N366NW
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
DE - DUE TO BRAKES AUTO BRK FAULT ECAM WARNING. REPLACED NORMAL BRAKE SERVO VALVE (15GG) AND BSCU (10GG). (LP: 8749444, AIRCRAFT WAS GROUNDED).
DIV - DUE TO LOUD POPPING NOISE FROM THE LEFT OVERWING EMERGENCY EXIT DOOR. NO PRESSURIZATION ISSUES REPORTED. UPPER WING TO BODY FAIRING PANEL 191DT WAS FOUND DAMAGED WITH LARGE CHUNKS MISSING, BUT NOT A TOTAL PANEL LOSS. : MAINTENANCE IN PROGRESS. (LP: 8648856). AIRCRAFT WAS GROUNDED
ER/A 482536-14 IS NOW AT REVISION LEVEL C. NEW INSPECTIONS REQUIRED. INITIAL INSPECTION REQUIRED WITHIN 54,800 TFC OR 113,100 TFH, WHICHEVER OCCURS FIRST; REPETITIVE INSPECTION REQUIRED WITHIN 3,300 FC OR 6,600 FH THEREAFTER, WHICHEVER OCCURS FIRST. ASSOCIATED ER/A 00-482536 ADDED FOR AC 3266. (LP: 1553977). AIRCRAFT WAS GROUNDED
NR 1 ENG DRAIN MAST MISSING. INSTALLED DRAIN AT AFT END OF DRAIN MAST IAW AMM 71-73, A/C OK FOR SVC. (LP: 8108788)
EPSU BATTERY EMER L FAULT ON EMERGENCY LIGHTS TEST. C/A: R/R BATTERY PACK AR 11WL EPSU PER A320 AMM 33-51. TESTS PASS. (LP: 6684007)
SHIP 3266 DISC: L1 DOOR ASSIT REQUIRES SERVICE. C/A: SERVICED L1 DOOR REF A320 AMM 52-10. OK FOR SVC. (LP: 7404911)
SHIP 3266 DISC: FOUND 19D EMERGENCY LIGHT HANGING DOWN. C/A: REPLACED EMERGENCY LIGHT HOUSING. LIGHT CHECKS GOOD AND OK FOR SERVICE. (LP: 0820847)
SHIP3266 DISC: EMERGENCY LIGHT IN SEAT 24D BROKEN OFF OF BOTTOM OF SEAT. C/A: RESECURED EMER. LIGHT AS REQUIRED. (LP: 6396804)
SHIP 3266 DISC: CRACK INDICATION ON FRAME 4 LH SIDE IN UPPER ATTACHMENT HORIZONTAL ST IFFENER. CRACK DIMENSIONS ARE: X1: 0.438 INCH APPROX, X3: 0.356 INCH A PPROX. AD RELATED. IN COCKPIT (1 EA). AA CARD 5316-01052-05A. C/A: COMPLIED WITH ER/A 544200-14AD REV. C APPROVED DATE: 24-JAN-25 MATCHES WITH ALL STEPS ON PRI 544200-14AD REV.0, REV.1, REV.2 ITIS BEEN VALIDATED. PERFORMED PERMANENT REPAIR INSTRUCTIONS LOC . ON FR4 LH LATERAL WINDOW FRAME UPPER ATTACHMENTS STIFFENER ASPER ER/A 544200-14AD REV. C SECTION V HAS BEEN COMPLIED. SEE LOG PAGE: 0776194 FOR TIME CONTROLLED ITEMS SECTION DTE. TOOL USED:UT EQUIPMENT P/N:45MG S/N: 232017609 DUE DATE: 08-OCT-25 MICROMETER P/N: 293-345-30 S/N: 71699816 DUE DATE: 11 MAR 25 . SEEINDIVIDUAL SIGN-OFF ON ORNRC 54/200 RII INSPECTION COMPLETE JOB COMPLETE. (LP: 0780063)
SHIP 3266 DISC: *DTE* DURING H2 AND WHILE INSPECTING PER EM 5316-01052-05A 2 EA CRACK INDICATIONS FOUND EMATATING FROM TEH SPOT FACE OF HOLE 1 AT THE UPPER FWD CORNER OF LHS FR4 LATERAL WINDOW FRAME. C/A: ***DTE REQUIRED*** PER SECTION DTE OF 544200-14, REV C, THE REPAIR OF SECTION V IS LIMITED TO 26,200 FC FROM SECTION V (15JAN25). ADDITIONAL ENG'G AUTHORIZATION REQUIRED FOR SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 32-544200 ADDED FOR AC 3266. (LP: 0776194)
