N333NW
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2016-07-07 – 2016-07-07 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2016-07-07 – 2016-07-07 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SHIP 3233 -ATO- DISCONTINUED TAKEOFF AT 50 KNOTS DUE TO LOSS OF RIGHT ENGINE OIL QUANTITY INDICATION. (SHOWED XXS). CORRECTIVE ACTION: MEL FOR OIL QTY. INDICATION APPLIED. REMOVED AND REPLACED ENG #2 OIL TRANSMITTER PER A320 AMM 79-31. ALL INDICATIONS NORMAL. MEL/PLAC REMOVED. (LP: 6084100)
DUE TO L/G LGCIU 2 FAULT ECAM MESSAGE WITH A LEFT GEAR DOOR AMBER. CORRECTIVE ACTION: R/R PROXIMITY SENSORS 33GA AND 35GA. FOUND FORWARD GEAR DOOR PIVOT HINGE BUSHING EXTREMELY WORN, REPAIRED SAME. R/R LEFT MAIN GEAR DOOR ASSY. GAPS AND OPS CHECK GOOD.
SHIP 3233 - ATO - AT APPROXIMATELY 80KTS DUE TO CAPTAIN'S AIRSPEED UNRELIABLE. FOUND #1 PITOT PROBE (9DA1) BLOCKED WITH DEBRIS. R/R PITOT PROBE 1 (9DA1). OPS AND LEAK CHECK GOOD.
SHIP 3233 - ATO - AT APPROXIMATELY 80KTS DUE TO CAPTAIN'S AIRSPEED UNRELIABLE. CORRECTIVE ACTION: MAINTENANCE STILL IN PROGRESS.
SHIP 3233 DISC: 'DIRTY SOCK' SMELL AS SOON AS APU BLEED WAS SELECTED ON AFTER LANDING. NO SMELL NOTED DURING FLIGHT WITH PACKS ON ENG BLEEDS. C/A: TS PER WC 4900-2001. UNDER UV LIGHTING PERFORMED DVI TO LOAD COMPRESS DRAIN, SURGE CNT'L VLV AND DUCTING , INTAKE PLENUM, BLEED VLV AND DUCTING. NTF.(416429 DB) COMPLETED W/C 0550-2002, RAN BOTH ENGINE BLEEDS, ISOLATED PACKS WITH NO SMELL NOTED. RAN APU BLEED WITH NO SMELL NOTED, PER W/C 4900-2001. PER MCC C/W W/ C 2100-2005 UP TO STEP 7.(DE335038) COMPLETED UP TO STEP 28 ON W /C 2100-2005, MCC REQUIRES COMPLETION OF W/C 7900-2001. COMPLTED UP TO STEP 14 OF W/C 7900-2001. (727698) COMPLETED WC 7900-2001 . COMPLETED WC 2100-2005. COMPLETED WC 4900-2001. ALL ODI STEPS REQUESTED BY MCC ARE C/W. OK FOR SVC. (LP: 5865702)
SHIP 3233 DISC: 2 O2 MASK AT DOOR 2R DEPLOYED. C/A: REPACKED MASKS PER A320 AMM 35-21. VERIFIED 02 GENERATOR WAS NOT DEPLOYED. A/C OK FOR SVC. (5847878)
SHIP 3233 DISC: OXYGEN PANEL MASK DEPLOYED / LOCATIONS:105. 2 MASKS DEPLOYED DURING TAKEOFF. C/A: REPACKED OXYGEN MASK ASSY. PER A320 AMM 35-21-43-550-801A. OK FOR SVC. (LP: 0217718)
SHIP 3233 DISC: O2 MASK IN ROW 31 DEF DEPLOYED. C/A: *** CONTRACT MAINTENANCE EVENT - OCM: 277091 *** INSPECTED O2 GENERATOR, NOT DEPLOYED. STOWED O2 MASK. AC OK FOR SERVICE. (LP: 5567110)
SHIP 3233 DISC: ALL LAV'S WILL NOT FLUSH. C/A: SECURED CANNON PLUG ON WASTE TANK LEVEL XMTR. LAVS OPS NML. REF A320 AMM 38-30. C/W A320 ODI ATA 38-31. (LP: 5374943)
SHIP 3233 FOUND ALL 4 AFT GALLEY/ATTENDANT AREA MASKS INCORRECTLY INSTALLED. CORRECTIVE ACTION: REINSTALLED PER A320 AMM 35-21. OK FOR SERVICE. (4485322)
SHIP 3233 COCKPIT EMERG LOC XMITTER DID NOT PASS TEST. CORRECTIVE ACTION: R/R ELT. (4651070)
SHIP 3233 CRACK INDICATION AT HOLE #6. CORRECTIVE ACTION: COMPLIED WITH ERA 580975-14AD REV A. (2610835)
SHIP 3233 -ATB- FLIGHT CREW PERFORMED AN AIR TURN BACK TO LAX DUE TO HIGH #2 VIBRATION. MAINTENANCE FOUND METAL IN THE TAIL PIPE. CORRECTIVE ACTION: ENGINE CHANGE IN PROGRESS.
