N919AT

Part: COALESCER BAG — ODOR (ZONE 100) · airframe 59,018 hrs · 43,134 cycles

SMOKE AND ODOR IN CABIN AT GATE WITH PASSENGERS ON BOARD AT DEPARTURE TIME. F/A SAYS SHE SMELLS OIL IN THE CABIN. DECONTAMINATED AFT BULKHEAD AND INSTALLED NEW INSULATION PER B717 AMM 25-85. R & R COALESCER BAG ASSEMBLY PER AMM 21-54. (1219929)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,137 hrs · 42,347 cycles

CRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER ERA 626154-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626154-14 REV 3. SEC II ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR, LOG 0961069. (LP #0963096)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,137 hrs · 42,347 cycles

CRACK ON FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE. SUMMARY OF NRC 00056: FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE WAS REPAIRED PER PRI 626216-14 REV 1 AND ER/A 626216-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0964238)

Part: SKIN — CRACKED (ZONE 200) · airframe 58,137 hrs · 42,347 cycles

CRACKS ON FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00048: FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER ERA 626165-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626165-14 REV 3. ASSOCIATED ER/A 14-626165 ADDED FOR AC 9579. (LP #0961401)

Part: CABLE — OUT OF TRACK (ZONE 100) · airframe 58,105 hrs · 42,320 cycles

GOT A TAILCONE UNLOCK MSG DURING TAXI IN TO GATE. WHILE VERIFYING M PROCEDURES FOR MEL 53-52-018, FOUND LOCKING CABLE LEADS LOOSE, MEL STATES LEADS SHOULD BE TIGHT/NO EVIDENCE OF SLACK. FOUND CABLE OUT OF T FITTING. THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE BEING OUT OF THE FITTINGS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001 TAILCONE SERVICE. FUNCTIONAL CHECK WAS SATISFACTORY. RESECURED CABLE UNSAFE LIGHT IS NOW OUT. PERFORMED FUNCTIONAL TEST OF TAILCONE RELEASE SYSTEM IAW B717 AMM 53-52-01. OK TO INSTALL TAIL SLIDE QC 5424 ALL RII COMPLETED QC 5424. (LP #7236068)

Part: SKIN — DENTED (ZONE 800) · airframe 58,043 hrs · 42,268 cycles

GATE AGENT REPORTS L1 DOOR NOT CLOSING AUTO LEVER NOT INSTALLED. MTC INSPECTED DOOR FOUND DENT IN BOTTOM LEFT CORNER WITH DOOR CLOSED FROM JET BRIDGE PUSHING UP ON DOOR. FOUND DAMAGE ON INNER DOOR BUSSLE AND OUTER LEFT BOTTOM CORNER (NR 592713). COLD WORKED LOWER DOOR EDGE STRAIGHT. NO DEFECT NOTED IAW B717 SRM 52-00-00-2R PROCEDURE 3 REPAIR 3. (LP #7236002)

Part: HINGE FITTING — GOUGED (ZONE 600) · airframe 57,754 hrs · 42,019 cycles

-AD- WHILE ACCOMPLISHING NDT INSPECTION PER AMDS 5720-01103-01B FOUND GOUGE IN THE RH AFT SPAR ROUGHLY 8" OUTBOARD OF FLAP HINGE. AREA MARKED. COMPLIED WITH ALL STEPS IF ER/A 624537-14AD PRI REV 1, 728756 BB. ALL WORK ACCOMPLISHED PER FINAL ER/A 624537-14AD. (LP #825281)

Part: TRANSMITTER — OUT OF TOLERANCE (TE FLAPS) · airframe 57,707 hrs · 41,983 cycles

SHIP 9579 -ATB/DE- THE CREW ACCOMPLISHED AN AIR TURN BACK TO ATL DUE TO A "FLAPS DISAGREE" MESSAGE AFTER FLAP AND SLAT RETRACTION. AN EMERGENCY WAS DECLARED WITH ATC. CORRECTIVE ACTION: MAINTENANCE FOUND THE RIGHT FLAP POSITION TRANSMITTER OUT OF TOLERANCE, REPLACED TRANSMITTER AND PERFORMED ALL RETURN TO SERVICE TESTS. (LP #6857332)

Part: IDG — FAILED (LT GENERATOR) · airframe 57,331 hrs · 41,659 cycles

SHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE "LEFT GENERATOR FAIL" MESSAGE DURING APPROACH INTO PHL. THE APU WAS ALREADY ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT IDG, PERFORMED ALL OPERATIONAL CHECKS, AND RETURNED THE AIRCRAFT TO SERVICE. (LP #6681876)

Part: LIGHT — INOPERATIVE (CABIN OVERWING) · airframe 56,438 hrs · 40,874 cycles

CABIN OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACKS AT B5-118 & B5-130 BAD. REPLACED THE EMERGENCY BATTERY PACKS PER B717 AMM 33-51. OPERATIONAL CHECK OK. AIRCRAFT OK FOR SERVICE. (LP #6186026)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,101 hrs · 39,684 cycles

TWO FWD WINDOW SIGN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED FWD WINDOW EMERGENCY EXIT SIGN BATTERY PACK IAW B717 AMM 33-51. THE OPERATIONAL CHECK PERFORMED WAS GOOD. THE AIRCRAFT RETURNED TO SERVICE. (LP #9376083)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,929 hrs · 39,548 cycles

SHIP 9579 -FCNT/DE- THE CREW NOTED A "PSEU" MESSAGE DISPLAYED ON THE EAD DURING CRUISE. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED WITH ATC, AND THE CREW SAFELY LANDED IN EWR WITH ZERO DEGREE FLAPS AND SLATS. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE PSEU WAS FAULTY AND REPLACED IT. ALL RTS TESTS PERFORMED PASSED AND THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4289890)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,857 hrs · 38,627 cycles

SHIP 9579 -DIV- THE AIRCRAFT WAS DIVERTED TO IAD DUE TO A SUSPECTED HIGHER THAN NORMAL FUEL CONSUMPTION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE CENTER TANK FUEL QUANTITY INDICATION SYSTEM IS FAULTY. CENTER FUEL QUANTITY INDICATION SYSTEM WAS FORWARDED TO MEL AND THE AIRCRAFT RETURNED TO SERVICE. (LP #4705996)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

CRACK ON FRAME STA 1037 AND S-14L AT PAX CABIN. SUMMARY OF NRC 00398: CRACK ON FRAME STA 1037 AND S-14L AT PAX CABIN WAS REPAIRED PER ER/A 609263-14 REV. ORIGINAL SECTION I (PERMANENT REPAIR). ASSOCIATED ER/A 14-609263 ADDED FOR AC 9579. (LP #2832477)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

EXISTING REPAIR LOCATED BETWEEN FS 427-446 AT STR 28R HAS DAMAGE EXTENDING FORWARD OF THE REPAIR DOUBLER. SUMMARY OF NRC 0489: THIS ACTIVITY MUST BE FOLLOW-UP WITH ER/A 526543-14. ACCOMPLISH SECTION I REPETITIVE INSPECTION INSTRUCTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES FROM 24,361, AIRCRAFT TOTAL FLIGHT CYCLES UNDER LOG #1469621. ASSOCIATED ER/A 14-526543 ADDED FOR AC 9579. (LP #2830150)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

