N959AT

Part: HINGE FITTING — CORRODED (ZONE 300 ELEV) · airframe 56,077 hrs · 39,291 cycles

RT ELEVATOR GEARED TAB INBD CRANK FITTING-HINGE HAS SIGNS OF CORROSION ON HARDWARE AND PUSH ROD END HAS SIDE TO SIDE PLAY. REPLACED HARDWARE REF B717 AMM 27-31-05 (1193806)

Part: LIGHT — DETACHED (ZONE 200) · airframe 55,611 hrs · 38,878 cycles

AIRCRAFT 9518, EMERGENCY EXIT LIGHT HANGING DOWN ROW 19. CORRECTIVE ACTION: SECURED LIGHT ASSY REF B717 AMM 33-51. (LP 7263518)

Part: REPAIR — NOT REPORTED (NOT REPORTED) · airframe 55,601 hrs · 38,870 cycles

SHIP 9518 EXISTING REPAIRS FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ERA 621388-14AD (0994041)

Part: REPAIR — NOT REPORTED (NOT REPORTED) · airframe 55,601 hrs · 38,870 cycles

SHIP 9518 EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621443 (0994030)

Part: NONE — NONE (NONE) · airframe 55,510 hrs · 38,776 cycles

SHIP 9518 ACCOMPLISH ERA 624994-14 KA1717 STRUCTURAL SHIMMING FOR HUGHES WIFI INSTALLATION, CORRECTIVE ACTION: COMPLIED WITH ERA 624994-14 REV. (0969673)

Part: BATTERY — NO TEST (ZONE 200) · airframe 55,498 hrs · 38,765 cycles

DURING TESTING FOUND 1EA LIGHT IN CEILING AT AFT EXIT / FA SEAT AREA TO BE INOPERATIVE. REPLACED BATTERY AT B5-116. NOW LIGHT TEST GOOD REF B717 AMM 33-51-00. (LP #0957765)

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 55,500 hrs · 38,766 cycles

DUE TO CRACK IN RH WING REAR AFT SPAR LOWER CAP, COMPLY WITH PRI 621388-14. CRACKED SPAR CAP REPLACED ON PRI 621388-14 REVS 0 THRU 22. COMPARED PRI 621388-14 REVS 0 THRU 22 AND ERA 621388-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621388-14 REV ORIG. ALL RII ITEMS C/W. REF LOG PAGE 0939997 FOR MONITOR. (LP #6413448)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 55,500 hrs · 38,766 cycles

DUE TO CRACK IN LH WING LOWER SPAR CAP, COMPLY WITH PRI 621443-14. CRACKED SPAR CAP REPLACED ON PRI 621443-14 REVS 0 THRU 24. COMPARED PRI 621443-14 REVS 0 THRU 24 WITH ERA 621443-14 REV A. ALL ITEMS MATCH. COMPLIED WITH ERA 621443-14 REV A. ALL RII ITEMS C/W. REF LOG PAGE 0941945 FOR MONITOR. ASSOCIATED ER/A 14-621443 ADDED FOR AC 9518. (LP #6413447)

Part: NUT — OUT OF LIMITS (TRIM SYSTEM) · airframe 54,421 hrs · 37,846 cycles

AD -- DURING FUNCTIONAL TEST OF THE TRIM ACME SCREW AND NUT FOUND DIMENSION BG IS OUT OF LIMIT. UNSAFTIED TURNBUCKLE CONNECTING CABLES 130B TO 130A AND CABLE TURNBUCKLE TO 129B AND 129A. BROKE SAFTEY WIRE ON STOP BOLT (AB) PER B717 AMM 27-40-00 FIGURES 504 AND 503. CW STEPS A THROUGH G (2)(D) RIGGED CABLES 129 AND 130 REF B717 AMM 27-40-60 820-80. C/W STEPS G (36) B717 AMM 27-40-00. COMPLETED ADJUSTMENT OF THE STAB THRU G (38) PER B717 AMM 27-40-00. ALL RII TASKS COMPLETE. COMPLETED ADJUSTMENT OF STAB PER B717 AMM 27-40-00.

Part: SUPPORT — CRACKED (HORIZONTAL STAB) · airframe 54,421 hrs · 37,846 cycles

AD -- DURING JACK SCREW LUBE, CYCLED HORIZ STAB FULL NOSE UP, SUPPORT ASSY CONTACTED STOP AND CRACKED. REMOVED HORIZONTAL STABILIZER ACTUATOR ASSEMBLY AND REPLACED JACKSCREW FOR HORIZONTAL STAB PER B717 AMDS WORKCARD 2740-0114-05. ALL RII TASK COMPLETE. (LP #5850979)

Part: COVER — MISALIGNED (EMER LIGHT SWTCH) · airframe 54,099 hrs · 37,576 cycles

DURING SERVICE CHECK, THE CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH C/B A11 PULLED. MAINTENANCE FOUND F/A PANEL SWITCH COVER MISALIGNED, CAUSING SWITCH TO NOT GO TO OFF POSITION FULLY. ADJUSTED SWITCH COVER AND OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #5401061)

Part: HOLDER — SHORTED (CHART) · airframe 54,087 hrs · 37,567 cycles

SHIP 9518 -SMKE- THE FLIGHT CREW REPORTED VISIBLE SMOKE FROM THE CAPTAIN SIDE CLIPBOARD LIGHT. THE SMOKE STOPPED AFTER ABOUT 10 SECONDS. THE QRH WAS COMPLIED WITH AND THE CREW CONTACTED MAINTENANCE TO PULL THE CIRCUIT BREAKERS. THE FLIGHT CONTINUED TO THE SCHEDULED DESTINATION AND AN UNEVENTFUL LANDING. CORRECTIVE ACTION: MAINTENANCE CAPPED AND STOWED TWO WIRES FOR THE CAPTAIN CHART HOLDER PER ENGINEERING RI INSTRUCTIONS. (LP #5401048)

