N891AT

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 50,522 hrs · 36,079 cycles

DURING SERVICE CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION B5-259 IAW AMM 33-51. ALL LIGHTS WORK NORMAL. OK FOR SVC. (8218009).

Part: SLIDE — NO TEST (ZONE 800) · airframe 49,736 hrs · 35,350 cycles

AIRCRAFT 9551, SLIDE FAILED DEPLOYMENT TEST PER AMDS WORK CARD 2561-9003 FORCAST# 95-0525-8-0131. CORRECTIVE ACTION: SLIDE FAILED TO DEPLOY DUE TO A BROKEN CABLE P/N 2919845. REPLACED KEVLAR TAIL CONE CABLE REF B717 AMDS WORKCARD 2561-9003. (LP 7297639)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,023 hrs · 34,712 cycles

THE EMERGENCY LIGHTS FOR THE RH AFT EMERGENCY EXIT AND THE LH AFT LAVATORY WERE FOUND INOPERATIVE. SUMMARY OF NRC 00168: THE LAMPS FOR THE EMERGENCY LIGHTS AT THE RH AFT EMERGENCY EXIT AND LH AFT LAVATORY WERE REPLACED PER B717 AMM 33-52-18. THE SYSTEM NOW OPERATES CORRECTLY. (LP #0867831)

Part: VANE — CRACKED (ZONE 500 LE FLAP) · airframe 49,023 hrs · 34,712 cycles

CRACK ON UPPER SURFACE OF FLAP MOVABLE VANE AT LH WING. SUMMARY OF NRC 00063: FLAP MOVABLE VANE AT LH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE WITH B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0859916)

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 49,023 hrs · 34,712 cycles

CRACK ON INTERCOSTAL STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00146: INTERCOSTAL ON STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0858310)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,372 hrs · 33,249 cycles

ON SERVICE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FWD OVERWING UPPER EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE #6 &#7 EMERGENCY LIGHT BATTERY PACKS WERE REPLACED REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #5891524)

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 47,290 hrs · 33,182 cycles

THE FWD L1 DOOR EMERGENCY LIGHT IS INOPERATIVE. CONDITION WAS FOUND ON SERVICE CHECK. MAINTENANCE FOUND THE BATTERY ASSEMBLY BAD AND REPLACED IT IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5308068)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,697 hrs · 31,837 cycles

SHIP 9551 -ATB- THE CREW NOTED STRONG AIRFRAME VIBRATION AS THE AIRCRAFT ACCELERATED THROUGH 300 KTS AT 15,000 FT. THE VIBRATION WAS FELT THROUGH THE YOKE, SEATS, AND COULD EVEN BE HEARD. THE VIBRATION STOPPED AS THE AIRCRAFT SLOWED BELOW 285 KTS. AN EMERGENCY WAS DECLARED WITH ATC AND THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO AN UNEVENTFUL LANDING AT ATL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT FORWARD NOSE LANDING GEAR DOOR LINK DUE TO FAILED TENSION CHECK, ALSO REPLACED THE RIGHT AFT MOVABLE FLAP VANE SLIDER AND ADJUST THE FLAP VANE. (LP #4980902)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,442 hrs · 31,623 cycles

THE EMERGENCY LIGHT IS FLICKERING ON THE L SIDE OF GRATE. IS NOT RELATED TO AIR SWITCH/CONTROLS. *** CONTRACT MAINTENANCE EVENT - OCM: 265651 *** RESET EMERGENCY LIGHT C/B. THE AFT EMERGENCY LIGHTS NOW OPERATES NORMALLY REF B717 AMM 33-51. (LP #2854005)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,442 hrs · 31,623 cycles

THE AFT EXIT DOOR EMERGENCY LIGHT ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY (B5-260) IAW B717 FRM FIM 33-50-00 810-801. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #4397918)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00214: PAN ON FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER ER/A 607572-14 REV ORIGINAL SECTION A, B, AND C AND PRI 607572-14 REV 1, SECTION A, B, AND C. ASSOCIATED ER/A 14-607572 ADDED FOR AC 9551. (LP #2734321)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON INTERCOSTAL STA Y1110 AND STRINGERS R24 AND R25 AFT ACCESSORIES. SUMMARY OF NRC 00318: STRINGERS R25 STA Y=1110 WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #2730639)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

DURING STEP 3 AMDS 2060-1001 CORROSION WAS FOUND ON FWD PASSENGER STAIRWELL DOOR (CPAX). SUMMARY OF NRC 540: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B-717 AMM 52-63-01-020-801 AND AMM 52-63-01-420 -801. (LP #2729492)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

