N942AT

Part: BATTERY — INOPERATIVE (ZONE 100) · airframe 66,888 hrs · 47,963 cycles

BATTERY CHARGER FAIL MSG ANNUNCIATED SHORTLY AFTER TAKEOFF IN ATL IT CLEARED IN FLIGHT DURING PRE FLIGHT FOR RETURN LEG IT RE OCCURED CB WAS RESET AT MTC DIRECTION THERE WAS NO CHANGE THEN SMOKE WAS SEEN COMING FROM E AND E COMPARTMENT. REMOVED AND REPLACED SHIPS BATT SET AND BATT CHARGER PER B717 AMM 24-34 AND 24-34 COMPLETED NO GO ODI 21-72 NO DUCT BURN OUT REQ. BATT AND CHARGING SYSTEM NORMAL AND OK FOR SERVICE CHARGER (7729918)

Part: EEC — FAULTED (LT ENGINE) · airframe 66,451 hrs · 47,577 cycles

SHIP 9505 -ATB- DUE TO LEFT ENGINE NOT MAKING EPR ON CLIMB OUT. CORRECTIVE ACTION: REPLACE EEC, FUEL FLOW TRANSMITTER, AND FMU. NO HELP, REPLACED FUEL PUMP AND FILTER. OPS CHECK NORMAL.(7479280)

Part: ENGINE — FAILED (RIGHT) · airframe 65,640 hrs · 46,851 cycles

SHIP 9502 -ATB/IFSD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO ATL DUE TO SMOKE IN THE CABIN. CREW REPORTED RIGHT ENGINE OIL QTY WENT TO ZERO WITH SMOKE IN CABIN. CREW SHUTDOWN RIGHT ENGINE PER QRH. AFTER LANDING PAX EVACUATED AIRCRAFT USING SLIDES WHILE STILL ON RWY 27L. CORRECTIVE ACTION: ENGINE WAS REPLACED. (LP #6411298)

Part: DOOR — DAMAGED (ZONE 800) · airframe 65,640 hrs · 46,851 cycles

THE RIGHT SIDE OVERWING EXIT DOOR WAS FOUND DAMAGED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE RIGHT FWD OVERWING EMERGENCY EXIT DOOR PER B717 AMM 52-21. INSPECTION OF RIGHT FWD OVERWING EMERGENCY EXIT DOOR WAS COMPLIED WITH PER B717 AMM 52-21-01 211-801. REQUIRED STATIC LEAK CHECK WAS GOOD IAW B717 AMM 52-21. (LP #7097603)

Part: BATTERY — NO TEST (ZONE 200) · airframe 65,530 hrs · 46,751 cycles

THERE ARE MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE AFT CABIN. MAINTENANCE REPLACED THE BATTERIES IN POWER SUPPLY B5-116 AND B5-260 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6411235)

Part: UNKNOWN — FUMES (ZONE 200) · airframe 65,359 hrs · 46,595 cycles

SHIP 9502 -FUMES/DE- THE FLIGHT ATTENDANT REPORTED A "RUBBER SMELL" COMING FROM ROW 26 IN THE CABIN. SMELL STAYED FAIRLY CONTAINED BUT DID MIGRATE TO OTHER ROWS. THE SOURCE COULD NOT BE IDENTIFIED SO THE PILOT DECLARED AN EMERGENCY WITH ATC. A FOLLOW-UP LOG PAGE (0736345) DETAILS THE REPLACEMENT OF THE COALESCER BAGS AND THE PERFORMANCE OF A DUCT BURNOUT. ALL SYSTEMS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (LP #6930881)

Part: BLADES — DAMAGED (ENGINE) · airframe 65,377 hrs · 46,610 cycles

SHIP 9502 -ATB- THE CREW RETURNED THE AIRCRAFT TO PHL DUE TO MULTIPLE COMPRESSOR STALLS DURING CLIMB OUT. CORRECTIVE ACTION: INSPECTION PERFORMED BORESCOPE INSPECTION AND FOUND NUMEROUS HPC STAGE 1 BLADES DAMAGED. THE POWERPLANT WAS REPLACED. (LP #6930842)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 65,259 hrs · 46,505 cycles

BOTH OF THE AFT EMERGENCY OVERWING EXIT DOOR LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (B5-230) PER B717 AMM 33-51-04. LIGHT OPERATIONS CHECK GOOD. OK FOR SERVICE. (LP #6930841)

Part: SKIN — DAMAGED (ZONE 500) · airframe 65,252 hrs · 46,500 cycles

-AD- REF TO LOG PAGE #6930830. ORIGINAL WRITE UP: FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS+164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A #FC5720-0110-01A. ALL WORK COMPLETED PER ERA 622950AD REV ORIGINAL PRI REV 2 & FINAL ERA 622950-14AD REV ORIGINAL. NO LEAKS NOTED. PLACARD INSTALLED PER DAL P.S. 900-5-1, NO 4. (LP #0714281)

Part: SKIN — DAMAGED (ZONE 500) · airframe 65,252 hrs · 46,500 cycles

-AD- FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS=164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A. #FC5720-01103-01A. REFER TO NRC 0714281 FOR COMPLETION OF ERA 622950-14AD. NO LEAKS NOTED. OK FOR SERVICE. (LP #6930830)

Part: SUPPORT FITTING — CRACKED (ZONE 500) · airframe 65,252 hrs · 46,500 cycles

-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #1 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC 2013. REINSPECTED FWD HINGE SUPPORT FITTING BHEC INSPECTION IAW PY6 06-10-01-003 WITH FS STANDARD NO CRACKS NOTED QC 5158. (LP #0713965)

Part: TANK — NOT REPORTED (ZONE 500) · airframe 65,252 hrs · 46,500 cycles

-AD- STEP 16 OF ER/A 622950-14AD REV 0 PRI REV 2. C/W STEP 16 A&B PR1422A2 USED AT 1700 13DEC24. C/W STEP 16 STEP B PR1422B1/2 USED 0100 15DEC24. C/W STEP 16 STEP C UP TO LT TANK LEAK CHECK. LEAK CHECK COMPLETED. SENT TO REFUEL FOR LEAK CHECK. TANK FILLED WITH 5K NO LEAKS NOTED. (LP #0713998)

Part: SUPPORT FITTING — CRACKED (ZONE 500) · airframe 65,252 hrs · 46,500 cycles

-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #8 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC2013. REINSPECTED INBD FLAP HINGE SUPPORT FITTING #8 BHEC INSPECTION IAW NDTSPM PY6 06-10-01-003 NO CRACK INDICATIONS NOTED QC5158. (LP #0713987)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 64,491 hrs · 45,837 cycles

THE OVERWING EMERGENCY EVACUATION LIGHT IS INOPERATIVE. OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. SATISFACTORY TEST. (LP #5841724)

Part: FRAME — CRACKED (ZONE 200) · airframe 64,488 hrs · 45,835 cycles

CRACK ON FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00468: FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ER/A 619238-14 REV ORIGINAL AND PRI REV 1. ASSOCIATED ER/A 14-619238 ADDED FOR AC 9502. (LP #0449625)

Part: FINGER DOUBLER — CORRODED (BS 867-918) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

CORROSION ON FINGER DOUBLER BTW STA Y=867 TO STA Y=918 L26L, STA Y=946 TO STA Y=1002 L26L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FINGER DOUBLER BTW STA Y=867 TO STA Y=918 L26L, STA Y=946 TO STA Y=1002 WAS FABRICATED PER DWG 5911424 REV CZ AND DPS S2912900 AND REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0437979)

Part: LONGERON — CRACKED (BS 1133 L2L9) · airframe 64,488 hrs · 45,835 cycles

CRACK ON LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT. LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2.

