N603AT

Part: SPAR — CRACKED (NOT REPORTED) · airframe 52,213 hrs · 42,726 cycles

WHILE PERFORMING AMDS 5720-01103-01B. INSPECTION FOUND A CRACK AT APPROX STA XRS= 170REAR SPAR. COMPLIED WITH ER/A- 628659-14AD REV. ORIGINAL (1215975)

Part: NONE — NONE (NONE) · airframe 52,466 hrs · 42,956 cycles

SHIP 9594 ER/A 628659-14AD REV ORIGINAL REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: COMPLIED WITH ERA 628659-14AD REV ORIGINAL REP INSPECTION II. (1215579)

Part: REPAIR — OUT OF POSITION (ZONE 600) · airframe 52,203 hrs · 42,715 cycles

EXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. FOUND AT RT WING REAR SPAR INSPECTION AREA DURING ACCOMPLISHMENT OF AA EM 5720-01103. REPAIR PER ER/A 624368-14AD (1143045)

Part: STRUCTURE — CHAFED (ZONE 500) · airframe 52,203 hrs · 42,715 cycles

NUMBER 2 LT SLAT ATTACH POINT INSPECTION, SLAT DRIVE TRACK NR 5 CHAFED WING STRUCTURE ON INBD AT EDGE. REPAIRED ERA 628327-14 REV. (1143308)

Part: SKIN — CORRODED (ZONE 600) · airframe 51,376 hrs · 41,963 cycles

-AD- CORROSION FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER INSPECTION FC5720-01103. SUMMARY SEE NRC 004-0001:5720-01103- 01B/001 00001: COMPLIED WITH PRI 624368-14AD REV 0, PRI 624368-14AD REV 1, PRI 624368-14AD REV 2, PRI 624368-14AD REV 3, PRI 624368-14AD REV 4, AND ER/A 624368-14AD REV ORIGINAL. ORIGINAL MATERIAL THICKNESS .180 MATERIAL REMOVED .060. CORROSION LEVEL 1. (LP #0854618)

Part: SKIN — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 52,273 hrs · 42,777 cycles

EXFOLIATING CORROSION FOUND ON RIGHT WING REAR SPAR LOWER CAP AT APPROXIMATELY STATION XRS=164. (6925752)

Part: HINGE FITTING — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 51,376 hrs · 41,963 cycles

RIGHT WING INBOARD FLAP HINGE FITTING LOWER OUTBOARD STUD ON AFT SPAR HAS HEAVY RUST/PITTING. SUMMARY SEE NRC 004-0001:5720-01103-01B/006 00006: CORROSION LEVEL 2. REPLACED 4 EA MOUNTING STUDS PER B717 AMM 57-55-25-300-801. (LP #0849083)

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 51,176 hrs · 41,773 cycles

THE AFT EMERGENCY EXIT DOORS OVERWING LIGHTS, LT AND RT, ARE NOT COMING ON WHEN TESTED AT ROW 20. MAINTENANCE REPLACED THE B5-119 EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6967194)

Part: LIGHT — MALFUNCTIONED (EXTERIOR) · airframe 50,076 hrs · 40,809 cycles

EXTERIOR EMERGENCY ILLUMINATION SYSTEM LEFT AFT WING EXTERIOR EMERGENCY LIGHT STAYING ON. LEFT WING EMERGENCY ILLUMINATION WAS FOUND ON DURING PRE-FLIGHT. RELAMEPED WING EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK & RELAY PER B717 33-50 (B5-125 & R2-273). RELAMPED RIGHT AFT BULB. REPLACED BATTERY PACK PER B717 AMM 33-51. OPS CHECK NORMAL. (LP #0452296)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,352 hrs · 40,195 cycles

FOUND LEFT AND RIGHT AFT EMERGENCY EXIT DOOR LOCATOR SIGNS INOPERATIVE AT THE AFT OVERWING DOORS. MAINTENANCE REPLACED THE EMERGENCY BATTERY (B5-115) POWER SUPPLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5333890)

Part: RELAY — UNKNOWN (UNKNOWN) · airframe 48,894 hrs · 39,791 cycles

THE OVERWING ESCAPE PATH LIGHTING IS ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTS REMAINED ILLUMINATED WITH SWITCH IN OFF POSITION TOO. THE RELAY R2-273, WAS REPLACED PER B717 SWPM 20-20. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9375000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,602 hrs · 39,552 cycles

THE EXTERIOR EMERGENCY LIGHTS STAY ON WHEN SWITCH IS PLACED IN "ARM" POSITION. MAINTENANCE RESET THE EMERGENCY LIGHTS SYSTEM. PERFORMED AN OPERATIONAL CHECK IAW FIM B717 33-50 AND THE EEPL SYSTEM TESTED NORMAL. (LP #4996206)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,092 hrs · 39,098 cycles

