N905NN

Part: PIN — LOOSE (ZONE 800) · airframe 36,864 hrs · 15,972 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT THE PIN FROM THE GIRT BAR ON MAIN ENTRY DOOR CAME LOOSE WHEN OPENING DOOR AT GATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 08L22125001 IN ORDER TO PREVENT ANY ACCIDENTAL DEPLOYMENTS OR OTHER ISSUES.

Part: SLIDE — DEPLOYED (ZONE 800) · airframe 36,845 hrs · 15,963 cycles

AIRCRAFT WAS GROUNDED: AFTER PARKING AT GATE FLIGHT ATTENDANT 1 REPORTED AN ISSUE WITH THE GIRT BAR AND L1 DOOR WOULD NOT OPEN RESULTING IN A PARTIAL SLIDE DEPLOYMENT. MAINTENANCE INSPECTED THE DOOR AREA AND SLIDE PACK COVER FOR DAMAGE WITH NO ISSUES NOTED. MMAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 08L22125001.

Part: TRACK — WORN (ZONE 300) · airframe 34,982 hrs · 15,102 cycles

AIRCRAFT IN BASE MAINTENANCE: STABILIZER TORSION BOX COMPARTMENT, LEFT HAND FORWARD SPAR SLIDING PANEL GUIDE TRACK (FUSELAGE BODY TO LEFT HAND HORIZONTAL STABILIZER SLIDING SEAL STRUCTURE) AT STA 1095, WL 278, WORN. REPAIRED TRACK PER EA 358016.

Part: SLIDE — FRAYED (ZONE 800) · airframe 34,739 hrs · 14,978 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: THE R1 DOOR SLIDE HAS A FRAYED APRON. MAINTENANCE INSTALLED A NEW SERVICEABLE R1 DOOR SLIDE PACK IAW AMM 25-66-01.

Part: SLIDE RAFT — DAMAGED (ZONE 800) · airframe 34,740 hrs · 14,987 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: L1 FWD ENTRY DOOR SLIDE DAMAGED (08L80025001/001). MAINTENANCE REPLACED L1 DOOR SLIDE NON-ROUTINE 08L80025001/001 IAW AMM 25-66-01.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 3, WL 208. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 3, WL 206. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 328 AND STA 344, LBL 44. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500H TO STA 5001, S25L. REPLACED BAFFLE PER AARD 51-00-05-1

Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500E TO STA 500F, S25L. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500F TO STA 500F, S25L. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500G TO STA 500H, S25L. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR LOWER CUT OUT WEB FROM STA 807 TO STA 847, S25R. REPLACED WEB PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500F TO STA 500I, RBL 24. REPLACED TRANSITION PANEL PER SRM 51-40-02 AND AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500D+10 INCHES TO STA 500I, LBL 24. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 5, AND AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 947 TO STA 960, LBL 50. REPLACED INTERCOSTAL PER SRM 53-70-51-2R.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER FLOOR SUPPORT AT STA 990, FROM RBL 34 TO RBL 41. REPLACED SUPPORT PER AARD 51-00-05.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT GIRT BAR TIEDOWN MOUNTING HOLE, STA 986, WL 206, RBL 43. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCES: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 947 TO STA 967, LBL 16. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: TIE DOWN — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR AFT FLOOR MOUNTED GIRT BAR TIEDOWN AT BS 344, LBL 54. REPLACED TIEDOWN PER 51-00-05-1. REPLACED TIEDOWN PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 947, LBL 50. REPAIRED FLOOR BEAM UPPER CHORD PER SRM 53-70-51-2R REPAIR 5.

Part: TIE DOWN — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,740 hrs · 14,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FORWARD FLOOR MOUNTED GIRT BAR TIEDOWN AT BS 330.62, WL 208. REPLACED TIE DOWN PER SRM 51-40-02 AND SRM 51-10-02-0G.

Part: BATTERY — NO TEST (AFT FLASHLIGHT) · airframe 34,181 hrs · 14,705 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT ON AIRCRAFT RIGHT AFT IS SHOWING A RED BATTERY LIGHT. REPLACED FLASHLIGHT BATTERY. PER AMM 25-64-00.

