N373NW
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 | 2025-08-28 – 2025-08-28 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2025-08-28 – 2025-08-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DIRTY SOCK ODOR AFTER APU BLEED SELECTED. OPENED APU COMPARTMENT, SAW SIGNS OF OIL ON APU AND APU DOOR IAW AMM 49-00. RUN APU AND STILL GETTING ODOR AT HIS TIME. INSPECTED APU ACCESS DOOR AND COMPARTMENT FOUND NO EVIDENCE OF CONTAMINATION. REF MD LOG 1531675 & APU REPLACEMENT ON LOG 1531804. (LP: 8423672) AIRCRAFT WAS GROUNDED.
FUMES - DESCENDING AT FL140 UNTIL LANDING, CREW REPORTED DIRTY SOCK ODOR. DECLARED EMERGENCY AND DONNED OXYGEN MASKS. APU WAS ON MEL FROM PRIOR EVENT IN YYZ. FOUND APU COOLING FAN AND FCU LEAKING OIL. REPLACED COOLING FAN AND FCU. INLET DOOR CONTAMINATED WITH OIL AND DIFFUSER DELAMINATED. REPLACED INLET DOOR ASSY, CLEANED APU COMPARTMENT. APU LEAK CHECKS OK. LEVEL C ECS DECONTAMINATION IN WORK. MTC IN PROGRESS. (LP: 8423668) AIRCRAFT WAS GROUNDED
AT 15000 FEET ON DESCENT DIRTY SOCK SMELL ALL WAY UNTIL SHUTDOWN. FLIGHT ATTENDANT SMELLED IT. FO PUT MASK ON AS PRECAUTION. EMERGENCY DECLARED. C/A: INSPECTED. OIL PRESENT IN APU COMPARTMENT. APU DEFERRED ON LOG 8423667. C/W MSI PREVENTION 2172. A- CREW NOT AVAIL. B- C/W. C- FORM NOT COMPLETED. D- N/A. E/F - APU BELIEVED TO BE CULPRIT. NO PTRACK SPIKES DURING ENGINE RUNS. G/H - N/A. I - C/W. J/K/L - C /W. FILTERS REPLACED. REF A320 AMM 21-21-. LEVEL B CONTAMINATION REMOVAL C/W. REF AMM 21-00. AIRCRAFT WAS GROUNDED
ON BOARDING ACFT WITH APU RUNNING, A STRONG ODOR WAS NOTICED. IT SMELLED LIKE A MUSTY BURNING OVEN CLEANER. THE APU BLEED WAS TURNED OFF NO VISIBLE ODOR WAS NOTICED. ODOR WAS IN COCKPIT AND CABIN. ISOLATED SOURCE OF SMOKE & FUME ODOR TO APU OIL LEAK. C/W W/C 0550- 2002. COMPLIED WITH LEVEL B DECONTAMINATION & ECS REVERSE DUCT BURN PROC. PER W/C 2100-2005. RAN BOTH ENG'S W/ BOTH BLEEDS TOGETHER + SEPERATLY AT HIGH PWR FOR 45 MINS. R+R'D BOTH CABIN RECIRC FILTERS PER A320 AMM 21-21. PERFORMED CONFIRMATION RUN OF BOTH ENG'S + PACKS, NO ODORS THROUGHOUT CABIN. A/C OKAY FOR SVC. (LP: 8036074)
WHILE WORKING ACFT, FOUND EXPIRED AFT LEFT FA O2 GENERATOR. R & R O2 GENERATOR AND INDUCTED EMERGENCY EQUIPMENT IAW AMM 35-21. ALL CHKD NORMAL AT THIS TIME. (LP: 8036017)
FUME EVENT AT GATE, APU ON WITH BLEED ON. SMELLED OF BURNING RUBBER IN FLIGHT DECK AND FRONT GALLEY. PAX ON BOARD. DURATION WAS LESS THAN 30 SEC BEFORE BLEED WAS TURNED OFF.
