N974AT

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 61,246 hrs · 43,408 cycles

RT OVERWING EMERGENCY EXIT LIGHT NOT OPERATIONAL. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT PER B717 AMM 33-51. (8143300)

Part: CYLINDER — FAULTED (SLAT DRIVE) · airframe 60,636 hrs · 42,844 cycles

SHIP 9536-FCNT-THE CREW RECEIVED A SLAT DISAGREE MESSAGE ON APPROACH WITH ASSOCIATED ROLL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT INBOARD SLAT DRIVE CYLINDER.(7345922)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 59,951 hrs · 42,234 cycles

THE R1 AND L1 SMALL EMERGENCY EXIT SIGNS ARE INOPERATIVE (LOWER). AFTER TROUBLESHOOTING MAINTENANCE FOUND THAT THE BATTERY PACK (B5-118) INSIDE THE OVERHEAD BIN ABOVE 2D WAS NOT CONNECTED. THE PLUG WAS RECONNECTED AND THE OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51-03 000-802.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,449 hrs · 41,825 cycles

MAINTENANCE FOUND ROW 19 LT & RT EMERGENCY EXIT SIGN LIGHTS WERE INOPERATIVE. THEY REPLACED THE EMERGENCY LIGHT BATTERY PACK LOC B5-121 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6776224)

Part: FUEL SYS — LEAKING (ZONE 500) · airframe 59,610 hrs · 41,957 cycles

FUEL LEAK FOUND DURING INSP OF LH WING AFT LOWER SKIN DOUBLER AT XRS 164. ACCOMPLISHED PRI 623309-14 REV O THROUGH 3 REMAINING FUEL SEE POST PRI'S WITHIN B717 AMM 28-11-00 GROUP A ALLOWANCE. FORWARD TO MON PER ER/A 623309-14 AD REV O REPETITIVE INSP REQ DAILY TERMINATING ON 30 DAYS. PERMANENT REPAIR WILL BE REQUIRED. SEE ER/A 623309-14AD FIGURE 8 FOR INSP/SEEP AREAS. OK FOR SVC. C/W REPETITIVE INSPECTION OF DISCREPANT AREA OF L/H WING AREA PER ERA 623309-14AD REV ORIG AND B717 AMM 28-11-00. NO LEAKS NOTED. C/W SECTION III OF ERA 623309-14AD REV A, NO DAMAGE, NO LEAKS ON LHS WING AREA. OK TO CLOSE THIS LOG. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 07FEB25 AND LOG COMMENTS. (LP #0752655)

Part: WIRE — OVERTEMP (ZONE 200) · airframe 59,416 hrs · 41,804 cycles

SHIP 9536 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO DTW AND DECLARED AN EMERGENCY WITH ATC DUE TO BURNING SMELL IN THE CABIN AROUND ROW 17. AN OVERWEIGHT LANDING RESULTED BUT WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE PED POWER OUTLET AND ATTACHING WIRES AT SEAT 17B HAD EVIDENCE OF OVERHEATING. THE OUTLET AND ATTACHING HARNESS WAS REPLACED. OPERATIONAL CHECK WAS NORMAL AND THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #6490084)

Part: CONTROL UNIT — FAULTED (GENERATORS) · airframe 59,301 hrs · 41,708 cycles

SHIP 9536 -MISC/DE- FLIGHT CREW NOTED THE "LEFT GENERATOR OFF" MESSAGE WITH A POSSIBLE ELECTRICAL SMELL IN THE CABIN. THE PILOT DECLARED AN EMERGENCY WITH ATC AND WAS MET BY ARFF AFTER A NORMAL SAFE LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE EPCU, L PCDU, AND THE L GENERATOR POWER RELAY. RAN LEFT ENGINE WITH NO ISSUES. INVESTIGATED ORIGIN OF ELECTRICAL SMELL WITH NO FINDINGS. A/C RETURNED TO SERVICE. (LP #6693894)

Part: PUMP — FAILED (ZONE 100) · airframe 59,409 hrs · 41,799 cycles

SHIP 9536 -MISC/DE- DECLARED AN EMERGENCY DUE TO LEFT HYDRAULIC PUMP FAIL MESSAGE AND LEFT GENERATOR OFF MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT IDG. ALL RETURN TO SERVICE TEST PASSED. (LP #0690281)

Part: COVER — DETACHED (ZONE 200) · airframe 58,582 hrs · 41,083 cycles

MISSING FWD ''EXIT'' PLACARD/SIGN. MAINTENANCE RE-INSTALLED EXIT SIGN COVER REF B717 AMM 33-51. (LP #6186440)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 58,292 hrs · 40,837 cycles

WHILE IN ATL FOR SCHEDULED MAINTENANCE AND DURING ACCOMPLISHMENT OF WORKCARD 5530-01048-02, MAINTENANCE REPORTED CRACK INDICATIONS AT TWO EXISTING FASTENER LOCATIONS IN THE RH FRONT SPAR CAP LAYER FORWARD FLANGE. SUBJECT FASTENERS ARE IDENTIFIED AS HOLE 4 AND HOLE 5 BELOW ZFS=52.267. MAINTENANCE REPORTED THAT THE CRACK INDICATION WAS ISOLATED TO THE SKIN LAYER ONLY WITH NO CRACKS REPORTED IN THE SPAR CAP. THE HOLES ARE COMMON TO AN EXISTING WRAP AROUND DOUBLER INSTALLED PER B717 SRM 55-30-01 REPAIR 7. ER/A 600805-14 AUTHORIZES THE BUSHING OF MULTIPLE HOLES, TRIMMING OF THE SKIN COMMON TO HOLE 5, REPAIR OF THE INTERNAL BONDED DOUBLER, AND INSTALLATION OF AN ENLARGED EXTERNAL DOUBLER.

