N378NW
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A320 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH. (LP: 1677696, AIRCRAFT WAS GROUNDED)
LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH.SEE INDIVIDUAL SIGN OFF ON ORNRC 68/400. RII INSPECTION COMPLETE. (LP: 1677117, AIRCRAFT WAS GROUNDED)
EMERGENCY SEAT MOUNTED LIGHTING DAMAGED, INOPERATIVE. LOCATION: 20D. LIGHT ASSEMBLY DETACHED, HANGING FROM SEAT. R &R REPLACED 20D LIGHT ASSY HOUSING AND OPS TEST GOOD ALL WORK DONE IAW AMM 33-20. (LP: 1399329)
AFTER T/O, TE FLAP DID NOT FULLY RETRACT WING TIP BREAK ON. LANDED WITH SLATS EXTENTED, FLAP <1 MED BRAKES. T/S IN REF A320 TSM 27-51-00-810-840-A RESET WTB FAULT WENT AWAY NO OTHER FAULTS NOTED. OPS CK FLAP SYS IN REF A320 AMM 27-54 OPS CK GOOD NO DEFECTS OR FAULTS NOTED AT THIS TIME. INSPECTED FLAP TRANSMISSION IN REF A320 AMM 27-54 NO DEFECTS NOTED AT THIS TIME. CK TORQUE LIMITERS IN REF A320 AMM 27-50 NONE FOUND TRIPPED. LUBRICATED FALP ACTUATORS IN REF A320 A320 12-22. NO OTHER DEFECTS NOTED A/C GOOD FOR SVC. (LP: 7907306)
AFT OUTBOARD LAV O2 MASK IS HANGING DOWN. RESTOWED O2 MASK IN AFT OTBD LAV PER AMM 35-21. (LP: 8104016)
PERFORMING OPS CHECK OF MANUAL MASK RELEASE FOUND MULTIPLE MASKS FAIL DROP. WHEN INITIATING DROP TEST OF MASKS FOUND BREAKER HA06 ON THE OVERHEAD C/B PANEL POPPED WHEN PUSHING THE MAN MASK BUTTON. SUSPECT WIRES SHORTING. CHECKED WIRES END TO END, AND END TO GROUND FROM PIN 2 OF C/B HA06 TO C1 OF RELAY 10 WB. WIRE CHECKED GOOD. FOUND SHORT TO GROUND WHEN CHECKING PIN C2 ON RECEPTACLE OF RELAY 10WB. DISCONNECTED CONNECTOR 2405VC & STILL HAD SHORT TO GROUND COMING FROM PIN C2 ON RELAY RECEPTACLE 10WB. RECONNECTED CONNECTOR 2405VC & DISCONNECTED CONNECTOR 1184VC. SHORT TO GROUND GONE FROM C2. COULD NOT FIND A SHORT TO GROUND ON PIN 3 OF CONNECTOR 1184VCA. SUSPECT CONNECTOR OR RECEPTACLE. IAW AWM 35-23-1. REF AWM 35-23-01 THRU 35-23-07. FOUND DEAD SHORT AT O2 BOX SOLENOID 33WR IN AFT CABIN. SEAT ROWS 11L & 11R+32L WILL NOT RELATCH. RELATCHED 11L, 11R, & 32L, REPLACED O2 BOX AT AFT GALLEY IAW AMM 25-25-43. OPS CHKD GOOD. ALL MASK PANELS OPEN & NO BREAKERS POPPED ON DROP TEST. (LP: 1350472)
AFT GALLEY PORT COFFEE MAKER EMITTING BURNT ELECTRICAL SMELLS WHEN ON. F/A TURNED OFF AND SMELL STOPPED. INSPECTED BOTH COFFEE MAKERS (508&509). NOT ABLE TO REPLICATE SMELL. COMPLETED W/C 0550-2002 NOGO ODI SMOKE AND FUMES. FWD BOTH 508 & 509 COFFEE MAKERS TO NEF 25-36-02. DEF REMARKES C/W. C/B'S PULLED, COFFEE MAKERS PLACARDED. DID NOT FIND EVIDENCE OF SMOKE OR ELECTRICAL SMELL. (LP: 8117874)