SHIP 3233 -ATB/DE- FLIGHT RETURNED TO ATL DUE TO HEARING A LOUD BANG FOLLOWED BY HIGH ENGINE VIBRATIONS FROM #1 ENGINE. ATL MAINTENANCE FOUND METAL IN THE TAILPIPE. CORRECTIVE ACTION: ENGINE CHANGE REQUIRED. R/R #1 ENGINE PER A320 AMDS WORK CARD 7100-9901-LT. (8681554)
SHIP 3233 DURING TEST PSU/O2 PANEL AT SEAT 32 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8552015)
SHIP 3233 DURING SVC, FOUND L1 SLIDE WIRE HARNESS DAMAGED. CORRECTIVE ACTION: R/R L1 SLIDE ASSY. (7835430)
SHIP 3233 RMLG RETRACT ACTUATOR ACTUATOR FITTING LOWER FACE AND SPHERICAL BEARING BORE HAS CORROSION. CORRECTIVE ACTION: REPAIRED RH MLG RETRACT ACTUATOR ANCHORAGE FITTING PER A320 SRM 57-26-13. CONTINUE ON MON. (2307659)
SHIP 3233 - DIV - DUE TO #1 ENGINE GENERATOR LOST EN-ROUTE TO ATL, AND APU ON MEL, DIVERTED TO GSO. CORRECTIVE ACTION: R/R IDG 1. OPS CHECK AND LEAK CHECK GOOD. OIL LEVEL CHECK GOOD. (9297632)
SHIP 3233 1L DOOR VERY DIFFICULT TO OPEN AND CLOSE. CORRECTIVE ACTION: RIGGED DOOR PER A320 AMM 52-11. OK FOR SERVICE AFTER ADJUSTMENT. (7898266)
DURING TEST OF THE EMER LIGHT SYSTEM, EMERGENCY POWER SUPPLY UNIT 12WL (BATTERY PACK) DID NOT FUNCTION. CORRECTIVE ACTION: REPLACED PER A320 FAM AMM 33-51-38. OK FOR SERVICE.
SHIP 3233 NEED TO PERFORM INSPECTION ON FASTENER HOLE LOC. ON FR 51 BTW STR 6R TO7R UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED INSPECTION PER A320 SRM 53-41-11-300-014 AND SRI53-41-11-205-030 PAGE 2 TABLE 001. CONTINUE ON MON. (1884319)
SHIP 3233 NEED TO PERFORM INSPECTION ON FASTENER HOLE LOC. ON STR 7R BTW FR 60 TO FR 59 UPPER SKIN. CORRECTIVE ACTION: PERFORMED INSPECTION PER A320 SRM 53-41-11-300-014 AND SRM 53-41-11. CONTINUE ON MON. (1884310)
SHIP 3233 CORROSION EXTERNAL SKIN LOCATED BTW FR69 TO FR70 AND STR 31R TO STR 32R AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-11. (1880889)
SHIP 3233 L1 DOOR DAMPER AND EMERG. OPERATION CYLINDER (EMER EGRESS) PRESSURE LOW. CORRECTIVE ACTION: SERVICED CYLINDER IAW A320 AMM 52-10-00. OK FOR SERVICE. (7323026)
SHIP 3233 - AFT L/H EMERGENCY EXIT SLIDE DEPLOYED. CORRECTIVE ACTION: REMOVED BLOWN SLIDE PER AMDS W/C 2561. (3998274)
SHIP 3233 DTI FOR REPAIR REQUIRED AT FS 50 & STR 3R/4R COMMON TO GOGO INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ER/A 00-563639 CLOSED LOG AND REMOVED MONITOR INSP. (1781923)
DURING TEST PSU OXY PANEL 26DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OK FOR SERVICE.
DURING TEST FOUND PSU PANEL 24ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OK FOR SERVICE.
