N946AT

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 65,422 hrs · 47,055 cycles

SHIP 9506 CRACK WAS FOUND ON HOLE 6 HRS AT STA ZFS=51.267 APROX. FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE. CORRECTIVE ACTION: REPAIR ON FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE WAS PERFORMED PER PRI 606161-14 (1254228)

Part: SKIN — DAMAGED (ZONE 300) · airframe 65,422 hrs · 47,055 cycles

FASTENERS (45 EA) ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR STA ZFS =52. CORRECTIVE ACTION: VERTICAL STAB LEADING EDGE REPAIR STA ZFS =52 WERE REMOVE AND INSTALL PER CARD 5530-01048-02 AND DVI WAS PERFORMED ON RH/LH VERTICAL STAB LEADING EDGE STRUCTURE SPLICE STA ZFS =52.267 (1249936)

Part: SERVICE PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,422 hrs · 47,055 cycles

SHIP 9506 CORROSION ON LOWER AREA OF LAVATORY SERVICE PANEL BTW TRAY-PANEL AND PREVIOUS REAPAIR INTERNAL FILLER. CORRECTIVE ACTION: REPAIRED PER ER/A 542102- 14 REV. (1245325)

Part: VANE — DENTED (ZONE 500 FLAP) · airframe 65,420 hrs · 47,054 cycles

DISBOND OF 2.300IN X 3.100IN. ON DENT LOCATED AT LH AFT MOVABLE FLAP VANE, LOWER SURFACE. REPAIRED PER B717-200 SRM 57-53-01-2R (1239681)

Part: NONE — NONE (NONE) · airframe 65,420 hrs · 47,054 cycles

DTA ER/A 542233-14 REV D REPAIR MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-OCT-25. C/W ER/A 542233-14. (1245089)

Part: TRANSFER VALVE — FAILED (ZONE 700) · airframe 64,129 hrs · 45,825 cycles

SHIP 9506-ATB- THE FLIGHT CREW PERFORMED AN AIR TURN BACK DUE TO A RIGHT HYDRAULIC SYSTEM FAILURE. AN EMERGENCY WAS DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDING GEAR DOORS CONTACTING THE RUNWAY UPON ROLLOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR TRANSFER VALVE AND DEFERRED BOTH DOOR BUMPERS TO MONITOR FOR BUMPER REPLACEMENTS. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #7108608)

Part: UNKNOWN — NOT REPORTED (UNKNOWN) · airframe 63,649 hrs · 45,417 cycles

-AD- MONITOR LOG REQUIRES PERMANENT REPAIR INSTRUCTIONS FOR ER/A 542233-14AD SECTION IV PRIOR TO 30-NOV-2025. CONTACT LIAISON ENGINEERING, DEP 555, FOR INSTRUCTIONS. DISCONTINUE REVENUE SERVICE ON OR PRIOR TO 30-NOV-25. PERMANENT REPAIR REQUIRED PER ERA 542233-14AD. ASSOCIATED ER/A 00-542233 ADDED FOR AC 9506. **REDEFERRED LOG TO QC, ESTAB MON INSP **. (LP #0692109)

Part: BULKHEAD — ABNORMAL (REAR CANTED BULK) · airframe 63,598 hrs · 45,372 cycles

-AD- ACCOMPLISH ER/A 542233-14AD REV B SEC II. ACCOMPLISH ER/A 542233-14AD REV B SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-542233 ADDED FOR AC 9506. ACCOMPLISHED ERA 542233-14AD REV B SECTION II ALTERNATIVE INSPECTION FOR AD 2024-20-02. NO FURTHER DEFECTS NOTED. OK TO CLOSE LOG-PAGE. MONITOR INSPECTION REMOVED. (LP #0658380)

Part: SPLICE — CRACKED (ZONE 300) · airframe 62,896 hrs · 44,755 cycles

-AD- FOUND 2 CRACK INDICATIONS ON LEFT SIDE OF VERTICAL STAB BELOW SPLICE AT STA 2F552.267 WHILE PERFORMING BHEC PER AA 5530-01048 STEP 8 REF AD2018-10-08. HOLES ARE MARKED. AFTER SEPARATION OF LAYERS CONFRIMED CRACK INDICATIONS FROM FWD FLANGE LAYER REF AA5530-01048 AND AD2018-10-08. COMPLIED WITH CRACK VERIFICATION PER STEP 16 OF AA5530-01048 AND AD2018-10-08. NO CRACK FOUND (QC1428). (LP #5583789)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,979 hrs · 43,184 cycles

INSPECTOR FOUND THE HALF HINGE INSTALLED WRONG ON THE TAIL EMERGENCY SLIDE COVER. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00212: HALF HINGE ON TAIL EMERGENCY SLIDE COVER WAS INSTALLED CORRECTLY PER B717-200 AMM 25-61-02 400-801 STEP D (1) (D) TO (F). (LP #0024577)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,977 hrs · 43,183 cycles

SEVERAL DENTS ON LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING. SUMMARY OF NRC 00033: LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE TO B717-200 SRM 57-53-01-2R PROCEDURE 1 PAR 4 AND ADJUST WAS ATTENDED UNDER NRC 00066. (LP #0020645)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,977 hrs · 43,183 cycles

CRACK ON PAN IN BEAM 2 AND ON PAN BTW BEAM 7 TO 8 ON AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00095: PAN IN BEAM 2 AND PAN BTW BEAM 7 TO 8 AT AFT SIDE OF PASSENGER DOOR L1 WERE REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0018804)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,977 hrs · 43,183 cycles

CRACK ON BEAM 6 AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00094: BEAM 6 AFT SIDE OF PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 12. (LP #0016617)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,977 hrs · 43,183 cycles

CORROSION ON AFT PRESSURE BULKHEAD FWD FACE LOWER AREA BTW LONG PROJECTION 28L TO 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. AFT PRESSURE BULKHEAD FWD FACE LOWER AREA BTW LONG PROJECTION 28L TO 28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-08-2R REPAIR 7. (LP #0016850)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,977 hrs · 43,183 cycles

CORROSION ON INTERCOSTAL BTW STA Y=927-946 ON LONGERON 29R. ALSO CORROSION ON INTERCOSTAL BTW STA 1022 TO 1037 AND LONGERON 30 AT AFT CARGO. SUMMARY OF NRC 00111: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=927-946 ON LONGERON 29 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. INTERCOSTAL BTW STA 1022 TO 1037 AND LONGERON 30 AT AFT CARGO WAS CLEANED PER DAL P.S. 900 1-2-2 NO. 02 AND GENERAL VISUAL INSPECTION WAS PERFORMED PER B717-200 SRM 51-00-06-0G PROCEDURE GENERAL STEP 5 A (2) (B) AND NO DISCREPANCY WAS FOUND. (LP #0017256)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,977 hrs · 43,183 cycles

HIDDEN CRACK ON FRAME WEB RH, AND ENLOGATED HOLES BTW LONGERON 27 RH TO LONGERON 28 RH, FROM STA 1053 (AFT CARGO). SUMMARY OF NRC 00184: CRACK AND ELOGATED HOLES ON FRAME WEB RH BTW LONGERON 27 RH TO LONGERON 28 RH FROM STA 1053 WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0016055)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,977 hrs · 43,183 cycles

CORROSION ON LONGERON 30 BTW FRAME STA 908 AND 1022.901 INCLUDING SPLICE (1 EA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00109: CORROSION LEVEL 2. LONGERON 30 BTW FRAME STA 908 AND 1022.901 INCLUDING SPLICE (1 EA) AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0015678)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 60,977 hrs · 43,183 cycles

CORROSION ON FWD REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: FWD PREVIOUS REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND SRM 53-20-15-0G PROCEDURE REPAIR 7. (LP #0013350)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,188 hrs · 42,503 cycles

THE EMERGENCY EXIT SIGN AT THE AFT CABIN BULKHEAD DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE BF-260 BATTERY PACK PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4742276)

Part: NONE — NONE · airframe 59,657 hrs · 42,021 cycles

FOUND DAMAGE AFT CARGO DOOR OPENING. AFT SIDE SEAL RETAINER SPLICE ANGLE CRACKED NEAR TEFLON GUIDE. REMOVED AFT DEPRESSOR SPLICE PER B717 SRM 53-20-15-2R-10. REPAIRED JAMB SEAL DEPRESSOR PER B717 SRM 53-20-15-2R-4. OK FOR SERVICE. (LP #9493774)

Part: NONE — NONE · airframe 59,644 hrs · 42,009 cycles

THE R1 DOOR EMERGENCY INDENTIFIER SIGN LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9493766)