REPAIR DOUBLER LOCATED AT THE AFT CARGO DOOR-AFT FRAME (FS 994 AND STR 26R) IS DAMAGED ON THE EXTERIOR SURFACE. SUMMARY OF NRC 00477: REPAIR DOUBLER LOCATED AT THE AFT CARGO DOOR AFT-FRAME (FS 994 AND STR 26R) WAS REPLACED PER B717-200 SRM 53-20-15-2R PRODECURE 11 (PERMANENT REPAIR). PERFORM VISUAL INSPECTION INTIAL AT 8000 CYCLES AND REPETITIVE EVERY 8000 CYCLES PER B717-200 SRM 53-20-15-2R PROCEDURE 11 REPAIR 11 STEP 7 TABLE 202 OPTION 1. (LP #2829539)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,839 hrs · 38,609 cycles

CORROSION AROUND SETTLEMENT AREA OF VOR/LOC ANTENNA PANELS UPPER LH (2L), LOWER LH (1L), UPPER RH (2R), AND LOWER RH (1R). SUMMARY IN REF NRC 00403: LEVEL CORROSION 2. SETTLEMENT AREA OF VOR/LOC ANTENNA PANELS UPPER LH (2L), LOWER LH (1L), UPPER RH (2R), AND LOWER RH (1R) WERE REPLACED PER BOEING CMM 34-51-02. (LP #2826891)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

CRACKS ON FRAME STA 1022 AND S-7L AT PAX CABIN. SUMMARY OF NRC 00397: CRACKS ON FRAME STA 1022 AND S-7L AT PAX CABIN WAS REPAIRED PER ER/A 609314-14 REV. ORIGINAL SECTION I (PERMANENT REPAIR) AND PRI 609314-14 REV 1. ASSOCIATED ER/A 14-609314 ADDED FOR AC 9579. (LP #2827753)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,839 hrs · 38,609 cycles

CORROSION ON RH OUTBRD SEAT TRACK FROM STA Y=865 TO 1002 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 503: LEVEL CORROSION 2. SEAT TRACK FROM STA Y=865 TO 1002 AT PASSENGER CABIN STRUCTURE WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2819691)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,839 hrs · 38,609 cycles

AFTER CORROSION REMOVAL ON OTBD SEAT TRACK LH ON STA Y:577 TO 578 AT PAX CABIN, THE TRACK WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00500: CORROSION LEVEL 2. SEAT TRACK LH OUT OF LIMITS ON STA Y:577 TO 578 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1. (LP #2808098)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

CRACK ON DOOR BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT. SUMMARY OF NRC 00163: BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (LP #2800335)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 53,839 hrs · 38,609 cycles

CORROSION ON FWD AND AFT REPAIRS SPLACE DOUBLERS DOOR JAMB AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00100: CORROSION LEVEL 2. FWD AND AFT REPAIR SPLICE DOUBLERS AT AFT CARGO COMPARTMENT DOOR JAMB (C2) WERE REPLACED PER B717-200 SRM 53-20-15-2R-7, 51-41-05-0G PAR 8, AND 51-41-02-0G. (LP #2798699)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

GOUGE WAS FOUND ON PERMANENT REPAIR BTW STA Y=243 AND 3" ABOVE OF LONGERON 17L AT FUSELAGE. SUMMARY OF NRC 00283: DOUBLER ON PERMANENT REPAIR BTW STA Y=243 AND 3" ABOVE OF LONGERON 17L AT FUSELAGE WAS REPLACED PER B717 SRM 53-00-01-2R PROCEDURE 6. PERFORM A GVI EVERY 8000 CYCLES PER B717-200 SRM 53-00-01-2R-6. (LP #2798609)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

CRACK ON CUSP MEMBRANE (WEB) X=56 AND STA 611 AT CPAX. CRACK WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 204. (LP #2795916)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,839 hrs · 38,609 cycles

CRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX. SUMMARY OF NRC 00431: CRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX WAS REPAIRED PER B717-200 SRM 55-00-55-2R PROCEDURE 4 PAR 5 FIG 217. (LP #2793591)

Part: CUSP WEB — CRACKED (BS 715) · airframe 53,839 hrs · 38,609 cycles

CRACK CUSP MEMBRANE AT STA 715 L-18LH. SUMMARY OF NRC 00296: CUSP MEMBRANE AT STA 715 L-18LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R- PROCEDURE 4. (LP #2787531)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,745 hrs · 38,524 cycles

SHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC INTO ATLANTA DUE TO A SUSPECTED LEFT SIDE BRAKES GRABBING CONDITION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THE PROBLEM WAS AN INTERNAL BEARING FAILURE OF THE #1 MLG WHEEL ASSEMBLY. (LP #4746476)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,973 hrs · 37,856 cycles

DURING PRE-FLIGHT CHECK, FOUND BOTH AFT EMERGENCY OVER WING EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT B5-119 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #9509744)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,760 hrs · 37,656 cycles

EMERGENCY LIGHTS ON CEILING FROM ROW 13 AND FORWARD ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHTS BATTERY REF B717 AMM 33-51. OPERATIONAL CHECK PASSED. (LP #9419705)

Part: WIRE — BROKEN · airframe 52,672 hrs · 37,578 cycles

LOOSE ANTI-FOG WIRES AT CAPTAIN SIDE WINDOW. ARCHED TWICE WITH ANTI-FOG ON. MAINTENANCE FOUND BROKEN WIRES ON CAPTAIN SIDE WINDOW. REPAIRED WIRES REF ERA 95-521804-14. AIRCRAFT IS OK FOR SERVICE. (LP #9491044)

Part: NONE — NONE · airframe 52,535 hrs · 37,440 cycles

THE FORWARD OVERHEAD EXIT SIGN IS MISSING. MAINTENANCE FOUND THE MISSING LENS COVER AND RESECURED IT TO THE LIGHT. OPERATIONAL CHECK WAS NORMAL IAW B717-AMM 33 -51. (LP #9590556)

Part: NONE — NONE · airframe 50,646 hrs · 35,711 cycles

THE EXIT SIGN ON CEILING NEXT TO ROW 1 FELL FROM ITS MOUNT UPON LANDING. MAINTENANCE REPLACED THE EXIT SIGN REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #8120394)

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 49,896 hrs · 35,058 cycles

AFT CARGO DOOR SKIN BENT ON FWD SIDE JUST UP FROM SCUFF PLATE REF NRC 92. REMOVED AND REPLACED AFT CARGO DOOR PER B717 AMM 53-31-01 ON NRC 92. (LP #1875796)

Part: DOOR FRAME — GOUGED (FWD CARGO) · airframe 49,877 hrs · 35,042 cycles

FWD CARGO DOOR CUTOUT, AFT SIDE, HAS DEEP GOUGES AND SCRATCHES APPROX. FROM LONGERON 25R TO 26R. MARKED. REPAIRED PER B717 SRM 53-20-15-2R REPAIR 12. SEE NR 123, TASK CARD # 001-0372:5231-2002/005. (LP #1874032)

Part: LONGERON — CORRODED (BS 907-966) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

AFT CARGO BILGE AREA HAS CORROSION L29L STA 907 TO STA 966 "MARKED". REPLACED LONGERON PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1871297)

