N896AT

Part: COMPUTER — FAULTED (FLT CONTROL) · airframe 51,648 hrs · 37,448 cycles

SHIP 9556 -MISC/DE- THE FLIGHT CREW NOTICED THAT THE AIRCRAFT WAS FLYING UNCOORDINATED DURING THE DESCENT AND THEN THEY RECEIVED "RUDDER RESTRICTED" MESSAGE ON APPROACH. AN EMERGENCY WAS THEN DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE PERFORMED ALL ASSOCIATED NO GO ODI PREVENTION TASKS WITH NO FINDINGS. REPLACED FCC #2 DUE TO AN AUTO FLIGHT SYSTEM FAULT. (LP #6384075)

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 51,578 hrs · 37,396 cycles

-AD- CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING. SUMMARY OF NRC 0015: CORROSION LEVEL 2. CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING WAS REAPAIRED PER PRI 623423-14 REV 2 AND ERA 623423-14AD REV ORIGINAL. ASSOCIATED ER/A 14-623423 ADDED FOR AC 9556. (LP #0764901)

Part: SKIN — NICKED (ZONE 100) · airframe 51,578 hrs · 37,396 cycles

NICK BETWEEN STA 994 AND STGR 24-26 RH AT EXTERNAL FUSELAGE SKIN. SUMMARY OF NRC 00007: EXTERNAL SKIN BETWEEN STA 994 AND STGR 24-26 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12, REPAIR 12. PERFORM INITIAL GENERAL VISUAL INSPECTION AT 8,000 CYCLES AND THEN REPETITIVE EVERY 8,000 CYCLES PER B717-200 SRM 53-20-15-2R PROCEDURE 12, REPAIR 12 PAR 7. (LP #0759277)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,924 hrs · 35,075 cycles

ROW 21 BOTH L/H AND R/H OVERWING EXIT SIGNS (LOWER) ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-51 AT LOCATION B5-1119. OPERATIONAL CHECK WAS GOOD. (LP #4615512)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,921 hrs · 34,214 cycles

THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS DAMAGED AT LOCATION 603. MAINTENANCE RESECURED THE EMERGENCY EXIT COVER LIGHT LENS OVER AISLE AT ROW 20 AS REQUIRED. NO DEFECTS NOTED. (LP #2776663)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 47,293 hrs · 33,673 cycles

CORROSION ON RH TIE TRACK UPPER SURFACES FROM STA Y=900 TO Y=954. SUMMARY OF NRC 0556: CORROSION LEVEL 2. TIE TRACK RH ON STA Y=900 TO Y=954 WAS REPLACED PER B717-200 SRM 51-41-08-0G, 51-41-02 -0G, AND 51-41-01-0G. (LP #2620761)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 47,293 hrs · 33,673 cycles

SECONDARY IN REFERENCE NRC 496: CORROSION ON LH TIE TRACK UPPER SURFACES FRON STA Y=900 TO Y=1028. SUMMARY OF NRC 00555: CORROSION LEVEL 2. TIE TRACK SECTION FROM Y=900 TO Y=1028 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2620158)

Part: TAB — DEBONDED (LT AILERON) · airframe 47,293 hrs · 33,673 cycles

IN REF TO NRC 00041, DISBONDED AREA WAS FOUND ON DENT #1 WITH A MEASURE OF 0.500 IN LENGTH X 0.500 IN WIDTH AT AILERON CONTROL TAB OUTBOARD UPPER FACE AT LH WING. SUMMARY OF NRC 00195: AILERON CONTROL TAB OUTBOARD UPPER FACE AT LH WING WAS REPAIRED AND WEIGHT AND BALACE STAYING WITHIN LIMITS (WEIGHT 5.68) PER B717-200 SRM 51-70-02-2R PROCEDURE 3 REPAIR 3 AND B-717-200 SRM 51-60-01-0G. CORRECTED SUMMARY OF NRC 00195: AILERON TRIM / TAB OUTBOARD UPPER FACE AT LH WING WAS REPAIRED AND WEIGHT AND BALANCE STAYING WITHIN LIMITS (WEIGHT 5.68) PER B717-200 SRM 51-70-02-2R PROCEDURE 3 REPAIR 3 AND B-717-200 SRM 51-60-01-0G. (LP #2603921)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 47,293 hrs · 33,673 cycles