THE OVERWING EXIT EXTERIOR LIGHTS ARE ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE REPLACED THE OVERWING EMERGENCY POWER SUPPLY PER B717 AMM 33-51. ALL OPERATIONAL CHECKS WERE NORMAL. OK FOR SERVICE. (LP #4617678)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACK ON AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN. SUMMARY OF NRC 00286: AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN WAS REPAIRED PER ER/A 610327-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 610327-14 REV. 2. (LP #2900343)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 610474-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 610474-14 REV. 2. ACCOMPLISH SECTION II REPETITIVE INSPECTIONS EVERY 8,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR PER ER/A 610474-14 REV ORIG UNDER LOG #2895988. ASSOCIATED ER/A 14-610474 ADDED FOR AC 9594. (LP #2899771)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFT CARGO. IN REF NRC0337. C2. SUMMARY OF NRC 00664: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFT CARGO WAS REPAIR PER ER/A 610520-14 REV ORIGINAL AND PRI 610520-14 REV 3. ACCOMPLISH SECTION II REPETITIVE INSPECTIONS EVERY 8,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR PER E/RA 610520-14 REV ORG. SECC II UNDER LOG 2897873. ASSOCIATED ER/A 14-610520 ADDED FOR AC 9594. (LP #2898345)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND 28LH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00317: LEVEL CORROSION 2. FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND 28LH BILGE AREA AT FWD CARGO COMPARTMENT WERE FABRICATED AND REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND DWG 5936597 REV AG. (LP #2897059)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON LOWER JAMB PAN INTERNAL AND EXTERNAL STRUCTURE STA 946 TO STA 1002 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00337: DOOR JAMB WAS REPLACED PER B717-200 SRM 51 -41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #2898062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00306: CORROSION LEVEL 2. TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER DWG 5936663, B717-200 SRM 51-40-04-0G AND 51-41-05-0G. (LP #2888418)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00645: CORROSION LEVEL 2. FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2886682)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR. SUMMARY OF NRC 00264: CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2884821)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACK ON FLOOR MEMBRANE WAS FOUND BTW STA Y 813-832 AND X=-44 TO X=-54 AT PAX CABIN. SUMMARY OF NRC 00648: FLOOR MEMBRANE BTW STA Y 813-832 AND X=-44 TO X=-54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIG 221. (LP #2880828)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACK WAS FOUND ON RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN. SUMMARY OF NRC 00630: RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIG 226, 51-41-02-0G, AND 51-41-05-0G PAR 10. (LP #2880836)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON PRODUCTION DOUBLER OF INNER FUSELAGE SKIN DRAIN STA 1007 BTW L30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00300: CORROSION LEVEL 2. DOUBLER OF INNER FUSELAGE SKIN DRAIN STA 1007 BTW L30 AT AFT CARGO COMPARTMENT (C2) WERE FABRICATED PER DWG 5971141 REV AND REPLACED PER B717 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2881168)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1). SUMMARY OF NRC 00643: CORROSION LEVEL 2. FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1) WAS REPLACED PER DWG 9936534 REV BW, DWG S2929169, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2877366)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON FLOOR SUPPORT (1 EA) BTW X 55 AND STA 200-204.5 WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.063 IN. MAXIMUM MATERIAL REMOVED IS 0.030 IN AND THEREFORE ALL AREAS REWORKED ARE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A, PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 (C) FIG 103 AND DC-MD/BOEING NDTSPM PART 4 04-00-06 PARA 4. SUMMARY OF NRC 00647: CORROSION LEVEL 2. FLOOR SUPPORT (1 EA) BTW X 55 AND STA 200-204.5 WAS REPLACED PER DRAWING 9936535 REV CS AND PER B717-200 SRM 51-41-05-0G PAR 8. (LP #2877363)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON GUSSET WITH NP: 3925389-1 UNDER VENTRAL DOOR STA Y=1065 AND X=18 AT CABIN PAX. SUMMARY OF NRC 00442: CORROSION LEVEL 2. GUSSET WITH NP: 3925389-1 UNDER VENTRAL DOOR STA Y=1065 AND X=18 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2875094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

FLOOR SUPPORT BTW X=13 TO 38.5 BTW STA Y=180 AT W1 AREA, IS CORRODED OUT OF LIMITS IN CABIN PAX. SUMMARY OF NRC 00638: CORROSION LEVEL 2. FLOOR SUPPORT BTW X=13 TO 38.5 BTW STA Y=180 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-02-0G PAR 4. (LP #2875085)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON SEAT TRACK, X-44 BTW STA 200-205 AT PAX CABIN. SUMMARY OF NRC 00369: CORROSION LEVEL 2. SEAT TRACK, X-44 BTW STA 200 TO 264 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 AND SRM 51-41-01-0G PROCEDURE GENERAL. (LP #2876390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON FLOOR FITTING ON AFT BULKHEAD BTW STA Y=1060 AND X=-22 AT AFT PAX CABIN. SUMMARY OF NRC 00374: CORROSION LEVEL 2. FLOOR FITTING ON AFT BULKHEAD BTW STA Y=1060 AND X=-22 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2876410 )

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX. SUMMARY OF NRC 00356: CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX WERE REPAIRED PER B717 SRM-53-00-55-2R-4 REPAIR 4 PAR 5 FIGURE 203 AND 204. (LP #2869967)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION OUT OF LIMITS ON LH MEMBRANE WEB UPPER, LOWER SURFACE BTW STA 463 TO STA 466 AT PAX CABIN IN REF NRC 0353. SUMMARY OF NRC 00657: CORROSION LEVEL 2. CORROSION OUT OF LIMITS ON LH MEMBRANE WEB UPPER/LOWER SURFACE BTW STA 463 TO STA 466 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-00-2R. (LP #2869217)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACK ON INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN. SUMMARY OF NRC 00438: INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR 4 FIGURE 201 AND 51-41-05-0G. (LP #2867499)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION OUT OF LIMIT ON FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 AND X=44, AND FROM STA Y=1022 TO STA Y=1053 AND X=53.5 AT CABIN PAX. (W2) IN REF NRC 0441. SUMMARY OF NRC 00622: FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 AND X=44, AND FROM STA Y=1022 TO STA Y=1053 AND X=53.5 AT CABIN PAX WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (LP #2866187)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,952 hrs · 38,976 cycles

CRACKED CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00399: CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #2862517)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,952 hrs · 38,976 cycles

CORROSION ON BULKHEAD STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00314: CORROSION LEVEL 2. BULKHEAD DOUBLER STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2856373)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,872 hrs · 38,911 cycles

SEVERAL EMERGENCY LIGHTS IN CABIN CEILING ARE INOPERATIVE. MAINTENANCE RELAMPED THEM IAW B717 AMM 33-51. (LP #6674820)

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 44,803 hrs · 36,648 cycles

THE AFT BULKHEAD EMERGENCY DOOR EXIT SIGN IS INOPERATIVE AND THE MID CABIN OVERHEAD AISLE EMERGENCY EXIT LIGHT IS ALSO INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLIES FOR AFT AND MID EMERGENCY LIGHTS IAW B717 AMM 33-50. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #3743077)

Part: BATTERY PACK — SHORTED (CABIN) · airframe 44,434 hrs · 36,406 cycles

ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR BOTH LEFT AND RIGHT FORWARD FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THAT BATTERY PACK ASSEMBLY B5-119 HAD INTERNAL SHORT. BATTERY PACK B5-119 WAS REPLACED. THE EMERGENCY LIGHTS NOW CHECK OK REF AMM 33-51.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 44,260 hrs · 36,290 cycles

EMERGENCY EXIT AT DOOR 1L HAS A DAMAGED DIFFUSER LENS ON THE EXIT SIGN AND THE COVER FALLS OFF. MAINTENANCE REPLACED THE LIGHT COVER ABOVE DOOR 1L AND INSTALLED A NEW DIFFUSER. CHECKS ARE GOOD. (LP 0784436)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,231 hrs · 36,267 cycles

8 EMERGENCY LIGHTS INOP AISLE OVHD DURING SVC CK. RELAMPED INOP LTS, NO HELP. FOUND 3 BULBS BURNT OUT. RELAMPED. OPS CKD PER AMM 33-52-00. ALL LIGHTS WORK. OK FOR SERVICE.