Part: NONE — NONE · airframe 59,644 hrs · 42,009 cycles

FOUND 2 HOLES WITH CRACK INDICATIONS ON LH VERT STAB FRONT SPAR CAP FWD FLANGE, REF AA 5530-01048 AND AD 2018-10-08. REMOVED LH FASTENERS FROM VERT LEADING EDGE. REMOVED VERT LEADING EDGE PER B717 AMM 55-32-01. C/W BHEC OF SEPERATED LAYERS, FOUND CRACK INDICATIONS IN SKIN ONLY REF AA 5530-01048 AND AD 2018-10-08 (QC 1428). STEPPED UP 2 HOLES ON L/H LEADING EDGE SKIN HOLE #5 & #6 FROM ZFS 52.267. HOLE #5 STEPPED UP TO .311' AND HOLE #6 STEPPED UP TO .25". C/W BHEL OF 2 EA HOLES CONFIRMED NO CRACKS AFTER OVERSIZING REF AA5520-01048 AND AD 2018-10-08(QC1428). INSTALLED RH ANTENNAS FOR VOR/ILS IAW B717 AMM 34-32-03. INSTALLED LH LOWER ANTENNA PER B717 AMM 34-32-03. INSTALLED LH UPPER VOR ANTENNA IAW PER B717 AMM 34-32-03. RTS AND OP CHECK OF ALL ANTENNAS WAS GOOD. REF BUFF NR 001 LH VERT STAB FRONT SPAR CAP FWD FLANGE REPAIRED PER ERA 606161-14 REV ORIG PRI 606161-14 REV ORIG. PRI 606161-14 REVS 0-6 MATCH FINAL ERA. ASSOCIATED ER/A 14-606161 ADDED FOR AC 9506. (LP #9493752)

Part: SKIN — DAMAGED (ZONE 300) · airframe 63,663 hrs · 45,430 cycles

-AD- AMOC 606161-14AD - B717-200 VERTICAL STABILIZER LEADING EDGE SKIN ZFS 52.267 OVERSIZE HOLES. REPAIR APPROVAL IS LIMITED TO TWENTY-FOUR (24) MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. ASSOCIATED ER/A 14-606161 ADDED FOR AC 9506. **REDEFERRED LOG TO QC, ESTAB MON INSP**. PER ER/A 606161-14AD REV A, DTE STAGE 2 AND 3 ACCOMPLISHED. ER/A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED AND ARE TRACKED ON NEW LOG PAGE #0703672. PLEASE CLOSE THIS LOG PAGE, #2644140. TERMINATED LOG PER LINE 5 COMMENTS. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 11DEC24 AND LOG COMMENTS. (LP #2644140)

Part: NONE — NONE · airframe 58,779 hrs · 41,241 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS FOR ROWS 1-10, TO BE INOPERATIVE. THE BATTERY PACK B5-227 WAS REPLACED AND THE EMERGENCY LIGHTS RETURNED TO AN OPERATIONAL STATUS. (LP #9128785)

Part: NONE — NONE · airframe 58,251 hrs · 40,729 cycles

ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY BATTERY PACK 135-119 WERE INOPERATIVE. REPLACED 135-119 AND APPLICABLE POWER SUPPY PER B717 AMM 33-51. (LP #8829612)

Part: NONE — NONE · airframe 58,251 hrs · 40,729 cycles

ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY B5-231 WERE INOPERATIVE. REPLACED B5-231 AND APPLICABLE POWER SUPPY PER B717 AMM 33-51. (LP #8829616)

Part: BATTERY PACK — INOPERATIVE · airframe 58,024 hrs · 40,528 cycles

THE EMERGENCY EXIT SIGN FOR THE OVER WING EXIT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME REF B717 AMM 33-51. (LP #8804889)

Part: BATTERY PACK — INOPERATIVE · airframe 58,024 hrs · 40,528 cycles

THE FIRST CLASS EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME REF B717 AMM 33-51. (LP #8804888)

Part: SIGN — MISSING · airframe 57,742 hrs · 40,297 cycles

SERVICE CHECK FOUND THAT THE EXIT SIGN IS MISSING AT 1R DOOR. MAINTENANCE REPLACED THE EXIT SIGN AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP #8758656)

Part: NONE — NONE · airframe 57,154 hrs · 39,794 cycles

**THIS LOG REPLACES LOG 2010626.** DENTS LEFT UPPER FLAP MOVEABLE VANE. SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSP CONDITION EVERY "C" CHECK PER TOPP 30-10-70. (LP #2060077)

Part: VANE — DENTED (LT TE FLAP) · airframe 62,073 hrs · 44,059 cycles

DENTS LEFT UPPER FLAP MOVEABLE VANE (AI). SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30- 10-70 PAGE 14 PAR I. TERMINATED LOG DUE TO NOT TRACKING PROPERLY. SEE NEW LOG PAGE 2060077 FOR TRACKING. (LP #2010626)

Part: NONE — NONE · corrosion level 2 · airframe 56,876 hrs · 39,556 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW L-28L TO L-28R. SUMMARY OF NRC 00199: CORROSION LEVEL 2: AFTER BLENDING FOUND DAMGE TO BE OUT OF LIMITS. PERMANENT REPAIR WAS PERFORMED ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW L-28L TO L-28R PER ETI-17-21-033 REV. 2 AND ER/A 595233-14 REV. ORIGINAL, SECTION I ASSOCIATED ER/A 14-595233 ADDED FOR AC 9506. (LP #2008478)

Part: NONE — NONE · airframe 56,876 hrs · 39,556 cycles

ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ASSOCIATED AA 5530-01048 ADDED FOR AC 9506. SUMMARY OF NRC 00224: VA 84027 MA AD WAS ACCOMPLISHED IN CONJUNTION WITH EM WORKCARD 5530-01048-02. (LP #2000317)

Part: NONE — NONE · airframe 56,876 hrs · 39,556 cycles

ELONGATED HOLE WAS FOUND ON RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND WING AILERON STRUCTURE. SUMMARY OF NRC 00027: RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND WING AILERON STRUCTURE WAS REPAIRED PER B717 SRM 57-00-00-2R. (LP #1996324)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,941 hrs · 38,733 cycles

THE AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE ON ARRIVAL. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK PER B717 AMM 3-51. (LP #7298548)

Part: SIGN — DETACHED (CABIN) · airframe 55,339 hrs · 38,250 cycles

THE EXIT ROW SIGN ON THE AIRCRAFT LEFT IS DETACHED. MAINTENANCE REATTACHED THE SIGN. OPERATIONAL CHECK IS GOOD. (LP #7581138)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,196 hrs · 38,138 cycles

THE INTERIOR OVERWING EXIT DOORS, AFT BOTTOM POSITION ON LEFT AND RIGHT SIDES, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK BS-119, PER B717 AMM 33-51.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 53,095 hrs · 36,346 cycles

BROKEN ON OVER WING EMERGENCY EXIT SIGN (2 EA) (CPAX). SUMMARY OF NRC 00544: OVER WING EMERGENCY EXIT SIGNS (2 EA) P/N: BR9051-001 WERE REPLACED PER B717-200 AMM 33-51-05. (LP1323338)

Part: FRAME — CRACKED (BS 1225) · airframe 53,091 hrs · 36,344 cycles

INITIAL INSPECTION: CRACK ON CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ER/A 581847-14TR REV.ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI- 17-19-177 REV.3. (LP1320117) / S

Part: DOOR FRAME — CRACKED (BS 994) · airframe 53,091 hrs · 36,344 cycles

HIDDEN DAMAGED: IN REF NRC= 00103: CRACK ON LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00639: LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 582240- 14 REV.ORIGINAL (SECTION I: PERMANENT REPAIR MINOR DEVIATION TO AN EXISTING SRM REPAIR). (LP1317941)

Part: CUSP WEB — CANNING (BS 430-445) · airframe 53,091 hrs · 36,344 cycles

INITIAL INSPECTION: OIL CAN ON CUSP WEB BTW STA= 430 AND STA=445 LH SIDE CABIN PAX . SUMMARY OF NRC 00502: CUSP WEB BTW STA= 430 AND STA= 445 LH SIDE CABIN PAX WAS REPLACED PER B717-200 SRM 53-00-55-2R-4, SRM 51- 41-02-0G AND 51-41-05-0G. (LP1317341)

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 53,091 hrs · 36,344 cycles

INITIAL INSPECTION: CRACK ON PAN OF FWD CARGO DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00184 PAN OF FWD CARGO DOOR INTERNAL STRUCTURE WAS REPAIRED PER ETI -17-19-180 REV 6 AND ERA 582177-14 REV ORIGINAL SECTION I PERMANENT REPAIR. (LP1318513)

Part: FRAME — CORRODED (BS 1022) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

FRAME CORRODED OUT OF LIMITS, BS 1022, LONGERON 27L TO 27R . THE FRAME 2 WAS REPAIRED PER SRM 53-20-07-2R-3.