MISC/DE - DUE TO A F/CTL FLAPS LOCKED ECAM WARNING ON APPROACH. NO TROUBLE FOUND DURING INSPECTIONS OF THE TRANSMISSION SYSTEM. INTERCONNECTING STRUT SENSORS 38CV AND 40CV WILL BE REPLACED. (LP: 8016200)
SHIP 3273 DISC: DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 831 (REFER TO AMDS CARD 5210-7089-LF RII). C/A: REMOVED DOOR DAMPER P/N FE174-004 S/N 341 ON UNSERVICEABLE CONDITION OF PASSENGER CREW DOOR 831 AS PER A320 FAM AMM-52-11- 14-000-001-B STEP 3.B, D AND STEP 4 JOB IN PROGRESS. REPLACED EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-14-000-001-B AND AS PER A320 FAM AMM52-11-14 -400-001-B,
PERFORM ER/A 628645-14 REV. ORIGINAL SECTION III ON EXTERNAL SKIN FR 3 AND 10.5 INCH ABOVE STATIC PORT RVSM AREA REFERENCE TO LOG PAGE 1153824. PERFORMED REPAIR ON UPPER SKIN BETWEEN FR2 TO FR4 RH SIDE AND 10.5 INCH ABOVE STATIC PORT RVSM AREA AS PER A320 SRM53-11-11- 300-041 2.A. THIS REPAIR IS CATEGORY B. PERFORMED REPAIR ON UPPER SKIN BETWEEN FR2 TO FR4 RH SIDE AND 10.5 INCH ABOVE STATIC PORT RVSM AREA IAW SRM 53-11-11- 300-041 2.A. INSTALLED AND STABLISHED DECAL MONITOR WITH L/P NUMBER 1232816 AT EVERY CHECK AS PER TOPP 30-10-70 PAGE 14 ITEM I ANDPS 900-5-1 N.4. RII INSPECTION COMPLETE 1792357 (AE418QC) JOB COMPLETE. (LP: 1232816)
OILY SMELL FROM BLEED AIR WHEN TURNING ON APU BLEED. VISUALLY INSPECTED APU COMPARTMENT AND APU NO DEFECTS FOUND. .
BIRDS STRIKE AT APPROX 8000 FT ON DEPARTURE. NO ENGINE. COMPLIED W/ AMM 05-51 BIRD STRIKE INSPECTION. ALL DAMAGES FORWARDED TO NON-ROUTINE DOCUMENTS. (LP: 7403248)
DECLARED EMERGENCY DUE TO FLAPS LOCKED AT ZERO FOR THE APPROACH. NR 3 FLAP TORQUE LIMITER FOUND TRIPPED DURING T/S. REPLACED LH WING TIP BRAKE DUE TO HISTORY.
SHIP 3273 DISC: DURING PREFLIGHT, STARTED APU AND TURNED ON APU BLEED. NOTICEABLE DIRTY SOCK SMELL ON A/C. C/A: FOUND & REPLACED LEAKING APU COOLING FAN ON LOG#1063584. (LP: 7023078)
SHIP 3273 PRIOR TO BOARDING, NOTICED DIRTY SOCK ODOR IN CABIN. SMELL WENT AWAY WITH APU BLEED CLOSED. CLEANED APU AIR INTAKE & COMPARTMENT PER WORK CARD 4916-2001( 671052) C/W AMDS WORKCARD 4900-2001. FOUND OIL PUMP GASKET IN POOR CONDITION, R&R GASKET PER A321 AMM 49-92. NO LEAKS NOTED.( 935158) C/W AMDS WORKCARD 2100-2005 STEP 1&2. (119599) C/W AMDS WORKCARD 2100-2005 THROUGH STEP 7.(138472) ACCOMPLISHED DECONTAMINATION OF THE ECS REF A320 AMM 21-00-00-615-803-A( 138472) C/W AMDS WORKCARD 2100-2008 STEP 8 THROUGH 11(362683). REMOVED AND REPLACED RECIRCULATION FILTER REF A320 AMM 21-21. ( 948117) PERFORMED ENGINE AND APU BLEED CHECK FOR SMELL. NO SMELL NOTED.