Part: SUPPORT — CORRODED (BS 1022-1037) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

CORROSION WAS FOUND BETWEEN STA 1022 AND 1037 ON WASTE BLOWER SUPPORT CONNECTED TO L30. MARKED IN RED. SUMMARY SEE NRC 001-0291:2550-2003/001 00187: REPLACED INTERCOSTAL PER B717 SRM 51-40-02. (LP #1870653)

Part: FRAME — CORRODED (BS 1022 S29L-R) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

CORROSION WAS FOUND ON FRAME AT STA 1022 IN MULTIPLE LOCATIONS. BETWEEN L29 AND R29. BETWEEN L27 AND L25. BETWEEN R27 AND R28. ALL MARKED IN RED. SUMMARY SEE NRC 001-0291:2550-2003/002 00188: INSTALLED NEW FRAME PER B717 SRM 53-20-07-2R. (LP #1870223)

Part: FRAME ANGLE — CORRODED (BS 1022 S25L-R) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

REPLACE FRAME CLIP AT STA 1022 25L TO 25R DUE TO CORROSION. SUMMARY FROM NRC 00401: REPAIRED FRAME CLIP PER B717 SRM 53-00- 06-2R PROCEDURE 3. (LP #1870910)

Part: INTERCOSTAL — CORRODED (BS 1022-1037 L30) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

THE AFT CARGO BILGE AREA HAS CORROSION ON INTERCOSTAL AT L30 STA 1022 TO STA 1037 "MARKED". SUMMARY NRC 062-0008:5331-2001/015 00363: REPLACED INTERCOSTAL PER B717 SRM 51-40-02. (LP #1870642)

Part: SPLICE — CORRODED (BS 900-966) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

AFT CARGO BILGE AREA HAS CORROSION L30 STA 900 AT FACTORY SPLICE TO STA 966. "MARKED". SUMMARY NRC 062-0008:5331-2001/009 00357: INSTALLED NEW SPLICE PER LONG BEACH DRAWING #3914677, AND PER B717 SRM 51- 40-02. (LP #1869668)

Part: SHEAR TIE — CORRODED (BS 907 L28-29L) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

AFT CARGO BILGE AREA HAS CORROSION STA 907 FRAME SHEAR CLIP L29R - L28L "MARKED". REPLACED FRAME CLIP PER B717 SRM 53-00-06-2R PROCEDURE 2, REF NRC 353. (LP #1868907)

Part: PAN — CORRODED (FWD CARGO) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

THE FWD CARGO DOOR PAN IS HEAVILY CORRODED IN FOUR LOCATIONS AROUND THE LOWER STOP FITTINGS. MARKED IN RED. REPAIRED PER B717 SMR 53-20-15-2R PROCEDURE 6. (LP #1869660)

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 49,877 hrs · 35,042 cycles

FLOOR PANEL 211BF AT L-1 DOOR O/B FLOOR SUPPORT IS CORRODED. SUMMARY NRC 001-0024:2040-0024/002 00416: REPLACED SUPPORT REF DWG #9936534. (LP #1866600)

Part: PAN — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

FWD CARGO DOOR PAN HEAVILY CORRODED IN FOUR (EACH) LOCATIONS AROUND THE LOWER STOP FITTINGS. MARKED IN RED. REPAIRED PER B717 SMR 53-20-15-2R PROCEDURE 6. (LP #1862112)

Part: PRESSURE BLKHD — CORRODED (BS 1053 L30) · corrosion level 2 · airframe 49,877 hrs · 35,042 cycles

CORROSION AFT OF STA 1053 ON LOWER PART OF P-DOME NEAR L30. MARKED IN RED. (FROM N/R 191). REPLACED DOUBLER PER B717 SRM 51-40-02. (LP #1862416)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 49,873 hrs · 35,041 cycles

FOUND TWO BATTERY PACKS FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE TWO BATTERY PACKS IN THE FORARD CABIN PER B717 AMM 33-51-03. (LP #1814149)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,264 hrs · 33,129 cycles

EMERGENCY LIGHTS AT SEAT 20 LT AND RT ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT 23 OVERHEAD. OPERATIONAL CHECK WAS GOOD PER AMM 33-51. (LP #5026121)

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 47,206 hrs · 33,084 cycles

THE EMERGENCY EXIT SIGN IN CENTER AISLE CEILING ABOVE OVER WING EXITS LIGHT WAS TOO DIM TO BE OF PROPER USE. FOUND SEVERAL LAMPS OUT IN EXIT SIGN IN CENTER AISLE IN CEILING ABOVE OVER WING EXITS AND RE-LAMPED IN REF WITH AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #4250665)

Part: COVER — BROKEN (EXIT SIGN) · airframe 46,701 hrs · 32,720 cycles

THE RIGHT AFT OVERWING EXIT SIGN COVER IS BROKEN. MAINTENANCE REPLACED THE EXIT SIGN COVER AT THE RIGHT AFT OVERWING EXIT HATCH PER AMM 33-50.

Part: BUFFER VALVE — LEAKING (NR 1 ENGINE) · airframe 46,576 hrs · 32,615 cycles

WHILE TAXIING IN, DURING APU START-UP, OILY FUEL FUMES ARE NOTICEABLE THROUGHOUT THE ENTIRE CABIN AND COCKPIT. SMELL DISSIPATES A MINUTE OR TWO AFTER APU RUNNING. C/W NO GO ODI CHECK STEPS 1 THRU 5 PER STEP 6 REMOVED L/H AND R/H BUFFER VALVES, R/H SHOWS NO OBVIOUS DAMAGE OR BLOCKAGE, SUSPECT L/H HAS LEAK. REF 717 AMM 75-22-01-000-801. REINST. NUM 2 ENG BUFFER VLV. AND INST. NEW BUFFER VLV. ON NUM 1 ENG PER B717 AMM 75-22. NO GO ODI PREVENTION COMPLETED. APU DEFERRAL ON LP 5081052. VERIFICATION FLT. ON LP 5081054. (LP5081050)

Part: PIN — BENT (COCKPIT LIGHT) · airframe 46,550 hrs · 32,598 cycles

ELECTRICAL PANEL LIGHTS INCORRECT. BURNING SMELL FROM OVHD PANEL. ELECTRICAL PANEL LIGHTS ARE CORRECT PER SSM 31-12-0. FOUND LEFT APU ANNUNCIATOR LIGHT FOR LEFT BUS DAMAGED WITH BENT PINS. REMOVED AND REPLACED INDICATOR LIGHT ASSY L2-1510 PER WDM 24-27. PERFORMED DETAILED INSPECTION OF COCKPIT AREA, OVERHEAD AND C/B PANELS. OPERATED COCKPIT LIGHTING FULL BRIGHT AND DIM. NO OTHER DEFECTS NOTED.

Part: SIGN — DAMAGED (CABIN) · airframe 46,257 hrs · 32,399 cycles

ON CEILING AT ROW 1, THE EXIT SIGN IS MISSING HALF ALSO CLOSE NOT ILLUMINATED. MAINTENANCE REPLACED THE EXIT SIGN PER AMM 33-51-18. OPERATIONAL CHECK IS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP 4689852)

Part: LANYARD — DAMAGED (TAILCONE RELEASE) · airframe 45,302 hrs · 31,697 cycles

TAILCONE DEPLOYMENT SYSTEM LANYARD FRAYED AND WORN. REPLACED TAILCONE LANYARD IAW AMM 53-52-01, AND 25-61-02.