LEFT OPENABLE WINDOW HEAT MALFUNCTION ACTIVE BUBBLING, BOTTOM LEFT CORNER EXTREMELY HOT, REST OF WINDOW COLD. FOLLOWING BURNING SMELL COMPLIED WITH FCOM PROCEDURE, PULLED CB X14 ON 122VU PANEL. R & R LT WINDOW HEAT COMPUTER 2DG1 PER A320 AMM 30-42. WINDOW HEAT OPS TEST REQ'D AFTER WINDOW INSTALL (WIP 381173) CHECKS GOOD PER A320 AMM 30-42. (LP: 8117837)
NUMBER 4 FLAP HAS BIRD SRIKE DAMAGE. REMOVED DAMAGE AT LEADING EDGE (SMALL CUTOUT) PER A320 SRM 57-53 -00-283-082/57-53-00-300-029 REV 154.00 OCT 03 2025. INSTALLED CONICAL WASHERS. DRILLED UP AND SIZED DOUBLER, COUNTER SUNK DOUBLER FOR FASTENERS PER A320 SRM 57-53-00-283-082/57-53-00-300 -029 REV 154.00 OCT 03 2025. PREPPED AREA TO LAYUP ISOLATION PLY . (QC5238) A320 SRM 57-53-00-283-082. OK TO LAYUP PLYS. BONDED ON ISOLATION PLY PER A320 SRM 57-53-00-283-082 REV 154.00 OCT 03 2025. OK TO INSTALL DOUBLER (QC5238) INSTALLED AND EDGE SEALED DOUBLER A320 SRM 57-53-00-283-082 REV 154.00 OCT 03 2025. CURED AND COMPLETED REPAIR SRM 57-53-00-283-082 REV 154.00 OCT 03 2025. (LP: 1269019)
POSSIBLE BIRD STRIKE FO SIDE RADOME. DURING BIRD STRIKE INSPECTION FOUND DELAMINATION OF RADOME OUT OF LIMITS PER A320 AMM 53-15. REMAINING BIRD STRIKE INSP WILL NEED TO BE C/W. R/R RADOME PER A320 AMM 53-15. C/W BIRD STRIKE INSPECTION PER A320 AMM 05-51. FOUND HOLE ON LEADING EDGE OF RIGHT WING OF OUTBOARD FLAP. REMOVED LEADING EDGE STRUCTURE ON NON ROUTINE #1. INSTALLED LEADING EDGE STRUCTURE PANEL ON RT WING AFT FLAP. (LP: 7724302)
ROW 28DEF EMERGENCY SEAT LIGHT BOX BROKEN/INOP. C/A: TAPED BOX BACK UP TO SEAT. WILL NEED TO BE REPLACED. FWD TO MEL 33-50-03A. NO "M" PROC. MEL AND PLACARD INSTALLED. A/C OK FOR SVC. R/R EPL SHROUD ASSY AT 28DEF REF A320 CMM 25-22-53 OPS GOOD MEL PLACARD RMVD "M" PROC REVERSED OK FOR SVC. (LP: 7605030)
AFT FA REPORTS SULFUR SMELL COMING OUT OF VENTS IN AFT GALLEY. NO ODOR OR SULFUR SMELL NOTED.
SHIP 3278 - DIV - TO CMH DUE TO ENG 1 + 2 INLET ANTI-ICE VALVES INDICATING CLOSED. COULD NOT CONTINUE DUE TO ICING. T/S. PERFORMED IDLE ENGINE RUN AND OPS TESTED TENG A/I SYS ON BOTH. CYCLED BOTH P/B 4 X'S. COULD NOT DUPLICATE FAULT. OPS CK OK. MEL/PLAC RMVD. TO CMH DUE TO ENG 1 + 2 INLET ANTI-ICE VALVES INDICATING CLOSED. COULD NOT CONTINUE DUE TO ICING. CORRECTIVE ACTION: LOCKED BOTH VALVES OPEN PER MEL AND CONTINUED.
