N940AT

Part: PRESSURE SWITCH — FAULTED (FUEL SYS) · airframe 65,933 hrs · 47,395 cycles

ATB - RIGHT ENGINE SYSTEM FAIL MESSAGE ALONG WITH A RIGHT ENGINE FUEL FILTER MESSAGE ON CLIMB OUT. INSPECTED FILTERS WITH NO DEBRIS NOTED. BOTH HIGH AND LOW PRESSURE FILTERS REPLACED. FILTER DIFFERENTIAL PRESSURE SWITCH REPLACED. HIGH POWER RUN PERFORMED, OPS CHECK NORMAL.(7974762)

Part: PIN — MISSING (GIRT BAR) · airframe 65,719 hrs · 47,181 cycles

SPRING AND PIN MISSING FROM L1 GIRT BAR FLOOR FITTING (AFT ONE). REPLACED L1 CABIN EVACUATION SLIDE LATCH (AFT ONE) IAW CMM 25-60-02. (7585426)

Part: FASTENER — LOOSE (REPAIR) · airframe 64,255 hrs · 45,851 cycles

CRACK AND LOOSE FASTENERS (HI-LOCKS) ON EXTERNAL REPAIR DOUBLER ON STA Y=1022 AND BTW LONGERONS 13R/14R AT FUSELAGE WERE FOUND DURING REPETITIVE INSPECTION PER ER/A 577210-14 REV ORIGINAL SECTION II, STEP 1. SUMMARY OF NRC 00021: SKIN ON STA Y=1022 AND BTW LONGERONS 13R/14R AND CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R AT FUSELAGE WAS REPAIRED PER ER/A 577210-14 REV A SECTION I: PERMANENT REPAIR AND PRI 577210-14 REV 6. ASSOCIATED ER/A 14-577210 ADDED FOR AC 9501. (LP #0897457)

Part: SKIN — CRACKED (ZONE 200) · airframe 64,259 hrs · 45,856 cycles

CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R. SUMMARY OF NRC 00056: CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R WAS REPAIRED PER ER/A 625068-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND UNDER PRI 577210-14 REV 6. ASSOCIATED ER/A 14-625068 ADDED FOR AC 9501. (LP #0897470)

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 65,454 hrs · 46,915 cycles

AFTER REMOVAL OF INBOARD AND OUTBOARD BUSHINGS OF HINGES LOCATED AT XE= 206 AND XE= 223, CORROSION WAS FOUND ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND OUTBOARD LUG OF HINGE XE= 206. CORRECTIVE ACTION: CORROSION ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND OUTBOARD LUG OF HINGE XE= 206. WAS REAPAIRED PER PRI 625435-14 REV 2 & ER/A 625435-14 REV ORIGINAL. (0895866)

Part: LONGERON — CRACKED (ZONE 200) · airframe 64,253 hrs · 45,850 cycles

CRACK LONGERON 4LH & STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00090: LONGERON 4LH BTW STA Y=1169 AND STA Y=1138 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0883561)

Part: SKIN — DENTED (ZONE 800) · airframe 64,253 hrs · 45,850 cycles

SEVERAL DENTS ON EXTERNAL SKIN OF FWD CARGO DOOR. SUMMARY OF NRC 00025: EXTERNAL SKIN OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8. PERFORM AN EXTERNAL GVI OF THE REPAIR DOUBLERS ON FWD CARGO DOOR EVERY C-CHECK PER B717-200 SRM 52-00-01-2R, PROCEDURE 8, REPAIR 8, PAR 6, A, TABLE 203. (LP #0878858)

Part: RELEASE MECH — OUT OF ADJUST (ZONE 100) · airframe 64,255 hrs · 45,851 cycles

THE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. 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 00166: TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER B717 AMM 53-52-03 AND WAS VERIFIED AND INSTALLED CORRECTLY POSITION OF RELEASE PER B717 AMM 53-52-01. (LP #0871358)

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,253 hrs · 45,850 cycles

CORROSION ON INTERCOSTALS (2 EA) AND INTERNAL DOUBLER BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT. SUMMARY OF NRC 00077: CORROSION LEVEL 2. REPAIR DOUBLER WAS REPLACED PER DWG 9923686-25 REV D, PER B717 SRM 51-41-02-0G AND 51-41-05-0G. CORROSION WAS REMOVED ON INTERCOSTALS (2 EA) BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT PER B717 SRM 51-10-04-0G PAR 26 C. INTERCOSTALS (2 EA) BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT ORIGINAL THICKNESS OF 0.050IN AND REMAINING THICKNESS IS 0.042IN AND THEREFORE THIS AREA IS WITHIN LIMINTS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 C FIG 103 AND DC-MD/BOEING NDT SPM PART 4, 04-00-06 PAR 4 FIG 9. (LP #0870650)

Part: WIRE — DAMAGED (ZONE 200) · airframe 63,686 hrs · 45,372 cycles

SHIP 9501 -ATB/FUME- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO AN ACRID BURNING SMELL IN THE CABIN. CORRECTIVE ACTION: MAINTENANCE REPAIRED DAMAGED WIRES AND RING TERMINALS AT THE SERVICE DOOR OVERHEAD LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (LP #6556652)

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 63,682 hrs · 45,367 cycles

SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE NEAR FWD SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT AT CANNON PLUG P1-259 PER B717 AMM 22-51. OPERATIONAL CHECK WAS GOOD. (LP #6556658)

airframe 63,655 hrs · 45,340 cycles

SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC GOING INTO ATL DUE TO "PSEU FAIL" MESSAGE AND THE RESULTANT FLAPS-UP LANDING AS PER THE QRH. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT SLAT A SENSOR WIRES TO BE SHORTED TO GROUND. THE WIRE WAS REPLACED AND A VERIFICATION FLIGHT WAS PERFORMED. OPERATIONAL CHECK WAS GOOD. (LP #6556630)

Part: SENSOR — INOPERATIVE (LT SLAT SENSOR A) · airframe 63,648 hrs · 45,333 cycles

SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED EMERGENCY WITH ATC INTO CHA DUE TO THE "PSEU FAIL" MESSAGE. A FLAPS-UP LANDING FOLLOWED PER THE QRH. CORRECTIVE ACTION: MAINTENANCE PERFORMED BITE OF THE PSEU WHICH RETURNED CODES 326029 (PSEU INTERNAL FAULT INTERMITTENT) AND CODE 326089 (LT SLAT SENSOR A FAULT INTERMITTENT). THE PSEU AND LT SLAT SENSOR A WERE BOTH REPLACED. MAINTENANCE ALSO REPLACED THE LANDING GEAR POSITION INDICATOR AS A PRECAUTION. OPERATIONAL CHECK WAS GOOD. (LP #6556622)

Part: NONE — NONE (NONE) · airframe 63,682 hrs · 45,367 cycles

-AD- ACCOMPLISH ER/A 539703-14AD REV A SEC II. ACCOMPLISH ER/A 539703-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-539703 ADDED FOR AC 9501. **REDEFFERED LOG TO QC, ESTABLISHED MONITOR INSP** C/W ER/A 539703-14AD REV B SECTION 2. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 03DEC24 AND LOG COMMENTS. (LP #0671339)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 63,273 hrs · 45,006 cycles

THE OVERHEAD EMERGENCY EGRESS LIGHTS ARE INOPERATIVE FROM ROW 24 THROUGH TO ROW 29. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT 25DEF (B5-231) PER B717 AMM 33-51. CHECK IS GOOD. (LP #6103393)