FOUND CORROSION ON FITTING FOR FIXED STRUT AT AFT FACE RH MLG. SUMMARY OF NRC 00489: CORROSION LEVEL 2. FITTING FOR FIXED STRUT AT AFT FACE RH MLG WAS REPAIRED PER PRI 607264-14 REV 0 AND ER/A 607264-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2729276)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH. SUMMARY OF NRC 00043: FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH WAS REPAIRED PER PRI 606978-14 REV.2 AND ER/A 606978-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-606978 ADDED FOR AC 9551. (LP #2727348)

Part: NONE — NONE (NONE) · airframe 48,829 hrs · 34,545 cycles

DTA MONITOR INSPECTION LOG REF ERA 606978-14 PENDING DTE APPROVAL DUE PRIOR TO 11APR25. DISCONTINUE REVENUE SERVICE ON OR BEFORE 11APR25 PENDING DTE APPROVAL FROM ENABLING TECHNOLOGIES. ASSOCIATED ER/A 95-606978 ADDED FOR AC 9551. UPDATED MONITOR TITLE. **REDEFERRED LOG TO QC, ESTAB MON INSP ** ER/A 606978-14 REV A DELETES THIS LOG PAGE. ALL FOLLOW-ON WORK IS ON SECTION II LOG PAGE #0786135. OK TO CLOSE THIS LOG PAGE. TERMINATED LOG PAGE PER ENGINEERING COMMENTS ON LINE 5 AND REMOVED MONITOR INSP PER ALERT 29JAN25 AND LOG COMMENTS. (LP #2727109)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORTS (2EA) BTW STA 148-200, X=7 AND X=-7 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1 ). SUMMARY OF NRC 00356: CORROSION LEVEL 2. FLOOR SUPPORTS (2EA) BTW STA 148-200, X=7 AND X=-7 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WERE REPLACED PER DWG 9936534 AND PER B717-200 SRM 51- 41-01-0G. (LP #2718813)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACKS ON FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE). SUMMARY OF NRC 00373: FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE) WERE REPAIRED PER PRI 607334-14 REV 0 AND ER/A 607334-14 REV O SECTION I. PERMANENT REPAIR. (LP #2719829)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT BTW STA 157-200 FROM X=44. SUMMARY OF NRC 00523: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 157-200 FROM X=44 WAS REPLACED PER B717-200 SRM 51-40-08-0G PAR 3, SRM 51-10-04-0G. PAR 26(C) AND SRM 51-41-05-0G. (LP #2718715)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WAS REPLACE PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #2717059)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT STA Y=179 BTW X=-8 TO X=-40, ALSO ON FLOOR SUPPORT BTW STA Y=157-195 AND X=-44 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00357: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=179 BTW X=-8 TO X=-40, ALSO ON FLOOR SUPPORT BTW STA Y=157-195 AND X=-44 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WERE REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2718341)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44. SUMMARY OF NRC 00524: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #2718337)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=- 8 AND X=-44 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00362: CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2717156)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

IN REF 429: CORROSION OUT LIMITS ON RH CENTER SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT. SUMMARY OF NRC 00516: SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-01-0G. (LP #2716662)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00041: EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2716669)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00042: EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2716523)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 541-560, ALSO BTW STA 598-617 AND BTW STA 617-636, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00390: CORROSION LEVEL 2. CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 541-560, ALSO BTW STA 598-617 AND BTW STA 617-636, X=-57 AT PAX COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2715482)

Part: SKIN — CRACKED (ZONE 200) · airframe 48,829 hrs · 34,545 cycles

FUSELAGE SKIN Y=1037, L13R TO L14R HAS CRACK REPAIR & INSPECTIONS. ACCOMPLISH ER/A 606978-14 REV A SECTION II INSPECTION WITHIN EVERY 15,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. ASSOCIATED ER/A 00-606978 ADDED FOR AC 9551. (LP #0786135)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00365: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 51-41-01-0G. (LP #2711899)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX. SUMMARY OF NRC 00443: FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2708504)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON CUSP WEBS INNER AND UPPER SURFACE (4EA) BTW STA Y=433 AND STA Y=503, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00398: CORROSION LEVEL 2. CUSP WEB BTW STA Y=389 TO Y=503, X=-57 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2708772)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

SEVERAL CORROSION POINTS ON MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00358: CORROSION LEVEL 2. MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2, PAR 4.A FIG 201. (LP #2708422)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