SHIP 3266 DISC: EXISTING REPAIR ON FR68 LH AT LEVEL DOOR STOP FITTING 1 ON OPEN HOLES H1= 0.280, H2= 0.280 , H3= 0.280 AND H4= 0.280 AA 5311-01216 AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT ENGINEERING EVALUATION REQUIRED, CONTACT LIAISON ENGINEERING FOR FURTHER DIRECTION. C/A: VERIFIED EXISTING REPAIR ON DOOR STOP 1 FR68 LH MEET ALL REQUIREMENTS AS PER A320 SRM 53-41-12-300-011 AND A320 SRM 53-41-12-300-012. TOOK MEASURES ON EXISTING HOLES H1= FRAME: 0.282 INCH, REPAIR PART:0.281 INCH; H2 = FRAME AND REPAIR PART:0.281 INCH; H3= FRAME AND REPAIR PART: 0.281 INCH; H4= FRAME AND REPAIR PART: 0.281 INCH.TOOL USED: SMALL HOLE GAUGE P/N:2205A5,S /N:AE-420873, DUE DATE: 30-AUG-25; MICROMETER P/N: 293-344-30, S/N: 77011101, DUE DATE: 23-MAR-25. PERFORMED ROTOTEST INSPECTION IN OPEN HOLES (4EA) H1 TO H4 ON FR68LH AT LEVEL DOOR STOP #1 AS PER NTM 51-10-01. CRACK INDICATION NOT FOUND. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200053402, DUE DATE:16-SEP-25. RII INSPECTION COMPLETE 0294551 AE166QC JOB COMPLETE. (LP: 0767900)
SHIP 3266 DISC: DETERIORATED STUD OF SLIDE RAFT PASSENGERS CREW DOOR 831, 841, 832 (6EA) (REFERENCE RII AMDS CARD 5219-7089-LA,RF, LF.). C/A: OBTAINED NEW HARDWARE STUD OF SLIDE RAFT PASSENGERS CREW DOOR 831, 841, 832 (6EA) AS PER A320 FAM IPC 25-62-04-02D AND THEINSTALLATION IS ACCOMPLISHED IN AMDS CARD 5210-7089. LA,RF,LF. STEP 27.C.(7)(B)(4) THRU STEP 27. C.(7)(B)(6) RII INSPECTION COMPLETE 0920413 AE352QC JOB COMPLETE. (LP: 0752324)
SHIP 3266 DISC: DOESNT WORK CORRECTLY. DAMPER PASSENGER CREW DOOR 832 (REFERENCE RII AMD S CARD 5210-7089-LA) AT AFT GALLEY AREA. C/A: REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13-14-000-001-B AND AS PER A320 FAM AMM52-13-14-400-001-B . JOB COMPLETE. (LP: 0736388)
ACRID SMELL REPORTED BY MULTIPLE FLT ATTN. MID CABIN ONLY. C/A: C/W MD LOG REF LOG 0535670 FOR MTC PERFORMED. APU REPLACED.
SHIP 3266 DSIC: CABIN SMELLS LIKE MOLDY AND DAMP WHEN AIR IS ON. FIRST CLASS/ COMFORT+ ARE THE WORST SECTIONS. C/A: FAINT SMELL PRESENT UPON ARRIVAL TO A/C. PER MC REQIUST AMDS CARDS 4900-2011 AND 2100-2005. REF LOG 0525881. INSPECTION OF APU SHOW SIGNS OF OIL IN PLENUM AND APU BLEED VALVE. /UBE WIP 906371. THIS LOG TRANSFERRED TO MD LOG 0525881 FOR SMOKE /FUME ODI EVENT. (LP: 0525424)
SHIP 3266 DISC: UNUSUAL ODOR/DIRTY SOCK SMELL WHEN APU BLEED ON WHILE AT THE GATE. C/A: C/W W/C 4916-2001 (D. EDWARDS 794502) C/W W/C 4900-2001, FOUND OIL LEAK COMING FROM APU OIL HEATER. R/R APU OIL HEATER PER A320 AMM 49-96. LEAK AND OPS CHK GOOD. MEL AND PLACARD REMOVED, NO " M" PROCEDURES. CONTACED MCC FOR ODI ALERT, SPOKE WITH SARGE. A/C OK FOR SVC. (LP: 6029130)
DIRTY SOCK SMELL AT THE GATE. C/A: C/W AMDS W/C 0550-2002. FOUND OIL CONTAMINATION IN APU. PERFORMED ECS DECONTAMINATION PER AMDS W/C 2100-2005. NO ADDITIONAL FINDINGS @ THIS TIME OK FOR CONTINUED SVC.