Part: LENS — MISSING (ZONE 200) · airframe 63,273 hrs · 45,006 cycles

THE OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER IS MISSING AT 25/26DEF. DEFERRED 25/26DEF OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER PER NEF 33-51-02. DEFERRAL REMARKS NOTED. MAINTENANCE REPLACED THE MISSING COVER ASSEMBLY REF B717 AMM 33-51. THIS ACTION CLEARS NEF 33-51-02. DEFERRAL REMARKS NOTED. (LP #0596013)

Part: SKIN — PUNCTURED (BS 256 L17-18L) · airframe 62,784 hrs · 44,586 cycles

ON WALKAROUND FOUND PUNCTURE IN SKIN AT STATION Y256 BETWEEN LONGERONS L18 AND L17. REMOVED THE PUNCTURED REPAIR SKIN AT FR 229-FR245 BETWEEN STGR L16L & L18L PER B717 SRM 51-40-02. C/W HFEC OF DAMAGED AREA. NO CRACK INDICATIONS. FABRICATED AND INSTALLED SKIN REPAIR IN REF B717 SRM 53-00-01-2R. CONT ON LG PG 5144739. INSTALL COMPLETE ALL RII C/W. (LP #5144734)

Part: CONNECTOR — DIRTY (TAILCONE) · airframe 62,189 hrs · 44,061 cycles

SHIP 9501 -MISC/DE- THE "TAILCONE UNLOCK" MASTER CAUTION ILLUMINATED THREE TIMES DURING FLIGHT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY ATC FOR THE CREW. EWR MAINTENANCE CLEANED THE CONNECTOR PLUGS OF BOTH THE INTERNAL AND EXTERNAL TAILCONE UNLOCK SWITCHES. THE DCU WAS ALSO REPLACED PER AMM 31-43. THE OPERATIONAL TEST WAS GOOD. THE "TAILCONE UNLOCKED" MASTER CAUTION MESSAGE HAS NOT RETURNED. THE AIRCRAFT IS OK FOR SERVICE. NO THIRTY DAY HISTORY. (LP #5287624)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,653 hrs · 43,605 cycles

SHIP 9501 -MISC/DE- AT 13K, THE F/A REPORTED A STRONG ELECTRICAL SMELL COMING FROM FORWARD GALLEY. COCKPIT FLIGHT CREW ALSO SMELLED IT AND DONNED O2 MASKS. SOON AFTER, IT WAS ALSO REPORTED TO BEING SMELLED IN THE TAIL AS WELL. ODOR WAS GONE BY 6K IN THE DECENT. NO INDICATION OF WHERE IT WAS COMING FROM. CORRECTIVE ACTION: MAINTENANCE RAN ALL COFFEE MAKERS AND THE OVEN. OPERATED ALL ELECTRICS AND ALL LIGHTS IN CABIN AND COCKPIT. PERFORMED DUCT BURNOUT USING ALL 3 BLEED SOURCES, WITH THE ISOLATION OF EACH. NO UNUSUAL ODOR FOUND. REPLACED BOTH COALESCER BAGS REF B717 AMM 21-54. COMPLIED WITH ALL NO-GO ODI PROCEDURES. AIRCRAFT IS OK FOR SVERVICE. (LP #4479732)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,418 hrs · 43,408 cycles

THE GATE AGENT COULD NOT OPEN THE MAIN CABIN DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE BRACKET, THAT THE DOOR HANDLE MOUNTS TO, WITH THREE BOLTS LOOSE AND ONE BOLT MISSING. THE LOOSE BOLTS WERE SECURED AND THE MISSING BOLT WAS INSTALLED. HANDLE IS NO LONGER SLOPPY AND OPENS SMOOTHLY REF B717 AMM 52-11. AIRCRAFT OK FOR SERVICE. (LP #4294386)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 27L AND 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 27L AND 27R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR. 8. (LP #2765742)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

AFTER REMOVING DOUBLER, CORROSION WAS FOUND ON TEE CAP AFT PRESSURE GROUP BULKHEAD FORWARD FACE LOWER SECTION STA=1053 BTW LONGERON 25R AND 28R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00181: CORROSION LEVEL II. TEE PRESURE DOME ON STA 1053 WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND 51-41-02-0G PAR 8. A. (LP #2761165)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

CORROSION ON WEB AFT FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00115: CORROSION LEVEL II. WEBS #9915561-53 AND #9915561-3 WERE REPLACED PER DOUGLAS DWG 9915561 REV CG AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G, PAR. 8. (LP #2759696)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

CORROSION AT END LONGERON CLIPS STA 1032 (5 EA), 27RH, 28RH, 29RH, 28LH, AND 26RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00176: LEVEL CORROSION 2. END LONGERON CLIPS #26RH, #27RH, #28RH, AND #28LH WERE REPLACED PER B-717-200 SRM 51-40-08-0G AND END LONGERON #29RH WAS ATTENDED WHITHIN NRC 0211. (LP #2758403)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

CORROSION WAS FOUND ON FITTING END OF LONGERON 23 RH STA 1053 AFT CARGO COMPARTMENT. SUMMARY OF NRC 00185: LEVEL CORROSION II. FITTING (END LONGERON) ON LONGERON 23 RH STA 1053 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-40-08-0G. (LP #2757963)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,201 hrs · 42,337 cycles

CORROSION ON AFT PRESSURE BULKHEAD DOME WEB FORWARD FACE LOW AREA STA Y=1053 BTW LONGERON 29L AND 28R AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS OF 0.063IN AND REMAINING THICKNESS OF 0.045IN,.THE AREA REWORKED IS OUT OF LIMITS PER B717-200 SRM 53-20-08-2R PROCEDURE 2 PAR. 4.A.(1)(B). SUMMARY OF NRC 00195: CORROSION LEVEL 2. AFT PRESSURE BULKHEAD DOME WEB FORWARD FACE LOW AREA STA Y=1053 BTW LONGERON 29L AND 28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20 -08-2R-7, FIG. 201. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP MANUAL 30-10-70 PAR. I PAGE. 14. (LP #2746618)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,201 hrs · 42,337 cycles

IN REFERENCE NRC 0014: AFTER DOOR STOP #3 REMOVAL, CRACK WAS FOUND BELOW AFT EDGE OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00171: PAN OF AFT EDGE OF AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8. PAR 4.A.(1). FIGURE 201. DETAIL V-V. (LP #2723081)

Part: NONE — NONE · corrosion level 2 · airframe 59,144 hrs · 41,414 cycles

LEFT HAND WING UPPER SURFACE HAS CORROSION AT XRS 310 STR 6. MAINTENANCE SMOOTHED AND BLENDED THE CORROSION ON THE LFT HAND WING AT XRS 315 STR 6 PER B717 SRM 57-10-01. MEASURED AREA AFTER BLENDOUT PER B717 SRM 57-10-01-1A-1 FIG 105 SHEET 3 AND FOUND AREA AT XRS 315 STR 6 TO BE OUT OF LIMITS PER B717 SRM 57-10-01-1A-1 FIG 106 SHEET 4. ACCOMPLISHED HFEC OF BLENDED AREA PER MDC 93K0393 NDT SPM PART 06-10-01.001 NO DEFECTS NOTED. ALSO ACCOMPLISHED UT REMAINING THICKNESS MEASUREMENT PER MDC 93K0393 NDT SPM PART 04- 00-06. INSPECTION RESULTS PROVIDED TO ENGINEERING FOR EVALUATION. ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR STEPS 1-7 PER ER/A 602582-14 REV A SHEET 2. ASSOCIATED ER/A 14-602582 ADDED FOR AC 9501. (LP #2435747)