Part: HINGE FITTING — DAMAGED (TR NR 3 FLAP) · airframe 58,230 hrs · 40,793 cycles

ELONGATED HOLE AND DAMAGED BOLT WAS FOUND AT RH FLAP HINGE #3. SUMMARY OF NRC 00776: ELONGATED HOLE AND DAMAGED BOLT AT RH FLAP HINGE #3 WAS REPAIRED PER PRI 617866-14 REV 1 & ER/A PRI 617866-14 REV ORIG. DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM MAY 18, 2024. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. UNDER LOGPAGE 0353380 ASSOCIATED ER/A 14-617866 ADDED FOR AC 9536. (LP #0406119)

Part: BEAM — DAMAGED (BS 190-200) · airframe 58,229 hrs · 40,792 cycles

CRACK BEYOND STOP DRILL ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00174: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7 PAR. 6 FIGURE 201. (LP #0402980)

Part: WINDOW FRAME — CRACKED (LEFT) · airframe 58,229 hrs · 40,792 cycles

CRACK ON RETAINER AND FRAME AT LH SLIDING WINDOW A COCKPIT. SUMMARY OF NRC 00182: FRAME AT LH SLIDING WINDOW A COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1 AND RETAINER LH SLIDING WINDOW COCKPIT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. PERFORM AN EXTERNAL VISUAL INSPECTION ON EXTERNAL REPAIR EVERY "C" CHECK PER B717 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1, TABLE 203. (LP #0400375)

Part: SKIN — DAMAGED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION WAS FOUND ON VERTICAL AND HORIZONTAL UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABILIZER. UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABILIZER WERE REPAIRED PER ER/A 617894-14 REV ORIGINAL & PRI 617893-14 REV 2 AND ER/A 617893-14 REV ORIGINAL & PRI 617894-14 REV 3 BY ER/A 617894-14 REV O.

Part: PAN — CRACKED (AFT CARGO) · airframe 58,229 hrs · 40,792 cycles

CRACK ON PAN BTW 5 AND STOP FITTINGS NBR 5 OF AFT CARGO DOOR. SUMMARY OF NRC 00781: INNER PAN ON BEAM 5 AT AFT CARGO DOOR WAS REPAIRED PER ERA 617933-14. REV ORIGINAL AND PRI 617933-14 REV 2 ASSOCIATED ER/A 14-617933 ADDED FOR AC 9536. (LP #0376682)

Part: LUG — CORRODED (ELEVATOR) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON FITTING LUGS OF ELEVATOR HINGE EYEBOLT STA XHS=50 AROUND BUSHINGS, WAS FOUND ON LH AND RH SIDE. SUMMARY OF NRC 00775: ELEVATOR HINGE EYEBOLT STA XHS=50 ON LH AND RH SIDE WERE REPAIRED PER ER/A 618032-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 618032-14 REV 2. ASSOCIATED ER/A 14-618032.

Part: SKIN — DENTED (BS 205 L17L) · airframe 58,229 hrs · 40,792 cycles

DENT ON FUSELAGE SKIN STA 205, 1" ABOVE LONGERON 17L WITH DIMENSIONS AS A FOLLOW D (WIDTH)=1.300, X (DEPTH)=0.110, D/X=11.81 IS OUT OF LIMITS PER B717 SRM 53-01-01-1A, PROCEDURE 3 ALLOWABLE DAMAGE 3 PAR 4. C CONDITION 1B. SUMMARY OF NRC 00388: PREVIOUS REPAIR (IN REFERENCE LOG PAGE 1844543) WAS REMOVED ON FUSELAGE SKIN, AND NEW REPAIR WAS PERFORMED ON FUSELAGE SKIN STA 205, 1" ABOVE LONGERON 17L PER ER /A 617434-14 REV. ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 617434-14 REV 1. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 8,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR. REFER TO LP 0334591. ASSOCIATED ER/A 14-617434 ADDED FOR AC 9536. (LP #0354135)

Part: DOOR FRAME — DAMAGED (BS 427 L25R) · airframe 58,229 hrs · 40,792 cycles

ELONGATED HOLE ON DOOR JAMB STA Y=427 AND LONGERON 25R. SUMMARY OF NRC 00173: DOOR JAMB STA Y=427 AND LONGERON 25R WAS REPAIRED PER PRI 617550-14 REV 3 AND ER/A 617550-14 REV 0, SECTION I: REPAIR. ASSOCIATED ER/A 14-617550 ADDED FOR AC 9536. (LP #0353594)

Part: SKIN — CRACKED (BS 1022-1076) · airframe 58,229 hrs · 40,792 cycles

CRACK ON FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R. SUMMARY OF NRC 00164: FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR, UNDER LOG 0351829. ASSOCIATED ER/A 14-617295 ADDED FOR AC 9536. (LP #0352108)

Part: SKIN — CRACKED (BS 1087 L13-14R) · airframe 58,229 hrs · 40,792 cycles

CRACK ON FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R. SUMMARY OF NRC 00165: FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR, UNDER LOG 0351829. ASSOCIATED ER/A 14-617295 ADDED FOR AC 9536. (LP #0352099)

