREA CHECKED LIMITS REF B717-200 SRM 53-00-00-1A. REPLACE FASTENERS AS REQUIRED REF B717-200 SRM 51-40-02-0G. SUMMARY NRC 096-0022:5310-2014/003 00258: REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 1 CLOSING REQUIREMENTS RII: INSPECTOR 003 81621. SUMMARY NRC 096-0022:5310-2014/003 00258: REPAIRED WEB PER B717-200 SRM 51-70-10-2R REPAIR 1. CORROSION LEVEL CHANGED FROM: N TO: 1. SDR INDICATOR WAS CHANGED FROM: TO: Y. CORROSION LEVEL CHANGED FROM: 1 TO: 2. SUMMARY NRC 096-0022:5310-2014/003 00258: REPAIRED WEB PER B717-200 SRM 51-70-10-2R REPAIR 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,155 hrs · 44,030 cycles

THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. MAINTENANCE REPLACED THE EMERGENCY EXIT COVER AT R1 DOOR. (LP #2858553)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,898 hrs · 42,932 cycles

THE OVERWING EMERGENCY EXIT LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT SEAT ROW 20 IAW AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,441 hrs · 42,500 cycles

AIRCRAFT 9504, DURING SVC CHECK FOUND ROW 17 EMERGENCY LIGHTS NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMER LIGHT POWER SUPPLY BATTERY AT STA 645. LP 9420941

Part: NONE — NONE · airframe 59,284 hrs · 41,400 cycles

AN OUT OF LIMIT CRACK ON FLOOR BEAM STA Y=737 AND BTW X=52 RH TO X=56 RH. SUMMARY OF NRC 00095: FLOOR BEAM STA Y=737 AND BTW X=52 RH TO X=56 RH WAS REPAIRED PER ER/A 598428-14 REV. ORIGINAL SECTION 1 PERMANENT REPAIR AND PRI 598428-14 REV. 0 AND 1. REPETITIVE GENERAL VISUAL INSPECTION EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR IS FOLLOW UNDER LOG 2188880 PER ER/A 598428-14 REV ORIG.SECTION II. ASSOCIATED ER/A 14-598428 ADDED FOR AC 9504. (LP #2189997)

Part: NONE — NONE · corrosion level 2 · airframe 59,284 hrs · 41,400 cycles

HIDDEN CORROSION IN REF NRC 013: CORROSION ON INTERNAL PRODUCTION DOUBLER BELOW PAN ON AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 00091: LEVEL CORROSION 2, INTERNAL PRODUCTION DOUBLER CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PER PRI 598420-14 REV. 7 AND ER/A 598420-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II: REPETITIVE GENERAL VISUAL INSPECTION AT 8,000 CYCLES AND THEN EVERY 8,000 CYCLES AFTER 07 APRIL 2022, REPAIR FOLLOW UNDER LOG . 2189751 PER ER/A 598420-14 REV ORIG. SECTION II. ASSOCIATED ER/A 00-598420 ADDED FOR AC 9504. (LP #2190022)

Part: NONE — NONE · corrosion level 2 · airframe 59,284 hrs · 41,400 cycles

CORROSION ON LOWER DOOR JAMB REPAIR AT AFT CARGO DOOR JAMB BTW STA 954 TO 990 (CCT). SUMMARY OF NRC 00013: LEVEL CORROSION 2, LOWER DOOR JAMB AFT CARGO DOOR WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7, REPAIR 7. (LP #2190030)

Part: VANE — DENTED · airframe 59,291 hrs · 41,405 cycles

DENTS 2EA ON UPPER SURFACE OF UPPER VANE STA XRS 91.000 LH WING (LW). SUMMARY OF NRC 00027: FWD MOVABLE FLAP VANE LH WAS REMOVED AND INSTALLED PER B717 AMM 27-50-03 AND AMDS 2750-4009 ALSO WAS REPLACED UNDER LOG PAGE 2176221. (LP #2188594)

Part: VANE — DEBONDED · airframe 59,291 hrs · 41,405 cycles

DISBOND OF 1.10 IN X 1.00 IN LENGHT/WIDTH ON OUTBOARD FIXED GUIDE VANE AT RH WING. SUMMARY OF NRC 00239: OUTBOARD FIXED GUIDE VANE AT RH WING WAS REPAIRED PER B717 SRM 57-53-01-2R-1. (LP #2187656)

Part: SKIN — CRACKED · airframe 59,266 hrs · 41,382 cycles

CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH. SUMMARY OF NRC 00114: CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH WAS REPAIRED PER ER/A 598251-14 REV. ORIGINAL / PRI REV. 0 AND PRI REV. 1, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-598251 ADDED FOR AC 9504. (LP #2183872)

Part: ACCESS PANEL — MISSING (VERTICAL STAB) · airframe 58,280 hrs · 40,488 cycles

THE ACCESS PLATE IS MISSING FROM THE UPPER VERTICAL RIGHT SIDE STABILIZER BEARING DOOR 370PR. FOUND ON WALK AROUND AT GATE. MAINTENANCE INSTALLED THE ACCESS COVER PLATE ON THE RIGHT VERTICAL AT STABILIZER BEARING DOOR PER B717 AMM 55-35. AIRCRAFT IS OK FOR SERVICE. (LP #8049704)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,580 hrs · 39,081 cycles

THE AFT TAIL COMP EMERGENCY WALKWAY LIGHTS ARE NOT WORKING. MAINTENANCE REPLACED THE BATTERY PACK AT B5-260 AT STA 1037L, IAW B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 55,566 hrs · 38,148 cycles

THREE (3) ROWS JUST FORWARD OF OVERWING EXIT ROWS, EACH HAVE THE EMERGENCY EXIT PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT THE EMERGENCY LIGHT BATTERY PACK, B5 -120, CONNECTOR WAS LOOSE. RECONNECTED IT AND THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS GOOD. OK FOR SERVICE. (LP #5596394)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,329 hrs · 37,940 cycles

THE CABIN SIDEWALL EMERGENCY LIGHT IS MISSING IT'S COVER. MAINTENANCE INSTALLED A NEW COVER. OPERATIONAL CHECK WAS GOOD. (LP #1503125)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,962 hrs · 36,907 cycles