Part: BULKHEAD — PUNCTURED (BS 218) · airframe 45,292 hrs · 31,687 cycles

FWD CARGO BULKHEAD, BS 218, RBL 15, Z=-20 HAD A PUNCTURE. REPAIRED THE BULKHEAD IAW ER/A 567762-14, REV ORIGINAL.

Part: BULKHEAD — PUNCTURED (E/E BAY) · airframe 45,292 hrs · 31,687 cycles

E & E BAY, AFT BULKHEAD, 12 INCHES RIGHT OF BL 0, 5 INCHES UP FROM BILDGE, THE BULKHEAD WAW PUNCTURED. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-00, REPAIR 2.

Part: BULKHEAD — PUNCTURED (BS 218) · airframe 45,292 hrs · 31,687 cycles

FWD CARGO BULKHEAD BS 218, LBL 33, Z=-30 HAD A PUNCTURE. ACCOMPLISHED A PERMANENT REPAIR TO FWD CARGO FWD BULKHEAD IAW SRM 53-00-00, REPAIR 2.

Part: BLOWER — FAILED (LAVATORY) · airframe 43,092 hrs · 30,159 cycles

AT GATE PRIOR TO PUSH BACK, A STRONG ELECTRICAL ODOR EMANATED FROM THE AFT LAVATORY AREA IN THE CABIN. MAINTENANCE FOUND THE LAVATORY BLOWER MOTOR CIRCUIT BREAKER HAD TRIPPED OPEN. MAINTENANCE REPLACED THE LAVATORY WASTE VENT SYSTEM BLOWER.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 41,187 hrs · 28,873 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER LENS WAS DAMAGED. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 40,768 hrs · 28,546 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY EXIT IDENTIFIER IN THE FLOOR AT SEAT 19AB IN THE CABIN WAS MISSING, AND INOPERATIVE. MAINTENANCE INSTALLED THE FLUORESCENT STRIP FOR THE NOTED AREA AND THE OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,161 hrs · 28,016 cycles

EIGHT EMERGENCY LIGHTS INOPERATIVE. LIGHTS WERE REPLACED IAW 33-52-00.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,183 hrs · 28,037 cycles

CORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW=10, XCW=50 AT LT MLG WHEEL WELL. SM, MLG. CORROSION ON WING BOX SKIN WAS ATTENDED WITH ER/A 545162-14, REV ORIGINAL AND SRM 51-41-03, 51-41-01, 51-41-05, 51-10-04 PAR 14, 21, 26. OLYMPUS NDT 3DL, SONO PEN V260 SM EXP. DATE: 08DEC16. RII COMPLETED.

Part: SKIN — CORRODED · airframe 40,161 hrs · 28,016 cycles

CORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS=10 TO XCW=50 AT RT MLG WELL CORROSION ON WING SKIN WAS ATTENDED WITH ER/A NR 545162-14, REV ORIGINAL 546475-14, REV ORIGINAL AND SRM 51-10-04, 51-41-03, 51-70-10, 51-70-11 AND 51-41-05.

Part: CARGO TRACK — CORRODED (BS 813-889) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON RT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. RT TIE TRACK FROM BS 813 TO 889 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. OLYMPUS 38 DL PLUS SONOPEN V260SM 25AUG16 AMX-PND-148. ORIGINAL THICKNESS IS 0.090" REMAINING THICKNESS IS 0.025" OUT LIMITS IAW SRTM 53-20-52, FIG 105.

Part: CARGO TRACK — CORRODED (BS 994-1022) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON RT TIE TRACK FROM BS 994 TO 1022 AT AFT CARGO COMPARTMENT, C2. TIE TRACK FROM BS 994 TO 1022 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. ORIGINAL THICKNESS IS 0.090" MINIMUN REMAINING IS 0.030" OUT LIMITS IAW SRM 53-20-52, FIG 101. OLYMPUS 38DL PLUS SONOPEN SM AMX-PND-145 25AUG16.

Part: CARGO TRACK — CORRODED (BS 908-1022) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON LT TIE TRACK FROM BS 908 TO 1022 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 908 TO 1022 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, CIC APPLIED, AND REPAIR PARTS WERE INSTALLED IAW SRM 53-20-51, FIG 1, ITEM 9, 51-40-08, 51-10-04, PAR 15/21, 37, 51-41-02, 51-41-01, 51-41-05, AND 53-20-52 REP 4, FIG 201. OLYMPUS 38DL PLUS SONOPEN V260 SM AMX PND 148 25AUG16.

Part: CARGO TRACK — CORRODED (BS 813-889) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON LT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 813 TO 889 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, AND CIC APPLIED IAW SRM 53-20-51, FIG 1, ITEM 3, 51-40-08, 51-10-04, PAR 15, 21, 37, 51-41-02, 51-41-01, 51-41-05. OLYMPUS 38DL PLUS SONOPEN V260SM AMX-PND -148 25AUG16.

Part: SKIN — CRACKED (BS 100) · airframe 40,158 hrs · 28,014 cycles

CRACKED EXTERNAL FUSELAGE SKIN BS 100 AND LONGERON 28R. FUSELAGE SKIN WAS PERFORMED IAW SRM 53-10-01, FIG 201.

Part: FRAME — CRACKED (BS 1087) · airframe 40,158 hrs · 28,014 cycles

CRACKED FRAME ANGLE BS 1087 BTW LONGERONS 13-14R AT AFT ACCESSORIES COMPARTMENT. FRAME ANGLE WAS REPLACED IAW AMM 21-22-01, 21-51-04, SRM 51-41-02, 51-41-05, DWG 9971140, REV F.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 40,158 hrs · 28,014 cycles

DELAMINATED RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214. RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214 WAS REPAIRED IAW SRM 51-70-02, REPAIR 3. RT WING INBD SPOILER, PANEL WAS REMOVED AND INSTALLED TO FACILITATE OTHER ACTIVITIES IAW AMM 27-60-01-400-801. RII COMPLETED BY INSPECTION STAMP DELTA ID NR 693373 INSPECTOR JMSM 200100699 TECHOPS.

Part: SKIN — CANNING (BS 1189-1200) · airframe 40,158 hrs · 28,014 cycles

DENT WITH OIL CAN EFFECT ON EXTERNAL FUSELAGE, SKIN BS 1189 CANT TO 1200 CANT BETWEEN 6-7 O'CLOCK POSITION, SM, FS. FUSELAGE SKIN WAS REPAIRED IAW ER/A 545165-14, REV ORIGINAL.

Part: BEARING — WORN (LT AILERON) · airframe 40,158 hrs · 28,014 cycles

FREEPLAY ON AILERON SECTOR BUSS AT LT WING. FREE PLAY ON AILERON SECTOR BUS WAS CORRECTED BY REPLACING BEARING ON BUS SECTOR IAW CMM 27-10-16. RII COMPLETED BY INSPECTION.