SHIP 3266 DISC: SHORTLY AFTER T/O VHF1 WENT INOP NO INDICATION OTHER THAN UNABLE TO HEAR OR TRANSMIT. C/A: UPON ARRIVAL FOUND VHF1 ANTENNA DEPARTED AIRCRAFT. PERFORMED VISUAL INSPECTION FOR DAMAGE FROM DEPARTED ANTENNA, NONE FOUND. REPLACED VHF 1 ANTENNA REF A320 AMM 23-12. REPAIRED VHF 1 ANTENNA COAX CONNECTOR PER ESPM 20-44-32. OPS CHECK GOOD. A/C OK FOR SVC. (LP: 6206048)
SHIP 3266 DISC: SMOKE FUMES SMELL IN THE AFT OF THE AIR CRAFT, SOME HAZE ROW 30 AFT. LIKE A PLASTIC/BURNING SMELL. HAPPENED AFTER DEPLANING AND AFTER SECURITY CHECKLIST COMPLETED. C/A: R&R VACUUM GEN PER A320 AMM 38-31 OPS CHECK GOOD THIS CLEARS MEL 38-30-01D "M" PROCEDURES REVERSED PLACARDS REMOVD DISPATCH APPROVED. A/C OK FOR SVC. (LP: 5103182)
SHIP 3266 DISC: STAGE III DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAI R INSTALLED AT FR68 STOP 1, S-22LH PER ER/A 614779-14AD SECTION III. C/A: SECTION III OF ER/A 614779-14AD TO BE REVISED PRIOR TO 61500FC F ROM 08JAN24 ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01244 ADDED FOR AC 3266 ASSOCIATED ER/A 14-614779 ADDED FOR AC 3266. (LP: 0147257)
SHIP 3266 DISC: STAGE III DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAI R INSTALLED AT FR68 STOP 1, S-22LH PER ER/A 614779-14AD, SECTION IV. C/A: SECTION IV OF ER/A 614779-14AD TO BE REVISED PRIOR TO 47300FC FR OM 08JAN24 ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01244 ADDED FOR AC 3266. (LP: 0147262)
SHIP 3266 DISC: ER/A 614779-14AD ISSUED FOR REPAIR INSTALLED AT FR68, STOP 1, S- 22LH. FOLLOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION IV EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01244 ADDED FOR AC 3266 ASSOCIATED ER/A 14-614779 ADDED FOR AC 3266. (LP: 0147264)
SHIP 3266 DISC: STAGE III DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAI R INSTALLED AT FR68 STOP 1, S-22LH PER ER/A 614779-14AD, SECTION II. C/A: SECTION II OF ER/A 614779-14AD TO BE REVISED PRIOR TO 37900FC FR OM 08JANUARY24 ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01244 ADDED FOR AC 3266. (LP: 0147255)
SHIP 3266 DISC: AD RELATED: (5311-01244-01A) L/H FR.68 STGR 22L/H, FRAME WEB HORIZONTAL FLANGE CRACKED AT LOWER RADIUS I/B SIDE APROX" 1.0" IN LENGTH. "REQUESTING REPAIR DISPOSITION, ADDITIONAL ENGINEERING DOCUMENTATION REQUIRED, AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311-01244. WORK SECTION 01A, 2B A320-53-1491 REV 01, AND FAA AD 2022-15-05, EASA AD 2020-0030". C/A: COMPLIED WITH ALL STEPS OF PRI 614779-14AD REV. 0 AWAITING FINAL ER/A. V.STREET 2501233 - REVEIVED FINAL ER/A 614779-14AD REV, 0 IT MATCHES PRI 614779-14AD REV. O ALL WORK COMPLETE. (LP: 0147478)
SHIP 3266 DISC: F/A'S REPORT SULFUR SMELL FWD CABIN C/A: PERFORMED TYPE 9 SECTION INSPECTION FOR WORKCARD 0550-2002 - IDENTIFY AND TROUBLESHOOT SMOKE AND FUMES IN COCKPIT AND / OR CABIN. CONTACTED MCC WITH TYPE 9 SECTION COMPLETE AND MCC GOOD WITH WORK PERFORMED. ALL WORK PERFORMED IN ACCORDANCE WITH A320 W/C 0550-2002. NO SMELL NOTED. (LP: 0070033)
SHIP 3266 FOUND R2 DOOR SLIDE HANGING DOWN ON FLOOR DURING SERVICE CK CABIN WALK AROUND. CORRECTIVE ACTION: R/R DOOR SLIDE PER A320 AMM 25-61. (4585588)
SHIP 3266 - HYD/MISC/DE - DUE TO HYD G RSRVR LO LVL ECAM MESSAGE. CORRECTIVE ACTION: FOUND GREEN SYSTEM PTU MANIFOLD PRIORITY VALVE LEAKING. R/R PRIORITY VALVE (1064GM), LEAK CHECK GOOD. OK FOR SERVICE. (4384136)