Part: ACCESS PANEL — CORRODED (WATER WASTE) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON INTERNAL STRUCTURE OF WATER WASTE ACCESS PANEL. WATER WASTE PANEL WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND DWG 5965767 REV. J.

Part: LONGERON — CORRODED (BS 908-1037) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION LONGERON AT L=30 BTW Y=908/1037 AFT CARGO COMPARTMENT. (CORROSION LEVEL 2) LONGERON WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-00-05-2R-2 REPAIR 2 FIGURE 201. (LP1314196)

Part: WIRE — BROKEN (LOCKING CABLE) · airframe 53,091 hrs · 36,344 cycles

BROKEN WIRES ON LOCKING CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 CANT. CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 WAS REPLACED PER B717-200 AMM 20-00-02 AND WAS ADJUSTED PER B717-200 AMM 53-52-01-830-802.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON LOWER DOOR JAMB OF AFT COMPARTMENT CARGO. (CORROSION LEVEL 2) LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 53-20-15-2R-7 PROCEDURE 7 AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP1313860)

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 53,091 hrs · 36,344 cycles

CRACK ON FWD DOOR JAMB OF RH MLG. FWD DOOR JAMB OF RH MLG WAS REPAIRED PER ETI-17-19-186 REV. 2 AND ER/A 582048-14 REV. ORIGINAL. SECTION I : PERMANENT REPAIR.

Part: SKIN — CRACKED (BS 1025-1035) · airframe 53,091 hrs · 36,344 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDE. EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDEL WAS REPAIRED PER ER/A 582117-14 REV.ORIGINAL (SECTION I PERMANENT REPAIR) AND ETI-17-19-175 REV.2. (LP1310886)

Part: FRAME ANGLE — CORRODED (BS 908) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION FRAME CLIP STA. Y=908 BTW L= 29R/28L, Y=927 BTW L= 29R/29L, Y=954 BTW L= 29L/28R, Y=974 BTW L= 29R/26L AND Y=1002 BTW L= 29L/29R AT AFT CARGO COMPARTMENT. (CORROSION LEVEL 2): FRAME CLIPS STA Y= 974 AND 1002 WERE REPLACED PER B717-200 SRM 51-41-02-0G, DWG 9957739 REV. DN AND DWG 9958215 REV. AM. AND FRAMES STA Y= 908, 927 AND 954 WERE REPAIRED PER B717-200 SRM 53-00-06-2R REP. 2. (LP1310920)

Part: FRAME — CRACKED (BS 1178) · airframe 53,091 hrs · 36,344 cycles

CRACK ON FRAME STA Y= 1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT. DOUBLER ON FRAME STA Y=1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG SR95530005 REV . G. (LP1310562)

Part: FRAME — CRACKED (BS 1037) · airframe 53,091 hrs · 36,344 cycles

CRACK ON FRAME STA 1037 AND LONGERON 17L (CPAX) (SM). NRC 00529: FRAME STA 1037 AND LONGERON 17L WAS REPAIRED PER ER/A 581846-14 REV. ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-581846 ADDED FOR AC 9506. (LP #1309535)

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 53,091 hrs · 36,344 cycles

CRACKED DOOR JAMB ON THE TOP AT LH FWD OVERWING EMERGENCY EXIT DOOR (PTAS). NRC 00065: DOOR JAMB ON THE TOP AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B-717-200 SRM 53-20-15-2R PROCEDURE 8 REPAIR 8 FIGURE 201. (LP #1309531)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON COUNTERSINK AREA ON ACCESS PLATES #620EB, 520LB, AND 620FT. CORROSION ON COUNTERSINK AREA ON ACCESS PLATES #620EB, 520LB, AND 620FT WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR.26. REMAINING MATERIAL IS OUT OF LIMITS PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 B. (CONDITION II) TABLE 201. FUEL ACCESS PLATES #620EB, 520LB, AND 620FT WERE REPAIRED PER B717-200 SRM 57-10-01-2R-2 CONDITION II. (LP #1308324)

Part: BRACKET — CORRODED (BS 1022-1037) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

EXCESSIVE CORROSION ON LOWER BRACKET BTW STA Y=1022 AND 1037 AT AFT CARGO COMPARMENT. (CCT). NRC 00646: CORROSION LEVEL 2, LOWER BRACKET BTW STA Y=1022 AND 1037 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #5936667 REV. BU.

Part: FRAME — CRACKED (BS 674) · airframe 53,091 hrs · 36,344 cycles

CRACK WITH 0.125 IN OF LENGTH WAS FOUND ON OVERWING FRAME AT STA Y=674.000 RH. OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 CARD 5310-01436-03B. (LP #1306202)

Part: LONGERON — CORRODED (BS 1002) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON LONGERONS ENDS #25 AND 27 OF CCT BTW STA=1002 RH SIDE (SM). NRC 00593: COROSION LEVEL 2, LONGERONS ENDS #25 AND 27 OF CCT BTW STA=1002 RH SIDE WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1306330)

Part: FLOOR SUPPORT — DAMAGED (BS 235-240) · airframe 53,091 hrs · 36,344 cycles

ENLOGATED HOLE OF FLOOR SUPPORT W1 X=7 BTW STA=235 AND STA=240 CABIN PAX (SM). NRC 00415: FLOOR SUPPORT W1 X=7 BTW STA=235 AND STA=240 CABIN PAX WAS REPLACED PER B717-200 SRM 53-10-51-0I-2 AND SRM 51-41-05-0G.

Part: FRAME — CRACKED (BS 1037) · airframe 53,091 hrs · 36,344 cycles

CRACK ON FRAME LONGERON 17R AND STA 1037 (CPAX) (SM). NRC 00535: FRAME LONGERON 17R AND STA 1037 WERE REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON FUEL ACCESS CUTOUTS (RUBSTRIPS) #520CT, 520DT, 520FT, AND 141AL AT LH WING. (AI). NRC 0564: CORROSION LEVEL 2, FUEL ACCESS (RUBSTRIPS) #520CT, 520DT, 520FT, AND 141AL WERE REPLACED PER B717-200 SRM 57- 10-01-2R-3. (LP #1303518)

Part: RUB STRIP — CORRODED (RT WING) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION AT CUTOUTS (RUBSTRIPS) #620CT, 620DT, 620FT, AND 141AR RH WING. ORIGINAL THICKNESS ARE .020" AND REMAINING THICKNESS ARE .011" THEREFORE ARE OUT OF LIMITS IN REF NRC 00565. NRC 0627: CORROSION LEVEL 2, FUEL ACCESS (RUBSTRIPS) #620CT, 620DT, 620FT, AND 141AR WERE REPLACED PER B717-200 SRM 57-10-01-2R-3. (LP #1303504)

Part: CUSP WEB — CRACKED (BS 433-435) · airframe 53,091 hrs · 36,344 cycles

CRACK ON CUSP WEB MEMBRANE CABIN PAX BTW STA 433 TO 435 RH SIDE (SM). NRC 00650: CUSP WEB MEMBRANE CABIN PAX BTW STA 433 TO 435 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 211.

Part: LONGERON — CRACKED (BS 1022) · airframe 53,091 hrs · 36,344 cycles

CRACKED LONGERON 4LH STA 1022 AT CPAX. NRC 00534: LONGERON 4LH STA 1022 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON COUNTERSINK AREA ON ACCESS PLATES 520FT AND 141AR. CORROSION ON COUNTERSINK AREA ON ACCESS PLATES #520FT AND 141AR ARE OUT OF LIMITS IAW SRM 57-10-01 REPAIR 2 PAR. 5 C. (CONDITION III) TABLE 201 AND WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. FUEL ACCESS PLATES 520FT AND 141AR WERE REPLACED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY. DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY WAS REPLACED PER ER/A 542102-14 REV. ORIGINAL, SECTION 1.

Part: CUSP WEB — CORRODED (BS 832-851) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

EXCESSIVE CORROSION ON CUSP MEMBRANE WEB LH SIDE FROM STA Y=832 TO STA Y=851 IS OUT OF LIMITS. CUSP MEMBRANE WEB LH SIDE FROM STA Y=832 TO STA Y=851 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215.

