N983AT

Part: ANTI-SKID SYS — FAULTED (ZONE 700) · airframe 47,491 hrs · 33,865 cycles

PERFORMED GO AROUND AND DECLARED AN EMERGENCY DUE TO LEFT ANTISKID CAUTION MESSAGE ON FINAL APPROACH. RECORDED BCU INTERNAL FAULT CODE 32417A. REPLACED BCU. OPS CHECK GOOD. (LP 7834420)

Part: DOOR — NOT SEATED (ZONE 800) · airframe 46,960 hrs · 33,378 cycles

AIRCRAFT RETURNED TO ATL DUE TO A CABIN INFLOW MSG. FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION AND REPLACED THE AFT CARGO DOOR. OPS AND LEAK CHECK GOOD.(7595084)

Part: LATCH — NOT SEATED (ZONE 800) · airframe 46,833 hrs · 33,261 cycles

SHIP 9560-ATB- AIRCRAFT RETURNED TO CLT DUE TO A CABIN INFLOW MSG. CORRECTIVE ACTION: FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, RESECURED DOOR AND PERFORMED A FUSELAGE LEAK TEST, AFT CARGO DOOR PROX SENSORS TESTED NORMAL. A/C RETURNED TO SERVICE.(7731932)

Part: SKIN — GROUND DAMAGE (ZONE 500) · airframe 46,772 hrs · 33,202 cycles

GSE TOW TRUCK CAME IN CONTACT OF LH, OUTBOARD UNDER WING. C/W ER/A 628016-14.

Part: DUCT — DISCONNECTED · airframe 45,063 hrs · 31,715 cycles

SHIP 9560 -FUME/DE- DURING THE DECENT WHEN THE POWER WAS REDUCED TO IDLE, THE F/A REPORTED A "BURNT CARPET/CRAYON" SMELL IN THE CABIN. F/O NOTIFIED THE CAPT THAT HE TOO SMELLED IT IN THE COCKPIT AND BOTH DONNED O2 MASKS. THE CAPT DECLARED AN EMERGENCY WITH ATC. ARFF MET THE AIRCRAFT UPON ARRIVAL. THE FUMES DISSIPATED AFTER ENGINE SHUTDOWN. MAINTENANCE FOUND A DISCONNECTED RAM/FAN DISCHARGE DUCT AND REPLACED THE BOOT. ALSO REPLACED THE COALESCER BAGS. (LP #5725322)

Part: ACCESS DOOR — DETACHED (ZONE 300) · airframe 45,064 hrs · 31,716 cycles

HORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS WERE DISCOVERED MISSING DURING POSTFLIGHT INSPECTION. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED PANEL 370SL BEARING COVER PANEL MISSING. DEFER MISSING HORIZONTAL STAB BEARING ACCESS COVER LT SIDE 370SL TO CDL 55-35-02. MCO/PLACARD INSTALLED. NO M PROCEDURES. UPDATE PARTS REQUIRED NEEDS PART NUMBER 5981063-501 IPC REF 55-34-35-01 #240. THESE PARTS MAY BE REQUIRED. VERIFY EFFECTIVITY BEFORE INSTALL. (LP #6413313)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 44,187 hrs · 30,970 cycles

DURING EMERGENCY LIGHTS CHECK, THE EXTERIOR EMERGENCY LIGHTS TURN ON WITH FLIGHT CABIN SWITCH IN ARM POSITION. SUMMARY OF NRC00627: CONTINUITY WAS PERFORMED PER B717-200 WDM 33-51-11 IN CONNECTOR (P1-125) OF EMERGENCY EVACUATION BATTERY POWER SUPPLY. A MELTED PIN (F) WAS FOUND AND THE EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717-200 AMM 33-51-06.TEST OK. (LP #0354818)

Part: BEAM — CRACKED (AFT CARGO) · airframe 44,187 hrs · 30,970 cycles

CRACK ON BEAM #1 AT AFT CARGO DOOR. SUMMARY OF NRC 00575: BEAM #1 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 617654-14 REV ORIGINAL. ASSOCIATED ER/A 14-617654 ADDED FOR AC 9560. (LP #0351759)

Part: SKIN — SCRATCHED (LT NR 1 SLAT) · airframe 44,187 hrs · 30,970 cycles

SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0. SUMMARY OF NRC 00610: SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0 WAS REPAIRED PER ER/A 618009-14 REV ORIG. SECTION I PERMANENT REPAIR AND PER PRI 618009-14 REV 1. ASSOCIATED ER/A 14-618009 ADDED FOR AC 9560. (LP #0352239)