Part: FRAME — CRACKED (BS 1200 L8L) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CRACKED ON CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-30-08-2R REPAIR 4 FIG 201. (LP 0427347)

Part: FRAME — CRACKED (BS 1037 S13-14L) · airframe 64,488 hrs · 45,835 cycles

CRACKS ON FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 1 TABLE 203 FIG 201.

Part: FRAME — CRACKED (BS 1200 L17R) · airframe 64,488 hrs · 45,835 cycles

CRACK ON CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT. CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.

Part: FRAME — CRACKED (BS 715 L27R) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CRACK AT FRAME STA 715 AND L27R CANTED KEEL AREA. CORRECTIVE ACTION: FRAME STA 715 AND L27R CANTED KEEL AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP 0425118)

Part: FRAME — CRACKED (BS 1200 L17L) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CRACK ON CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.

Part: SKIN — DAMAGED (EMERGENCY EXIT) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: ELONGATED HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR. CORRECTIVE ACTION: HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR WERE REPAIRED PER ERA 618743-14 REV. ORIGINAL. (LP 0417200)

Part: LONGERON — CRACKED (BS 1022) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CRACK ON LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX. CORRECTIVE ACTION: LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 PAR 5 FIGURE 201. (LP 0415340)

Part: LONGERON — CORRODED (BS 323 L25R) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CORROSION ON LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1). CORRECTIVE ACTION: LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1) WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2, PAR 5, FIG 201. (LP 0416544)

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 64,488 hrs · 45,835 cycles

AIRCRAFT 9502, INITIAL INSPECTION: CRACK (2EA) ON ANGLE AND INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH. CORRECTIVE ACTION: INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH WAS REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE 1, REPAIR 1. AND ANGLE WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 51-41-02-0G. (LP 0414388)

Part: LONGERON — CORRODED (BS 1022 L6L) · airframe 64,488 hrs · 45,835 cycles

CRACK ON LONGERON 6L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00544: LONGERON 6L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 AND 51-41-05-0G. (LP #0411816)

Part: SKIN — GOUGED (BS 1013) · airframe 64,488 hrs · 45,835 cycles

GOUGE WAS FOUND ON SKIN BS 1013. THE SKIN WAS REPAIRED IAW SRM 53-02-01-2R REP 1 PAR 5.B(5)(C) FIG 202 SHEET 15. PERFORMED VISUAL INSPECTION, INITIAL AND REPETITIVE, EVERY 8,000 CYCLES PER B717-200 SRM 53-02-01-2R PROCEDURE 1, REPAIR 1, STEP 6.A, TABLE 202. MAINTENANCE REQUIREMENTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,488 hrs · 45,835 cycles

CRACK ON INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00307: INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R-1, CATEGORY A REPAIR. (LP #0409764)

Part: FLOORBEAM — CRACKED (BS 1022) · airframe 64,488 hrs · 45,835 cycles

ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00701: ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #0406653)

Part: LONGERON — CRACKED (BS 1032 L13R) · airframe 64,488 hrs · 45,835 cycles

CRACK ON LONGERON 13R STA Y=1032 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00545: LONGERON 13R STA Y=1032 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404102)

Part: LONGERON — CRACKED (BS 1022 L8L) · airframe 64,488 hrs · 45,835 cycles

CRACK ON LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00543: LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404336)

Part: WEB — CRACKED (BS 316) · airframe 64,488 hrs · 45,835 cycles

PUNCTURE ON MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00515: MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4 REPAIR 4 FIG 220. (LP #0404013)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

CORROSION ON LOWER EDGE AND FWD EDGE DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00297: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0402912)

Part: WINDOW FRAME — CRACKED (RIGHT) · airframe 64,488 hrs · 45,835 cycles

CRACK ON UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW IN REF TO NRC 00027. SUMMARY OF NRC 00661: UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1 PROCEDURE 1, REPAIR 1. (LP #0400469)

Part: WINDOW FRAME — CRACKED (LEFT) · airframe 64,488 hrs · 45,835 cycles

DURING INSPECTION AFTER REMOVAL OF INTERNAL CAP UPPER AFT SIDE, A CRACK WAS FOUND ON THE UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW IN REF TO NRC 00024. SUMMARY OF NRC 00660: UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1 PROCEDURE 1. (LP #0395991)

Part: SEAT TRACK — CORRODED (BS 200-276) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

CORROSION OUT OF LIMITS ON RH INBOARD SEAT TRACK X=-22 BTW STA Y=200-276 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00664: CORROSION LEVEL 2. SEAT TRACK X=-22 BTW STA Y=200-276 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0396078)

Part: WEB — CRACKED (BS 218) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

CORROSION ON WEB FROM STA 218 COORDINATE X=55 PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00695: CORROSION LEVEL 2. WEB FROM STA 218 COORDINATE X=55 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0394095)

Part: BEAM — CRACKED (BS 192) · airframe 64,488 hrs · 45,835 cycles

CRACK ON BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00235: BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7 FIGURE 201. (LP #0390916)

Part: CUSP WEB — CORRODED (BS 794-813) · corrosion level 2 · airframe 64,488 hrs · 45,835 cycles

CORROSION ON CUSP MEMBRANE FROM STA Y=794 TO 813 BTW X=-55 TO -60 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00663: CORROSION LEVEL 2. REPAIR PARTS WERE FABRICATED PER B717-200 SRM 53-00-55 2R-4 FIG. 215 AND INSTALLED PER B717-200 SRM 51-41-02-0G. (LP #0392523)

Part: PAN — CRACKED (FWD CARGO) · airframe 64,488 hrs · 45,835 cycles

CRACK INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1). SUMMARY OF NRC 00227: INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1) WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0390698)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,123 hrs · 45,514 cycles

CAPTAIN WINDSHIELD ARCED AND OUTER PANEL CRACKED ON DESCENT. MAINTENANCE REPLACED THE CAPT LH WINDSHIELD IAW B717 AMM 56-11. MAINTENANCE REPLACWD THE LH WINDSHIELD TEMPERATURE CONTROLLER IAW B717 AMM 30-41. WINDSHIELD WAS WIPER REMOVED AND REINSTALLED IAW B717 AMM 30-43. TAPE APPLIED TO WINDSHIELD SEALANT REF LOG 5007044 FOR MONITOR. WINDOW CONTROLLER AND WINDSHIELD HEAT OPERATE NORMALLY. WINDOW SEAL CHECK AND PRESSURIZED AIRCRAFT. NO DEFECTS OR LEAKS NOTED. AIRCRAFT OK FOR SERVICE. (LP #5007042)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,448 hrs · 44,925 cycles

CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 1 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ACTIVATED. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHT BATTERY ASSY PER B-717 AMM 35-51. ALL LIGHTS OPERATE NORMAL NOW. AIRCRAFT OK FOR SERVICE. (LP #9986094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,517 hrs · 44,121 cycles

SURFACE CORROSION ON SKIN CLIP STA 1022, BETWEEN STR 25-26L. - MARKED- SUMMARY NRC: 077-0001:0514-2001/010 00377 CLEANED AREA, EDGE SEALED, AND APPLIED CIC PER B717 SRM 53-00-06-2R PROCEDURE 2. (LP #2748010)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 62,582 hrs · 44,178 cycles