Part: PAN — CRACKED (FWD CARGO) · airframe 58,229 hrs · 40,792 cycles

CRACK WAS FOUND ON PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE). SUMMARY OF NRC 00610: INNER PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE) WAS REPAIRED PER ER/A 617689-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617689-14 REV 2. ASSOCIATED ER/A 14-617689 ADDED FOR AC 9536. (LP #0347254)

Part: FRAME — CRACKED (BS 1037 S17L&R) · airframe 58,229 hrs · 40,792 cycles

CRACK ON MAIN FRAME STA 1037 LONGERON 17L AND LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00459: MAIN FRAME STA 1037 LONGERON 17L WAS REPAIRED PER ER/A 617631-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND MAIN FRAME STA 1037 LONGERON 17R WAS REPAIRED PER B717 SRM 53-20-07-2R REPAIR 4. ASSOCIATED ER/A 14-617631 ADDED FOR AC 9536. (LP #0347698)

Part: FLOORBEAM — DAMAGED (BS 696 LBL56) · airframe 58,229 hrs · 40,792 cycles

-AD- REWORK ON WEB BELOW FLOOR BEAM DOES NOT MEET WITH EDGE DISTANCE REQUIREMENTS AT STA 696 X=56 LH. SUMMARY OF NRC 00439: WEB BELOW FLOOR BEAM ON STA 696 X=56 LH WAS REPAIRED PER ER/A 617901-14AD REV ORIGINAL, SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 10MAY2024. ADDITIONAL ENGINEERING AUTORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT IN REF TO LOG PAGE #0345803. ASSOCIATED ER/A 14-617901 ADDED FOR AC 9536. (LP #0347704)

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON DOOR JAMB BTW L24 AND L24 LOWER AREA AFT CARGO. SUMMARY OF NRC 00205: CORROSION LEVEL 2. DOOR JAMB AND REPAIR DOUBLERS (ANGLES) BTW L24 AND L24 LOWER AREA AFT CARGO WERE REPLACED PER B717 SRM 53-20-15-2R REP 7.

Part: DOOR FRAME — CORRODED (BS 370-427) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON DOOR JAMB BTW STA Y=370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00172: CORROSION LEVEL 2. DOOR JAMB BTW STA Y =370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R-REP 6, PAR 6. (LP #0344791)

Part: SKIN — CRACKED (BS 1037 L14L) · airframe 58,229 hrs · 40,792 cycles

CRACK ON FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L. SUMMARY OF NRC 00162: FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L WAS REPAIRED PER ER/A 617297-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617297 ADDED FOR AC 9536. (LP #0344789)

Part: CARGO TRACK — CORRODED · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION WAS FOUND ON TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE, CORROSION LEVEL 2. TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE WAS REPLACED PER B717 SRM 51-41-01-0G. (LP #0345653)

Part: INTERCOSTAL — CRACKED (BS 832-851) · airframe 58,229 hrs · 40,792 cycles

CRACK ON INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00509: INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR. 4. (LP #0344606)

Part: PIN — OUT OF POSITION (TAILCONE RELEASE) · airframe 58,229 hrs · 40,792 cycles

INCORRECT HRS POSITION OF TAILCONE RELEASE MECHANISM CAM PIN STA Y=1225 CANT AT AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00817: TAILCONE RELEASE MECHANISM CAM PIN WAS POSISIONATED IN THE CORRECT POSITION AND ADJUSTED PER B717 AMM 53-52-03 820-801 STEP A TO STEP C AND STEP E. (LP #0344183)

Part: LONGERON SPLICE — CORRODED (BS 889-908) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON LOWER SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00514: CORROSION LEVEL 2. SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 9930612 REV CG AND B717 SRM 51-41-05-0G. (LP #0340715)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 58,229 hrs · 40,792 cycles

CRACK WAS FOUND OVER THE VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP. SUMMARY OF NRC 00469: CRACK ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP WAS REPAIRED (WELDED) PER ER/A 382101-14MA REV H. SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-382101 ADDED FOR AC 9536. (LP #0339215)

Part: CUSP WEB — CORRODED (BS 940) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON LOWER SURFACE OF CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN. SUMMARY OF NRC 00594: CORROSION LEVEL 2. CORROSION ON CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 209 CONFIGURATION-7013. (LP #0331931)

Part: LUG — CRACKED (BS 715 RBL 54) · airframe 58,229 hrs · 40,792 cycles

CRACK ON OVERWING FRAME LUG STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR. OVERWING FRAME STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR WAS REPLACED PER AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9536.

Part: CUSP WEB — CORRODED (BS 832-845) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON CUSP WEB LOWER AND UPPER SIDE IN SECTION STA Y: 832 TO 845 X: 56, PAX CABIN. SUMMARY OF NRC 00784: CORROSION LEVEL 2. CORROSION ON CUSP WEB STA Y: 832 TO 845 X: 56, PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4, FIGURE 215. (LP #0331554)

Part: FRAME — CRACKED (BS 715) · airframe 58,229 hrs · 40,792 cycles

CRACK ON FRAME CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE. SUMMARY OF NRC 00494: FRAMES CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE WERE REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0331520)

Part: CUSP WEB — CORRODED (BS 526-571) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON CUSP WEB LOWER AND UPPER SIDE STA Y=526 AND Y=571 APPROX X=58 LH SIDE AT PAX CABIN (CPAX). SUMMARY OF NRC 00728: CORROSION LEVEL 2. CUSP WEB STA Y=526 AND X=58 WAS MEASURED ON LIGHTENING HOLE AND MATERIAL REMOVAL IS 0.100IN THERFORE IS WITHIN LIMITS PER B717 SRM 53-00-00-1A FIG .101 LIGHTENING HOLE AND CUSP WEB STA Y=571 APPROX X=58 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4.