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00589: CORROSION LEVEL 2. HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 617688-14 REV 3 AND ER/A 617688-14 REV ORIG SECTION I: TIME LIMITED REPAIR DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT UNDER LOG PAGE 0347210. ASSOCIATED ER/A 14-617688 ADDED FOR AC 9560. (LP #0348840)

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON HOLES 27 AND 28, CENTER BOX RH, AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00581: HOLES 27 AND 28 CENTER BOX RH AT HORIZONTAL STABILIZER. WERE REPAIRED PER PRI 617657-14 REV 1 AND ER/A 617657-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617657 ADDED FOR AC 9560. (LP #0346973)

Part: DOUBLER — DAMAGED (NOT REPORTED) · airframe 44,187 hrs · 30,970 cycles

MISSING MATERIAL IN ONE HOLE WAS FOUND AT INNER DOUBLER. SUMMARY OF NRC 00583: AREA WAS REPAIRED PER ER/A 617844-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617844 ADDED FOR AC 9560. (LP #0346414)

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 44,187 hrs · 30,970 cycles

DENT WITH CRACK (1 EA) 19" FROM OTBD EDGE AND 5.500" FROM LEADING EDGE AND DENT WITH DISBOND (1 EA) 34" FROM OUTBD EDGE AND 4" FROM TRALING EDGE ON LOWER SURFACE AT AFT FLAP MOVABLE VANE AT RIGHT WING. SUMMARY OF NRC 00563: LOWER SURFACE AT AFT FLAP MOVABLE VANE AT RIGHT WING WAS REPAIRED PER ER/A 617662-14 REV ORIGINAL. ASSOCIATED ER/A 14-617662 ADDED FOR AC 9560. (LP #0342625)

Part: BOTTLE — LOW PRESSURE (TAIL SLIDE) · airframe 44,187 hrs · 30,970 cycles

PRESSURE WAS FOUND TO BE OUT OF RANGE ON THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00519: TAIL CONE SLIDE WAS REMOVED UNDER AMDS 5352-4001 AND REPLACED PER B717 IPC 25-61-02-01 ITEM 280 AND INSTALLED UNDER AMDS 5352-4002. (LP #0340855)

Part: FRAME — CRACKED (BS 1116 L21R) · airframe 44,187 hrs · 30,970 cycles

CRACK ON FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00238: FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-07-2R REPAIR 1 FIG 201. (LP #0337618)

Part: DOUBLER — CORRODED (BS 119-199) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E. SUMMARY OF NRC 00186: CORROSION LEVEL 2. DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E WAS REPLACED PER B717-200 DWG 9923686 REV D AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. FORWARD WATER DRAIN MAST HEATER INSTALL IS UNDER NRC 00615. (LP #0336861)

Part: DOOR FRAME — DAMAGED (FWD CARGO) · airframe 44,187 hrs · 30,970 cycles

BENT AND MISSING MATERIAL ON AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00008: AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 617722-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617722 ADDED FOR AC 9560. (LP #0336197)

Part: SUPPORT FITTING — CORRODED (R1 GIRT BAR) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS. ALSO CORROSION ON PANEL LOCATED BELOW FITTINGS. SUMMARY OF NRC 00426: CORROSION LEVEL 2. R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS AND PANEL LOCATED BELOW FITTINGS PANEL WERE FABRICATED AND REPLACED PER DRAWING 9957828 REV AB. (LP #0333365)

Part: INTERCOSTAL — CRACKED (BS 636) · airframe 44,187 hrs · 30,970 cycles

CRACK ON INTERCOSTAL STA Y=636, X=0 AT C1. SUMMARY OF NRC 00183: INTERCOSTAL STA Y=636, X=0 AT C1 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0331871)

Part: SEAT TRACK — CORRODED (BS 200-215) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215. SUMMARY OF NRC 00343: SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215 WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0331571)

Part: CUSP WEB — CORRODED (BS 294-313) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION OUT OF LIMITS IN REF NRC 298, CUSP WEB BTW X=-56 TO -60 AND Y=294-313 AND STA 420 TO 437, STA 674, STA 889 ALSO ON RH CUSP WEB BTW STA X=-44 TO -56 WITH ORIGINAL THICKNESS IS 0.020" AND MINIMUM REMAINING THICKNESS IS 0.08". THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-55-1A ALLOWABLE DAMAGE 1 AND PAR 4 C FIG 103A. SUMMARY OF NRC 00560: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO -60 AND Y=294-313 AND STA 420 TO 437, STA 674, STA 889 ALSO ON RH CUSP WEB BTW STA X=-44 TO -56 WERE REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0326860)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 44,187 hrs · 30,970 cycles