Part: NONE — NONE · airframe 59,120 hrs · 41,391 cycles

FOUND ROW 21 LEFT AND RIGHT OVER WINDOW EXIT SIGN LIGHTS INOPERATIVE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY PACK B5-230 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD AND ALL LIGHTS ILLUMINATE. AIRCRAFT OK FOR SERVICE. (LP #9098652)

Part: NONE — NONE · airframe 58,020 hrs · 40,375 cycles

NLG RETRACT SCISSORS LINK BOLT COTTER KEY CUT INTO CENTER LT SUPPORT WEB IN RETRACT POSITION (FOUND ON FREE FALL). NO ALLOWABLE DAMAGE PER B717 SRM. REMOVED DAMAGED SUPPORT WEB. FABRICATED, DRILLED, AND INSTALLED STIFFENERS ON NEW SUPPORT WEB. TREATED, PRIMED, & PAINTED SUPPORT WEB. INSTALLED SUPPORT WEB PER BOEING DWG 9911599 & B717 SRM 51-40. (LP #2160264)

Part: SKIN — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 56,150 hrs · 38,743 cycles

CORROSION ON INNER SKIN STA 966-977 AT AFT CARGO DOOR CUTOUT. REPAIRED PER ER/A 591210-14 REV ORIG ON NON-ROUTINE CARD 271. (LP #1793130)

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 56,150 hrs · 38,743 cycles

THE AFT CARGO DOOR JAMB IS CORRODED ALONG LOWER EDGE. MARKED. REPLACED C2 DOOR JAMB PAN PER B717 SRM 51-41-00. AFT CARGO DOOR JAM PAN WAS TRIMMED, DRILLED, PAINTED, AND INSTALLED PER B717 SRM 53-20-15-2R. ALL WORK ABOVE ACCOMPLISHED BY B717 RII QUALIFIED INSP. REF NRC 24, C CHK. ATL. (LP #1790850)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,072 hrs · 38,680 cycles

THE OVERHEAD EMERGENCY LIGHTS AT ROW 15-18 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-120 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7576411)

Part: BATTERY — MISSING (EXTERIOR LIGHTS) · airframe 55,778 hrs · 38,454 cycles

FOUND CARGO EMERGENCY EXTERIOR LIGHTS POWER SUPPLY BATTERY MISSING. REPLACED BATTERY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #7614440)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,778 hrs · 38,454 cycles

THE EMERGENCY LIGHT IN THE AFT TAIL COMPARTMENT IS MISSING THE LENS. MAINTENANCE INSTALLED THE LENS ON THE EMERGENCY VENTRAL LIGHT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7614434)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 55,538 hrs · 38,257 cycles

THE EMERGENCY LIGHT BATTERY POWER SUPPLY IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, REF B717 AMM 33-51-03.

Part: RELEASE MECH — INOPERATIVE (TAILCONE) · airframe 53,102 hrs · 36,439 cycles

MAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM DOOR TAPED SHUT WITH THE DECAL. DURING REMOVAL, THE TAIL CONE WAS DEPLOYED, BUT THE SLIDE DID NOT DEPLOY. MAINTENANCE THEN FOUND THE LANYARD BROKEN ON THE DEPLOYED TAIL CONE AND REPLACED THE TAIL CONE WITH A NEW ONE PER AMDS WORK CARD# 5352-4013. (LP #5287658)

Part: DOOR FRAME — CORRODED (BS 954-985) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION ON LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT (C2). NRC 00238: CORROSION LEVEL2, LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R-7.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION ON LOWER/RH FWD FACE AT DOOR JAMB VENTRAL DOOR. CORROSION LEVEL2, LOWER/RH FWD FACE AT VENTRAL DOOR JAMB WAS REPAIRED PER ETI-17-19-052 REV. 3 AND ER/A 577238-14 REV. ORIGINAL.

Part: SKIN — CRACKED (BS 1076) · airframe 53,095 hrs · 36,435 cycles

CRACK AT FUSELAGE SKIN STA 1076 LONG 14 LH. (FUS). NRC 00568: FUSELAGE SKIN STA 1076 LONG 14 LH WAS REPAIRED PER ETI-17-19-053 REV. 2 AND ER/A 577167-14 REV. ORIGINAL. ASSOCIATED ER/A 14-577167 ADDED FOR AC 9501. (LP #1028464)

Part: HINGE — DAMAGED (LT WING TE FLAP) · airframe 53,095 hrs · 36,435 cycles

FREE PLAY DUE TO ELONGATED HOLES AT OUTBOARD FLAP HINGE LH WING (AI). LH OUTBOARD FLAP HINGE WAS REPAIRED PER ETI-17-19-059 REV 2. AND ER/A 577279-14 REV. ORIGINAL. FREE PLAY WAS CORRECTED.

Part: SKIN — CRACKED (BS 1022) · airframe 53,095 hrs · 36,435 cycles

FOUND 2 CRACKS IN FUSELAGE SKIN AT STA 1022 LONG 14 RH. (FUS). NRC 00569: FUSELAGE SKIN STA 1022 LONG 14 RH WAS REPAIRED PER ETI-17-19-051 REV 3 AND ER/A 577210-14 REV. ORIGINAL. ASSOCIATED ER/A 14-577210 ADDED FOR AC 9501. (LP #1028458)

Part: SKIN — CRACKED (BS 1087) · airframe 53,095 hrs · 36,435 cycles

CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14RH. (FUS). NRC 00571: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14RH WAS REPAIRED PER ETI-17-19-056 REV. 2 AND ER/A 577171-14 REV. ORIGINAL. ASSOCIATED ER/A 00-577171 ADDED FOR AC 9501.

Part: CARGO TRACK — CORRODED (BS 588-655) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

EXCESSIVE CORROSION AT FWD CARGO COMPARTMENT RH TIE TRACK BETWEEN STA 588/655 IN REF NRC 00264. (CCD). NRC 00612: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER B717- 200 SRM 51-41-01 AND 51-41-02 0G.

Part: GUSSET — CRACKED (PYLON SUPPORT) · airframe 53,095 hrs · 36,435 cycles

CRACK ON GUSSET AFT FACE OF ENGINE PYLON SUPPORT BULKHEAD AND LONG 7LH AT PAX CABIN. NRC 00377: GUSSET WAS REPAIRED PER ETI-17-19-048 REV.2 AND ER/A 577138-14 REV. ORIGINAL. (LP #1024147)

Part: FITTING — CRACKED · airframe 53,095 hrs · 36,435 cycles

CRACK ON RIGHT MAIN FRAME WING TO FUSELAGE FITTING, LONGERON NUMBER 22. NRC 00464: FITTING WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP #1023991)

Part: GUSSET — CRACKED (PYLON) · airframe 53,095 hrs · 36,435 cycles

CRACK ON GUSSET AFT FACE OF ENGINE PYLON SUPPORT BULKHEAD AND LONG 7RH AT PAX CABIN. NRC 00376: GUSSET WAS REPAIRED PER ETI-17-19-048 REV. 2 AND ER/A 577138-14 REV. ORIGINAL. ASSOCIATED ER/A 00-577138 ADDED FOR AC 9501. (LP #1024144)