Part: FAN — ODOR (RECIRCULATION) · airframe 34,107 hrs · 146,678 cycles

AIRCRAFT WAS GROUNDED: VERY STRONG "DIRTY SOCK" SMELL ON DESCENT. REPLACED THE LEFT HAND RECIRCULATION FAN. NO ADDTIONAL SMELL NOTED. PER AMM 21-25-02.

Part: LOCK — OUT OF ADJUST (LAVATORY DOOR) · airframe 33,762 hrs · 14,507 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY-D DOOR LOCK STICKING. CUSTOMERS GETTING TRAPPED INSIDE. ADJUSTED AFT LAVATORY-D DOOR LOCK. PER AMM 25-40-15.

Part: FUEL FILTER — CONTAMINATED (ZONE 400 - NAC/P) · airframe 31,457 hrs · 13,407 cycles

AIRCRAFT WAS GROUNDED: ENGINE #1 "FILTER BYPASS" LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF AND WENT OUT IN DESCENT. REMOVED AND REPLACED LEFT HAND ENGINE FUEL FILTER.

Part: DIODE — LOOSE (ZONE 200 - FUSE) · airframe 30,583 hrs · 12,968 cycles

AIRCRAFT WAS NOT GROUNDED: ON APPROACH TRAILING EDGE FLAP EXTENDED ON SCHEDULE (30DEG) LEADING EDGE DEVICES SHOWED NO "LE FLAPS TRANSIT" OR "LE FLAPS EXT" AT ANY TIME. AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY. **SUPPLEMENTAL REPORT FOR AALA202303310641: MAINTENANCE TROUBLESHOT TO A FLIGHT DECK LIGHTING ISSUE, MASTER DIM AND TEST SWITCH PANEL. REPLACED DIODE ASSEMBLY M00208 (AALA202303310641) AND RECONNECTED LOOSE DIODE ASSEMBLY M00210 (AALA202304144019). MASTER DIM AND TEST WORK OK PER AMM 33-18-00 AND WDM 33-14-12.** (CLOSED)

Part: DIODE — FAULTY (ZONE 200 - FUSE) · airframe 30,583 hrs · 12,968 cycles

AIRCRAFT WAS NOT GROUNDED: ON APPROACH TRAILING EDGE FLAP EXTENDED ON SCHEDULE (30DEG) LEADING EDGE DEVICES SHOWED NO "LE FLAPS TRANSIT" OR "LE FLAPS EXT" AT ANY TIME. AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY. **SUPPLEMENTAL REPORT FOR AALA202303310641: MAINTENANCE TROUBLESHOT TO A FLIGHT DECK LIGHTING ISSUE, MASTER DIM AND TEST SWITCH PANEL. REPLACED DIODE ASSEMBLY M00208 (AALA202303310641) AND RECONNECTED LOOSE DIODE ASSEMBLY M00210 (AALA202304144019). MASTER DIM AND TEST WORK OK PER AMM 33-18-00 AND WDM 33-14-12.** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,583 hrs · 12,968 cycles

AIRCRAFT WAS NOT GROUNDED: ON APPROACH TRAILING EDGE FLAP EXTENDED ON SCHEDULE (30DEG) LEADING EDGE DEVICES SHOWED NO "LE FLAPS TRANSIT" OR "LE FLAPS EXT" AT ANY TIME. AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: WINDOW — FAILED (COCKPIT) · airframe 30,010 hrs · 12,687 cycles

AIRCRAFT WAS GROUNDED: RT FLIGHT DECK FIRST OFFICERS WINDOW SHATTERED. REMOVED AND REPLACED FIRST OFFICERS COCKPIT WINDOW.

Part: DOOR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 29,512 hrs · 12,457 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR HARD TO CLOSE. LUBRICATED L1 ENTRY DOOR PER AMM 52-11-00.