1L DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: SERVICED PER A320 AMM 52-10-00. SAFETY PIN REMOVED RII. REQUIRED RII INSPECTION ITEM COMPLETED.
DOOR PIN 1L NOT STOPPING ARMING LEVER FROM GOING DOWN. CORRECTIVE ACTION: RESEAT PIN AT 1L. OPERATIONS CHECK GOOD AT THIS TIME. OK FOR SERVICE.
1R DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: REPLACED DOOR ASSIST BOTTLE PER 52-15. OK FOR SERVICE.
SHIP 3233 RH ELEVATOR HINGE BORE BUSHINGS FOUND CORRODED AND OUT OF TOLERANCE. CORRECTIVE ACTION: COMPLIED WITH 537373-14, REV A. ACCOMPLISH SECTION IV REPETITIVE INSPECTION WITHIN EVERY 6 YEARS. (1659976)
FOUND PSU 02 PANEL AT 11ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXYGEN PANEL 11ABC. OPERATIONS CHECKED GOOD.
FOUND PSU 02 PANEL 10DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXYGEN PANEL 10DEF. OPERATIONS CHECKED GOOD.
FOUND PSU 02 PANEL 17DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXYGEN PANEL 17DEF. OPERATIONS CHECKED GOOD.
FOUND PSU 02 PANEL AT 13ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXYGEN PANEL 13ABC. OK FOR SERVICE.
SHIP 3233, ENTRY DOOR HARD TO OPEN OR CLOSE. CORRECTIVE ACTION: ADJUSTED L1 DOOR GUIDE FITTING, PAR A320 AMM 52-11. OPS CHECK GOOD.
SHIP 3233 WHILE ACCOMPLISHING ALI 531153-02-1 (JIC 5311-2036), CRACKS WERE FOUND IN FR16 RHS IN HOLES #6,#C,#D,AND #F. CORRECTIVE ACTION: PERFORMED INSPECTION AS PER ER/A 580975-14AD REV.ORIGINAL. OK TO CONTINUE TO MONITOR. JOB COMPLETE. (1309622)
CRACK INDICATION ON INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES OF DOOR STOP FITTING NUMBER 7 LOC. FRAME 16 RH SIDE IN PASSENGER CABIN (CRACK DIRECTION IS 3 AND 9 O'CLOCK), REPLACED INTERCOSTAL FITTING OF DOOR STOP FITTING NUMBER 7 LOC. FRAME 16 RH SIDE IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG NO.D53112300
CRACK INDICATION ON INTERCOSTAL ON UPPER AND LOWER INBOARD HOLES OF DOOR STOP FITTING NUMBER 7 ON FRAME 16 LT IN PASSENGER CABIN (CRACK DIRECTION IS 3 AND 6 O'CLOCK), REPLACED INTERCOSTAL ON STOP FITTING NUMBER 7 ON FRAME 16 LH IN PASSENGER CABIN AS PER SRM 51-72-11 AND DRAWING D5311233100
CORROSION WEB LOCATED BETWEEN FR58 TO FR59 AND STR38L IN AFT CARGO COMPARTMENT (1 EA), REPLACED WEB LOC BTW FR58 TO FR59 AND STR 38 LH IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DWG NO.D53470320
CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL FWD IN PASSENGER CABIN, REPLACED TRANSMITTING PROFILE FWD ON EMERGENCY EXIT DOOR AS PER A320 SRM 51-72-11 AND DWG D522279010
CRACK INDICATION ON INTERNAL STRUCTURE OF FRAME 20 ON DOOR STOP FITTING NUMBER 1 IN LOWER INBOARD HOLE OF RH SIDE IN PASSENGER CABIN (CRACK DIRECTION IS 3 O'CLOCK WITH D =O.079"), REPLACED FITTING ON INTERNAL STRUCTURE FR20 TO FR21 AND STR 22R AS PER A320 SRM 51-42-11 AND DRAWING #D53112331
CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED TRANSMITTING PROFILE ON EXIT DOOR 833 AS PER SRM 51-72-11 AND DWG D52279010.
PASSENGER CREW DOOR 831 DOOR DAMPER DOES NOT PASS OPERATIONAL TEST, REPLACED PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA.
CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 TRANSMITTING PROFILE AFT IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.
CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 TRANSMITTING PROFILE AFT IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.
CORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 12 TO FR 16 Y+503 .2 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTN FR 12 TO FR 16 Y +503.2 IN PASSENGER CABIN AREA AS PER SRM 51-72-11 AND DWG #D53112825
CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL FWD IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL FWD IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.