CORROSION ON COUNTERSINK HOLE OF LH WING ACCESS PLATE NBR 520CB REF NRC 417. SUMMARY NRC 00506: CORROSION LEVEL 2. FUEL ACCESS PLATE NBR 520CB AT LH WING WAS REPAIRED PER B717-200 SRM 57-10- 01-2R PROCEDURE 2 PAR. 5 CONDITION II. (LP #2591579)

Part: BEAM — CRACKED · airframe 47,293 hrs · 33,673 cycles

CRACK ON BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR. SUMMARY OF NRC 00106: CRACKED BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R-13. (LP #2590277)

Part: PAN — CRACKED (BS 197) · airframe 47,293 hrs · 33,673 cycles

CRACK ON UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR. UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR WAS REPAIRED IAW SRM 52-10-02- 2R PROCEDURE 3 REPAIR 3.

Part: BEAM — CRACKED · airframe 47,293 hrs · 33,673 cycles

CRACK ON BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR. BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-02-2R-7.

Part: CUSP WEB — CRACKED (BS 656) · airframe 47,293 hrs · 33,673 cycles

DURING REMOVAL OF RH CUSP WEB, DVI WAS PERFORMED AND 3 CRACKS WERE FOUND (EAS). A CRACK AT HOLE OF FASTENER AT CUSP WEB STA 656, A CRACK ON EDGE OF CUSP WEB STA 657, AND CRACK AT HOLE OF FASTENER AT CUSP WEB STA 694 PAX CABIN FLOOR. CUSP WEB BS 656 TO 657 WAS REPAIRED IAW SRM 53-00-55-2R FIG 203. (LP #2587175)

Part: CUSP WEB — CRACKED (BS 229 RBL46) · airframe 47,293 hrs · 33,673 cycles

CRACK ON CUSP WEB ON STA 229 AT BL 46R AT PAX CABIN. SUMMARY OF NRC 00258: CUSP WEB ON STA 229 AT BL 46R WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP #2582373)

Part: DIAPHRAGM — CORRODED (BS 187-192 RBL44) · corrosion level 2 · airframe 47,293 hrs · 33,673 cycles

CORROSION ON DIAPHRAGM STA=192 AND STA=187 RBL=44 ARE OUT OF LIMITS IN REF NRC 00325. SUMMARY OF NRC 00451: LEVEL CORROSION 2. DIAPHRAGM STA=192 AND STA =187 RBL=44 WAS REPAIRED PER B717-200 SRM 53-00-00-1A PAR 4.B.(2). FIG. 102.

Part: NONE — NONE · airframe 46,695 hrs · 33,142 cycles

DURING A SERVICE CHECK, THE AFT GROUP OF EMERGENCY LIGHTS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY B5-260 REF B717 AMM 33-51. THEY ALSO REPLACED THE MIDDLE EMERGENCY LIGHT ON THE TAILCONE CATWALK REF B717 AMM 33-51. (LP #8940332)

Part: NONE — NONE · airframe 46,695 hrs · 33,142 cycles

THE EMERGENCY LIGHTS BATTERY WAS DISCOVERED TO BE DISCHARGED. MAINTENANCE REPLACED THE POWER SUPPLY AT THE EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. AIRCRAFT READY FOR SERVICE. TESTS OK. (LP #8940315)

Part: NONE — NONE · airframe 45,553 hrs · 32,092 cycles

MAINTENANCE FOUND THAT THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE DURING THE SERVICE CHECK. TROUBLE SHOOTING PER WD 33-51-12 FOUND THE EMERGENCY LIGHT BATTERY PACK WAS INOPERATIVE. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8919523)

Part: NONE — NONE · airframe 45,222 hrs · 31,803 cycles

CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-22-001 REV. 3 AND ER/A 596558-14AD SECTION I. PERMANENT REPAIR REPAIR APPROVAL IS LIMITED TO 60,000 FLIGHT CYCLES. DAMAGE TOLERANCE ANALYSIS (DTA) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93 ON REF 2094374 ACCOMPLISH THE SECTION II: REPETITIVE INSPECTIONS EVERY 24 MONTHS AFTER 21JAN2022. ON REF LOG 2094384 SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING ASSOCIATED ER/A 14-596558 ADDED FOR AC 9556. (LP #2094621)