INNER LAP SKIN HAS SURFACE CORROSION. STA 1006-1047, JUST ABOVE STR 26L. -MARKED-. SUMMARY SEE NRC 077-0001:0514-2001/008 00375: REPLACED INNER SKIN SIN LAP FINGER DOUBLER REF DACDWG 5919707. (LP #2746141)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,517 hrs · 44,121 cycles

ORROSION ON STR 26L BETWEEN STA 1022-1043. -MARKED-. INSTALLED STRINGER 26L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746142)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,517 hrs · 44,121 cycles

FOUND STR 27L AND 28L END CLIPS CORRODED AT STA 1053. SUMMARY SEE NRC 077-0001:0514-2001/006 00369: REPLACED END CLIPS AT STR 27L AND 28L STA 1053 PER B717 SRM 51-40-02. (LP #2746150)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,517 hrs · 44,121 cycles

AREAS OF CORROSION ON STR 27L, BETWEEN STA 1022-1050. -MARKED-. INSTALLED STRINGER 27L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746146)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,517 hrs · 44,121 cycles

TASK CARD NUMBER: 001-0231:2520-1002/002 REF NR 00325. FOUND CORROSION ON SKIN UNDER FORWARD DRAIN MAST. CORROSION LEVEL 2. REPLACED DOUBLER AND INTERCOSTAL PER B717 DRAWING 9923686. (LP #2731615)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,517 hrs · 44,121 cycles

LT WING FIXED FLAP VANE DELAMINATED ON UPPER SURFACE 30 INCHES FROM I/B END AND 6 INCHES FROM T/E. SUMMARY NRC 001-0292:5750-2001/001 00109: FLAP VANE FOUND TO BE OUT OF LIMITS. REPLACED LH IB FLAP VANE REF B717 AMM 27-50-02. (LP #2726069)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,500 hrs · 44,104 cycles

THE LEFT AND RIGHT FORWARD OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY B5-121 ABOVE ROW 19E PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #9494080)

Part: NONE — NONE · airframe 60,662 hrs · 42,484 cycles

LEFT AND RIGHT OVERWING EXIT IDENTIFIER EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THE B5-118 EMERGENCY BATTER POWER SUPPLY BAD. REPLACED THE B5-118 EMERGENCY BATTERY POWER SUPPLY ASSY PER B717 AMM 33- 51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #8575758)

Part: LIGHT — INOPERATIVE · airframe 60,281 hrs · 42,120 cycles

THE EMERGENCY LIGHT AT ROW 19 IS INOPERATIVE. MAINTENANCE TROUBLE SHOT PER B717 WDM 33-51-12 AND REPLACED THE EMERGENCY BATTERY CHARGER, B5-118, PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8658626)

Part: LIGHT — INOPERATIVE · airframe 60,232 hrs · 42,074 cycles

THE OVER WING EMERGENCY EXIT DOORS LOWER FWD LIGHTS ARE INOPERATIVE. MAINTENANCE DISCOVERED A BLOWN FUSE IN THE POWER SUPPLY AND REPLACED THE POWER SUPPLY PER B717 AMM 33-51. (LP #6822396)

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 60,055 hrs · 41,922 cycles

THE OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS ARE INOPERATIVE ON BOTH SIDES AT FLOOR LEVEL. THERE ARE FOUR EACH. MAINTENANCE REPLACED THE POWER SUPPLY B5-119 PER B717 AMM 33-51. ALSO FOUND WIRE C9302-301-16, TO BE CONNECTED TO TERMINAL BLOCK S3-388 STUD 8. PER WDM 33-51-14 SHEET 2, THAT WIRE NEEDS TO BE CAPPED AND STOWED. CAPPED & STOWED SAME. NOW BOTH AFT FLOOR LEVEL OVERWING EMERGENCY EXIT SIGNS OPERATE NORMALLY. MAINTENANCE FOUND THE FUSE (B5-118), FOR FORWARD THE OVERWING EXITS SIGNS, TO BE BAD. REPLACED B5-118 EMERGENCY LIGHT POWER SUPPLY PER B717 AMM 33-51. THE OPERATIONAL TEST WAS NORMAL. (LP #8268290)

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 60,055 hrs · 41,922 cycles

EMERGENCY LIGHT POWER SUPPLY AT B5-230 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8268292)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,055 hrs · 41,922 cycles

EMERGENCY LIGHT POWER SUPPLY AT B5-121 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT B5-121 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8268291)

Part: NONE — NONE · airframe 59,741 hrs · 41,660 cycles

LOWER LIGHTED OVERWING EMERGENCY EXIT SIDEWALL SIGNS ARE INOPERATIVE. T/S EMERGENCY LIGHT POWER SUPPLIES PER B717 FRM/FIM 33-50 810-801. R&R BATTERIES AT LOCATIONS 342R, 398R, 646R, 685R, 726R, 804R, 880R, 1050L, 1045R, & 841L. R&R OVERWING POWER SUPPLY PER B717 AMM 33-51-06. OPERATIONAL CHECK WAS GOOD. T/S PER B717 SSM 33-51-11 AND WDM 33-51. REPLACED EMERGENCY BATTERY PACK LIGHTING PER B717 AMM 33-51. OPERATIONAL CHECK OK. OK FOR SERVICE. (LP #8602400)

Part: SKIN — CORRODED (BS 1003 S26-28R) · corrosion level 2 · airframe 58,060 hrs · 40,193 cycles

CORROSION ON INTERIOR SKIN STA 1003 STR 26R TO STR 28R. NEC 001-0002:2040-0016/004 00518: REPAIRED PER ER/A 591313-14 REV A. ASSOCIATED ER/A 00-591313 ADDED FOR AC 9502. (LP #1802011)

Part: LONGERON — CORRODED (BS1022-1045 L19R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON STR 19R BTW STA 1022 TO 1045. NRC 001-0002:2040-0016/018 00550: REPLACED LONGERON SECTION 19R, FROM STATION 1022-1045 PER DOUGLAS DWG #5911424. (LP #1800722)

Part: FRAME — CORRODED (BS 1022 S19R) · airframe 58,042 hrs · 40,183 cycles

CORROSION ON FRAME AT STA 1022 AND STR 19R. NRC 001-0002:2040-0016/010 00524: BURNISHED AREA. CHECKED LIMTS PER B717 SRM 53-00-01A PARA. 4 AND SPLICED FRAME PER B717 SRM 53-20-07-2R PROCEDURE 3. (LP #1800748)

Part: INTERCOSTAL — CORRODED (BS1022-1037 S19R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON INTERCOSTAL AT 19R BTW STA 1022-1037. NRC 001-0002:2040-0016/011 00525: REPLACED INTERCOSTAL AT STR 19R BTW STA 1022-1037 PER DOUGLAS DWG #9957707. (LP #1800717)

Part: FRAME — CORRODED (BS 1037 S19-21R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON FRAME AT STA 1037 BTW STR 19R AND STR 21R. NRC 001-0002:2040-0016/012 00526: SPLICEED FRAME PER B717 SRM 53-20-07-2R PROCEDURE 3, AND REPLACED FRAME SEGMENT IAW DOUGLAS DWG #9958238. (LP #1800731)