DURING CHECK OF CONDITION OF THE LIGHTED EXIT SIGN LOCATED ABOVE VENTRAL DOOR THE LIGHT DID NOT WORK.. REF CARD 1130-2002 STEP 28. EMERGENCY LIGHTS POWER SUPPLY WAS REMOVED AND A SERVISEABLE EMERGENCY LIGHTS POWER SUPPLY WAS INSTALLED IAW AMM 33-51-03-400-802, TESTED OK.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATES #520FT, 620AT, AND 620FT WERE FOUND OUT OF LIMITS REF SRM 57-10-01-2R REPAIR 2 CORROSION LEVEL II. NRC 00801: FUEL ACCESS PLATES WERE REPLACED AND WILL BE INSTALLED ON 2040- 0012 AND AMDS 2040-0010. (LP #1196242)

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 53,959 hrs · 36,905 cycles

ELONGATED HOLES IN ACCESS PLATE #520MB AND 520FT AT FUEL TANK LEFT WING (AI). NRC 00611: ELONGATED HOLES IN FUEL ACCESS PLATE #520MB WAS REPAIRED PER SRM 57-10-01-2R, REPAIR 2, CONDITION II AND FUEL ACCESS PLATE #520FT WAS REPLACED AND MUST BE INSTALLED ON 2040-0010. (LP #1194847)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

EXFOLATION ON FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT. NRC 00362: CORROSION LEVEL 2, FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-07-2R PROCEDURE 3, REPAIR 3 FIG 201 SHEET 4 AND 5. (LP #1191865)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON INTERCOSTAL FROM STA Y=946 TO Y=954 ABOVE LONG PROJECTION 29R AT AFT CARGO COMPARTMENT. NRC 00348: CORROSION LEVEL 2, INTERCOSTAL FROM STA Y=946 TO Y=954 ABOVE LONG PROJECTION 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 51-70-11-2R. (LP #1193274)

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 53,959 hrs · 36,905 cycles

CRACKS (2 EA.) IN CHANNEL FLOOR PANEL #222ZF. NRC 00797: CHANNEL FLOOR PANEL #222ZF WAS REPAIRED PER SRM 53-20-50-2R-5 REPAIR 5. (LP #1193258)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CARGO COMPARTMENT. NRC 00338: CORROSION LEVEL 2, FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-07-2R-3- FIG. 201. (LP #1191594)

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

PUNCTURE ON FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 30 LT SIDE (SM). NRC 00126: FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 30 LT SIDE WAS REPAIRED PER ETI-17-19-115 REV: 2 AND ER/A: 579976-14 REV: ORIGINAL. ASSOCIATED ER/A 00-579976 ADDED FOR AC 9504. (LP #1191216)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON HOLES COUNTERSUNK AND AREA SETTLEMENT AT ACCESS #620CT AND 520CT. FUEL TANK (AD,AI). NRC 00612: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED AND INSTALLED PER 2040-0012 AND 2040-0010. (LP #1189306)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK (0.250" LENGTH) ON THE UPPER RADIUS OF THE FRAME TAB OF THE RH OVERWING FRAME AT STA Y=715. NRC 0283: RH OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B. (LP #1189792)

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 53,959 hrs · 36,905 cycles

BROKEN FLOOR PANEL #1680B AT PAX CABIN. NRC 00613: FLOOR PANEL #1680B WAS FABRICATED, REPLACED, AND IDENTIFIED PER AMM 53-01-01-201. (LP #1189752)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON FRAME CLIP STA Y=954 BTW LONG 30 TO 29L AT AFT CARGO COMPARTMENT. NRC 00352: CORROSION LEVEL 2, FRAME CLIP STA Y=954 BTW LONG 30 TO 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-06-2R FIGURE 201. (LP #1189505)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON FRAME CLIP STA Y=927 BTW LONG 28L TO LONG 28R AT AFT CARGO COMPARTMENT. NRC 00337: CORROSION LEVEL 2, CORROSION ON FRAME CLIP STA Y=927 BTW LONG 28L TO LONG 28R AT AFT CARGO COMPARTMENT WAS REMOVED PER SRM 51-10-04 PAR 26. FRAME CLIP WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-00-1A FIG 103. FRAME CLIP WAS REPAIRED PER SRM 53-00-06-2R-2 AND 51-41-02-0G. (LP #1188321)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK (0.218" LENGTH) ON THE UPPER RADIUS OF THE FRAME TAB OF THE RT OVERWING FRAME AT STA Y=674. NRC 0282: RT OVERWING FRAME AT STA Y=674 WAS REPLACED PER CARD 5310-01436-03B. (LP #1189770)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

INTERCOSTAL WAS FOUND CRACKED ON STA Y=674 LONGERON 17R, IN REF 5310-01436-03B STEP F, AT CABIN PASSENGER (CPAX). NRC 00741: INTERCOSTAL ON STA Y=674 LONGERON 17R WAS REPLACED PER SRM 51-41-02-0G. (LP #1187582)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON RT CUSP WEB BTW STA Y=579 TO 598 UPPER AND LOWER SURFACES (CPAX). NRC 00593: CORROSION LEVEL 2, RT CUSP WEB BTW STA Y=579 TO 598 UPPER AND LOWER SURFACES WAS REPLACED PER DWG #9910151-116 AND SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0. (LP #1185779)

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK ON WINDOW FRAME BTW STA 715 RT SIDE CABIN PAX (SM). NRC 00677: WEB FRAME STA 715 BTW LONG 12 TO LONG 15 SIDE RT WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05- 0G. (LP #1185809)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON RT CUSP WEB BTW STA Y=465 TO 484 UPPER AND LOWER SURFACES (CPAX). NRC 00600: CORROSION LEVEL 2, RT CUSP WEB BTW STA Y=389 TO 503 UPPER AND LOWER SURFACES WAS REPLACED PER DWG #9930538-75 AND SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #1185775)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON FUEL TANK ACCESS PLATE. NRC 774: CORROSION LEVEL 2, CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE WAS FOUND OUT OF LIMITS REF SRM 57-10-01-2R REPAIR 2. FUEL ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED ON 2040-0012. (LP #1183539)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK ON SUPPORT OF FLOOR ACCESS PANEL #223AF (SM). NRC 00642: SUPPORT OF FLOOR ACCESS PANEL #223AF WAS REPAIRED PER SRM 53-20-50-2R-5. (LP #1184074)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON LONG 30 BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. NRC 00331: CORROSION LEVEL 2, LONG 30 BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-05-2R-2 FIG. 201. (LP #1183517)