Part: DOOR FRAME — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 43,842 hrs · 36,008 cycles

SEVERAL AREAS ON THE FORWARD LOWER CARGO DOOR FRAME HAD SIGNS OF CORROSION. REPLACED THE FWD CARGO DOOR LOWER FRAME PAN IAW SRM 53-20-15-2R, REPAIR 6.

Part: CAM — COCKED (TAILCONE RELEASE) · airframe 43,832 hrs · 35,998 cycles

TAILONE RELEASE CAM TAB WAS CLOCKED INCORRECTLY. ADJUSTED THE RELEASE CAM IAW AMM 53-52-03.

Part: BRACKET — DAMAGED (BATTERY PACK) · airframe 43,070 hrs · 35,428 cycles

FOUND THE EMERGENCY LIGHT BATTERY PACK BRACKET TO BE DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,942 hrs · 35,341 cycles

EMERGENCY EXIT SIGN LENS MISSING IN THE FIRST CLASS CABIN. MAINTENANCE INSTALLED THE LENS. THE AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,891 hrs · 35,301 cycles

DURING SERVICE CHECK, FOUND BOTH AFT OVERWING EXIT HATCH LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE FOUND BATTERY PACK TO BE BAD. REPLACED THE BATTERY PACK ASSEMBLY B5-119. THE EMERGENCY LIGHTS TEST NORMAL IAW AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,694 hrs · 35,180 cycles

THE EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE AT THE FWD RIGHT GALLEY OVERHEAD, THE EXIT LOCATOR IN THE CEILING AT ROW 1, AND AT THE FWD DROP DOWN CEILING NEXT TO THE LAVATORY. MAINTENANCE REPLACED THE BATTERY PACK B5-259 IAW AMM 33-51 AND THE EMERGENCY LIGHTS RETURNED TO OPERATIONAL STATUS. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,297 hrs · 34,931 cycles

EMERGENCY LIGHTS AT 19A AND C ABOVE THE OVERWING EXITS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY (P1-12) AT POWER SUPPLY IAW AMM 33-51.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 41,277 hrs · 34,238 cycles

DURING A SERVICE CHECK, FOUND FLIGHT DECK EMERGENCY FLOOD LIGHT INOPERATIVE. FOUND CONNECTOR OF EMERGENCY LIGHTS BATTERY PACK B5-123 LOOSE. RESECURED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,102 hrs · 33,339 cycles

LOWER SIDEWALL EXIT IDENTIFIERS AT BOTH AFT EMERGENCY OVERWING DOORS INOP. REPLACED B5-119 PWR SUPPLY & BATTERY PER B717 AMM 33-51. CKS GOOD PER AMM.

Part: FRAME — DAMAGED (BS 974) · airframe 39,885 hrs · 33,173 cycles

FRAME DAMAGED BS 974, REPAIRED IAW ER/A 554277-14 REV O.

Part: SKIN — DAMAGED (BS 207-220) · airframe 38,922 hrs · 32,545 cycles

FUSELAGE SKIN BS 207-220 18R-21R DAMAGED. INSTALLED PERMANENT SKIN REPAIR IAW ER/A 549610-14, REV 0.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

WHILE GAINING ACCESS TO L/L REPAIR, FOUND CUSP WEB MEMBRANE CORRODED AT STA 200-218, RBL 56-RBL44. FABRICATED NEW CUSP WEB IAW DWG 9936535. ALODINED, PRIMED, TOP COATED NEW CUSP WEB IAW AMM 51-10-00 370-803. INSTALLED NEW WEB IAW SRM 51-41-02, SEC 4 AND 51-41-08, SEC 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

REPAIRED LT FUSELAGE EXTERIOR SKIN CRACK AT STA 1095 JUST ABOVE LONGERON 14L IAW ER/A 547512-14. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY 3000 CYCLES IAW ER/A 547512-14. ACCOMPLISH SECTION II REPETITIVE INSPECTIONS EVERY 3000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR ASSOCIATED ER/A 95-547512.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

FORWARD RT SERVICE DOOR LOWER HORIZONTAL FRAME CRACKED AT LOWER DOOR HINGE. REPLACE LOWER FRAME. REMOVED CRACKED FRAME AND REPLACED WITH FABRICATED FRAME, PN 9911582-21 IAW DWG 9911582, REV T AND SRM 57-41-01, FABRICATION CERTIFICATE OF CONFORMANCE AMES REF 71130-0000-0011. CUST REF NR 900213559, MATERIAL 7075-0-080QQAA-250/13 TAG 1672321, HEAT TREAT TO T6 CONDITION.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

SEAT TRACK ATTACH ANGLE RBL 56, STA 200-214 HAS CORROSION AND DAMAGED FASTENER HOLES. BLEND CHECK LIMITS. SEAT TRACK ATTACH ANGLE RBL 56, STA 200-214 FASTENER HOLES FOUND TO BE OUT OF LIMITS. REPLACEMENT ATTACH ANGLE WAS MATCH DRILLED IAW SRM 51-40-08, PG 1, PAR 3. INSTALLATION OF TRACK ANGLE WAS COMPLIED WITH ON ORNRC 71129-0200-0248, ITEM NR 6.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

CUSP WEB RBL 44-58, STA 218-237 IS CORRODED AT MARKED LOCATIONS. CLEAN AND RE-EVALUATE. CUSP WEB, RBL 44-58, STAS 218-237 WAS BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-41-02, PG 3, PAR F, TAG 12663.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

CUSP WEB MEMBRANE CORRODED BEYOND LIMITS AT STA 200-160, RBL 54. REMOVED AND TRIMMED CUSP MEMBRANE STA 160-200 IAW SRM CHAPTER S1 & ER/A 549606-14. PERFORMED HFEC OF CUTOUT AREA IAW NON DESTRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6 PRECEDURE 06-10-01.001. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION IAW ER/A NR 549606-14. NO DAMAGE NOTED. FABRICATED CUSP MEMBRANE AND SPLICE DOUBLER IAW ER/A 549606-14 STEP 5. INSTALLED IAW ER/A 549606-14, STEP 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