CRACK ON AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR. SUMMARY OF NRC 00247: AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0321706)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,187 hrs · 30,970 cycles

CRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00086: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DWG 9955763 REV M AND REPLACE PER B717-200 SRM 51-41-02-0G. (LP #0316698)

Part: FLOOR PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00411: CORROSION LEVEL 2. CORROSION WAS FOUND ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. IN ACCORDANCE B717-200 SRM 51-10-04-0G PROCEDURE GENERAL FIG 2 THE PANELS WERE MANUFACTURED AND REPLACED PER ER/A 591778-14TR REV ORIGINAL SECTION L: PERMANENT REPAIR AND B717-200 AMM 25-58-01-350-801C2. ASSOCIATED ER/A 14-591778 ADDED FOR AC 9560. PLEASE SHOW SECTION L TO READ SECTION I. (LP #0315017)

Part: CUSP WEB — CORRODED (BS 359-382) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON LOWER SURFACE OF LH CUSP WEB BTW STA 359-382. ALSO UPPER SURFACE BTW 660-664 PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00315: CORROSION LEVEL 2. CUSP WEB ON STA 660-664 PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 216. CORROSION LEVEL 1 CORROSION ON CUSP WEB BTW STA 359-382 PAX CABIN FLOOR STRUCTURE WAS REMOVED AND EVALUATED PER B717-200 SRM 51-10-04-0G PAR 26.C (1) AND PER B717-200 SRM 53-00-55-1A, 51-10-02-0G PAR 8 (F), AND DWG 9930538 REV BR. (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LOWER SURFACE OF LH CUSP WEB BTW STA 359-382 PAX CABIN FLOOR STRUCTURE WITH ORIGINAL THICKNESS:0.020"" AND REMAINING THICKNESS: 0.018" THEREFORE IT IS WITH-IN LIMITS AND BTW STA 660-664 WITH ORIGINAL THICKNESS: 0.040" AND REMAINING THICKNESS: 0.028" THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-55-1A, 51-10-02-0G PAR 8 (F), AND DWG 9930538 REV BR. (LP #0313911)

Part: CUSP WEB — CORRODED (BS 188-313) · corrosion level 2 · airframe 44,187 hrs · 30,970 cycles

CORROSION ON CUSP WEB BTW STA Y 188\X=58, Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX. SUMMARY OF NRC 00650: CORROSION LEVEL 2. CUSP WEB BTW STA Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 FIG 201. BTW STA Y 188\ X=58 CORROSION WAS ACCOMPLISHED ON NRC 584. MINOR C. (LP #0312275)

Part: PAN — CRACKED (FWD CARGO) · airframe 44,187 hrs · 30,970 cycles

CRACK ON FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR. SUMMARY OF NRC 00246: FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0312268)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,668 hrs · 30,552 cycles

UPON ARRIVAL IN BDL, GATE AGENT REPORTED DENT IN L1 DOOR, FORWARD LOWER CORNER NEAR THE EDGE. APPRX 5 TO 6 INCH LONG BY 1 INCH DEEP. *** CONTRACT MAINTENANCE EVENT - OCM: 272623 *** INSPECTED DAMAGE AT 1L DOOR, NO CRACKS OR DAMAGE TO FASTENERS. PERFORMED REPAIR PER B717 SRM 52-00-00-2R PROCEDURE 3, STRAIGHTENED DOOR FLANGE, NO CRACKING OR STRETCHING OF DOOR FLANGE. NO EVIDENCE OF SHEARED RIVETS, ELONGATED HOLES, OR CRACKS. A/C OK FOR SERVICE. (LP #4996042)

Part: NONE — NONE · corrosion level 2 · airframe 39,592 hrs · 26,957 cycles

AFTER CORROSION REMOVAL IN RH SIDE PLATE BTW STA Y=946-Y=956 AT AFT CARGO COMPARTMENT, CARGO SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS IS: 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.031IN AND THEREFOR IT IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PAR 4 C (2) FIG. 103 (REF. NRC 00059). SUMMARY OF NRC 00167: CORROSION LEVEL 2, RH SIDE PLATE BTW STA Y=946-Y=956 AT AFT CARGO COMPARTMENT WAS REPAIRED PERMANENTLY PER ER/A 597529-14 REV. ORIGINAL AND PRI REV. 0 AND 1. ASSOCIATED ER/A 00-597529 ADDED FOR AC 9560. (LP #2136518)

