N915AT

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 53,930 hrs · 38,572 cycles

ATO, ABORTED TAKE-OFF AT 60KTS DUE TO A STABILIZER CONFIGURATION MESSAGE. MAINTENANCE PERFORMED A HORIZONTAL STABILIZER CHECK, THE SYS OPS PROPERLY, AND AIRCRAFT WAS RETURNED TO SERVICE.(8144086)

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 53,778 hrs · 38,416 cycles

AFT CARGO DOOR FRAME STATION 944 - FOUND PLUG RIVET UNDER SPLICE PLATE REMOVED FOR REPAIR. REPAIRED PER ER/A 630377-14 REV. ORIG. (1338586)

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 53,778 hrs · 38,416 cycles

CORROSION IN THRESHOLD PAN SEVERAL LOCATIONS. CORROSION DAMAGE SPLICE REPAIR - CHECKED AND REPLACED HI-SHEAR FASTENERS REF: B717-200 SRM 51-41-04 (1336682)

Part: SPAR — CORRODED (ZONE 500) · airframe 53,668 hrs · 38,307 cycles

WORKING PRI 629584-14 REV 0, REV1, REV 2, REV 3, AND ERA 629584- 14AD REV ORIG. LT REAR SPAR XRS 179 CORROSION. ACCOMPLISHED PRI 629584-14AD REV 3 LT WING REAR SPAR XRS 179 REPAIR. SFAR 88 AND CDCCL REQUIREMENTS C.W. (1232961)

Part: HOLDER — SPARKS (ZONE 200) · airframe 52,663 hrs · 37,357 cycles

WHILE MOVING CAPT NOTE PAD HOLDER HAD SPARKS BEHIND THE HOLDER & ALL MAP LIGHTS WENT OUT. ALSO, CIRCUIT BREAKER W29 TRIPPED. MAINTENANCE REPAIRED BARE WIRES PER B717 SWPM 20-10-03. NO FURTHER ISSUES. OPERATIONAL CHECK WAS NORMAL ON CHART HOLDER. (LP #7237748)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 51,568 hrs · 36,397 cycles

BOTH AFT OVERWING LOWER SIDE WALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #6342840)

Part: PSEU — FAILED (ZONE 700) · airframe 51,256 hrs · 36,118 cycles

SHIP 9580 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO A "PSEU FAIL" MESSAGE. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR POSITION INDICATIONS WERE NORMAL FOLLOWING GEAR EXTENSION FOR LANDING. HOWEVER, THE LEADING EDGE SLATS FAILED TO EXTEND RESULTING IN A "NO FLAPS, NO SLATS" LANDING. THE LANDING WAS GOOD EXCEPT FOR A BRAKE OVERHEAT CONDITION. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND PERFORMED APPLICABLE RETURN TO SERVICE TESTS. ALL TESTS PASSED. (LP #4010566)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,729 hrs · 34,754 cycles

SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. SECOND ATTEMPT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR MALFUNCTIONED. NORMAL GEAR RETRACTION ON TAKEOFF. FCF CHECKLIST REQUIRED GEAR EXTENSION INFLIGHT; WHEN RETRACTING, CREW RECEIVED A RED "LEFT GEAR UNSAFE" INDICATION. THE QRH 14.18, GEAR UNSAFE WAS COMPLIED WITH. LOWERING THE GEAR, CREW RECEIVED THREE GREEN INDICATIONS. RAISING THE GEAR AGAIN, CREW RECEIVED RED LEFT GEAR UNSAFE INDICATION AGAIN. CREW DECLARED EMERGENCY WITH ATC AND RETURNED TO QRO. GEAR HANDLE PLACED BACK IN THE DOWN POSITION ON APPROACH, THREE GREEN GEAR DOWN AND LOCKED INDICATIONS RECEIVED. NORMAL LANDING AND TAXI TO THE HANGER. (LP #5049614)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,729 hrs · 34,754 cycles

SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR FAILED TO RETRACT PROPERLY. GEAR RETRACTION SHORTLY AFTER TAKEOFF PRODUCED A RED "RIGHT GEAR UNSAFE" INDICATION. QRH 14.18 WAS COMPLIED WITH. LOWERING THE GEAR, CREW RECEIVED THREE GREEN SAFE INDICATIONS. RAISING THE GEAR AGAIN, CREW RECEIVED BOTH LEFT & RIGHT RED GEAR UNSAFE INDICATION. CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO QRO. GEAR HANDLE PLACED BACK IN THE DOWN POSITION, THREE GREEN GEAR RECEIVED. NORMAL LANDING AND TAXI TO THE HANGER. (LP #5049610)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,728 hrs · 34,752 cycles

CRACKS ON OUTER PAN (3 EA) ON STOP FITTING AREA (AFT EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 0072: CRACKS OUTER PAN ON STOP FITTINGS AREA (AFT EDGE) AT AFT CARGO DOOR WERE REPAIRED PER ERA 613600-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 613600-14 REV 2. ASSOCIATED ERA 14-613600 ADDED FOR AC 9580. (LP #0092145)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,726 hrs · 34,751 cycles

CORROSION FRAMES CLIP STA=927 STGR 29RH TO STGR 28LH AT AFT CARGO COMPARTMENT C2 (ON REFERENCE NRC 0139). SUMMARY OF NRC 00493: CORROSION LEVEL 2. FRAME CLIP STA=927 STGR 29RH TO STGR 28LH AT AFT CARGO COMPARTMENT C2 WAS FABRICATED PER DWG 9915524 REV P AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0089240)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,726 hrs · 34,751 cycles

CRACK ON LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00496: LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM-53-00-05-2R-2 PAR 5, FIG 201. (LP #0083405)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,726 hrs · 34,751 cycles

CORROSION ON DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00058: CORROSION LEVEL 2. DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CARGO COMPARTMENT (C2) WAS REPAIRED PER B717-200 SRM 53-20-15 2R PROCEDURE 7. (LP #0079727)

Part: TRUNNION — CORRODED (MLG) · corrosion level 2 · airframe 50,146 hrs · 35,090 cycles

WEAR AND CORROSION ON FIXED STRUT MLG ATTACH FITTING AND BUSHING ALSO (TRAPEZOIDAL PANEL) AND BUSHING AT RH MLG IN REF AMDS 3211-4004 STEP 4. SUMMARY OF NRC 00434: CORROSION LEVEL 1. WEAR AND CORROSION ON FIXED STRUT MLG ATTACH FITTING AND BUSHING ALSO (TRAPEZOIDAL PANEL) AND BUSHING AT RH MLG WAS REPAIRED PER ERA 613761-14 REV ORIGINAL SECTION 1: PERMANENT REPAIR. ASSOCIATED ERA 14-613761 ADDED FOR AC 9580. (LP #0078477)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,726 hrs · 34,751 cycles

CORROSION ON DOOR JAMB STA Y 370 TO STA Y 424 AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00057: CORROSION LEVEL 2. DOOR JAMB AT FWD CARGO COMPARTMENT (C1) WAS REPAIRED PER SRM 53-20-15-2R PROCEDURE 6 REPAIR 6 PAR 6 FIG 201 AND 51-41-02-0G. (LP #0067222)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,726 hrs · 34,751 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=160 TO STA Y=200 AND X=56 AT LOWER SIDE OF FWD PASSENGER DOOR JAMB. SUMMARY OF NRC 00254: CORROSION LEVEL 2. FLOOR SUPPORT FROM STA Y=160 TO STA Y=200 AND X=56 AT LOWER SIDE OF FWD PASSENGER DOOR JAMB WAS REPLACED PER DWG 9936534-07, PER B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #0063300)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,726 hrs · 34,751 cycles