FLOOR SUPPORT AT STA HAS CORROSION AT MARKED LOCATIONS ON REPAIR RACK BLEND CHECK LIMITS. BLEND FLOOR SUPPORT STA 200 IAW SRM 51-10-04. ORIGINAL .070 REMAINING .042 OUT OF LIMITS IAW B DWG S00074, TAG 6887. FABRICATED FLOOR SUPPORT IAW SRM 51-20-09. TREATED, PRIMED, AND TOPCOATED IAW AMM 51-10-00 370-803, PAR C & D. INSTALLED SUPPORT IAW SRM 51-40-02.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

BULKHEAD TO LONGERON ATTACH CLIP AT STA 1087, LONGERON 20R CORRODED. BLEND CHECK LIMITS. REPLACED BULKHEAD TO LONGERON ATTACH CLIP -51 AT STA 1087, L20R IAW SRM 51-41-02 AND 51-10-04, PARA 26 AND 51-41-05, PG 17, PARA 8.

Part: FORMER — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

ALL 3 RT CANTED KEEL FORMERS ARE CRACKED ON OTBD ENDS AT STA 674, 696, AND 714. REMOVED AND REINSTALLED FOR CANTED KEEL FORMERS ON OTBD ENDS AT STATIONS 674, 696, AND 714 IAW SRM 51-41-02 AND SRM 51-41-05. REPAIRED DAMAGE TO CANTED KEEL FORMERS ON OTBD ENDS AT STA 674, 696, AND 714 IAW ER/A 545683-14 MA REV. REMOVED DAMAGE FROM FORMERS IAW ER/A 545683-14 MA REV-STEP 1. FABRICATED REPAIR ANGLES AND REPAIR FILLERS. HEAT TREATED FABRICATED PARTS TO 7075 T6 IAW ER/A 545683-14 MA REV REFER TO WO 71130-0007. HFEC PERFORMED IAW ER/A 545683-14 STEP 2 IAW NDT SRM PART 06, NO DEBRIS TAG. OPEN HOLE SEAM PERFORMED IAW ER/A 545683-14, MA STEP 3 IAW NDT SPM PART 06. NO DEFECTS, TAG 6742.

Part: SLAT — GOUGED (RT WING) · airframe 38,920 hrs · 32,543 cycles

L/E RT WING OTBD OF NR 5 SLAT AT WING TIP HAS SLAT, WING TIP, AND WING L/E CHAFING. CHECK LIMITS. L/E RT WING OTBD NR 5 SLAT REMOVED IAW SRM 51-41-02 DUE TO GOUGE AND WAS OUT OF LIMITS .025. REMOVED ORIGINAL THICKNESS WAS .063, TAG 2721 IAW SRM 57-00-00, FIG 103. WELD REPAIRED DAMAGED ON FORWARD UPPER SIDE WING TIP IAW ER/A 545680-14MA, STEPS 2 THRU 8. L/E WING TIP SUPPORT PN 5920519-2 INSTALLED IAW SRM 51-41-08, FIG 5 AND 51-40-03, PG 22 AND 23.

Part: TIP CAP — DAMAGED (RT WING) · airframe 38,920 hrs · 32,543 cycles

L/E RT WING OTBD OF NR 5 SLAT AT WING TIP HAS SLAT, WING TIP, AND WING L/E CHAFING. CHECK LIMITS. L/E R/W OTBD NR 5 SLAT REMOVED IAW SRM 51-41-02 DUE TO GOUGE AND WAS OUT OF LIMITS .025. REMOVED ORIGINAL THICKNESS WAS .063, TAG 2721 IAW SRM 57-00-00, FIG 103, WELD REPAIRED DAMAGED ON FORWARD UPPER SIDE WING TIP IAW ER/A 545680-14MA, STEPS 2 THRU 8 L/E WING TIP SUPPORT, PN 5920519-2, INSTALLED IAW SRM 51-41-08, FIG 5 AND 51-40-03, PG 22 AND 23.

Part: FRAME — CORRODED (BS 889) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

CORROSION ON LOWER SECTION OF A FRAME AT BS 889, LONGERONS 25 - 28R IN THE AFT CARGO. BLENDED TO REMOVE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-20-07 REPAIR 3.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

AFTER REMOVAL OF LIFE LIMITED REPAIR, FOUND LONGERON 19R HOLES TO BE DAMAGED AT STA 207-218. REPLACED LONGERON 19R STA 188-218 IAW SRM 51-41-02 AND 51-41-05 FABRICATED NUT CHANNEL AND .063 SPLICE IAW SRM 53-00-55, REPAIR 2.

Part: RIB — CRACKED (CARGO DOOR) · airframe 38,920 hrs · 32,543 cycles

FORWARD CARGO DOOR HAS CRACKED RIBS ON LOWER SIDE IN 2 PLACES. MARKED, FABRICATED, -41 WEB AND -43 ANGLE FOR LOWER FORWARD AND AFT RIBS IAW BP 9957664. PROTECTIVE TREATMENT APPLIED IAW SRM 51-10-04, TABLE 1 AND DPSM 900-3-6, NR 34. INSTALLED FORWARD AND AFT LOWER RIBS IAW DWG 9957664 AND SRM 51-41-05.