CORROSION ON CUSP WEB BTW STA 927-946 AND ON STA 807 X-57. SUMMARY OF NRC 00522: CORROSION LEVEL 2. CUSP WEB BTW STA 927-946 AND ON STA 807 X-57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2705390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACKS ON PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Y=427 OF AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00212: PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Y=427 OF AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2705807)

Part: UNKNOWN — UNDERTORQUED (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

SECONDARY NRC, HIDDEN DAMAGE: CRACK ON CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00490: CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2703902)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,007 hrs · 31,266 cycles

IN REF NRC 00384: CORROSION ON LH CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57. SUMMARY OF NRC 00521: CORROSION LEVEL 2. CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2704179)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON PAN FWD UPPER SECTION AT L1 PASSENGER DOOR. SUMMARY OF NRC 00051: PAN ON FWD UPPER SECTION AT L1 PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 3, PAR. 4, FIGURE 201. (LP #2698099)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

CRACK ON PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00213: PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R, REPAIR 1, PAR. 6, FIG. 201. (LP #2697134)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

AIRCRAFT 9551, INITIAL INSPECTION: CRACK ON INNER FITTING OF BEAM # 2 IN FWD EDGE AND BEAM # 3 ON FWD EDGE APPROX BTW STA Y=954 AND STA Y=964 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER FITTING OF BEAM # 2 IN FWD EDGE AFT CARGO COMPARTMENT DOOR WAS REPLACED PER B-717/200 SRM 51-41-05- 0G AND SRM 51-41-01-0G AND (ET) HFEC INSPECTION WAS ACCOMPLISHED ON BEAM # 3 ON FWD EDGE APPROX BTW STA Y=954 AND STA Y=964 AT AFT CARGO COMPARTMENT DOOR. NO CRACKS WERE FOUND. (LP 2693739)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

AIRCRAFT 9551, INITIAL INSPECTION: CRACK ON BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR (L1). CORRECTIVE ACTION: BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP 2683386)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,007 hrs · 31,266 cycles

AIRCRAFT 9551, INITIAL INSPECTION: CRACK ON UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR (L1). CORRECTIVE ACTION: UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 2682859)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,996 hrs · 31,260 cycles

MAINTENANCE NOTED THAT THE OVERHEAD EMERGENCY EXIT LIGHT (INTERIOR) AT THE OVERWING EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, B5-120, PER B717 AMM 33-51.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,102 hrs · 29,609 cycles

THE EMERGENCY LIGHTS IN THE FIRST CLASS SECTION ARE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY PER B-717 AMM 33-51. ALL EEPL CHECK GOOD NOW. (LP #6630556)

Part: FRAME — CRACKED (BS 674) · airframe 42,887 hrs · 29,439 cycles

RH OVERWING EXIT FRAME STA 674 CRACKED AT UPPER RADIUS OF FRAME TAB. CRACK IS CONDITION 3 (GREATER THAN 0.125 INCHES). NRC 025-0004:5310-01439-01D/001 00052: C/W AMDS WORK CARD 54310-01436-03B. (LP #1334164)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 45,004 hrs · 31,265 cycles

ERA 564482-14AD REVISED TO REV 'A'. SECTION I ORIGINALLY ISSUED FOR DAMAGE TO V STAB FRONT SPAR CAP SKIN. DAMAGE TOLERANCE EVALUATION COMPLETE. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION PRIOR TO 5100 FLIGHT CYCLES FROM SECTION I ACCOMPLISHMENT (17JAN18) AND EVERY 4100 CYCLES THEREAFTER. ASSOCIATED AA 5530-01048 ADDED FOR AC 9551. ASSOCIATED ER/A 00-564482 ADDED FOR ACFT. ERA REVISED TO REV 'B'. SECTION II LANGUAGE CLARIFIED. NO CHANGE TO SCHEDULING OR ADDITIONAL WORKSTEPS INCLUDED. COMPLIED WITH SECTION 2 STEP 1 IAW ERA 564482-14AD REV B. COMPLIED WITH SECTION 2 STEP 2&3. REF ERA 564482-14AD REV B NO DEFECTS NOTED QC 4003.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,701 hrs · 28,556 cycles

THE EMERGENCY LIGHTS L2-786, L2-771, AND L2-772 ARE INOPERATIVE. MAINTENANCE FOUND THE GROUNDS 5238D AND 5239D TO BE LOOSE. THE GROUNDS WERE RE-INSTALLED PER WDM 33-51-12 AND ALL CHECKS WERE GOOD. (LP #5691118)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,701 hrs · 28,556 cycles