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 53,959 hrs · 36,905 cycles

DELAMINATED FLOOR PANELS #211AJF AND 211ANF IN THE COCKPIT (COM). NRC 00629: DELAMINATED FLOOR PANEL #211ANF WAS REPLACED PER SRM 53-20-50-2R-3. THE FLOOR PANEL #211AJF IS METALLIC THEREFORE CANNOT BE DELAMINATED PER DWG #9957805 REV: Y. (LP #1182776)

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON OUTBOARD SEAT TRACK OF FIRST OFFICE SEAT. (CPIL). NRC 00776: CORROSION LEVEL 2, SEAT TRACK OF FIRST OFFICE SEAT WAS REPLACED PER SRM 51-41-01-0G. (LP #1181920)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON WEB FROM STA Y=946 TO STA Y=992 BTW LONG POJECTION 29R TO 28R AT AFT CARGO COMPARTMENT. NRC 00367: CORROSION LEVEL 2, WEB FROM STA Y=946 TO STA Y=992 BTW LONG POJECTION 29R TO 28R AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG #5910158-121 AND SRM 51-41-02 -0G, 51-41-05-0G, AND 51-41-04-0G. (LP #1180466)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON RT CUSP WEB FROM STA Y=522 TO Y=541 UPPER/LOWER SURFACES (CPAX). NRC 00759: CORROSION LEVEL 2, CUSP WEB FROM STA Y=522 TO Y=541 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 215. (LP #1181419)

Part: SKIN — DENTED (TE FLAP) · airframe 53,959 hrs · 36,905 cycles

NICKS WERE FOUND ON SURROUNDING EXISTING DENTS ON LEFT INBD FIXED VANE LOWER SKIN STA XV1. AI. IN REF, MON JOB 076. NRC 00726: REPAIR WAS PERFORMED ON LEFT INBD FIXED VANE LOWER SKIN STA XV1 PER SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR.4.D. AND 51-70-02-0G PAR.15.A(1)-(15). (LP #1180454)

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

EXCESIVE CORROSION ON RUB STRIPS OF LOWER RT SKIN FUEL ACCESS PANEL CUT OUTS #620LB & 620MB. IN REFERENCE NRC 00503. AD. NRC 00728: CORROSION LEVEL 2, RUB STRIPS OF LOWER RT SKIN FUEL ACCESS PANEL CUT OUTS #620LB & 620MB WERE REPLACED PER SRM 57-10-01-2R-3. (LP #1179589)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

PITTING CORROSION ON RH CUSP MEMBRANE WEB BTW STA Y=813 TO 794 UPPER AND LOWER SURFACE (CPAX). NRC 585: CORROSION LEVEL 2, DAMAGED AREA WAS REPAIRED PER SRM 53-00-55-2R-4 FIG.216. (LP #1180261)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

PITTING CORROSION ON CUSP MEMBRANE WEB STA Y=218 BTW X=-44 TO X=-54 AT CABIN PAX (CPAX). NRC 489: CORROSION LEVEL 2, CUSP MEMBRANE WEB STA Y=218-237 BTW X=-44 TO X=-60 WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #1178696)

Part: CUSP WEB — CANNING (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

OIL CANNING ON LH CUSP WEB STA Y=813 BTW SEAT TRACK 44 TO 56 (CPAX). NRC 580: CUSP WEB WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #1177031)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK ON LT CUSP WEB BTW STA Y=889 TO 908 APPROX (CPAX). NRC 0581: CRACK WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 215. (LP #1176278)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK FRAME BTW STA Y=1037 AND L=17R (CPAX). NCR 00555: FRAME BTW STA Y=1037 AND L=17R WAS REPAIRED PER SRM 53-20-07-2R REPAIR 4 FIG 201. (LP #1171859)

Part: STRUCTURE — CRACKED (SLIDING WINDOW) · airframe 53,959 hrs · 36,905 cycles

CRACK ON LT SLIDING WINDOW INTERNAL STRUCTURE AFT UPPER CORNER AT FLIGHT COMPARTMENT (CPIL). NRC 00658: LT SLIDING WINDOW INTERNAL STRUCTURE AFT UPPER CORNER AT FLIGHT COMPARTMENT WAS REPAIRED PER SRM 56-10-02-2R-1. (LP #1171856)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION ON LONG 29L BTW STA Y=903 TO STA Y=954 AT AFT CARGO COMPARTMENT. NRC 00333: CORROSION LEVEL 2, LONG 29L BTW STA Y=903 TO STA Y=954 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #1173381)

Part: STRUCTURE — CRACKED (SLIDING WINDOW) · airframe 53,959 hrs · 36,905 cycles

CRACK ON RT SLIDING WINDOW INTERNAL STRUCTURE AFT UPPER CORNER AT FLIGHT COMPARTMENT (SM). NRC 00657: RT SLIDING WINDOW INTERNAL STRUCTURE AFT UPPER CORNER AT FLIGHT COMPARTMENT WAS REPAIRED PER SRM 56-10-02-2R-1. (LP #1171176)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACKED LONGERON #17L IN STA Y=1022 (CPAX). NRC 00554: CRACK ON LONGERON #17L IN STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R FIG 201. (LP #1171072)

Part: DOUBLER — WORN (CABIN DOOR) · airframe 53,959 hrs · 36,905 cycles

WEAR ON DOUBLER OF MANUFACTURED INTERNAL STRUCTURE IN THE AFT CABIN BULKHEAD DOOR (SM). NRC 00689: DOUBLER OF THE AFT CABIN BULKHEAD DOOR WAS REPAIRED PER SRM 52-10-02-2R-16. (LP #1171498)

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1087 STRINGERS 13 AND 15R SIDE (SM). NRC 00158: SKIN BTW STA 1087 STRINGERS 13 AND 15R SIDE WAS REPAIRED PER ER/A :579571-14 REV ORIGINAL. ASSOCIATED ER/A 14-579571 ADDED FOR AC 9504. (LP #1168668)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 53,959 hrs · 36,905 cycles