Part: STRINGER — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

PROTECTIVE COATING MISSING FROM LONGERON L-29L, STA 932. POSSIBLE CORROSION. REPAIRED DAMAGED AREA BY BLENDING IAW 53-00-00, FIG 103 AND INSTALLING REPAIR U-CHANNEL DOUBLER OVER AREA IAW SRM 53-00-05, REPAIR 3, FIG 201. ORIGINAL THICKNESS .125" REMOVED .031. WHICH IS WITHIN REPAIRABLE LIMITS IAW SRM 53-00-05, REPAIR 3, FIG 201. APPLIED SCEPTER DECAL IAW DSPM 900-5-1, NR 04.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

SHEER TIE CLIP ON THE FWD SIDE OF STA 1002, BULKHEAD AT LONGERON 14R IS CRACKED. REPLACED SHEAR TIE CLIP ON THE FWD SIDE OF STA 1022 BULKHEAD 14R IAW SRM 51-41-05, 51-41-02, PAL-4.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

RIGHT CUSP WEB CRACKED AT LIGHTNING HOLE FUSELAGE STA 807, MARKED. REPLACED CUSP WEB AT RT FLOOR FUSELAGE STA 807 IAW SRM 51-41-01, 51-41-05, 51-41-08.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

RIGHT CUSP WEB RBL 60, STA 389-STA 408 CORROSION FOUND TO BE OUT OF LIMITS. REPAIR CORRODED CUSP WEB BY REMOVING AND REPLACING DAMAGE SECTION OF CUSP WEB FROM FS 370 TO FS 440 IAW SRM 53-00-55, REPAIR 4, FIG 223, USING SECTION OF CUSP WEB, PN 9930538475. APPLIED LOG DECAL IAW DPM 900-5-1, NO 4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

SHEER TIE CLIP ON THE FWD SIDE OF STA 1022 BULKHEAD AT LONGERON 7L IS CRACKED. REPLACED SHEAR TIE CLIP ON FWD SIDE OF STA 1022 BULKHEAD AT LONGERON 7L IAW SRM 51-41-05, PG 1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

SHEAR TIE CRACKED AT LONGERON L15, STA 1022, MARKED. REPLACED SHEAR TIE AT LONGERON 14L, STA 1022 BULKHEAD IAW SRM 51-41-05, PG 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

FORWARD CARGO FUSELAGE STA 636, BL0 INTERCOSTAL CRACKED. REPAIRED CRACK IAW SRM 53-00-00, REPAIR 1, FIG 201 & SRM 51-41-05, PG. 17, NR 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

FRAME FORMER ON THE AFT SIDE OF STA 1022, BULKHEAD AT LONGERON 7L IS CRACKED. REPAIRED FRAME FORMER ON THE AFT SIDE OF STA 1022, BULKHEAD AT 7L LONGERON IAW SRM 51-70-11, REPAIR 1 .

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,920 hrs · 32,543 cycles

RIGHT CUSP WEB STA 936-946, RBL 60 HAS CORROSION. BLENDED OUT ALL SIGNS OF CORROSION. TREATED AND PRIMED AREAS OF REPAIR, BLEND IAW SRM 51-10-04, MATERIAL LOSS WAS OUT OF LIMITS AT RT CUSP WEB STA 936-946, RBL60, FABRICATED, DRILLED, AND INSTALLED A PRIMARY DOUBLER AND RING DOUBLER OVER AREA OF BLEND OUT IAW SRM 53-00-55, CONFIGURE 7027, FIG 216, REPAIR 4.

Part: CUSP WEB — DENTED (FUSELAGE) · airframe 38,920 hrs · 32,543 cycles

FORWARD CARGO FUSELAGE STA 560-579, RT CUSP WEB DENTED AND CUSP WEB HAS A GAP UNDER 3 RIVET HEADS, JUST AFT OF DENT, MARKED. CHECKED DENT LIMITS ON CUSP WEB AT FS 575 IAW SRM 53-00-01. ALLOWABLE DAMAGE 1, FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED RT CUSP WEB IAW SRM 53-00-55 REPAIR 4. GAPPED FASTENERS REPLACED WITH REPAIR INSTALLATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,288 hrs · 31,254 cycles

DURING LINE CHECK, NOTED AFT EMERGENCY LIGHTS OUT STARTING AT ROW 25C. REPLACED EMERGENCY LIGHT BATTERY, CHARGER AND OPERATION CHECKED GOOD.

Part: SHROUD — CRACKED (FUEL TANK) · airframe 37,215 hrs · 31,200 cycles

DURING PILOT WALKAROUND IN PBI, NOTED FUEL SMELL THROUGHOUT ACFT AND IN THE AFT CARGO COMPARTMENT. THE ODOR WAS STRONGEST NEAR SEAT ROWS 19-24. AFTER PROVIDING ACCESS IN THE AFT BAG BIN, FOUND FUEL RETURN TO TANK SHROUD CRACKED, LEAKING WITH SURROUNDING INSULATION BLANKETS FUEL SOAKED. REPLACED LINE ALONG WITH LEAKING O-RINGS AT COUPLING SEAL, REF: B717 IPC 28-24-03-01 ITEM 330. ENGINE RUN AND ASSOCIATED LEAK CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,124 hrs · 31,139 cycles

EMERGENCY EXIT SIGNS TO COCKPIT DOOR 1LT, 1RT AND BOTH FWD OVERWING DOORS ARE INOPERATIVE. REPLACED B5-235 BATTERY. REPLACED B5-118 POWER SUPPLY AND BATTERY. FUNCTIONAL CHECK IS GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,718 hrs · 30,815 cycles

EMERGENCY LIGHT SIGN OVER F/A SEAT IN GALLEY INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED NORMAL IAW MM 33-51.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 36,284 hrs · 30,441 cycles

CABIN PRESSURE INFLOW LOW MESSAGE AT APPROXIMATELY 6000 FT ON CLIMB, CABIN PRESSURE SEEMED NORMAL. CLIMBED TO FL 250, LIMITED DUE TO EXISTING MEL 21-50-01, RELATED TO A RT PACK OVERHEAT. THE CABIN CONTINUED TO CLIMB SO DESCENDED TO FL190. AT FL190 CABIN STABILIZED AT ABOUT 7000 FT. DURING DESCENT INTO LAX THE CABIN DID NOT DESCEND AS RAPIDLY AS IT SHOULD HAVE, AT 5000 FT, CABIN WAS 4400 FT. DECLARED EMERGENCY. THERE WAS NO EXPEDITED DESCENT OR OXYGEN MASK DEPLOYMENT. MAINTENANCE REPLACED THE RT ACM & FLOW CONTROL VALVE. ALSO REPLACED NR 2 CABIN PRESSURE CONTROLLER. SYSTEM CHECKS NORMAL. 14 CFR PART 121.703 DOES NOT DIFFERENTIATE REPORTING CRITERIA IF ATC DECLARES AN EMERGENCY ON BEHALF OF THE FLIGHT CREW.