Part: NONE — NONE · corrosion level 2 · airframe 45,206 hrs · 31,789 cycles

CORROSION ON PAN BTW STA Y=954 TO Y=994 AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 00008: CORROSION LEVEL 2, PAN BTW STA Y=954 TO Y= 994 AT AFT CARGO DOOR JAMB WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 7. (LP #2088850)

Part: NONE — NONE · airframe 45,206 hrs · 31,789 cycles

CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L. SUMMARY OF NRC 00056: CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L WAS REPAIRED PER B717-200 SRM 53-03-01-2R, REPAIR 1 STEP 6 PAR G, FIG 20. REQUIRES VISUAL REPETITIVE (8,000 CYCLES) INSPECTION IN REF B717 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1. STEP 7.A. (LP #2087613)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,898 hrs · 30,595 cycles

FOUND EMERGENCY LIGHT BATTERY INOPERATIVE IN FIRST CLASS. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHTS BATTERIES (2) REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7462600)

Part: SLIDING WINDOW — FAILED (COCKPIT RIGHT) · airframe 43,694 hrs · 30,444 cycles

WHILE ATTEMPTING TO CLEAN THE WINDOWS, MAINTENANCE DETERMINED THAT THE COPILOTS SLIDING WINDOW WILL NOT UNLOCK AND OPEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE UPPER RETAINER SPRING WAS ADJUSTED AND THE WINDOW NOW OPENS AND CLOSES NORMALLY. (LP #7593792)

Part: COVER — MISSING (LT NACELLE) · airframe 43,138 hrs · 30,009 cycles

THE INBOARD COWL HOIST COVER IS MISSING ON LEFT ENGINE. CONTRACT MAINTENANCE FORWARDED THE DISCREPANCY TO NEF 71- 10-02. COWL HOIST SCREW COULD NOT BE INSTALLED, PER AIPC 71-11-05-10 ITEM 95. OK TO CONTINUE. ATL 22JAN21 THE NR 1 ENGINE WAS CHANGED WITH A NEW FAN COWL. ALL HOIST SCREW PLUGS INSTALLED ON NEW COWL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,586 hrs · 28,651 cycles

THE EXTERIOR EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT IS SHUTDOWN. MAINTENANCE REPLACED THE POWER SUPPLY AND RELAY PER B717 AMM 33-51. THE OPERATIONAL CHGECK WAS GOOD. (LP #1511748)

Part: WINDSHIELD WIPER — BROKEN (CAPTAIN'S SIDE) · airframe 41,498 hrs · 28,573 cycles

THE CAPTAIN SIDE WIPER ARM BROKE OFF ON TOUCH DOWN (22L) AT JFK. MAINTENANCE REPLACED THE CAPTAIN SIDE WINDSHIELD WIPER IN REF B717 AMM 30-43. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #6954789)

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 40,832 hrs · 28,081 cycles

KEVLAR RELEASE CABLE IS WORN IN THE TAILCONE. REMOVED WORN KEVLAR RELEASE CABLE, INSTALLED NEW KEVLAR RELEASE CABLE, WITH COMPLETION OF KEVLAR CABLE ON AMDS CARD #5352-2001. (LP #1343143)

Part: BRACKET — WORN (TAILCONE) · airframe 40,832 hrs · 28,081 cycles

THE TAILCONE KEVLAR CABLE SPRING BRACKET ON THE RIGHT SIDE IS WORN. MAINTENANCE REPLACED THE TAIL CONE KEVLAR CABLE SPRING BRACKET WITH A NEW BRACKET. (LP #1343012)

Part: LIGHT — INOPERATIVE (CATWALK) · airframe 40,475 hrs · 27,794 cycles

WHILE PERFORMING SERVICE CHECK FOUND 2ND FROM FORWARD EMERGENCY ESCAPE PATH LIGHT ABOVE TAIL CATWALK INOPERATIVE. MAINTENANCE REPAIRED THE WIRE PER SWPM 20 AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9875618)

Part: DOOR — MISSING (POTABLE WATER) · airframe 40,228 hrs · 27,593 cycles

POTABLE WATER DOOR MISSING. REF LP 5476442. (LP #5476460)

Part: SPOILER — DELAMINATED (LT WING)

DELAMINATED LT INBOARD SPOILER.