SHIP 3278 DISC: BIRD STRIKE @3400 RADOME @ 9 O'CLOCK POSITION CA SIDE (250 KNOTS). C/A: PERFORMED BIRD STRIKE INSPECTION PER A320AMM 05-51.FOUND DAMAGE TO RADOME WILL REQUIRED REPLACEMENT . THE REST OF THE AIRCRAFT NO DAMAGE NOTED.(336118) R/R RADOME PER A320 AMM 53-15. OPS CHECK NML. (LP: 6736964)
SHIP 3278 DISC: EMER ESCAPE PATH LIGHT AT ROW 10 INOP. C/A: R/R EMER ESCAPE PATH LIGHT PER A320 AMM 33-51. OPS CHECK GOOD. (LP: 6010708)
SHIP 3278 DISC: "DIRTY SOCK" SMELL IN COCKPIT WHILE APU BLEED WAS SUPPLYING AIR TO PACKS. HAPPENED SHORTLY AFTER GROUND AIR WAS REMOVED. C/A: FOUND APU GENERATOR LEAKING OIL PER WC 0550-2002. PERFORMED CLEANING OF APU INTAKE + COMPARTMENT PER W/C 4916-2001. PERFORMED DECONTAMINATION OF THE ECS WITH INOP APU (REVERSE FLOW ) PER WC 2100-2005. FOUND NO FURTHER EVIDENCE OF OIL CONTAMINATION. PERFORMED STAGE 1+2 CLEANING OF THE ECS. RECIP FILTERS CHANGED TWICE, NO FURTHER EVIDENCE OF ODOR EXISTS. VERIFICATION OF RESIDUAL ODOR WC 0550-2003 C/W. WILL REQUIRE GENERATOR MPN: 5913667-4 STK# 32-2420-9-0003. MCC NOTIFIED. (LP: 6200960)
SHIP 3278 DISC: FLOTATION EQUIPMENT - 1 LIFE RAFT MISSING. C/A: FLIGHT CREW PLACARD INSTALLED AT ALB PER MEL25-60-16D. PER SHIP 3278 ATTRIBUTES LIFE RAFTS NOT INSTALLED MCO/PLAC REMOVED. (LP: 0379481)
SHIP 3278 DISC: METALLIC BURNING ELECTRIC SMELL WITH NO VISABLE SMOKE, NOTICED BY PILOTS, FLIGHT ATTENDANTS, PASSENGERS. COMPLIED WITH QRH SECTION 8.1 AND SMELL DISSIPATED. C/A: IDENTIFIED SMELL AS TYPE 9 PER W/C 0550-2002, FOUND THE FC OVEN HAD A METALLIC SMELL AND THE LEFT RECIRC FAN WAS SEIZED. R3EPLACED BOTH. REPLACEED BOTH FILTERS AND THE AVIONIC BAY FILTER. OK FOR SERVICE. (LP: 5664236)
SHIP 3278 DISC: OXYGEN PANEL MASK DEPLOYED / LOCATIONS:202 O2 MASKS FALL OUT ON LANDING. C/A: OUND STRINGS & TUBES JAMMED BEHIND LOCKING MECH. REINSTALLED IAW A320 AMM 35-21. OK FOR SVC. (LP: 0271347)
SHIP 3278 DISC: OVERWING ESCAPE LIFE LINE MISSING AT 15DEF. C/A: REPLACED MISSING OVERWING ESCAPE LIFE LINE AT SEAT 15DEF MCO AND PLACARD REMOVED. (LP: 5107078)
SHIP 3278 DISC: (DIV) ENG 2 THR LEVER DISAGREE CATION ECAM MSG. PERFORMED ECAM ACTIONS FOLLOWED BY QRH PROCEDURES. DECLARED EMERGENCY. OVERWEIGHT LANDING 144800LBS. THRUST DID REDUCE SIGNIFICANTLY ON ENG 2. C/A: C/P 407VC BACKED OFF SEVERAL TURNS-SECURED SAME- RAN ENG CKS OK . REF LOG 5499052 FOR OVERWEIGHT LANDING AND LOG 5499053 FOR FOQA DOWNLOAD. (LP: 549050)
SHIP 3278 EXISTING REPAIR FRAME 20 ON FASTENER HOLE A DOCUMENTED ON ER/A 587474-14 REV.ORIGINAL LOCATION FRAME 20 LH SIDE DOUBLER JOGGLE AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 587474-14AD REV A PRI REV 1 AND PRI REV 0. (2958503)
SHIP 3278 FR16RH AT DOOR STOP # 1 & # 7 LEVEL, DBL JOGGLE AREA/ HOLE B / CRACK. CORRECTIVE ACTION: INSPECTED AND CONTINUE ON MON. OK FOR SERVICE. (2957801)