THE RIGHT & LEFT AFT OVERWING EMERGENCY EXIT IDENTIFIERS L2-837, L2-836 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THAT THERE WAS NOT ANY POWER AT PIN 9 ON THE POWER SUPPLY B5-119. THE POWER SUPPLY WAS REPLACED PER AMM 33-51-03 400-802. CHECK WAS GOOD. (LP #5691119)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 45,004 hrs · 31,265 cycles

VERTICAL STAB LE INDICATES CRACKING AT 4EA HOLES OF DOUBLER REPAIR STRAP. COMPLIED WITH ERA 564482-14AD REV ORIG.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 45,004 hrs · 31,265 cycles

DURING INSPECTIONS PER WORKCARD 5530-01048-01 & AD 2016-09-05, MTC FOUND A CRACK INDICATION COMMON TO THE VERTICAL SPLICE BETWEEN LOWER DORSAL ASSEMBLY SKIN & FRONT SPAR FORWARD CAP ON LT OF STAB. WORKCARD DOES NOT GIVE INSTRUCTIONS IF A CRACK IND IS FOUND. ER/A ASSOCIATED WITH LOG PAGE AUTHORIZES MTC TO REPAIR THE CRACK. BOEING HAS GIVEN SPECIFIC APPROVAL TO FLY FOR 24 MONTHS UNTIL A DAMAGE TOLERANCE EVALUATION CAN BE ACCOMPLISHED. THIS TIME RESTRICTIONS IS AD RELATED AND CANNOT BE DEVIATED FROM. CHANGED FROM 00-564482 TO 14-564482, REVISED TO REV 'A'.

Part: LONGERON — DAMAGED (BS 1110) · airframe 39,723 hrs · 27,185 cycles

LONGERON 23R, BS 1110 WAS DAMAGED. CUT OUT DAMAGED SECTION OF THE LONGERON AND REPAIRED IAW SRM 53-00-05, REPAIR 2.

Part: LONGERON — DAMAGED (BS 1110) · airframe 39,723 hrs · 27,185 cycles

LONGERON 24R, BS 1110 WAS DAMAGED. CUT OUT THE DAMAGED SECTION AND REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 2.

Part: DOUBLER — DAMAGED (BS 1116) · airframe 39,723 hrs · 27,185 cycles

THE FUSELAGE SKIN BUTTSPLICE DOUBLER WAS DAMAGED AT BS 1116 BETWEEN LONGERONS 24R AND 23R. REMOVED, FABRICATED, AND INSTALLED A NEW BUTTSPLICE DOUBLER IAW SRM 51-40-02, AND DWG 5911429, REV DZ.

Part: FRAME — DAMAGED (BS 1116) · airframe 39,723 hrs · 27,185 cycles

FRAME BS 1116, BETWEEN LONGERONS 23R AND 24R WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-40-02, AND DWG 9915559, REV AB.

Part: SKIN — DAMAGED (BS 1110) · airframe 39,723 hrs · 27,185 cycles

FUSELAGE SKIN AT BS 1110, LONGERON 24R WAS DAMAGED. REPAIRED THE SKIN IAW ER/A 569013-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 1116-1140) · airframe 39,723 hrs · 27,185 cycles

FUSELAGE SKIN DAMAGED BETWEEN BS 1116 - 1140, LONGERON 23R - 25R. REPAIRED THE SKIN IAW ER/A 569014-14, REV ORIGINAL.

Part: FRAME — DAMAGED (BS 1116) · airframe 39,723 hrs · 27,185 cycles

FRAME BS 1116, LONGERON 24R WAS DAMAGED. REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND DWG 5913596, REV AN.

Part: SKIN — CORRODED (LT WING) · airframe 38,274 hrs · 26,220 cycles

DURING A C CHECK, FOUND CORROSION THE LT WING UPPER SKIN. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01 ALLOWABLE DAMAGE 1. THE CORROSION WAS BLENDED IAW SRM 51-10-02 AND PERFORMED A UT THICKNESS INSPECTION IAW NDT SPM 04-00-00. THE SKIN WAS REPLACED IAW PRI 564505-14 REV O.

Part: ANGLE — CORRODED · airframe 38,274 hrs · 26,220 cycles

AN ANGLE IS CORRODED AT C2 BB LOWER DOOR CUT OUT, FWD SIDE TO AFT OF MIDDLE FITTING. REPAIRED IAW SRM 53-20-15, REPAIR 7.