Part: SKIN — DEBONDED (SPOILER) · airframe 36,610 hrs · 25,090 cycles

DISBONDED AREA OF 1.5"X 1.5" ON RH INBD SPOILER LWR SURFACE. THE SPOILER LOWER SURFACE WAS REPAIRED IAW SRM 51-70-02-2R-3.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 36,614 hrs · 25,092 cycles

THE OUT OF PLACE INFLATION CABLE PIN WAS ALSO MISSING VALVE LOCK PIN ON L1 DOOR SLIDE. THE DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-61-01.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 36,610 hrs · 25,090 cycles

DISBONDED AREA OF 2"X2" ON RT AFT MOVEABLE VANE LOWER SURFACE. THE VANE LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4, FIGURE 201.

Part: FRAME — CRACKED (BS 1225) · airframe 36,606 hrs · 25,088 cycles

CRACKED FRAME, BS 1225, BETWEEN 6 AND 7 HRS. THE FRAME WAS REPLACED IAW SRM 51-41-02 AND 51-40-08.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 36,606 hrs · 25,088 cycles

CRACKED CHANNELS OF FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187. PERMANENT REPAIR. FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187 WERE REPAIRED PER SRM 53-20-50-2R FIG 102. INSPECTION WAS ACCOMPLISHED ON FLOORS PANELS 222AFF AND P/N 9952521U187. NO CRACKS WERE FOUND AFTER STOP DRILLED PER SRM 53-20-50-2R-5, FIG 201, GENERAL NOTES, ITEM 25 AND NDT SPM PART 6 06-10-01.001.

Part: WIRE — SHORTED (SLAT SYSTEM) · airframe 36,511 hrs · 25,017 cycles

DURING SLAT RETRACTION, AFTER TAKEOFF RECEIVED A PSEU FAIL CAUTION INDICATION. DURING APPROACH, EXTENSION OF SLATS, DOWN ARROW STAYED ON, THOUGH INTERMITTENT. PERFORMED A NO FLAP, NO SLAT LANDING IAW QRH. REPLACED THE LT SLAT A SENSOR D1-65 IAW AMM 27-84 WDM 27-84-00. FOUND WIRE 9506-22-20RD HAD SHORTED TO GROUND BETWEEN P1 6005 AND D1-65. REPLACED THE WIRES 9506-22-20RD AND 9506-22-02BL IAW SWPM 20-10-03 20-00-09. REPLACED THE PSEU IAW AMM 32-61. PERFORMED A FUNCTIONAL TEST OF THE SLAT SYSTEM IAW AMM 27-80. TESTED OK. PERFORMED AN OPERATIONAL SLAT SENSOR TEST IAW AMM 27-84, NO FAULTS.

Part: FMS — MALFUNCTIONED · airframe 35,953 hrs · 24,663 cycles

THE CREW DECLARED AN EMERGENCY ON APPROACH AFTER THE LOSS OF FMS GUIDED FLIGHT PLAN. MAINTENANCE FOUND BOTH VIA NR 1 & 2 DATA BUSS FAULT CODES 344343 AND 344344. REPLACED BOTH VIA NR 1 AND 2 IN ACCORDANCE WITH THE AMM. ALL TESTS NORMAL AND THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: ENGINE — OVERHEATED (LEFT) · airframe 33,506 hrs · 22,988 cycles

THE CREW DIVERTED, FOLLOWING AN OVERHEAT OF THE LEFT ENGINE BEARING AND ASSOCIATED ROLLBACK. THE ENGINE WAS REPLACED.

Part: FUEL TANK — CORRODED (BS 706) · airframe 31,652 hrs · 21,539 cycles

LEFT CTR WING TANK UPPER SURFACE, BS 706 SKIN EXFOLIATED. REPAIRED IAW PRI 543588-14, REV 3 AND ER/A 543588, REV A.

Part: CUSP WEB — DAMAGED (BS 157-1002) · airframe 31,652 hrs · 21,539 cycles

LT CUSP WEB HAS MULTIPLE DEFECTS FROM BS 157 TO BS 1022. REPAIRED MULTIPLE DEFECTS IN LT CUSP WEB FROM BS 157 TO BS 1022 IAW SRM 53-00-55, REPAIR 4, DEPTH GAUGE USED, SN ABXF593.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,418 hrs · 20,517 cycles

LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED OVERWING EMERGENCY EXIT LIGHT BATTERY.