CORROSION FRAME 71 ANGLE LOCATED BETWEEN STR 27R AND STR 32R AT LOWER FUSELAGE, REPLACED ANGLE LOC AT FR 71 BTW STR 27R AND STR 32R LOWER FUSELAGE AS PER SRM 51-42-11 AND DWG D53571510.
CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 Y- 1292 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 Y-1292 IN PASSANGER CABIN (1E/A) AS PER SRM 51-72-11 AND DWG D53112814.
CORROSION FLOOR STRUCTURE LOCATED AT FR 67+16INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN, REPLACED FLOORBEAM STRUCTURE LOCATED AT FR 67 +16 INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN AREA AS PER SRM 51-72-11 AND DWG# D5347200.
CORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 14 TO FR 16 Y+940 IN PASSENGER CABIN (1EA), REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR14 TO FR16 Y+940 IN PASSENGER CABIN (1E/A) AS PER SRM 51-72-11 AND DWG D53112822.
CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66+6INCH TO FR 70 Y-765 IN PASSENGER CABIN (1E/A), REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR66+6" TO FR70 Y-765 IN PASSENGER CABIN (1E/A) AS PER SRM 51-42-11 AND DWG D53-472816.
DURING SERVICE CHECK FOUND ALL 4 OVERWING EXIT DOOR PULL HANDLE LIGHTS INOP, RELAMPED LEFT FORWARD AND AFT AND RIGHT FORWARD PULL HANDLE LIGHTS
FR50 PARTIAL FRAME PERMANENT REPAIR ERA 563639-14 SECTION 2 ITEM #5 MAJOR REPAIR PER SRM 53-00-12-300-004.
EMERGENCY LIGHT ILLUMINATED IN FLIGHT WITHOUT POWER LOSS. REMOVED AND REPLACED THE 4WL EMERGENCY LIGHT SWITCH. OPS CHECKED OK.
SHIP 3233 CORROSION IN LH/RH WING BOTTOM SKIN ACC PNL FASTENER HOLES. CORRECTIVE ACTION: PERFORMED POST-REPAIR REPETITIVE INSPECTION-LEFT WING AND RIGHT WING BOTTOM SKIN LOWER SURFACE AS PER ER/A 563122-14AD REV.ORIGINAL, SECTION I AND SECTION II AND ADDITIONAL DAMAGE WAS NOT FOUND, OK TO CONTINUE MONITOR. (0293918)
FR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND RMLG AFT UPPER ACTUATOR FITTING HAS SEVERAL OUT OF ROUND HOLES. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.
FR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND CRACK INDICATION NOTED IN TOP LAYER OF MATERIAL AT HOLE NR 9. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.
FR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND OUT OF ROUND HOLES AIRCRAFT SIDE COMMON TO RT MLG UPPER ACTUATOR FITTINGS. HOLES MARKED AS 4,5,6,7,9,10,11,12, COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.
FR43 KEEL BEAM FWD HINGE FITTING, RT MLG DOOR FOUND CRACK INDICATIONS ON AIRCRAFT SIDE COMMON TO RMLG UPPER ACTUATOR FITTINGS. HOLES MARKED AS 7,8,10. COMPLIED WITH PRI'S 560120-14AD REV A REV 1 THRU 6. REPAIRED REF ERA 560120-14AD REV A.
EPSU INT LOAD AFT L ON SERVICE CK, R AND R EPSU WITH BATTERY 13WL.
FR43 LT SIDE CENTER HOLE CRACKED IN CENTER LAYER BEAM. REPAIRED FR43 LT SIDE BEAM PER 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.
FR43 LT SIDE AFT HOLE CRACKED IN UPPER LAYER PRESS PLATE AND CENTER LAYER BEAM. REMOVED AND REPLACED LT PRESSURE PLATE AND REPAIRED BEAM. REF; 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.
ON WALK AROUND PREFLIGHT F/O FOUND A DENT ON AIRCRAFT LEFT, AFT OF RADOME. RECTANGULAR IN SHAPE. BARE METAL SHOWING. CORRECTIVE ACTION: C/W TERMINATING ACTION, PER SRM 53-11-11-205-031. OK FOR SERVICE.
CORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R IAW ER/A 542037-14, REV ORIGINAL.