SHIP 3266 FLAP LEVER VERY DIFFICULT TO MOVE FROM FLAPS 1 TO 2 AND 3 TO FULL. CORRECTIVE ACTION: CLEANED DIRT AND DEBRIS FROM FLAP CHANNEL AND DETENT. OK FOR SERVICE. (9498449)
SHIP 3266 NOTIFY OF MAJOR REPAIR INSTALLATION ONLY OF ANTENNA FOR VIASAT WIFI INSTALLATION PER WORK CARD #4430-01007-01D. CORRECTIVE ACTION: COMPLIED WITH DELTA WORK CARD AMDS 4430-01007-01D. OK FOR SERVICE. (2441642)
SHIP 3266 DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595131-14AD. (2250355)
SHIP 3266 DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595131-14AD. (2250360)
SHIP 3266 DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595131-14AD. (2250347)
SHIP 3266 DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595131-14AD. (2250339)
SHIP 3266 DAMAGE AT FR35 BULKHEAD AND STR-30LH AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 595131-14AD. (2250351)
SHIP 3266 EXIT LIGHT ABOVE DOOR 2R INOP. CORRECTIVE ACTION: REPLACED EPSU (13WL) & BATTERY PER A320 AMM 33- 51. OPS CHECK GOOD. (8847712)
SHIP 3266 EXIT LIGHT OVER 2L DOOR INOP. CORRECTIVE ACTION: INSTALLED L/H EPSU. OPS CHECK GOOD. (7854532)
SHIP 3266 EXIT LIGHT OVER DOOR 2R INOP. CORRECTIVE ACTION: R/R ESPU. OPS CHECK GOOD. (7854533)
SHIP 3266 2L EVACUATION SLIDE BUSTLE COVER LOOSE. CORRECTIVE ACTION: SECURED COVER. DOOR IS OK FOR SERVICE. (2094648)
SHIP 3266 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/INOP AT SEAT LOCATIONS 22D. CORRECTIVE ACTION: REPAIRED AND STOWED WIRES. OPS CHECK GOOD. (2094361)
SHIP 3266 RT PYLON UPPER IB CHANNEL CRACKED. CORRECTIVE ACTION: REPLACED RT PYLON UPPER I/B CHANNEL IAW A320 SRM 51-44-11. (2052030)
SHIP 3266 EXTERIOR FUSELAGE UPPER CROWN OUTER SURFACE AT FR 69+18 STGR 1R-2R HAS CORROSION. CORRECTIVE ACTION: COMPLIED WITH DELTA ERA 595543-14 REV. ORIGINAL. (2048484)
SHIP 3266 INTERNAL FUSELAGE DOOR STRUCTURE UPPER SURFACE AT FR 16 STGR 20 HAS CORROSION. CORRECTIVE ACTION: R/R INTERNAL FUSELAGE L-1 DOOR LOWER SILL FITTING IAW A320 SRM 51-42-00. (2048640)
SHIP 3266 EXTERIOR FUSELAGE UPPER CROWN OUTER SURFACE AT FR 69+18 STGR 1L- 2L HAS CORROSION. CORRECTIVE ACTION: COMPLIED WITH DELTA ERA 595543-14 REV ORIGINAL PART B. (2048479)
SHIP 3266 COMPLY WITH WORKCARD AMDS 53311-01239-01B (HOLE CRACKS). CORRECTIVE ACTION: COMPLIED WITH AMDS 53311-01239-01B. (2044114)
SHIP 3266 CRACK-LIKE INDICATION NOTED IN HOLE "C" OF R/H SIDE FR 16 AT 9 O'CLOCK LOOKING INBOARD, FROM OUTSIDE OF AIRCRAFT. CORRECTIVE ACTION: COMPLIED WITH DELTA ERA 594895-14AD REV ORGINAL. (2044119)
SHIP 3266 DTA MONITOR INSPECTION REQUIRED PER ER/A 595543-14. CORRECTIVE ACTION: COMPLIED WITH ERA. (2047270)
SHIP 3266 CRACK ON FWD CARGO COMPARTMENT FRAME 35 (L/H SIDE), FWD SIDE OF WEB. CORRECTIVE ACTION: COMPLIED WITH DELTA ERA 595131-14AD. (2043807)
SHIP 3266 NEED TO COMPLY WITH ER/A 595131-14. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2039533)
SHIP 3266 NOSE FWD FUSELAGE / FR16RH AT DOOR STOP NO 7 LEVEL, DOUBLE JOGGLE AREA / FASTENER HOLES 7, A & C / CRACK & ELONGATION. CORRECTIVE ACTION: COMPLIED WITH ER/A 594895-14. (2031392)
SHIP 3266 AFT CABIN UTILITY AREA FLOOR BEAM Y-1292 AT FR 66 HAS CORROSION. CORRECTIVE ACTION: R/R FLOOR BEAM PER A320 SRM 51-42-11. (2029390)