Part: RECEIVER — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 27,287 hrs · 11,375 cycles

AIRCRAFT WAS GROUNDED: THE HANDLE ON THE RIGHT AFT SERVICE DOOR DOES NOT STAY IN THE FULLY CLOSED AND LOCKED POSITION. MOVES TOWARDS OPEN POSITION. ALL COCKPIT INDICATIONS NORMAL. ADJUSTED/RIGGED R4 DOOR FORWARD AND AFT LOWER LATCH RECEIVER'S PER AMM 52-41-00.

Part: WINDOW — DELAMINATED (ZONE 200 - FUSE) · airframe 27,034 hrs · 11,247 cycles

AIRCRAFT WAS NOT GROUNDED: L1 WINDOW DELAMINATED NEAR LH EDGE. **SUPPLEMENTAL REPORT: REPLACED L1 WINDOW WITH SERVICEABLE UNIT IAW WORKCARD 08C21156001, LEAK AND OPS CHECK GOOD.** (CLOSED)

Part: NONE — NONE · airframe 27,034 hrs · 11,247 cycles

AIRCRAFT WAS NOT GROUNDED: L1 WINDOW DELAMINATED NEAR LH EDGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: MODULE — FAULTED (FIRE DETECTION) · airframe 25,596 hrs · 10,573 cycles

RH ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF, FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD. REPLACED FIRE DETECTION CONTROL MODULE, OPS CHECK GOOD.

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 25,088 hrs · 10,351 cycles

AIRCRAFT WAS GROUNDED: DOOR L2 ESCAPE SLIDE REQUIRES REPLACEMENT. REMOVED AND REPLACED L2 DOOR ESCAPE SLIDE PER WORK CARD 08L22125001.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 22,622 hrs · 9,224 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE FALLING OUT OF COVER. REMOVED AND REINSTALLED SLIDE PACK IN L1 DOOR IAW AMM 25-66-01. SLIDE PACK OK FOR SERVICE.

Part: CONNECTOR — BURNED (HYDRAULIC SYS) · airframe 21,942 hrs · 8,902 cycles

AIRCRAFT WAS GROUNDED: (REFERENCE LOG PAGE 39071980, AFTER #1 ENGINE START, ELEC 2 (SYS A) HYDRAULIC OVERHEAT LIGHT ILLUMINATED. RAN QRH PROCEDURE AND RETURN TO GATE). SYS A ELEC 2 ELEC HYD PUMP CONN D2664 BURNT. REPLACED PUMP CONNECTOR IAW WDM 29-11-12 D2664 AND IAW STANDARD PRACTICE 20-00, 20-61-11.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 18,897 hrs · 7,564 cycles

MAIN CABIN AISLE FLOOR PANELS WERE SOFT AT SEAT ROW 22. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLOOR PANEL IAW EA 285810.

Part: STOP FITTING — OUT OF ADJUST (SERVICE DOOR) · airframe 18,897 hrs · 7,564 cycles

AFT SERVICE DOOR LIGHT ILLUMINATED IN FLIGHT. HANDLE WAS SLIGHTLY RAISED FROM DOWN DETENT. PUSHED HANDLE DOWN AND LIGHT EXTINGUISHED. ACCOMPLISHED AFT ENTRY DOOR (SOFT UNLATCH) CHECK IAW AMM 52-13-00. ADJUSTED DOOR STOP PINS IAW AMM 52-13-00 STEP Q. DOOR OPERATIONS CHECK GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 18,897 hrs · 7,564 cycles

MAIN CABIN AISLE FLOOR PANELS WERE SOFT AT SEAT ROW 22. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLOOR PANELS IAW EA 285810.