Part: HINGE FITTING — WORN (HORIZONTAL STAB) · airframe 40,158 hrs · 28,014 cycles

FREEPLAY ON EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STAB. AYP, CARD 14, ZONE 340. EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STABILIZER WAS REPLACED IAW CMM 27-30-2 AND FREE PLAY WAS CORRECTED. RII COMPLETED

Part: HINGE FITTING — DAMAGED (RT ELEVATOR) · airframe 40,158 hrs · 28,014 cycles

SCRATCHES ON BUSHINGS ON RT ELEVATOR HINGE FITTINGS BS XE=49. AYP, CARD 1, ZONE 340. UPPER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WAS CLEANED IAW PS 900-1-2-1 NR 001 AND DAMAGE WAS NOT FOUND. LOWER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WAS REPLACED WITH REF CARD NR 25 A/C ZONE 340.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS NR 520CB, 520DB, 520EB, AND 520GB, AYP. CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS 520CB, 520DB, 520EB, AND 520GB WAS REMOVED, COUNTERSINK HOLES AT FUEL ACCESS 520CB AND 520EB WERE MEASURED THIS IS OUT OF LIMITS AND MUST BE REPAIRED UNDER CARD 56, ZONE 000, COUNTERSINK HOLES AT FUEL ACCESS 520DB AND 520GB WERE MEASSURED THIS IS OUT OF LIMITS THEREFORE WERE REPLACED IAW SRM 57-10-01, TOOL USED, PN:1127, SERIAL 60555, DUE DATE 15FEB17 OLYMPUS 38DL PLUS. TRANSDUCER, SONOPEN, V260 RM.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 620DB AND 620HB, AYP, IN REF OR NRC 48, ZONE 000. FUEL ACCESS PLATES 620DB AND 620HB WERE REPAIRED UNDER CONDITION II IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620JB, 620LB, 620MB, AND 620PB, AYP. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS NR 620JB, 620LB, 620MB, AND 620PB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III. TOOL USED, PN 1127, SN 60555, DUE DATE 15FEB17.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620CB AND 620EB IN REF ORNRC 48, ZONE 000, CARD 53, ZONE 000. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PLATE NR 620CB AND 620EB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON LT FUEL ACCESS PLATE COUNTERSINK NR 520CB AND 520EB. CORROSION ON LT FUEL ACCESS PLATE 520CB AND 520EB WAS REMOVED AND FUEL ACCESS WERE REPAIRED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PANEL. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PANEL REPLACED IAW SRM 57-10-01 UNDER CONDITION III.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE 620DT. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS WAS REMOVED, COUNTERSINK HOLES AND SETTLEMENT AREA ON FUEL ACCESS 620DT WERE MEASURED THIS IS OUT OF LIMITS. ACCESS WAS REPLACED.

Part: SUPPORT FITTING — CRACKED (BS 737) · airframe 40,158 hrs · 28,014 cycles

CRACKED FITTING SUPPORT ON BS 737, X=-44, AND Z=5 AT PASSENGER STRUCTURE WING BOX AREA, SM, CARD 23, ZONE 140. FITTING SUPPORT WAS REPLACED IAW DWG 3925812, REV A, SRM 51-41-02, 51-40-05, 51-10-04 PAR 15, 21.

Part: HINGE FITTING — DAMAGED (RT ELEVATOR) · airframe 40,158 hrs · 28,014 cycles

NICK ON LOWER HOUSING ON RT ELEVATOR HINGE FITTING XE=49. REPAIR WAS PERFORMED IAW ER/A 545166-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 520FT CARD 52, ZONE 000. DUE TO EXCESSIVE DAMAGE AT FUEL ACCESS 520FT THIS WAS REPLACED IAW SRM 57-10-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 40,158 hrs · 28,014 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE NR 620AT AND 620DT, AYP IN REF ORNRC 50, ZONE 000, CARD 55, ZONE 000. FUEL ACCESS 620AT WAS REPAIRED UNDER CONDITION II IAW SRM 57-10-01.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 40,158 hrs · 28,014 cycles

CRACK ON TEE FITTING ON LOWER SECTION OF FWD CARGO DOOR BS 401 APPROXIMATELY C1, SM, CARD 12, ZONE 810. TEE FITTING WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.

Part: INTERCOSTAL — CRACKED (LT ELEVATOR) · airframe 40,158 hrs · 28,014 cycles

CRACKED INTERCOSTAL ON LT ELEVATOR INTERNAL STRUCTURE BS XE=13.213, SM, IN REF ORNRC 4, ZONE 300. CRACKED INTERCOSTAL WAS REPAIRED IAW SRM 51-41-02, 55-00-00, FIG 201. RII COMPLETED BY INSPECTION.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 40,158 hrs · 28,014 cycles

PUNCTURE AND CRACK ON UPPER SKIN, LT ELEVATOR, BS PROYECTION XE=13.213, APPROACH. SM VHS. UPPER SKIN LT ELEVATOR WAS REPAIRED IAW SRM 51-41-02, 41-41-08, 51-70-13, PAGE 201, SHT 1-3, REPAIR 2, RII COMPLETED

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON RT FUEL ACCESS PLATE NR 620CT. FUEL ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01.

Part: PAN — CRACKED (BS 373) · airframe 40,158 hrs · 28,014 cycles

CRACKS ON LOWER PAN BETWEEN STOP 1 AND 2 BS 373 APPROXIMATELY AT FWD CARGO COMPARTMENT DOOR. 1, SM CARD 11, ZONE 810. PAN BETWEEN STOP 1 AND 2 WAS REPAIRED IAW SRM 52-30-02, FIG 201.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 40,158 hrs · 28,014 cycles

CRACKED AFT BRACKET SUPPORT TOP AREA OF L1 DOOR. BRACKET WAS REPLACED IAW SRM 51-41-02 AND DWG 5961804, REV 2F.

Part: BEAM — CRACKED (PAX DOOR) · airframe 40,158 hrs · 28,014 cycles

CRACK ON BEAM 1, AFT EDGE AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-2, FIG 201, SHEET 3.

Part: DOOR FRAME — CRACKED (BS 35-46) · airframe 40,158 hrs · 28,014 cycles

CRACK ON DOOR FRAME RT SIDE BETWEEN BS 35 TO BS 46 AT NOSE GEAR WHEEL WELL. DOOR FRAME WAS REPAIRED IAW SRM 53-10-14, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.

Part: CUSP WEB — CORRODED (BS 874) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION OUT OFF LIMITS ON CUSP WEB UPPER/LWR SURFACE ON BS 874 . REPAIRED IAW SRM 53-00-55, FIG 212, SRM 51-10-04 PAR 15, 21, 37, 26, SRM 51-41-01, 51-41-02, AND 51-41-05.

Part: DOOR FRAME — CRACKED (BS 35-46) · airframe 40,158 hrs · 28,014 cycles

CRACK ON DOOR FRAME LT SIDE BETWEEN BS 35 TO BS 46 NOSE GEAR WHEEL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-14-4, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.

Part: CUSP WEB — CORRODED (BS 397-477) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON RT CUSP WEB UPPER, LWR SURFACE BETWEEN BS 397-405 AND 465 TO 477, SM, IN REF OR NRC 37, ZONE 200, CARD 57, ZONE 200. CUSP WEB BS 397 TO 405 AND 465 AND 465 TO 477 WERE REPAIRED IAW SRM 53-00-55, FIG 219 AND FIG 216 AND 51-41-02, 51-41-01, 51-41-05, 51-10-04 PG 21, 15, AND 37.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 40,158 hrs · 28,014 cycles

CRACKED FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.