Part: INTERCOSTAL — CORRODED (BS1002-1022 L19R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON INTERCOSTAL AT LONGERON 19R BETWEEN STA 1002 AND STA 1022. NRC 001-0002:2040-0016/019 00551: REPLACED INTERCOSTAL AT LONGERON 19R BETWEEN STA 1002 AND STA 1022 REF BOEING LONGBEACH DWG #5910158. (LP #1800720)

Part: INTERCOSTAL — CORRODED (BS 1002-1022 L19) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON INTERCOSTAL STR 19 STA 1002-1022.NRC 001-0002:2040-0016/021 00555: REPLACED INTERCOSTAL AT STR 19R BTW STA 1002-1022 PER B717 DWG #9958233. (LP #1800721)

Part: STRINGER — CORRODED (BS 1002-1025 S20) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON STR 20R BTW STA 1002 AND 1025. NRC 001-0002:2040-0016/009 00523 REPLACED LONGERON 20R FROM STATION 1002-1053 PER DOUGLAS DWG #5911424. (LP #1800710)

Part: STRINGER — CORRODED (BS 1053 S26R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON END FITTING STR 26 RT AT 1053. NRC 001-0002:2040-0016/020 00554: REPLACED STR 26R END CLIP AT STA 1053 REF B717 DWG #5919707. (LP #1799468)

Part: STRINGER — CORRODED (BS 1002-1030 S22) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION STR 22R BTW STA 1002-1030. NRC 001-0002:2040-0016/007 00521: REPLACED LONGERON PER DOUGLAS DWG #5911424. (LP #1798898)

Part: STRINGER — CORRODED (BS 1010-1022 S24) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

STR 24R CORRODED 1010-1022. NRC 001-0002:2040-0016/022 00561: REPLACED STRINGER 24R FROM STA 1002-1022 PER DOUGLAS DWG #5911424. (LP #1799000)

Part: LONGERON — CORRODED (BS 1003 S24R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

C-2 LONGERON END CLIP CORRODED STA 1003 STR 24R. NRC 001-0002:2040-0016/002 00516: REPLACED CLIP PER DOUGLAS DWG #5911424. (LP #1798894)

Part: LONGERON — CORRODED (BS 1003 S23R) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

C-2 LONGERON END CLIP CORRODED STA 1003 STR 23R. NRC 001-0002:2040-0016/001 00515: REPLACED CLIP PER DOUGLAS DWG #5911424. (LP #1798903)

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

FORWARD CARGO LOWER DOOR JAMB AREA HAS CORROSION (MKD). NRC 001-0373:5231-2003/002 00146: REPLACED LOWER JAMB PAN REF B717 SRM 53-20-15-2R, REPAIR 6. (LP #1788709)

Part: LANYARD — FRAYED (TAILCONE SLIDE) · airframe 58,042 hrs · 40,183 cycles

THE NYLON SLIDE DEPLOY LANYARD ON TAIL CONE IS FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED CABLE REF. B717 AMM 53-52-01. (LP #1787246)

Part: SHEAR TIE — CORRODED (BS 908 S29-30L) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON SKIN CLIP AT STA 908 BETWEEN STR 30 & 29L. MARKED. REPAIRED SKIN CLIP REF B717 SRM 53-00-06-2R PROCEDURE 2. (LP #1785370)

Part: SHEAR TIE — CORRODED (BS 994) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON SKIN CLIP AT STA 994 AFT SIDE 30. MARKED. SPLICED IN NEW SECTION OF FORMER REF B717 SRM 53-00-06-2R PROC 2. (LP #1784322)

Part: BULKHEAD WEB — CORRODED (BS 1053 S28-29L) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION AT AFT PRESSURE BULKHEAD FS1053 BETWEEN LONGERONS 28L AND 29L. NRC 031-0022:5310-2014/003 00411: REPAIRED PER PRI 590913- 14 REV ORIG AND ER/A 590913-14 REV ORIG. ALL STEPS MATCH. ASSOCIATED ER/A 00-590913 ADDED FOR AC 9502. (LP #1782629)

Part: LONGERON SPLICE — CORRODED (BS 908 L30) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION STR 30 STA 908 THRU APPROX. 1010. NRC 030-0008:5331-2001/009 00350: TASK COMPLETE. REPLACE LONGERON AND SPLICE PER B717 SRM 53-20-05-2R REPAIR 1. (LP #1781487)

Part: SHEAR TIE — CORRODED (BS 927 S30) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION SKIN CLIP @ STA 927 BETWEEN STR 30. NRC 030-0008:5331-2001/010 00351: TASK COMPLETE. REPLACE SKIN CLIP SECTION REF B717 SRM 53-00-06-2R-2. (LP #1781637)

Part: SHEAR TIE — CORRODED (BS 908 S30) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION SKIN CLIP @ STA 908 BETWEEN STR 30. NRC 030-0008:5331-2001/006 00347: TASK COMPLETE. REPAIR SKIN CLIP REF B717 SRM 53-00-06-2R PROCEDURE 2. (LP #1781635)

Part: INTERCOSTAL — CORRODED (BS 1022 S25L) · airframe 58,042 hrs · 40,183 cycles

AFT CARGO INTERCOSTAL CORRODED AT STR 25L, STA 1022. NRC 030-0008:5331-2001/022 00368: REMOVED CORROSION AND CHECKED LIMITS REF B717 SRM 53-00-00 1A. FOUND OUT OF LIMITS. REPLACED ON NRC 387. (LP #1780556)

Part: LONGERON — CORRODED (BS 1053 L24L) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

CORROSION ON LONGERON 24L END CLIP FS 1053 AFT OF P-DOME. NRC 031-0022:5310-2014/004 00432: REPLACED END FITTING PER B717 DWG 3914653. (LP $1781172)

Part: INTERCOSTAL — CORRODED (BS1022-1042 S25L) · airframe 58,042 hrs · 40,183 cycles

INTERCOSTAL CORRODED AT 25L STA 1022 TO 1042. NRC 030-0008:5331-2001/027 00387: REPLACED PER DOUGLAS DWG #9957695. (LP #1780553)

Part: SHEAR TIE — CORRODED (BS 974) · airframe 58,042 hrs · 40,183 cycles

CORROSION SKIN CLIP @ STA 974. MARKED. NRC 030-0008:5331-2001/016 00357: REPAIRED FORMER / SKIN CLIP PER B717 SRM 53-00-06 FIGURE 201 REPAIR 2. (LP #1781097)

Part: FRAME — CORRODED (BS 1053 S30) · airframe 58,042 hrs · 40,183 cycles

CORROSION FRAME 1053 STR 30. NRC 030-0008:5331-2001/018 00359: REPLACED LOWER DOUBLER AND WEBS REF DRWG #9915561. (LP #1780229)

Part: STRINGER — CORRODED (BS 1053 S25L) · airframe 58,042 hrs · 40,183 cycles

CORROSION STR 28L CORRODED @ STA 1053. MARKED. NRC 031-0022:5310-2014/002 00365: REPLACED STR 28L END CLIP AT STA 1053 REF LONG BEACH BOEING DWG #4912515. (LP #1780221)

Part: LONGERON — CORRODED (BS 984-1053 L23L) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

LONGERON 23L IS CORRODED FROM STA 984 TO 1053. NRC 031-0022:5310-2014/012 00468: MAINTENANCE REPLACED THE LONGERON SECTION PER DWG #5936021 AND B717 SRM 53-00-05-2R-2 REPAIR 2. (LP #1776850)