Part: FLOOR SUPPORT — CORRODED (BS 1022-1076) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION FLOOR SUPPORT STA X-44 BTW Y1022 TO Y1076 (W2). NRC 00449: CORROSION LEVEL 2, FLOOR SUPPORT STA X-44 BTW Y1022 TO Y1076 (W2) WAS REPLACED DUE TO EXCESSIVE DAMAGE PER B717-200 SRM 51-30-05-0G. AND DWG 9981474 REV: L , CORROSION ON FLOOR SUPPORT STA X-44 BTW Y1022 TO Y1076 (W2) WAS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A FIGURE 103. (LP #1299399)

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON COUNTERSINK ON ACCESS PLATES #520CT AND 620CT (AI)(AD). NRC 00571: CORROSION LEVEL 2, FUEL ACCESS PLATES 520CT AND 620CT WERE REPLACED PER AMDS 2040-0010 AND 2040-00 12. (LP #1300191)

Part: CUSP WEB — CORRODED (BS 516-522) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

EXCESSIVE CORROSION ON STA Y=516 TO Y=522 RH SIDE CUSP WEB AREA IS OUT OF LIMITS. NRC 00644: CORROSION LEVEL 2, RH SIDE CUPS WEB ON STA Y= 516 TO Y=522 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 FIG 216.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 53,091 hrs · 36,344 cycles

DELAMINATED FLOOR PANEL #222YF PAX CABIN. CPAX (W -1). NRC 00600: FLOOR PANEL 222YF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1299472)

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 53,091 hrs · 36,344 cycles

CRACKED FLOOR PANEL #211ANF IN COCKPIT. (CPIL). NRC 00602: FLOOR PANEL #211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B717-200 SRM 53-20-50-2R-3. (LP #1299518)

Part: DOOR FRAME — CRACKED (NLG) · airframe 53,091 hrs · 36,344 cycles

CRACK ON DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 LH SIDE. DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 LH SIDE WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG. 201. (LP #1300907)

Part: DOOR FRAME — CRACKED (NLG) · airframe 53,091 hrs · 36,344 cycles

CRACK ON DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 RH SIDE (SM). NRC 00441: DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 RH SIDE WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG. 201. (LP #1300863)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON COUNTERSINK ON ACCESS PLATES #520DT, 520CB, AND 520GB (AI). NRC 00570: CORROSION LEVEL 2, CORROSION ON COUNTERSINK ON ACCESS PLATES #520DT, 520CB, AND 520GB WAS REMOVED PER B717-200 SRM 51-10-04-0G. CORROSION WAS OUT OF LIMITS PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 C. (CONDITION III) TABLE 201. FUEL ACCESS PLATES #520DT, 520CB, AND 520GB WERE REPLACED AND PART NUMBERS WERE VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 015 AND 57-23-01-01 ITEM 345 AND 465. FUEL ACCESS PLATE MUST BE INSTALLED UNDER AMDS 2040-0010. (LP #1299538)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 53,091 hrs · 36,344 cycles

CORROSION ON FLOOR SUPPORT 160G OF W1 AREA CABIN PAX (SM). CORROSION LEVEL 2. FLOOR SUPPORT 160G OF W1 AREA WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 53-10-51-0I-2. CORROSION ON FLOOR SUPPORT 160G OF W1 AREA CABIN PAX WAS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A FIGURE 103. (LP #1299810)

Part: CUSP WEB — CRACKED (BS 560-567) · airframe 53,091 hrs · 36,344 cycles

CRACK ON CUSP WEB MEMBRANE CABIN PAX BTW STA 560 TO 567 LH SIDE (SM). LH SIDE CUPS WEB ON STA Y=560 TO Y=567 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 FIG 215.

Part: RETAINER — CRACKED (COCKPIT WINDOW) · airframe 53,091 hrs · 36,344 cycles

CRACK ON RETAINER AT AFT UPPER CORNER OF THE COCKPIT RH SLIDING WINDOW CUT OUT ON REFERENCE OF NRC NBR 00132 (CPIL) (SM). NRC 00520: RETAINER WAS REPAIRED PER B717-200 SRM 56- 10-02-2R-1. CRACK WAS CONFIRMED AND STOPPED ON EXISTING FASTENER HOLE PER NDTSPM PART 6, 06-10-01.001.

Part: FLOOR SUPPORT — CRACKED (BS 218) · airframe 53,091 hrs · 36,344 cycles

CRACK ON FLOOR SUPPORT OF W1 X=11 BTW STA 218 CABIN PAX (W1). NRC 00414: FLOOR SUPPORT OF W1 X=11 BTW STA 218 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #1297992)

Part: CUSP WEB — CRACKED (BS 715-734) · airframe 53,091 hrs · 36,344 cycles

CRACK ON CUSP MEMBRANE WEB RH SIDE FROM STA Y=715 TO STA Y=734 AT PAX CABIN. (CPAX) NRC 00490: CUSP MEMBRANE WEB RH SIDE FROM STA Y=715 TO STA Y=734 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 206. (LP #1299273)

Part: LONGERON — CRACKED (BS 1037) · airframe 53,091 hrs · 36,344 cycles

CRACK ON LONGERON 17L AND STA 1037 (CPAX) (SM). NRC 00532: LONGERON 17L AND STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2. (LP #1298001)

Part: FORMER — CRACKED (BS 674) · airframe 53,091 hrs · 36,344 cycles

CRACKED FORMER BTW STA Y674 AND X33 AT KEEL BEAMS INTERNAL STRUCTURE (FUS). NRC 00422: CRACKED FORMER BTW STA Y674 AND X33 WAS REPAIRED PER B717-200 SRM 51-70-11 -2R REP 1 FIG 201. (LP #1297596)

Part: FORMER — CRACKED · airframe 53,091 hrs · 36,344 cycles

CRACKED FORMER BTW STA Y696 AND X28 AT KEEL BEAMS INTERNAL ESTRUCTURE (FUS). NRC 00421: FORMER BTW STA Y696 AND X28 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1 FIG 201.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 53,091 hrs · 36,344 cycles

CRACK ON RETAINER AT AFT UPPER CORNER OF THE COCKPIT LH SLIDING WINDOW CUT OUT ON REFERENCE OF NRC NBR 00131 (CPIL). NRC 00518: UPPER CORNER OF THE COCKPIT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1. (LP #1290372)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON UP/AFT RING PAN BTW STA Y=813/832 RH SIDE AT PAX CABIN (CPAX). NRC 00368: RING PAN UP/AFT BTW STA Y=813/832 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288615)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON UP/AFT RING PAN BTW STA Y=813/832 LH SIDE AT PAX CABIN (CPAX). NRC 00365: RING PAN UP/AFT BTW STA Y=813/832 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288575)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON UP/AFT RING PAN BTW STA Y=851/870 LH SIDE AT PAX CABIN (CPAX). NRC 00367: RING PAN UP/AFT BTW STA Y=851/870 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288594)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON LWR/FWD RING PAN BTW STA Y=617/636 LH SIDE AT PAX CABIN. NRC 00362: RING PAN LWR/FWD BTW STA Y=617/636 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288531)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON LWR/FWD RING PAN BTW STA Y=794/813 LH SIDE AT PAX CABIN (CPAX). NRC 00364: RING PAN LWR/FWD BTW STA Y=794/813 LH WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288517)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON UPPER/FWD RING PAN BTW STA Y=696/715 RH SIDE AT PAX CABIN (CPAX). NRC 00369: RING PAN UPPER/FWD BTW STA Y=696/715 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288626)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON LWR/FWD RING PAN BTW STA Y=655/636 LH SIDE AT PAX CABIN (CPAX). NRC 00363: RING PAN LWR/FWD BTW STA Y=655/636 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288586)

Part: PAN — CRACKED (CABIN) · airframe 53,091 hrs · 36,344 cycles

CRACK ON LWR/FWD RING PAN BTW STA Y=889/908 LH SIDE AT PAX CABIN (CPAX). NRC 00366: RING PAN LWR/FWD BTW STA Y=889/908 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288590)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,142 hrs · 32,900 cycles

VERTICAL STABILIZER LEADING EDGE HAD SIGNS OF DISTRESS TO COUNTERSINKS, ALL FASTENERS ARE LOOSE. REPAIRED IAW PRI 562910-14AD REV 0, REV 1. AND REV 2, ER/A 562910-14AD, REV ORIGINAL.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 48,142 hrs · 32,900 cycles

RT VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE, FIRST HOLE BELOW LEADING EDGE SKIN SPLICE IS OUT-OF-ROUND & UNABLE TO PERFORM OPEN-HOLE HFEC INSPECTION. REPAIRED IAW PRI 561916-14AD, REV 0, & 1, AND ER/A 561916-14AD, REV ORIG.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 48,142 hrs · 32,900 cycles

VERTICAL STAB LOWER LE SKIN AT ZFS 52 WORN AND CHAFED. SKIN SPLICE ON INNER SURFACE 15 INCHES ALONG LEADING EDGE. REPAIRED IAW PRI 562910-14AD REV. 0, REV 1, AND REV. 2 AND ER/A 562910-14AD REV. ORIGINAL.