Part: NONE — NONE · corrosion level 2 · airframe 39,594 hrs · 26,958 cycles

CORROSION ON INTERCOSTAL BTW Y=994 AND Y=1002, BTW L30 AND L29 RH (SM). SUMMARY OF NRC 00081: CORROSION LEVEL 2, INTERCOSTAL CORRECTIVE ACTION LOCATION PENDING. FOLLOW-UP DUE... "SUPPLEMENTAL INFORMATION": UPDATE DISCREPANCY COMMENT TO STATE: CORROSION ON INTERCOSTAL BTW Y=946 AND Y=954, BTW L30 AND L29 RH AT AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00081: CORROSION LEVEL 2, INTERCOSTAL BTW Y=946 AND Y=954, BTW L30 AND L29 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G PAR. 8.A. & SRM 51-41-02-0G PAR. 4. (LP #2133268)

Part: NONE — NONE · corrosion level 2 · airframe 39,592 hrs · 26,957 cycles

CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00028: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2130071)

Part: NONE — NONE · corrosion level 2 · airframe 39,592 hrs · 26,957 cycles

CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00029: CORROSION LEVEL 2. BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, AFT CARGO COMPARTMENT DOOR WERE REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2130074)

Part: NONE — NONE · airframe 39,592 hrs · 26,957 cycles

DUE TO THAT THE SAFETY PIN DOES NOT ALIGN WITH THE ESCAPE SLIDE L1, MCC REQUESTED TO REPLACE THE ESCAPE SLIDE. SUMMARY OF NRC 00154: FORWARD ENTRY EVACUATION SLIDE L1 WAS REPLACED. IT WAS VERIFIED PER B-717 IPC 25-61-01-01 FIGURE 01 (SHEET 001) ITEM 140J THEN MUST BE INSTALL WITH CARD 5211-4002. (LP #2130537)

Part: NONE — NONE · corrosion level 2 · airframe 39,592 hrs · 26,957 cycles

CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, FWD CARGO COMPARTMENT DOOR (C1). SUMMARY OF NRC 00030, CORROSION LEVEL 2: FWD LOWER SPLICE RETAINER AT LOWER DOOR JAMB, FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B-717 SRM 53-20-15-2R PROCEDURE 6. A DETAILED VISUAL INSPECTION WITH 10X MAGNIFYING LENS AT AFT LOWER SPLICE RETAINERS AT LOWER FWD CARGO DOOR JAMB WAS PERFORMED PER B717 SRM 51-10-04-0G PARAGRAPH 26 C.(2). AND NO CORROSION WAS FOUND. (LP #2122798)

Part: COVER — DEPARTED (TE FLAP) · airframe 38,138 hrs · 25,862 cycles

PART DEPARTED AIRCRAFT. ROUND ACCESS PANEL MISSING FROM LEFT WING INBOARD FLAP FAIRING COVER. INSTALLED ACCESS PANEL PER PS 900-7-3 NR 03. (LP #5156790)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 35,356 hrs · 23,856 cycles

EMERGENCY EXIT LENS WAS DAMAGED.

Part: DOOR — UNSECURE (AC BAY) · airframe 35,115 hrs · 23,681 cycles

GROUND AIR CONDITIONER DOOR FELL OFF. DEFERRED. WILL NEED A SUPPLEMENTAL SDR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,231 hrs · 22,301 cycles

BOTH AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPS CHECKED NORMAL IAW AMM 33-51.

Part: SKIN — CRACKED (BS 1022) · airframe 32,026 hrs · 21,386 cycles

CRACK ON SKIN BS 1022 BETWEEN LONGERONS 12 - 14R. REPAIRED IAW ETI-17-17-037 REV. 3, AND ER/A 556344-14 REV ORIGINAL.

Part: SKIN — CRACKED (BS 1076) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CRACK ON SKIN BS 1076 BETWEEN LONGERONS 12 - 14R. DAMAGED WAS REPAIRED IAW ETI-17-17-042 REV. 1 AND ER/A 556350-14 REV. ORIG.

Part: SKIN — CRACKED (BS 1087) · airframe 32,026 hrs · 21,386 cycles

CRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 14L. DAMAGED WAS REPAIRED IAW ETI-17-17-040 REV 1 AND ER/A 556347-14 REV. ORIG.