CORROSION ON WEB (LOWER SURFACE) BTW STA Y=1022-1037 -X=57 TO -X=60 AT RH WEB PAX CABIN. SUMMARY OF NRC 00291: CORROSION LEVEL 2. WEB (LOWER SURFACE) BTW STA Y=1022-1037 -X=57 TO -X=60 AT RH WEB PAX CABIN WAS REPLACED PER DWG 9981474 REV K AND PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #0054792)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,722 hrs · 34,749 cycles

EMERGENCY EXIT LIGHT ASSEMBLY ABOVE R1 DOOR HANDLE, BR9051-001, IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE R1 DOOR. OPERATIONAL CHECK WAS GOOD. (LP #7217465)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,722 hrs · 34,749 cycles

THE EMERGENCY LIGHT BATTERY CHARGER AT STA 332 - 351 PANEL P1-118 EIN B5-118 IS DEFECTIVE REF B717 33-51-14. MAINTENANCE REPLACED THE EMERGENCY LIGHT CHARGER AT STA 332 REF B717 WDM 33-51- 14. (LP #7217464)

Part: SKIN — DENTED (BS 427) · airframe 47,764 hrs · 33,298 cycles

DENTS ON FUSELAGE SKIN AT STA 427 BETWEEN LONGERON 27L AND 29L. ACCOMPLISHED PERMANENT REPAIR REF PRI #578768-14, REV. 1 AND ER/A #578768 -14 REV. ORIGINAL. REQUIRED INSPECTION COMPLETE QC1981. (LP #1116346)

Part: SKIN — DENTED (BS 524-527) · airframe 47,764 hrs · 33,298 cycles

DENT ON FUSELAGE SKIN AT STA 524 TO 527 1" BELOW LONG 26L LAP SEAM. PER B717 SRM 53-01-01-1A-3 CONDITION 5 DENT IS OUT OF LIMITS. REMOVED DAMAGE 1" X 3" PER B717 SRM 53-03-01-2R-1 FIG. 110 SHEET 3. FUSELAGE SKIN MISDRILLED AT STA 520 ON LONG 26L, REMOVED DAMAGE PER B717 SRM 53-03. FABRICATED, PAINTED, AND INSTALLED REPAIR PARTS PER B717 SRM 53-03. (LP #1114483)

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 46,630 hrs · 32,527 cycles

THE AFT WALKWAY EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TERMINAL BROKEN. THE WIRE TERMINAL WAS REPAIRED PER SWPM CHAPTER 20. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #5521308)

Part: SEAL — MISSING (LT WING SLAT) · airframe 46,409 hrs · 32,384 cycles

LEFT WING INBOARD SLAT MISSING ABOUT 9.5" OF SEAL. MISSING SEAL STARTS AT 30 IN. FROM MOST INBD EDGE OF SEAL ON LT WING #1 SLAT. FWD TO CDL 57-48-01. SDR REPORTED DUE TO POSSIBILITY THAT PART MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP4252114)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,836 hrs · 31,991 cycles

THE CREW ABORTED THE TAKEOFF AFTER 110 KNOTS FOLLOWING AN AURAL STABILIZER MOTION WARNING AND AN ILLUMINATED RED "STAB TRIM" MESSAGE. MAINTENANCE VERIFIED THAT NO FAULTS WERE RECORDED IN THE VERSATILE INTEGRATED AVIONICS SYSTEMS 1 OR 2. BOTH VIA 1 AND 2 WERE RETURNED TO SERVICE AFTER PASSING ALL CHECKS AND TEST.

Part: LIGHT — UNKNOWN (CABIN) · airframe 45,821 hrs · 31,983 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. MAINTENANCE REINSTALLED THE EMERGENCY LIGHT AT 28B.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,691 hrs · 29,054 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT WING EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK.

Part: WEB — DAMAGED (FUSELAGE) · airframe 40,052 hrs · 27,910 cycles

TOOL MARK ON WEB STA Y=674 BETWEEN LONGERON 11RT TO 10RT AND LONGERON 14RT TO 15RT AT CPAX, SM, CARD 6, ZONE 201. WEB WAS REPAIR IAW ER/A 547802-14, REV ORIGINAL AND ETI 17-16-064, SRM 51-40-08, 51-20-09 AND 51-10-04, PAR 15/21.

Part: ANGLE — CORRODED (BS 157-218) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON CUSP ANGLE AT LBL 60 BETWEEN BS 157 AND 218. DUE TO EXCESSIVE DAMAGE BY CORROSION. CUSP ANGLE WAS REPAIRED IAW ETI 17-16-054, REV 1 AND ER/A 547810-14, REV ORIGINAL.

Part: STRAP — CRACKED (L1 DOOR) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD STRAP AT BEAM NR 6 L1 PASSEGER DOOR. STRAP WAS REPLACED IAW SRM 51-41-02, 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND DWG 9955750, REV. U. CRACK LENGTH .500".

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,052 hrs · 27,910 cycles

CRACK ON DOUBLER AFT END AT BEAM NR 7 L1 DOOR. AFT END AT BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 13. CRACK LONG 0.812".

Part: STRUCTURE — BENT (L1 DOOR) · airframe 40,052 hrs · 27,910 cycles

BEND ON FWD/AFT LOWER CORNER AT EXTERNAL SURFACE PASSENGER L1 DOOR. LOWER CORNER AT EXTENAL SURFACE PASSENGER ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2. WEIGHT IS 1.52 LB. RII INSPECTOR EVP 200801883 TECHOPS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,052 hrs · 27,910 cycles

CRACKED FUSELAGE SKIN ON CUTOUT OF RT/LT NLG AFT DOOR AFT HINGE. SKIN WAS REPLACED IAW SRM 53-10-01, 51-41-02, 51-41-05, 51-10-3 P. 21, 15.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 40,052 hrs · 27,910 cycles

CRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG .656 AND .468".

Part: DOUBLER — WORN · airframe 40,052 hrs · 27,910 cycles

WEAR ON DOUBLER PRODUCTION AT INNER RT PAN A SIDE LOWER HINGE AFT EMERGENCY EXIT. DOUBLER PRODUCTION WAS REPAIRED IAW SRM 52-10-02, FIG 201, REP 16. MEASURE: OT IS 0.050" AND REMAINING THICKNESS IS 0.028". THEREFORE OUT LIMITS. EQ: DIGITAL ULTRASONIC THICKNESS 38DLP.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520EB AT LT WING. CORROSION ON COUNTERSINK OF ACCESS DOOR 520EB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.545", 0.555", AND 0.540" AND WAS REPLACED IAW SRM 57-10-01, CONDITION II.

Part: ANGLE — CRACKED (BS 712-714) · airframe 40,052 hrs · 27,910 cycles

CRACK ON ANGLE OF WING BOX FLOOR STRUCTURE BS 712 TO 714 X -20 AND Z -8. ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05 AND DWG 5910464, REV "DE" ITEM 24.

Part: CARGO TRACK — CORRODED (BS 900-954) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON RT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 900-954. DUE TO EXCESSIVE DAMAGE, CARGO TRACK SECTION WAS REPLACED IAW SRM 51-41-05 AND 51-41-02.