Part: CUSP WEB — CRACKED (BS 715-737) · airframe 58,229 hrs · 40,792 cycles

TWO CRACKS WERE FOUND ON RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X=45 TO -X=60 IN PAX CABIN. SUMMARY OF NRC 00534: RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X= 45 TO -X=60 IN CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329432)

Part: CUSP WEB — CRACKED (BS 655) · airframe 58,229 hrs · 40,792 cycles

CRACK ON LOWER SURFACE OD CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT PAX CABIN. SUMMARY OF NRC 00591: CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329495)

Part: CUSP WEB — CRACKED (BS 657-715) · airframe 58,229 hrs · 40,792 cycles

CRACK ON CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00599: CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0325055)

Part: CUSP WEB — CRACKED (BS 225) · airframe 58,229 hrs · 40,792 cycles

CRACK ON CUSP WEB STA Y=225 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y=225 AND X=56 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-PROCEDURE 4 FIG 216. (LP #0325208)

Part: FLOOR SUPPORT — CORRODED (BS 150-200) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASSENGER CABIN (W1). SUMMARY OF NRC 00700: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASSENGER CABIN WERE REPLACED PER B717 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0323341)

Part: FLOORBEAM — CRACKED (BS 737) · airframe 58,229 hrs · 40,792 cycles

CRACK ON FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN. SUMMARY OF NRC 00438: FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN WERE REPLACED PER B717 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0323733)

Part: CUSP WEB — CORRODED (BS 471) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION CUSP WEB PREVIOUS REPAIR LOWER SIDE STA Y=471 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00598: CORROSION LEVEL 2. PREVIOUS REPAIR PART (RING DOUBLER) WAS REPLACED PER B717 SRM 53-00-55-2R-4 REPAIR 4, PAR. 5, FIGURE 216 AND 51-41-02-0G. (LP #0320091)

Part: ANGLE — DAMAGED (BS 1072 L18R) · corrosion level 2 · airframe 58,229 hrs · 40,792 cycles

CORROSION ON CLIP STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA. SUMMARY OF NRC 00381: CORROSION LEVEL 2. CLIP (GUSSET) STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #0314835)

Part: RELEASE CABLE — CORRODED (TAIL CONE) · airframe 58,229 hrs · 40,792 cycles

RUSTED CABLES AND ALL PINS ON TAILCONE RELEASE CABLE AND PULLEY MECHANISMS. ALSO BROKEN STRANDS OF CABLE AT 10 HRS POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00180: CABLES ON TAILCONE RELEASE WERE CLEANED AND LUBRICATED PER B717 AMM 20-00-02 911-802 AND NEW CABLE OF TAIL CONE RELEASE WAS REPLACED PER B717-200 AMM 53-52-01 830-802. (LP #0312628)

Part: SKIN — DELAMINATED (RT WING) · airframe 55,436 hrs · 38,342 cycles

RIGHT WING, UPPER SKIN OF INBOARD SPOILER IS DELAMINATED IN SEVERAL AREAS. REPLACED RIGHT INBOARD PANEL IAW AMM 27-60-01.

Part: SIGN — DETACHED (CABIN) · airframe 55,180 hrs · 38,116 cycles

AIRCRAFT 9536, WHEN GATE AGENT OPENED L1 DOOR EXIT SIGN FELL OFF AND CRACKED. CORRECTIVE ACTION: REINSTALLED SIGN COVER . LP 8316521

Part: NONE — NONE · airframe 55,071 hrs · 38,015 cycles

THE 1L SLIDE FELL OUT OF THE CONTAINER UPON DOOR OPENING AS THE GIRT BAR WAS CONNECTED. THE SLIDE DID NOT INFLATE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REINSTALLED THE L1 DOOR SLIDE PER WORK CARD 5211-4002. RII INSPECTION OF THE SLIDE ASSEMBLY INSTALL WAS COMPLIED WITH. [INSP STAMP DELTA QC5158). (LP #8936954)

Part: NONE — NONE · airframe 54,656 hrs · 37,627 cycles

SHIP 9536 - THE CREW SAFELY ABORTED THE TAKEOFF ROLL AT 110 KTS DUE TO A BIRD STRIKE. NO UNUSUAL VIBRATIONS, ODORS, OR NOISES. CORRECTIVE ACTION: MAINTENANCE COMPLIED WITH REQUIRED BIRD STRIKE INSPECTION, CLEANED DEBRIS FROM WINDSHIELD AREA, AND RETURNED THE AIRCRAFT TO SERVICE. (LP #9275204)

Part: NONE — NONE · airframe 54,650 hrs · 37,621 cycles

FOUND CRACK INDICATION WHILE PERFOMING BHEC IN STRAP/SKIN SPLICE ON RH VERT L/E IN 4 EA HOLES IN REPAIR AREA. REF 5330-01048-02 AD 2018-10-08. MAINTENANCE COMPLIED WITH THE SKIN REPAIR PER PRI 600805-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, AND REV 7. PRI 600805-14 REV 0-7 REPAIR INSTRUCTIONS AND ERA 600805-14 REV ORG MATCH. (LP #2330575)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,503 hrs · 34,862 cycles

CORROSION ON STRINGER 30 FROM STA 908-974. MARKED. MAINTENANCE REPLACED STRINGER SECTION PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1734931)

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 51,424 hrs · 34,798 cycles

IN THE AFT CARGO COMPARTMENT THERE IS CORROSION IN MULTIPLE LOCATIONS OF THE C-2 DOOR LOWER JAMB AREA. MAINTENANCE REPLACED THE PAN PER B717 SRM 53-20-15-2R-7 ON NON-ROUTINE CARD 104 DURING C2 MTC VISIT.