Part: THRESHOLD — CORRODED (LAVATORY) · airframe 48,142 hrs · 32,900 cycles

CORROSION AT FWD LAVATORY ENTRY DOOR LOWER THRESHOLD. REPAIRED IAW PRI 561911-14, REV 0, AND ER/A 562911-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1076) · airframe 48,142 hrs · 32,900 cycles

FUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE 6 INCHES ABOVE RT PYLON, BS 1076. REPAIRED THE SKIN IAW PRI 562852-14, REV 0, REV 1, REV 2, AND ER/A 562852-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1095) · airframe 48,142 hrs · 32,900 cycles

FUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE AT BS 1095, 8 INCHES ABOVE THE LT PYLON. PERFORMED HFEC IAW AMM NDT SPM 06-10-01.001. REPAIRED THE SKIN IAW PRI 562854-14, REV 0, REV 1, AND REV 2, AND ER/A 562854-14, REV ORIGINAL.

Part: PAN — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 48,135 hrs · 32,897 cycles

AFT LOWER LEFT FUSELAGE, LAVATORY SERVICING PAN HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW ER/A 561915-14, REV ORIG.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 47,921 hrs · 32,749 cycles

EMERGENCY EXIT SIGN IS MISSING THE LENS. FOUND EXIT SIGN LENS, INSPECTED THE LENS, NO DAMAGE NOTED AND INSTALLED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,257 hrs · 32,318 cycles

EMERGENCY CEILING LIGHTS FROM ROWS 15 THRU 19 AND EMERGENCY CEILING EXIT SIGN INOP. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY B5-120 PER AMM 33-51-03, OPS CK GOOD.

Part: FRAME — DAMAGED (BS 237) · airframe 46,492 hrs · 31,786 cycles

BS 237 FRAME BETWEEN LONGERONS 17 AND 18L IS CRACKED AND BENT. REMOVED AND REPLACED THE FRAME IAW SRM 51-41.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 46,280 hrs · 31,638 cycles

THE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER AT AFT F/A SEAT WAS MISSING. MAINTENANCE REPLACED THE LENS AND OPS CHECKED GOOD.

Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 46,145 hrs · 31,537 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT PANELS 3 & 4 IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A FAILED WIRE CONNECTOR AT PANEL 4 AND REPLACED IT. THEY FOUND AN INCORRECT BULB AT PANEL 3 WHICH CAUSED THE FUSE TO BLOW. THE BULB AND POWER SUPPLY WERE REPLACED AND THE OPERATIONAL CHECK WAS GOOD. (LP #9364166)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,145 hrs · 31,537 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN, THE AISLE EMERGENCY LIGHTS, THE FORWARD LAVATORY, AND THE SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,008 hrs · 31,429 cycles

DURING THE TURN-AROUND CHECK, MAINTENANCE FOUND THAT SEVERAL EMERGENCY PATHWAY LIGHTS IN THE COCKPIT AND CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,724 hrs · 31,225 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN THE MID-SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THREE OF THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,071 hrs · 30,763 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK 3D AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,845 hrs · 30,563 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 3-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,331 hrs · 30,112 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE MAIN CABIN DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: HANDLE — DIRTY (L1 DOOR) · airframe 43,796 hrs · 29,649 cycles

CREW DISCOVERED THAT THE 1L DOOR WAS STUCK CLOSED AND THEY WERE UNABLE TO OPEN IT. THE DOOR HANDLE WAS CLEANED IAW PS 900-1, NR 6. MAINTENANCE OPERATED THE DOOR SEVERAL TIMES AND FOUND ALL OPERATIONS WERE NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 43,619 hrs · 29,502 cycles

TAIL COMPARTMENT AFT OVERHEAD EMER LIGHT LOOSE. SECURED LIGHT IAW SWPM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,619 hrs · 29,502 cycles

FORWARD LT OVERWING DOOR EMER SIGN LIGHT BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,619 hrs · 29,502 cycles

TAIL COMPARTMENT FWD OVERHEAD EMER LIGHT LOOSE. SECURED LIGHT IAW SWPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,619 hrs · 29,502 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 43,619 hrs · 29,502 cycles

RIGHT OVERHEAD BIN EMER BATTERY LIGHT COVER LOOSE. SECURED COVER IAW AMM.

Part: BATTERY PACK — DISCONNECTED (CABIN) · airframe 43,196 hrs · 29,219 cycles

TAIL COMPARTMENT EMER LIGHT INOPERATIVE. RECONNECTED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,196 hrs · 29,219 cycles

AFT CABIN CEILING EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,196 hrs · 29,219 cycles

MID CABIN CEILING EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: TEE FITTING — CRACKED (LT SPOILER) · airframe 43,196 hrs · 29,219 cycles

LEFT WING OTBD SPOILER, OTBD END WERE SPOILER LAND ON ACFT TEE SUPPORT CRACKED. R & R TEE CHORD IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CUSP WEB CORRODED AT BS 550, LBL 55. REPAIRED CUSP WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

LEFT VERTICAL BOX LOWER AFT ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FORMER INTERCOSTAL CORRODED, BETWEEN BS 920 - 930, LONGERON 30. R & R INTERCOSTAL IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 636 - 655, RBL 44. REPAIRED CUSP WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FRAME CRACKED AT BS 1133, STRINGER 2R. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 7 TO LBL 2. R & R SUPPORT IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FRAME CUSP T CORRODED AT BS 484, RBL 55.5. R & R CUSP T IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FRAME ANGLE SUPPORT CORRODED AT BS 1053, LONGERON 30. R & R ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED AT BS 813, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED AT BS 960, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED AT BS 939, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED, BETWEEN BS 636 - 655, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED, BETWEEN BS 200 - 218, RBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED, BETWEEN BS 636 - 653, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED AT BS 317, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

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

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

AFT ACCESSORY COMPARTMENT, RT SIDE ON GND AC Y DUCT SUPPORT BRACKET CRACKED. R & R BRACKET IAW SIP & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

ANGLE CRACKED AT BS 1152, LONGERON 2R. R & R ANGLE IAW EA.

Part: STRUCTURE — CRACKED (WALKWAY) · airframe 43,196 hrs · 29,219 cycles

AFT ACCESSORY COMPARTMENT WALKAWAY, APU ACCESS DOOR CRACKED ON WALKWAY. REPAIRED WALKWAY IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

AFT ACCESSORY COMPARTMENT CANT FRAME 1178 LT LOWER FITTING ON LOUVER CRACKED. R & R FITTING IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

AFT ACCESSORY COMPARTMENT CANT FRAME 1178, RT SIDE HAND TAIL SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,619 hrs · 29,502 cycles

SKIN DOUBLER CRACKED AT BS 1178, LONGERON 2R. REPAIRED SKIN IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

RIGHT BARREL KEEL, FORMER CRACKED AT BS 674, OTBD END. REPAIRED FORMER IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

ANGLE CRACKED AT BS 1152, LONGERON 2L. R & R ANGLE IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

LEFT SIDE KEEL BEAM FORMER CRACKED AT BS 696, OTBD END. R & R FORMER IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

RIGHT KEEL BEAM AREA, FORMER CRACKED AT BS 696, OTBD END OF FORMER. R & R FORMER IAW SRM & DWG.

Part: STRAP — CRACKED (L1 DOOR) · airframe 43,196 hrs · 29,219 cycles

L1 DOOR VERTICAL STRAP CRACKED AT BS 172. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

BARREL KEEL VERTICAL ANGLE CRACKED AT BS 674, LONGERON 30L. R & R ANGLE IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SKIN DOUBLER CRACKED AT BS 1178, LONGERON 2R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT AILERON) · airframe 43,196 hrs · 29,219 cycles

LEFT WING AILERON, OTBD HINGE T ANGLE CRACKED. R & R T ANGLE IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT MLG WW) · airframe 43,196 hrs · 29,219 cycles

RIGHT WW FWD DOOR CUT OUT INBD SUPPORT FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 794 - 813, RBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 43,196 hrs · 29,219 cycles

FORWARD CARGO DOOR, INTERNAL FITTING AT UPPER EDGE CUT OUT CRACKED. R & R FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 43,196 hrs · 29,219 cycles

CRACKED FITTING FWD CARGO DOOR INTERNAL STRUCTURE, POWER EDGE CUT OUT. R & R FITTING IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 43,196 hrs · 29,219 cycles

LEFT WING FIXED LE OTBD SIDE OF VORTILON ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LE SLAT) · airframe 43,196 hrs · 29,219 cycles

LEFT WING INBD SIDE OF NR 12 SLAT TRACK ON SLAT SIDE, ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FORMER CRACKED AT BS 674, LONGERON 26L. R & R FORMER IAW SRM & EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FORWARD CABIN LT SIDE, AFT WALL LOWER SUPPORT ANGLE, CORRODED ALONG EDGE ATTACHED TO FLOOR PANEL SUPPORT ANGLE. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

L1 DOOR WEB SKIN CRACKED AT BS 210, LONGERON 11L. REPAIRED SKIN IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FORWARD FACE OF APB DOUBLER PLATE, CORRODED AT THE 6 O CLOCK POSITION. R & R PLATE IAW DWG & SRM.