SHIP 3266 AFT CABIN UTILITY AREA FLOOR BEAM Y765 AT FR68 HAS CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (2029378)
SHIP 3266 AFT CABIN UTILITY AREA FLOOR BEAM Y-1292 AT FR67 +4 HAS CORROSION. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK PER A320 SRM 51-42-11. (2029370)
SHIP 3266 FWD CABIN UTILITY AREA FLOOR BEAM Y-765 AT FR 20 HAS CORROSION. CORRECTIVE ACTION: R/R FLOOR BEAM PER A320 SRM 53-11-15. (2029448)
SHIP 3266 LH LOWER W/B SUPPORT STRUCTURE VERTICAL ANGLE CRACKED. CORRECTIVE ACTION: R/R L/H LOWER W/B SUPPORT STRUCT VERTICAL ANGLE IAW A320 SRM 51-42-11. (2029220)
SHIP 3266 FWD CABIN UTILITY AREA FLOOR BEAM Y1292 AT FR 20 HAS CORROSION. CORRECTIVE ACTION: R/R SEAT TRACK PER A320 SRM 53-00-14, 53-11-15, 51-42-11. (2029512)
SHIP 3266 AFT CABIN UTILITY AREA PASS/CREW L2 DOOR SILL AT FR68 HAS CORROSION. CORRECTIVE ACTION: REPLACED DOOR SILL PER A320 SRM 51-42-11. (2029497)
SHIP 3266 FWD CABIN UTILITY AREA FLOOR BEAM Y765 AT FR20 HAS CORROSION. CORRECTIVE ACTION: R/R SEAT TRACK PER A320 SRM 53-00-14, 51-42-11, 51-21-00. (2029459)
SHIP 3266 FWD CABIN UTILITY AREA FLOOR BEAM Y-1292 AT FR20 HAS CORROSION. CORRECTIVE ACTION: R/R SEAT TRACK PER A320 SRM 53-00-14, 51-42-11, 51-21-00. (2029440)
ESTABLISH MONITOR FRAME 60-61 ALONG STR 44 REQUIRES INSPECTION THIS REPAIR IS A CATEGORY B WITH SUBSEQUENT INSPECTIONS. ACCOMPLISHED INSPECTION REQUIREMENTS IAW A320 SRM 53-00-11 REPAIR WAS INSTALLED PER A320 SRM 53-00-11-300-029 AND AA 2335- 01033-05 ACCORDING TO ERA 575670-14 REPAIR IS A CATAGORY B REPAIR WITH SUBSEGMENT INSPECTIONS SEE LOG PAGE # 2019766. (LP: 2028322) AIRCRAFT WAS GROUNDED
SHIP 3266 AFT CABIN UTILITY AREA FLOOR BEAM Y1292 AT FR 68 HAS CORROSION. CORRECTIVE ACTION: R/R AFT CABIN FLOOR BEAM PER A320 SRM 51-42-11. (2022410)
SHIP 3266 AFT CABIN UTILITY PASS/CREW DOOR SILL AT FR68 HAS CORROSION. CORRECTIVE ACTION: REPLACED WITH NEW DOOR SILL PER A320 SRM 51-42-11. OK FOR SERVICE. (2018615)
SHIP 3266 MAIN CABIN TOP BEAM -Y765 AT FR-68 IS CORRODED AROUND FASTENER HOLE. CORRECTIVE ACTION: REPLACED WITH NEW FLOOR BEAM PER A320 SRM 51-42-11. (2017538)
SHIP 3266 #2 PYLON SPIGOT BEARING CORRODED AND FROZEN IN RACE. CORRECTIVE ACTION: R/R LOWER SPIGOT FITTING IAW A320 SRM 54-51-12. JOB COMPLETE. (2015337)
SHIP 3266 LT PYLON SPIGOT FITTING BEARING HAS CORROSION AND IS FROZEN IN BEARING. CORRECTIVE ACTION: R/R LT PYLON SPIGOT FITTING IAW SRM 54-51-12. (2015375)
SHIP 3266 NEED TO ACCOMPLISH STEP 20 OF AMDS 5311-01229-06 DUE TO CRACK INDICATION AT DOOR STOP #7, FR16, RH SIDE HOLE #3 IN THE INTERCOSTAL. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01229-06. (1753117)
SHIP 3266 NEED TO ACCOMPLISH STEP 20 OF AMDS 5311-01229-02 DUE TO CRACK INDICATION AT DOOR STOP #7, FR16, LH SIDE HOLE #1 IN THE INTERCOSTAL. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01229-02. (1752420)
SHIP 3266 ACCOMPLISH STEP 20 OF AMDS 5311-01229-05 DUE TO CRACK INDICATION AT DOOR STOP #1, FR16, RH SIDE HOLE #3 IN THE INTERCOSTAL. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01229-05. (1750180)
SHIP 3266 CRACK INDICATION AT DOOR STOP #1, FR16, LH SIDE HOLE #1 IN THE INTERCOSTAL. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01229-01. (1750184)
L2 SLIDE COVER STICKING OUT ON AFT SIDE. CORRECTIVE ACTION: TIGHTENED SLIDE BUSTLE STRAPS.