SHIP 3278 EXISTING REPAIR FRAME 16 ON FASTENER HOLE B DOCUMENTED ON ER/A 587478-14 REV.ORIGINAL LOCATION FRAME16 RH SIDE DOUBLER JOGGLE AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 587478-14. (2958466)
SHIP 3278 FUSELAGE / FRAMES/FORMERS / FR20LH AT DOOR STOP NO 7 LEVEL / DOUBLE JOGGLE AREA / HOLE A / CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 587474-14, REV A. (2954518)
SHIP 3278 DENT EXTERNAL SKIN LOCATED FR8 TO FR9 8 INCHES ABOVE LOWER RH SIDE STRINGER LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED AND FOUND WITHIN LIMITS. CONTINUE ON REPEAT MONITOR. (2936582)
SHIP 3278 SLAT 3 LEADING EDGE AREA RH WING DAMAGE. CORRECTIVE ACTION: INSPECTED OK FOR SERVICE. PUT ON REPEAT MONITOR. (2936615)
SHIP 3278 DENT EXTERNAL SKIN BTW FR 21 TO FR 23 AND BTW STR 24L TO STR 25L LOWER FUSELAGE. CORRECTIVE ACTION: FOUND TO BE WITHIN LIMITS. (2933330)
SHIP 3278 RH FLAP TRUNNION DAMAGE PRIOR BLENDING EXCEEDS MAX LIMITS OF .236", X=.307", Y=.309", DEPTH=.249" TRUNNION DIAMETER 3.000". CORRECTIVE ACTION: COMPLIED WITH ERA 608693-14AD. (2769967)
SHIP 3278 LH FLAP TRUNNION DAMAGE EXCEEDS MAX DEPTH OF .236 BEFORE BLENDING. X=.258, Y=.330, DEPTH=.249 TRUNNION DIAMETER MEASURES 3.020. CORRECTIVE ACTION: COMPLIED WITH ER/A 608691-14AD. (2769961)
SHIP 3278 DAMAGE TO RH INBD FLAP TRUNNION. CORRECTIVE ACTION: COMPLIED WITH ERA 608693-14AD. (2764370)
SHIP 3278 DAMAGE TO LH INBD FLAP TRUNNION. CORRECTIVE ACTION: COMPLIED WITH ERA 608691-14AD. (2764279)
SHIP 3278 2L DOOR FOUND DAMAGE TO HARDWARE IN DOOR HANDLE OPENING. HANDLE WILL NOT STAY UPRIGHT POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED HARDWARE AT 2L OPENING HANDLE PER A320 IPC 52-13 AND A320 AMM 20-21. OPS CHECK GOOD. (9447040)
A/C DEPARTED ICE COVERED TAXIWAY. INSPECTED AIRCRAFT. NO DAMAGE FOUND.
SHIP 3278 AFT LEFT DOOR (DOOR 3L) WHEN SLIDE IS ARMED AC PRESSURIZED WILL CONSTANLY FLASH "SLIDE" ON DOORS ECAM PAGE AND RED PRESSURE LIGHT ON THE 3L DOOR WILL FLASH RED. THE ARM LEVER AT THE 3L DOOR IS NOT FULLY SEATED IN ITS ARMED POSITION. CORRECTIVE ACTION: CLEANED AND ADJUSTED DOOR PER A320 AMM 52-13. OPS CHECK GOOD. (9852861)
SHIP 3278 PSU DOOR AT ROW 25 WILL NOT LATCH. CORRECTIVE ACTION: REPLACED PSU HOUSING ASSY PER A320 AMM 35-21-41. OPS CHECK GOOD. (8336992)
SHIP 3278 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AT SEAT 1C. CORRECTIVE ACTION: REPLACED LIGHT ASSY. (1983171)
DURING TEST PSU/O2 PANEL IN SEAT 23DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 19DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 31DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 29ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 15ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 12DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
DURING TEST PSU/O2 PANEL IN SEAT 3AB DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.