Part: FRAME — CORRODED (BS 908) · airframe 40,052 hrs · 27,910 cycles

CORROSION ON FRAME ANGLE BS 908 BETWEEN LONGERON 29 AND 30L IN AFT CARGO COMPARTMENT. FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06, FIG 201.

Part: LONGERON — CORRODED (BS 960) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON LONGERON 29 LT BELOW OF SPLICE BS 960 IN AFT CARGO COMPARTMENT. DAMAGE ON SECTION LONGERON WAS REMOVED AND WAS REPAIRED IAW SRM 51-10-04 AND 53-20-05, FIG 201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620EB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 620EB WERE REMOVED AND FOUND OUT LIMITS WITH 3 ADVANCED HOLES .545, .549, .544 THEREFORE WAS REPLACED IAW SRM 57-10-01 AND AMM 28-42-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DB AT RT WING. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01 AND 51-10-04 AND FUEL ACCESS PLATE WERE MEASSURED, 4 HOLES FOUND OUT LIMITS .535, .534, .549, .554 IAW SRM 57-10-01 THE HOLES WERE REPAIRED WITH BUSHINGS FABRICATED IAW SRM 57-10-01. PANAMETRICS 38DL PLUS DATE EXP 27OCT16 SONOPEN V260 RM.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620CB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01. FUEL ACCESS PLATE NR 620CB WAS MEASURED, 6 EAS, HOLES FOUND OUT LIMITS .554, .534, .546, .541, .565, .540 IAW SRM 57-10-01 BUSHING WERE FABRICATED IAW SRM 57-10-01. PANAMETRICS 38DL PLUS CATE EXP 27OCT 16 SONOPEN V260-RM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 40,052 hrs · 27,910 cycles

CRACKED STIFFENERS ON PASSENGER CABIN FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 40,052 hrs · 27,910 cycles

CRACKED FLOOR PANEL 211ACF. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,052 hrs · 27,910 cycles

DAMAGE AND MISSING FERRULES ON FLOOR PANELS 221FF, 221CF, 22BF, 22LF, 222JF, 222RF, AND 222UF. SM, CARD 77, ZONE 000. DAMAGE FERRULES ON FLOOR PANEL NR 222BF, 222RF, 222LF, 222JF, AND 221EF WERE REPLACED IAW DWG NR 9936546 AND ER/A 546544-14, REV. ORIGINAL FLOOR PANELS, NR 222UF AND 221CF WERE FABRICATED IAW DWG 9936546 AND ER/A 546544-14, REV. ORIGINAL ASSOCIATED ER/A 00-546544, ADDED FOR AC 9580.

Part: FLOOR PANEL — DAMAGED · airframe 40,052 hrs · 27,910 cycles

CRACK ON PASSENGER CABIN FLOOR PANEL NR 222ZF. SM, CARD 52, ZONE 000. FLOOR PANEL 222ZF WAS REPAIRED IAW SRM 53-00-00, REPAIR 2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. TREATED, PAINTED, AND APPLIED CIC IAW SRM 51-10-04, PAR 21, 15, AND 37. CRACK ON FLOOR PANEL WAS FOUND WITH DIMENTION AS FOLLOWS 0.390". RII COMPLETED.

Part: FLOOR PANEL — DAMAGED · airframe 40,052 hrs · 27,910 cycles

DAMAGE AND MISSING FERRULES ON FLOOR PANELS, NR 222ABF, 222AAF, 222AEF, AND 222AKF AT PAX CABIN. SM, CARD 79, ZONE 000. DAMAGE FERRULES WERE REPLACED ON FLOOR PANELS NR 22ABF, 222AAF, 222AEF, AND 222AKF IAW ER/A 546544-14, REV. ORIGINAL ASSOCIATED ER/A 00-546544 ADDED FOR AC 9580.

Part: FRAME — CRACKED (BS 696) · airframe 40,052 hrs · 27,910 cycles

CRACKED FRAME BS 696, LONG 26 RT AND FRAME BS 715, LONGERON 27R AT UNDERWING BARREL KEELBEAM INTERNAL STRUCTURE. SM, CARD 16, ZONE 140. FRAMES WERE REPAIRED IAW SRM 51-70-11, REPAIR 1, SRM 51-41-02, SRM 51-10-04 PAR 15 AND 21. RII COMPLETED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520CB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520CB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.538 AND 0.540 ACCESS PLATE WAS REPLACED IAW SRM 57-10-01 IN TO CONDITION III.

Part: FRAME — CRACKED (BS 696) · airframe 40,052 hrs · 27,910 cycles

CRACKED FRAME BS 696, LONG 26LT AND FRAME 715, LONG 27 LT AT UNDERWING BARREL KEEL BEAM INTERNAL STRUCTURE. FRAMES WERE REPAIRED IAW SRM 51-70-11 REPAIR 1, FIG 201, SRM 51-41-02, SRM 51-10-04 PAR 15-21, 37, 51-41-05.

Part: SKIN — CORRODED · airframe 40,052 hrs · 27,910 cycles

CORROSION ON CENTER WING UPPER SKIN, JUST FWD OF SLANT PANEL AND BS X= 40.5, CARD 3, ZONE 140). FUEL LINE WAS REMOVED AND INSTALLED IAW AMM 20-10-03 917-81 FASTENERS WERE REMOVED AND INSTALLED IAW SRM 51-41-05 CORROSION WAS REMOVED IAW SRM 57-10-01 AND (UT) WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2, ORIGINAL THICKNESS IS 0.252" AND REMAINING THICKNESS IS 0.218" THEREFORE WITH ITS LIMITS IAW ETI-17-16-052, REV. 1 AND ER/A 546525-14, REV. ORIGINAL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,052 hrs · 27,910 cycles

DAMAGE AND MISSING FERRULES ON FLOOR PANELS NR 222AVF AND 223CF AT CABIN PAX. FLOOR PANEL NR 222AVF WAS REPLACED FERRUL IAW ER/A 546544-14 REV. ORIGINAL. FLOOR PANEL NR 223CF WAS FABRICATED IAW ER/A 546544-14 REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520DB WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.552, 0.538, 0.563 IAW SRM 57-10-01 AND ACCESS PLATE WAS REPLACED IAW SRM 57-10-01 IN TO CONDITION III.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520GB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520GB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .560, .553 AND .558 IAW 57-10-01 ACCESS PLATE WAS REPLACED IN TO CONDITION III.

Part: DOOR FRAME — CRACKED (NLG) · airframe 40,052 hrs · 27,910 cycles

CRACKED NLG DOOR JAMB BS Y=46 X=18 LT Z=-33 AT NLG W/W. NLG DOOR JAMB WAS REPAIRED IAW SRM 53-10-14, FIG 201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620LB AT RT WING. CORROSION ON COUNTERSINK AT ACCESS PLATE 620LB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.536, 0.550, AND 0.545 AND WAS REPLACED WITH CONDITION III IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520LB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520LB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .579, .538, .543 IAW SRM 57-10-01, ACCESS PLATE WAS REPLACED IAW SRM 57-10-01 IN TO CONDITION III.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 40,052 hrs · 27,910 cycles

CRACKS RT CUSP WEB BETWEEN BS 218 TO 237 X 44. CUSP WEB WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 9930538, REV CC.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 40,052 hrs · 27,910 cycles

BROKEN CORE ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV ORIGINAL.