Part: SPRING — OUT OF ADJUST (NLG) · airframe 29,991 hrs · 20,114 cycles

DECLARED AN EMERGENCY BECAUSE THE NOSE GEAR DID NOT EXTEND USING NORMAL PROCEDURES. THE ALTERNATE GEAR EXTENSION WAS SUCCESSFUL AND THE FLIGHT CREW HAD A 3 GREEN INDICATIONS PRIOR TO AN UNEVENTFUL LANDING. THE ACFT WAS MAINTENANCE FERRIED FOR REPAIR. MAINTENANCE PERSONNEL PERFORMED MULTIPLE GEAR SWINGS WITH NO FAULTS NOTED, HOWEVER, THE PROXIMITY SWITCH ELECTRONICS UNIT, PSEU, FAULTED THE NOSE DOWNLOCK SENSOR B AT THE TIME OF THE INCIDENT. THE LANDING GEAR CONTROL VALVE, BUNGEE CYCLINDER AND RETRACT ACTUATOR WERE ALL REPLACED WITH NO POSITIVE EFFECT. THE OVERCENTER PIN INSTALLATION APPEARED INCORRECT. THE INSTALLATION WAS CORRECTED AND THE OVERCENTER SPRINGS WERE ADJUSTED AS WELL AS THE VERIFYING THE PROPER GAP DIMENSION OF THE DOWN SENSOR B. NUMEROUS GEAR SWINGS WERE PERFORMED WITH NO SUBSEQUENT FAULTS. THE PSEU WAS ALSO REPLACED AS A PRECAUTION, LP 7240019. THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,841 hrs · 19,989 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS ABOVE FWD F/A SEAT AND CEILING WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AMM 33-51 AND CHECKS WERE GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 29,404 hrs · 19,651 cycles

DURING LANDING GEAR EXTENSION, RT HYD QUANTITY LOW MESSAGE DISPLAYED. QUANTITY OF RIGHT HYD SYSTEM WAS INDICATING 3.5 AND HELD THERE WITH 3,000 PSI PRESSURE. DECLARED AN EMERGENCY, LANDED UNEVENTFULLY AND TAXIED NORNALLY TO THE GATE. MAINTENANCE DISCOVERED NO LEAKS, BUT SERVICED AND BLED THE SYSTEM, JACKED THE ACFT AND PERFORMED NUMEROUS LANDING GEAR RETRACTION & EXTENTION CYCLES AND SYSTEM CHECKED INCLUDING ENGINE RUNS WITH NO LEAKS NOTED. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (BS 715) · airframe 29,365 hrs · 19,621 cycles

FOUND LT OVERWING FRAME STA 715 HAS CRACK INDICATION THE LENGTH IS GREATER THAN .125. VERIFIED CRACK IAW NDT SPM 06-10-01.001 WIP QC1965. REPLACED LT STA 715 OVERWING FRAME IAW WC 5310-01436-03A. LP 1852707.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,567 hrs · 18,970 cycles

DURING CABIN CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE IN FWD GALLEY AND FWD AISLE CEILING PANEL. FOUND BATTERY PACK AT B5-259 POWER SUPPLY AT FAULT. REPLACED BATTERY PACK IAW AMM 33-51. OPS CKS NORMAL IAW AMM 33-51.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (NLG) · airframe 28,338 hrs · 18,778 cycles

DURING APPROACH, CREW SELECTED GEAR DOWN AND RECEIVED RED NLG "UNSAFE" INDICATION WITH LT MAIN GEAR & RT MAIN GEAR INDICATING SAFE. ACCOMPLISHED ALTERNATE GEAR EXTENSION AND NLG EXTENDED. ACFT WAS FERRIED WITH GEAR EXTENDED AND PINNED. AFTER JACKING ACFT, GEAR SWING AND INDICATIONS WERE NORMAL. ADJUSTED THE RT SIDE DOWN SENSOR WHICH WAS FOUND OUT OF ADJUSTMENT. THE NOSE GEAR STRUT WAS SERVICED AND THE BUNGEE CYLINDER WAS REPLACED AS A PRECAUTION. SUBSEQUENT GEAR SWINGS WERE ALL GOOD DURING FUNCTIONAL CHECK. THE ACFT HAS RETURNED TO SERVICE.