Part: LONGERON — CORRODED (BS 1002 L23L) · airframe 58,042 hrs · 40,183 cycles

LONGERON 23L AT STA 1002 IS CORRODED. NRC 030-0008:5331-2001/024 00384: MAINTENANCE REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2. (LP #1776853)

Part: STRINGER — CORRODED (BS 1022-1053 S22) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

STRINGER L22 BELOW OUTFLOW VALVE CORRODED STA 1022-1053. NRC 030-0008:5331-2001/033 00465: REPLACED STRINGER L22 PER BAC DWG #5936021. (LP #1776349)

Part: STRINGER SPLICE — CORRODED (S22L) · corrosion level 2 · airframe 58,042 hrs · 40,183 cycles

STR 22L SPLICE CORRODED BELOW OUTFLOW VALVE. NRC 030-0008:5331-2001/021 00367: REPLACED SPLICE PER BAC DWG #5936021. (LP #1776348)

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,802 hrs · 39,989 cycles

THE EMERGENCY LIGHT SIGNS BELOW THE OVERWING EXIT AT ALL FOUR LOCATIONS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BALLAST B5-119 PER B717 AMM 33-51. THE EMERGENCY LIGHTS AT THE OVER WING POSITION NOW OPERATE NORMALLY. (LP #7682718)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,290 hrs · 39,558 cycles

THE PASSENGER DOOR EMERGENCY LIGHT COMES ON THEN GOES OUT. LIGHT POSITION L2-833. MAINTENANCE REPLACED THE BATTERY PACK AT POSITION B5-118, PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL.

Part: LANYARD — UNSECURE (L1 DOOR SLIDE) · airframe 56,951 hrs · 39,219 cycles

THE L1 DOOR SLIDE LANYARD WAS FOUND TO BE DISCONNECTED AT SLIDE BASE. THIS WOULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE L1 DOOR SLIDE LANYARD CORRECTLY PER B717 AMM 25-61.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,625 hrs · 38,940 cycles

THE OVERHEAD EMERGENCY LIGHTS, BETWEEN ROW 1-18, WERE FOUND TO BE INOPERATIVE DURING THE SERVICE CHECK. MAINTENANCE REPLACED BATTERY PACKS B5-118 AND B5-227 PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: PIN — OUT OF POSITION (EVAC SLIDE) · airframe 53,842 hrs · 36,931 cycles

L1 DOOR SLIDE INFLATION CABLE PINS OUT OF PLACE. REPLACED SLIDE ON CARD #5211-4002. SLIDE, EVAC, FO OFF 97-2561-9-0003 03149 ON 97-2561-9-0003 02527. (LP1000901)

Part: FASTENER — LOOSE (RT SPOILER) · airframe 53,842 hrs · 36,931 cycles

RT WING; FASTENERS LOOSE ON I/B SPOILER LOWER SURFACE AT ACTUATOR LINK ATTACH PLATE. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0302:5750-2002/004 00080 INSTALLED SPOILER, REF AMM 27-60-01. (LP0998805)

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 53,842 hrs · 36,931 cycles

AFT CARGO COMPARTMENT HAS CORROSION AT THE AFT CARGO DOOR THRESHOLD. MKD. NRC 001-0306:0593-2006/002 00012: REPLACED DOOR JAMB REF SRM 53-20-15-2R PRO 7. (LP #0992523)

Part: VANE — DAMAGED (TE FLAP) · airframe 53,842 hrs · 36,931 cycles

LT WING I/B T/E FIXED VANE L/E DAMAGED. REPLACED FLAP VANE REF. AMM 27-50-02 ADJUSTMENT AND OPERATIONAL CHECK OKAY. (LP0989219)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,140 hrs · 36,445 cycles

GALLEY CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK P1-259 IAW B717 AMM 33-51. OPS TESTED GOOD. OK FOR SERVICE. P/N 803925-1. S/N OFF 96842. S/N ON 98372. (LP0848239)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 52,518 hrs · 36,040 cycles

RT SIDE OF VERTICAL STABILIZER AT ZFS=52.267 IS CRACKED. REFERENCE AA 5530-01048 AND AD 2018-10-08. REPAIRED VERT STAB UPPER L/E SKIN/CRACK PER ER/A 571285-14 REV ORIG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,064 hrs · 35,734 cycles

EMERGENCY ESCAPE PATH LIGHT INOP AT 22CDE. R&R ASSY PER AMM 33-51, OPS NML.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK, THE LEFT INBD SPOILER FOUND DELAMINATED.

Part: SKIN — CRACKED (BS 1076) · airframe 48,860 hrs · 33,526 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT BS 1076 LONGERON 14R. REPAIRED IAW ER/A 555597-14 REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,860 hrs · 33,526 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT STA 1087 L14R. HFEC VERIFIED IAW NDT SPM ETHF PROCEDURE 1, 06-10-01.001. EXTERNAL FUSELAGE SKIN CRACK AT STA 1087 L14R WAS REPAIRED IAW ER/A 555596-14 REV ORIGINAL. ER/A 555596-14 WAS COMPLIED WITH.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 48,860 hrs · 33,526 cycles

BARREL NUTS ACROSS LOWER AREA OF THE CARGO DOOR FRAME HAVE SIGNS OF CORROSION AROUND EDGES. BLENDED AREAS IAW SRM 53-00-00, FIG 103. FOUND AREAS TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG. 103. REPLACED THE FWD CARGO DOOR LOWER FRAME PAN IAW SRM 53-20-15-2R-6, AND 51-41-02-OG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,860 hrs · 33,526 cycles

FORWARD CARGO STA 636, BL0 AFT ANGLE ON INTERCOSTAL IS CRACKED. REPAIRED CRACKED FLOOR SUPPORT "INTERCOSTAL" AT STA 636 BL0 IAW SRM 51-70-11-2R-1.

Part: CUSP WEB — PUNCTURED (BS 298) · airframe 48,860 hrs · 33,526 cycles

PUNCTURE IN LEFT OTBD CUSP WEB BS 298. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: CUSP WEB — CORRODED (BS 545-551) · airframe 48,860 hrs · 33,526 cycles

CORROSION ON LOWER SURFACE OF LEFT OTBD CUSP WEB LIGHTNING HOLE, BS 545 AND 551. BLENDED CORROSION IAW SRM 53-00-00-1A AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55-1A-1. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.

Part: CUSP WEB — CORRODED (BS 494) · corrosion level 2 · airframe 48,860 hrs · 33,526 cycles

CORROSION ON LOWER SURFACE OF LT OTBD CUSP WEB LIGHTNING HOLE AT BS 494. FOUND TO BE OUT OF LIMITS. FABRICATED A DOUBLER. TREATED, PRIMED, AND INSTALLED THE DOUBLER IAW SRM 53-00-55-2R-4, FIG 215, 4 C & D, 51-40-02, AND 51-10-04, PG 24, PAR 21, PG 16, PAR 12A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,860 hrs · 33,526 cycles

CORROSION ON CUSP WEB TOP SIDE BETWEEN ST 927-908 LBL 59. BLENDED CORROSION ON CUSP WEB TOPSIDE STA 908-927 LBL 59 WEB FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .020" REMAINING .011" REMOVED .009" IAW SRM 53-00-55-1A-1 REPAIRED WEB BY INSTALLING DOUBLER IAW SRM 53-00-55-2R-4 GOUGE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,514 hrs · 33,305 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS AT BOTH L1 AND L2 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,369 hrs · 33,204 cycles

DURING LINE CHECK, MAINTENANCE NOTED THAT THE LOWER EMERGENCY LIGHTS FOR THE OVERWING EXITS WERE INOPERATIVE. REPLACED THE BATTERIES AND THE OPS CHECKED GOOD.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 45,509 hrs · 31,036 cycles

FUEL LEAKING LT AFT FUEL DRAIN MAST WHILE ENGINE IS RUNNING. FOUND FUEL RETURN TO TANK, FRAME TT, LINE LEAKING AT CONNECTION IN AFT BAGGAGE BIN. REPLACED O-RINGS AT CONNECTION.