Part: WEB — CORRODED (BS 195-200) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON DIAPHRAGM FROM BS 195 TO 200 AND BETWEEN X -52 TO X -58. DIAPHRAGM WAS REPAIRED IAW SRM 51-70-10, FIG 201.

Part: STIFFENER — CRACKED (FLOOR PANEL) · airframe 40,052 hrs · 27,910 cycles

CRACK ON STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, 222AJF. SM, CARD 57 ZONE 000. STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, AND 222AJF WERE REPAIRED IAW SRM 53-20-50, REPAIR 5, FIG 201 AND 202. CRACK L=0.235", CRACK L=0.324", CRACK L=0.430".

Part: SKIN — DAMAGED (RUDDER) · airframe 40,052 hrs · 27,910 cycles

DAMAGE ON LT SIDE OF RUDDER SKIN PANEL, LOWER SECTION. SM, CARD 5, ZONE 370. DAMAGED AREA WAS REPAIRED IAW SRM 51-70-13 R1.

Part: FITTING — CRACKED (BS 737) · airframe 40,052 hrs · 27,910 cycles

CRACKED FITTING AT BS 737, X 43 AND Z -11. FITTING WAS REPLACED IAW SRM 51-41-05, 51-41-02, 51-40-08, AND 51-10-04 PAR 15 AND 21.

Part: FLOOR SUPPORT — CRACKED (BS 636) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FLOOR SUPPORT BS 636, X 0. CRACK WAS STOPP DRILLED IAW SRM 53-00-00, FIG 1. REPAIR PART WAS FABRICATED IAW SRM 53-00-00 FIG 201. REPAIR INSTALLED IAW SRM 51-40-02.

Part: CUSP WEB — CRACKED (BS 813-825) · airframe 40,052 hrs · 27,910 cycles

CRACKED LT CUSP WEB BS 813 AND 825. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 226.

Part: CUSP WEB — CRACKED (BS 674-676) · airframe 40,052 hrs · 27,910 cycles

CRACKED LT CUSP WEB BS 674-676, X 44 TO 46. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 223,

Part: FLOORBEAM — CRACKED (BS 737) · airframe 40,052 hrs · 27,910 cycles

CRACKED FLOORBEAM BS 737 AND X -50. FLOORBEAM WAS REPLACED IAW 51-41-02 AND 51-41-05.

Part: STIFFENER — CRACKED · airframe 40,052 hrs · 27,910 cycles

CRACKED STIFFENER ON AFT PRESSURE BULKHEAD BETWEEN LONGERONS 7RT AND 8 RT AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-41-05 DWG 9915558, REV BA CRACK L= 0.750".

Part: FRAME — CRACKED (BS 1037) · airframe 40,052 hrs · 27,910 cycles

CRACKED FRAME BS 1037 AT INTERSECTION WITH LONG 17RT. RT AFT LAV AREA. FRAME ON STA Y=1037, RT WAS REPAIRED IAW SRM 53-20-07, FIG 201.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON SETTLEMENT AREA AND ELONGATED HOLE OF COUNTERSINK OF FUEL ACCESS DOOR 141AR. CARD 44, ZONE 000. CORROSION SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 141AR WERE REMOVED AND MEASURED, AND FOUND OUT OF LIMITS WITH 5 HOLES 0.700", 0.662", 0.661", 0.665", AND 0.662". THEREFORE WILL BE REPAIRED WITH BUSHINGS IAW SRM 57-10-01, SETTLEMENT AREA WAS MEASSURED ORIGINAL THICKNESS IS 0.180". REMOVING THICKNESS IS 0.176", THEREFORE IT IS WITHIN LIMITS THE COUNTERSINK AND HOLES WERE REWORKED AND COUNTERSINK WAS MEASSURED WITH 0.835". THEREFORE OUT LIMITS OF MINIMUM DIAMETER OF REPAIR AND WAS REPLACED IAW SRM 57-10-01, CONDITION 2.

Part: LONGERON — CORRODED (BS 927-946) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON LONGERON TERMINAL 24 RT, BETWEEN BS 927 TO 946 AT AFT CARGO COMPARTMENT. LONGERON END WAS REPLACED IAW DWG 5911494, REV CZ AND SRM 51-41-05, PAR 8, UT, WAS ACCOMPLISHED ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.025 THEREFORE IT IS OUT OF LIMITS IAW SRM 53-00-00. OLYMPUS 38DL EXP DATE 22-JUL-16 TRANSDUCER SONOPEN V260-RM.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DT AT LT WING. CORROSION AT FUEL ACCESS PLATE 520DT ON COUNTERSINK WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES DIAMETER MAX 0.619IN, 0.672IN AND 0.694 IN IAW SRM 57-10-01 AND ACCESS PLATE WAS REPLACED IAW SRM 57-10-01 IN TO CONDITION 2. TOOL USED, PN 1127, SN 60555.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620DT WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .680 IN, 0.680 IN AND 0.665 IN, IAW SRM 57-10-01 AND ACCESS PLATE WAS REPLACED IAW 57-10-01 IN TO CONDITION 2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION AND COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620AT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620 AT WAS REMOVED AND COUNTERSINK WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.661 IN, 0.665 IN, 0.666 IN, IAW ARM 57-10-01, FUEL ACCESS PLATE WAS REPLACED IAW SRM 57-10-01, SRM IN TO CONDITION 2.

Part: PAN — CRACKED (BS 696-715) · airframe 40,052 hrs · 27,910 cycles

CRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 696 TO 715. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 203, TYPE C.

Part: CUSP WEB — CORRODED (BS 503-522) · corrosion level 2 · airframe 40,052 hrs · 27,910 cycles

CORROSION ON RT CUSP WEB BS 503 TO 522. CUSP WEB WAS REMOVED, AND FOUND OUT OF LIMITS. CUSP WEB WAS REPAIRED IAW SRM 51-41-02, SRM 51-10-04 PAR 15, 21, 26, AND 37, SRM 53-00-55.

Part: PAN — CRACKED (BS 832-851) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 832 TO 851 IN CPAX, SM, ZONE: 201 CARD: 3. DAMAGE ARE WAS TRIMED OUT IAW SRM 56-20-02, FIG 202. REPAIR PARTS WERE FABRICATED IAW SRM 50-20-02, FIG 202, REPAIR PARTS WERE INSTALLED IAW SRM 51-40-02 AND 51-40-05. DIMENTIONS OF DAMAGE L=0.240". EQUIPMENT: DIGITAL CALIPER EXP DATE: 02FEB17 N/C:1427.

Part: PAN — CRACKED (BS 636-655) · airframe 40,052 hrs · 27,910 cycles

CRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 636 TO 655. RING PAN WAS REPAIRED IAW SRM 50-20-02. REPAIR 1, FIG 202, TYPE B.

Part: PAN — CRACKED (BS 832-851) · airframe 40,052 hrs · 27,910 cycles

CRACKED RT UPPER, AFT CORNER ON RING PAN BETWEEN BS 832 TO 851. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, TYPE B.

Part: CUSP WEB — CRACKED (BS 587-589) · airframe 40,052 hrs · 27,910 cycles

CRACKED LT CUSP WEB BETWEEN BS 587 TO 589, X=45. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 221.

Part: PAN — CRACKED (BS 756-775) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.

Part: PAN — CRACKED (BS 851-870) · airframe 40,052 hrs · 27,910 cycles

CRACK ON AFT/UPPER CORNER BETWEEN BS 851 TO 870 AT LT RING PAN. PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.