Part: LIGHT — SPARKS (MAP LIGHT) · airframe 54,014 hrs · 37,509 cycles

AFTER TAKEOFF ON RWY 6 IN BHM, AT APPROX 600 FT, CAPTAIN SIDE MAP LIGHT SPARKED AND BEGAN TO SMOKE. THE CIRCUIT BREAKER W29 TRIPPED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PUSHED C/B IN AND BOTH LIGHT WORKED ON CAPTAIN AND FIRST OFFICER SIDES. UPON INSPECTION FOUND SOME BULBS MISSING. NOT SEEING ANY DAMAGE TO WIRES OR ANY DEFECTS. FOUND BULB SHORTED AND REPLACED THOSE BULBS. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT IS OK FOR SERVICE. (LP #5401008)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,276 hrs · 36,888 cycles

SHIP 9518 -DE- THE CREW DECLARED AN EMERGENCY DUE TO INTERMITTENT RIGHT HYDRAULIC PUMP FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE SWITCH. (LP #4594298)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

AD RELATED, MISSING TO PERFORM STEP 14 A (2) AND 22 A (2) OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY OF NRC 00520: STEP 14 A (2) AND 22 A (2) OF 2521-01701- 01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 WERE PERFORMED. ASSOCIATED AA 2521-01701 ADDED FOR AC 9518. (LP #2915144)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

AD RELATED, MISSING TO PERFORM STEP 14 A (2), 21 A (2) AND 34 A (2) OF 2521-01701-01A-SINGLE AND DOUBLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY OF NRC 00521: STEP 14 A (2), 21 A (2), AND 34 A (2) OF 2521-01701-01A-SINGLE AND DOUBLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 WERE PERFORMED. ASSOCIATED AA 2521-01701 ADDED FOR AC 9518. (LP #2915136)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

AD RELATED, MISSING TO PERFORM TORQUE OF TRIPLE TOURIST CLASS SEATS. SUMMARY OF NRC 00518: STEP 8J OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 WAS PERFORMED PER TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01 STEP 8.J.(1) AND TOOL: TORQUE WRENCH 10-50LB/IN. ASSOCIATED AA 2521-01701 ADDED FOR AC 9518. (LP #2915140)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

CRACK ON WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX. SUMMARY OF NRC 0170: WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX WAS REPAIRED PER B-717-200 SRM 55-00-00-2R REPAIR 1 FIG 201. (LP #2901626)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

NICKS ON DOUBLER REPAIR BTW STA Y=996 TO Y=1002. SUMMARY OF NRC 099: 2ND. DOUBLER WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 FIGURE 202. PERFORM VISUAL INSPECTION EACH 8000 CYCLES PER B 717-200 SRM 53-20-15-2R PROCEDURE 10 PAR 7 TABLE 202. (LP #2901810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 00179: CORROSION LEVEL 2. WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #2897086)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

DISBOND ON RH CENTER FIXED VANE, UPPER SURFACE OF 0.700IN LENGTH X 0.600IN WIDTH AT DENT #1, (53.25" FROM IB EDGE, 5" FROM TE) IN REF MON JOB 032-0001 LOG 1549344. SUMMARY OF NRC 00407: RH CENTER FIXED VANE, UPPER SURFACE WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #2894377)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON GENERATION FLOOR ACCESS PANELS 221SF, 222EF, 221NF, 222AWF, AND 222SF. SUMMARY OF NRC 00283: CORROSION LEVEL 2. FLOOR ACCESS PANELS 222EF AND 222SF WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, FLOOR PANELS 221SF AND 221NF WERE FABRICATED PER DWG: 9952521 REV BB. GVI WAS PERFORMED ON FLOOR PANEL 222AWF AND NO CORROSION WAS FOUND PER B717-200 AMM 05-21-02-210-801 PARAGRAPH A (1). (LP #2894592)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON FLOOR PANEL 211AMF AT COCKPIT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PANEL (SKIN) OF FLOOR PANEL 211AMF AT COCKPIT WAS FABRICATED AND REPLACED PER DWG 9957826 REV AA, B717-200 SRM 51-20-05-0G AND 51-41-02-0G. (LP #2891380)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON RH CTR SEAT TRACK FROM STA Y=216 TO STA Y=245 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0174: CORROSION LEVEL 2. SECTION SEAT TRACK FROM STA Y=200 TO STA Y=245 AT FWD PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (LP #2888403)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

CRACK ON FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN WAS REPAIRED PER B717 SRM-53-20-07-2R-4 (PERMANENT REPAIR). (LP #2890030)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON FITTINGS (2 EA) OF FWD SERVICE DOOR JAMB AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0180: CORROSION LEVEL 2. FITTINGS (2 EA) WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2887630)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON LH CUSP MEMBRANE (WEB) STA 832 TO STA 870. SUMMARY OF NRC 0438: CORROSION LEVEL 2. CUSP MEMBRANE WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 209 AND 210. (LP #2883139)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

CRACKED FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 0197: FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 PAR 4 C FIG 201 DETAIL A-A. (LP #2880918)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

CRACKS ON RH WINDOW PANS ON STA Y=238 FWD UP CORNER, STA Y=294 FWD UP CORNER, STA Y=370 FWD UPPER CORNER, STA Y=636 FWD LOWER CORNER, STA Y=851 AFT LOWER CORNER, AND STA Y=870 AFT LOWER CORNER AT PAX CABIN. SUMMARY OF NRC 292: ON RH WINDOW PANS ON STA Y=238 FWD UP CORNER, STA Y=294 FWD UP CORNER, STA Y=370 FWD UPPER CORNER, STA Y=636 FWD LOWER CORNER, STA Y=851 AFT LOWER CORNER, AND STA Y=870 AFT LOWER CORNER AT PAX CABIN WERE REPAIRED PER B-717-200 SRM 56-20-02-2R PROCEDURE 1 STEP 2 B FIGURE 202. (LP #2874952)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,003 hrs · 36,647 cycles