Part: COVER — MISSING (CABIN) · airframe 27,155 hrs · 17,720 cycles

TAIL CONE COMPARTMENT EMERGENCY EXIT SLIDE LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 27,155 hrs · 17,720 cycles

TAIL CONE COMPARTMENT EMERGENCY EXIT LIGHT ABOVE SLIDE MISSING LENS. INSTALLED LENS IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 27,155 hrs · 17,720 cycles

R1 DOOR RT AFT EXIT SIGN CRACKED. R & R SIGN IAW WDM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,814 hrs · 17,499 cycles

FWD EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 26,814 hrs · 17,499 cycles

R1 DOOR LOWER FLOOR STRUCTURE WEB CRACKED AT BS195, LBL 52.35. REPAIRED WEB IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,814 hrs · 17,499 cycles

LT HAND AFT LAVATORY EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 26,814 hrs · 17,499 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 26,814 hrs · 17,499 cycles

RT CUSP WEB CORRODED AT BS 190. R & R CUSP WEB IAW SRM & DRAWING.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 26,264 hrs · 17,158 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE IAW AMM. R&R DOOR L1 DOOR SLIDE IAW AMM 25-61-01

Part: LANDING GEAR — FAULTY (NLG) · airframe 25,871 hrs · 16,905 cycles

HAD TO EXTEND NOSE GEAR MANUALLY. STOWED EMERGENCY EXTEND HANDLE FOR NORMAL OPERATIONS. NOTICED GEAR HANDLE EXTENDED DURING CRUISE. REPAIRED NOSE LANDING GEAR IAW W/O 286867.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,506 hrs · 16,093 cycles

EMERGENCY LIGHTS ROW 1, 2, 3, AND 10 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY PER AMM.

Part: LIGHT — MISSING (CABIN) · airframe 23,082 hrs · 15,173 cycles

EEPLS BULBS MISSING AT ROW 2. INSTALLED BULBS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,082 hrs · 15,173 cycles

FRAME CORRODED AT BS 908, BETWEEN STR 26L TO STR 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,082 hrs · 15,173 cycles

FRAME CORRODED AT BS 974, BETWEEN STR 29R TO STR 29L. REPAIRED FRAME IAW SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 23,520 hrs · 15,458 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: STRIP — LOOSE (TAIL CONE) · airframe 22,893 hrs · 15,054 cycles

TAIL CONE EMERGENCY RELEASE COVER PLASTIC STRIP LOOSE. SECURED PLASTIC STRIP PER MM.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 22,466 hrs · 14,769 cycles

AFT F/A'S FLASHLIGHT INOP. RESEATED FLASHLIGHT PER MM. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT)

RT ENG FAILURE ON TAKEOFF AT 300 FT. REMOVED AND REPLACED RT ENG PER TASK CARD 603.

Part: SLIDE — DISLODGED (L1 DOOR)

STATION REPORTED L-1 DOOR SLIDE PACK DISLODGED. RE-INSPECTED L-1 DOOR PER MM 25-61-02 C/W STW 500591.

Part: LONGERON CLIP — SHEARED (FUSELAGE)

AFT ACCESSORY COMPARTMENT LONGERON CLIP, STA 1144, LONG L2R, SHEARED. ACCOMPLISHED LONGERON CLIP REPLACEMENT PER EA 17-53-02938IR.

Part: LONGERON CLIP — SHEARED (FUSELAGE)

AFT ACCESSORY COMPARTMENT LONGERON CLIP, STA 1144, LONG L2L, SHEARED. ACCOMPLISHED LONGERON CLIP REPLACEMENT PER EA 17-53-02937IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER CABIN FLOOR SUPPORT, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (FUSELAGE)

AFT ACCESSORY COMP INTERNAL FUSELAGE AFT CANTED STA 1200.019 L SIDE UPPER CORNER HAS CRACK. DRILLED STOP HOLE ON END OF CRACK PER REF BOEING SB 717-53-0006 CONDITION 3 OPTION 1.

Part: MEMBRANE — CORRODED (FUSELAGE)

UPPER CABIN SUBFLOOR CORRODED AS SEEN FROM E&E COMPARTMENT. CUT OUT DIMENSION 40" X 18" STA 160 TO STA 200 AND REPLACED SUBFLOOR (WEB) PER SRM 51-41-02 & 51-70-10 MATERIAL USED 7075 T6 .032 AND 2024 T3 .040.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: PANEL — CRACKED (FUSELAGE)

AFT ACCESSORY COMPARTMENT INTERNAL FUSELAGE AFT CANTED STA 1200.019 RT SIDE UPPER CORNER OF VENT BOX PANEL, PREVIOUS SHEETMETAL REPAIR DOUBLER HAS CRACK. REMOVED DAMAGE REPAIR DOUBLER, FABRICATED NEW DOUBLER REPAIR. MATERIAL USED .040 7075 T6 PO 1075312 AND INSTALLED PER REF SRM 51-20-09 AND 51-41-02.