Part: LATCH — OUT OF ADJUST (TAILCONE) · airframe 44,339 hrs · 30,073 cycles

AFT CABIN DOOR TAIL SLIDE, ARMING PAD BOTTOM LATCH OUT OF ADJUSTMENT. ADJUSTED LATCH IAW SRM.

Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 44,339 hrs · 30,073 cycles

AFT EMER FLASHLIGHT INOPERATIVE. RECONNECT BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,339 hrs · 30,073 cycles

L1 DOOR EXIT SIGN LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,339 hrs · 30,073 cycles

LEFT OVERWING EMER EXIT DOOR LIGHT BULB INOPERATIVE. REPAIRED BULB IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,043 hrs · 29,190 cycles

AFT OVERHEAD EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

VERTICAL WEB CORRODED AT BS 1053, BETWEEN LONGERON 28L - 28R. REPAIRED WEB IAW SRM & DWG.

Part: TAIL CONE — DELAMINATED (VERTICAL STAB) · airframe 43,043 hrs · 29,190 cycles

RIGHT SIDE OF VERTICAL STABILIZER DELAMINATED TAIL CONE AREA. REPAIRED TAIL CONE IAW SRM.

Part: TAIL CONE — DELAMINATED (VERTICAL STAB) · airframe 43,043 hrs · 29,190 cycles

LEFT VERTICAL STABILIZER DELAMINATED ON THE TAIL CONE. REPAIRED STABILIZER IAW EA.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT DOOR, FWD DOOR CUT OUT LOWER STOP FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

SKIN CORRODED BETWEEN BS 1022 - 1037, BETWEEN LONGERON 29R TO 28R. REPAIRED SKIN IAW FAS EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FITTING CORRODED AT BS 1057, LONGERON 29R. R & R FITTING IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN AFT EMER EXIT DOOR RT LOWER DOOR JAMB CORRODED. REPAIRED JAMB IAW FAS EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 201, RBL 54. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

LOWER FUSELAGE N FITTING CORRODED AT BS 1057, LONGERON 25R. R & R FITTING IAW DWG.

Part: SCOOP — CRACKED (VERTICAL STAB) · airframe 43,043 hrs · 29,190 cycles

VERTICAL STABILIZER, INLET SCOOP AT LT SIDE CRACKED. REPAIRED STABILIZER IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FWD CEILING EMER EXIT SIGN ASSEMBLY CRACKED. R & R SIGN ASSEMBLY IAW AMM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN MEMBRANE CORRODED AT BS 200, RBL 10. REPAIRED MEMBRANE IAW EA.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

L1 DOOR MEMBRANE CORRODED BETWEEN BS 200 - 157, LBL 58. R & R MEMBRANE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

WING TO BODY FAIRING LOWER SUPPORT FITTING ANGLE CORRODED AT BS 832, LONGERON 30. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESSURE BULKHEAD AFT FACE LOWER BRACKET CORRODED AT BS 1060, LBL 24. R & R BRACKET IAW DWG & SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD AFT LOWER FACE BRACKET CORRODED AT BS 1060, LBL 11. R & R BRACKET IAW SRM & DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD AFT FACE, LOWER BRACKET CORRODED AT BS 1060, RBL 12. R & R BRACKET IAW SRM & DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD AFT FACE LOWER BRACKET CORRODED AT BS 1060, BL 0. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD SKIN AFT LOWER FACE CORRODED AT BS 1076, BL 0. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

RIGHT CUSP ANGLE CORRODED BETWEEN BS 1037 - 1053. REPAIRED CUSP ANGLE IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT SKIN CORRODED AT BS 946, LONGERON 28R. REPAIRED SKIN IAW FAS EA.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

LONGERON CORRODED AT BS 1006, LONGERON 30R. R & R LONGERON IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT INTERNAL DOUBLER CORRODED BETWEEN BS 1022 - 1037, BETWEEN LONGERON 29R - 28R. REPAIRED DOUBLER IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,339 hrs · 30,074 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 946.5 - 964, BETWEEN LONGERON 28R - 29R. REPAIRED SKIN IAW FAS EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 44,339 hrs · 30,074 cycles

AFT PRESS BULKHEAD FWD LOWER FACE WEB CORRODED BETWEEN LONGERON 30 - 26R. REPAIRED WEB IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN WEB CORRODED BETWEEN BS 1037 - 053, RBL 60. R & R WEB IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR TIE DOWN FITTING CORRODED AT BS 160, RBL 50. R & R FITTING IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CABIN SUB FLOOR CORRODED AT BS 185, RBL 47. REPAIRED FLOOR IAW SRM & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FRAME CORRODED AT BS 1022, BETWEEN LONGERON 19R - 21R. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN WEB CORRODED BETWEEN BS 1037 - 1053, LBL 0. R & R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1053 - 1037, RBL 20. R & R SUPPORT IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,339 hrs · 30,074 cycles

AFT CARGO FRAME CORRODED AT BS 1022, BETWEEN LONGERON 19R - 21R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1053 - 1037, LBL 20. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1022 - 1053, RBL 52. R & R SUPPORT IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD FWD LOWER FACE CORRODED BETWEEN LONGERON 30L - 26R. REPAIRED BULKHEAD IAW FAS EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

INTERCOSTAL CORRODED AT BS 1002, BETWEEN LONGERON 28R - 27R. R & R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

WEB CORRODED BETWEEN BS 1022 - 1037, RBL 60. R & R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 1022 - 1053, LBL 52. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AT BS 655, LBL 15. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 1022 - 1033, RBL 44. R & R SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR WEB CORRODED BETWEEN BS 218 TO BS. 506, LBL 56. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 210, RBL 10. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 275, BETWEEN RBL 22 - RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN BELLOW FLOOR SEAT TRACK SUPPORT FITTING CRACKED AT BS 737, LBL 44. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR SUPPORT CORRODED AT BS 200, LBL 56. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 218, BL 0. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 198, LBL 16. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 170 - 196, LBL 56. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 196, BETWEEN LBL 22 - LBL 36. R & R SUPPORT IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

SHEAR TIE CRACKED AT BS 1022, BETWEEN LONGERON 6R - 7R. R & R SHEAR TIE IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 170, LBL 53. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN BELLOW FLOOR AT BS 737, RBL 44 SEAT TRACK SUPPORT FITTING CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

LONGERON CRACKED AT BS 1022, LONGERON 5R. REPAIRED LONGERON IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FLOOR TIE DOWN UPPER SURFACE FITTING CORRODED AT BS 160, RBL 12. R & R FITTING IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

LEFT WING TO BODY WEB CORRODED AT BS 813, BETWEEN LONGERON 24L - 23L. R & R WEB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