Part: LENS — CRACKED (EXIT SIGN) · airframe 35,468 hrs · 24,142 cycles

THE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS CRACKED. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 34,757 hrs · 23,635 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE CENTER SECTION OF THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND THE WIRE HARNESS DISCONNECTED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,437 hrs · 22,593 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE CEILING BETWEEN ROWS 1-16 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT ROW 10 AND THE OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CRACKED (VERICAL STAB) · airframe 33,190 hrs · 22,440 cycles

LEFT BS 1155, EMPENNAGE SKIN CRACKED AT SHEAR TIE FASTENER BETWEEN STR 2L & 3L. REPAIRED SKIN CRACK AT STR 2L AND NR LT SHEAR TIE AT LT F/S 1155 IAW ER/A 541025-14 INSTRUCTIONS 1-11.

Part: SKIN — CRACKED (BS 1155) · airframe 33,190 hrs · 22,440 cycles

EMPENNAGE SKIN CRACKED AT SHEAR TIE FASTENER BETWEEN STR 2R & 3R. REPAIRED SKIN AT STRINGERS 2 - 3R BS 1155 IAW ER/A 541025-14, INSTRUCTIONS 1-11.

Part: PAN — CHAFED (SERVICE DOOR) · airframe 33,190 hrs · 22,440 cycles

SERVICE DOOR LOWER PAN IS CHAFED. R & R SERVICE DOOR LOWER PAN IAW SRM 51-41-02, PARA 4 & 51-41-05, PARA 8.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

CORROSION ON UPPER SURFACE OF SUBFLOOR, UNDER FWD CABIN FLOOR PANEL 221MF. BLENDED CORROSION REMOVE .010 MATERIAL ORGINAL THICKNESS .020 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. FABRICATED NEW CUSP IAW DWG 9936535 INSTALLED IAW SRM 51-41-02, PG 1 PARA4, 51-41-05, PG 1 PARA 2 AND 51-41-08 P91 PARA 4, JOB COMPLETE.

Part: LONGERON SPLICE — CORRODED · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

30 LONGERON SPLICE AND SHIMS ARE CORRODED, M PARTS LOCATED ON REPAIR RACK. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105, FIG 103. BLENDED SHIMS AND FOUND TO BE OUT OF LIMITS IAW SRM PG 105, FIG 103, FABRICATED SHIMS IAW SRM 53-20-05, PG 204, FIG 201. ALODINED PARTS IAW SRM 51-10-04, PG 24, PARA 21. PRIMED SHIMS IAW SRM 51-10-04, PG 16, PARA 12A. APPLIED TOP COAT IAW PSM 900-03-06, NR 3 REMAINING "T" WAS 0.132. JOB COMPLETED SB-28, NR 62627-0100-171.

Part: ANCHOR — CRACKED · airframe 33,190 hrs · 22,440 cycles

FLOOR ANCHOR IS CRACKED & CORRODED IN THE CORNER RADIUS, ON REPAIR RACK. REPLACED CRACKED AND CORRODED ALC FLOOR ANCHOR, INTERCOSTAL, IAW SRM 51-41-02 AND 51-41-05 JOB COMPLETE.

Part: CUSP WEB — CRACKED (BS 674) · airframe 33,190 hrs · 22,440 cycles

CUSP MEMBRANE CRACKED BS 674 AT LT OTBD SEAT TRACK FWD OF SEAT TRACK ATTACH POINT, BELOW FLOOR. REPAIRED CRACKED CUSP MEMBRANE AT BS 674 IAW SRM 53-00-55, REPAIR 4.

Part: DOOR SILL — CORRODED (BS 339) · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

FWD LOWER CARGO DOOR CUTOUT LOWER SILL AREA HAS CORROSION AROUND SEVERAL FASTENERS ALONG ENTIRE LENGTH OF CUTOUT. REPAIRED IAW SRM 53-20-15, FIG 201, SHT 4-6.

Part: STRUCTURE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

CORROSION IN POCKET JUST AFT OF R-1 SERVICE DOOR LOWER AFT CORNER. BLENDED CORROSION NOMINAL .071 REMAINING .090 FOUND TO BE OF LIMITS IAW SRM 53-00-00, FIG 103, PG 105. REPLACED UPPER CUSP IAW SRM 51-41-05, PARA 8, JOB COMPLETE.

Part: FRAME — CRACKED (BS 715) · airframe 33,190 hrs · 22,440 cycles

RIGHT OVERWING FRAME AT BS 715.000 CRACKED BELOW FLOOR FROM TAB INTO POCKET. CONDITION 3, CRACK GREATER THAN 0.125, REF: CARD 5310-01436-01C, FIG 2, SH 1 FOR LOCATION. RIGHT OVERWING FRAME AT BS Y=715.000 WAS REPLACED ON JOB CARD 5310-01436-03B.