SHIP 3273 DISC: DIRTY SOCK ODOR ON APPROACH WHEN POWER WAS AT IDLE FROM DESCENT WAS VERY APPARENT AT 9000FT. C/A: C/W NO GO ODI LOG 0976817 CHANGED COOLING FAN PERFORMED ECS CLEAN AND RECIRC FILTER CHANGE. (LP: 7386906)
SHIP 3273 - DIV - TO GEG DUE TO F/CTL FLAPS LOCKED AND F/CTL FLAP SYS 2 FAULT ECAM WARNINGS BETWEEN 1-2 FLAP SETTING. CORRECTIVE ACTION: RESET WTB, FAULT CLEARED. OK TO CONTINUE. LATER IN MSP FOUND LEFT #3 FLAP ACTUATOR POPPED AND RIGHT #4 FLAP ACTUATOR WITH SIGNS OF LEAKAGE. REPLACED LEFT #3 FLAP ACTUATOR (6221CM). OPS CHECK GOOD. NO MORE LEAKS NOTED. (LP: 6974194)
SHIP 3273 DISC: POSSIBLE BIRD INJESTION IN ENGINE #2 ON TAKEOFF FROM KBWI POSSIBLE BIRD STRIKE. BIRD FLEW BY WINDSCREEN THEN N1 VIB IMMEDIATELY CLIMBED TO 8.0 BUT QUICKLY DECREASED TO 4.1. ALL OTHER ENGINE PARAMETERS NORMAL ENG #2. C/A: PERFORMED BIRD STRIKE INSPECTION REF A320 AMM 05-51-14, BIRD REMAINS FOUND ON BLADES 11, 12, AND 13 WITH 12 AND 13 BEING SHINGLED TOGETHER. REMAINS CLEANED OFF WITH NO EVIDENCE OF GOING THROUGH CORE. UNSHINGLED BLADES AND INSPECTED FAN BLADES REF A320 AMM 72-21-00 NO DAMAGE ON BLADE 11. BLADE 12 AND 13 DISTORTED OUT OF LIMITS IN AREA C. (WIP) 522863. R/R FAN BLADE PAIR 12 AND 30, R/R FAN BLADE PAIR 13 AND 31 IAW A320 AMM 72-21. (LP: 6974144)
SHIP 3273 - MISC/DE - DUE TO FLAPS LOCKED MESSAGE WHEN SELECTING FLAPS 2 FOR APPROACH. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS. (LP: 6037654)
SHIP 3273 DISC: PRIMARY OBSERVERS SLIDING SEAT - SEAT UNUSABLE - O2 MASK WILL NOT TEST. C/A: FWD TO MEL 25-11-06A. DISPATCH APPROVED. OK FOR SVC. UPON FURTHER INSP. FOUND THE CAPT. O2 MASK BOX NOT TESTING ( 177277). REMOVED AND INSTALLED NEW CAPT O2 BOX PER A320 35-12. INSTALLED SAME OXY MASK PER AMM 35-12. OPS CHECK GOOD. "M" PROCEDURES REMOVED, PLACARDS REMOVED, AND MEL 25-11-06A REMOVED. (LP: 6037644)
SHIP 3273 DISC: FOUND ROWS 14-17 ON RT SIDE OF AC EMER. LIGHTS OUT. C/A: FOUND BLACK WIRE UNDER SEAT 14 BROKEN. REPAIRED WIRE WITH SPLICE PER A320 ESPM 20-53. OPS CHK C/W PER A320 AMM 33-51. AC OK FOR SVC. (LP: 6444675)