CRACKED FLOOR PANELS #222ABF AND 222ANF ON PAX CABIN (CPAX). NRC 00663: FLOOR PANELS #222ABF AND 222ANF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1168812)

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK FRAME BTW STA Y=1037 AND L=17L (CPAX). NRC 00556: FRAME WAS REPAIRED PER SRM 53-20-07-2R REPAIR 4 FIG 201. (LP #1170157)

Part: SUPPORT BRACKET — CORRODED (RUDDER) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

CORROSION WAS FOUND ON SUPPORT BRACKET OF RUDDER YOKE BEARING ASSEMBLY IN REF 2720-2004 (EHV). NRC 00253: CORROSION LEVEL 2, SUPPORT BRACKET OF RUDDER YOKE BEARING ASSEMBLY WAS REPLACED PER SRM 51-41-02-0G AND DWG #5913121 REV D. (LP #1168559)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

CRACK ON LT CUSP WEB BTW STA 832 AND 851 PASSENGER CABIN (SM). NRC 00654: CRACK ON LT CUSP WEB BTW STA 832 AND 851 PASSENGER CABIN WAS REPAIRED PER SRM 53-00-55-2R-4. (LP #1168628)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 53,959 hrs · 36,905 cycles

PARTS RACKS: DELAMINATED FLOOR PANEL NR 221DF ON PAX CABIN. SUMMARY OF NRC 00665: FLOOR PANEL NR 221DF WAS FABRICATE REPLACED AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP1165057)

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,959 hrs · 36,905 cycles

INITIAL INSPECTION. CORROSION ON FINGER DOUBLER BTW STA Y: 585 TO Y: 570, S26L AT FWD CARGO COMPARMENT. FINGER DOUBLER WAS REPLACED PER SRM 51-00-07-0G, PAR. 5. CORROSION LEVEL 2. (LP1164589)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

AWR: HIDDEN DISCREPANCY: IN REF NRC 568: CRACK ON LT CUSP WEB BTW STA 446 AND 465 PASSENGER CABIN. SUMMARY OF NRC S/N 00656: CRACK ON LT CUSP WEB BTW STA 446 AND 465 PASSENGER CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 215. (LP1163685)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

INITIAL INSPECTION: CRACK LONGERON NR 6L IN STA Y=1022. LONGERON NR 6L IN STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2 FIG. 201. (LP1162983)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,959 hrs · 36,905 cycles

INITIAL INSPECTION: CRACK LONGERON NR 6R IN STA Y=1022. LONGERON N 6R IN STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2 FIG. 201. (LP1162729)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,451 hrs · 35,847 cycles

AFT EXIT AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. REPLACED BATTERY AT B5-116, STA.1045R AND REPLACED BATTERY AND POWER SUPPLY AT B5-260 STA. 1050L. EMERGENCY LIGHTS OP NORMALLY. REF B717 AMM 33-51. (LP5088037)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,353 hrs · 35,787 cycles

THE TAIL CONE CAT WALK EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY B5-260 FOR THE TAIL CONE WALK WAY AND THE EMERGENCY LIGHTS RETURNED TO NORMAL OPERATION. (LP #5100286)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,205 hrs · 34,984 cycles

THE B5-260 EMERGENCY LIGHT POWER SUPPLY WAS FOUND INOPERATIVE. REPLACED THE POWER SUPPLY, ALL TESTS WERE NORMAL AND THE AIRCRAFT IS OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,148 hrs · 34,948 cycles

DURING SERVICE CHECK, THE L1 AND R1 EXIT SIGNS FAILED TO ILLUMINATE DURING EMERGENCY LIGHT TEST. MAINTENANCE FOUND THAT THE BATTERY POWER SUPPLY WAS BAD AT POSITION B5-123. THE BATTERY POWER SUPPLY WAS REPLACED AND OPS CHECKED GOOD IAW AMM 33-51-03, WDM 33-51-12, AND FIM 33-50-00 810-801.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,980 hrs · 34,819 cycles

EMERGENCY LIGHT LENS DAMAGED. MAINTENANCE REPLACED THE LENS. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,145 hrs · 34,242 cycles

MAINTENANCE FOUND THE FORWARD OVERWING EMERGENCY EXIT DOOR SIGNS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,471 hrs · 33,810 cycles

FOUND THE AFT DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-260 IAW AMM 33-51. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,062 hrs · 33,544 cycles

SKIN CRACKED LEFT SIDE OF FUSELAGE JUST BELOW SKATE ANGLE OF VERTICAL LEADING EDGE. COMPLIED WITH ER/A 560998-14AD, REV A.

Part: SKIN — DAMAGED (BS 1118) · airframe 49,062 hrs · 33,544 cycles

FUSELAGE SKIN UNDER VERTICAL STAB FWD FAIRING, THREE FASTENER HOLES DAMAGED BS 1118, RBL 4. REPAIRED IAW ER/A 560967-14AD, REV 0. AND ER/A 560967-14AD, REV ORIGINAL.

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 49,067 hrs · 33,549 cycles

TAILCONE RELEASE CABLE ASSEMBLY ON THE LT SIDE HAS WORN AND BROKEN STRANDS. REPLACED THE CABLE ASSEMBLY IAW AMM 53-52-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,789 hrs · 33,359 cycles

FOUND EMERG LIGHTS ALONG WALKWAY IN 48 SEC OUT. REPLACED BATTERY AND POWER SUPPLY PER AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,136 hrs · 32,865 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THAT THE TAIL CONE EMERGENCY LIGHTS WERE INOPERATIVE. THE TAIL CONE EMERGENCY LIGHT BATTERY WAS REPLACED PER AMM 33-55. ALL CHECKS ARE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,672 hrs · 32,518 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT BATTERY POWER SUPPLY HAD FAILED. REPLACED THE BATTERIES IN THE POWER SUPPLY AND FUNCTIONALLY TESTED THE SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,372 hrs · 30,070 cycles

FORWARD LT OVERWING EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,372 hrs · 30,070 cycles

AFT EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,372 hrs · 30,070 cycles

AFT RT OVERWING EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,372 hrs · 30,070 cycles

AFT LT OVERWING EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — DIM (EXIT SIGN) · airframe 44,372 hrs · 30,070 cycles