Part: COVER — MISSING (EXIT SIGN) · airframe 49,591 hrs · 33,290 cycles

THE EMERGENCY EXIT SIGN COVER IS LOOSE AT LOCATION: 6.2 INTERIOR. UPON ARRIVAL MAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN COVER WAS MISSING. THE EXIT SIGN COVER WAS REINSTALLED AND THE OPERATIONAL CHECK WAS GOOD PER AMM 25-60. (LP #1167004)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,474 hrs · 33,207 cycles

THE CEILING EMERGENCY LIGHT AT 1R DOOR IS NOT ILLUMINATING. MAINTENANCE DISCOVERED THAT NO POWER WAS GETTING TO THE LIGHT. THEY REPLACED THE BATTERY POWER SUPPLY B5- 259 PER AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #5947570 )

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 48,602 hrs · 32,659 cycles

CORROSION ON LEFT UPPER WING PLANK AT STATION XRS324 FWD OF STRINGER 5. NRC 004-0001:0514-2001/003 00003: REPAIRED PER PRI 575475-14 REV 0 AND REV 1. AND ER/A 575475-14. (LP #0978149)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 48,550 hrs · 32,619 cycles

DURING SANDING OF WING LT UPPER SURFACE CORROSION WAS FOUND APROX WING STA XRS 324.00. BLENDED CORROSION FOUND AT WING STA XRS C324.00 AT STRINGER 5 PER SRM 57-10-01-1A. WING THICKNESS MEAS AT POINT 153 PER SRM 57-10-01-1A FIG 105. MAT REMOVED MEASURED AT .039 ALLOWABLE MAT REMOVED .020 PER SRM 57-10-01-1A FIG 106. REMAINING MAT .004. AREA FOUND TO BE OUT OF LIMITS PER SRM 57-10-01-1A AND ER/A 576096-14 REV ORIG APPR DATE 05MAR19. SPECIAL FERRY PERMIT APPROVAL. ASSOCIATED ER/A 14-576096 ADDED FOR AC 9536. ER/A 576096-14 COMPLIED WITH FOR FERRY FLIGHT. REPAIRED PER PRI 575475-14 REV. O AND REV. 1. ER/A 575475 REV ORIGINAL COMPLETE. PERMANENT REPAIR COMPLIED WITH. OK TO CLOSE QC LOG. (LP #0973944)

Part: FRAME — CRACKED (BS 696) · airframe 48,447 hrs · 32,547 cycles

OVER WING FRAME CRACKED R/H STA Y=696.00. CONDITION 3, CRACK EQUAL TO OR GREATER THAN 0.125. (VISUAL INSPECTION). NRC 029-0003:5310-01436-04C/002 00043: REPLACED CRACKED FRAME REF JOB 83-0002 TASK CARD 5310-01436-03B STEPS 1-47. (LP #0938117)

Part: FRAME — CRACKED (BS 674) · airframe 48,447 hrs · 32,547 cycles

OVER WING FRAME CRACKED R/H STA Y=674.00. CONDITION 3, CRACK EQUAL TO OR GREATER THAN 0.125. (VISUAL INSPECTION). NR 029-0003:5310-01436-04C/001 00042: REPLACED CRACKED FRAME REF JOB 83-0002 TASK CARD 5310-01436-03B STEPS 1-47. (LP #0938115)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,282 hrs · 32,432 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. EXTERIOR EMERGENCY ILLUMINATION SYSTEM MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERED REQUIRED. SUSPECT POSSIBLE RELAY R2-273. FORWARD TO MEL AND PLACARD INSTALLED. MAINTENANCE REPLACED THE BATTERY PACK B5-125. REPLACED RELAY R2-273 AND INSTALLED FULLY CHARGED BATTERY REF ASM 33-51-0. RELAMPED RT SIDE BULB. OPERATIONAL CHECK WAS GOOD. MEL AND PLACARD WAS REMOVED. (LP #5096740)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 47,025 hrs · 31,590 cycles

NR 1 HOLE FROM TOP RT VERT STAB FRONT SPAR HAS CRACK INDICATION. REPAIR COMPLETE REF ER/A 570300-14AD ORIGINAL. ASSOCIATED ER/A 14-570300.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,216 hrs · 31,717 cycles

MAINTENANCE REPORTED A CRACK IN ONE OF THE RT LEADING EDGE SKIN. REPAIRED IAW ER/A 570300-14AD, REV O.

Part: SKIN — CRACKED (RT L/E) · airframe 47,216 hrs · 31,717 cycles

MAINTENANCE REPORTED A CRACK IN ONE OF THE RT LEADING EDGE SKIN ATTACH FASTENER HOLES. THE HOLE IS THE NR 1 ABOVE ZFS 52.267. REPAIRED IAW ER/A 570300-14AD, REV O.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,346 hrs · 30,412 cycles

EMERGENCY LIGHTS AT THE LT OVERWING EXIT ROW MISSING BLUE LENSES. INSTALLED IAW AMM 35-51. OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 45,278 hrs · 30,366 cycles

THE EMERGENCY LIGHT AT 19AB IS INOPERATIVE. MAINTENANCE REPLACED AND SECURED A SECTION OF EMERGENCY LIGHT STRIP IAW AMM 33-51-01. OK FOR SERVICE.