Part: SKIN — DAMAGED (BS 219) · airframe 35,590 hrs · 29,925 cycles

FUSELAGE SKIN DAMAGED, STA 219, L19R, REF LOG 159514 & 1596511. REMOVED DAMAGE, INSTALLED DOUBLER IAW PRI 533592-14, REV 01. RII COMPLETED. WAITING FINAL ER/A. ACCOMPLISHED ER/A 533592-14, REV O, SEC 1, QC1976.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,960 hrs · 29,415 cycles

DURING LINE CHECK, FOUND LT EMERGENCY LIGHT INOPERATIVE, EXTERIOR AFT OF WING. REPLACED THE LAMP IAW AMM 33-51-05.

Part: LANYARD — MISROUTED (L1 DOOR) · airframe 34,226 hrs · 28,840 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LANYARD MISROUTED. REROUTED LANYARD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,226 hrs · 28,840 cycles

OVERWING DOOR EMER LIGHTS BULB INOPERATIVE. R & R BULB IAW AMM.

Part: MOUNT BRACKET — BROKEN (CABIN) · airframe 34,226 hrs · 28,840 cycles

FORWARD CEILING EMER LIGHT MOUNT BRACKET BROKEN AT BOTH FASTENERS. REPAIRED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,226 hrs · 28,840 cycles

TAIL COMPARTMENT 3RD AFT EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,226 hrs · 28,840 cycles

AFT EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SLIDE — OUT OF POSITION (TAILCONE) · airframe 34,146 hrs · 28,789 cycles

TAIL CONE EMER EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW AMM.

Part: SKIN — CANNING (APU DOOR) · airframe 34,146 hrs · 28,789 cycles

LEFT APU DOOR SKIN LARGE AREA OIL CANNING APPROXIMATELY 6 INCHES FROM FWD EDGE & 12 INCHES FROM INBD EDGE. REPAIRED SKIN IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

CUSP WEB CRACKED AT BS 218, RBL 44.5. REPAIRED CUSP WEB IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

AFT CARGO BILGE AREA FORMER CORRODED AT BS 973 BETWEEN LONGERON 29L TO 29R. REPAIRED FORMER IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

FRAME FLOOR SUPPORT CORRODED AT BS 937 LONGERON 28L. REPAIRED SUPPORT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

AFT CARGO FLOOR STRUCTURE D RING MOUNTING FITTING CRACKED AT BS 946. R & R FITTING IAW SRM & DWG.

Part: BEAM — CRACKED (L1 DOOR) · airframe 34,146 hrs · 28,789 cycles

L1 DOOR UPPER BEAM CRACKED IN RADIUS AFT END. R & R BEAM IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

FORWARD CARGO DOOR PAN CORRODED. R & R PAN IAW SRM.

Part: SUPPORT FITTING — CORRODED (R1 DOOR) · airframe 34,146 hrs · 28,789 cycles

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

Part: PAN — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

AFT CARGO DOOR LOWER JAMB PAN CORRODED. REPAIRED PAN IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200 BETWEEN RBL 9 TO RBL 47. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 237 BL 0. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 256 LBL 14. REPAIRED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 218 BETWEEN LBL 13 TO RBL 8. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 34,146 hrs · 28,789 cycles

LEFT WING TO BODY AFT SECTION ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (RT WING) · airframe 34,146 hrs · 28,789 cycles

RIGHT WING FIXED TE BEHIND AILERON SECTOR QUADRANT LOWER EDGE CORRODED. REPAIRED QUADRANT IAW SRM & EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 34,146 hrs · 28,789 cycles

RIGHT WING FLAP LOWER INBD FAIRING CRACKED. R & R SKIN IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (LT AILERON) · airframe 34,146 hrs · 28,789 cycles

LEFT WING OTBD AILERON HINGE SUPPORT FITTING CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

SKIN CORRODED BETWEEN BS 957 TO 993 LONGERON 29R. REPAIRED SKIN IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,789 cycles

FUSELAGE SKIN DOUBLER CRACKED AT BS 1022. REPAIRED DOUBLER IAW EA.

Part: BRACKET — CRACKED (FLOOR) · airframe 34,146 hrs · 28,789 cycles

LEFT MLG WW NEAR KEEL BEAM ANGLE BRACKET CRACKED AT BS 748. R & R BRACKET IAW SRM & DWG.

Part: PSEU — FAULTY (E&E BAY) · airframe 34,170 hrs · 28,804 cycles

BOTH MLG POSITION LIGHTS INDICATION CYCLED SEVERAL TIMES, ON APPROACH PSEU LIGHT INDICATION. R & R PSEU IAW MM.

Part: PSEU — FAULTY (COCKPIT) · airframe 34,170 hrs · 28,804 cycles

IN ROUTE THE LT & RT MAIN GEAR LIGHT CYCLED SEVERAL TIMES. R & R PSEU IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,045 hrs · 28,724 cycles

RIGHT EMERGENCY EXIT LIGHT LOOSE AT ROW 27D. SECURED LIGHT ASSEMBLY IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,443 hrs · 27,043 cycles

EMERGENCY LIGHT POWER SUPPLY INOP BETWEEN BS 231 AND BS 121. REMOVED AND REPLACED POWER SUPPLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,108 hrs · 27,446 cycles

FUSELAGE SKIN CRACKED AT STA 1022. REPAIRED SKIN IAW SRM & EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,443 hrs · 27,043 cycles

EMERGENCY LIGHTS INOP BETWEEN BS 259 TO BS 235. REMOVED AND REPLACED CHARGER ASSY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,443 hrs · 27,043 cycles

RT EMERGENCY ESCAPE PATH LIGHTS INOP BETWEEN ROWS 25 TO ROW 30. REMOVED AND REPLACED CHARGER ASSY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RIGHT SIDE AFT FUSELAGE EXTERIOR SKIN CRACKED ABOVE FWD TOP SIDE PYLON - FS 1022. REPAIRED DOUBLER IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RIGHT CUSP WEB CRACKED AT STA 820, RBL 44.5. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RIGHT SIDE CUSP WEB CRACKED AT STA 652.5, RBL 51.0. R & R CUSP WEB IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LEFT AFT WING TO BODY LOWER SECTION OF FRAME CORRODED AT FS 851. REPAIRED DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LEFT AFT WING TO BODY FRAME CRACKED AT FL 832, LONG 23L. R & R FRAME IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 588 TO STA 646, RBL 44. REPAIRED SEAT TRACK IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,443 hrs · 27,043 cycles

LT AFT LAV EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW B717 AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 256 TO STA 588, LBL 44. R&R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 256 TO STA 588, LBL 44. R&R SEAT TRACK IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT STA 1161, LONG 2R. R & R FORMER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 256 TO STA 588, RBL 22. / R&R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

SEAT TRACK SECTION CORRODED BETWEEN STA 646 TO STA 821, RBL 44. R & R SEAT TRACK IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT STA 1161, LONG 2L. R & R FORMER IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 715 TO STA 813, RBL 44.5. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 550 TO STA 617, RBL 44.5. R & R PANEL IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

CENTER SECTION VERTICAL SUPPORT CRACKED BELOW SEAT TRACK STA 737, LBL 44. R & R SUPPORT IAW SRM AND DWG.