CORROSION INTERCONNECTING STRUT OUTBOARD FLAP ON LT WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OUTBOARD FLAP ON LT WING, AS PER A320 FAM AMM 27-51-44-400-001-A. PERFORMED ADJUSTMENT OF THE INTERCONNECTING STRUT, AS PER A320 FAM AMM 27-51.
CRACK INDICATION ON FRAME 16 AT DOUBLE JOGGLE AREA, RT SIDE, HOLE B, AT LEVEL DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: RT SIDE AT LEVEL DOOR STOP 7, AS PER PRI 587478-14AD REV 0 AND REV 1 ER/A NR 587478-14AD REV.
CORROSION FLAP TRACK FAIRING 632CB GROUND PLATE ON RT WING. CORRECTIVE ACTION: REPLACED FLAP TRACK FAIRING 632 CB GROUND PLATE ON RT WING, AS PER ER/A 587521-14 PRI REV 0. ER/A 587521-14 REV ORIGINAL.
CORROSION FLAP TRACK FAIRING 633CB GROUND PLATE ON RT WING. CORRECTIVE ACTION: REPLACED FLAP TRACK FAIRING 633 CB GORUND PLATE ON RT WING, AS PER ER/A 587521-14 PRI REV 0 ER/A 587521-14 REV ORIGINAL.
INOP EPSU-EMERGENCY POWER SUUPLY UNIT 11WL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT (11WL) IN PASSENGER CABIN (1EA) ON SERVICEABLE CONDITION PN 3214-54-10 SN 2448, AS PER A320 FAM AMM 33-51-38-400-001-A. OPERATIONAL TEST OF THE EPSU AMM 33-51-00-710-001-A. TEST IS GOOD.
CRACK INDICATION ON FRAME 20 AT THE DOUBLE JOGGLE AREA, LT SIDE, HOLE. CORRECTIVE ACTION: REPAIRED FRAME 20 AT THE DOUBLE JUGGLE AREA LT SIDE HOLE A, AT LEVEL DOOR STOP 7 AT FWD GALLEY AREA, AS PER PRI 587474-14AD REV 0 1 AND ER/A 587474-14AD REV ORIGINAL.
CRACK INDICATION ON FRAME 16 LT SIDE, DOOR STOP 7 HOLE ?1 AT FWD GALLEY AREA (1 EA), CRACK AT 5 O CLOCK. CORRECTIVE ACTION: REPLACED INTERCOSTAL ON FRAME 16 LT SIDE DOOR STOP 7 AT FWD GALLEY AREA, AS PER SRM A320 51-72-11 AND DRAWING D53112300 ISSUE "HOO" RELEASE DATE 30JUN98 AND PRI 587497-14AD REV 0 AND ER/A 587497-14AD REV ORIGINAL.
CRACK INDICATION ON FRAME 16 RT SIDE DOOR STOP 7 HOLE 3 AT FWD GALLEY AREA. CORRECTIVE ACTION: C/W ER/A 587495-14AD.
CRACK INDICATION ON FRAME 16 RT SIDE DOOR STOP 7 HOLE ?1 AT FWD GALLEY AREA (1 EA), CRACK AT 8 O CLOCK, REQUESTING REPAIR DISPOSITION REPAIR. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING ON FRAME 16 RT SIDE DOOR STOP 7 AT FWD GALLEY AREA (1E/A), AS PER PRI 587495-14AD REV 0 AND ER/A 587495-14AD REV ORIGINAL.
NICK EXTERNAL SKIN BETWEEN STRG 42L AND STRG 43L AND 4.5 INCH AHEAD OF FR 26 AT LOWER FUSELAGE (2 EA). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN STR 42L AND STR 43L AND BETWEEN FR 23 TO FR 23 AT LOWER FUSELAGE, AS PER PRI 587690-14 REV O AND ER/A 587690-14 REV ORIGINAL.
SHIP 3278 A CRACK WAS FOUND IN FR 16 RHS AT HOLE B. CORRECTIVE ACTION: COMPLIED WITH ERA 587478-14AD. (1615327)
CORROSION HINGE FITTING LUG NR 2 ELEVATOR ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) OF HINGE FITTING NR 2 ELEVATOR RT HORIZONTAL STABILIZER, AS PER AIRBUS CMM 55-21-15.