Part: SKIN — DELAMINATED (RT SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK R/H O/B SPOILER FOUND DELAMINATED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 43,435 hrs · 29,137 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 19B. REPLACED EMERGENCY FLOOR LIGHT SEAT 19B. OPS CHECK GOOD.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

LT CUSP WEB CORRODED BOTH SIDES STA 617-655. REPLACED LT CUSP WEB AT STA 617-655 IAW SRM 51-40-02 SEE 75663-0500-0047 FOR HOLD DOWN ACTUATOR. CUSP WEB P/N 8910151.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 43,336 hrs · 29,076 cycles

SEVERAL LOOSE FASTENERS WITH ELONGATED HOLES IN L/E VERTICAL WRAP AROUND SKIN PANEL ZFS 148.858. LT AND RT SIDES. REPAIRED THE SKIN PANEL IAW ER/A 553690-14 REV 0.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 43,336 hrs · 29,076 cycles

LEFT BS 1022 FRAME SHEAR TIE CRACKED ON END BETWEEN LONGERONS 16 - 17L. REPLACED THE FRAME IAW SRM 53-00-06 2, REPAIR 3.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,336 hrs · 29,076 cycles

FOUND LONGERON 17L TO BE CRACKED AT BS 1022. PERFORMED A LONGERON HAT SECTION SPLICE REPAIR IAW SRM 53-00-05 2, REPAIR 2.

Part: LONGERON — CORRODED (BS 946-974) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

CORROSION ON LONGERON 30 BS 946 - 974. REPLACED THE LONGERON FROM BS 908 - 965 IAW SRM 51-41-05, AND 51-41-02.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,339 hrs · 29,079 cycles

LONGERON 16L CRACKED AT 1022 BULKHEAD. INSTALLED REPAIR ON L16L STA 1022 IAW SRM 53-00-05 REPAIR 2 TRIMMED PYLON ANGLE TO REMOVE TRAPPED FASTENERS IAW ER/A 553686-14 REV O.

Part: FRAME — CORRODED (BS 927) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

CORROSION ON FRAME BS 927 BETWEEN LONGERONS 29L-29R. REPAIRED THE FRAME IAW SRM 53-00-06, REPAIR 2.

Part: ANGLE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

CUSP ANGLE AT THE R1 DOOR IS CORRODED. REPLACED THE ANGLE FROM BS 146 TO 239 IAW SRM 51-41-02 0G AND SRM 53-00-55 2R-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

FORWARD CABIN FLOOR SUPPORT AT STA 178, RBL 14 - RBL 32 CORRODED SEVERAL PLACES. REPLACED FORWARD FLOOR SUPPORT IAW SRM 51-41-05. DAMAGE WAS OUT OF LIMITS IAW SRM 53-00-00-1A AND 53-10-51.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 43,336 hrs · 29,076 cycles

VERTICAL STAB L/E SKIN RIGHT SIDE AT ZFS=52.267 FWD 2 ROWS OF FASTENERS BELOW SPLICE ARE PULLING THROUGH SKIN AND HAVE EVIDENCE OF FRETTING CORROSION AROUND FASTENERS. J.C. 5530-01048-01, STEP 4. REPAIRED THE VERTICAL STAB L/E SKIN IAW JC 5530-01048-01 AND SG 95550001. NO CORROSION NOTED.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 43,336 hrs · 29,076 cycles

RIGHT CUSP WEB AT BS 218 - 237 IS CRACKED. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.

Part: CUSP WEB — CORRODED (BS 851-870) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

RIGHT OTBD CUSP WEB HAS AREAS OF CORROSION FROM BS 851 - 870. BLENDED, AND FOUND OUT OF LIMITS IAW SRM 53-00-55 1A. FABRICATED A DOUBLER AND RING DOUBLER. INSTALLED IAW SRM 53-00-55 2R-4.

Part: SKIN — DAMAGED (RUDDER) · corrosion level 2 · airframe 43,336 hrs · 29,076 cycles

RUDDER LT SKIN LOWER EDGE IS DAMAGED AT MARKED LOCATION. PRIMED OUT DAMAGE FABRICATED DOUBLER .032 FILLER .050. ALODINE, PRIMED, AND TOP COAT REPAIR AND INSTALLED IAW SRM 51-70-13-2R-1-01 FIG 201 IAW PSM 900-2-4-1 NR 2 PSM 900-3-6 NR 3 IAW AMM 51-21-10 370-805.

Part: LENS — MISSING (EXIT SIGN) · airframe 42,649 hrs · 28,618 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE AFT CABIN DOOR EMERGENCY EXIT SIGN LOST THE LENS/COVER. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.

Part: ENGINE — FIRE (NR 1) · airframe 41,698 hrs · 27,837 cycles

THE CREW SAFELY ABORTED THE TAKEOFF AT LESS THAN 80 KTS DUE TO A FIRE INDICATION ON THE NR 1 ENGINE. THE FIRE WAS CONFIRMED, BUT THE CAUSE HAS NOT BEEN IDENTIFIED. MAINTENANCE HAS REPLACED THE NR 1 ENGINE.