Part: LINER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT CARGO FWD BULKHEAD LOWER LT LINER SUPPORT STRAP CRACKED. R & R LINER IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

CENTER SECTION VERTICAL SUPPORT CRACKED AT STA 737, RBL 44. R & R SUPPORT IAW SRM AND DWG.

Part: LINER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT CARGO FWD BULKHEAD UPPER RT LINER SUPPORT STRAP CRACKED. R & R LINER IAW SRM.

Part: LINER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT CARGO FWD BULKHEAD LOWER RT LINER SUPPORT STRAP CRACKED. R & R LINER IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RIGHT CUSP CORRODED BETWEEN STA 522 TO STA 541. REPAIRED CUSP IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 484 TO STA 522, RBL 44.5. R & R PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RT CUSP CRACKED AT STA 660. REPAIRED CUSP WEB IAW SRM AND AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RT CUSP CORRODED AT STA 456. R&R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 323 TO STA 389, RBL 44.5. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 400 TO STA 465, RBL 44.5. REMOVED AND REPLACED PANEL IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

C-2 DOOR CUTOUT FWD SIDE OF DOOR PAN CORRODED. R & R PAN IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED BETWEEN STA 285 TO STA 294, RBL 44.5. R&R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

MAIN CABIN FLOOR PANEL #222 YF DELAMINATED. R&R PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RIGHT CUSP CORRODED BETWEEN STA 465 TO STA 484. REPAIRED WEB IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

ENGINE PYLON SUPPORT CRACKED AT BULKHEAD, BS 1022, BETWEEN LONG 13R TO LONG 14R. R & R FORMER IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LEFT AFT WING TO BODY LOWER SKIN SURFACE CORRODED AROUND NUTPLATE HOLES FS 851, LONG 28L. REPAIRED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,108 hrs · 27,446 cycles

LEFT AFT WING TO BODY LOWER SKIN CORRODED AROUND NUT PLATE HOLES AT FS 851, LONG 28L. REPAIRED DOUBLER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LEFT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22L. R & R FITTING IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOOR PANEL CORRODED AT STA 725, LBL 44.5. R & R PANEL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FLOORBEAM CRACKED AT FS 737 AND LONG 18L. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (TAILCONE) · airframe 31,443 hrs · 27,043 cycles

TAIL CONE INTERIOR JETTISON HANDLE STOWAGE ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PAN — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN INTERNAL WINDOW FRAME STRUCTURE CRACKED AT FWD LOWER CORNER BETWEEN FS 696 TO FS 715 LT SIDE. R & R RING PAN IAW SRM AND DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LT CUSP CORRODED AT STA 440. REPAIRED DOUBLER IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT ACCESSORY COMPARTMENT LT LOWER BOX ATTACH ANGLE CRACKED AT FRAME 1200. R & R ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

MAIN CABIN LT OVER CENTER WING AREA CUSP WEB CRACKED FROM LIGHTENING HOLE INBRD TO WEB EDGE STA 674. REPAIRED WEB IAW SRM,

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

RT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW SRM & DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD 222AMF DELAMINATED. R & R PANEL IAW SRM AND AMM.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

LONGERON SPLICE CRACKED AT FS 1144, LONG 2R. R & R LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

AFT ACCESSORY COMPARTMENT LONGERON CRACKED AT FS 1144, LONG 2L. R & R LONGERON SECTION IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222AEF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222AAF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222AHF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 22PF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222ATF DELAMINATED. R & R PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

OVERWING FRAME CRACKED AT BS 715, BETWEEN LONG 9L TO LONG 18L. R&R LONGERON IAW MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222APF DELAMINATED. R & R PANEL IAW SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

C-1 DOOR PAN AFT SPLICE CRACKED. R&R C1 DOOR PAN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,443 hrs · 27,043 cycles

FRAME CRACKED AT BS 696, BETWEEN LONGERON 9L TO LONGERON 18L. R & R FRAME IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222JF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222ACF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD # 222ABF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222LF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222RF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #221 UF DELAMINATED. R&R PANEL IAW MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 223DF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD NR 222AVF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222 AGF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #221WF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 31,443 hrs · 27,043 cycles

PAX CABIN FLOORBOARD #222FF DELAMINATED. R&R PANEL IAW SRM AND MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,643 hrs · 26,536 cycles

F/A REPORTS AFT F/A FLASHLIGHT NOT FLASHING. REMOVED AND REPLACED BATTERY PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 30,364 hrs · 26,355 cycles

RIGHT EEPLS LOOSE AT ROW 19. REMOVED AND REPLACED EEPLS PER MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 29,744 hrs · 25,928 cycles

RIGHT EEPLS INOP AT ROW 27. REPAIRED CONNECTOR IAW AMM.

Part: ACTUATOR — FAULTY (RT SPOILER) · airframe 28,967 hrs · 25,408 cycles

DIVERSION -- AT CRUISE LOUD NOISE IN AFT SECTION ACCOMPANIED BY A VIBRATION IN THE FLOOR. FOUND RT WING O/B SPOILER ACTUATOR FAULTY. REMOVED AND REPLACED SPOILER PER MM.

Part: CABLE — LOOSE (L1 DOOR) · airframe 28,964 hrs · 25,406 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE LOOSE. SECURED CABLE PER MM.

Part: COVER — LOOSE (CABIN)

LIGHT COVER AT AFT F/A OVERHEAD FELL OUT (MX SECURED WITH TAPE). OPEN DEFECT.