Part: FLOOR SUPPORT — CORRODED (BS 1022-1076) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION AT FLOOR SUPPORT ELEMENTS BETWEEN STA 1022/1076 AND X-22 (W2) IN REF NRC 00537. NRC 00574: CORROSION LEVEL 2, FLOOR SUPPORT WAS OUT OF LIMITS BETWEEN STA 1022/1076 AND X-22 AND WAS REPLACED PER B-717-200 SRM 51-41-01 AND DWG #9936656 REV. AM. (LP #1022599)

Part: SKIN — CORRODED (BS 1037) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION AT FUSELAGE SKIN SPLICE STA 1037 BETWEEN LONG 18/20RH. (W2). NRC 0538: CORROSION LEVEL 2, WAS DETERMINED TO BE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A FIGURE 103 (SHEET1). SKIN SPLICE STA 1037 BETWEEN LONG 18/20RH WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1022289)

Part: FITTING — CRACKED (BS 954) · airframe 53,095 hrs · 36,435 cycles

CRACK ON INNER FITTING STA Y=954 AND BEAM #3. AFT CARGO COMPARTMENT(FYT). NRC 00604: INNER FITTING STA Y=954 AND BEAM #3 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 DWG #3914025 REV. C AND B717-200 SRM 51-41-05-0G. (LP #1020512)

Part: LONGERON — CRACKED (BS 1037) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 13RH AT STA 1037 (CPAX). NRC 00498: LONGERON 13RH AT STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1020787)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 5RH AT STA 1022. (CPAX). NRC 00494: LONGERON 5RH AT STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1021073)

Part: FORMER — CRACKED (BS 715) · airframe 53,095 hrs · 36,435 cycles

CRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37.(FYT). NRC 00594: FORMER RH SIDE STA Y=715 AND X=-37 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019506)

Part: FORMER — CRACKED (BS 655) · airframe 53,095 hrs · 36,435 cycles

CRACK ON KEEL BEAM FORMER RH SIDE STA Y=655 AND X=-21. FORMER RH SIDE STA Y=655 AND X=-21 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019497)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 16LH AT STA 1022 (CPAX). NRC 00493: CRACK ON LONGERON 16LH AT STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1019714)

Part: FORMER — CRACKED (BS 655) · airframe 53,095 hrs · 36,435 cycles

CRACK ON KEEL BEAM FORMER LH SIDE STA Y=655 AND X=21.(FYT). NRC 00593: FORMER LH SIDE STA Y=655 AND X=21 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1019503)

Part: KEELBEAM — CRACKED (BS 696) · airframe 53,095 hrs · 36,435 cycles

CRACK ON KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30.(FYT). NRC 00590: FORMER LH SIDE STA Y=696 AND X=30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1. (LP #1018524)

Part: KEELBEAM — CRACKED (BS 696) · airframe 53,095 hrs · 36,435 cycles

CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30.(FYT). NRC 00591: FORMER RH SIDE STA Y=696 AND X=-30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 53,095 hrs · 36,435 cycles

HOLE ON FLOOR PANEL 211ANF AT COCKPIT (CPIL). NRC 00598: FLOOR PANEL 211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B717-200 SRM 53-20-50 2R REP.3. (LP #1015597)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION IN ACCESS #520FT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK LEFT. (AI). NRC 00565: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUND OUT OF LIMITS, AND ACCESS PLATE #520FT WAS REPLACED PER B-717/200 SRM 57-10-01 REPAIR 2 PAR. 5 A. (CONDITION III) TABLE 201 AND PAR.5 D. PART NUMBER WAS VERIFIED PER B717-200 IPC 57-22-01-01. (LP #1013975)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #520DB AT FUEL TANK LEFT. (AI). NRC 00576: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #520DB AT SETTLEMENT AND COUNTERSINK HOLES AREAS WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUND OUT OF LIMITS PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 A. (CONDITION III) TABLE 201 AND PAR.5 D., AND WAS REPLACED. PART NUMBER WAS VERIFIED PER B717-200 IPC 57-23-01-01. (LP #1013964)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 6RH AT STA 1022. (CPAX). NRC 00495: LONGERON WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1014048)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION IN ACCESSES 520CT AND 620CT ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK. (AI) (AD). NRC 533: CORROSION LEVEL 2, ACCESS PLATES 520CT AND 620CT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. (LP #1013646)

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION ON COUNTERSUNK AND SETTLEMENT ON FUEL ACCESS PLATE #620FT AT FUEL TANK RIGHT. (AD). NRC 00577: CORROSION LEVEL 2, CORROSION ON FUEL ACCESS PLATE #620FT AT SETTLEMENT AND COUNTERSINK HOLES AREA WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26, WAS FOUND OUT OF LIMITS PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 A. (CONDITION III) TABLE 201 AND PAR.5 D., AND WAS REPLACED. PART NUMBER WAS VERIFIED PER B717-200 IPC 57-22-01-01. (LP #1013966)

Part: LONGERON — CRACKED (BS 1022) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 8RH AT STA 1022. (CPAX). NRC 00497: LONGERON WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1014057)

Part: CUSP WEB — CORRODED (BS 889-896) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION OUT OF LIMITS AT PASSENGER CABIN CUSP WEB BETWEEN BS 889-896 X-54/X-60. IN REF NRC 00309. NRC 00582: CORROSION LEVEL 2, CUSP WEB BETWEEN STA 889-896 X-54/X-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #1012536 )

Part: SEAT TRACK — CRACKED (BS 715) · airframe 53,095 hrs · 36,435 cycles

CRACK ANGLE STA Y=715 AND X=-43 BELOW SEAT TRACK AT WING BOX. NRC 00345: ANGLE STA Y=715 AND X=-43 WAS REPLACED PER B717-200 SRM 51-41-05. (LP #1012333)

Part: CUSP WEB — CORRODED (BS 862-870) · corrosion level 2 · airframe 53,095 hrs · 36,435 cycles

CORROSION OUT OF LIMITS AT PASSENGER CABIN CUSP WEB BETWEEN STA 862-870 X-54/X-60. IN REF NRC 00309. NRC 00581: CORROSION LEVEL 2, CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4- FIG. 211, 51-41-02-0G, AND 51-41-05-0G. (LP #1012544)

Part: PAN — CRACKED (CARGO DOOR) · airframe 53,095 hrs · 36,435 cycles

CRACK PAN ON LOWER FWD CORNER AT FWD CARGO COMPARTMENT DOOR (CCD). NRC 00364: CRACK PAN ON LOWER FWD CORNER WAS REPAIRED PER B717-200 SRM 52-30-02-2R-1. (LP #1011692)

Part: CUSP WEB — CORRODED (BS 775) · airframe 53,095 hrs · 36,435 cycles

CRACK ON CABIN FLOOR CUSP WEB AT STA 775 X=57 (CPAX). NRC 00302: CUSP WEB AT STA 775 X=57 WAS REPAIRED PER B717-200 SRM 53-00-55-2R FIG. 206. (LP #1012553)

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

CRACK ON FITTING STA Y=737 AND X=-44 BELOW SEAT TRACK AT WING BOX. NRC 00344: FITTING STA Y=737 AND X=-44 WAS REPLACED PER SRM 51-41-05. (LP #1008181)

Part: PAN — CRACKED (CARGO DOOR) · airframe 53,095 hrs · 36,435 cycles

CRACK PAN ON UPPER AFT CORNER AT FWD CARGO COMPARTMENT DOOR(CCD). NRC 00239: CRACK PAN ON UPPER AFT CORNER AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER SRM 52-30-02-2R-1. (LP #1007668)