SHIP 3273 - ATO - AT 20KTS DUE TO F/CTL ELAC 1 PITCH FAULT. CORRECTIVE ACTION: R/R SERVO VALVE AT LEFT BLUE ELEVATOR SERVOCONTROL (34CE3). OPS CHECK GOOD. (LP:5718676)
SHIP 3273 DISC: ENG 2 FIRE PB SELECTED AGENT 1 BOTTLE DISCHARGED. C/A: REMOVED#2 ENG #1 BOTTLE IAW A320 AMM 26-21. INSTALLED #2 ENG #1 BOTTLE UP UNTIL STEP A320 AMM 26-21-41-400-001-A STEP 4.(H).(N BRIGHT 038228) C/W REMAINING STEPS OF A320 AMM 26-21. OPS CK GOOD. (LP: 5152019)
SHIP 3273 - ATB/IFSD - RIGHT ENGINE FAILURE AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN TAIL PIPE; ENGINE CHANGE REQUIRED. REMOVE AND REPLACED #2 ENGINE ON LOG 0435692. (LP; 5152018)
SHIP 3273 - HYD/DIV - TO DEN DUE TO HYD G RSVR LO LVL ECAM MESSAGE. CORRECTIVE ACTION: FOUND HCU PIPE (SOV FILTER PIPE) AT LH PYLON DAMAGED AND LEAKING. R/R ENGINE #1 GREEN EDP (1030GK). REMOVED LH PYLON SOV FILTER PIPE AND PLACED ENGINE #1 T/R ON MEL DEFERRAL. LEAK CHECK GOOD. NEEDS NEW SOV FILTER PIPE. OK TO CONTINUE. (LP: 6138198)
SHIP 3273 DISC: DIV - RECEIVED ENG 1 FIRE INDICATION INFLIGHT, RAN QRH & ECAM WHEN THRUST LEVER PLACED AT IDLE WARNING WENT AWAY. LEFT ENGINE AT IDLE AND DIVERTED TO PIB. C/A: FOUND BOROSCOPE PLUG AT 6 O'CLOCK POSITION OFF. REINSTALLED PLUG PER A320 AMM 72-51. PERFORMED GVI INSPECTION PER A320 AMM 05-24 . NO DEFECTS NOTED. RAN ENGINE FOR 5 MINUTES, ALL INDICATIONS. (LP: 6138135)
SHIP 3273 - ATB - DUE TO BURNING PLASTIC SMELL IN AFT CABIN. CORRECTIVE ACTION: NO TROUBLE FOUND. CLASSIFIED AS TYPE 10 ODOR OF UNKNOWN ORIGIN. PERFORMED LEVEL A DECONTAMINATION PER TSM AND RETURNED TO SERVICE. (LP: 6138110)
AFT CENTER FUSELAGE - FR58- 60, STGR25-26L, EXISTING REPAIR. THIS IS A MONITOR INSPECTION LOG FOR ERA 613977 -14AD REV A. THIS ERA REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ERA 613977-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 12,100 FC FROM SECTION I REPAIR EMBODIMENT OR 24,200 FH FROM SECTION I REPAIR EMBODIMENT, WHICHEVER OCCURS FIRST. THEREAFTER, REPEAT SECTION II WITHIN EVERY 1,600 FC OR 3,200 FH, WHICHEVER OCCURS FIRST. ASSOCIATED ER/A 00-613977.