Part: FRAME — CORRODED (BS 1037) · airframe 33,190 hrs · 22,440 cycles

FRAME CORRODED AT STRINGER 30. REPAIRED FRAME AT BS 1037, STR 30 IAW SRM 53-20-07, REPAIR 3.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 33,190 hrs · 22,440 cycles

VERTICAL STABILIZER HAS NUMEROUS WORKING/SMOKING FASTENERS IN THE L/E. REPAIRED VERTICAL STABILIZER BY REMOVING DAMAGED AREA IAW SRM 55-30-01, REPAIR 7. FABRICATED REPAIR PART AND INSTALLED REPAIR PARTS IAW SRM 55-30-01, REPAIR 7.

Part: STRINGER — CORRODED (BS 954) · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

STRINGER 30R AND FRAME AT BS 954 CORRODED. STRINGER 30 REPLACED FROM BS 935 - 1012 IAW SRM 53-20-05, REPAIR NR 1.

Part: STRINGER — CORRODED (BS 908-927) · corrosion level 2 · airframe 33,190 hrs · 22,440 cycles

STR 30 CORROSION IN BETWEEN BS 908 - 927. REPLACED THE STR IAW SRM 51-40-02, PAGES 1 THRU 4 AND 51-40-05, PAGES 1 THRU 5.

Part: WINDOW FRAME — CRACKED (BS 795) · airframe 33,190 hrs · 22,440 cycles

LEFT CABIN WINDOW INTERNAL FRAME AT APPROXIMATELY BS 795 HAS A CRACK APPROXIMATELY .1250" LONG ON THE FWD LOWER CORNER. VERIFIED CRACK AND MARKED END OF CRACK USING HFEC WITH MODEL NORTEC 500D, TAG 6782, SN N500D000D030. REPAIRED LT CABIN WINDOW INTERNAL FRAME AT APPROXIMATELY BS 795 ON FWD LOWER CORNER IAW SRM 56-20-02, REPAIR 1, TYPE B, FIGURE 202.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 33,190 hrs · 22,440 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L WAS DAMAGED, NOT SPECIFIED. THE DOOR SLIDE WAS REPLACED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,980 hrs · 22,305 cycles

TWO BULBS INOPERATIVE IN AFT EMERGENCY EXIT IDENTIFIER LIGHT. REPLACED THE BULBS IAW AMM 33-51.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 32,454 hrs · 21,878 cycles

RAMP CREW REPORTED A TEAR ON THE L/E OF THE FWD CARGO DOOR. DAMAGE IS 2", TEAR 20" FROM LOWER THRESHOLD RT SIDE. REPAIRED IAW SRM 53-20-15, REPAIR 11. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 2,079 hrs · 1,845 cycles

THE SUBJECT FLIGHT SPOILER IS TYPICALLY FOUND WITH DISBONDS & DELAMINATION’S ALONG THE UPPER & LOWER SURFACES. THE UPPER & LOWER SKINS ARE ORIGINALLY MANUFACTURED FROM 0.032” 2024-T81CLAD SHEET & THE UNDERLYING DOUBLERS ARE MANUFACTURED FROM 0.020” 2024-T81 CLAD SHEET. SRM 51-70-02 DOES NOT PROVIDE REPAIR INSTRUCTIONS FOR FULL REPLACEMENT OF THE SKINS & DOUBLERS.

Part: SEAT TRACK — DAMAGED (BS 312) · airframe 31,238 hrs · 20,881 cycles

ONE FASTENER MISSING AT BS 312 RBL 54 SEAT TRACK. REPAIRED IAW ER/A 95-531456-14.

Part: COVER — OUT OF POSITION (TAILCONE SLIDE) · airframe 29,127 hrs · 19,010 cycles

DURING CONFORMITY INSPECTION, THE TAIL CONE SLIDE PRESSURE INDICATOR WAS NOTED TO BE UNREADABLE. MAINTENANCE ADJUSTED THE COVER TO ENABLE PROPER READING.

Part: SIGN — CRACKED (CABIN) · airframe 29,125 hrs · 19,007 cycles

CEILING EMERGENCY EXIT SIGN AT ROW 1 CRACKED. R & R SIGN IAW AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 28,958 hrs · 18,899 cycles

MAIN CABIN FLOOR PANEL 2224F METAL COVERS DAMAGED. R & R PANEL IAW SRM & DRAWING.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 28,958 hrs · 18,899 cycles

MAIN CABIN FLOOR PANEL 222ADF METAL COVERS DAMAGED. R & R PANEL IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 28,958 hrs · 18,899 cycles

RT WING INBD BUTTE DOOR LOWER SKIN INBD END CRACKED. R & R SKIN IAW SRM & DRAWING.