Part: ANGLE — CRACKED (LE SLAT) · airframe 43,196 hrs · 29,219 cycles

RIGHT WING INBD SIDE OF NR 12 SLAT TRACK ANGLE CRACKED. R & R ANGLE BUMPER IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN ENTRANCE DOOR JAMB WEB SKIN CRACKED AT BS 210, LONGERON 15L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 43,196 hrs · 29,219 cycles

LEFT MLG WW DOOR, SKIN AT FWD LOWER CORNER OF FITTING CUT OUT CRACKED. R & R DOOR IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

WING TO BODY FITTING CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FLOOR SUPPORT FITTING CORRODED, BETWEEN BS 200 - 216, RBL 55. R & R FITTING IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FORWARD CARGO COMPARTMENT BEHIND AFT WALL STIFFENER ON CTR WING BL 0 CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

AFT CARGO FWD BULKHEAD, RT UPPER & LOWER PANEL SUPPORT CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CUSP WEB CRACKED BETWEEN BS 275 - 294, RBL 47. REPAIRED CUSP WEB IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

C1 DOOR CUT OUT LOWER JAMB CORRODED. R & R JAMB PAN IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 715, RBL 55. R & R CUSP WEB IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SEAT TRACK CORRODED, BETWEEN BS 200 - 256, RBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

LEFT FRAME CRACKED AT BS 715. R & R FRAME IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 715, LBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR MEMBRANE CORRODED, BETWEEN BS 160 - 200, LBL 55. REPAIRED MEMBRANE IAW SRM.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR MEMBRANE CRACKED AT BS 175, LBL 8. REPAIRED MEMBRANE IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR MEMBRANE CORRODED AT BS 160, BETWEEN LBL 18 - 22. R & R MEMBRANE IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR SUPPORT, CORRODED AT BS 196.25, BETWEEN LBL 43 - LBL 15. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FLOOR SUPPORT CORRODED AT BS 160, BETWEEN LBL 4 - . R & R FLOOR SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR SUPPORT CORRODED, BETWEEN BS 160 - 196, LBL 43. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

R1 DOOR FLOOR SPLASH ANGLE, CORRODED AT AFT OF DOOR CUT OUT. R & R ANGLE IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 - 196, LBL 55. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 456 - 503, RBL 54. REPAIRED CUSP WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

FLOOR SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 44.5. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR, AFT GIRT BAR FITTING, CORRODED AT R1 DOOR. R & R FITTING IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 7 - 43. R & R FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 7 - 45. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CRACKED AT BS 654, LBL 48. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CORRODED AT BS 808, LBL 54. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CUSP WEB CRACKED AT BS 716, LBL 50. REPAIRED CUSP WEB IAW SRM.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR FALSE TRACK CORRODED, BETWEEN BS 148 - 200, RBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: SPACER — CORRODED (R1 DOOR) · airframe 43,196 hrs · 29,219 cycles

R1 DOOR GIRT BAR SPACER CORRODED. R & R SPACER IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CUSP WEB CRACKED AT BS 219, RBL 44. R & R CUSP WEB IAW DWG.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN FLOOR FALSE TRACK CORRODED, BETWEEN BS 148 - 200, LBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 851 - 870, LBL 54. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

CUSP WEB CORRODED AT BS 215, RBL 55. R & R CUSP WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,196 hrs · 29,219 cycles

SKIN CRACKED AT LOWER RT CORNER OF LAVATORY SERVICE PANEL. REPAIRED SKIN IAW EA.

Part: COVER — DAMAGED (CABIN) · airframe 42,855 hrs · 28,986 cycles

EMERGENCY EXIT LIGHT COVER INOPERATIVE ON THE OVERHEAD MOOD LIGHT PANEL FWD OF BUSINESS CLASS ROW NR 1. REPAIRED COVER IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,533 hrs · 28,772 cycles

OVERWING EMERGENCY EXIT BATTERY POWER SUPPLY FAILED OPERATIONS CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,493 hrs · 28,105 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROWS 21 TO ROW 25. R & R BATTERY IAW AMM.

Part: SKIN — CRACKED (LAV SERVICE PNL) · airframe 40,936 hrs · 27,735 cycles

LOWER RT CORNER OF LAVATORY SERVICE PANEL SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,919 hrs · 27,724 cycles

AIRCRAFT SKIN AT LOWER RT CORNER OF THE LAVATORY SERVICE PANEL CRACKED. REPAIRED SKIN IAW EA.

Part: FLANGE — CRACKED (RUDDER) · airframe 39,749 hrs · 27,011 cycles

LOWER RUDDER HINGE CUTOUT PANEL MOUNTING FLANGE CRACKED. REPAIRED FLANGE IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 40,161 hrs · 27,269 cycles

R1 DOOR EMERGENCY LIGHT COVER LOOSE. INSTALLED LENS PER AMM.

Part: LONGERON — CRACKED (LT PYLON) · airframe 38,791 hrs · 26,425 cycles

CRACK LOCATED ON NR1 ENGINE PYLON APRON AT UPPER AFT COWL HINGE CUT OUT. STOP DRILLED 2 CRACKS IN UPPER LONGERON OF NR 1 ENGINE PYLON AT AFT CUT OUT, FABRICATED AND INSTALLED REPAIR Z ANGLE IAW B-717 SRM 51-41-05 51-41-01, 51-41-04.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 37,694 hrs · 25,709 cycles

MAIN CABIN FLOORBOARD RIGHT SIDE PNL 222AEF LOCATED ADJACENT TO OVERWING HATCH IS DELAMINATED. REMOVED AND REPLACED PANEL 222AEF IAW SRM.

Part: HOUSING — CRACKED (CABIN) · airframe 37,694 hrs · 25,709 cycles

AFT ACCESSORY COMPARTMENT FWD OVERHAUL EMERGENCY EXIT LIGHT HOUSING CRACKED. REMOVED AND REPLACED LIGHT HOUSING IAW SRM.

Part: HOUSING — CRACKED (CABIN) · airframe 37,694 hrs · 25,709 cycles

AFT ACCESSORY COMPARTMENT AFT OVERHEAD EMERGENCY EXIT LIGHT HOUSING CRACKED. REMOVED AND REPLACED LIGHT HOUSING IAW SRM.

Part: RUB STRIP — CRACKED (LT HORIZ STAB) · airframe 37,694 hrs · 25,709 cycles

LEFT LOWER BANANA FAIRING HAS CRACKED RUBSTRIP AT FWD END 81-20. REMOVED LT LOWER BANANA FAIRING REMOVED & REPLACED RUBSTRIP RE-INSTALLED LEFT LOWER BANANA FAIRING IAW B717 AMM 55-10-01 AND 55-10-02.

Part: LENS — BROKEN (CABIN) · airframe 37,694 hrs · 25,709 cycles

LENS AT SEAT 18R FOR EMERGENCY EXIT LIGHT IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS AT SEAT 18R IAW B717 AMM 33-51-04.

Part: LENS — BROKEN (TAIL CONE) · airframe 37,694 hrs · 25,709 cycles

TAIL CONE EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 37,694 hrs · 25,709 cycles

CRACK APPROX 5/16" LONG LOCATED ON NR 1 ENGINE PYLON APRON AT UPPER AFT COWL HINGE CUTOUT. REMOVED AND REPLACED 2 ANGLES IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 37,568 hrs · 25,624 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOYED, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MM.