Part: PAN — CRACKED (CARGO DOOR) · airframe 53,095 hrs · 36,435 cycles

CRACK PAN ON BEAM 5 CORNER AT FWD CARGO COMPARTMENT DOOR(CCD). NRC 00412: CRACK PAN ON BEAM 5 CORNER AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER SRM 52-30-02-2R-1. (LP #1007676)

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

CRACK ON FITTING STA Y=737 AND X=44 BELOW SEAT TRACK AT WING BOX. NRC 00343: FITTING STA Y=737 AND X=44 WAS REPLACED PER SRM 51-41-05. (LP #1006757)

Part: DOUBLER — WORN (EMERGENCY EXIT) · airframe 53,095 hrs · 36,435 cycles

WEAR PRODUCTION DOUBLER ON RT LOWER CORNER OF THE AFT PRESSURE BULKHEAD EMERGENCY EXIT DOOR (FUS). NRC 00426: PRODUCTION DOUBLER ON RT LOWER CORNER OF THE AFT PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER SRM 52-10-02-2R PROCEDURE 16 OPTION 1. (LP #1005139)

Part: PAN — WORN (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

WEAR ON PAN AT LT LOWER CORNER OF THE AFT PRESSURE BULKHEAD EMERGENCY EXIT DOOR (FUS). NRC 00425: PAN ON LT LOWER CORNER OF THE AFT PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER SRM 52-10-02-2R-15 PROCEDURE 15, REPAIR 15, FIG 201. (LP #1005138)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

CRACK ON LONGERON 6L AT STA 1022 (CPAX). NRC 00492: LONGERON 6L AT STA 1022 WAS REPAIRED PER SRM 53-00-05-2R REPAIR 2. (LP #1005133)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

CRACKED LONGERON 8L AT STA 1022 (CPAX). NRC 00491: LONGERON 8L AT STA 1022 WAS REPAIRED PER SRM 53-00-05-2R REPAIR 2. (LP #1003666)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

CRACK ON CABIN FLOOR CUSP WEB FROM 275 TO 294 X=-58 (CPAX). NRC 00357: CUSP WEB FROM 275 TO 294 X=-58 WAS REPAIRED PER SRM 53-00-55-2R PROCEDURE 4 FIG. 215. (LP #1003405)

Part: CUSP WEB — CANNING (FUSELAGE) · airframe 53,095 hrs · 36,435 cycles

INITIAL INSPECTION: OIL CANNING ON CABIN FLOOR CUSP WEB BTW STA 665/674 LT. WEB WAS REPAIRED PER SRM 53-00-55-2R-4. (LP1002124)

Part: PAN — CRACKED (CABIN) · airframe 53,095 hrs · 36,435 cycles

INITIAL INSPECTION: CRACK ON UPPER/FWD RING PAN STA Y=756 RT SIDE AT PAX CABIN. UPPER/FWD RING PAN STA Y=756 RT SIDE AT PAX CABIN WERE REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, TYPE B. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON UPPER/FWD RING PAN STA Y=756 RT SIDE AT PAX CABIN, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10- 01.001 (LP1000621)

Part: PAN — CRACKED (CABIN) · airframe 53,095 hrs · 36,435 cycles

INITIAL INSPECTION: CRACK ON UPPER/AFT RING PAN STA Y=832 RT SIDE AT PAX CABIN. UPPER/AFT RING PAN STA Y=832 RT SIDE AT PAX CABIN WERE REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, TYPE B. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON UPPER/AFT RING PAN STA Y=832 RT SIDE AT PAX CABIN, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10- 01.001. (LP1000585)

Part: PAN — CRACKED (CABIN) · airframe 53,095 hrs · 36,435 cycles

INITIAL INSPECTION: CRACK ON UPPER/FWD RING PAN STA 636 LT SIDE AT PAX CABIN. UPPER/FWD RING PAN STA 636 LT SIDE AT PAX CABIN WERE REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, TYPE B. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON UPPER/FWD RING PAN STA 636 LT SIDE AT PAX CABIN, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10-01.001. (LP1000455)

Part: PAN — CRACKED (CABIN) · airframe 53,095 hrs · 36,435 cycles

INITIAL INSPECTION: CRACK ON LOWER/FWD RING PAN STA Y= 541, 655, 794 AND 889 LT SIDE AT PAX CABIN. LOWER/FWD RING PAN STA Y= 541, 655, 794 AND 889 LT SIDE AT PAX CABIN WERE REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, TYPE B. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LOWER/FWD RING PAN STA Y= 541, 655, 794 AND 889 LT SIDE AT PAX CABIN, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10-01.001. (LP1000458)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,562 hrs · 36,049 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND THE MID EXIT ROW EMERGENCY SIGN LIGHT AT ROW 20 TO BE INOPERATTIVE. MAINTENANCE REPLACED THE BATTERY PACKS B5-230 AND B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5243255)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,086 hrs · 35,736 cycles

DURING CARGO CONDITION CK - FOUND C1 DOORWAY LWR AFT SHIM LIKE METAL PIECE CORODED. REMOVED CORRODED SPLICE & LOWER STAINLESS STEEL TRIM PLATE PER PRI 572183. 725013. INSTALLED SPLICE AND LOWER EXTERNAL SCUFF PLATE PER PRI 572183-14 AND DAC DWG 5910142. OK FOR SERVICE. (LP4254604)

Part: OVEN — SMOKE (GALLEY) · airframe 51,342 hrs · 35,246 cycles

OVEN NR 1 SMOKING ACCORDING TO FA. TURNED IT OFF. R&R GALLEY OVEN PER AMM 25-35. OP CHKS NORMAL.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 49,420 hrs · 33,874 cycles

DISBONDING WAS FOUND ON DENTS AT THE INBD FIXED FLAP VANE LOWER SKIN XRS=137 OF THE RT WING. REPAIRED IAW SRM 57-53-01-2R-1.

Part: VANE — DEBONDED (LT WING TE FLAP) · airframe 49,420 hrs · 33,874 cycles

THREE DISBONDS WERE FOUND AT OTBD FLAP FIXED VANE UPPER SURFACE OF THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1, AND JIC 5552700.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 49,420 hrs · 33,874 cycles

DISBOND WAS FOUND ON DENTS AT AFT MOVABLE FLAP VANE LOWER SURFACE, ON THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1.

Part: RUB STRIP — CRACKED (RT WING) · airframe 49,420 hrs · 33,874 cycles

CRACK ON THE RT WING LEADING EDGE AILERON RUBSTRIP UPPER SURFACE XRS 410. THE RUBSTRIP WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9957571, REV Z.

Part: DOUBLER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 49,420 hrs · 33,874 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON THE AFT CARGO DOOR FRAME BS 954. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-7, FIG 201.

Part: PANEL — CRACKED (LT WING) · airframe 49,420 hrs · 33,874 cycles

CRACK ON TRAILING EDGE PANEL XRS 164, LT WING UPPER SURFACE. THE PANEL WAS REPAIRED IAW SRM 57-00-00-2R-2.

Part: DOOR FRAME — CRACKED (L1 DOOR WAY) · airframe 49,420 hrs · 33,874 cycles

L1 DOOR FRAME CRACKED. THE DOOR FRAME WAS REPAIRED AND REFURBISHED IAW ER/A 534742-14 REV. ORIGINAL.

Part: BEAM — CRACKED (NLG) · airframe 49,420 hrs · 33,874 cycles

CRACKED LEFT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.