Part: FRAME — CRACKED (BS 1037) · airframe 40,158 hrs · 28,014 cycles

CRACKED FRAME BS 1037 LONGERON 17R AT PAX CABIN. FRAME WAS REPAIRED IAW SRM 53-20-07, FIG 201, 51-41-03 PAR 11, AND 51-41-02, 51-41-05. RII INSPECTOR SGMR ID 796792.

Part: INTERCOSTAL — CRACKED (HORIZONTAL STAB) · airframe 40,158 hrs · 28,014 cycles

CRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA XE=204 ACCESS 340UB. SM, CRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA BS XE=204 ACCESS 340UB, WAS REPAIRED IAW SRM 55-00-00, FIG 201.

Part: CUSP WEB — CORRODED (BS 486-501) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

CORROSION ON RT CUSP WEB UPPER, LOWER SURFACE BETWEEN BS 486 TO BS 501. AREA WAS REPAIRED IAW SRM 53-00-55, FIG 216 AND 51-10-04, PAR 15, 21, 37 UT WAS ACCOMPLISHED NDT SPM 04-00-07, PAR 5, FIG 3, ORIGINAL THICKNESS ON WEB IS 0.020" REMAINING IS 0.010". THEREFORE AREA OUT OF LIMITS IAW SRM 53-00-55, FIG 101. OLYMPUS 38DL PLUS SONOPEN V260 SM 23-JUL-16.

Part: CUSP WEB — CORRODED (BS 447-452) · corrosion level 2 · airframe 41,187 hrs · 28,873 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB UPPER & LOWER SURFACE BS 447 - 452. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG. 215 AND 51-10-04 PAR 21-15 AND 37, 51-40-02.

Part: CUSP WEB — OUT OF LIMITS (BS 525-531) · corrosion level 2 · airframe 40,158 hrs · 28,014 cycles

OUT OF LIMITS LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 525 TO 526 AND 530 TO 531, X 60 TO X 54. REPAIRED IAW SRM 53-00-55, FIG 216 51-10-04 PAR 15, 21, AND 37.

Part: CUSP WEB — CRACKED (BS 645) · airframe 40,158 hrs · 28,014 cycles

CRACK ON RT CUSP WEB, BS 645. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215, SRM 51-41-05, 51-41-02, SRM 53-20-51, 51-10-04, PAR 15, 21.

Part: FRAME — CRACKED (BS 256) · airframe 40,158 hrs · 28,014 cycles

CRACK ON FRAME BS 256 LONGERON 18L. FRAME WAS REPLACED IAW DWG 9911524, REV N AND SRM 51-40-5, 51-40-2, AND 51-10-04, PAR 15 AND 21.

Part: PAN — CRACKED (BS 560) · airframe 40,158 hrs · 28,014 cycles

CRACK ON LWR FWRD CORNER WINDOW RING PAN BS 560 LONGERON 14 LT AT PAX CABIN. SM, CARD 21, ZONE 201. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21. CRACK LENGTH: 0.093.

Part: CUSP WEB — PUNCTURED (BS 715) · airframe 40,158 hrs · 28,014 cycles

PUNCTURE ON LT CUSP WEB BS 715, BETWEEN X 54 - 44. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 219, SHEET 1 AND 51-10-04, PAR 15, 21.

Part: PAN — CRACKED (BS 851) · airframe 40,158 hrs · 28,014 cycles

CRACK ON UPPER/AFT WINDOW RING PAN STA 851. DAMAGE WAS REPAIRED IAW SRM 56-20-02. REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04 PAR 15 AND 21.

Part: PAN — CRACKED (BS 636) · airframe 40,158 hrs · 28,014 cycles

CRACK ON LOWER/FWD WINDOW RING PAN BS 636. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21.

Part: SKIN — DAMAGED (BS 858) · airframe 40,158 hrs · 28,014 cycles

BLEND OUT ON UPPER FUSELAGE SKIN BS 858 BETWEEN LONG 5-6R. AREA WAS REPAIRED IAW SRM 53-02-01, FIG 202, SHEET 3 AND 51-10-04, PAR 15, 21. HFEC WAS PERFORMED AND CRACKS WERE NOT FOUND. PERFORM GENERAL VISUAL INSPECTION INITIAL AND REPETITIVE EA 8,000 CYCLES IAW SRM 53-02-1, PAR 6, REP 1.

Part: CUSP WEB — CRACKED (BS 655-715) · airframe 37,152 hrs · 25,561 cycles

LEFT CUSP WEB BS 655-715, CRACKED IN 3 PLACES. INSTALLED SERVICEABLE CUSP WEB IAW SRM 51-10-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,802 hrs · 25,257 cycles

DURING SERVICE CHECK, FOUND F/A PANEL EMERGENCY SWITCH NOT WORKING IN ARM POSITION. REPLACED OVERWING EVAC BATTERY POWER SUPPLY IAW AMM 33-51-06-00-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,802 hrs · 25,257 cycles

DURING SERVICE CHECK, NOTED THE EXTERIOR EMERGENCY ILLUMINATION SYS WAS INOPERATIVE. REPLACED THE LAMPS.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 36,212 hrs · 24,784 cycles

DURING PILOT WALK AROUND, NOTED THE RT OVERWING EXTERIOR EMERGENCY LIGHT WAS ILLUMINATED. MAINTENANCE FOUND THE LIGHT TO GO OUT WHEN THE EMERGENCY LIGHT SWITCH WAS TURNED ON. THE AFT CARGO EMERGENCY CHARGER RACK WAS REPLACED AND OPS CHECKED NORMALLY.

Part: FRAME — CRACKED (LT MLG) · airframe 35,553 hrs · 24,224 cycles

LEFT MLG FWD CUT OUT FRAME CRACKED AT UPPER OTBD END. REPAIRED FRAME IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,021 hrs · 23,879 cycles

EMERGENCY BATTERY PACK INOPERATIVE AT BS 230 ABOVE SEAT NR 20. R & R BATTERY CHARGER IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221 FF DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221DF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221JF DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN CEILING PANEL NR 1 EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 211ALF DELAMINATED. R & R PANEL IAW MM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221EF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221KF DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 221CF DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 222ATF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 222AVF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,021 hrs · 23,879 cycles

MAIN CABIN FLOOR PANEL 222APF DELAMINATED. R & R PANEL IAW SRM & DWG.

Part: SUPPORT — CORRODED (R1 DOOR) · airframe 35,021 hrs · 23,879 cycles

R1 DOOR EMER EVAC SLIDE FWD GIRT BAR FITTING MOUNTING SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: FITTING — LOOSE (LT MLG DOOR) · airframe 35,021 hrs · 23,879 cycles

LEFT MLG STRUT DOOR LANDING ROD FITTING LOOSE. R & R FITTING IAW SRM & AMM.