Part: HINGE — CRACKED (RT WING) · airframe 28,958 hrs · 18,899 cycles

RT WING CENTER BUTTE DOOR INBD SIDE OF HINGE CRACKED. R & R HINGE IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 28,958 hrs · 18,899 cycles

RT WW FWD BULKHEAD OTBD SIDE HYD LINES SUPPORT CLAMP CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 28,958 hrs · 18,899 cycles

LT WW FWD DOOR CUTOUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 28,958 hrs · 18,899 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2R. R & R LONGERON IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 28,958 hrs · 18,899 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2L. R & R LONGERON IAW SRM.

Part: PIN — MISSING (EVAC SLIDE) · airframe 26,442 hrs · 17,352 cycles

L1 DOOR SLIDE PACK MISSING PIN. REMOVED AND REPLACED L1 DOOR EMERGENCY SLIDE PER M/M.

Part: STRUT — CRACKED (RT MLG) · airframe 24,718 hrs · 16,201 cycles

RT MLG STRUT CYLINDER CRACKED .961 INCHES ABOVE BASE. REMOVED AND REPLACED RT MLG ASSY PER MM.

Part: LOCK — LOOSE (GIRT BAR) · airframe 24,326 hrs · 15,949 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT)

OVERHEAD LIGHTED EMERGENCY EXIT SIGN COVER AT ROW 1 MISSING. INSTALLED SIGN COVER AT ROW 1.

Part: STRAP — CORRODED (FUSELAGE)

AFT CARGO UPPER FRAME STRAP, STA 1002, RBL 10, CORROSION. ACCOMPLISHED UPPER FRAME STRAP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 24546.

Part: COVER — CORRODED (CABIN)

RT SIDEWALL LOWER GRILL, CORROSION. OPEN DEFECT. SEE NR 24597.

Part: FRAME — CHAFED (LT COWLING)

LT ENGINE LOWER COWL FRAME, CHAFED. OPEN DEFECT. SEE NR 24565.

Part: FLOOR PANEL — CORRODED (COCKPIT)

FLIGHT COMPARTMENT FLOOR PANEL 211 AMF, CORROSION. ACCOMPLISHED FLOOR PANEL 211 AMF REPLACEMENT PER B717 SRM 51-40-08, 51-10-04.

Part: SHEAR WEB — PUNCTURED (FUSELAGE)

FLIGHT COMPARTMENT SHEAR WEB, STA 120, RBL12, PUNCTURED. OPEN DEFECT.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK FLANGE, STA 237 RBL22, CORROSION. ACCOMPLISHED SEAT TRACK FLANGE REPLACEMENT PER B717 SRM 53-20-52 AND 51-10-04. SEE NR 24574.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT ANGLE, STA 200, RBL 27, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 53-10-51.

Part: SKIN — CORRODED (FUSELAGE)

RIGHT LOWER FUSELAGE EXTERIOR SKIN, STA 884, LONG 27R, RBL 21, CORROSION. ACCOMPLISHED FUSELAGE EXTERIOR SKIN DOUBLER REPAIR PER B717 SRM 53-20-70.

Part: INTERCOSTAL — CRACKED (L1 DOOR)

L1 DOOR INTERIOR INTERCOSTAL FORMER, CRACKED. OPEN DEFECT. SEE NR 24594.

Part: PAN — CORRODED (FUSELAGE)

CABIN PAN BETWEEN FALSE TRACKS, STA 190, CORROSION. ACCOMPLISHED PAN BETWEEN FALSE TRACKS, FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10, REP 2.

Part: PAN — CORRODED (FUSELAGE)

PAN BETWEEN FALSE TRACKS, STA 173, CORROSION. ACCOMPLISHED PAN BETWEEN FALSE TRACKS FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10, REP 2.

Part: PAN — CRACKED (CARGO DOOR)

C2 DOOR PAN, CRACKED. ACCOMPLISHED DOOR PAN DOUBLER AND FILLER REPAIR PER B717 SRM 52-00-00, 52-30-02 AND 51-10-04. SEE NR 24487.

Part: PAN — CORRODED (FUSELAGE)

R1 DOOR FLOOR PAN, CORROSION. ACCOMPLISHED FLOOR PAN DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 REP 2, FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

L1 DOOR FLOOR SUPPORT, STA 180, LBL44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 53-10-51, 51-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 195, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-10-51, 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

L1 DOOR FLOOR SUPPORT, LBL54, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-10-51, 51-41-02.

Part: DUMMY RAIL — CORRODED (FUSELAGE)

CABIN RT FALSE TRACK, STA 160, RBL7, CORROSION. ACCOMPLISHED RT FALSE TRACK REPLACEMENT PER B717 SRM 51-41-01.