Part: FILTER — FAULTY (HYDRAULIC SYS) · airframe 37,321 hrs · 25,463 cycles

DIVERSION - RT HYDRAULIC LOW QUANTITY ALERT AFTER APPROX 45 MINS IN FLIGHT. REMOVED AND REPLACED RT ENGINE PRESSURE AND CASE DRAIN FILTER HOUSING PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

ALL EMERGENCY ESCAPE PATH LIGHTS ON SIDE OF SEAT 3D ARE INOP. REMOVED AND REPLACED EMERGENCY BULBS ON SEAT 3D, OPS CHECK GOOD AMM 33-51.

Part: INVERTER — FAULTY (ELECTRICAL SYS)

AC DROPS AC EMER BUS WHEN EMERGENCY POWER SWITCH IS PLACED TO ARM. REMOVED AND REPLACED THE EMERGENCY INVERTER PER B717 AMM 24-24-01, OPS CHECK GOOD.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

R1 DOOR EMERGENCY SLIDE INDICATING RED ON PRE FLIGHT. REMOVED AND REPLACED R1 DOOR EMERGENCY SLIDE ASSY IAW B717 AMM 25-61-03(RII).

Part: SLIDE — DETACHED (L1 DOOR)

SLIDE DETACHED FROM L-1 DOOR WHEN DOOR OPENED ON ARRIVAL AT GATE. (PINS VERIFIED TO BE INTACT). INSPECTED L-1 DOOR LANYARD AWI CLEARS MDDR 213306 REF 25-61MM.

Part: POWER SUPPLY — UNSERVICEABLE (CABIN)

AFT ACCESSORY EMERGENCY LIGHTS POWER SUPPLY NEEDS TO BE REPLACED (B5-260 POWER SUPPLY IDENTIFIER). REMOVED AND REPLACED BATTERY SUPPLY ASSY REF MM 33-51, OPS CHECK GOOD.

Part: SIGN — LOOSE (CABIN)

EXIT SIGN AT ROW 1 NEEDS TO BE RE-SECURED. RE-SECURED EXIT SIGN AT ROW 1 AS REQUIRED.

Part: LONGERON — CORRODED (BS 927 L30L)

AFT CARGO COMPARTMENT FUSELAGE LONGERON, STA 927, LONG L30, CORROSION. ACCOMPLISHED FUSELAGE LONGERON SPLICE REPAIR IAW SRM 53-20-05, FIG 201. SEE NR 480043, 480043-1 AND 480043-2.

Part: LONGERON — CRACKED (BS 1144 L21L)

LT FUSELAGE LONGERON, STA 1144 TO L21L, CRACKED. ACCOMPLISHED FUSELAGE LONGERON SPLICE REPAIR IAW EA 17-53-02784IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD CARGO, AFT BULKHEAD CENTER FLOOR SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED NEW SUPPORT INSTALLED AT FWD CARGO COMPARTMENT AFT BULKHEAD CENTER FLOOR SUPPORT IAW B717 SRM 51-41-02

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AT AFT CARGO FWD LWR SPLICE OF DEPRESSOR SEAL. FOUND CORROSION DAMAGE AT SPLICE, OUT OF LIMITS. CORROSION LEVEL 2. REMOVED AND REPLACED SPLICE AT AFT CARGO, FWD LWR DEPRESSOR SEAL POSITION AS PER B717 SRM 51-41-02 AND 51-40-08.

Part: COVER — MISSING (EXIT SIGN)

COVER ON EXIT SIGN IN AIRCRAFT FORWARD MISSING. RE-INSTALLED COVER ON EXIT SIGN AS REQUIRED.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING SERVICE CHECK FOUND EMERGENCY LIGHT INOP AT SEATS 20-24 AND AFT OVERWING EXIT IDENTIFIERS. REMOVED & REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLIES AT B5-118 & B5-119 IAW AMM 33-51-03. OP CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE)

LEFT CABIN FLOOR SEAT TRACK BETWEEN STA 294 AND 579 HAS CORROSION AND GOUGE AT LBL 46. ACCOMPLISHED SPLICE REPAIR TO SEAT TRACK AT STA 513.5 PER DC9 SRM 53-05 FIGURE 4F, EA 17-53-02016IR DATED 09/18/09 AND BOEING MESSAGE CQT-CQT-09-0195-02B. SEE NR 5153, 5169 AND 5177.

Part: FRAME — DAMAGED (FUSELAGE)

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

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON 30 HAS CORROSION BETWEEN STA 994 AND 1006. INSTALLED NEW SECTION AT AFT CARGO COMPARTMENT LONGERON 30 BETWEEN LONGERON 994 AND 1006 PER B717 SRM 53-00-05. SEE NR 3155.

Part: RIVET — DAMAGED (FUSELAGE)

DAMAGED RIVETS FROM LIGHTNING STRIKE REPLACED WITH BLIND RIVETS. INSTALLED SOLID RIVET AT STA 337 L12R AND STA 251 L15R REF B717 SRM 51-40-02 AND EA 17-53-01480A DATED 01/22/09 RFE 09-0111. SEE NR 3003.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON 30 HAS CORROSION AT STA 954. INSTALLED REPAIR PART TO AFT CARGO COMPARTMENT LONGERON 30 BETWEEN STA 946 AND 1022 PER B717 SRM 53-00-05. SEE NR 3153 AND 3819.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 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: BRACKET — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT FUSELAGE COMPARTMENT TO CANTED FRAME 1103, AFT SIDE ANGLE BRACKET CRACKED BETWEEN LONGERON 1 AND 2L. INSTALLED NEW ANGLE AND STIFFENER AT AFT ACCESSORY COMPARTMENT FUSELAGE TO CANTED FRAME 1103 AFT SIDE PER EA 17-53-02020IR DATED 09/22/09. SEE NR 4168 AND 4361.

Part: CUSP WEB — CORRODED (FUSELAGE)

CUSP MEMBRANE CORRODED THROUGH FUSELAGE STA 256 RBL 52 AT NUT PLATE. INSTALLED CUSP MEMBRANE REPAIR AT FUSELAGE STATION 256 RBL 52 AT NUT PLATE PER EA 17-53-02048IR, DATED 09/22/09 RFE 09-1535. SEE NR 3821.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM FROM STA 160 TO STA 200 HAS CORROSION AT RBL 38. INSTALLED NEW CABIN FLOOR SUPPORT BEAM AT STA 160 TO STA 200 AT RBL 38 PER B717 SRM 51-41-02 AND 51-41-05. SEE NR 5130.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM BETWEEN LBL 21 AND RBL 51 AT STA 200 HAS CORROSION. INSTALLED NEW SUPPORT BEAM BETWEEN LBL 21 TO RBL 51 STA 200 PER B717 SRM 51-40-02. SEE NR 5133.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER JAMB CORRODED. INSTALLED NEW PAN SPLICES AND PARTS AT AFT CARGO COMPARTMENT LOWER JAMB AREA PRE B717 SRM 53-20-15. SEE NR 3006 AND 3009.

Part: LATCH — UNSERVICEABLE (TAIL CONE)

TAIL CONE EMEGENCY EXIT DOOR WILL NOT STAY OPEN. DOOR CATCH WILL NOT CATCH ON TOP OF THE DOOR. REPLACED AFT DOOR HOLD OPEN LATCH, REF 52-12.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT)

L-1 DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REF CARD NR 339. FAILED TO OP CHECK. REINSTALLED CONNECTOR FOR L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, REF CH 33-51-18 BOEING 717 MM.

Part: FRAME — DAMAGED (BS 1178 S25R)

FRAME DAMAGED AT STA 1178 BETWEEN LONG BL0 AND 25R. INSTALLED NEW LOWER CAP SECTION AND SPLICE AT STA 1178 BETWEEN LONGERON BL0 AND 25R IAW SRM 51-70-11, AIRTRAN EA17-53-00939A AND MESSAGE 1-CEY7NA.

Part: DOUBLER — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. DOUBLER DAMAGE BETWEEN LONG 25R AND LONG 25L ON CANTED FRAME 1161. INSTALLED NEW DOUBLER AT CANTED FRAME 1161 BETWEEN LONGERON 25R AND LONG 25L IAW B717 SRM 51-41-02 AND DRG 99118401. MATERIAL USED 7075 T6 .080.

Part: STIFFENER — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. STIFFENER AT 1178 FRAME AND LONGERON 22R DAMAGED. INSTALLED 2 EA NEW STIFFENER AT STA 1178 LONG 22R IAW B717 SRM 51-41-02.

Part: FRAME — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. CANTED FRAME 1178 DAMAGED BETWEEN LONG 24R TP BL 0. INSTALLED NEW CANTED FRAME AND SPLICE REPAIR AT STATION 1178 BETWEEN LONGERON 24R AND BL 0 IAW B717 SRM 51-41-02 AND AIRTRAN EA17-53-00939A. MATERIAL USED 7075 T6 .081.