CRACK INDICATION ON FRAME 16 LH SIDE ON CROSSBEAM SPLICING AT HOLE 4 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTIONS AT FR 16 CROSS BEAM SPLICING ON HOLE 4(D) L/H SIDE PASSENGER CABIN AS PER ER/A 586039-14 REV ORIGINAL AND PRI 586039-14 REV O, REV 1 AND REV 2
CRACK INDICATION ON FRAME 16 LH SIDE ON CROSSBEAM SPLICING AT HOLE 3 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTION AT FRAME 16 CROSSBEAM SPLICING ON HOLE 3(C) L/H SIDE PASSENGER CABIN AS PER ERA 586039-14 REV ORIGINAL AND PRI 586039-14 REV 0, REV 1 AND REV 2
CRACK INDICATION ON FRAME 16 CROOSSBEAM SPLICING AT HOLE 2 AT FRAME 16LH SIDE IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTIONS AT FRAME 16 CROOSBEAM SPLICING ON HOLE 2(B) L/H SIDE PASSENGER CABIN AS PER ERA 586039-14 REV ORIGINAL AND PRI 586039-14 REV O, REV 1 AND REV 2
CRACK INDICATION ON FRAME 68 STGR 8 LH UPPER CORNER BETWEEN UPPER FASTENER AND UPPER RADIUS. CRACK LENGTH IS 0.130 INCH APPROX. AT AFT GALLEY AREA (1 EA), PERFORMED PERMANENT REPAIR LOC. ON FRAME 68 STRG 8LH UPPER CONER BETWEEN UPPER FASTENER AND UPPER RADIUS, AS PER SRM A320 53-41- 12- 300-012 FIGURE 003
CRACK INDICATION ON OPEN FASTENER HOLE AT Y 1292 AND 0.585 TO INB THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH , REPAIRD CRACK AS PER JOB CARD 5311-01171-04A AA 5311-01171, SB A320-53-1263, AD-2018-06-04
FWD CARGO COMPARTMENT CRACK FOUND AT HOLE A, REPAIRED CRACK AS PER JOB CARD 5311-01171-04A (AA 5311-01171, SB A320-53-1264, AD-2018-06-04)
ON APPROACH INTO LGA WE LOST TOTAL RADIO CONTACT. VHF #1, #2 AND #3 WOULD NOT WORK. TRIED MULTIPLE FREQUENCIES. ON SHORT FINAL WE FINALLY WERE ABLE TO COMMUNICATE ON VHF 1 WITH TOWER, R/R NBR 1 RMP
PDA PART DEPARTING AIRCRAFT, FLAP TRACK MOVEABLE FAIRING PIVOT COVER LEFT CENTER MISSING, INSTALLED COVER ON MOVAEBLE FAIRING PIVOT COVER
SHIP 3266 DURING INSPECTIONS PER 544937-14 REV ORIGINAL AND LOG PAGE 2420422 A NEW CRACK FOUND ON FR4 LATERAL WINDSHIELD VERTICAL STIFFENER. CORRECTIVE ACTION: COMPLIED WITH ER/A 32-544937. (0490552)
SHIP 3266 DURING INSPECTIONS PER 544936-14 REV ORIGINAL AND LOG PAGE 2420424 A NEW CRACK FOUND ON FR4 LATERAL WINDSHIELD VERTICAL STIFFENER. CORRECTIVE ACTION: COMPLIED WITH ERA 32-544936. (0490439)
CORROSION ON THE LOWER SILL AFT GIRT BAR FITTINGS FRAMES 16 TO 20, FWD GALLEY AREA, REPLACED THE DOOR SILL IAW SRM 51-42-11, 51-72-11, DRAWING D53110339, AND DRAWING D53112225.
CORRODED FLOOR SUPPORT +Y1162, FRAME 66+5 INCHES TO FR 67+15 INCHES, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.
EMERG LIGHTS AT SEAT ROWS 24DEF AND 25 DEF INOP, RECONNECTED CONNECTOR.
DURING SERVICE CHECK, HAD AFT LEFT EPSU MESSAGE ON F/A PANEL. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY AT AFT LEFT POWER SUPPLY,
DEBONDED PITCH TRIM ACTUATOR PRESSURE SEAL IN THS COMPARTMENT, REPLACED LOWER CLAW STOP ON THS ACTUATOR IAW AMM 27-44-51-400-003-A.
CORROSION ON SEAT TRACK +1292, FRAMES 47 TO 64 FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWGS D53472770, D53470080.
CORROSION ON LOWER SILL AT AFT GALLEY AREA ON STR 23L BETWEEN FRAME 66 TO FRAME 68. REPLACED LOWER SILL AT AFT GALLEY AREA ON STR 23L BETWEEN FRAME 66 TO FRAME 68 IAW SRM 51-72-11 AND DWG D53480019.
CORROSION ON LOWER SILL AT AFT GALLEY AREA ON STR 23R BETWEEN FRAME 66 TO FRAME 68. REPLACED LOWER SILL LOCATED ON STR 23R BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.
CORROSION ON MOVABLE FAIRING OF HORIZONTAL WEB INTERNAL AREA ON LT PYLON . REPLACED IAW SRM.
CRACK AFT ON LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. REPLACED AFT LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833, SEGMENT ANGLE, IAW SRM 51-72-11 AND DWG D52279040, D52279010.
CRACK AFT ON LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. REPLACED AFT ON LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DWG D52279010.
CRACK FWD VERTICAL FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN. REPLACED VERTICAL FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D5227-9055.
CORROSION ON STR 44, LOCATION BETWEEN FRAME 30 TO FRAME 31 IN FWD CARGO COMPARTMENT. REPLACED STR LT LOC BETWEEN FRAME 30+10" TO FRAME 35 IAW SRM 51-72-11 AND DWG D53231712.