Part: TRANSITION PANEL — CORRODED (BS 500B-500F) · corrosion level 2 · airframe 18,893 hrs · 7,561 cycles

CORROSION FOUND ON THE FORWARD CARGO BAY LEFT TRANSITION PANEL, BS 500C - 500F. REPAIRED THE TRANSITION PANEL IAW 51-00-05, REPAIR 1, AND SRM 53-00-53-2R, REPAIR 5.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,893 hrs · 7,561 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TRANSITION PANEL BS 500C TO 500D. REPLACED REPAIR SLICE (PANEL) PER SRM 53-00-53.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 18,893 hrs · 7,561 cycles

CABIN RT, CENTER, INBOARD BS 540 FLOOR SUPPORT WAS FOUND CRACKED. REPLACED THE FLOOR SUPPORT IAW 51-00-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,893 hrs · 7,561 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED RIGHT HAND OUTBOARD CENTER FLOORBOARD SUPPORT AT STA 540. REPLACED RIGHT HAND OUTBOARD CENTER FLOORBOARD SUPPORT (INTERCOSTAL) PER 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 18,893 hrs · 7,561 cycles

THE CABIN FLOOR SUPPORT WAS FOUND CRACKED BETWEEN BS 328 - 344, LBL 45. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, AND PRINT 141A5400.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,893 hrs · 7,561 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO RT TRANSITION ANGLE HAS CORROSION LOCATED BETWEEN STA 727G -767. REPLACED TRANSITION ANGLE AND SPLICE PER 51-00-05-1, DRAWING 146A7502 AND SRM 53-00-53-2R-5.

Part: COVER — DISLODGED (EXIT SIGN) · airframe 17,397 hrs · 6,923 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN COVER DISLODGED AT ROW 15. MAINTENANCE REINSTALLED EMERGENCY EXIT SIGN ABOVE ROW 15 SEAT ISLE PER AMM 33-51-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SHADE — INOPERATIVE (CABIN) · airframe 17,016 hrs · 6,764 cycles

AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE AT EXIT ROW SEAT 14A WAS STUCK IN THE CLOSED POSITION. MAINTENANCE REPLACED SHADE PER AMM 25-21-12 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DAMAGED (CABIN) · airframe 14,913 hrs · 5,846 cycles

EXIT LIGHT DAMAGED AFT LEFT DOOR. R&R EXIT LIGHT ASSEMBLY AT AFT LEFT DOOR , OPS OK. ALL DONE PER MM 33-51-02. THE AIRCRAFT WAS NOT GROUNDED.

Part: LENS — MISSING (EXIT SIGN) · airframe 14,045 hrs · 5,492 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY R2 DOOR HAS A MISSING LENS COVER. REPLACED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,621 hrs · 3,695 cycles

DENT & GOUGE AT STATION 339, STRINGER 21R - S22R. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-01.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 9,621 hrs · 3,695 cycles

LOWER FAIL SAFE STRAP DAMAGED AT STATION 268, STRINGER 26R. ACCOMPLISHED PERMANENT REPAIR IAW AARD 51-00-05, SRM 51-40-05, SRM 51-40-02, SRM 51-20-01 & DWG 141A-1551.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 9,621 hrs · 3,695 cycles

STRINGER R26 DAMAGED FROM STATION 259 - 294. ACCOMPLISHED PERMANENT REPAIR IAW AARD 51-00-05 & DWG 141A3534.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 9,621 hrs · 3,695 cycles

LOWER FAIL SAFE STRAP AT STATION 277 DAMAGED, BETWEEN STRINGERS 26R & 25R. ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-11 & EA 254380.

Part: SIGN — DAMAGED (CABIN) · airframe 7,976 hrs · 3,053 cycles

R1 DOOR EMER EXIT SIGN COVER WILL NOT STAY ON THE LIGHT ASSEMBLY. REPLACED R1 DOOR EMER EXIT SIGN ASSEMBLY. SYS CHECKED NORMAL.

Part: WEB — DAMAGED (FUSELAGE) · airframe 9,621 hrs · 3,695 cycles

RIGHT WEB AT STATION 277 DAMAGED, BETWEEN STRINGERS R26 & R25. ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-13-2R, AARD 51-00-05 & DWG 141A1171.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,435 hrs · 1,704 cycles

SEAT 22DEF, SEAT MOUNTED ESCAPE PATH CLEAR LIGHT, LAMPS FOUND INOPERATIVE. REPLACED LAMPS FOR SEAT 22DEF EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.