Part: SKIN — CRACKED (RT WING TE) · airframe 49,420 hrs · 33,874 cycles

TWO CRACKS ON THE RT WING FIXED TRAILING EDGE PANEL UPPER AREA XRS 137. REPAIRED IAW SRM 57-00-00-2R-2.

Part: BEAM — CRACKED (NLG) · airframe 49,420 hrs · 33,874 cycles

CRACKED RT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · corrosion level 2 · airframe 49,420 hrs · 33,874 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 180 - 200, LBL. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,401 hrs · 33,860 cycles

AFT EMERGENCY LIGHT ON INTERMITTENTLY. ALL EMERGENCY LIGHTS FLASHED ON LOADING. FOUND B5-260 CHARGER INOPERATIVE. R & R IAW AMM 33-51. ALL CHECKED GOOD. OK FOR SERVICE.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 48,736 hrs · 33,404 cycles

EXIT SIGN MISSING IN MID-CABIN. INSTALLED EXIT SIGN LENS. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,514 hrs · 33,239 cycles

THE OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER AMM 33-50. OPERATIONAL CHECK IS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,428 hrs · 33,181 cycles

AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY AND BATTERY POWER SUPPLY PER AMM 33-51. OPS CHKS GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 47,091 hrs · 32,197 cycles

THE PILOT DISCOVERED THAT THE MAIN CABIN DOOR EMERGENCY EXIT SIGN HAS A LOOSE LENS. MAINTENANCE SECURED THE LENS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,385 hrs · 30,872 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,533 hrs · 30,235 cycles

R1 DOOR EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 43,092 hrs · 29,244 cycles

EMERGENCY LIGHT CHECK FOUND BATTERY POWER SUPPLY B5-119 TO BE INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: HOUSING — DAMAGED (CABIN) · airframe 43,092 hrs · 29,244 cycles

LOWER EMER EXIT IDENTIFIER HOUSINGS DAMAGED AT BS 598. R & R IDENTIFIER IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 43,092 hrs · 29,244 cycles

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

Part: SIGN — CRACKED (CABIN) · airframe 43,092 hrs · 29,244 cycles

FORWARD CABIN OVERHEAD CEILING EMER EXIT SIGN HOUSING CRACKED. R & R SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,092 hrs · 29,244 cycles

RIGHT EMER LIGHT OPERATIONS, TEST FOUND EMER BATTERY PACK INOPERATIVE AT BS 342. R & R BATTERY PACK IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 696, RBL 54.50. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

LEFT CUSP WEB CORRODED, BETWEEN BS 636 - 655. REPAIRED CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 346, RBL 55. REPAIRED CUSP WEB IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 245, LBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 389+5, LBL 58. REPAIRED DOUBLER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FRAME CORRODED AT BS 1022, LONGERON 30, ON THE AFT SIDE ABOVE LONGERON 30R. REPAIRED FRAME IAW SRM & DWG.

Part: BRACKET — CRACKED (RT WING) · airframe 43,092 hrs · 29,244 cycles

RIGHT WING LE BRACKET, BETWEEN SLAT TRACKS 3 & 4 CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SHIELD — CRACKED (RT MLG WW) · airframe 43,092 hrs · 29,244 cycles

RIGHT MAIN GEAR WW SHIELD CRACKED AT AFT BULKHEAD AREA. R & R SHIELD IAW SRM.

Part: FORMER — CRACKED (RT PYLON) · airframe 43,092 hrs · 29,244 cycles

RIGHT PYLON BULKHEAD FORMER CRACKED AT BS 1022, LONGERON 14R - 15R. R & R FORMER IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD CABIN FLOOR MEMBRANE CORRODED AT BS 157, RBL 50. R & R MEMBRANE IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 370, RBL 44. REPAIRED CUSP WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FLOORBEAM CORRODED AT BS 200, RBL 42. REPAIRED FLOORBEAM IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

CUSP WEB CRACKED BETWEEN BS 218 - 237, RBL 54. REPAIRED CUSP WEB IAW SRM.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD CABIN FALSE TRACK CORRODED, BETWEEN BS 170 TO 195, LBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 233, LBL 17. R & R SUPPORT IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD CABIN FLOOR MEMBRANE CORRODED, BETWEEN BS 202 - 218, RBL 44. R & R MEMBRANE IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD CABIN FLOOR MEMBRANE CORRODED, BETWEEN BS 178 - 200, BETWEEN RBL 44 - 55. REPAIRED MEMBRANE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD ENTRY DOOR LOWER JAMB AREA FLOOR SUPPORT CORRODED AT BS 195, BETWEEN LBL 45 TO LBL 55. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

APB FORWARD FACE CORRODED AT LONGERON 30 ON DOUBLER. R & R DOUBLER IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 1037, LONGERON 30. REPAIRED FRAME IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FORWARD LOWER CARGO COMPARTMENT DOOR JAMB CORRODED. R & R DOOR JAMB IAW SRM.

Part: STRAP — CRACKED (RT WING) · airframe 43,092 hrs · 29,244 cycles

RIGHT WING LE INTERNAL STRAP CRACKED, BETWEEN NR 3 & 4 SLAT TRACKS. R & R DOUBLER IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

AFT LOWER CARGO COMPARTMENT DOOR JAMB CORRODED. R & R DOOR JAMB IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

FUSELAGE TO VERTICAL STABILIZER INNER ATTACH ANGLE CRACKED AT BS 1135, LONGERON 2L. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 43,092 hrs · 29,244 cycles

R1 DOOR EMER EVAC SLIDE, AFT GIRT BAR FITTING CORRODED. R & R FITTING IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

R1 DOOR FWD GIRT BAR FITTING CORRODED. R & R FITTING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 908 - 927, RBL 55. REPAIRED CUSP WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

SEAT TRACK CORRODED BETWEEN BS 275 TO 588, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 794 TO 813, RBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 275 - 588, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 813 TO 832, RBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 579 TO 598, LBL 55. R & R CUSP WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

SEAT TRACK CORRODED BETWEEN BS 275 - 588, BETWEEN RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

CUSP WEB CORRODED BETWEEN BS 579 TO 598, RBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN CUSP WEB CORRODED BETWEEN BS 737 TO 757, RBL 55. R & R CUSP WEB IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

AFT CARGO FWD BULKHEAD PANEL CTR SUPPORT CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

LEFT CUSP WEB CRACKED AT BS 710, LBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 43,092 hrs · 29,244 cycles

LEFT WING INBD LE TO BODY FAIRING BOND STRAP CRACKED AT WING ROOT. R & R STRAP IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 54. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT, CORRODED AT BS 200, BETWEEN RBL 7 - 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 TO 200, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 10 - 44. R & R SUPPORT IAW SRM & DWG.

Part: SKIN — DAMAGED (TE FLAP) · airframe 43,092 hrs · 29,244 cycles

LEFT WING TE FLAP UPPER SKIN CREASED AT XFLS 216. R & R SKIN IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 44 TO RBL 54. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, BETWEEN LBL 12 TO 37. R & R SUPPORT IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

RIGHT CUSP WEB CRACKED BETWEEN BS 655 TO 715. R & R CUSP WEB IAW SRM & DWG.

Part: LENS — CRACKED (EXIT SIGN) · airframe 43,092 hrs · 29,244 cycles

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

Part: LANYARD — FRAYED (L1 DOOR) · airframe 43,092 hrs · 29,244 cycles

L1 DOOR EMER EVAC SLIDE LANYARD FRAYED. R & R LANYARD IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 43,092 hrs · 29,244 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 1037, LONGERON 30. R & R FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,092 hrs · 29,244 cycles

AFT CARGO FRAME CORRODED AT BS 1022, LONGERON 30. R & R FRAME IAW SRM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 44,245 hrs · 30,032 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FLAP OUT OF POSITION. REPOSITIONED GIRT BAR IAW MM.