OVERWING CEILING EMER EXIT SIGN LIGHT DIM. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,372 hrs · 30,070 cycles

CATWALK EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 42,789 hrs · 29,000 cycles

MID CABIN OVERHEAD CEILING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 42,789 hrs · 29,000 cycles

L1 DOOR OVERHEARD EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 42,789 hrs · 29,000 cycles

R1 DOOR LOWER AFT OVERHEARD EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 42,789 hrs · 29,000 cycles

RIGHT FWD OVERWING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 42,789 hrs · 29,000 cycles

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

Part: SPAR — CRACKED (LT WING) · airframe 42,789 hrs · 29,000 cycles

LEFT WING REAR SPAR WEB XRS 309.00 CRACKED. REPAIRED DOUBLER IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR UPLOCK AT AFT END CROSS MEMBER, ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BL 0. R & R SUPPORT IAW DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR LOWER JAMB INTERCOSTAL CORRODED AT BS 964. R & R INTERCOSTAL IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR LOWER JAMB TEE CORRODED AT BS 984. R & R TEE ANGLE IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR LOWER JAMB TEE ANGLE CORRODED AT BS 974. R & R TEE ANGLE IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

LEFT KEEL BEAM AREA FORMER CRACKED AT BS 679. R & R FORMER IAW FAS EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

RIGHT FORMER CRACKED AT BS 696. R & R FORMER IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 42,789 hrs · 29,000 cycles

RIGHT WING INBD BUTTE DOOR UPPER SKIN CRACKED. R & R BUTTE DOOR IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FORWARD PIT FRAME CORRODED AT BS 351, LONGERON 30. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FORWARD PIT FRAME CORRODED AT BS 541, BETWEEN LONGERON 30L - 29L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

AFT CARGO PIT INTERCOSTAL CORRODED AT BS 1025, LONGERON 29R. R & R INTERCOSTAL IAW SRM & DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FORMER CORRODED AT BS 579, LONGERON 28L. REPAIRED FORMER IAW EA.

Part: ANGLE — CRACKED (BS 1053) · airframe 42,789 hrs · 29,000 cycles

FUSELAGE ANGLE CRACKED AT BS 1053, LBL 56. R & R THE ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FRAME CORRODED AT BS 332, LONGERON 30. REPAIRED FRAME IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

AFT CARGO PIT, SKIN CORRODED AT BS 1009, LONGERON 26L. REPAIRED SKIN IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

WING TO BODY EXTERNAL SKIN LONGERON FITTING CORRODED AT BS 813, LONGERON 27R. R & R FITTING IAW DWG.

Part: SKIN — CRACKED (RT WING) · airframe 42,789 hrs · 29,000 cycles

RIGHT WING LE LOWER SKIN, CRACKED AT STATION XOSZ01, NUTPLATE HOLE GOING FWD. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 256, LBL 16. R & R SUPPORT IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

SKIN CRACKED AT BS 1022, LONGERON 14L. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

WING TO BODY FITTING CRACKED AT BS 735, BL 0. R & R FITTING IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 210, RBL 11. R & R SUPPORT IAW DWG.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SUPPORT FITTING CORRODED AT BS 210, RBL 55. REPAIRED FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 157 - 200, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, LBL 11. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 146, BETWEEN RBL 32 - 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 157, BETWEEN LBL 11 TO LBL 54. R & R FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 237, BL 0. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 899 TO 1022, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 237 TO 589, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 899 TO 1022, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 646 TO 823, LBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589 TO 646, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 TO 589, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 899 TO 1022, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 646 TO 823, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589 TO 646, RBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 646 TO 823, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 646 TO 823, LBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 823 TO 899, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 259 TO 589, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 823 - 899, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 237 TO 589, LBL 44. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

LEFT SIDE FORMER CRACKED AT BS 694. R & R FORMER IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

AFT LAVATORY LT SIDE ON FLOOR, THRESHOLD SUPPORT CORRODED AT LOWER EDGE. R & R SUPPORT IAW EA.

Part: CUSP WEB — CORRODED (BS 927-946) · airframe 42,789 hrs · 29,000 cycles

RIGHT CUSP WEB CORRODED AT BS 927 - 946. REPAIRED THE CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (BS 545) · airframe 42,789 hrs · 29,000 cycles

LEFT CUSP WEB CRACKED AT BS 545. REPAIRED THE CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN RT SIDE CUSP WEB CORRODED AT BS 965. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 160) · airframe 42,789 hrs · 29,000 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 160, BL 0. R & R SUPPORT IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

RIGHT KEEL BEAM AREA FORMER CRACKED AT BS 679. R & R FORMER IAW FAS EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FORMER CRACKED AT BS 1022, LONGERON 16R. R & R FORMER IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 178, RBL 25. R & R SUPPORT IAW DWG.

Part: CUSP WEB — CORRODED (BS 655) · airframe 42,789 hrs · 29,000 cycles

RIGHT CUSP WEB CORRODED AT BS 655. REPAIRED THE CUSP WEB IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FORMER CRACKED AT BS 1022, LONGERON 16R. R & R FORMER IAW DWG.

Part: CUSP WEB — CRACKED (BS 545-555) · airframe 42,789 hrs · 29,000 cycles

RIGHT CUSP WEB CRACKED AT BS 545 - 555. REPAIRED THE CUSP WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

COCKPIT FLOOR WEB CORRODED AT BS 149, RBL 16. REPAIRED FLOOR WEB IAW SRM.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

CABIN FALSE TRACK CORRODED BETWEEN BS 150 TO 200, LBL 7. R & R TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 42,789 hrs · 29,000 cycles

CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO 200, RBL 45. R & R THE FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 7 TO RBL 45. REPAIRED SUPPORT IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN CABIN FORMER CRACKED AT BS 1022, LONGERON 17L. R & R FORMER IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

LEFT KEEL BEAM AREA FORMER CRACKED AT BS 715. R & R FORMER IAW DWG.