SHIP 3278, GOUGE EXTERNAL SKIN AT LEVEL OF FR23 AND STRG 23L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL OF STR.23L FR 23 ON UPPER FUSELAGE, AS PER PRI 587548-14 REV. 0 AND ER/A 587548-14 REV ORIGINAL.
SHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LT T ANGLE POSITION, IN MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON SECTION I PERMANENT REPAIR ON FR.42 AT AFT LT SIDE "T" ANGLE POSITION IN MAIN WHEEL WELL, AS PER PRI 587574-14AD REV.O AND ER/A 587574-14AD REV ORIGINAL.
CORROSION INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT. CORRECTIVE ACTION: REPLACED INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT, AS PER A320 FAM AMM 21-26.
SHIP 3278, CRACK ACCESS PANEL 413DL ON LT PYLON. CORRECTIVE ACTION: REPAIRED BY WELDS ACCESS PANEL 413DL ON LT PYLON, AS PER ER/A NO.540187-14MA REV. ORIGINAL SECTION I.
SHIP 3278, CRACK ANGLE AFT TI ANGLE AT FR 42 RT SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: REPLACED TI ANGLE LOC AFT FR 42 RT SIDE IN MAIN WHELL WELL THE REPLACE WAS DOCUMENTED ON AMDS CARD 5353-01006-03.
SHIP 3278, CORROSION SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUE C00.
SHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT UPPER RT TI ANGLE POSITION AT MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A N. 587552 14 AD REV ORIGINAL SECTION I AND PRI N. 587552-14 AD REV O.
SHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LOWER RT TI ANGLE POSITION IN MAIN WHEEL WELL. PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A NO. 587552-14AD REV ORIGINAL SECTION I AND PRI N. 587552-14AD REV O.
SHIP 3278, CORROSION SHEAR TIE LOCATED AT FR 33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUE C00.
CORROSION WEB SUPPORT LOCATED AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED WEB SUPPORT AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11-001 AND DWG # D53112783, ISSUE F00 RELEASE DATE:28-MAY-98.
CORROSION SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. AS PER A320 SRM 51-72-11 AND DWG D53112786, ISSUE B00.
CORROSION SEAT TRACK -Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53112814 RELEASE DATE:14-MAR-03, ISSUE:B00 AND DWG D53110920, RELEASE DATE:07-DEC-99, ISSUE D00.
CORROSION FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG # 53472845 ISSUE A RELEASE DATE 02APR98
CORROSION SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED (FLOOR BEAM) SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA ASPER SRM A320 51-72-11 AND DRAWINGS # D53112812 ISSUE E00 RELEASE DATE 08JAN97, D53110984 ISSUE C00 RELEASE DATE 25JUN05 AND D53110920 ISSU D00 RELEASE DATE 07DEC99
CORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR68 TO FR69 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162.5 LOC BTW FR68 TO FR69 AT AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG #D53472458 ISSUE E RELEASE DATE 09MAY11 DWG # D53472089 ISSUE L RELEASE DATE 02OCT13 DWG # D53474180 ISSUE V RELEASE DATE 05FEB20
DURING S/C FOUND FWD EMER LIGHT BATTERY PAK INOP, R&R RWD BATT PAK
AFTER LANDING "DOOR L AFT CABIN" SHOWED OPEN FOR 2-3 MIN THEN WENT BACK TO CLOSED. F/A SAID DOOR WAS CLOSED AT ALL TIMES. ( ALSO SMOOTH LANDING). CYCLED DOOR, INDICATIONS NORMAL AT THIS TIME, REF A320 AMM 320 AMM 52-10.
(LP# 0883275) UPPER FUSELAGE LEFT HAND SIDE 2'X2' DENT IN FUSELAGE SKIN AT STRINGER 5L ST 1976 FR44. SEE NR FOR ADDITIONAL INFORMATION. CUT OUT DENTED SKIN. FABRICATED DOUBLER. INSTALLED STRINGER SPLICE AND DOUBLER REPAIR IAW SRM 53-31-11-300-01,
(LP# 0878548) UPPER FUSELAGE SURROUNDING SKIN AT FORWARD GPS ANTENNA MISSING PAINT AND PRIMER WITH DISCOLORATION IN SKIN. SEE NR FOR ADDITIONAL INFORMATION PREPPED AND PAINTED AREA.