Part: COVER — CRACKED (FUSELAGE) · airframe 35,021 hrs · 23,879 cycles

EMPENNAGE LT AFT UPPER VENT COVER LOUVER CLIP CRACKED. R & R COVER ASSEMBLY IAW SRM & DWG.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,213 hrs · 23,360 cycles

AFT FLASHLIGHT INOPERATIVE. R&R BATTERY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,521 hrs · 22,930 cycles

RIGHT EEPLS INOP AT ROW 10. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,521 hrs · 22,930 cycles

RIGHT EEPLS INOP AT ROW 3. RELAMPED IAW MM.

Part: SUPPORT — CORRODED (CARGO DOOR) · airframe 32,151 hrs · 22,078 cycles

C-1 BARRIER DOOR UPPER HINGE ATTACH STRUCTURE IS CRACKED. REMOVED DAMAGED C1 BARRIER DOOR UPPER ATTACH SUPPORT. LOCATED, DRILLED, DEBURRED & INSTALLED NEW SUPPORT P/N 5926003-82 PO 2229152 IAW B717 SRM 51-41-01, 51-40-08.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 32,151 hrs · 22,078 cycles

LEFT WING FUEL TANK ACCESS PANEL 520CB DOME NUT CHANNEL HAS A CRACK. REMOVED AND REPLACED DOME NUT CHANNEL AT LEFT WING FUEL TANK ACCESS PANEL 520CB IAW B717 SRM 57-10-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

RIGHT EMERGENCY EXIT SURROUND CRACKED AT FWD UPPER CORNER. REPAIRED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN NR 2 EMERGENCY WINDOW STOP ANGLE AT UPPER RIGHT SIDE, CRACKED (RT SIDE OF FUSELAGE). REMOVED AND REPLACED STOP ANGLE AT UPPER RIGHT SIDE NR 3 EMERGENCY WINDOW IAW B717 SRM 51-41-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

CUSP WEB RIGHT SIDE STA 408-427 CORRODED. REPAIRED WEB IAW SRM.

Part: MECHANISM — LOOSE (TAILCONE) · airframe 32,151 hrs · 22,078 cycles

TAIL CONE EMERGENCY RELEASE; LEFT LOWER RELEASE PIN MECHANISM IS LOOSE AT FRAME ATTACHMENT. TIGHTENED TAIL CONE EMERGENCY RELEASE LEFT LWR RELEASE PIN MECHANISM IAW B717 SRM 51-41-01.

Part: PIN — LOOSE (TAILCONE) · airframe 32,151 hrs · 22,078 cycles

TAIL CONE EMERGENCY RELEASE CABLE PULLEYS AT 8:00, 9:30, AND 11:00 POS.'S ON THE 1225 CANTED FRAME LOOSE GUIDE/SECURITY PINS. SECURED PINS IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

RIGHT VENT BOX STRUCTURE CRACKED AT STA 1200 CANTED FRAME. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

SEAT TRACK AT STA 588-898 LBL 54 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: MECHANISM — LOOSE (TAILCONE) · airframe 32,151 hrs · 22,078 cycles

TAIL CONE EMERGENCY RELEASE; RIGHT LOWER RELEASE PIN MECHANISM IS LOOSE AT FRAME ATTACHMENT. TIGHTENED TAIL CONE EMERGENCY RELEASE RIGHT LWR RELEASE PIN MECHANISM IAW B717 SRM 51-41-01.

Part: SKIN — CANNING (TE FLAP) · airframe 32,151 hrs · 22,078 cycles

RIGHT WING TRAILING EDGE I/B FLAP UPPER SURFACE SKIN OIL CANNING. REMOVED AND REPLACED WEDGE IAW SRM.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 32,151 hrs · 22,078 cycles

D-RING TIE DOWN FITTING CRACKED - STA 950 BETWEEN L30 AND L29L 80-101. REMOVED AND REPLACED STRIP TIE DOWN STA 950 BETWEEN L30 AND L29R P/N 2957315-1 PO 22291145 IAW B717 SRM 51-41-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

RIGHT CUSP WEB STA 655-674 CRACKED. REMOVED AND REPLACED WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

SEAT TRACK CORRODED BETWEEN BS 237 TO BS 588, RBL 54. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

CUSP WEB LEFT SIDE STA 541-560 AREAS CORRODED. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222APF IS DELAMINATED. REMOVED FLOOR PANEL 222APF IAW B717 SRM 51-41-01 FABRICATED FLOOR PANEL 222APF (21"X76") IAW B717 SRM 53-20-50 R3 INSTALLED FLOOR PANEL 222APF IAW B717 SRM 51-41-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PNL 222PF IS DELAMINATED. REMOVED FLOOR PANEL 222PF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222PF (21"X76") IAW B717 SRM 53-20-50R3. INSTALLED FLOOR PANEL 222PF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222ABF IS DELAMINATED. REMOVED FLOOR PANEL 222ABF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222ABF (21"X22") IAW B717 SRM 53-20-50 R3. INSTALLED FLOOR PANEL 222ABF IAW B717 AMM 53-21-010.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222 ANF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222AF DELAMINATED. REMOVED FLOOR PANEL 222AAF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222AAF (21"X22") IAW B717 SRM 53-20-50R3. INSTALLED FLOOR PANEL 222AAF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 22BF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222RF IS DELAMINATED. REMOVED FLOOR PANEL 222RF IAW B717 SRM 51-41-01, FABRICATED FLOOR PANEL FROM B227002 TYPE 3 PO 790191416 DIM 21" X 76" IAW B717 SRM 53-20-50 R3 INSTALLED FLOOR PANEL IAW B717 SRM 51-41-01 & AMM 53-21-01.

Part: ROD — CORRODED (ELEVATOR TAB) · airframe 32,151 hrs · 22,078 cycles

RT ELEV TAB ROD I/B END HAS HEAVY RUST ON TUBE. REMOVED AND REPLACED RT ELEV TAB ROD I/B END IAW B717 CMM/OHM CH 27-30-1 AND ADJUSTMENT TEST IAW B717 AMM CH 27-31-04. TESTS OK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222 AKF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222ACF IS DELAMINATED. REMOVED FLOOR PANEL 222ACF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222ACF (21"X41") IAW B717 SRM 53-20-50 R3. INSTALLED FLOOR PANEL 222ACF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PNL 222JF IS DELAMINATED. FABRICATED FLOOR PANEL 222JF 21"X74" IAW B717 SRM 53-20-50R3 REMOVED AND INSTALLED FLOOR PANEL AT 222JF IAW B717 AMM 53-21-01/51-41-01 SRM

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222 AEF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222FFIS DELAMINATED. REMOVED FLOOR PANEL 222 FF IAW B717 SRM 51-41-01 FABRICATED FLOOR PANEL FROM B227002 TYPE 3 DIM 21"X49" IAW B717 SRM 53-20-52 R3 INSTALLED FLOOR PANEL IAW B717 SRM 51-41-01 AND 53-21-01

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222 LF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222AMF IS DELAMINATED. REMOVED FLOOR PANEL 222AMF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222AMF (21"X76") IAW B717 SRM 53-20-50 R3. INSTALLED FLOOR PANEL 222AMF IAW B177 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 222AGF IS DELAMINATED. REMOVED FLOOR PANEL 222AGF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL 222AGF (21"X76") IAW B717 SRM 53-20-50 R3 INSTALLED FLOOR PANEL 222AGF IAW B717 AMM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 221 WF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,151 hrs · 22,078 cycles

MAIN CABIN FLOOR PANEL 221UF IS DELAMINATED. REMOVED FLOOR PANEL 221UF IAW B717 SRM 51-41-01 AMM 53-21-01 FABRICATED FLOOR PANEL 221UF 21"X71" IAW B717 SRM 53-20-50 R3 INSTALLED FLOOR PANEL 221UF IAW B717 SRM 51-41-01 AMM 53-21-01.