Part: CUSP WEB — CRACKED (BS 655) · airframe 42,789 hrs · 29,000 cycles

RIGHT CUSP WEB CRACKED AT BS 655. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 42,789 hrs · 29,000 cycles

RIGHT WING NR 5 SLAT INBD SIDE OF NR 12 TRACK ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

MAIN FRAME WING TO BODY FITTING CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW DWG & EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR LOWER JAMB AREA, FUSELAGE SKIN INTERNAL DOUBLER CORRODED. R & R JAMB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

C2 DOOR LOWER JAMB CLOSE OUT WEB CORRODED AT CUT OUT. R & R WEB IAW DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

FORWARD CARGO COMPARTMENT LOWER DOOR JAMB, CORRODED AT FASTENER ATTACH POINTS. REPAIRED JAMB IAW SRM.

Part: CUSP WEB — CRACKED (BS 655-674) · airframe 42,789 hrs · 29,000 cycles

LEFT CUSP WEB CRACKED AT BS 655 - 674. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

RIGHT CABIN CUSP WEB CRACKED AT STATION 655 TO 696. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

CENTER SECTION SEAT TRACK VERTICAL SUPPORT CRACKED AT BS 737, RBL 45. REMOVED & REPLACED SUPPORT IAW DWG.

Part: VERTICAL SUPPORT — CRACKED (BS 737) · airframe 42,789 hrs · 29,000 cycles

SEAT TRACK CENTER SECTION VERTICAL SUPPORT CRACKED AT BS 737, LBL 45. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CRACKED (BS 715) · airframe 42,789 hrs · 29,000 cycles

SEAT TRACK CENTER SECTION VERTICAL ANGLE CRACKED AT BS 715, LBL 45. R & R ANGLE IAW DWG.

Part: ANGLE — CRACKED (TE FLAP TRACK) · airframe 42,789 hrs · 29,000 cycles

RIGHT WING INBD SIDE OF NR 1 FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,789 hrs · 29,000 cycles

LEFT WW CUT OUT FWD FRAME CRACKED ABOVE DOOR UPLOCK SWITCH. REPAIRED DOUBLER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,779 hrs · 28,995 cycles

AFT ACCESSORY TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,980 hrs · 28,490 cycles

FWD EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: LATCH — OBSTRUCTED (L1 DOOR) · airframe 41,690 hrs · 28,313 cycles

L1 DOOR SLIDE GIRT BAR HARD TO INSERT. CLEANED DEBRIS FROM GIRT BAR LATCH & LUBRICATED IAW MT.

Part: CLEAT — DIRTY (GIRT BAR) · airframe 41,258 hrs · 28,035 cycles

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

Part: FITTING — DIRTY (GIRT BAR) · airframe 41,242 hrs · 28,025 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 401,220 hrs · 27,324 cycles

LT WING FIXED LE RIB CRACKED ON LOWER END AT STATION 102. R&R RIB IAW B717 SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (LT WING) · airframe 401,220 hrs · 27,324 cycles

LT WING FIXED LE STRINGER SPLICE CRACKED AT STATION 168. R&R SPLICE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (LT WING) · airframe 401,220 hrs · 27,324 cycles

LT WING FIXED LE SPLICE STIFFENER CRACKED AT STATION 168. R&R STIFFENER IAW SRM & DRAWING.

Part: LINER — CRACKED (L1 DOOR) · airframe 401,220 hrs · 27,324 cycles

L1 DOOR LINER FWD OF DOOR SLIDE CRACKED. REPAIRED LINER IAW SRM.

Part: LONGERON — BROKEN (FUSELAGE) · airframe 401,220 hrs · 27,324 cycles

LONGERON BROKEN AT BS 1133, LONGERON 2L. R&R LONGERON IAW SRM.

Part: FRAME — BROKEN (FUSELAGE) · airframe 401,220 hrs · 27,324 cycles

FRAME BROKEN AT BS 1133, LONGERON 2. REPAIRED FRAME IAW SRM & DRAWING.

Part: LONGERON — BROKEN (FUSELAGE) · airframe 401,220 hrs · 27,324 cycles

LONGERON BROKEN AT BS 1133, LONGERON 2R. R&R LONGERON IAW SRM.

Part: DOOR — CRACKED (EMERGENCY EXIT) · airframe 41,220 hrs · 27,324 cycles

LT FWD EMERGENCY EXIT DOOR HOLDER LOWER AFT CORNER CRACKED. REPAIRED DOOR IAW SRM. CORRECTION OF TOTAL TIMES FROM 401220 TO 41220.

Part: COVER — MISSING (CABIN) · airframe 40,706 hrs · 27,690 cycles

AFT CABIN CEILING LIGHT COVER MISSING. INSTALLED LIGHT IAW AMM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 37,678 hrs · 25,758 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED BRACKET PER MM.

Part: PIN — OUT OF ADJUST (EVAC SLIDE) · airframe 37,655 hrs · 25,740 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK PIN OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER AMM.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 37,440 hrs · 25,605 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,346 hrs · 25,545 cycles

FWD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: HOLDER — DIRTY (GIRT BAR) · airframe 37,207 hrs · 25,449 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HARD HOLDER TO ENGAGE. CLEANED HOLDER PER MM.

Part: CABLE — BROKEN (GIRT BAR) · airframe 36,896 hrs · 25,249 cycles

ASSEMBLY GIRT BAR LANYARD CABLE STRAND BROKEN. REPLACED LT SLIDE GIRT BAR LANYARD CABLE IAW MM.

Part: PIN — PULLED (EVAC SLIDE)

FOUND R1 DOOR SLIDE PINS PULLED, AWI. REMOVED AND REPLACED R1 DOOR SLIDE (EVACUATION) ASSY PER MM 25-61, OPS CK GOOD, AWI.

Part: CONNECTOR — DISCONNECTED (CABIN)

THE 14 DEF EM PATH LIGHT OUT. RECONNECTED EMERGENCY LIGHT SIDEWALL TO SEAT ASSEMBLY CONNECTOR IAW SWPM 20-31-13 OPS/FUNCTIONAL CHECKS NORMAL IAW AMM / 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

THE 3 EA EMERGENCY ESCAPE LIGHTS IN TAIL COMPARTMENT OUT. RELAMPED OPS CHECK GOOD REF MM 33-51.

Part: PIN — BACKED OUT (CABIN)

THE 19 DEF EM PATH LIGHT OUT. RESEATED 2 EACH PUSHED PINS AT EMERGENCY LIGHT SIDEWALL TO SEAT ASSEMBLY CONNECTOR IAW SWPM 20-31-13 OPS/ FUNCTIONAL CHECKS / NORMAL IAW AMM 33-51-00.