SHIP 3273 DISC: PASSENGER SEAT 17D ESCAPE PATH LIGHT CONNECTOR DAMAGED. C/A: FWD TO MCO PER MEL 33-50-03A. NO "M" PROCEDURES. PLACARD INSTALLED. (LP: 5490511)
SHIP 3273 DISC: MATERIAL BURRED (OVALIZATION) ON LOWER LATERAL SUPPORT LH SIDE ON RACK 80VU (ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTH ER FLIGHT) (AD RELATED 2515-01014-02A. C/A: COMPLIED WITH ER/A 613674-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 613674-14AD REV 0, IT IS BEEN VALIDATED, PERFORMEDREPAIR INSTRUCTIONS ON LOWER LATERAL SUPPORT LH SIDE ON RACK 80VU AS PER ER/A 613674-14AD REV ORIGINAL SECTION I HAS BEENCOMPLIED WITH, SEE LOG PAGE 0111628 FOR TIME CONTROLLED ITEMS SECTION II, APPROVED DATE 15/DEC/23 RII INSPECTION COMPLETE1615834 (AE372QC) JOB COMPLETE. (LP: 0121196)
SHIP 3273 DISC: MATERIAL BURRED (OVALIZATION) ON LOWER LATERAL SUPPORT RH SIDE ON RACK 80VU (ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTH ER FLIGHT) (AD RELATED 2515-01014-02B) . C/A: COMPLIED WITH ER/A 613674-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 613674-14AD REV 0, IT IS BEEN VALIDATED, PERFORMEDREPAIR INSTRUCTIONS ON LOWER LATERAL SUPPORT RH SIDE ON RACK 80VU AS PER ER/A 613674-14AD REV ORIGINAL SECTION I HAS BEENCOMPLIED WITH, SEE LOG PAGE 0111628 FOR TIME CONTROLLED ITEMS SECTION II, APPROVED DATE 15/DEC/23. RII INSPECTION COMPLETE 1615834 (AE372QC) JOB COMPLETE. (LP: 0121149)
SHIP 3273 DISC: CRACK INDICATION FOUND AT HOLE C FR16 RH AT LEVEL DOOR STOP FITTING 7. CRACK DIRECTION 3 OCLOCK L= 0.091 INCH APROX. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FU RTHER FLIGHT. COMPLIED WITH ER/A 612899-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 612899-14AD REV.0 AND REV 1 IT HAS BEENVALIDATED.PERFORMED REPAIR INSTRUCTIONS ON FR16 RH AT DOOR STOP 1 AND 7 LEVEL DOUBLE JOGGLE AREA AS PER ER/A 612899- 14ADREV.ORIGINAL SECTION I HAS BEEN COMPLIED WITH APPROVED DATE: .01/DEC/23.SEE LOG PAGE 0090638 SECTION II FOR TIME CONTROLLEDITEMS.TOOL USED: MICROMETER P/N: 293-344-30 S/N: 77003978 DUE DATE: 11/AUG/24 JOB COMPLETE. (LP: 0119572)
SHIP 3273 DISC: CRACK INDICATION FOUND AT HOLE 6 FR16 LH AT LEVEL DOOR STOP FITTING 7. CRACK DIRECTION 9 OCLOCK L= 0.144 INCH APROX. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: COMPLIED WITH ER/A 612874-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 612874-14AD REV.0,REV.1 AND REV.2 IT HAS BEENVALIDATED.PERFORMED REPAIR INSTRUCTIONS ON FR16 LH DOUBLE JUGGLE AREA AT LEVEL DOOR STOP FITTING #7 AS PER ER/A 612874- 14AD REV.ORIGINAL SECTION I HAS BEEN COMPLIED WITH APPROVED DATE: 19/DEC/23. SEE LOG PAGE 0117369 SEC.DTE FOR TIME CONTROLLED ITEMS.TOOL USED: MICROMETER P/N: 293-344-30 S/N:71735394 DUE DATE:23/SEP/24. RII INSPECTION COMPLETE 1715948 (AE403QC) JOB COMPLETE. (LP: 0119551)
SHIP 3273 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BT W FR 58 TO FR 59 AND STR 25L TO STR 26L LOWER FUSELAGE (REFERENCE NUMB ER AA CARD 5100-01821-01A -DE). C/A: COMPLIED WITH ER/A 613977-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 613977-14 REV 0 THRU REV 2 IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOCATED BTW FR 58 TO FR 60 AND STR 25L TO STR 26L LOWER FUSELAGE AS PER ER/A 613977-14AD REV ORIGINAL, SECTION I HAS BEEN COMPLIED WITH. (LP: 0117655)