Part: ATTACH ANGLE — CRACKED (BS 1022) · airframe 32,026 hrs · 21,386 cycles

CRACKED LONGERON ATTACH ANGLE ON AFT LAVATORY SUPPORT BULKHEAD BS 1022, LONGERON 7L. DAMAGE WAS REPAIRED IAW ETI-17-17-045 REV. 1, AND ER/A 556351-14 REV. ORIG.

Part: SKIN — CRACKED (BS 1022) · airframe 32,026 hrs · 21,386 cycles

CRACK ON FUSELAGE SKIN BS 1022 BETWEEN LONGERONS 13 - 14L. THE DAMAGE WAS REPAIRED IAW ETI-17-17-038 REV 1, AND ER/A 556345-14 REV. ORIG.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 32,026 hrs · 21,386 cycles

SEVERAL ELONGATED HOLES ON VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. REPAIRED IAW SRM 55-30-01-2R-7, 51-41-01, AND 51-41-05.

Part: CARGO TRACK — CORRODED (BS 994-1022) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON THE RIGHT CARGO TRACK BETWEEN BS 994 - 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACEDIAW SRM 51-41-01, AND 51-40-08.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 32,026 hrs · 21,386 cycles

CRACKED BEAM NR 3, BS 160 BETWEEN UPPER & LOWER HINGE YOKE, FORWARD RIGHT GALLEY SERVICE DOOR STRUCTURE. THE BEAM WAS REPAIRED IAW SRM 52-00-00 2R.

Part: ACCESS PANEL — DAMAGED (WING) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

ELONGATED HOLES ON FUEL TANK ACCESS 620GB, 620JB, 620HB (REF CARD 001-0619:5720-2002/001 N/SE 00026) (AD). NR 00454: REPAIR ON FUEL TANK ACCESS 620GB, 620JB, 620HB WAS REPAIRED PER B717 SRM 57-10-01-2R-2 PAR 5B (3).

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON RUB STRIP OF ACCESS PANEL. THE RUB STRIP WAS REPLACED IAW SRM 57-10-01 2R-3.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON FUEL TANK ACCESS 620AT. FUEL ACCESS PLATE 620AT WAS REPLACED PER SRM 57-10-01.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,026 hrs · 21,386 cycles

CRACKED FWD EDGE BEAM NR 4 AT FWD SERVICE DOOR (R1)(DR). DAMAGE BEAM WAS REPLACED PER SRM 51-41-02 AND 51-41-05.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 32,026 hrs · 21,386 cycles

RIGHT WING HAS DENTS ON LWR SURFACE AT AFT FLAP MOVEABLE VANE. REPAIRED THE VANE IAW SRM 57-53-01-2R, REPAIR 1, PARAGRAPH 4A, FIGURE 201.

Part: FRAME — CRACKED (BS 1152) · airframe 32,026 hrs · 21,386 cycles

AFT ACCESORIES COMPARTMENT HAS A CRACKED ON FRAME ANGLE BS 1152 BETWEEN LONGERONS 1 & 3L. REPLACED IAW SRM 51-41-05.

Part: FRAME — CRACKED (BS 1144) · airframe 32,026 hrs · 21,386 cycles

AFT ACCESORIES BAY, CRACKED FRAME ANGLE BS 1144 BETWEEN LONGERONS 2 - 3L. THE ANGLE WAS REPLACED IAW SRM 51-41-05 AND DWG 9911840, REV CR.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 32,026 hrs · 21,386 cycles

CRACK ON UPPER CORNER FWD EDGE INNER PAN AT THE FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R, PROCEDURE 1, REPAIR 1.

Part: PAN — CRACKED (PAX DOOR) · airframe 32,026 hrs · 21,386 cycles

CRACKED PAN ON AFT EDGE NR 1 BEAM AT MAIN ENTRANCE DOOR. THE PAN WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-04, AND 51-41-05.

Part: FRAME — CRACKED (BS 660) · airframe 32,026 hrs · 21,386 cycles

CRACKED FRAME BS 660, LONGERONS 25 - 28L. THE FRAME WAS REPLACED IAW SRM 51-41-05, AND SRM 51-41-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON FUEL TANK ACCESS PANELS 520GB AND 520DT. THE FUEL ACCESS PANEL WERE REPLACED PER B717 SRM 57-10-01. (LP #2956805)

Part: FRAME — CRACKED (BS 706) · airframe 32,026 hrs · 21,386 cycles

CRACKED FRAME BS 706, LONGERONS 25 - 28R. FRAME REPAIRED IAW SRM 51-70-11-2R, REP 1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON FUEL ACCES PANEL 520CT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.