Part: STRAP — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

STA 560 LONGERON 19R WING TO BODY FORMER GROUND STRAP CRACKED. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

LEFT WING TO BODY FAIRING RUB STRIP CRACKED AT STA 560- LONGERON 18L. REPAIRED RUB STRIP IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 32,151 hrs · 22,078 cycles

L1 DOOR INTERIOR, 2ND HORIZONTAL BEAM FROM TOP AT DOOR CRACKED. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 32,151 hrs · 22,078 cycles

CRACK IN FASTENER HOLE ON LT HORIZ STAB I/N EDGE ON UPPER SURFACE. REPAIRED SKIN IAW FAS.

Part: BEAM — CRACKED (L1 DOOR) · airframe 32,151 hrs · 22,078 cycles

L1 DOOR INTERIOR, 3RD HORIZ BEAM FROM BOTTOM AT DOOR CRACKED AT CORNER. REPAIRED BEAM IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

PIT FRAME STA 908 CORRODED AT LONG 30. REPAIRED FRAME IAW SRM.

Part: HANDLE — CRACKED (R1 DOOR) · airframe 32,151 hrs · 22,078 cycles

CRACKED FASTENER HOLE FOR FORWARD SERVICE DOOR ASSIST HANDLE ASSEMBLY. REMOVED AND REPLACED FORWARD SERVICE DOOR ASSIST HANDLE ASSEMBLY IAW B717 AMM 52-42-03.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

AFT PIT STA 1022 CORRODED AT LONG 30. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,151 hrs · 22,078 cycles

STA 715 FRAME CRACKED AT FLOORBEAM INTERSECTION 80-001. REMOVED AND REPLACED RIGHT FRAME STA 715 IAW B717 SRM 51-41-02 AND 51-4105 AND DRAWING 9923412.

Part: SKIN — CRACKED (LT PYLON) · airframe 32,560 hrs · 22,335 cycles

LTW MDDR 215893 LEFT APRON CRACKED AT FORWARD END AFT LOWER COWLING ATTACH POINT (REF EA 17-54-03471 R1). CUT OUT DAMAGE AT LT APRON FWD END AFT LOWER COWL ATTACH POINT, C/W HFEC, FABRICATED REPAIR DOUBLER FROM 2024T30.071. R&R SKIN IAW SRM.

Part: DOUBLER — CRACKED (LT PYLON) · airframe 32,151 hrs · 22,078 cycles

LEFT APRON CRACKED AT FWD END AFT LOWER COWLING ATTACH POINT (REF EA 17-54-03471 1R). CUT OUT DAMAGE AT LT APRON FWD END AFT LOWER COWL ATTACH POINT, ON HFEC FABRICATED REPAIR DOUBLER FROM 2024 T3.071 (8 3/4" X 2 1/2") PO #90015.

Part: COVER — CRACKED (CABIN) · airframe 31,660 hrs · 21,755 cycles

RIGHT EEPLS COVERS CRACKED BETWEEN ROW 16 TO ROW 30. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 31,660 hrs · 21,755 cycles

LEFT EEPLS COVERS CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,348 hrs · 21,545 cycles

EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 18 TO ROW 23. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 31,222 hrs · 21,461 cycles

RIGHT EEPLS COVER MISSING AT ROW 3. INSTALLED COVER PER MM.

Part: COVER — CRACKED (EVAC SLIDE) · airframe 30,723 hrs · 21,136 cycles

R1 DOOR EMERGENCY EVAC SLIDE STOW CLIP CRACKED. REMOVED AND REPLACED COVER ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT SEATS 20-24 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY AT SEAT 24 DEF. EMERGENCY LIGHTS OPS CHECK NORMAL.

Part: SLIDE — DETACHED (R1 DOOR)

GALLEY DOOR SLIDE DETACHED FROM FITTING. RE-SECURED GALLEY R1 DOOR SLIDE PER M/M 25-61.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE)

L1 DOOR SLIDE BOTTLE PRESSURE IN RED BAND. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM B717 25-61-01 P/N D29982-225 OFF 2594 ON 2623.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN CEILING PANELS 1 AND 3 INOP. TROUBLESHOT PER FIM 33-50 TASK 801, FOUND BATTERY PACK B5-227 OPEN AT PIN 9. REMOVED AND REPLACED BATTERY PACK B5-227, OPS CHECK GOOD REF AMM 33-51

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 169, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 8 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 195, LBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 169, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 169, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, LBL 14, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148, RBL 23 TO RBL 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 192, BL 0, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2 AND B717 SRM 51-41-02.

Part: LENS — UNKNOWN (CABIN)

LENS COVER FOR ESCAPE PATH LIGHTING AT 11D REMOVED FROM LIGHT. REPLACED CLEAR LENS COVER ON EPL AT 11D. OK FOR SERVICE REF 33-50.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE)

AT FL 23 0 'CABIN ALT' RAN AWAY QUICKLY FROM 4000 TO 10000 FT, CONDUCTED EMERGENCY DESCENT. ASSOCIATED CABIN IN FLOW LOW ALERT. TROUBLESHOT PER FIM 21-30, TASK CARD 802, 803. RAN NR 1, NR 2 ENGINES AND PRESSURIZED AIRCRAFT WITH RIGHT PACK, AND LOOKED, LISTENED FOR LEAKS IN AFT ACCESSORY COMPARTMENT AND CHECKED LEFT PACK CONDITIONED AIR CHECK VALVE AND COLD AIR CHECK VALVE. ALL CHECKS GOOD, NO DEFECTS NOTED. AIRCRAFT GOOD FOR SERVICE.

Part: COVER — MISSING (CABIN)

RED EMERGENCY LIGHT COVER AT SEAT 20D MISSING. INSTALLED NEW RED EMERGENCY LIGHT COVER. REF B717 AMM 33-51.

Part: PAN — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER PAN SECTION HAS CORROSION OUT OF LIMITS. CORROSION: TRIMMED OUT DAMAGED SECTION AND ACCOMPLISHED REPAIR REF B717 SRM 53-20-15 FIG 201.

Part: FRAME — DAMAGED (FUSELAGE)

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

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2976.

Part: LIGHT — MISSING (CABIN)

E-PATH LAMPS & WHITE LENS MISSING AT ROW 10. INSTALLED LENS & LAMPS AS REQ'D. OPS CHECK NORMAL IAW AMM 33-51.

Part: ACM — SEIZED (ACM BAY)

ACM SEIZED AND SENT SMOKE INTO THE CABIN, CAPTAIN'S RESPONSE WAS TO SHUT OFF BOTH PACKS, SMOKE DISSIPATED. RETURNED TO BWI AFTER DECLARING AN EMERGENCY. CONFIRMED ACM WAS CAUSE OF SMOKE AND PLACED ITEM ON MEL 80007. PACK NOT USABLE. REMOVED AND REPLACED ACM.