SHIP 3273 DISC: CRACK INDICATION FOUND ON WINDSHIELD CONTINUITY FITTING LH SIDE. C/A: COMPLIED WITH ER/A 612832-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 612832-14AD PRI REV 0 AND REV 1 IT HAS BEEN VALIDATED.PERFORMED REPAIR INSTRUCTION ON WINDSHIELD CONTINUITY FITTING LH SIDE AS PER ER/A 612832-14AD REV ORIGINAL SECTION 1 HASS BEENCOMPLIED WITH SEE LOG PAGE 0110513 FOR TIM. (LP: 0117561)
SHIP 3273 DISC: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER RADIUS LH SIDE. C/A: COMPLIED WITH ER/A 612832-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON ER/A 612832-14AD PRI REV 0 AND REV. 1 IT IS BEENVALIDATED. PERFORMED REPAIR INSTRUCTIONS NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH/RH AS PER ER/A 612832-14AD REV.ORIGINAL SECTION I HAS BEEN COMPLIED WITH. (LP: 0117546)
SHIP 3273 DISC: PERFORM PRI 613201-14AD REV 0 TO REV 6 AND ER/A 613201-14AD REV ORIGIN AL IN CONJUNCTION WITH JOB CARD 1244835-3273. C/A: COMPLIED WITH ER/A 613201-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 613201-14 REV 0 TO REV 6, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON LATERAL EXTERNAL SKIN BTW FR12 TO FR16 LH SIDE AS PER ER/A 613201-14AD REV. ORIGINAL, SECTION I HAS BEEN COMPLIED WITH. (LP: 0117552)
SHIP 3273 DISC: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER RADIUS RH SIDE. C/A: COMPLIED WITH ER/A 612832-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON ER/A 612832-14AD PRI REV 0 AND REV. 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH/RH AS PER ER/A 612832-14AD REV.ORIGINAL SECTION I HAS BEEN COMPLIED WITH. (LP: 0117590)
SHIP 3273 DISC: DTE ERA 612832-14AD. REPAIR AREAS OTHER THAN CONTINUITY FITTING AND OTHER THAN WINDSHIELD FRAMING PER ERA 612832-14AD. C/A: REVISE / UPDATE ERA 612832-14AD WITH DTE RESULTS PRIOR TO 90,143 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 14-612832 ADDED FOR AC 3273. (LP: 0110599)
SHIP 3273 DISC: INSPECTION ERA 613674-14AD. MODIFICATION PER ERA 613674-14AD AT 80VU RACK REQUIRES INSPECTION FOLLOW UP PRIOR TO 49,643 TOTAL FLIGHT CYCLES AND EVERY 1,000 FLIGHT CYCLES THEREAFTER. C/A: ACCOMPLISH INSPECTION AT 80VU RACK PER ERA 613674-14AD SECTION II PRIOR TO 49,643 TOTAL FLIGHT CYCLES AND EVERY 1,000 FLIGHT CYCLES THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3273. (LP: 0111628)
SHIP 3273 DISC: INSPECTION ERA 612832-14AD. REPAIR OF WINDSHIELD FRAMING PER ERA 612832-14AD REQUIRES FOLLOW-ON INSPECTIONS PRIOR TO 57,143 TOTAL FLIGHT CYCLES AND EVERY 4,700 FLIGHT CYCLES THEREAFTER. C/A: ACCOMPLISH INSPECTIONS AT WINDSHIELD FRAMING PER ERA 612832-14AD SECTION III PRIOR TO 57,143 TOTAL FLIGHT CYCLES AND EVERY 4,700 FLIGHT CYCLES THEREAFTER. ASSOCIATED ER/A 14-612832 ADDED FOR AC 3273. (LP: 0110574)