SHEAR TIE CRACKED AT BS 1095, LONGERON 15L. R & R SHEAR TIE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 200 - 589, LBL 22. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD DOOR FRAME FITTING CRACKED AT BS 1053, LONGERON 17L. R & R FITTING IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD DOOR FRAME FITTING CRACKED AT BS 1053, LONGERON 14R. R & R FITTING IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 899 - 1022, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD DOOR FRAME FITTING CRACKED AT BS 1053, LONGERON 14L. R & R FITTING IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PRESS BULKHEAD FRAME FITTING CRACKED AT STATION 1053, LONGERON 16L. R & R FITTING IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT LOWER CARGO DOOR CUT OUT LOWER JAMB PAN CORRODED. R & R PAN IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR BOARD 222LF DAMAGED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR BOARD 222AEF DAMAGED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOORBOARD 221AF DELAMINATED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOORBOARD 222 ACF DAMAGED. REPAIRED FLOORBOARD IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOORBOARD 222RF DAMAGED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOORBOARD 22EDF DAMAGED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,043 hrs · 29,190 cycles

MAIN CABIN FLOOR BOARD 221ALF DAMAGED. R & R FLOORBOARD PANEL ASSEMBLY IAW MM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

MEMBRANE CORRODED AT BS 160, BETWEEN LBL 10 - 14. REPAIRED MEMBRANE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT CARGO COMPARTMENT CTR CHANNEL STRINGER CORRODED BETWEEN BS 908 - 986, STRINGER 30. R & R STRINGER IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

SKIN CORRODED BETWEEN BS 994 - 1000, BETWEEN STRINGER 28R - 29R. REPAIRED SKIN IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT CARGO COMPARTMENT FRAME CORRODED BS 1028, BETWEEN STRINGER 29R - 29L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT CARGO COMPARTMENT FRAME AFT FLANGE CORRODED AT BS 870, 6 O'CLOCK POSITION. REPAIRED FRAME IAW FAS EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT CARGO COMPARTMENT FRAME LOWER FLANGE CORRODED AT BS 889, BETWEEN STRINGER 29L - 29R. REPAIRED FRAME IAW FAS EA.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

FORWARD CARGO COMPARTMENT LOWER DOOR JAMB PAN CORRODED AT STEEL INSERTS. REPAIRED JAMB PAN IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT AFT DOOR CUT OUT LOWER SECTION DOUBLER ON PAN CORRODED. REPAIRED PAN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

SKIN CORRODED BETWEEN BS 956 - 966, BETWEEN LONGERON 29R - 28R. REPAIRED SKIN IAW EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT DOOR UPPER JAMB WEB CORRODED BETWEEN BS 992 - 1002, BETWEEN LONGERON 26R - 24R. REPAIRED JAMB WEB IAW SRM.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT DOOR GUSSET CORRODED AT BS 992, LONGERON 29R. R & R GUSSET IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT DOOR LOWER JAMB WEB CORRODED BETWEEN BS 946 - 1002. R & R WEB IAW DWG & SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

AFT PIT DOOR DOUBLER ON PAN CORRODED AT BS 956, LONGERON 27R. R & R PAN IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,043 hrs · 29,190 cycles

AFT PIT LOWER DOOR JAMB SEAT TRACK TIE DOWN TRACK CORRODED AT BS 956. R & R TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CUSP WEB CORRODED AT BS 747, RBL 58. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CUSP WEB CORRODED AT BS 724, RBL 58. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CUSP WEB CORRODED AT BS 370, RBL 58. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CUSP WEB CORRODED AT BS 964, RBL 56. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,043 hrs · 29,190 cycles

CUSP WEB CORRODED BETWEEN BS 503 - 890, BETWEEN RBL 60 TO LBL 60. R & R CUSP WEB IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 44,339 hrs · 30,073 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR ATTACHMENT FITTING CORRODED. R & R FITTING IAW MM.

Part: LENS — MISSING (CABIN) · airframe 44,056 hrs · 29,881 cycles

RIGHT EEPLS LENS COVER MISSING AT ROW 3. INSTALLED COVER IAW MM.

Part: WIRE — LOOSE (CABIN) · airframe 43,854 hrs · 29,739 cycles

RIGHT LOOSE WIRE SEAT AT ROW 30. SECURED WIRE SIP.

Part: LATCH — LOOSE (R1 DOOR) · airframe 41,014 hrs · 27,893 cycles

R1 DOOR EMERGENCY EVAC SLIDE DEPLOY LATCH LOOSE. SECURED LATCH IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 41,014 hrs · 27,893 cycles

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

Part: LONGERON — CRACKED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

LONGERON CRACKED AT BS 1144, STR 2R. REMOVED AND REPLACED LONGERON IAW SRM.

Part: WEB — CRACKED (L2 DOOR) · airframe 39,836 hrs · 27,155 cycles

L2 DOOR WEB CRACKED RIGHT SIDE AT BS 1076. REPAIRED WEB IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

L2 DOOR JAMB CRACKED ON RT SIDE AT BS 1076. REPAIRED JAMB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

LONGERON CRACKED BETWEEN STA 1152, LONGERON 1R AND LONGERON 3R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

FLOOR SUPPORT CORRODED AT STA 1045, RBL 55. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SEAT FRAME — CRACKED (CABIN) · airframe 39,836 hrs · 27,155 cycles

FORWARD FLIGHT ATTENDANT SEAT FRAME LEFT UPPER SIDE CRACKED. REMOVED AND REPLACED SEAT IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

LEFT SIDE OF AFT FUSELAGE CRACKED VERTICAL ANGLE AT UPPER AFT CORNER FS 1200, LONGERON 6L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,836 hrs · 27,155 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,836 hrs · 27,155 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,836 hrs · 27,155 cycles

FLOOR SUPPORT CRACKED AT BS 655. REMOVED AND REPLACED SUPPORT IAW SRM AND DRAWING.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,542 hrs · 26,959 cycles

AFT FLASHLIGHT INOP. INSTALLED A NEW BATTERY, OPS CHECK GOOD.

Part: RECEPTACLE — FAULTY (FUEL SYSTEM) · airframe 39,434 hrs · 26,893 cycles

DIVERSION -- LEFT FWD FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED APPROX 5 MINS LATER THAN LEFT AFT FUEL LOW PRESSURE LIGHT ILLUMINATED. BOTH CIRCUIT BREAKERS WERE POPPED. REMOVED AND REPLACED RECEPTACLE R5-6001 PER WM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 38,444 hrs · 26,250 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LATCH — OBSTRUCTED (GIRT BAR) · airframe 38,135 hrs · 26,040 cycles

GALLEY DOOR GIRT BAR WILL NOT GO INTO FLOOR FITTING. REMOVED DEBRIS AND LUBRICATED GIRT BAR RELEASE LATCH PER AMM.

Part: LANYARD — BROKEN (EVAC SLIDE)

R1 DOOR ESCAPE SLIDE LANYARD IS BROKEN. REMOVED AND REPLACED BROKEN R-1 DOOR SLIDE GIRT LANYARD AS OUTLINED IN 717 M/M 25-61 AWI.

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK FOR UPPER FORWARD OVERHEAD LIGHT IAW B717 AMM 33-51-03. OPS CHECK GOOD AT THIS TIME.

Part: PAN — CORRODED (FUSELAGE)

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

Part: FITTING — CORRODED (FUSELAGE)

AFT CARGO SHEAR CLIPS, STA 974, LONG 28L TO 29R, CORROSION. ACCOMPLISHED SHEAR CLIPS REPLACEMENT PER B717 SRM 51-41-02.