Part: WEB — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. WEB AT STA 1178 BETWEEN LONG 24L AND 24R DAMAGED. INSTALLED NEW WEB AT STA 1178 BETWEEN LONGERON 24L AND LONGERON 24R IAW B717 SRM 51-41-02 AND MESSAGE 1-CEY7-MJ. MATERIAL USED 7075 T6 .032.

Part: SKIN — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. SKIN DAMAGED BETWEEN CANTED FRAME 1145.009 AND 1178. INSTALLED SKIN REPAIR AT CANTED FRAME FROM STA 1145 TO STA 1178 IAW B717 SRM 51-41-02 AND DRG 9911840 AND AIRTRAN EA17-53-00939A DATED 01/21/08. MATERIAL USED 7075 T6 .040.

Part: STIFFENER — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. VERTICAL STIFFENERS 1 AT STA 1161 DAMAGED AT APPROX RBL 8 AND 1 AT APPROX RBL 18. INSTALLED 2 EACH VERTICAL STIFFENER AT STA 161, AT RBL 8 AND RBL 18 IAW B717 SRM 51-41-02, MATERIAL USED FROM S114-15595-12000.

Part: SPLICE — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. HOLES ELONGATED ON SPLICE AT CANTED FRAME 1161 BL 0. INSTALLED NEW SPLICE AT CANTED FRAME STA 1161 BL 0 IAW B717 SRM 51-41-05 AND AIRTRAN ES17-53-00939A DATED 1/21/08.

Part: WEB — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. WEB AT FRAME AT STA 1161 DAMAGED BETWEEN BL 0 AND L24R. INSTALLED NEW WEB AT FRAME STA 1161 BETWEEN BL 0 AND LONGERON 24R IAW B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075 T6 .032.

Part: DOUBLER — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. DOUBLER DAMAGE BETWEEN LONG 25R AND LONG 25L ON CANTED FRAME 1178. INSTALLED NEW DOUBLER AT CANTED FRAME 1178 BETWEEN LONGERON 25R AND LONG 25L IAW B717 SRM 51-41-02 AND DRG 9911839. MATERIAL USED 7075 T6 .063.

Part: FRAME — DAMAGED (BS 1178 S25R)

A/C STRUCK BY BAGGAGE CART, STA 1178 FRAME DAMAGED BETWEEN LONGERON BL0 AND 25R. INSTALLED COMPLETE REPAIR PART AT STA 1178 BETWEEN LONG BL0 AND 25R IAW B717 SRM 51-41-05 AND MESSAGE 1-CEY7GK AND AIRTRAN EA17-53-009392.

Part: LONGERON — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. LONGERON DAMAGE AT 24R BETWEEN STA 1145 AND STA 1161. INSTALLED NEW LONGERON 24R BETWEEN STA 1145 AND STA 1161 IAW B717 SRM 51-41-02.

Part: SKIN — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. SKIN DAMAGE BETWEEN CANTED FRAME 1178 AND 1183. INSTALLED NEW SKIN SECTION AT CANTED FRAME BETWEEN STATION 1178 AND STATION 1200 IAW B717 SRM 51-41-02 AND DRG 9911840.

Part: ANGLE — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. ANGLE SUPPORT DAMAGE BETWEEN STA 1178 AND 1189. INSTALLED NEW ANGLE SUPPORT FROM STA 1178 TO STA 1189 IAW SRM 51-41-01 AND SRM 51-41-05 AND DRG 9911839.

Part: FRAME — DAMAGED (BS 1161)

HOLES ELONGATED ON FRAME STA 1161 LBL0 TO LBL14. INSTALLED NEW LOWER CAP SECTION AND SPLICE FROM LBL0 TO LBL14, STA 1161 IAW AIRTRAN EA17-53-00939A.

Part: FRAME — CRACKED (FUSELAGE)

A/C STRUCK BY BAG CART. LOWER CHORD ON CANTED FRAME 1161.801 IS CRACKED BETWEEN LONG 24R AND BL 0. INSTALLED NEW CANTED FRAME REPAIR ATA STATION 1161 BETWEEN LONGERON 24R AND BL 0 IAW B717 SRM 51-41-02 AND SRM 51-41-05 AND AIRTRAN EA17-533-00939 IR DATED 01/10/08.

Part: LONGERON — DAMAGED (FUSELAGE)

A/C STRUCK BY BAG CART. LONGERON 25R DAMAGED BETWEEN STA 1145 TO 1178. INSTALLED NEW LONGERON 25R BETWEEN STATION 1145 AND STATION 1178 IAW B717 SRM 51-41-02.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO THRESHOLD CUTOUT HAS AREAS OF CORROSION IN PAN. REPAIR LOWER DOOR JAMB PAN SECTION AT FWD CARGO COMP IAW B717 SRM 53-70-15 REPAIR 6.

Part: SEAT TRACK — CORRODED (FUSELAGE)

COPILOT'S AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. FABRICATED SEAT TRACK FROM RAW STOCK AND REPLACED TRACK.

Part: LIGHT — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTING SYSTEM LEFT ON AFTER TOWING SYSTEM FULLY DISCHARGED. C/W AMM 33-51-00, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT OVER THE TAIL CONE EXIT IS INTERMITTENTLY ON WHEN IT SHOULD BE OFF. REPLACED EMERGENCY LIGHT PACK ASSY OVER AFT FLIGHT ATTENDANT`S SEAT PER M/M 33-51, OPS CHECKS NORMAL. P/N OFF/ON 803925-1, S/N OFF 21144, S/N ON 20316.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED R2-5086 RELAY, NO HELP. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH IAW M/M 20-30-06. OPS CHECKS GOOD IAW M/M 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEAT ROWS 10 AND FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY SUPPLY ASSY REF 717 AMM 33-51-03.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY EXIT ROW LIGHTING FROM ROW 11 TO 19 INOPERATIVE DURING ROUTINE SERVICE CHECK. REPLACED POWER SUPPLY. OPS CHECK NORMAL.

Part: FUEL CAP — MISSING (LT WING)

ON T/O FUEL LEAKING OUT OF LEFT WING FROM FUEL CAP AREA. INSTALLED LEFT WING FUEL CAP REF MM 28-00. OK FOR SERVICE. INSPECTED LEFT WING, NO DAMAGE FOUND. INSPECTED LEFT ENG FAN, NO DAMAGE FOUND. FOUND LEFT OVERWING FUEL CAP MISSING.

Part: FRAME — CRACKED (BS 1178)

TWO CRACKS ON FUSELAGE CANTED FRAME STA 1178.225 BETWEEN LONGERON 16L AND 18L. INSTALLED ANGLE REPAIR AND FILLER AT FS CANTED FRAME STA 1178.225, BETWEEN LONGERON 16L AND 18L IAW B717 SRM 51-70-11 FIG 201. MATERIAL USED 7075-0-0.80, 15.5 X 2.5 AND 7075 T6 .071, 1 X 1 INCH AND 3 X 1 INCH H.T TO T6.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPENER)

UNCOMMANDED SMALL RUDDER MOVEMENTS IN CHOPPY AIR. NOSE MADE SMALL YAW CHANGES, ACTED LIKE NO YAW DAMP ON. NO PROBLEM NOTED WHILE IN SMOOTH AIR. NEITHER AUTOPILOT ON. PROBLEM STOPPED WHEN RUDDER HYDRAULIC CONT TURNED OFF. REMOVED AND REPLACED YAW DAMPENER ACTUATOR.

Part: HARNESS — LOOSE (CABIN)

E-PATH LIGHT INOPERATIVE AT ROW 17. FOUND HARNESS LOOSE. RECONNECTED HARNESS AND RESECURED TO SEAT ASSEMBLY IAW AVIO INTERIOR CMM 25-24. OPS CHECKED GOOD.

Part: DEFLECTOR — INOPERATIVE (NLG)

NOSE GEAR WOULD NOT FULLY RETRACT. FOUND THE NOSE GEAR SPRAY DEFLECTOR DAMAGED, CAUSED BY ARRESTOR CABLE ON RUNWAY. REMOVED AND REPLACED SPRAY DEFLECTOR, PERFORMED VISUAL INSPECTION OF NOSE GEAR AREA AND EXTENTION AND RETRACTION TEST IAW 717 MM 32-30.

Part: FMC — INOPERATIVE (NR 2 ENGINE)

FOUND NR 2 ENGINE FLAMED OUT AT CRUISE, 33,000 FT. ATTEMPTED TWO STARTS, ENGINE WOULD NOT RESTART. REMOVED AND REPLACED FMU IAW B717 MM 73-21-03, AND TEST 2A 71-00-11.