Part: PAN — CRACKED (BS 617-636) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.

Part: PAN — CRACKED (BS 636-655) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO BS 655 IN CPAX, SM, ZONE: 201 CARD: 10. ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO 655 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.

Part: PAN — CRACKED (BS 908-927) · airframe 40,052 hrs · 27,910 cycles

CRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".

Part: PAN — CRACKED (BS 813-832) · airframe 40,052 hrs · 27,910 cycles

CRACK ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832. ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, CRACK LENGTH, L= 0.235".

Part: CUSP WEB — CRACKED (BS 851-870) · airframe 40,052 hrs · 27,910 cycles

CRACKED CUSP WEB BETWEEN X=54 AND X=60 BETWEEN BS 851 AND 870. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,184 hrs · 25,620 cycles

DURING SERVICE CHECK, FOUND CATWALK AND AFT CABIN DOOR LIGHTED SIGN FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51.

Part: FRAME — CRACKED (BS 674) · airframe 36,997 hrs · 25,466 cycles

DURING SPECIAL VISIT, FOUND MAIN FRAME BS 674 RT CRACKED, HFEC VERIFIED. REPAIRED IAW ER/A 530437-14MA AND AMDS WC 5310-01436-03B.

Part: CUSP WEB — CRACKED (BS 655) · airframe 36,997 hrs · 25,466 cycles

DURING SPECIAL VISIT, FOUND RT CUSP WEB CRACKED AT BS 655 OVERWING FRAME CUTOUT. INSTALLED NEW WEB IAW ER/A 532911-14.

Part: CUSP WEB — CRACKED (BS 655) · airframe 36,984 hrs · 25,459 cycles

RIGHT CUSP WEB CRACKED AT BS 655 OVERWING FRAME CUTOUT. REPAIR DOUBLER INSTALLED IAW SRM FIG 201, 53-00-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,587 hrs · 24,330 cycles

R1 DOOR EMER LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,587 hrs · 24,330 cycles

TAIL CONE CATWALK FWD EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,587 hrs · 24,330 cycles

RIGHT AFT OVERWING EXIT EMER LIGHT BULB INOPERATIVE. RELAMPED IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,747 hrs · 24,431 cycles

RIGHT FUSELAGE AFT EDGE OF CARGO DOOR CUT OUT SKIN CRACKED AT BS 994. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 35,587 hrs · 24,330 cycles

FORWARD OVERWING DOOR EMER EXIT LIGHTS FAILED OPERATIONS CHECK. REMOVED BATTERY IAW AMM.

Part: PAN — CRACKED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

AFT LOWER FUSELAGE, CONDITIONED AIR GND CONNECTION CUT OUT PAN CRACKED AT UPPER AFT RADIUS. R & R PAN IAW AMM & DWG.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

FORWARD CARGO COMPARTMENT FASTENER CORRODED AT BS 332, BETWEEN 1L TO 1R. R & R FASTENER IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

L1 DOOR THRESHOLD CABIN FLOOR WEB CORRODED BETWEEN BS 160 TO 200. REPAIRED WEB IAW SRM.

Part: FITTING — BROKEN (LT MLG TRUNNION) · airframe 35,587 hrs · 24,330 cycles

LEFT MLG FWD TRUNNION FITTING ZERK FITTING BROKEN ON FWD FITTING. R & R FITTING IAW SIP.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

R1 DOOR THRESHOLD FWD CORNER VERTICAL FLANGE AFT SIDE OF FRAME ANGLE CORRODED. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

INTERCOSTAL CRACKED AT BS 1225, RUDDER ACTUATOR ROD END SUPPORT BRACKET. R & R INTERCOSTAL IAW AMM SRM.

Part: MOUNT — CORRODED (R1 DOOR) · airframe 35,587 hrs · 24,330 cycles

R1 DOOR FWD EMER EVAC SLIDE FLOOR LATCH MOUNT PAD CORRODED. R & R MOUNT ASSEMBLY IAW SRM & DWG.

Part: MOUNT — CORRODED (R1 DOOR) · airframe 35,587 hrs · 24,330 cycles

R1 DOOR AFT EMER EVAC SLIDE FLOOR LATCH MOUNT PAD CORRODED. R & R MOUNT ASSEMBLY IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

FLOOR PLATE PANEL ANGLE CORRODED BETWEEN BS 169 TO 173, RBL 56. R & R ANGLE IAW SRM.

Part: WINDOW — CRACKED (CABIN) · airframe 35,587 hrs · 24,330 cycles

RIGHT FUSELAGE CABIN WINDOW CRACKED BETWEEN BS 813 TO 832. R & R WINDOW IAW MM.

Part: WINDOW — CRACKED (CABIN) · airframe 35,587 hrs · 24,330 cycles

RIGHT FUSELAGE CABIN WINDOW CRACKED BETWEEN BS 889 TO 908 AT UPPER FWD CORNER ON EXTERIOR PANE. R & R WINDOW IAW MM.

Part: WINDOW — CRACKED (CABIN) · airframe 35,587 hrs · 24,330 cycles

RIGHT FUSELAGE CABIN WINDOW CRACKED BETWEEN BS 832 TO 851. R & R WINDOW IAW MM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 35,587 hrs · 24,330 cycles

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

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

FUSELAGE SKIN CUT OUT DOUBLER CRACKED AT BS 200. R & R SKIN IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,587 hrs · 24,330 cycles

FUSELAGE SKIN CRACKED AT BS 994, LONGERON 25R. REPAIRED SKIN IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 35,587 hrs · 24,330 cycles

CENTER AISLE EMER EXIT SIGN LENS CRACKED AT BS 331. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 35,587 hrs · 24,330 cycles

R1 DOOR EMER EXIT LIGHT LENS AFT OF DOOR CRACKED. R & R LIGHT IAW AMM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 35,438 hrs · 24,234 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 34,606 hrs · 23,692 cycles

AT FINAL APPROACH FIX GEAR DOWN ALL THREE UNSAFE SET ILLUMINATED CYCLED GEAR ALL THREE GREEN LANDED. R & R PSEU IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 33,240 hrs · 22,828 cycles

RIGHT EMERGENCY ESCAPE PATH LIGHT MISSING A BULB. INSTALLED BULB IAW MM.

Part: COVER — MISSING (CABIN) · airframe 33,240 hrs · 22,828 cycles

RT EMERGENCY ESCAPE PATH LIGHT MISSING A COVER. INSTALLED COVER IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 32,592 hrs · 22,446 cycles

RIGHT EEPLS BULB MISSING AT ROW 3. REMOVED AND REPLACED BULB PER AMM.

Part: LENS — MISSING (CABIN) · airframe 32,592 hrs · 22,446 cycles

RIGHT EEPLS LEN MISSING AT ROW 3. REMOVED AND REPLACED LENS PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,585 hrs · 22,440 cycles

FORWARD F/A EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY.

Part: SPRING — DIRTY (GIRT BAR) · airframe 32,432 hrs · 22,352 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. CLEANED MOUNT AND SPRING ASSY PER AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

STA 389 RBL 56 CUSP WEB IS CRACKED. CUT OUT DAMAGED AREA DIM 3 5/8 X 5 1/2 IAW B717 SRM 53-00-55 FIG 212, FABRICATED DOUBLER FROM 7075-T6 .032 DIM 9 1/2 X 6 3/4 FILLER FROM 7075-T6 .020 DIM 4 1/8 X 1 1/4 PO 90015962 IAW B717 SRM 53-00-55 FIG 21.