DURING INSPECTION, FOUND CORROSION ON WEB -Y1732 AT FRAME 16. REPLACED WEB IAW SRM 51-72-11 AND DWG D53112780.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 18+4" -Y254. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 TO FR 24 IAW SRM 51-72-11, DWG D53112819, D53112820, D53110984 , D53110900 AND ER/A 520675-14 REV ORIGINAL, REV 0 .
DURING INSPECTION, FOUND CRACK ON EXTERNAL SKIN AT FIXED L/E LOWER SURFACE AT LEVEL RIB 15 LT WING. REPAIRED EXTERNAL SKIN AT FIXED L/E LOWER SURFACE AT LEVEL RIB 15 LT WING IAW SRM 57-41-11, FIG 206.
DURING INSPECTION, FOUND CORROSION ON LOWER SILL OF LT PASSENGER CREW DOOR AREA BETWEEN FRAMES 66 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D534 80505.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT -Y189 FRAME 20+11 IN FWD PAX CABIN. REPLACED FLOOR SUPPORT BETWEEN FRAMES 20 AND 23 IAW SRM 51-72-11 AND DWG D53112834.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, Y 254. REPAIRED FLOOR SUPPORT IAW SRM 53-00-14, PARA 4.G, FIG 207, PAGE 250-256.
DURING INSPECTION, FOUND CORROSION ON PASSENGER DOOR AFT CORNER FITTING AT FRAME 68 . REPLACED FITTING IAW SRM A320 51-75-11 AND DWG D53480505.
DURING INSPECTION, FOUND CORROSION ON BORE OF SPIGOT RECEPTACLE FITTING ON LT PYLON. REPLACED RECEPTACLE FITTING IAW SRM 54-51-12.
DURING INSPECTION, FOUND CORROSION ON TWO BRACKETS, LOCATED EMERGENCY EXIT DOOR 844 THE OF HOOK BRACKET AREA, INTERNAL STRUCTURE. REPLACED BRACKETS, LOCATION ON EMERGENCY EXIT DOOR 844 THE OF HOOK BRACKET AREA INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D522-79040.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 65 TO 67, Y-308. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472282.
CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69 Y-1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.
DURING INSPECTION, FOUND CORROSION ON LOWER SILL OF RT AFT PASSENGER CREW DOOR AREA BETWEEN FRAMES 66 TO 68. . REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480505.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, Y-1292. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66 TO 68 Y-1292 - Y-1162. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG NR D53472000.
DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY BETWEEN STRINGERS 40 & 41R FRAME 30. REPLACED CLEAT AND FASTENERS IAW SRM 51-72-11 AND DWG D53231586.
DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 31 AND BETWEEN STRINGERS 41-42R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D5323 1586.
DURING INSPECTION, FOUND CORROSION ON LOWER SILL AREA AT LEVEL FRAME 16+6 AND S23L IN FWD PAX CABIN. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG NR D53110339.
DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY LOCATED AT LEVEL FRAME 33 AND BETWEEN STRINGERS 40-41R. REPLACED CLEAT AND FASTENERS IAW SRM A320 51-72-11 AND DWG D53231586.
DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 31 AND BETWEEN STRINGERS 40-41R. REPLACED CLEAT IAW SRM 51-72-11 AND DWG 53231586.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 AND Y 1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472090.
DURING INSPECTION, FOUND CORROSION ON TWO BRAKETS ON EMERGENCY EXIT DOOR. REPLACED BRACKETS IAW SRM 51-72-11 AND DWG D52279040.
DURING INSPECTION, FOUND CORROSION ON TWO BRACKETS, REPLACED BRACKETS AT EMERGENCY EXIT DOOR, IAW SRM 51-72-11 AND DWG D52279040.
DURING INSPECTION, FOUND CENTER FITTING WITH CORROSION AT STRINGER 23L BETWEEN FRAMES 66 AND 68. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480019.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 TO 69 AND Y 1162. REPLACED FLOOR SUPORT IAW SRM 51-72-11 AND DWG D53472000.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66 TO 68 AND BETWEEN Y 1292 AND Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 70 AND Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 70 AND Y512. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.
DURING INSPECTION, FOUND CORROSION ON WEB -Y1732 AT FRAME 20 IN FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 AND Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472090.
DURING INSPECTION, FOUND CORROSION ON WEB Y1732 AT FRAME 20 IN FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11.
DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT FRAME 20+10" IN FWD PAX CABIN. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112812, D53110900.
DURING INSPECTION, FOUND CORROSION ON FLOORBEAM LOCATED ON FRAME 18+5" AND Y254. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53112816.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FR 66 TO FR 70 AND Y-160. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.