WEAR ON TRAILING EDGE SLAT 3 IB SIDE ON LT WING. PERFORMED PERMANENT REPAIR ON SLAT NR 3 ON LT WING PER ER/A 553516-14 REVISION ORIGINAL.
EMERGENCY LIGHT FWD L EPSU UNIT FAULT, REPLACED FWD LEFT EPSU 10WL
SEAT ROW EMERGENCY LIGHT INOPERATIVE AT SEAT ROWS 1AB, 11ABC, 13ABC. REPAIRED THE CONNECTORS AT SEATS 1AB, 11ABC AND 13ABC.
DURING INSPECTION, FOUND CORROSION ON WEB, FRAMES 62 - 63 STRINGER 38R. REPLACED THE IAW SRM 51-72-11 AND DWG E53470321.
DURING INSTALLATION OF ACCESS PANEL 540HB BETWEEN RIB 13 AND RIB 14, FOUND BRIDGE PLATE IMPROPERLY INSTALLED. PERFORMED PERMANENT REPAIR, BRIDGING PLATE, ON INTERNAL AREA OF FUEL TANK BETWEEN RIB 13 TO RIB 14 ON POSITION OF ACCESS PANEL NR 540HB, LT WING IAW SRM 57-21-11, PARA 5.B (7), FIG 202.
DURING INSPECTION, FOUND CORROSION ON WEB -Y1732 BETWEEN FRAMES 12 TO 16. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53112545.
DURING INSPECTION, FOUND WEAR ON FWD MLG DOOR FITTING LT LOCATED ON MLG BAY. REPLACED FWD FITTING MLG DOOR ATTACHMENT LT SIDE LOCATED ON MLG BAY, SRM 51-72-11 AND DWGS N. D53370600 AND D53370622.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53111461 AND D53110984.
DURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORT BETWEEN FRAME 66 AND 68. REPLACED IAW SRM 51-72-11, DWG D53480505, AND D53470150.
DURING INSPECTION, FOUND WEAR ON RT WING NR 4 SPOILER CENTER FITTING STOP BOLT. REPAIRED IAW SRM 57-70-00, PARAGRAPH 5.C, FIG 201, SHEET 2.
DURING INSPECTION, FOUND WEAR ON FWD MLG DOOR FITTING RT LOCATION ON MLG BAY. REPLACED FWD MLG DOOR FITTING RT LOCATION ON MLG BAY IAW 51-72-11 AND DWG D53370600.
DURING INSPECTION, FOUND WEAR ON LT WING NR 4 SPOILER CENTER FITTING STOP BOLT. REPAIRED THE FITTING STOP BOLT IAW SRM 57-70-00, PAR 5C, FIG 201, SHEET 2.
DURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORT BETWEEN FRAMES 66 AND 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.
CORROSION ON AFT FACE FRAME 16 AT LEVEL STRINGER 23R. REPAIRED IAW ER/A.
CORROSION ON FLOOR PANEL 261FF. REPLACED THE FLOOR PANEL.
CORROSION ON FLOOR PANEL 262FF. REPLACED FLOOR PANEL.
CORROSION ON CABIN FLOOR PANEL 221FF. REPLACED THE FLOOR PANEL.
CORROSION ON SEAT TRACK -Y765 LOCATED BETWEEN FRAMES 64 - 66+5. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472229.
AFTER REMOVAL OF SHEAR PLATE, FOUND CORROSION ON SUPPORT FRAME LOCATED BETWEEN FRAMES 69 - 70 STRINGER 23R. REPLACED THE SUPPORT FRAME IAW SRM 51-72-11 AND DWG D53470100.
CORROSION ON FLOOR SUPPORT -Y765 BETWEEN, FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
CORROSION ON CABIN FLOOR PANEL 222FF. REPLACED THE CABIN FLOOR PANEL.
DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472832.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+17 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.