Part: SKIN PANEL — CORRODED (RT WING) · airframe 31,763 hrs · 21,943 cycles

RIGHT WING , UPPER SURFACE, CUTOUT FOR FUEL ACCESS PANEL 620 AT CORRODED. REMOVED CORROSION AT RUB STRIP IAW B717 SRM 51-40-4.

Part: FITTING — CRACKED (RT HORIZ STAB) · airframe 31,763 hrs · 21,943 cycles

RIGHT HORIZONTAL STABILIZER REAR SPAR CUTOUT FOR O/B ATTACH POINT FOR GEARED TAB DRIVE LINK PLASTIC CUP IS CRACKED. REPAIRED RIGHT HORIZONTAL STABILIZER REAR CUTOUT PLASTIC CUP IAW B717 SRM 51-70-05 PG 201 REPAIR 1.

Part: ROD END — LOOSE (RT ELEVATOR) · airframe 31,763 hrs · 21,943 cycles

RIGHT ELEVATOR CONTROL TAB ADJUSTABLE ROD END IS LOOSE. RE-SECURED RIGHT ELEVATOR CONTROL TAB ADJUSTABLE ROD END IAW B717 AMM CH 27-31-04.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

FWD PIT STA 237 BETWEEN LONGERON 28L- 27L INTERCOSTAL ATTACH CLIP IS CRACKED. REMOVED DAMAGED ANGLE FROM FRAME STATION 237 LONGERON 28L-27L. LOCATED, DRILLED AND DEBURRED NEW ANGLE P/N 991554-11, PO 2304443. INSTALLED NEW ANGLE AT FRAME STATION 237 LONGERON 28L-27L IAW B-717 SRM 51-41-05 SRM 51-41-05 SRM 51-40-08, SRM 51-10-04, AMM 51-10-00 AND SRM 51-41-05 FIG 7.

Part: FITTING — CRACKED (LT HORIZ STAB) · airframe 31,763 hrs · 21,943 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR CUTOUT FOR I/B ATTACH POINT ON GEAR TAB, PLASTIC CUP IS CRACKED. REPAIRED LEFT HORIZONTAL STAB REAR SPAR CUTOUT PLASTIC CUP IAW B717 SRM 51-70-05 PG 201 REPAIR 1.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

FWD PIT BETWEEN LONG 28R-27R INTERCOSTAL ATTACH ANGLE IS CRACKED STA 237. REMOVED DAMAGED ANGLE FROM FRAME STATION 237 LONG 28E-27R. LOCATED, DRILLED AND DEBURRED NEW ANGLE P/N 9915554-11 PO 2301143. INSTALLED NEW ANGLE AT FRAME STATION 237 LONG 28R-27R IAW B717 SRM 51-41-05, SRM 51-40-08, SRM 51-10-04, OHM 51-10-00 AND SRM 51-41-05 FIG 1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

STA 217 RBL 54 CUSP WEB IS CRACKED. CUT OUT DAMAGED AREA 4"X 2 1/2" IAW B717 SRM 53-00-55 FABRICATED DOUBLER FROM 7075-T6 .032 DIM 5 3/8"X 4 1/8 " PO 90015254 FILLER FROM 7075-T6 .020 DIM 4"X 2 1/8" PO 90015962 IAW B717 SRM 53-00-55 FIG 205 R

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 31,763 hrs · 21,943 cycles

RIGHT W/W FWD WING TO BODY FAIRING FRAME ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED RIGHT W/W FWD WING TO BODY FAIRING FRAME ATTACH BRACKET IAW B717 SRM 51-41-05.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

AFT CABIN FLOOR STA 1053 LEFT BEAM ATTACH FITTING CRACKED. REMOVED AFT CABIN BEAM ATTACH PLATE STA 1053 LEFT. FABRICATED ATTACH PLATE OUT OF 7075-T6.063" PO 90015971 DIM 2 1/2 X 1 3/4. ALODINED, PRIMED, TOP COATED, INSTALLED ATTACH PLATE

Part: SCREW — CORRODED (RT HORIZ STAB) · airframe 31,763 hrs · 21,943 cycles

RIGHT HORIZONTAL STABILIZER, REAR SPAR, FROM O/B TO I/B SIDE, NR 4 ELEVATOR HINGE SUPPORT, SEVERAL SCREWS CORRODED. REMOVED LIGHT CORROSION ON SEVERAL SCREWS AT RIGHT STABILIZER REAR SPARE NR 4 ELEVATOR HINGE SUPPORT IAW B717 SRM 51-10-04.

Part: SCREW — CORRODED (LT HORIZ STAB) · airframe 31,763 hrs · 21,943 cycles

LEFT HORIZONTAL STABILIZER AT REAR SPAR, O/B TO I/B AREA, AT NR 4 ELEVATOR HINGE SUPPORT SEVERAL SCREWS CORRODED. REMOVED LIGHT CORROSION ON SEVERAL SCREWS AT LEFT HORIZONTAL STABILIZER AT REAR SPARE AT NR 4 ELEVATOR HINGE SUPPORT IAW B717 SRM 51-1-04.

Part: SCREW — CORRODED (LT HORIZ STAB) · airframe 31,763 hrs · 21,943 cycles

LEFT HORIZONTAL STABILIZER AT REAR SPAR, O/B TO I/B AREA AT NR 3 ELEVATOR HINGE SUPPORT HAS SEVERAL SCREWS CORRODED. REMOVED LIGHT CORROSION ON SEVERAL SCREWS AT LEFT HORIZONTAL STABILIZER AT REAR SPARE NR 3 ELEVATOR HINGE SUPPORT IAW B717 SRM 51-10-04.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

AFT CARGO FWD BULKHEAD UPPER LINER SUPPORT CRACKED/BENT. REMOVED UPPER LINER SUPPORT AFT PIT FWD BULKHEAD IAW B717 SRM 51-41-02. LOCATED AND DRILLED IAW B717 SRM 51-41-08; ALODINED, PRIMED AND TOP COAT IAW B717 SRM 51-10-04 INSTALLED LINER SUPPORT P/N 5956040-11 PO 2301130 IAW B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

AFT ACCESSORY STA 1126 L2R CRACKED. CUT OUT DAMAGED AREA, AT AFT ACCESORY STA 26 LONG NR 2, FABRICATED NEW LONG SECTION, FABRICATED SPICES FROM EXTRUSION P/N S2641454-1200 PO 79019157 DIM 12.6" AND INSTALLED PORTS REPAIR OIW B717 SRM 53-00-05 R

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

AFT CARGO FWD BULKHEAD LWR LINER SUPPORT CRACKED/BENT. REMOVED UPPER LINER SUPPORT INTERCOSTAL AFT PIT FWD BULKHEAD IAW B717 SRM 51-41-02. LOCATED AND DRILLED NEW LINER SUPPORT P/N 5956010U13-PO 790191620 IAW B717 SRM 51-41-02. ALODINED, PRIMED & TOP COATED IAW B717 SRM 51-10-04; INSTALLED LINER SUPPORT IAW B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