DURING INSPECTION, FOUND CRACK ON UPPER SLIDING WINDOW RAIL LT LOCATED IN COCKPIT. MAINTENANCE PERFORMED REPAIR ON DAMAGE AREA ON UPPER SLIDING WINDOW RAIL LT LOCATED IN COCKPIT IAW SRM 53-11-12.
DURING NON ROUTINE CHECK, FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE AT 13C. MX REINSTALLED LIGHTING ASSY AND FUNCTIONAL CHECK WAS NORMAL.
DURING NON ROUTINE CHECK, FOUND SEAT 24 EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPAIRED CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETUNED TO SERVICE.
DURING NON ROUTINE CHECK, FOUND SEVERAL FLOOR PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED AFT EPSU AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.
ON DESCENT APPROXIMATELY 20000 FEET, FLIGHT ATTENDANT CALLED WITH A SLIGHT SMOKEY SMELL IN AFT GALLEY AREA. PILOT IN JUMP SEAT CONFIRMED SLIGHT SMELL, GALLEY POWER WAS TURNED OFF FOR REMAINDER OF FLIGHT AND LANDING WAS UNEVENTFUL. REPLACED RIGHT AFT LAVATORY WATER HEATER AND TESTS OK.
DURING CRUISE, THE CREW NOTED THAT THE RT TANK WAS DROPPING AA MUCH HIGHER RATE THAN NORMAL, SO THEY INITIATED THE RETURN WITH THE THOUGHTS OF A FUEL LEAK. ABOUT 50 MILES NW OF THE FIELD DID QRH PROCEDURE AND THE RT ENGINE WAS SHUTDOWN, THE LANDING WAS UNEVENTFUL. FOUND RELAY FAILED, WAS REPLACED ANDTHE RE-FUEL PANEL WAS REPLACED AS A PRECAUTION AND FUEL SYSTEM TESTED OK.
DURING A NON ROUTINE CHECK, FOUND ESCAPE PATH MARKING LIGHT AT ROW 16 AND 24 INOPERATIVE. MAINTENANCE REPAIRED WIRE AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL AND A/C RETURNED TO SERVICE.
DURING TEST FOUND EMERGENCY LIGHT AT SEAT 3A/B INOP. REPLACED WIRING HARNESS AND TEST OK.
FLIGHT ATTENDANT REPORTED WIRING AT ROW 25 EMERGENCY PATH LIGHT IS INOPERATIVE. MAINTENANCE RE-SECURED LIGHTING WIRING UNDER CONDUIT AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING A NON ROUTINE CHECK, FOUND POWER SUPPLY UNIT AT 13 WL WILL NOT TEST. REPLACED POWER SUPPLY AND TEST WAS NORMAL.
DURING TEST PATH LIGHT SEAT 3B WAS INOP, SECURED LOOSE PIN IN PLUG AND TEST OK.
FORWARD EMERGENCY LIGHT BATTERY PACK INOP. CORRECTED BY REPLACING BATTERY PACK. CHECKS OK.
EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 1, 2, 3, 5, 6, 7, 13, 14, 15, 18, 19, 20, 24, 25, 26. CORRECTED BY REPLACING FWD AND AFT POWER SUPPLY UNITS, AND REPAIR OF SHORTED WIRE AT ROW 20. ALL LIGHTS CHECK OK. Â
EMERGENCY LIGHTS AT ROWS 14, 15, 16, 18, 20, 24, 25, 26 INOP. CORRECTED BY REMOVING AND REPLACING AFT RIGHT POWER SUPPLY UNIT. TESTS OK. Â
DURING TAKEOFF AT APPROXIMATELY 200 FT AGL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND EGT ROSE. THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT CREW RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE.
DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED TO TEST. FOUND BOTH RIGHT OVERWING EXIT LIGHTS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHECK OK.
THE RIGHT WING NR 2 SPOILER ACTUATOR FAILED TO EXTEND ON LANDING. THE LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. DURING TAXI INTO GATE THE YELLOW HYDRAULIC SYSTEM FLUID DEPLETED. MAINTENANCE REPLACED THE RIGHT WING NR 2 SPOILER ACTUATOR, LEAK AND OPS CHECK OK.
DURING C-CHECK, FOUND THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE INBOARD AFT MOUNT LINK WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY RHOR CMM 71-22-07. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.0005 INCH TO 0.001 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-095310 AND 32-96330.