CORROSION ON PLATE IN STA Y=1053 BTW LONGERONS 29R-29L AT AFT BULKHEAD AT AFT CARGO COMPARMENT. SUMMARY OF NRC 203: LEVEL CORROSION 2. DOUBLER (PLATE) WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND PER DGW 5910130-61 REV "ET". (LP #2869463)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,003 hrs · 36,647 cycles

CRACK ON CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX. SUMMARY OF NRC 421: CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203 AND (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND ON TRIM OUT PER B717 DC/MD BOEING NDT SPM PART 6 06-10-01.001. (LP #2869339)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,850 hrs · 36,525 cycles

REAR AIRCRAFT, ABOVE JUMPSEAT, THE EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY PER AMM 33-51-03. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6396492)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,592 hrs · 36,305 cycles

EMERGENCY OVER WING EXIT SIGN IS INOPERATIVE AT B20DC. MAINTENANCE REPLACED THE POWER SUPPLY, EMERGENCY BATTERY AT 20DC, RIGHT HAND AFT EMERGENCY EXIT PER AMM 33-51-06. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,308 hrs · 36,091 cycles

OVERHEAD EMERGENCY LIGHTS IN REAR TAIL CONE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, B5-116, IN THE AFT RIGHT LAVATORY. THE OVERHEAD EMERGENCY LIGHTS IN THE REAR TAIL CONE RETURNED TO NORMAL OPERATION. (LP #6607840)

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 52,286 hrs · 36,077 cycles

THE AFT CATWALK AND AFT EMERGENCY EXIT DOORWAY LIGHTS ARE FLICKERING ON AND OFF. MAINTENANCE REPLACED THE AFT CATWALK EMERGENCY POWER SUPPLY IAW B717 AMM 33-51-03. OPERATIONAL TEST WAS GOOD. (LP #6607820)

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,810 hrs · 35,766 cycles

UPON ARRIVAL AT THE GATE IN ATL, THE AFT EMERGENCY EXIT LIGHT WAS FLASHING. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY. OPERATIONAL CHECK WAS GOOD PER AMM 33-51. (LP #5966954)

Part: LUG — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,797 hrs · 35,757 cycles

CORROSION FOUND ON RT FWD AND AFT FACES OF THE RHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581446-14 REV ORIGINAL. ASSOCIATED ER/A 14-581446 ADDED FOR AC 9518. (LP #1276499)

Part: LUG — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,797 hrs · 35,757 cycles

CORROSION FOUND ON LT FWD AND AFT FACES OF THE LHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581445-14 REV ORIGINAL. ASSOCIATED ER/A 14-581445 ADDED FOR AC 9518. (LP #1276502)

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 51,060 hrs · 35,215 cycles

EXIT LIGHT OVER TAILCONE EXIT AND AIRCRAFT RIGHT STANDBY EMERGENCY LIGHT FLICKER INTERMITTENTLY DURING ALL PHASES OF FLIGHT. MAINTENANCE RE-SET AFT POWER PACK AND THE FLICKER CEASED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #6285367)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,294 hrs · 34,673 cycles

THE EMERGENCY EXIT SIGN IS INOPERATIVE AT LOCATIONS:102. MAINTENANCE FOUND THE AFT LIGHT AND ESCAPE SECTION EMERGENCY LIGHT POWER PACK TO BE INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED TO SERVICE. REPLACEMENT OF THE BATTERY FOR SAID POWER SUPPLY WAS IAW B717 AMM 33-51. (LP #0952024)

Part: COVER — DAMAGED (TAILCONE SLIDE) · airframe 50,181 hrs · 34,592 cycles

THE TAIL-CONE SLIDE COVER HAS A BROKEN CLIP FOR THE RELEASE CABLE. MAINTENANCE INSTALLED A NEW CLIP. (LP #0926413)

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 49,320 hrs · 34,025 cycles

THE EMERGENCY EXIT SIGN ABOVE THE DOOR TO THE AFT ACCESSORY COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BASE AND THE LIGHT RETURNED TO NORMAL OPERATION. (LP #5111438)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 43,956 hrs · 30,214 cycles

VERTICAL STAB RIGHT SIDE BELOW AND FORWARD OF LOWER RIGHT VOR ANTENNA SEVERAL SCREWS PULLED THROUGH SKIN. REPAIR WAS ACCOMPLISHED IAW ER/A 549263-14AD REV. ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUTERSINKS AT FUEL TANK ACCESS NR 520JB, SM. CORROSION OF COUNTERSINK WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND 5 ADJACENT HOLES OUT OF LIMITS WERE FOUND. MAX DIAMETER MEASURED IS 0.557", IT IS OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPLACED AND PN VERIFIED IAW AIPC 57-27-01.