Part: DUMMY RAIL — CORRODED (FUSELAGE)

CABIN LT FALSE TRACK, STA 160, CORROSION. ACCOMPLISHED LT FALSE TRACK REPLACEMENT PER B717 SRM 51-41-01.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO LOWER JAMB, STA 954 TO 994, CORROSION. ACCOMPLISHED LOWER JAMB REPLACEMENT PER B717 SRM 53-20-15.

Part: SIGN — MISSING (CABIN)

FIRST CLASS CABIN EMERGENCY EXIT SIGN MISSING. REPLACED LENS ASSY PER B717 AMM 33-51. OK FOR SERVICE.

Part: CYLINDER — DEFECTIVE (L1 DOOR)

L1 DOOR WILL NOT STAY SECURED IN GUST LOCK COME OUT W/OUT USING HANDLE. REMOVED AND REPLACED DOOR CYLINDER ON L1 DOOR AND ADJUSTED L1 FWD DOOR HOLD OPEN HOOK OPS CHECK GOOD REF 52-11-04.

Part: COALESCER BAG — DIRTY (AC BAY)

BLUISH HAZE IN CABIN NOTICEABLE BEFORE CABIN DOOR CLOSED; MORE PRONOUNCED AFTER CABIN DOOR CLOSED. REMOVED AND REPLACED BOTH COALESCER BAGS AND LEAK CHECKED; REF MM 21-54. INSPECTED CABIN, NO SMOKE SMELL FOUND. CHECKED C/B'S, CARGO AND APU COMPARTMENTS; PERFORMED 'BURNOUT' PROCEDURE, NO UNUSUAL SMELL NOTED REF MM 21-54.

Part: FRAME — DAMAGED (FUSELAGE)

AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2973.

Part: FRAME — DAMAGED (FUSELAGE)

AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 1. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2984.

Part: SLIDE — UNSERVICEABLE (R2 DOOR)

FORWARD SERVICE DOOR SLIDE PACK PRESSURE GAUGE IN RED. REMOVED AND REPLACED FORWARD SLIDE PACK REF AMM 25-61.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR)

R1 DOOR SLIDE INADVERTENTLY DEPLOYED BY A/C CLEANERS. INSTALLED NEW FORWARD SERVICE DOOR SLIDE PER B717 AMM 25-61-03.

Part: CONNECTOR — MALFUNCTIONED (CABIN)

FWD F/A SEAT & L1 EMERGENCY LIGHTS REMAIN ILLUMINATED WITH O/H & FWD F/A PANEL SWITCHES IN OFF POSITION. RESET CONNECTOR AT EMERGENCY LIGHT BATTERY PACK AT STA 121 IN CTR DRP DOWN CEILING. LIGHTS EXTINGUISHED AND COMPLETE EMERGENCY IS FULLY FUNCTIONAL.

Part: GUIDE — DEFECTIVE (R1 DOOR)

R-1 GALLEY DOOR CANNOT BE OPENED FROM INSIDE GALLEY. TRIMMED EDGE OF R-1 DOOR OUTER HANDLE DEFLECTOR GUIDE.

Part: COALESCER BAG — DIRTY (A/C BAY)

ELECTRIC ODOR DETECTED IN FORWARD GALLEY. ON FIRST ENTRY INTO AIRCRAFT, MORE OF A HEAT SMELL THAN AN ELECTRICAL SMELL. T/S REF FIM 21-22. NO ODORS NOTED, ALSO INSPECTED XM STATIONS, COFFEE MAKERS, ENGINE AND APU AREAS FOR LEAKS. NO DEFECTS NOTES. REPLACED COALESCER BAGS REF 21-54.

Part: BATTERY — OVERHEATED (EMERGENCY LIGHT)

EXTERNAL EMERGENCY LIGHTS ALWAYS ON WHEN SYSTEM OFF. REPLACED BATTERY ASSY B5-125 & OPS GOOD PER AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

LOWER WALKWAY TAIL CONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AT PER AMM 24-00. OPS CHECK NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE)

RIGHT HAND VENT BOX CRACKED. INSTALLED DOUBLER REPAIR AT RIGHT HAND VENT BOX IAW AIRTRAN T/C 17-5320-2023.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

ROWS 1 - 10 AND L1 AND R1 EXIT SIGNS INOPERATIVE. SWAPPED BATTERIES, NO HELP. REMOVED AND REPLACED POWER SUPPLY, CORRECTED PROBLEM. ALL LIGHTS WORK PROPERLY.