Part: POWER SUPPLY — OVERHEATED (BEACON) · airframe 40,259 hrs · 26,745 cycles

AFTER LANDING, DURING TAXI, F/A NOTICED ACRID, ELECTRICAL ODOR BEFORE GETTING TO RAMP. STRONG ODOR, NO VISIBLE SMOKE. BOTH ENGINES & BOTH PACKS RUNNING. AT GATE AFTER SHUTDOWN WITH BOTH PACKS ON APU ODOR WAS NOTICABLE, ODOR AT OVERWING EXIT ROW. CONFIRMED PROBLEM TO BE OVERHEATED UPPER BEACON POWER SUPPLY. REPLACED POWER SUPPLY IAW AMM 33-42-13, CKS GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 39,415 hrs · 26,060 cycles

EMERGENCY LIGHT BATTERIES FAILED OPS TEST. REPLACED BOTH BATTERIES.

Part: FRAME — CRACKED (BS 696) · airframe 39,415 hrs · 26,060 cycles

OVERWING FRAME AT BS 696, LT CRACKED. REPLACED FRAME IAW AMDS 5310-01436-03A.

Part: LENS — CRACKED (CABIN) · airframe 37,332 hrs · 24,573 cycles

R1 SERVICE DOOR EMERGENCY LIGHT LENS COVER CRACKED. R & R COVER IAW AMM.

Part: LONGERON — CRACKED (NR 1 COWLING) · airframe 34,007 hrs · 22,482 cycles

NR 1 ENGINE APRON LONGERON AT AFT COWL ATTACH POINT CRACKED. REPAIRED LONGERON IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FUSELAGE SKIN CRACKED AT STA 218, LONG 7L. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FLOOR PANEL CORRODED AT STA 674, RBL 44.5. REPAIRED PANEL IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FUSELAGE EXTERNAL SKIN CORRODED BETWEEN STA 851 TO STA 870, LONG. 28R TO 30R. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FLOOR PANEL CORRODED BETWEEN STA 389 TO STA 765, RBL 44.5. REPAIRED PANEL IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FUSELAGE EXTERNAL SKIN CORRODED BETWEEN STA 851 TO 870, BETWEEN LONG 28L TO 30. REPAIRED SKIN IAW SRM.

Part: TORQUE BOX — CRACKED (L1 DOOR) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN L1 DOOR TORQUE BOX WEB CRACKED AT LONG 15L. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FLOOR PANEL CORRODED BETWEEN STA 313 TO STA 389, RBL 44.5. REPAIRED PANEL IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FRAME 965 RT SIDE LOWER SUPPORT FITTING CORRODED. R & R FITTING IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FLOOR PANEL CORRODED AT STA 361, RBL 44. REPAIRED PANEL IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

VERTICAL SUPPORT CRACKED AT STA 737, LBL 44. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

RIGHT CUSP WEB CORRODED AT STA 440. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

CENTER SECTION VERTICAL SUPPORT ANGLE CRACKED AT STA 715, RBL 44. REPAIRED ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

VERTICAL SUPPORT ANGLE CRACKED AT STA 665, RBL 22. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

SUPPORT ANGLE CRACKED AT STA 715, LBL 44. R & R ANGLE IAW SRM AND DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

RIGHT CUSP WEB CORRODED BETWEEN STA 950 TO STA 965 RIGHT SIDE. R & R WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,970 hrs · 23,050 cycles

FUSELAGE SKIN CORRODED BETWEEN STA 851 TO STA 870, BETWEEN LONG 28L TO LONG 30L. REPAIRED SKIN IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 34,007 hrs · 22,482 cycles

L1 DOOR UPPER BEAM CRACKED AFT CORNER. R & R DOUBLER IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

CUSP WEB CRACKED AT STA 674 RT. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

OVERWING MAIN FRAME CRACKED AT BS 715, RBL 65. R & R FRAME IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 223 FF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

FLOOR PANEL EDGE CORRODED AT STA 780, LBL 44.5. REPAIRED PANEL IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

LEFT CUSP CORRODED AT STA 550. R & R CUSP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

LEFT CUSP CORRODED AT STA 470. R & R CUSP IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222ABF DELAMINATED. R & R PANEL IAW SRM.

Part: DOOR — CRACKED (NLG WW) · airframe 34,007 hrs · 22,482 cycles

LEFT NLG STRUT DOOR AFT HINGE CUTOUT CRACKED. REPAIRED DOOR IAW MM.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 34,007 hrs · 22,482 cycles

LEFT WING TO BODY BONDING STRAP CRACKED. R & R STRAP IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222AHF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222GF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 22LF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222AGF DELAMINATED. R & R PANEL IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 34,007 hrs · 22,482 cycles

LEFT WING TO BODY - INBD SIDE OF INBD FLAP TRACK WEB ANGLE CRACKED. R & R BRACKET IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 221UF DELAMINATED. R & R PANEL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

LEFT WING TO FUSELAGE FITTING CRACKED AT STA 661, LONG 22L. R & R FITTING IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222JF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222FF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222AVF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

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

Part: PANEL — CRACKED (RT WING) · airframe 34,007 hrs · 22,482 cycles

RT WING TO BODY PANEL NR 160 BR CRACKED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL 222ACF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222AMF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 221WF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222AAF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL 222BF DELAMINATED. R & R PANEL IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

AFT ACCESSORY COMPARTMENT CRACKED AT STA 1133, BETWEEN LONG 1L AND 2L. R & R SHEAR TIE IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222ATF DELAMINATED. R & R PANEL IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 34,007 hrs · 22,482 cycles