Part: SKIN — GOUGED (RT WING LE) · airframe 43,956 hrs · 30,214 cycles

GOUGES ON RIGHT WING FIXED LE BETWEEN XIS 83.5, XIS 90 AND XIS 120. GOUGES WERE BLENDED IAW SRM 57-00-00 FIG 103. BHEC INSPECTION WAS ACCOMPLISHED ON DRILLED HOLES , HOLE 2, CRACKS WERE FOUND IAW ETI-17-16-109. REPAIRED IAW ETI-17-16-109 REV 2 AND ER/A 549231-14 REV ORIGINAL. SECTION I.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COURTERSINKS AT FUEL TANK ACCESS NR 520EB, SM. CORROSION OF COUNTERSINKS WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND 3 ADJACENT HOLES OUT OF LIMITS WERE FOUND, MAX DIAMETER MEASURED IS 0.562", IT IS OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 RT, CARD 14, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14 AD REV ORIGINAL. LENGTH CRACK 0.150". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REV WITH AMOC IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER 24 MONTHS FROM REPAIR ACCOMPLISHMENT. DAMAGE TOLERANCE ANALYSIS AND A NEW AMOC IS REQUIRED IAW PROCEDURES ESTABLISHED BY ADVISORY CIRCULAR 120-43 UNDER LOG 2634653. AMOC APPROVAL TO AD 2007-11-13 IS REQUIRED FOR SERVICE BEYOND 60,000 TOTAL FLIGHT CYCLES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 LT, CARD 13, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14, REV ORIGINAL. LENGTH CRACK 0.200". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REVISION WITH AMOC IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM REPAIR ACCOMPLISHMENT. DAMAGE TOLERANCE ANALYSIS, AND A NEW AMOC, IS REQUIRED IAW PROCEDURES ESTABLISHED BY ADVISORY CIRCULAR 120-43, UNDER LOG 2634653. AMOC APPROVAL TO AD 2007-11-13 IS REQUIRED FOR SERVICE BEYOND 60,000 TOTAL FLIGHT CYCLES UNDER LOG NR 2634665.

Part: CARGO TRACK — CORRODED (BS 994-1002) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON CARGO TRACK BS 994 - 1002 BETWEEN LONGERONS 27 AND 28R. DUE TO EXCESSIVE CORROSION, THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON PASSENGER ENTRANCE STAIR DOOR. DOOR WAS REPLACED DUE TO EXCESSIVE CORROSION (MORE THAN HALF THICKNESS) IAW SRM 52-00-00 FIG.103.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COURTESINKS ACCESS PANEL 620. CORROSION WAS REMOVED IAW SRM 51-10-04 AND FOUND OUT OF LIMITS IAW SRM 57-10-01 AND THE ACCESS PANELWAS REPLACED. .

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACKS ON NLG JAMB AT STA Y=45 AND STA X=20 AND X=-20, SM, CARD 1, ZONE 115. REPAIR WAS ACCOMPLISHED IAW ER/A 549227-14, REV ORIGINAL AND ETI-17-16-107, REV ORIGINAL.

Part: DRAG BRACE — CORRODED (NLG) · corrosion level 2 · airframe 44,933 hrs · 30,905 cycles

RUST ON NLG DRAG BRACE ASSY. (TAPPER PIN LT/RT, END BEARING LT, RT, AND CROSS TUBE). NOSE LANDING GEAR ASSY WAS REPLACED IN REFERENCE WITH IPC 32-00-00-01 AND THE CARD 3221-4001 ZONE 710 JOB #000-0003. RII COMPLETED.

Part: THRUST WASHER — CORRODED (NLG) · corrosion level 2 · airframe 44,933 hrs · 30,905 cycles

CORROSION ON THRUST WASHER AT NOSE LANDING GEAR. NOSE LANDING GEAR ASSY WAS REPLACED IAW IPC 32-00-00-01 AND THE CARD 3221-4001, ZONE 710 JOB 000-0003. RII COMPLETED.

Part: BEAM — CRACKED (PAX DOOR) · airframe 43,956 hrs · 30,214 cycles

CRACK ON BEAM NR 7, STA 162.5 AT FWD PASSENGER DOOR STRUCTURE, SM, CARD 15, ZONE 820. CRACK ON BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-01.001. CRACK LONG .750" PHASEC 3D C/N: 1381 EXP DATE: 20OCT16. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 484 - 503. REPAIRED IAW SRM 51-41-02, 53-00-55. FIG.215 AND 51-41-05.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER LOWER SKIN BS 446 - 465, X 56 - X 60. REPAIRED PER SRM 53-05-55 FIG. 216, 51-41-02, 51-40-8 PAR. 3, AND 51-10-04 PAR 21-15 AND 37, 51-41-05.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,956 hrs · 30,214 cycles

CRACKED CHANNEL ON FLOOR PANEL. FLOOR PANEL REPAIRED PER SRM 53-20-50 FIG. 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CORROSION ON LT SEAT TRACK, X=44.5 BETWEEN STA 957-STA 960, ON REF CARD 23, ZONE 200. CUT OUT IN TRACK WAS ACCOMPLISHED IAW SRM 53-20-52, FIG 201, ON STA 957-STA 960, X=44.5 NDT INSPECTION ON AREA NO CRACKS WERE FOUND AROUND CUTOUT, IAW NDT SPM 06-10-01-001, AREA WAS TREATED IAW SRM 51-10-04, PAR 21-PAR 15, A PLUG REPAIR WAS INSTALLED IAW SRM 51-41-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACKED LT CLIP FRAME ON CANTED KEELBEAM, STA 681 AND STA 696, CARD 16, ZONE 140. FRAME CLIPS ON STA Y=681 AND Y=696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACKED RT CLIP FRAME ON CANTED KEELBEAM STA 681 AND 696, CARD 17, ZONE 140. FRAME CLIPS ON STA 681 AND STA 696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

EXCESSIVE CORROSION ON LT CUSP MEMBRANE BETWEEN STA 756-775 IN REF CARD 62, ZONE 200. WB, CARD 104, ZONE 200. DUE TO CUSP WEB MEASURE OUT OF LIMITS .028" OF .040", REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 215. RII COMPLETED.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 44,463 hrs · 30,554 cycles

CORROSION ON ACCESS PANEL 370KR VOR / LOCALIZER ANTENNA PANEL.. UPPER RT VOR / LOCALIZER ANTENNA WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01 TEST OK.