Part: COWLING — CRACKED (RT ENGINE)

RT ENGINE UPPER COWLING 2ND HINGE CUT OUT CRACKED ON APRON SIDE. INSTALLED DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHT IN FORWARD GALLEY AND SEAT ROWS 1, 2, 3 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY LOCATED AT BS-118, STATION 342R. OPS CHECK GOOD.

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

MULTIPLE COMPRESSOR STALLS ON RIGHT ENGINE ON CLIMBOUT (FL200-220). N1, TGT, AND N2 INDICATIONS NORMAL. FOUND DAMAGE ON STAGES 3 & 4 OF HPC. REMOVED AND REPLACED NR 2 ENGINE PER TASK CARD 603.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY EXIT LIGHT ABOVE REAR EMERGENCY EXIT WAS ILLUMINATED IN FLIGHT. ALL OTHER SIGNS WORKED NORMALLY. FOUND REAR EMERGENCY LIGHT AT EXIT HAD BATTERY PACK CONNECTOR LOOSE. SECURED CONNECTOR. OP CHECK GOOD PER AMM 33-51-00.

Part: POWER SUPPLY — ACTIVATED (CABIN)

EMERGENCY EXIT LIGHT INOP AT AFT DOOR. REPLACED EMERGENCY LIGHT POWER SUPPLY REF AMM 33-51-03 (B5-260 LOCATION).

Part: LIGHT — INTERMITTENT (COCKPIT)

RT MAIN GEAR INDICATING LIGHT INTERMITTENT. T/S PER FIM 32-60-801. NO CURRENT OR STORED RT GEAR FAULTS. R-T-S TEST PASS. ALL RT SENSOR % IN RANGE AND SENSORS OK. INDUCTANCE DATA OK. DOWNLOCK SENSOR TARGET GAP IN LIMITS. JACKED A/C PER AMM 07-11. SWUNG GEAR NUMEROUS TIMES PER AMM 32-30. NO FAULTS. OP CK GOOD.

Part: PAN — CORRODED (AFT CARGO BAY)

AFT CARGO COMPARTMENT DOOR CUTOUT LOWER JAMB CORRODED. INSTALLED AFT CARGO CUTOUT LOWER JAMB PAN AND SPLICE REPAIR PER B717 SRM 53-20-15 F 201.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT DISARM WITH SWITCH IN OFF POSITION. OVERWING EXIT LIGHTS WILL COME ON WITH ALL POWER OFF. DISCONNECTED EMERGENCY BATTERY PACK IN AFT CARGO CEILING PANEL, REMOVED AND REPLACED OVERWING EVACUATION EMERGENCY BATTERY POWER SUPPLY PER M/M B-717 M/M REF 33-51-06. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING EMERGENCY LIGHTS WILL NOT STAY OFF. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK. OP'S CHECK GOOD. REF AMM 33-50.

Part: SLIDE — LOW PRESSURE (R1 DOOR)

R1 DOOR SLIDE PACK QUESTIONABLE PRESSURE. REPLACED R1 DOOR EVAC SLIDE ASSY PER AMM 25-60.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT ABOVE TAIL CONE ILLUMINATES DURING TAKEOFF. LIGHT IN CEILING ON AIRCRAFT RIGHT (LOCATED IN TAIL CONE) ALSO ILLUMINATED. BOTH LIGHTS EXTINGUISHED IN FLIGHT AFTER 15 MINUTES. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. REF M/M 33-51-00.

Part: SKIN — CRACKED (FUSELAGE)

RIGHT DOUBLER REPAIR CRACKED. INSTALLED DOUBLER REPAIR AT AFT FUSELAGE RIGHT SIDE VENT BOX IAW AIRTRAN T/C 17-5320-2023 FIG 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING THE OPERATIONAL TEST OF EMERGENCY EVACUATION LIGHT SYSTEM IAW SERVICE CHECK WORK CARD 604, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FROM ROW 10 FORWARD. REPLACED BATTERY PACK B5-118, SYSTEM OPS CHECKED NORMAL