Part: HOLDER — BROKEN (R1 DOOR) · airframe 44,114 hrs · 29,939 cycles

R1 DOOR SLIDE GIRT BAR HOLDER BROKEN. R & R GIRT BAR HOLDER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,950 hrs · 29,830 cycles

RIGHT EMER PATH LIGHT ASSEMBLY INOPERATIVE AT ROW 1. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 43,551 hrs · 29,564 cycles

L1 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 43,483 hrs · 29,515 cycles

AFT EXTERIOR EMER LIGHT WILL NOT SHUT OFF. R & R BATTERY PACK IAW MM.

Part: AVIONICS UNIT — FAULTY (NR 2) · airframe 42,729 hrs · 29,006 cycles

DIVERSION, DECLARED EMERGENCY LT ENG FIRE WARNING IN FLIGHT INTERMITTENT, UNABLE TO TEST DUE TO INTERMITTENT MALFUNCTION DECLARED EMERGENCY & LANDED IN IND. R & R NR 2 VERSATILE INTEGRATED AVIONICS UNIT IAW AMM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 42,153 hrs · 28,636 cycles

AIR TURN BACK DECLARED EMERGENCY RT ENG COMPRESSOR STALL ALERTS INCLUDED COMPRESSOR STALL & ENG RT SYSTEM FAIL. ENG BROUGHT TO IDLE, NOT SHUT DOWN. R & R NR 2 ENG IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,944 hrs · 28,501 cycles

AFT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LANYARD — LOOSE (L1 DOOR) · airframe 40,177 hrs · 27,392 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED LANYARD PER AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,148 hrs · 27,373 cycles

FRAME CORRODED AT BS 1022, LONGERON 30. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,148 hrs · 27,373 cycles

FRAME CORRODED AT BS 1037, LONGERON 30. REMOVED AND REPLACED FRAME IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 39,787 hrs · 27,157 cycles

R1 DOOR JAMB FWD AND AFT CLIPS ATTACHED TO GIRT BAR LATCHES CORRODED. REMOVED AND REPLACED FITTING IAW SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 39,787 hrs · 27,157 cycles

L1 DOOR WEB CRACKED AT BS 207, LONG 15L. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 39,787 hrs · 27,157 cycles

L1 DOOR INSIDE HANDLE AREA ANGLE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,787 hrs · 27,157 cycles

FRAME CORRODED AT BS 1022, LONG 30. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,787 hrs · 27,157 cycles

FRAME CORRODED AT BS 1037, LONGERON 30. REPAIRED FRAME IAW SRM.

Part: COVER PLATE — CRACKED (LT WING) · airframe 39,787 hrs · 27,157 cycles

LEFT WING - BETWEEN STA NR 1 AND 2 - COVER PLATE CRACKED. REMOVED AND REPLACED PLATE IAW SRM.

Part: CABLE — DISCONNECTED (L1 DOOR) · airframe 39,557 hrs · 27,015 cycles

GIRT BAR CONNECTING CABLE DISCONNECTED L1 DOOR. RECONNECTED GIRT BAR CABLE PER MM.

Part: COVER — MISSING (CABIN) · airframe 39,261 hrs · 26,820 cycles

SEAT 1D EMERGENCY EXIT LIGHT BULB COVER MISSING/ BULB INOP. RELAMPED AND REPLACED COVER. OPS CHECKED REF AMM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 38,153 hrs · 26,087 cycles

RIGHT WING AILERON INBOARD TAB DELAMINATED. REPAIRED TAB IAW SRM.

Part: TAB — DELAMINATED (RT AILKERON) · airframe 38,153 hrs · 26,087 cycles

RIGHT WING AILERON INBD TAB DELAMINATED. REMOVED AND REPLACED TAB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,798 hrs · 25,859 cycles

RIGHT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: ACTUATOR — MALFUNCTIONED (RT MLG)

GEAR DOOR OPEN MESSAGE ON FINAL APPROACH. REMOVED AND REPLACED RT MLG DOOR ACTUATOR. REMOVED AND REPLACED LT AND RT MLG DOOR TORQUE TUBES; LEAK CHECK GOOD. ACCOMPLISHED ALL ADJUSTMENTS; TEST AND OPERATIONAL CHECKS REF AMM 32-34.

Part: SOCKET — DEFECTIVE (CABIN)

ROW 24 E-PATH LIGHTS INOP. REMOVED AND REPLACED E-PATH LAMP SOCKET ASSEMBLY IAW AMM 33-51-04. REPAIRED 2 BROKEN SPLICES AFT OF ROW 23 IAW SWPM 20-10-03, OPS CHECK OF EMERGENCY LIGHTING SYSTEM NORMAL IAW AMM 33-51-00.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

L-1 DOOR PAX SLIDE PSI IN RED. REMOVED AND REPLACED L-1 DOOR SLIDE REF 717 MM 25-61.

Part: WIRE — DAMAGED (CABIN)

EMERGENCY LIGHTS ON THE LAST 7 ROWS OF SEATS INOP. REPLACED POWER SUPPLY WITH NO HELP. AT APPROX FS 813 REPAIRED WIRING AS REQUIRED REF WDM 33-51. REPLACED POWER SUPPLY AGAIN AND ALL OPS NORMAL REF MM 33-51.

Part: LIGHT — INOPERATIVE (CABIN)

L-1 DOOR EMERGENCY EXIT IDENTIFIER INOP/DAMAGED. REPLACED IDENTIFIER LIGHT ASSY PER MM 33-51.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME SECTION, STA 908, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FRAME SECTION REPLACEMENT PER B717 SRM 53-20-07 FIG 201 REPAIR 3.

Part: SKIN — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR CENTER FWD EDGE SKIN, CRACKED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B717 SRM 52-82-02 AND BOEING DWG SR09520012-4.

Part: SKIN — DAMAGED (FUSELAGE)

EXTERIOR FUSELAGE SKIN, STA 237, LONG L17L, CREASED. ACCOMPLISHED FUSELAGE SKIN FILLER AND DOUBLER REPAIR PER B717 SRM 53-00-01 FIG 201 REPAIR 6.

Part: DOOR — OPEN (LT MLG)

GEAR DOOR OPEN ALERT ILLUMINATED ON SHORT FINAL. LEFT GEAR DOOR DRAG ON RUNWAY. REMOVED AND INSTALLED LEFT GEAR DOOR REF B717 AMM 32-14-01, ALL CLEARANCE AND OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

LT WING EMERGENCY LIGHT INOPERATIVE. RELAMPED LT WING EMERGENCY LIGHT ASSEMBLY IAW B717 AMM 33-51, OPS CHECK NORMAL.

Part: SIGN — MISSING (CABIN)

EXIT SIGN MISSING AT R1 EXIT DOOR. INSTALLED LENS/SIGN. REF AMM 33-51. OK FOR SERVICE.