Part: ACCESS PANEL — CORRODED (VOR/LOCALIZER) · corrosion level 2 · airframe 44,454 hrs · 30,548 cycles

CORROSION ON ACCESS PANEL 370GR VOR/LOCALIZER ANTENNA PANEL. LOWER RT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.

Part: ACCESS PANEL — CORRODED (VOR) · corrosion level 2 · airframe 44,463 hrs · 30,554 cycles

CORROSION ON ACCESS PANEL 370JL VOR / LOCALIZER ANTENNA PANEL. UPPER LT VOR / LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.

Part: ACCESS PANEL — CORRODED (VOR) · corrosion level 2 · airframe 44,463 hrs · 30,554 cycles

CORROSION ON ACCESS PANEL 370DL VOR/LOCALIZER ANTENNA PANEL. LOWER LT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.

Part: PAN — CRACKED (BS 794) · airframe 43,956 hrs · 30,214 cycles

CRACKED RT RING PAN FWD LWR BS 794. REPAIRED IAW SRM 56-20-02 TYPE B REPAIR FIG 202.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACKED AFT LOWER RING PAN STA Y=636 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 6, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.140" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACKED AFT LOWER RING PAN STA Y=560 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 8 ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH=0.158" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACK FORWARD LOWER RING PAN STA Y=579 RT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 3, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.159" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER AND ADJACENT AREA BETWEEN STA Y=465 AND STA Y=484 UPPER LOWER SKIN FROM X=56 TO X=60 AT PASSENGER CABIN, CARD 50, ZONE 200. DUE EXCESSIVE DAMAGE, CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACKED AFT LOWER RING PAN STA Y=851 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 4, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.132" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACKED AFT UPPER RING PAN STA Y=832, LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 5, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.109" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.

Part: PAN — CRACKED (CABIN WINDOW) · airframe 43,956 hrs · 30,214 cycles

CRACKED AFT LOWER RING PAN, STA Y=617 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 7, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.125" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACK ON STRAP BETWEEN LONGERON 13/14 RT STA 1022, REAR FACE OF BULKHEAD, CARD 23, ZONE 220. SHEAR CLIP WAS REPLACED IAW SRM 53-20-07, 51-40-02, AND 51-41-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 13RT AND 14RT STA Y=1078 TO Y=1074, CARD 1 ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1078 TO Y=1074 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14 REV ORIGINAL SECTION II. REPETITIVE INSPECTIONS EVERY 3,000 FC AFTER SECTION I. PERMANENT REPAIR ACCOMPLISHMENT UNDER LOG 2614111. RII COMPLETED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,956 hrs · 30,214 cycles

CRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONG 13RT AND 14RT STA Y=1087, CARD 2, ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1087 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14, REV ORIGINAL SECTION II. REPETITIVE INSPECTIONS EVERY 3,000 FC AFTER SECTION I. PERMANENT REPAIR ACCOMPLISHMENT UNDER LOG 2614111. RII COMPLETED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

INITIAL CORROSION ON COUNTERSINK AT FUEL TANK ACCESS NR 520, SM, CARD 69, ZONE 000. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01-01 AND MUST BE INSTALLED WITH CARD 2040-0010, ZONE 520, JOB 001-0265. WERE FOUND 9 ADJACENT HOLES AND MAXIMUM DIAMETER ALLOWABLE .660" AND MAXIMUM DIAMETER MEASURED IS .679".

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUNTESINKS AT FUEL TANK ACCESS NR 620 GB, SM, CARD 66, ZONE 000, CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED, IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 620. JOB 001-0281 FOUND 7 HOLES OUT OF LIMITS. MAXIMUM DIAMETER ALLOWABLE IS .532 IN AND MAXIMUM DIAMETER MEASURED IS .628 IN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON RT FLOOR SUPPORT BETWEEN STA 1053-STA 1056 X=-55, W2, SM. CARD 87, ZONE 200. DUE TO EXCESSIVE CORROSION FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02 AND 51-41-05, ORIGINAL THICKNESS 0.080", REMAINING THICKNESS 0.053", THEREFORE IS OUT LIMITS IAW SRM 53-00-00, FIG 103.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620DT, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 620. JOB 001-028I, FOUND 11 HOLES OUT OF LIMITS, MAXIMUM DIAMETER ALLOWABLE IS .660" AND MAXIMUM DIAMETER MEASURED IS .679".

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUNTERSINKS AT FUEL TANK ACCESS NR 620JB, SM. CORROSION WAS REMOVED, REWORKED AREA WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 620. JOB 001-0281, FOUND 13 ADJACENT HOLES, MAX DIAM ALLOWABLE IS .532 IN AND MAXIMUM MEASURED IS .577".

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 520 MB. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0010, ZONE 520, JOB 001-0265 WERE FOUND 10 HOLES OUT OF LIMITS MAXIMUM DIAMETER ALLOWABLE IS .532" AND MAXIMUM DIAMETER MEASURED IS .585".

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620 CB, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 57-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 620. JOB 001-0281 WERE FOUND 6 ADJACENT HOLES AND MAXIMUM DIAMETER ALLOWABLE IS .532 IN AND MAXIMUM DIAMETER MEASURED IS .582".