CABIN SEAT TRACK SECTION 952-1022 RBL 54 HAS CORROSION AT STA 972, 939, 955, 970, 994, 1002, 1018. ORIGINAL MAT .100", REMAINING .0" LOSS 100% CABIN SEAT TRACK, BETWEEN STA 952 TO 1022 - RBL 54 OUT OF LIMITS IAW B717 SRM 53-20-52, AD1 REMOVED SEAT TRACK SECTION 952-1022 RBL 54 IAW B717 SRM 51-41-01 123 7/8" FABRICATED NEW SEAT TRACK SEC FROM SR 9530115-7005 PO# 90015295 DIM 123 7/3" IAW B717 SRM 53-20-51 INSTALLED SEAT TRACK SEC IAW B717 SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

CABIN SEAT TRACK SECTION 237-588 RBL 54.0 HAS CORROSION AT STA 262, 283, 321, 364, 397, 410, 427, 440, 460, AND 469. EVALUATED CORROSION, MATERIAL LOSS 100 % FOUND TO BE OUT OF LIMITS, IAW B717 SRM 53-20-52 FIG 101. REMOVED SEAT TRACK SECTION RBL 54 BETWEEN REPAIR 5 STA 217 TO 588 IAW B717 SRM 51-41-01. FABRICATED 2 EA REPAIR SECTIONS IAW B717 SRM 53-20-52. LOCATED AND DRILLED HOLES AT SPLICE PARTS IAW B717 SRM 51-40-08. INSTALLED SEAT TRACK 2 EA BS 237-303 AND 303-588 RBL 54 AND INSTALLED SPLICED AT BS 303 IAW B717 SRM 51-41-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

RIGHT CUSP WEB STA 1002-1022 HAS CORROSION. REMOVED RIGHT CUSP WEB IAW B717 SRM 53-00-00 FIG 103& 53-00-55 FIG 205.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

CABIN SEAT TRACK SECTION 237-588 RBL 24 HAS CORROSION AT STA 278, 300, 322, 363, 394, 458, 487, 518, 547, AND 579. REMOVED CORROSION SEAT TRACK STA 278 TO 579 IAW B717 SRM 51-10-04; OUT LIMITS STA 394 MAT LOSS .052" REM MAT .048 ORIG MAT .100 CUT OUT DAMAGE AREA DIM 77" IAW B717 SRM 53-20-52. REP 5 CUT OUT ST 360.5 TO 436 RBL 24 FABRICATED NEW SECTION SEAT TRACK FROM SR09530115-7001 PO 79019659 DIM 77" LOCATED & DRILLED SEAT TRACK AND SPLICES 2 EA. IAW B717 SRM 53-20-52 REP 5 AND INSTALLED PARTS REPAIR IAW B717 SRM 53-20-52 REP 5 FG 201 DETAIL A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

CABIN SEAT TRACK SECTION 589-898 RBL 54.0 HAS CORRSION AT STA 637, 650, 670, 684, 705, 727, 746, 758, 775, AND 790. EVALUATED MATERIAL LOSS ORIG.100 REMAIN 0 LOSS .100 IS OUT OF LIMITS IAW B717 SRM 53-20-52 AD1. REMOVED SEAT TRACK SECTION FROM RBL 54 STA 589 TO 898 IAW B717 SRM 51-41-01. LOCATED AND DRILLED SEAT TRACK 2 EA SECTION 1 EA SPLICES PER SECTION FROM P/N SR09530115-7075 PO 90015631 DIM 234 1/8"X 20" SEC FROM SR09530085-25 PO 790191275, STRAP P/N SR09530085-27 PO 790191275 FITTING P/N SR953005-13 PO 790191355 ON SPLICEP/N 3925837-501 IAW B7177 SRM 53-20-52. INSTALLED SEAT TRACK SECTION 2 EA END SPLICES RBL 54 BETWEEN STA 589-898 IAW B717 SRM 53-20-52 FIG 201 REPAIR 5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

RIGHT CUSP WEB STA 446-503 HAS CORROSION 26-033. CUT OUT DAMAGED AREA DIM 4 "X 3/4" IAW B717 SRM 53-00-055 FIG 205. FABRICATED DOUBLER FROM 7075 T6 .032 DIM 7 1/4"X 5 7/8" PO 90014369 FILLER FROM 7075-T6 .020 DIM 3 3/4X 7/8 PO 90015962 IAW B717 S

Part: TRIM PANEL — CRACKED (L1 DOOR) · airframe 31,763 hrs · 21,943 cycles

L-1 DOOR UPPER HINGE CUTOUT TRIM PANEL IS CRACKED. - COMPOSITE REMOVED L1 DOOR UPPER HINGE TRIM PANEL IAW B717 SRM 51-41-01, SANDED, CLEANED AND PREPED AREA, IAW B717 SRM 51-70-09 P 202, PAR S REPAIR 10. APPLIED REPAIR IAW B717 SRM 51-70-09 P 202 PAR S REPAIR 10, FINISHED REPAIR IAW B717 SRM 51-70-09 GEN REINSTALLED TRIM PANEL IAW B717 SRM 51-41-01.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 31,763 hrs · 21,943 cycles

RIGHT WING LEADING EDGE WING AT WTB-BONDING STRAP CRACKED UPPER & LWR ENDS (2 PLCS) FS 639 L-20R 36-1. REMOVED AND REPLACED RIGHT WING - L/E WTB BONDING STRAP'S UPPER AND LWR ENDS AT FS 639 L-20-R IAW B717SRM 51-41-05. BONDING CHECK IS GOOD IAW B717 SWP

Part: BONDING STRAP — CRACKED (LT WING) · airframe 31,763 hrs · 21,943 cycles

LEFT WING - LEADING EDGE WING AT WTB-BONDING STRAP CRACKED ON LWR END FS 639 L-20L 36-9. REMOVED AND REPLACED LEFT WING L/E WTB - BONDING STEP LWR END FS 639 L-20-L P/N 9191104U97 PO 790191208 IAW B717 SRM 51-41-05. BONDING CHECK IS GOOD IAW B717 SWP

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 222RF IS DELAMINATED. REMOVED FLOOR PANEL 222PF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222PF IAW B717 AMM 53-21-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

RIGHT CUSP WEB HAS CRACK AT STA 979 26-039. CUT OUT DAMAGE DIM (6 3/4"X2") IAW B717 SRM 53-00-55 FIG 205. FAB DOUBLER MAT USED 7075T6.050"PO 90014344. DIM (11"X4 1/4") FILLER 7075T6.040" PO 90014579. DIM (6 3/4"X2") IAW - B717 SRM 53-20-51 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,763 hrs · 21,943 cycles

CABIN SEAT TRACK SECTION 237-588 LBL 54.0 HAS CORROSION AT STA 487, 500, 517, 548, AND 579. REMOVED & REPLACED SEAT TRACK IAW B717 SRM 51-41-08, 51-10-04, 53-20-52R5 & AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222BF IS DELAMINATED. REMOVED FLOOR PANEL 222BF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222BF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222ACF IS DELAMINATED. REMOVED FLOOR PANEL 222ACF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 41" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222ACF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222WF DELAMINATED. REMOVED FLOOR PANEL 221WF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 221WF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 221 UF IS DELAMINATED. REMOVED FLOOR PANEL 221UF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76". IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 221UF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN NR 222JF IS DELAMINATED. REMOVED FLOOR PANEL 222JF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222JF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222AAF IS DELAMINATED. REMOVED MAIN CABIN FLOOR PANEL 222AAF IAW B717 SRM 51-41-01 FABRICATED FLOOR PANEL FROM P/N BZZ7002TYPE3 PO 790191470 DIM 21"X22" IAW B717 SRM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 22RF IS DELAMINATED. REMOVED FLOOR PANEL 222RF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222RF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 222LF IS DELAMINATED. REMOVED FLOOR PANEL 222LF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222LF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 222EF IS DELAMINATED. REMOVED FLOOR PANEL 222AEF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 41" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222AEF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222AMF IS DELAMINATED. REMOVED FLOOR PANEL 222AMF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 76" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222AMF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222 DF IS DELAMINATED. REMOVED FLOOR PANEL 222DF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 19" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222DF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