Part: BEAM — CRACKED (PAX DOOR) · airframe 32,026 hrs · 21,386 cycles

CRACKED AFT EDGE OF THE NR 1 BEAM AT THE MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7 FIG 201.

Part: FRAME — CRACKED (BS 1022) · airframe 32,026 hrs · 21,386 cycles

CRACKED FRAME ANGLE BS 1022, LONGERONS 13 - 14L. REPLACED IAW SRM 51-41-02, DWG 9912243, REV JS, AND REPAIRED IAW SRM 53-00-06-2R.

Part: DOOR FRAME — CRACKED (BS 45) · airframe 32,026 hrs · 21,386 cycles

CRACKS ON NLG DOOR FRAME LT AND RT BS 45. THE DOOR FRAMES WERE REPAIRED IAW SRM 53-10-14, REP 2, FIG 201.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 32,026 hrs · 21,386 cycles

CRACKED DOOR FRAME WEB BS 207, LONGERON 15L. . REPAIRED IAW SRM 53-10-15-2R-1.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 32,026 hrs · 21,386 cycles

DELAMINATION FLOOR PANEL 211 ANF AT COCKPIT. SN 00403 FLOOR PANEL 211 ANF AT COCKPIT WAS FABRICATED AND REPLACED PER SRM 53-20-50.

Part: STRUCTURE — CRACKED (FWD CARGO DOOR) · airframe 32,026 hrs · 21,386 cycles

FWD CARGO DOOR, A CRACK WAS FOUND ON THE FWD EDGE BETWEEN BEAMS 1 AND 2. REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

ELONGATED HOLES ON FUEL TANK ACCESS PANEL 520LB. REPAIRED THE ACCESS PANEL IAW SRM 57-10-01-2R-2 PAR. 5 B. (3).

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

ELONGATED HOLES ON FUEL TANK ACCESS PANEL 520CB. REPAIRED THE ACCESS PANEL IAW SRM 57-10-01-2R-2, PAR. 5 B. (3).

Part: FLOOR SUPPORT — CORRODED (BS 161-198) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON FLOOR SUPPORT FROM BS 161 - 198, RBL 44 IN THE PAX CABIN. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-04, PAR 26, 51-41-02, AND 51-41-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,026 hrs · 21,386 cycles

CRACK ON RT CUSP WEB STA Y=218 X=-45 (CPAX). DAMAGE WAS REPAIRED PER SRM 53-00-55 FIG 221 REPAIR 4, HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ALONG TRIM LINE PER NDT SPM 06-10-01.001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON LT CUSP WEB STA Y=549 BTW X=40 TO X=60. HFEC WAS ACCOMPLISHED ON LT CUSP WEB STA Y=549 BTW X=40 TO X=60, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55 2R REPAIR 4. PERFORM DECAL CONDITION INSPECTION EVERY "C" CHECK, PER TOPP 30-10-70 PAR (I), PAG 14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=130 TO Y= 148 X=-51 APPROX A COCKPIT. SUPPORT WAS REPLACED PER DWG 9936533 REV CM AND SRM 51-41-05 AND SRM 51-41-02.

Part: CUSP WEB — CORRODED (BS 530) · corrosion level 2 · airframe 32,026 hrs · 21,386 cycles

CORROSION ON LT CUSP WEB BS 530, LBL 40 - 60. REPAIRED IAW SRM 53-00-55 2R.

Part: PAN — CRACKED (BS 756-775) · airframe 32,026 hrs · 21,386 cycles

CRACK ON RING PAN , BS 756 AND 775. RING PAN WAS REPAIRED IAW SRM 56-20-02-2R.

Part: PAN — CRACKED (BS 636) · airframe 32,026 hrs · 21,386 cycles

CRACK ON RING PAN BS 636. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R.,

Part: BALLAST — FAILED (EMERGENCY LIGHTS) · airframe 32,022 hrs · 21,384 cycles

WHEN OVERHEAD AND SIDEWALL LIGHTS WERE TURNED ON DURING DESCENT, THE F/A OBSERVED FLICKERING AND A HOT BALLAST ODOR FROM FWD CABIN AREA. TURNED LIGHTS OFF AND ODOR DISSIPATED. FOUND A DAMAGED LIGHT L2-6607 CONNECTOR, IT ALSO HAD AN ELECTRICAL ODOR. DISCONNECTED THE LIGHT CONNECTOR AND REMOVED THE LAMP IAW ER/A 555702-14, REV ORIG. REPLACED THE BALLAST IAW AMM 33-21. OPS CHECKED NORMAL.