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,956 hrs · 30,214 cycles

DELAMINATION ON FLOOR PANEL RT AFT LAVATORY. SM, CARD 30, ZONE 000. FLOOR PANEL RT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09, REPAIR 3, PARA 6.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,956 hrs · 30,214 cycles

DAMAGE FLOOR PANEL AT LT AFT LAVATORY, N/P 9981474-71, SH-CP-SM, CARD 51, ZONE 000. FLOOR PANEL AT LT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09 REPAIR 3, PARAGRAPH 6.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION UNDER FLOOR SUPPORT BETWEEN STA 190/205 AREA NEXT TO CUSP ANGLE. IN REF CARD 65, ZONE 200, CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION WEB WAS REPAIRED IAW SRM 51-70-10, FIG 201.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,956 hrs · 30,214 cycles

CORROSION ON RT CUSP LOWER ANGLE SPLICE X=60 BETWEEN STA Y=579 AND Y=598 AT PASSENGER CABIN, SM, CPAX CARD 55, ZONE 200. LOWER ANGLE SPLICE WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,434 hrs · 29,033 cycles

DURING SERVICE CHECK. FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPERATION CHECKED NORMALLY.

Part: FRAME — CRACKED (BS 674) · airframe 40,873 hrs · 27,755 cycles

DURING SPECIAL VISIT FOR FRAME INSPECTION, FOUND RT FRAME STA Y=674.00 RT CRACKED IN UPPER RADIUS. R & R RT OVERWING FRAME AT STA 674 IAW AMDS 5310-01436-03B.

Part: FRAME — CRACKED (BS 674) · airframe 40,873 hrs · 27,755 cycles

DURING FRAME INSPECTION, A CRACK FOUND IN THE RT FRAME. REPAIRED IAW ER/A 530437-14MA.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,331 hrs · 27,312 cycles

DURING SERVICE CHECK, FOUND OVER WING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726. FOR OVER WING AFT EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,246 hrs · 26,406 cycles

AFT CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,246 hrs · 26,406 cycles

FORWARD CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,246 hrs · 26,406 cycles

MID CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 39,246 hrs · 26,406 cycles

FORWARD CTR AISLE OVERHEAD EMER LIGHT CRACKED. R & R LENS IAW AMM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 39,246 hrs · 26,406 cycles

LEFT VERTICAL DORSAL ANGLE FWD 6 INCHES CRACKED AT BS 1121. REPAIRED DORSAL IAW EA.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 39,246 hrs · 26,406 cycles

LEFT VERTICAL STABILIZER TRANSITION FAIRING CRACKED. R & R FAIRING IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 223DF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 221KF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222GF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222VF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 221BF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222AAF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222DF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222ABF DELAMINATED. R & R BOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOORBOARD 222AEF DELAMINATED. R & R BOARD IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 39,246 hrs · 26,406 cycles

RIGHT WING FLAP TRACK FAIRING 630NB CRACKED. REPAIRED FAIRING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

CUSP WEB CORRODED AT BS 436, RBL 54. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

CORROSION ON CUSP WEB AT STATION 526, RBL 54. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

CORROSION ON CUSP WEB AT STATION 517, RBL 54. REPAIRED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT AILERON) · airframe 39,246 hrs · 26,406 cycles

RIGHT WING AILERON OTBD SUPPORT FITTING CRACKED. R & R FITTING IAW SWPM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 180, BL0 TO RBL 20. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 45 TO 52. R & R SUPPORT IAW SRM & DWG.

Part: TRACK — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

TRACK CORRODED BETWEEN BS 160 TO 200, BL 0. R & R TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 3 TO 45. R & R SUPPORT IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 39,246 hrs · 26,406 cycles

R1 DOOR EMER EVAC SLIDE FLOOR FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

R1 DOOR JAMB FWD PANEL CORRODED. R & R PANEL IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

RIGHT WW FWD VERTICAL DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM & ER.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

LEFT WW FWD DOOR CUT OUT INBD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,246 hrs · 26,406 cycles

FRAME CORRODED AT BS 1022 BETWEEN LONGERON 29L TO 29R. REPAIRED FRAME IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,280 hrs · 26,429 cycles

AFT ACCESSORY COMPARTMENT OVERHEAD FWD EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 37,962 hrs · 25,592 cycles

AIR TURN BACK, AT 12K FEET IN CLIMB LOUD BANG MOMENTARILY COMPRESSOR STALL ALERT. R & R NR 2 ENGINE IAW TC.

Part: COVER — UNSECURE (L1 DOOR) · airframe 37,343 hrs · 25,204 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OFF. SECURED COVER IAW MM.

Part: LANYARD — DEFECTIVE (R1 DOOR) · airframe 36,538 hrs · 24,692 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FELL OUT OF HOLDER. REMOVED AND REPLACED LANYARD ASSEMBLY IAW AMM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT SIDE CUSP WEB BETWEEN BS 655 TO BS 715 CRACKED. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT CUSP WEB CRACKED AT BS 675. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 715 TO BS 756. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT CUSP WEB BETWEEN BS 256 TO BS 275 CRACKED. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL DELAMINATED BETWEEN BS 889 TO BS 954, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL DELAMINATED BETWEEN BS 889 TO BS 954, BETWEEN LBL 22 TO LBL 44. REMOVED AND REPLACED PANEL IAW MM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

SEAT TRACK CORRODED BETWEEN BS 897 TO BS 955, RBL 44.5. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 35,543 hrs · 24,069 cycles

L1 DOOR FWD TOP BEAM CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

CUSP WEB CORRODED BETWEEN BS 560 TO BS 579, LONGERON 18L. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 541 TO BS 560. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 35,543 hrs · 24,069 cycles

L1 DOOR TOP INTERCOSTAL AFT SUPPORT CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