CRACK AFT VERTICAL FRAME ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. REPLACED AFT VERTICAL FRAME ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.
CRACK FWD ON LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. REPLACED FWD LOAD TRANSMITTING PROFILE EMERGENCY EXIT DOOR 833, SEGMENT ANGLE, IAW SRM 51-72-11 AND DWG D52279040, D52279010.
CORROSION ON CENTER FITTING LT SIDE IN FWD GALLEY AREA FROM FRAMES 16 TO 20. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112225.
CORROSION ON LOWER FLOOR SUPPORT AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM.
CORROSION ON DUMMY RAIL Y503.2 IN FWD GALLEY AREA BETWEEN FRAMES 14 TO 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11 AND DWG D53112826.
CORROSION ON FLOOR SUPPORT 1292 AT FWD GALLEY AREA ON FRAME 20. REPLACED THE FLOOR SUPPORT BETWEEN FRAME 12 TO FR 24 AIAW SRM 51-72-11, DWG D53110984, AND D53112812.
REWORK OF EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAMES 68 TO 70 BETWEEN STRINGERS 25 - 28R . FOUND OUT LIMITS IAW SRM 53-41-11. PARA 4F FIG 108, SHEET1,ON P2. PERFORMED A PERMANENT REPAIR IAW SRM 53-41-11, PARA 5M FIG 214.
CORROSION ON FLOOR SUPPORT 765 AT FWD GALLEY AREA AT FRAME 20. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 24.
CORROSION ON DUMMY RAIL 81 AT FWD GALLEY AREA ON FRAME 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, SRM 51-72-11, SRM 51-42-11 AND DWG 53112828, D53110984.
CORROSION ON RAIL DUMMY -Y189 AT FWD GALLEY AREA BETWEEN FRAME 20 TO FRAME 21. REPLACED RAIL DUMMY -Y189 AT FWD GALLEY AREA BETWEEN FRAME 20 TO FRAME 21 IAW SRM 51-72-11 AND DWG D53111406.
CORROSION ON RAIL DUMMY -Y1379.5 AT FWD GALLEY AREA ON FRAME 16. REPLACED THE RAIL DUMMY IAW SRM 51-72-11 AND DWG D53112831.
CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 16 - 17. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53111462.
CORROSION ON SEAT TRACK +Y765 FRAMES 47 - 64 WAS FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 DWG D53472770 AND DWG D53470080.
ELONGATED HOLE ON CROSSBEAM SECTION FRAME 68. REPLACED THE CROSSBEAM SECTION IAW SRM 51-72-11 AND DWG D53474250.
CORROSION ON FLOOR SUPPORT -Y1225 IN AFT GALLEY AREA BETWEEN FRAMES 66+15 - 67+15". REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG: DS3472816.
CORROSION ON SEAT TRACK -Y765, FRAMES 47 - 64 FOUND OUT LIMITS IN PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWGS D53472770, D53472000.
CORROSION ON INTERNAL STRUCTURE DOUBLER IN FWD CARGO COMPARTMENT FROM FRAME 25 TO FRAME 26 BETWEEN STR 39R TO STR 41R. REPLACED INTERNAL STRUCTURE DOUBLER IN FWD CARGO COMPARTMENT FROM FR 25 TO FR 26 BETWEEN STR 39R TO STR 41R IAW SRM 51-72-11 AND DWG D53231767.
CORROSION ON FLOOR SUPPORT +Y512 AT AFT GALLEY AREA BETWEEN FRAMES 64 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.
CORROSION ON FLOOR SUPPORT -Y1162 AT AFT GALLEY AREA BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.
CORROSION ON FLOOR SUPPORT +Y1292 AT FWD GALLEY AREA ON FRAME 20+4. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11, SRM 51-42-11 AND DWG D53112812.
CORROSION ON WEB FRAME 20 LT SIDE AT FWD GALLEY AREA. REPLACED WEB LOCATED BETWEEN FRAME 20 TO FRAME 24 AT LEVEL STR 23L FWD GALLEY AREA FLOOR STRUCTURE IAW SRM 51-72-11.
CORROSION ON FLOOR SUPPORT +Y1225 AT AFT GALLEY AREA BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.
CORROSION ON FLOOR SUPPORT +Y1162 AT AFT GALLEY AREA BETWEEN FRAMSE 67+15 - FRAME 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
CORROSION ON SEAT TRACK Y1292, FRAMES 47 - 64 FOUND OUT LIMITS IN PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472077.
CORROSION ON FLOOR SUPPORT +Y254 AT FWD GALLEY AREA ON FRAME 17+2. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 24 AS IAW SRM 51-72-11, SRM 51-42-11 AND DWG D53112816.
ROW 14 SEAT, EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE HARNESS AS REQUIRED IAW ESPM 20-48-20. OPS CHECK WAS NORMAL.
DURING INSPECTION, FOUND SEAT 26C FLOOR PATH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN SPLICEAND FUNCTIONAL CHECK WAS NORMAL.