DURING INSPECTION, FOUND CORROSION ON COUPLING AT STRINGER 44 AND FRAME 27+12. REPLACED THE COUPLING IAW SRM 51-72-11 AND DWG D53231598.
DURING INSPECTION, FOUND CORROSION ON WEB Y1732 BETWEEN FRAMES 20 - 24. REPLACED THE WEB IAW SRM 51-72-11, D53112783 AND D53112545 .
DURING INSPECTION, FOUND CORROSION ON WEB -Y1732 BETWEEN FRAMES 20 - 24. REPLACED THE WEB IAW SRM 51-72-11, DWG D53112783, D53112545 AND D53110920.
DURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 66 - 68 . REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D534 80019 .
DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 LOCATED BETWEEN FRAMES 47 - 64, FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWGS D53470080, D53472000, AND D53472832.
FOUND CORROSION ON AFT LOWER CORNER FITTING ON FRAME 68 AT STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN -Y1162 TO -Y1292 AND FRAMES 66+5 - 67+17. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.
DURING INSPECTION, FOUND CORROSION ON AFT CORNER FRAME 68 . REPLACED AFT CORNER IAW SRM 51-72-11 AND DWG D53480019.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53918123 AND D53110920.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN Y1162 TO Y1292 AND FRAMES 66+5 - 67+17. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 UPPER FLANGE LOWER SURFACE LOCATED BETWEEN FRAMES 67+17 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.
DURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y189 BETWEEN FRAMES 20 - 23. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53111406.
DURING INSPECTION, FOUND CORROSION ON WEB Y1732 BETWEEN FRAMES 12 - 16. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D531 12545.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292, BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.
DURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 16 - 20. REPLACED THE CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.
DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 LOCATED BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.
FOUND CORROSION ON SUPPORT STRUCTURE BETWEEN FRAMES 69 - 70. REPLACED THE SUPPORT IAW SRM 51-72-11 AND DWG D53470100.
DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS AND REPLACED IAW SRM 51-72-11 AND DWG D53370500.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24 . REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812, D53110984.
DURING INSPECTION, FOUND AFTER REMOVED LOWER SILL OF L2 AFT GALLEY. PERFORMED A VISUAL INSPECTION ON ADJACENT AREA AND FOUND CRACK ON SECTION CONNECTION LOCATED AT LEVEL OF FR 68, Y1162.
DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT -Y81 BETWEEN FRAMES 12 - 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG N.D53112828, AND D53110984.
DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT Y254 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110984.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT COVER -Y81 BETWEEN FRAMES 12 & 16. REPLACED THE COVER IAW 51-72-11 AND DWG D53112620.
DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y503.2 BETWEEN FRAMES 12 - 16.
DURING SERVICE CHECK, F/C PAX SEAT 1B AFT EMERGENCY LIGHT INOPERATIVE. FOUND UNDERSEAT CONNECTOR WIRE BROKEN & CONNECTOR DAMAGED. REPLACED LIGHT ASSY AT 1B AND FUNCTIONAL CHECKED NORMAL.
CORROSION FOUND UNDER AFT CARGO BIN FLOOR FRAMES 56 & 57 AND AT STRINGER 42L. REMOVED CORROSION, MANUFACTURED A DOUBLER, TREATED AND PRIMED. INSTALLED THE STRINGER REPAIR IAW SRM.
DURING NON ROUTINE CHECK, FOUND ROW 24 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR, MX INSTALLED NEW SPLICE AND FUNCTIONAL CHECK WAS NORMAL.
DURING NON ROUTINE CHECK, FOUND ROW 5C EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
CATERING REPORTS CRACK IN RT AFT LOWER CORNER OF SERVICE DOOR. CUT OUT DAMAGED SKIN 1" BY 1.625" PER SRM 5210-00 FIG 203, 730014. FABED DOUBLER FROM 2024T3 .125 AND FILLER FROM 2024T3 .100, AND PRIMED PER SRM 52-10-00. ACCOMPLISHED REPAIR IAW A320 SRM 52-10-00.
DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 2 INOPERATIVE. MX REPAIRED A BROKEN WIRE AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
EMERGENCY PATH LIGHT SEAT 2B IS INOP, SECURED LOOSE CONNECTION AND CHECKS OK.