Part: STARTER — SMOKE (APU) · airframe 30,457 hrs · 20,257 cycles

FLIGHT EXPERIENCED SMOKE COMING FROM THE APU COMPARTMENT AFTER ARRIVAL. THE PASSENGERS DEPLANED NORMALLY THROUGH THE L1 DOOR. MAINTENANCE FOUND THE APU STARTER SMOKING AND GLOWING. MAINTENANCE USED THE GROUND BASED FIRE EXTINGUISHER TO SECURE APU COMPARTMENT. THE APU STARTER CB WAS PULLED IAW ER/A 549458-14, THE COMPARTMENT WAS CLEANED, AND APU MEL 49-10-01 WAS APPLIED. NO STRUCTURAL DAMAGE WAS FOUND. ACFT RELEASED FOR SERVICE WITH APU INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,185 hrs · 19,227 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING BATTERY PACK WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,371 hrs · 17,874 cycles

TAIL COMPARTMENT MOST FWD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LANYARD — MISSING (TAIL CONE) · airframe 25,839 hrs · 16,845 cycles

TAIL CONE LANYARD MISSING. INSTALLED LANYARD IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,839 hrs · 16,845 cycles

AFT OVERWING EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 25,839 hrs · 16,845 cycles

RIGHT ELEVATOR GEAR TAB CRACKED AT OTBD HINGE CUT OUT, LOWER SIDE. REPAIRED TAB IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

LEFT CUSP WEB CRACKED AT STATION 689, LBL 45. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

MAIN CABIN FRAME CRACKED AT BS 715, LBL 55. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,375 hrs · 17,875 cycles

MAIN CABIN FRAME CRACKED AT BS 715, LBL 55. R & R FRAME IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 813 - 832, RBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

CUSP WEB CRACKED AT BS 798, LBL 58. REMOVED CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 674, RBL 47. R & R CUSP WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,375 hrs · 17,875 cycles

MAIN CABIN FRAME CRACKED AT BS 674, RBL 55. R & R FRAME IAW DWG.

Part: DOOR — CRACKED (CARGO BAY) · airframe 25,839 hrs · 16,845 cycles

C-1 DOOR CRACKED ON AFT EDGE JUST ABOVE AFT LOWER LATCH CAM. REPAIRED DOOR IAW SRM & EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

MAIN CUSP WEB CRACKED AT BS 674, LBL 47. REPAIRED CUSP WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

MAIN CABIN, FRAME CRACKED AT BS 674, RBL 55. R & R FRAME IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

FORWARD CARGO COMPARTMENT DOOR CUT OUT CORRODED ON LOWER JAMB. R & R JAMB PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 25,839 hrs · 16,845 cycles

AFT PIT AT DOOR CUT OUT PAN CORRODED AROUND RIVNUTS. R & R PAN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,375 hrs · 17,875 cycles

RIGHT EMER FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,375 hrs · 17,875 cycles

LEFT EMER FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 27,202 hrs · 17,759 cycles

AFT GALLEY EMER LIGHT LENS COVER LOOSE. R & R COVER IAW MM.

Part: LANYARD — LOOSE (L2 DOOR) · airframe 26,823 hrs · 17,504 cycles

L2 DOOR EMER EVAC SLIDE PACK LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: LATCH — DIRTY (EVAC SLIDE) · airframe 26,675 hrs · 17,406 cycles

R1 DOOR EMER EVAC SLIDE LATCH DIRTY. CLEANED LATCH IAW SIP.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 26,484 hrs · 17,280 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

AFT PIT FWD BULKHEAD HORIZONTAL SUPPORT STRAPS CRACKED AT BS 817. R & R STRAPS IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

RT FWD PNEUMATIC "Y" DUCT SUPPORT ROD BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

AFT ACCESSORY COMPARTMENT FORMER SHEAR TIE CRACKED AT STATION 1152 STRINGER 2R. R&R CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

AFT ACCESSORY COMPARTMENT FRAME 1178 LT LOUVER ANGLE CRACKED. REPAIRED ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

FRAME CORRODED BETWEEN BS 908 TO BS 994, LONGERON 30. REPAIRED FRAME SECTION IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 24,298 hrs · 15,859 cycles

AFT PIT AT DOOR CUTOUT PAN CORRODED. R & R PAN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

LT WW FWD DOOR CUT OUT CLIP CRACKED. R & R CLIP IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

LONGERON CORRODED BETWEEN STATION 965 TO STATION 946 STRINGER 29L. R & R LONGERON IAW SRM.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 23,187 hrs · 15,150 cycles

R1 DOOR EMERGENCY EVAC SLIDE FAULTY. R & R SLIDE IAW AMM.