DURING NON ROUTINE CHECK, FOUND FAILED EMERGENCY LIGHT TEST OF BATTERY AT LT CABIN. MX REPLACED LEFT EMERGENCY BATTERY AND FUNCTIONAL CHECK WAS NORMAL.
DURING NON ROUTINE CHECK, FOUND AFT CABIN PAX DOORS NUMEROUS OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX REPLACED BULBS AND OPS CHECKED NORMAL.
DURING NON ROUTINE CHECK, FOUND THE EMERGENCY EPSU BATTERY FAILED TEST. MAINTENANCE REPLACED BATTERY PACK AND FUNCTION TESTED NORMAL.
AIRCRAFT 3266. DURING SERVICE CHECK, FOUND LEFT SIDE EMERGENCY EPSU UNIT FAILING TEST. INSTALLED NEW POWER SUPPLY PER AMM. CHECKS GOOD.
DURING NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT WITH BROKEN HARNESS AT SEAT 19. MAINTENANCE REPAIRED BROKEN WIRE HARNESS AT CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING NON ROUTINE CHECK, FOUND AFT CABIN EPSU FAILED TO TEST. MAINTENANCE REPLACED EPSU AT 13 WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING A NON ROUTINE CHECK, THE LEFT EPSU AT OVERWING EXIT WOULD NOT TEST. MAINTENANCE REPLACED BATTERY PACK AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT ROW 16 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING M-CHECK FOUND CHAFE DAMAGE ON RT & LT MLG FWD DOOR HINGE FITTINGS, FWD LUG, FWD FACE. IAW ERA 482533-14AD, FOLLOW UP INSP IS REQUIRED ON THE LT & RT MLG DOOR FWD HINGE FITTING. ACCOMPLISH SECTION II INSP NTE 3500 CYCLE INTERVALS FROM 03JUN10.
DURING M-CHECK FOUND LT WING INBOARD FLAP TRUNNION WEAR MAXIMUM REWORK DEPTH EXCEEDS 0.236 INCHES, DEPTH MEASUREMENT IS 0.3375 INCHES. REPLACED LT WING INBD FLAP TRUNNION SUPPORT IAW ERA 482530-14AD.
DURING M-CHECK FOUND RT MLG DOOR FWD HINGE FITTING LUG DAMAGED. REPAIRED IAW ERA 482533-14AD.
DURING M-CHECK FOUND LT MLG DOOR FWD HINGE FITTING LUG DAMAGED. REPAIRED IAW ERA 482533-14AD.
DURING M-CHECK FOUND LT WING INBD FLAP TRUNNION WEAR MAXIMUM REWORK DEPTH EXCEEDS 0.236 INCHES, DEPTH MEASUREMENT IS 0.3375 INCHES. REPLACED LT WING INBD FLAP TRUNNION SUPPORT IAW ERA 482530-14AD.
DURING M-CHECK FOUND SHEAR TIE CORRODED AT FR31 BETWEEN S40R & S42R. REPAIRED IAW SRM 51-44-11, SRM 51-21-11, SRM 51-42-11.
DURING M-CHECK FOUND SHEAR TIE CORRODED AT FR30 BETWEEN S40R & S41R. REPAIRED IAW SRM 51-44-11, SRM 51-21-11, SRM 51-42-11.
DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT BEAM +Y1292 FR66 â FR68. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.
DURING M-CHECK FOUND CORROSION ON FLOORBEAM AT Y1732 FR 65- FR 66. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.
DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT BEAM Y1292 FR 64-FR 66. REPAIRED IAW SRM 51-42-11 & SRM 53-21-01.
DURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT BEAM Y1292 FR 66-FR 68. REPAIRED IAW SRM 51-42-11 & SRM 53-21-01.
DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 261EF. REPAIRED IAW SRM 53-02-00 FIG 209.
DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 261PF. REPAIRED IAW SRM 53-02-00 FIG 209.
DURING M-CHECK FOUND GOUGE AND CORROSION ON RT AFT CABIN UTILITY SHEAR PLATE SUPPORT FR69-FR70. REPAIRED IAW SRM 51-42-11.
DURING M-CHECK FOUND GOUGE AND CORROSION ON LT AFT CABIN UTILITY SHEAR PLATE SUPPORT FR69-FR70. REPAIRED IAW SRM 51-42-11.
DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT WEB ASSY AT Y1732 FR20. REPAIRED IAW SRM 51-42-11.
DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT BEAM +Y1292 FWD OF FR 68. REPAIRED IAW SRM 51-42-11.
DURING M-CHECK FOUND CORROSION ON MAIN CABIN FLOOR PANEL 222FF. INSTALLED REPLACEMENT PANEL IAW CARD NR 2500-6617.
DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 5L INOPERATIVE. MX REPAIRED WIRING AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
MULTIPLE SEAT MOUNTED EMERGENCY EGRESS LIGHTS ARE INOPERATIVE. REPLACED AFT LEFT EPSU (13WL), CHECKS GOOD.
DURING LINE CHECK TEST THE AFT EPSU FAULTED, REPLACED BATTERY PACK.