FLOOR PANEL MAIN CABIN 222ATF IS DELAMINATED. REMOVED FLOOR PANEL 222ATF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL FROM P/N BZZ7002 TYPE 3 PO 790191470 DIM 21"X 65" IAW B717 SRM 53-20-50. REPAIR 3 INSTALLED FLOOR PANEL 222ATF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,763 hrs · 21,943 cycles

MAIN CABIN FLOOR PANEL 222ABF IS DELAMINATED. REMOVED FLOOR PANEL FROM MAIN CABIN 222AAF IAW B717 SRM 51-41-01 FABRICATED FLOOR PANEL FROM P/N BZZ7002TYPE3 PO 790191470 DIM 21"X22" IAW B717 SRM 53-21-01 INSTALLED FLOOR PANEL IAW B717 SRM 51-41-0.1

Part: COVER — BROKEN (EXIT SIGN) · airframe 31,244 hrs · 21,610 cycles

R-1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,158 hrs · 21,551 cycles

RIGHT EEPLS BULBS INOP BETWEEN ROWS 10 TO ROW 19. REMOVED & REPLACED BULBS IAW AMM.

Part: SLIDE — OBSTRUCTED (R1 DOOR) · airframe 30,590 hrs · 21,183 cycles

R1 DOOR EMERGENCY EVAC SLIDE UNABLE TO ARM. REMOVED DEBRIS FROM SLIDE PER AMM.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 30,590 hrs · 21,183 cycles

L1 DOOR EMERGENCY EVAC SLIDE LANYARD FRAYED. REMOVED AND REPLACED LANYARD IAW MM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 30,540 hrs · 21,148 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: RETAINER — BROKEN (GIRT BAR) · airframe 30,216 hrs · 20,930 cycles

EMERGENCY EVAC SLIDE GIRT BAR RETAINER BROKEN. REMOVED AND REPLACED RETAINER PER MM.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 30,044 hrs · 20,814 cycles

FWD EMERGENCY FLASHLIGHT LOOSE. SECURED FLASHLIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 29,790 hrs · 20,657 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 20. INSTALLED COVER PER MM.

Part: LIGHT — MISSING (CABIN)

(2 EA.) CLEAR EPL LENSES MISSING AND (2 EA.) BULBS MISSING AT 10D. INSTALLED NEW LENSES AND BULBS AT 10D. OPS - OK.

Part: SIGN — MISSING (CABIN)

EXIT SIGN ABOVE ROW 2 AISLE MISSING FOUND IN GALLEY. INSTALLED NEW EMERGENCY EXIT SCREENED LENS AT SEAT ROW 2 IAW 717 AMM 33-51, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY INOP AT SEAT 2D. RELAMPED OPS CHECK NORMAL REF 33-50.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

LEFT ENGINE COMPRESSOR STALL (LEFT ENGINE WENT BOOM, PLANE YAWED, N2 WENT TO 56 PERCENT, LOTS OF VIBRATION). SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00.

Part: BRACKET — CORRODED (CABIN)

RIGHT CABIN VENT GRILL BRACKET, STA 200 TO 256, RBL 50, CORROSION. ACCOMPLISHED BRACKET DOUBLER REPAIR PER B717 SRM 51-70-11 FIG 201.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 240, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085 AND B717 SRM 53-20-52 PG 106.

Part: FLOOR SUPPORT — CORRODED (BS 148-200)

CABIN FLOOR SUPPORT, STA 148 TO 200, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-41-01.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 195, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: WEB — CRACKED (FUSELAGE)

CABIN LONGERON FINGER WEB, STA 208, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB FILLER AND DOUBLER REPAIR PER B717 SRM 53-00-00 REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 237)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: MOUNT — DETACHED (EVAC SLIDE)

TAIL SLIDE AFT LANYARD MOUNT TO COVER HAS BECOME UNATTACHED. RE-SECURED TAIL SLIDE AFT LANYARD MOUNT TO SLIDE COVER IAW AMM 25-61.

Part: ENGINE — FAILED (RIGHT)

RIGHT ENGINE FAIL DURING CLIMB AT 22,500 FT. MAX TGT 1091. NORMAL DESCENT TO LANDING AT 101,500 LBS. NO OVERWEIGHT LANDING INSP REQ'D. AIRCRAFT LANDED BELOW THE MSCW OF 110,00. REF ITEM 2 LOG PAGE 1767583 FOR ENG REMOVAL/REPLACEMENT.

Part: HANDSET — DEFECTIVE (CABIN)

FOUND IN AFT GALLEY HOT AND SMOKING, PULLED C/B, STILL HOT-NO SMOKE, DIVERTED TO PIT (AFT FLT ATTNT HANDSET). REPLACED AFT ATTENDANT HANDSET, OPS CHECKS GOOD REF AMM 23-30.

Part: LENS — MISSING (CABIN)

ROW 22 DEF RED LENS FOR EMERGENCY LIGHT MISSING. INSTALLED NEW RED LENS AT SEAT 22D IAW B717-200 AMM 33-51-04.

Part: SLIDE — DEPLOYED (L1 DOOR)

L1 DOOR SLIDE AND COVER FELL OFF A/C AND DEPLOYED. REMOVED AND REPLACED L1 DOOR SLIDE AND COVER PER AMM 25-61.

Part: LANYARD — BROKEN (EVAC SLIDE)

ESCAPE SLIDE AT L-1 DOOR WIRE LANYARD BROKEN. REMOVED AND REPLACED WIRE LANYARD IAW REF MM 25-61.

Part: POWER SUPPLY — DISCHARGED (CABIN)

FOUND AISLE EMERGENCY LIGHTS ROW 1 THROUGH 10 INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD. REF NRWC N064491.

Part: SKIN — DENTED (BS 235)

SMOOTH SKIN DENT AT FS 235, 6 INCHES ABOVE CUSP LINE WITHIN LIMITS PER SRM 53-00 ON LEFT SIDE. 3 INCHES IN DIA BY .125 INCH DEPTH. INSTALLED DOUBLER REPAIR AT FS 235, 6 INCHES ABOUT AS PER B717 SRM 53-00-01 REPAIR 6.

Part: PSEU — INOPERATIVE (RT MLG)

RT MAIN GEAR INDICATOR RED AFTER GEAR WAS RETRACTED BOTH INDICATOR AND CONFIG PAGE. REMOVED PSEU AND RT LANDING GEAR UPLOCK PROX SENSOR SWUNG GEAR SEVERAL TIMES WITH NO DEFECTS NOTED. A/C OK FOR SERVICE IAW MM 32-61.

Part: ACTUATOR — INOPERATIVE (RT MLG DOOR)

PUT THE GEAR HANDLE DOWN AND GOT 3 GREEN AND GEAR DOOR OPEN ALERT. FOLLOWED QRH. LANDED WITH GEAR DOORS OPEN. REMOVED AND REPLACED MLG DOOR ACTUATOR IAW MM 32-34. LEAK AND OPS CHECK GOOD.