Part: STRUCTURE — CRACKED (LT MLG DOOR)

OUTBOARD FWD EDGE LT MLG DOOR, CRACKED. ACCOMPLISHED LT MLG DOOR DOUBLER REPAIR PER B717 TRA 17-52-TR00139 FIG 2.

Part: SKIN — DAMAGED (FUSELAGE)

LEFT FUSELAGE SKIN SLICE REPAIR, GOUGED. ACCOMPLISHED SKIN SLICE REPAIR REPLACEMENT PER B717 SRM 53-00-00, 53-00-01 AND 51-41-02.

Part: SHEAR TIE — CRACKED (FUSELAGE)

AFT ACCESSORY COMP SHEAR TIE, CRACKED. ACCOMPLISHED SHEAR TIE REPLACEMENT PER B717 SRM 51-41-05 AND 51-41-02.

Part: SPLICE — CORRODED (CARGO DOOR)

AFT CARGO COMPARTMENT DOOR CUTOUT SEAL DEPRESSOR FWD SPLICE, CORROSION. ACCOMPLISHED SEAL DEPRESSOR FWD SPLICE REPLACEMENT PER B717 SRM 51-41-01 AND 53-20-15.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOTH OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING BATTERY PACK REF AMM 33-51.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

R1 DOOR SLIDE PRESSURE GAUGE IS IN RED. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

AFT ACCESSORY COMPARTMENT CATWALK (FORWARD) AREA EMERGENCY LIGHT HAS ONE BULB INOP. RELAMPED AND PERFORMED OPS CHECK.

Part: SOCKET — LOOSE (CABIN)

ROW 1 DF (AFT) E-PATH LIGHT SOCKET UN-SECURE AND MISSING LENS & BULB. SECURED SOCKET AS REQUIRED. INSTALLED LIGHT BULB AND LENS AS REQUIRED, AND PERFORMED OPS CHECK.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHT AT SEAT 25D INOP. FOUND CONNECTOR LOOSE. RE-ATTACHED CONNECTOR. LIGHTS OPERATE NORMAL REF B717 SWPM 20-31.

Part: CHANNEL — DAMAGED (FUSELAGE)

INSTALLED U-CHANNEL REPAIR AT STA 110 AND LONGERON 29R PER B717 SRM 51-70-11 FIGURE 201. SEE NR 2238 AND 3191.

Part: STRINGER — UNKNOWN (FUSELAGE)

INSTALLED NEW STRINGER SECTION AND SPLICES AT LONGERON 23R BETWEEN STA 160 AND 200 PER B717 SRM 53-00-05 FIG 201 REPAIR 2. SEE NR 3240.

Part: FRAME — DAMAGED (FUSELAGE)

INSTALLED FRAME REPAIR PARTS AT STA 180 BETWEEN LONGERON 22R AND 24R PER EA 17-53-02050IR DATED 09/28/09, B717 SRM 53-20-07, 53-20-07 PAGE 20, 51-41-05 AND 51-41-02. SEE NR 3245 AND 2233.

Part: SHEAR TIE — DAMAGED (FUSELAGE)

INSTALLED SHEAR TIE AND SPLICE REPAIR AT STA 180 LONGERON 23R PRE B717 SRM 53-00-06 FIGURE 201. SEE NR 3239.

Part: CUSP WEB — DAMAGED (FUSELAGE)

INSTALLED CUSP MEMBRANE REPAIR AT FUSELAGE STATION 636 LONGERON 18L PER DRAWING SG09530003. SEE NR 3071 AND 3235.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: CUSP WEB — DAMAGED (FUSELAGE)

INSTALLED CUSP MEMBRANE REPAIR BETWEEN FUSELAGE STATION 579 AND 560 LONGERON 18R PER DRAWING SG09530003. SEE NR 3068 AND 3234.

Part: STRUCTURE — DAMAGED (FUSELAGE)

INSTALLED DOUBLER REPAIR AT STA 213 AFT OF GALLEY RBL 54 PER EA 17-53-02049IR DATED 09/24/09 RFE 09-1538 AND B717 SRM 51-70-10. SEE NR 3096 AND 3505.

Part: DOOR FRAME — DAMAGED (FUSELAGE)

INSTALLED FWD CARGO LOWER JAMB PAN SECTION AND SPLICE REPAIR PER B717 SRM 53-20-15 FIGURE 201. SEE NR 3040 AND 3244.

Part: STRUCTURE — DAMAGED (FUSELAGE)

INSTALLED DOUBLER REPAIR FROM STA 168 TO 196, BETWEEN LONGERON 22R TO 24R PER DRAWING SG09530002. SEE NR 3019, 3238, 2225 AND 2231.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.

Part: LONGERON — UNKNOWN (FUSELAGE)

INSTALLED LONGERON 30 AND 29R AT E & E COMPARTMENT FROM STA 120 TO 134 AND INSTALLED DOUBLER REPAIR PER B717 SRM 53-00-06 FIG 20 AND B717 SRM 51-41-02. SEE NR 3190, 2217 AND 2224.

Part: CYLINDER — LEAKING (LANDING GEAR)

RIGHT HYDRAULIC PRESSURE LOW. REMOVED & REPLACED THE MAIN LANDING GEAR TRANSFER CYLINDER PER M/M REFERENCE 32-33, SERVICED HYDRAULIC SYSTEM AND SAFTIED RIGHT SPOILER BYPASS PER M/M REFERENCE 12-13 AND PERFORMED FUNCTIONAL CHECK OF THE MAIN LANDING GEAR EXTENSION AND RETRACTION PER M/M REFERENCE 32-30.

Part: LIGHT — INOPERATIVE (NLG INDICATOR)

NOSE GEAR INDICATOR DOES NOT INDICATE GREEN. RELAMPED NLG INDICATOR, OPS CHECKS GOOD REF AMM 33-00.

Part: PSU — MALFUNCTIONED (29 DEF)

THE 02 MASKS AT ROWS 29 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK GOOD PER MM 35-22.

Part: PSU — MALFUNCTIONED (SEAT 16 DEF)

THE 02 MASKS AT ROWS 16 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK GOOD PER MM 35-22.