FRAME CRACKED AT BS 927 BETWEEN LONGERON 30R AND LONGERON 29R. REPAIRED FRAME PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222ABF DELAMINATED BETWEEN BS 674 TO BS 696, BETWEEN RBL 22 TO RBL 44. REMOVED AND REPLACED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT CUSP PANEL CORRODED BETWEEN BS 715 TO BS 756. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 22JF, STA 465 TO STA 541 LBL 22 TO LBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL B222AMF, STA 813 TO STA 889, LBL 22 TO LBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR RIGHT CUSP WEB LOWER SURFACE CRACKED AT FS 220, RBL 54. REPAIRED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN OVERWING CENTER SECTION, LBL 45 SEAT TRACK SUPPORT FITTING CRACKED AT FS 737. REMOVED AND REPLACED SEAT TRACK IAW SRM AND AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222APF, STA 889, RBL 22 TO RBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN - CUSP WEB RIGHT SIDE HAS LIGHT CORROSION BETWEEN STA 294 - 313. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222YF, STA 694 TO STA 636, RBL 22 TO LBL 22 DAMAGED. REMOVED AND REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222ACF, STA 696 TO STA 737, LBL 22 TO LBL 34 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 221UF, STA 313 TO STA 389, RBL 22 TO LBL 22 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LEFT CUSP WEB CRACKED BETWEEN BS 655 TO BS 715. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 221WF, STA 313 TO STA 389, RBL 22 TO RBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LEFT CUSP WEB CRACKED AT STA 655. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

VERTICAL STIFFENER CRACKED AT FS 655, LBL 24. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222LF, STA 465 TO STA 541, RBL 22 TO RBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222RF, STA 541 TO STA 636, RBL 22 TO RBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT CUSP WEB CORRODED BETWEEN BS 617 TO BS 636. REMOVED AND REPLACED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222AGF, STA 737 TO STA 813, LBL 22 TO LBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN OVERWING CENTER SECTION, RBL 45 SEAT TRACK SUPPORT FITTING CRACKED AT FS 737. REMOVED AND REPLACED SEAT TRACK IAW SRM AND AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222PF, STA 541 TO STA 617, LBL 22 TO LBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222FF, SSTA 408 TO STA 446, RBL 22 TO RBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT SIDE CUSP WEB CORRODED BETWEEN BS 446 TO BS 465. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,543 hrs · 24,069 cycles

MAIN CABIN FLOOR PANEL 222BF, STA 289 TO STA 465 LBL 22 TO LBL 44 DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LONGERON CRACKED AT STA 1133, 2R. REMOVED AND REPLACED LONGERON PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT BS 696 FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM.

Part: RUB STRIP — CORRODED (LT WING) · airframe 35,543 hrs · 24,069 cycles

LEFT UPPER WING CUTOUT RUBSTRIP FOR ACCESS PANEL 520 CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

FRAME CORRODED AT BS 974, BETWEEN L28R - L30L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

RIGHT BS 715 FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LEFT BS 715 FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

FRAME CRACKED AT BS 674, STR 2L. REMOVED AND REPLACED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

EMPENNAGE TAIL SECTION REPAIR STRAP CRACKED AT BS 1200 LEFT SIDE. REMOVED AND REPLACED STRAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,543 hrs · 24,069 cycles

LEFT BS 696 FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 35,543 hrs · 24,069 cycles

LEFT WING AT I/B SIDE OF WING ROOT FWD AREA HAS BONDING STRAP, CRACK AT BOTTOM. REMOVED & REPLACED STRAPS IAW SRM.

Part: NUT PLATE — CORRODED (FAIRING) · airframe 35,543 hrs · 24,069 cycles

RIGHT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 851-927, BETWEEN LONG 19L-19R. REMOVED & REPLACED NUT PLATES IAW SRM.

Part: NUT PLATE — CORRODED (FAIRING) · airframe 35,543 hrs · 24,069 cycles

LEFT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 588-674, BETWEEN LONG 20L - 2R. REMOVED & REPLACED NUT PLATE IAW SRM.

Part: NUT PLATE — CORRODED (FAIRING) · airframe 35,543 hrs · 24,069 cycles

LEFT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 851-927, BETWEEN LONG 19L-19R. REMOVED & REPLACED NUT PLATES IAW SRM.

Part: NUT PLATE — CORRODED (FAIRING) · airframe 35,543 hrs · 24,069 cycles

RIGHT WING TO BODY FAIRING - HAS NUMEROUS CORRODED NUT PLATES BETWEEN STA 588-674, BETWEEN LONG 20L - 2R. REMOVED & REPLACED NUT PLATE IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 35,543 hrs · 24,069 cycles

RIGHT WING FIXED L/E - THE MOST IB END L/E - 2EA BONDING STRAP CRACKED. REMOVED & REPLACED STRAPS IAW SRM.

Part: MOUNT — OBSTRUCTED (R1 DOOR) · airframe 36,029 hrs · 24,380 cycles

R1 SLIDE BAR WILL NOT ENGAGE. REMOVED DEBRIS FROM R1 DOOR GIRT BAR FLOOR MOUNT. GIRT BAR ENGAGES NORMALLY PER AMM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,816 hrs · 24,244 cycles

AFT CARGO DOOR JAMB HAS CORROSION. REPAIRED WEB PER ER AND SRM.

Part: LENS — MISSING (CABIN) · airframe 34,944 hrs · 23,669 cycles

RIGHT EEPLS LENS MISSING AT ROW 3. INSTALLED LENS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,944 hrs · 23,669 cycles

RIGHT EELS BULB INOP AT ROW 3. INSTALLED BULBS PER MM.

Part: SLIDE — UNWANTED DEPLOY (TAILCONE) · airframe 33,966 hrs · 23,034 cycles

TAIL CONE EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 33,648 hrs · 22,825 cycles

COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK & CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS ABOVE GALLEY SERVICE DOOR ARE INOP. TROUBLESHOT PER FIM 33-50-801 FOUND BATTERY PACK B5-259 BAD AND WIRE AT LIGHTS ASSY L2-786 TERMINAL BROKE. REPAIRED WIRE REF SWPM 20-00 AND REPLACED BATTERY PACK B5-259 REF AMM 33-51-03 ALL PS CHECK GOOD.