Part: SEAT TRACK — WORN (FUSELAGE)

CABIN SEAT TRACK WORN FROM STA 246 TO 265 RBL 22. CUT OUT DAMAGED SECTION OF SEAT TRACK AND INSTALLED SPLICE REPAIR AND NEW SECTION OF SEAT TRACK PER REF EA 17-53-01591IR AND DC9 SRM 53-05 FIG 4F-7001 INSTALLATION.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN HAS A DENT AT STA 226 AND L-18L. CUT OUT DAMAGED SKIN SECTION LT BETWEEN STA 193 AND 228 AND L-15L TO L-18L, FABRICATED SKIN SECTION, DOUBLERS AND FINGER DOUBLERS, AND INSTALLED REPAIR PARTS PER B717 SRM 53-00-01 REPAIR 6.

Part: ATTACH FITTING — CRACKED (FUSELAGE)

FUSELAGE AFT SECTION FWD OF VERTICAL STABILIZER REAR SPAR ATTACH TANG STA Y=1178.225 AND LONG 2R TEAR STRAP IS CRACKED PASSING FASTENER HOLE. CUT OUT DAMAGED AREA OF TEAR STRAP ON AFT FUSELAGE SECTION FWD OF VERTICAL STAB REAR SPAR STA Y=1178.225 AND L2R, FABRICATED AND INSTALLED DOUBLER REPAIR AND FILLER PER REF B717 SRM 51-40-02, 51-41-05, AND EA 17-53-01579IR.

Part: LONGERON — CORRODED (FUSELAGE)

CABIN LONGERON CORRODED STA 160-220 LBL 7. BLENDED CORROSION BYL. REMOVED AND REPLACED FLOOR TRACK LONGERON.

Part: SHEAR TIE — CRACKED (FUSELAGE)

FUSELAGE INTERIOR FRAME SHEAR TIE CLIP IS CRACKED AT FS 1022 BETWEEN STR 15R AND 16R. FABRICATED NEW SHEAR TIE CLIP AND INSTALLED PER BOEING DRAWING 9912243.

Part: SHEAR TIE — CRACKED (FUSELAGE)

FUSELAGE INTERIOR FRAME SHEAR TIE CLIP IS CRACKED AT FS 1022 BETWEEN STR 13R AND 14R. CUT OUT DAMAGED AREA OF CLIP, FABRICATED REPAIR ANGLE AND FILLER, AND INSTALLED ANGLE REPAIR AND FILLER ON FRAME SHEAR TIE CLIP PER REF BOEING REPAIR SKETCH CQT-CQT-09-0023-01C.

Part: PAN — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER PAN HAS CORROSION. CUT OUT LOWER SECTION OF AFT CARGO DOOR CUTOUT LOWER PAN, FABRICATED AND INSTALLED NEW SECTION OF LOWER PAN AND SPLICES PER B717 SRM 53-20-15 REPAIR 7.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FLOOR SUPPORT WEB HAS A HOLE LOCATED 6FT AFT OF R1 DOOR AFT DOOR FRAME. CUT OUT DAMAGE SECTION AND INSTALLED TYPICAL WEB REPAIR PER REF B717 SRM 51-70-10 REPAIR 2 FIG 201.

Part: CUSP WEB — CRACKED (FUSELAGE)

RIGHT SIDE CABIN STA 389 STR 18R CUSP LINE WEB HAS CORROSION. CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR ON RIGHT STA 389 STR 18R PER REF B717 SRM 51-70-10 FIG 201 SHEET 2.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

CABIN FLOOR SUPPORT WEB HAS A HOLE LOCATED 6 INCHES I/B OF R1 DOOR THRESHOLD. CUT OUT DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED DOUBLER REPAIR AND FILLER PER REF B717 SRM 51-70-10 REPAIR 2 FIG 201.

Part: CUSP WEB — CRACKED (FUSELAGE)

LT CABIN STA 660 STR 18L CUSP LINE WEB CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER B717 SRM 51-40-02.

Part: CUSP WEB — CORRODED (FUSELAGE)

FUSELAGE INTERIOR RT SIDE CUSP WEB HAS CORROSION BETWEEN FS 579 AND FS 598. INSTALLED NEW CUSP WEB AT FUSELAGE INTERIOR RT SIDE BETWEEN FS 579 AND 598. REF B717 SRM 51-40-02 AND SRM 51-40-05.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN HAS A DENT AT APPROX STA 237 AND LONG 18L. CUT OUT DAMAGE AREA ON LT FUSELAGE SKIN FROM STA 229 TO 245 BETWEEN L-16L TO 18L. FABRICATED AND INSTALLED SKIN REPAIR PER REF B717 SRM 53-00-01.

Part: CUSP WEB — CRACKED (FUSELAGE)

AT CABIN FLOOR STA 680 AND LBL 48 CUSP WEB HAS A CRACK. CUT OUT DAMAGED WEB SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR AT STA 680 LBL 48 PER REF B717 SRM 51-70-10 REPAIR 2.

Part: ENGINE — FAILED (NR 1)

DEPARTING 12R THE LEFT ENGINE FAILED AT ABOUT 300' AGL. HIGH TGT NOTED. NO BIRDS SIGHTED. OVERWEIGHT LANDING AT 109K. FOUND NR 1 ENGINE FODDED DUE TO INTERNAL FAILURE. REMOVED AND REPLACED ENG IAW W/C 603 ON W/O 177916. ALL OPERATIONS NORMAL - AUTOLAND C/W ON T/C 625.

Part: PAN — CORRODED (CARGO DOOR)

FWD CARGO DOOR LOWER PAN, CUT OUT HAS CORROSION. INSTALLED LOWER SECTION OF JAMB PAN BETWEEN STA 370 & 427 AND SPLICED REPAIR PER SRM 53-20-15 REPAIR 6.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS)

ON TAKEOFF RECEIVED -A- RIGHT HYD PRESSURE LOW, RIGHT QUANTITY LOW, AND HYDRAULIC POWER OFF. THERMAL PLUG BLOWN, REMOVED AND REPLACED NR 2 EDP AND ELECTRIC AUX PUMP. SERVICED SYSTEM, ALL OPS NORMAL.

Part: WIRE — BROKEN (ROW 3F)

EMERGENCY LIGHTS AT ROW 3F INOPERATIVE. RETERMINATED BROKEN WIRE AT SEAT ROW 3 DISCONNECT IAW SWPM 20-31-00. FUNCTIONAL CHECK NORMAL IAW AMM 33-51-00.

Part: BULKHEAD — BENT (BS 37)

FUSELAGE STA 37 BULKHEAD WEB AND FLANGE ARE BENT ON LEFT EDGE BETWEEN LONGERON 18L AND NLG WHEEL WELL CUTOUT. INSTALLED FRAME SECTION AND SPLICE AT FUSELAGE BS 37 BETWEEN LONGERON 18L AND MLG WHEEL WELL PER RES NUMBER 02-0547 AND B717 SRM 53-10. MATERIAL USED 7075-T6 .050, 26 X 4 INCH FRAME AND 7075-T6 .063, 3.5 X 1 INCH (SPLICE PLATE).

Part: ENGINE — MALFUNCTIONED (NR 1)

ON TAKE OFF CLIMB NR 1 ENGINE SURGE FOLLOWED BY ENGINE FLAME OUT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE. IAW 717 MM 72-00

Part: POWER SUPPLY — INOPERATIVE (AFT CARGO)

FOUND DURING SERVICE CHECK EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT BATTERY PACK/POWER SUPPLY. IAW 717 MM 33-50

Part: LIGHT — INOPERATIVE (SEAT 22)

FOUND EMERGENCY PATH LIGHT LIGHTS INOPERATIVE AT SEAT 22 DEF. RE-CONNECTED PLUG AT SEAT 22 DEF IAW 717 MM 25-23-05.