Part: PSU — MALFUNCTIONED (30 DEF)

THE 02 MASKS AT ROWS 30 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK GOOD PER MM 35-22.

Part: DUCT — SEPARATED (CABIN PRESSURE)

AT 30,000 FT HEARD LOUD POP. CABIN ALT ALERT ON. DESCENDED TO 10,000 FEET. MASK DEPLOY IN CABIN. INSPECTED AND FOUND LARGE CHECK VALVE ON AIR CONDITION SYSTEM LOCATED AT AFT PRESSURE BULKHEAD WITH DAMAGED FLAPPER VALVE AND SPIDER DUCT SEPARATED. REMOVED AND REPLACED CHECK VALVE AND SPIDER DUCT ASSEMBLY PER AMM 21-22. PERFORMED CABIN PRESSURE CHECK. REF AMM 21-30, OPS CHECK GOOD.

Part: PSU — MALFUNCTIONED (SEAT 27 AC)

THE 02 MASKS AT ROWS 27 AC DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK GOOD PER MM 35-22.

Part: CHECK VALVE — DAMAGED (CABIN PRESSURE)

AT 30,000 FT HEARD LOUD POP. CABIN ALT ALERT ON. DESCENDED TO 10,000 FEET. MASK DEPLOY IN CABIN. INSPECTED AND FOUND LARGE CHECK VALVE ON AIR CONDITION SYSTEM LOCATED AT AFT PRESSURE BULKHEAD WITH DAMAGED FLAPPER VALVE AND SPIDER DUCT SEPARATED. REMOVED AND REPLACED CHECK VALVE AND SPIDER DUCT ASSEMBLY PER AMM 21-22. PERFORMED CABIN PRESSURE CHECK. REF AMM 21-30, OPS CHECK GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT DOOR JAM HAS CORROSION ON THE AFT AND CENTER SECTION. CORROSION OUT OF LIMITS PER SRM 53-00-00. REPLACED DOOR PAN.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT LOWER CARGO COMPARTMENT DOOR JAMB HAVE CORROSION ON THE AFT AND CENTER SECTION. INSTALLED REPAIR SPLICE ON AFT LOWER DOOR JAMB BETWEEN STA 994.000 AND STA 954.000 IAW SRM 53-20-15 FIG 201. 7075-0 40, SIZE 5 X 6 INCHES. HEAT TREATED IAW PMS24PS-01.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY)

AFT LOWER CARGO COMPARTMENT DOOR JAMB HAS CORROSION ON THE AFT AND CENTER SECTION. INSTALLED REPAIR SPLICE ON AFT LOWER JAMB BETWEEN STA 994.000 AND STA 954.000 IAW SRM 53-20-15 FIG 201. 7075-0. 40 SIZE 5 X 6 INCH. HEAT TREATED IAW PMS24PS-01.

Part: GUSSET — CORRODED (FUSELAGE)

TIE STRAP CORRODED IN AFT CARGO PIT STA 994 STRINGER 29R. REPLACED TIE STRAP (GUSSETT).

Part: STRUCTURE — CRACKED (FUSELAGE)

RIGHT HAND VENT BOX CRACKED AT UPPER CORNER. INSTALLED ANGLE DOUBLER REPAIR AT RIGHT HAND VENT BOX UPPER CORNER IAW TASK CARD 17-5320-2023 AND B717 SRM 51-41-02. MATERIAL USED 7075 T6 .090 SIZE 6" X 6".

Part: CONTROL UNIT — SHORTED (FIRE DETECTION)

(ENG L FIRE) LEVEL 3 INDICATION IN CRUISE FLIGHT. RAN QRH, PULLED T-HANDLE, EXPENDED FIRE BOTTLE 1 AND 2. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR CONTROL UNIT, REF 26-11, RAN ENGINE, PERFORMED FIRE TEST AND FAULT TEST, CHECKS GOOD, SEE 749178-3 AND 749178-2.

Part: SKIN — DENTED (FUSELAGE)

AIRCRAFT STRUCK BY BAG CART ON AIRCRAFT RIGHT AFT OF RIGHT ENGINE ON EMP. INSTALLED FLUSH SKIN REPAIR AT FRAMES 1059 AND 1076 BETWEEN LONGERON 24L AND 24R IAW SRM 53-00-01 FIG 201 AND SRM 51-70-11 FIG 201. MATERIAL USED 7075-T6 .040 MFG LOT 26911, 7075-T6 .050 MFG LOT 708-411 AND 6AL4V .32 LOT NO PQ0LXF61, HEAT TREATED TO 7075-T6 PER GENERAL PROCESS SPECIFICATION 98PS.247PS-01.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE AUTO SHUTDOWN. WHILE IN CLIMB POWER PASSING THROUGH FL 210 A LOUD POP WAS HEARD. NR 1 LEFT ENGINE OIL PRESSURE WENT TO ZERO. ENGINE RPM REDUCED TO IDLE AND CONTINUED WINDMILL, LEFT ENGINE OIL PRESSURE AND QUANTITY INDICATIONS WHERE X-OUT. ENGINE OIL PRESSURE QUANTITY LOW, EAD. REMOVED AND REPLACED NR 1 ENGINE.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN IS DENTED AT APPROX FS 260, LONGERON 17 LEFT. DENT IS 2 IN X .050. CONDITION FOUND TO BE 1B PER B717 SRM 06-00-07 PG 213. ACCOMPLISHED HIGH FREQ PER NDT SPM 06-00-07. INSTALLED DOUBLER REPAIR AT FS 260 LONGERON 17L IAW B717 SRM 53-00-01. MATERIAL USED 2024T3 .050 FOR FILLER SIZE 35.625" X 14", 2024 T3 .063 FOR DOUBLER SIZE 34.5" X 15.5" AND 2024 T3.0225 FOR FINGER DOUBLER SIZE 41" X 16.5".

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND EMERGENCY LIGHTS FAILED TO OPERATE WITH FLIGHT STATION SWITCH OFF AND FORWARD FLIGHT ATTENDANT PANEL SWITCH ACTIVATED. REMOVED AND REPLACED DISCHARGED BATTERY PACK AT BS 125 IAW B717 MM 33-51-00.