Part: SKIN — CRACKED (LT MLG DOOR)

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

Part: ATTACH FITTING — CORRODED (GIRT BAR)

GALLEY ENTRANCE FWD AND AFT GIRT BAR ATTACH FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR ATTACH FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: SKIN — DAMAGED (FUSELAGE)

PASSENGER ENTRANCE AREA FUSELAGE SKIN, STA 189 TO 229, LONG L15L TO L18L, DAMAGED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER B717 SRM 53-00-01 FIG 201 REPAIR 6.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 238, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 191, LBL 44.5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 238, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: LONGERON — CRACKED (FUSELAGE)

PASSENGER ENTRANCE AREA FUSELAGE LONGERON WEB, STA 208, LONG L15L, CRACKED. ACCOMPLISHED FUSELAGE LONGERON WEB FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 2 FWD EMERGENCY LIGHT MISSING BULBS & LENS. INSTALLED LAMP AND LENS IAW B717 MM 33-51-04.

Part: COVER — MISSING (EXIT SIGN)

ROW 1 OVERHEAD EXIT SIGN COVER REMOVED FROM AIRCRAFT 719. INSTALLED EXIT SIGN LENSE COVER PER 717 AMM 33-51.

Part: FITTING — DIRTY (GIRT BAR)

L-1 DOOR GIRT BAR WILL NOT ENGAGE FLOOR FITTING. CLEANED & OPS CHECK GOOD L-1 DOOR GIRT BAR ATTACH POINTS REF MM 52-11.

Part: LANYARD — LOOSE (EVAC SLIDE)

L1 DOOR SLIDE ATTACHMENT LOOSE. RE-SECURED FRONT ENTRY DOOR SLIDE ATTACHMENT LANYARD. REF AMM 25-61.

Part: COVER — LOOSE (EVAC SLIDE)

FRONT ENTRY SLIDE PACK PLASTIC COVER LOOSE AND SLIDE GIRT BAR CLIP BROKEN. RE-INSTALLED LANYARD ASSEMBLY CLIP, CHECKS OK. REF MM 25-61.

Part: PIN — MISSING (EVAC SLIDE)

MAIN FWD CABIN DOOR EMERGENCY SLIDE MISSING PIN FOR SECONDARY DEPLOYMENT. REMOVED AND REPLACED DOOR SLIDE, AND L1 DOOR LANYARD. REF B717 MM 25-61.

Part: PTU — FAULTY (HYDRAULIC SYS)

RIGHT HYDRAULIC QUANTITY LOW, 3.1. EMERGENCY DECLARED ON DESCENT. WHILE INSPECTING FOR HYDRAULIC LEAK FOUND PTU OVERFLOW JAR FULL AND OVERFLOWING. REMOVED AND REPLACED PTU IAW B717 MM 29-22-01. OPS AND LEAK CHECK GOOD.

Part: ENGINE — FAILED (LEFT)

PASSING 5000FT ON CLIMB LEFT ENGINE FAILED WITH AUDIBLE BANG, COMP STALL INDICATION AND 1150 TGT EXCEEDENCE. REMOVED & REPLACED NR 1 ENGINE IAW AIRTRAN ENG CHANGE CARD 603.

Part: CRADLE — DEFECTIVE (CABIN)

EMERGENCY LIGHTS OUT ON ROWS 1-10. REMOVED AND REPLACED BATTERY SUPPLY CRADLE ASSY IAW B717 MM 33-51.

Part: PAN — CORRODED (CARGO BAY)

FWD CARGO COMPARTMENT DOOR CUTOUT LOWER PAN HAS CORROSION BEYOND LIMITS. INSTALLED NEW PAN AND SPLICES AS PER B717 SRM 53-20-15 FIG 201.

Part: FRAME — CRACKED (FUSELAGE)

SMALL CRACK NOTICED AT AFT INTERIOR FUSELAGE TAIL COMP. LEFT SIDE CANTED AREA STA 1178.225 BETWEEN LONG 13 AND 14 LEFT. INSTALLED FORMED ANGLE REPAIR ON LEFT FUSELAGE CANTED FRAME 1178 BETWEEN LONG 13 AND 14 LEFT PER B717 SRM 51-70-11 FIG 201.

Part: TIRE — BLOWN (NR 3)

TIRE BLEW AT VR WITH ENG VIBE HIGH. REMOVED AND REPLACED NR 3 MLG TIRE.

Part: SWITCH — INOPERATIVE (MLG)

3 GEAR UNSAFE ON EXTENSION OF GEAR. BAD SWITCH (S-189) REPLACED (P/N DT2R-A7) SENSING AND CONTROL MICRO SWITCH.

Part: TURBINE — FAILED (NR 2 ENGINE)

NR 2 ENGINE FAILED IN CLIMB AT 9,600 FEET HEARD BANG AND SUDDEN YAW TO RIGHT. TURBINE GAS TEMPERATURE INDICATIONS AT 1150 CELSIUS RIGHT ENGINE INSTRUMENTS SPOOLED DOWN TO ZERO. ENGINE RIGHT BEARING OVERHEAT ALERT AND ENGINE RIGHT SYSTEM FAIL ALERT. REMOVED AND REPLACED NR 2 ENGINE.

Part: LIGHT — LOOSE (CABIN)

FOUND EMERGENCY PATH LIGHT ASSEMBLY LOOSE AT SEAT 26. REMOVED AND REPLACED LIGHT FAIRING ON SEAT 26 IAW B717 MM 25-23.

Part: LIGHT — LOOSE (CABIN)

FOUND EMERGENCY PATH LIGHT ASSEMBLY LOOSE AT SEAT 24. REMOVED AND REPLACED LIGHT FAIRING ON SEAT 24 IAW B717 MM 25-23.