Part: GROUND STUD — LOOSE (CABIN)

SEAT MOUNTED EMERGENCY FLOOR AISLE LIGHTS INOP AT SEAT ROW 11, 12, 14, 15, 16, 17 AND 18. PERFORMED FIM TASK 33-50 TASK 8/01. FOUND LOOSE GROUND STUD AT STATION 503R BETWEEN LONGERONS 7R AND 8R - TIGHTENED AS REQUIRED - REF B717 SWPM 20-50 AND WIRING DIAGRAM MANUAL 33-51-14, OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT TEST FAILS, SEAT 11 TO 18. REMOVED AND REPLACED EMERGENCY BATTERY ASSY AND SUPPLY ASSY PER AMM 33-51. OPS CHECKED GOOD.

Part: LENS — OUT OF POSITION (EXIT SIGN)

F/A'S DISCOVERED EMER EXIT SIGN COVER IN FWD GALLEY. SIGN COVER BELONGS ON BUSINESS CLASS CEILING EXIT SIGN. INSTALLED NEW LENS, SP8103, AT FWD EXIT SIGN.

Part: LENS — MISSING (CABIN)

EMERGENCY ESCAPE PATH LIGHT LENS MISSING AT SEAT 21D. REMOVED AND REPLACED LIGHT ASSY ON 22D. LENS INSTALLED ON 21D REF AMM 33-51.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FWD CARGO COMPARTMENT AFT LOWER BULK HEAD ATTACH ANGLE, STA 655, LONG 28L TO 28R, CRACKED. ACCOMPLISHED ATTACH ANGLE DOUBLER REPAIR PER B717 SRM 51-70-11.

Part: ATTACH ANGLE — CORRODED (RT WING)

RIGHT WING LOWER T/E PANEL, FWD OF MLG SIDE BRACE ATTACH ANGLE, CORROSION. ACCOMPLISHED ATTACH ANGLE REPLACEMENT PER B717 SRM 51-70-11 REPAIR 1.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME SECTION, STA 1002, LONG 30, CORROSION. ACCOMPLISHED FRAME SECTION REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05 AND BOEING DWG PL9957739-151.

Part: FITTING — CORRODED (FUSELAGE)

R1 DOOR GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 237, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01, B717 SRM 51-41-02 AND B717 SRM 51-10-04.

Part: DOOR FRAME — CRACKED (FUSELAGE)

MAIN CABIN LT FWD ENTRY DOOR JAMB, STA 205, LONG 15, CRACKED. ACCOMPLISHED ENTRY DOOR JAMB DOUBLER REPAIR PER B717 SRM 51-70-10 AND B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 198, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: SKIN — DENTED (TAILCONE)

FORWARD OF TAIL CONE FUSELAGE SKIN, DENTED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER B717 SRM 53-00-01 REP 6 AND EA 17-53-02869IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, LBL 12 TO RBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, B717 SRM 53-00-00 AND B717 SRM 51-10-04.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 200, RBL 9 TO RBL 47, CORROSION. ACCOMPLISHED FLOOR WEB REPLACEMENT PER B717 SRM 51-41-02 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 155 TO 198, RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01 AND BOEING DWG SR09936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 196, LBL 21, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160, LBL 3 TO RBL 3, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-42-02, AND 51-40-08 AND BOEING DWG SR09936534.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN RT INBOARD SEAT TRACK, STA 200 TO 254, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER BOEING DWG SR09530085.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 158 TO 193, LBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 160, LBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: WEB — CORRODED (FUSELAGE)

MAIN CABIN FLOOR WEB, STA 196, RBL 13, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT L-30 CORRODED BETWEEN STA 927 AND 980. INSTALLED NEW LONGERON SECTIONS L-30 AND SPLICES REF B717 SRM 53-00-05 FIG 201 REPAIR 2 AND REF 09-0840.

Part: DOOR FRAME — CORRODED (BS 370-427)

FWD CARGO DOOR JAMB SECTION CORRODED BEYOND LIMITS. CUT OUT LOWER PAN SECTION FROM FS 370 TO FS 427, INSTALLED NEW LOWER PAN SECTION AND SPLICES REPAIR PER REF SRM 53-20-15 REPAIR 6 FIG 201.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2985.

Part: SKIN — GOUGED (FS 215-244)

GOUGES IN FUSELAGE SKIN FS 215-244 LONGERON 16L. BLENDED DAMAGE, FABRICATED AND INSTALLED INTERNAL DOUBLER IAW B717 SRM 53-00-01 REPAIR 2.

Part: PAN — CORRODED (CARGO DOORWAY)

AFT CARGO DOOR JAM CUT OUT LOWER PAN HAS CORROSION. CUT OUT LOWER JAM SECTION AND INSTALLED LOWER JAM SECTION AND SPLICES AT AFT CARGO COMP IAW B717 SRM 53-20-15 REP 7.

Part: SKIN — DAMAGED (FUSELAGE)

CATERING TRUCK HIT ACFT WITH RAILING, DAMAGED JUST AFT OF R1 DOOR (DAMAGE IS AT FS 216R L19 MEASURES 4" X 1.5" X .125" D/X=12) CONDITION 3 PER 717 SRM 53-00-01 REPAIR 2 PAGE 210. REPAIR WITHIN 4500 FLT HOURS. COMPLIED WITH N/R-00001 ON AAR W/O 28402 NRWC 3588-359. REPLACED TEMP FASTENERS & FABRICATED NEW DOUBLER.

Part: EEC — MALFUNCTIONED (RT ENGINE)

DURING CLIMBOUT AT CLIMB THRUST AT APPROX 14,000 FEET THE RIGHT ENGINE ROLLED BACK (THROTTLES DID NOT MOVE) EPR & TGT FELL, AUTO-IGNITION CAME ON & ENGINE RECOVERED. NO AUDIBLE INDICATIONS, NO ALERTS, NO FAULTS. THIS REOCCURRED APPROXIMATELY 2 MINUTES LATER. AGAIN NO INDICATIONS AND ENGINE RECOVERED WHEN AUTO-IGNITION CAME ON. ACTED LIKE A FLAMEOUT THAT RESTARTED WHEN THE IGNITION CAME ON. CLEAR AIR. REMOVED AND REPLACED NR 2 EEC PER B717 AMM 73-21 PERFORMED RTS ON NR 2 EEC PER B717 AMM 73-21 RTS PASSED NO FAULTS NOTED.