Part: PIN — MISSING (EVAC SLIDE) · airframe 23,187 hrs · 15,150 cycles

L1 DOOR EMERGENCY EVAC SLIDE MISSING SAFETY PIN. INSTALLED PIN IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,298 hrs · 15,859 cycles

FRAME CORRODED BETWEEN BS 908 TO BS 944, LONGERON 30. REPAIRED FRAME IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 23,187 hrs · 15,150 cycles

AFT PIT AT DOOR CUT OUT PAN CORRODED AROUND RIB NUTS. R & R JAMB PAN IAW SRM & MM.

Part: PANEL — CRACKED (RT WING) · airframe 23,187 hrs · 15,150 cycles

RT WING INBD BUTTE DOOR INBD END PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: DUCT — CRACKED (VERTICAL STAB) · airframe 239,120 hrs · 15,612 cycles

VERTICAL STABILIZER RAM AIR INLET DUCT CRACKED. REPAIRED DUCT IAW EA.

Part: COVER — MISSING (CABIN) · airframe 22,491 hrs · 14,724 cycles

ROW 28 EMERGENCY ASILE LIGHT COVERS MISSING (2 LIGHTS). REMOVED AND REPLACED ROW 28 STANDBY LIGHT HOUSINGS PER AMM.

Part: SLIDE — OUT OF ADJUST (TAILCONE) · airframe 21,246 hrs · 13,925 cycles

TAIL CONE EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 21,067 hrs · 13,810 cycles

FORWARD AISLE EMERGENCY LIGHTS INOP. SECURED CONNECTOR PER MM.

Part: LOCK — OBSTRUCTED (L1 DOOR) · airframe 20,986 hrs · 13,759 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LOCK BRACKET NOT SPRING LOADED PROPERLY- TO LOCK GIRT BAR IN ARMED POSITION. REMOVED DEBRY FROM LOCK PER AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,919 hrs · 13,718 cycles

FLOOR WEB SUPPORT CORRODED AT BS 174, BETWEEN RBL 12 TO RBL 40. REPAIRED WEB PER SRM.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR)

L1 DOOR GIRT BAR WILL NOT LOCK INTO PLACE. REMOVED DEBRIS OK FOR SERVICE REF AMM 25-60.

Part: SKIN PANEL — CRACKED (RT WING)

RT INBOARDD BENT-UP PANEL, CRACKED. ACCOMPLISHED BENT-UP PANEL REPLACEMENT PER B717 SRM 51-41-01 AND 741091-1.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 10 SEAT EMERGENCY ESCAPE LIGHT INOP. REMOVED AND REPLACED ROW 10 EMERGENCY LIGHT ASSY IAW B717 MM 33-51-04.

Part: COVER — MISSING (CABIN)

EMERGENCY LIGHT ON CEILING ROW 3 A/C RIGHT MISSING COVER. INSTALLED COVER ON EMERGENCY LIGHT AS REQUIRED.

Part: COVER — OUT OF POSITION (CABIN)

BUSINESS CLASS EXIT SIGN COVER FELL OFF. RE-SECURED EXIT SIGN COVER PER AMM 33-51.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH WHITE LIGHT INOP ON AISLE SIDE OF SEAT 1D. RELAMPED, OPS CHECK NORMAL. REF MM 33-51.

Part: ENGINE — MALFUNCTIONED (LEFT)

LOUD NOISE FROM LEFT ENGINE FOLLOWED BY COMPRESSOR STALL ALERT, THEN HIGH LEFT ENGINE TGT. REMOVED AND REPLACED NR 1 ENG ON W/O 208109 TASK CARD 603. AUTO LAND ACCOMPLISHED ON W/O 208109 TASK CARD 625.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201. SEE NR 3236 AND 1133.

Part: SLIDE — DISCHARGED (L1 DOOR)

1 LT DOOR SLIDE PACK PRESSURE GAUGE IN RED. R&R L1 DOOR SLIDE. NO DEFECTS NOTED AT THIS TIME. REF. MM 25-61.

Part: SLIDE — LOW PRESSURE (R-1 DOOR)

R1 DOOR SLIDE GAUGE IS IN THE RED. REMOVED AND REPLACED R-1 DOOR SLIDE REF B717 AMM 25-61.