RIGHT WING TO BODY BONDING STRAP LOWER CRACKED. R & R STRAP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,007 hrs · 22,482 cycles

SHEAR TIE CRACKED AT STA 1161, LONG 2R. R & R SHEAR TIE IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL NR 222PF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,007 hrs · 22,482 cycles

MAIN CABIN FLOOR PANEL 223DF DELAMINATED. R & R PANEL IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 34,150 hrs · 22,562 cycles

OVERHEAD EXIT SIGN BUSINESS CLASS LOOSE. RE-ATTACHED AND SECURED OVERHEAD EXIT SIGN PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,838 hrs · 21,738 cycles

RIGHT EEPLS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,838 hrs · 21,738 cycles

LEFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACKS PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 32,827 hrs · 21,732 cycles

OVERHEAD CEILING EMERGENCY EXIT SIGN WIRE LOOSE AT ROW 1. SECURED SIGN IAW AMM.

Part: TRIM PANEL — CORRODED (CABIN)

R1 DOOR CABIN FLOOR TRIM PANEL AND GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED FLOOR TRIM PANEL AND GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-40-08 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 196, LBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 53-10-51, 51-40-08 AND 51-41-02.

Part: DUMMY RAIL — CORRODED (FUSELAGE)

CABIN FALSE TRACK, STA 148 TO 200, RBL 9, CORROSION. ACCOMPLISHED FALSE TRACK REPLACEMENT PER B717 SRM 53-10-51, 51-40-08 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, LBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 53-10-51, 51-40-08 AND 51-10-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 195 TO 200, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 53-10-51 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 160, BL 0 TO LBL 9, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 53-10-07, 51-40-08, 51-10-04 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, BL 0 TO RBL 37, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 51-40-08 AND 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 51-41-05, 53-10-51, 51-40-08 AND 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 237, RBL 24, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 11, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-40-08, 53-10-51, 51-10-04 AND 51-10-00.

Part: DUMMY RAIL — CORRODED (FUSELAGE)

CABIN FALSE TRACK, STA 200 TO 148, LBL 9, CORROSION. ACCOMPLISHED FALSE TRACK REPLACEMENT PER B717 SRM 51-10-04, 53-10-51, 53-00-00, 51-40-08 AND 51-40-02.

Part: FLOOR PANEL — CORRODED (CABIN)

CABIN FLOOR PANEL, STA 157 TO 200, LBL 44, CORROSION. ACCOMPLISHED FLOOR PANEL FILLER AND DOUBLER REPAIR PER B717 SRM 51-70-10 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02, 53-10-01 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 157 TO 200, RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 53-10-51 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 21, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 53-10-51 AND 51-40-08.

Part: LANYARD — DETACHED (GIRT BAR)

FORWARD ENTRY DOOR SLIDE GIRT CABLE DETACHED. REPLACED GIRT BAR LANYARD AT FWD ENTRY DOOR AMM 25-61.

Part: RELAY — MALFUNCTIONED (ELECTRICAL SYS)

BUS DC EMERGENCY OFF ALERT. REMOVED AND REPLACED EMERGENCY POWER RELAY AND EMERGENCY DC BUS SENSE RELAY. OPS CHECK GOOD REF MM24-24.

Part: STRINGER — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT STA 927-974 STRINGER 30 CORRODED BEYOND LIMITS. CUT OUT CORRODED STRINGER AND INSTALLED NEW STRINGER SPLICE PER B717 SRM 53-00-05 REPAIR 2.

Part: LONGERON — CRACKED (FUSELAGE)

FUSELAGE TAIL SECTION FS 1124 CRACK INDICATED AT THE END OF LONG 2R. CUT OUT DAMAGED SECTION OF LONG 2R FROM STA 1113 TO 1127 AND INSTALLED NEW SECTION OF LONGERON AND SPLICE REPAIR PER B717 SRM 53-00-05 REPAIR 2 FIG 201.

Part: FRAME — DAMAGED (BS 1178)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.

Part: FRAME — DAMAGED (BS 1178)

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: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY BATTERY PACK FOR 1ST ROW, RT SIDE (OVERHEAD BIN) NEEDS REPLACED. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY B1-118 AND OPS CHECKED REF AMM 33-00.

Part: O-RING — DEFECTIVE (RT SPOILER ACT)

HYDRAULIC RIGHT QUANTITY LOW ANNUNCIATION IN-FLIGHT. FOLLOWED QRH. FLUID LEVEL AT 3.9 WHEN PUMPS SHUT OFF. INCREASED AFTER HYDRAULIC PUMPS SHUT OFF. FOUND HYDRAULIC LEAK AT RIGHT O/B SPOILER ACT PRESSURE FITTING. REMOVED AND REPLACED O-RING AT PRESSURE FITTING. REF MM 27-67 LEAK AND OPS CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN)

CHECKED OPERATIONAL OF THE AIRCRAFT EMERGENCY LIGHTING SYSTEM, PER SERVICE CHECK. EMERGENCY EXIT SIGNS ABOVE EXIT DOORS AT ROW 22 FED AND 22 CA DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY FOR EMERGENCY EXIT SIGNS ABOVE EXIT DOORS 22 FED AND 22 CA. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEMS. OPERATIONAL TEST GOOD, IAW BOEING 717 AMM 33-51. NO DEFECTS NOTED AT THIS TIME.