Part: PAN — CORRODED (FUSELAGE)

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

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHT ASSY INOP ON SIDE OF SEAT 2D. RELAMPED AND REPLACED LENS COVER AT SEAT 2D.

Part: CUSP WEB — CORRODED (FUSELAGE)

RIGHT CABIN CUSP LINE BETWEEN STA 446 AND 465 WEB FLOOR HAS SURFACE CORROSION. INSTALLED REPAIR PER CUSP MEMBRANE REPAIR DRAWING SG 09530003 AND B717 SRM 51-10-04.

Part: CUSP WEB — CORRODED (FUSELAGE)

RT CABIN CUSP LINE BETWEEN STA 522 AND 541 WEB FLOOR HAS SURFACE CORROSION. INSTALLED REPAIR PER CUSP MEMBRANE REPAIR DRAWING SG 09530003 AND B717 SRM 51-10-02.

Part: LINE — CRACKED (NR 1 ENGINE)

LEFT ENGINE FRTT LINE CRACKED. REMOVED AND REPLACED LEFT ENG FUEL RETURN LINE AND O-RING PER 717 AMM 73-11-06. RAN ENG OPS AND LEAK CHECK GOOD.

Part: CUSP WEB — CORRODED (FUSELAGE)

RT CABIN CUSP LINE STA 465 TO STA 484 WEB FLOOR HAS CORROSION. INSTALLED CUSP MEMBRANE REPAIR PER DRAWING SG 09530003.

Part: CUSP WEB — CORRODED (FUSELAGE)

RT CABIN CUSP LINE STA 484 TO STA 503 WEB FLOOR HAS CORROSION. INSTALLED CUSP MEMBRANE REPAIR PER DRAWING SG 09530003.

Part: ADIRU — INOPERATIVE (E&E BAY)

NUMEROUS LEVEL 1 & 2 ALERTS LOSS OF APS, FLIGHT DIRECTORS, ALTITUDE ALERTS RUDDER LIMITER AIRSPEED VARIATIONS OF UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ADIRU DUE TO INOP COOLING FAN. NR 1 ADIRU CHECKS GOOD REF MM 34-43. REMOVED AND REPLACED CAPT'S PITOT ADM REF MM 34-11. OK FOR SERVICE. RVSM STATUS MAINTAINED.

Part: UNKNOWN — ODOR (CABIN)

BURNING PLASTIC SMELL IN FWD CABIN AREA. ALL 3 F/A'S VERIFIED SMELL. PILOT AND COPILOT SMELLED ODOR IN COCKPIT. AFT F/A STATED GETTING ODOR IN AFT CABIN. DECLARED EMERGENCY AND LANDED UNEVENTFULLY LANDING WT 103,500 AFT SECTION OF CABIN PASSENGERS ALSO SMELLED PLASTIC ODOR. PERFORMED SPECIAL INSPECTION REF AIR TRAN GMM 8115. INSPECTED AIRCRAFT, ALL ELECTRICAL POWER, LIGHTING, ENGINES, APU, PNEUMATIC SYS OR UNUSUAL ODORS NOTED. PERFORMED HIGH POWER RUN PER M/M 71-00, OPS CK'D GOOD. NO ODORS DETECTED, UPON INITIAL ENTRY INTO CABIN NO UNUSUAL ODORS NOTED.

Part: STRUCTURE — DENTED (BS 219-299 L16L)

DENT AT AFT OF L1 DOOR STA 219 - 229 L16L. CUT OUT DAMAGED AREA IAW B717 SRM 53-00-01, INSPECTED CUTOUT WITH HFEC IAW NDTSPM PART 6 10-01-001. NO CRACKS NOTED, INSTALLED NEW SKIN SECTION IAW B717 SRM 53-00-01.

Part: SLIDE — UNSERVICEABLE (L1 DOOR)

DURING RII INSPECTION THE PINS WERE FOUND PULLED. R&R L1 SLIDE ASSY( FOUND PIN PULLED ) IAW REF MM 25-61-01.

Part: LINE — CHAFED (HYD SYSTEM)

ON APPROACH HYD RT QTY LO RT RESERVOIR SHOWED 0. FOUND HYDRAULIC LINE PN NR 7972148-520 CHAFED. PREFORMED PERMA SWAGE TYPE 2 REPAIR REF MM 20-10-01 LEAK CHECK GOOD. SERVICED RT HYDRAULICS REF MM 12-13.

Part: LIGHT — INOPERATIVE (AFT ASSY BAY)

CATWALK EMERGENCY LIGHT ASSY HAS 3EA LAMPS NOT ILLUMINATED. REMOVED AND REPLACED LIGHT ASSY PER MM 20-20.

Part: FRAME — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT CANTED FRAME AT BS 1178 CRACKED IN TWO PLACES LONGERON 16 TO 18 LEFT. INSTALLED FORMED CHANNEL REPAIR AT AFT ACCESSORY COMPARTMENT CANTED FRAME AT BS 1178 BETWEEN LONGERON 16L AND LONGERON 18L IAW B717 SRM 51-70-11 FIG 201. SIZE OF REPAIR 30 INCHES.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO DOOR LOWER CUTOUT WELL WITH CORROSION. INSTALLED REPAIR AT FWD CARGO LOWER DOOR JAMB IAW DC9/MD80 SRM 531-05 AND RES 05-123 DATED 09/30/05.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED AT FS 237 LONGERON 17-18 LEFT. INSTALLED FUSELAGE SKIN REPAIR AT FS 237 BETWEEN LONGERON 17L AND LONGERON 18L IAW SRM 53-00-01 FIG 201, MATERIAL USED 2024 T3 .063, SIZE OF REPAIR 15.5" X 14.125".

Part: SLIDE — DEPLOYED (R1 DOOR)

R1 DOOR SLIDE DEPLOYED BY GROUND PERSONNEL. REMOVED AND REPLACED R-1 DOOR SLIDE.

Part: PUMP — INOPERATIVE (RT ENGINE)

AFTER HYD AUX & TRANS PUMPS TURNED ON DURING IN RANGE CK LIST, LEVEL 2 RT HYD QTY LO INDICATION APPEARED. PERFORMED QRH CHECKLIST & LANDED. PINNED GEAR & CHECKED GEAR DOORS UP BEFORE BEING TOWED TO GATE AT HYD INDICATED 0 QTY DURING ENTIRE PROCEDURE. FOUND LINE FROM HYD HAND PUMP TO HYD SYSTEM TO BE CRACKED. CAPPED BOTH ENDS OF DEFECTIVE LINE. REMOVED AND REPLACED RT ENGINE DRIVEN HYD PUMP AND RT SYSTEM HYD FILTERS. FOUND NO EVIDENCE OF HYD PUMP OR AUX PUMP FAILURE.

Part: CHECK VALVE — DAMAGED (BULKHEAD)

RIGHT PAC FLOW DISAGREE ALERT CAME ON IN FLT (HISTORY). FOUND RIGHT BULKHEAD CHECK VALVE FLAPPER DAMAGED AND STUCK CLOSED. REPLACED FLAPPER AND END ASSY IAW MM 21-20-01, OPS CHECK GOOD.

Part: MASK — FAILED TEST (ROW 1R&19L)

DURING OXYGEN MASK DROP TEST, OXYGEN MASKS AT SEAT 1R AND 19L DID NOT DROP.