SHIP 3273 DISC: DTE ERA 613977-14. REPAIR PER ERA 613977-14 REQUIRES DTE FOLLOW UP PRIOR TO 13JUN2024. C/A: REVISE / UPDATE ERA 613977-14 WITH DTE RESULTS PRIOR TO 13JUN2024. (LP: 0110107)
SHIP 3273 DISC: INSPECTION ERA 613832-14AD. CONTINUITY FITTING REPAIR PER ERA 613832-14AD REQUIRES FOLLOW-ON INSPECTIONS PRIOR TO 59,643 TOTAL FLIGHT CYCLES AND EVERY 8,700 FLIGHT CYCLES THEREAFTER. C/A: ACCOMPLISH INSPECTION AT CONTINUITY FITTING PER ERA 612832-14AD SECTION II PRIOR TO 59,643 TOTAL FLIGHT CYCLES AND EVERY 8,700 FLIGHT CYCLES THEREAFTER. ASSOCIATED AA 5311-01226 ADDED FOR AC 3273. (LP: 01110513)
SHIP 3273 DISC: DTE ERA 613201-14AD. REPAIR PER ERA 613201-14AD. C/A: ASSOCIATED ER/A 14-613201 ADDED FOR AC 3273. (LP: 0106953)
SHIP 3273 DISC: BENT INTERNAL STRUCTURE CROSS BEAM AT FR 27 BTW STR 38L TO STR 41R IN FWD CARGO COMPARTMENT. C/A: REPLACED INTERNAL STRUCTURE CROSS BEAM AT FR 27 BTW STR 38L TO STR41R FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11 AND DWG: D53230829. (LP: 0104332)
SHIP 3273 DISC: ROCKEN SUPPORT ANGLE ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER DUE TO WORK IS ITEM RII AND MUST BE PERFOR MED STEP BY STEP. C/A: REPLACED SUPPORT ANGLE ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER AS PER A320 SRM51-42-11, A320 SRM 51-72-11, A320 FAM AMM55-16-42-00-001-A SUBTASK 010-05A STEP 4.A ITEM 2 TO 4 AND A320 FAM AMM 55-16-42-400-A SUBTASK 42-050B STEP 4.A ITEM 3 TO 6 ,APPLIED TORQUE ON NUT AT 55 LBS. IN TOOL USED TORQUE P/N QD2R200 S/N 0718904743 , DUE DATE 10-NOV-24 RII INSPECTION COMPLETE 0007621 (AE332QC) JOB COMPLETE. (LP: 0099043)
SHIP3273 DISC: CORROSION FLOOR STRUCTURE WEB FRAME LOC. FR 69 TO FR 70 L/H AT AFT GA LLEY AREA. C/A: EPLACED STRUCTURE WEB FRAME LOC. FR 69 TO FR 70 L/H AT AFT GALLEY AREA AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWGD53474180. ISSUE: Z. RELEASE DATE: 14/JUL/22. RII INSPECTION COMPLETE 9238180 AE406QC JOB COMPLETE. (LP: 0096877)
SHIP3273 DISC: CORROSION STRINGER 43L LOC. BTW FR 54 AND FR 55 IN AFT CARGO COMPARTMENT (SSI 534107) C/A: REPLACED STRINGER 43L LOC BTW FR 54 AND FR 55 IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWGE53470342 RELEASE DATE 21 MAR 19 ISSUE AY. TOOK INITIAL MEASUREMENTS OF CORROSION ARE: L= 1.010 IN, W= 0.780 IN. TOOL USED DIGITAL CALIPER P/N: 500-196-30. S/N: A22348594, D /D: 13-JUL-24. RII INSPECTION COMPLETE. (LP: 0095585)
SHIP 3273 DISC: DENT EXTERNAL SKIN LOCATED BETWEEN FR4 TO FR5 AND 8 INCH ABOVE OF RH LOWER SIDE STRINGER LOWER FUSELAGE. C/A: EVALUATED DENT LOC EXTERNAL SKIN LOC BTW FR4 TO FR5 AND 8 INCH ABOVE OF RH LOWER SIDE STRINGER LOWER FUSELAGE AND FOUND WITHINLIMITS, AS PER A320 SRM 53-00-11-283-005 STEP 2.A FIGURE 002 (SHEET 01 TO SHEET 03) MEASUREMENTS OF DENT ARE: X= 0.980 IN Y=1.050 IN D=0.004 IN A=2.380 IN TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N:A18135078 D/D: 19-SEP-24, DEPTH GAUGE P/N: 8645A12S/N:72649 D/D: 25-JUL-24, PERFORMED DVI AND NOT FOUND MORE DAMAGE AS PER AIRBUS NTM 51-90-00, NOMINAL THICKNESS IS: 0.047 IN, ASPER A320 SRM 53-11-11-05A FIGURE 005 SHEET 2, PERFORMED HFEC INSPECTION ON DENTED AREA EXTERNAL SKIN AS PER NTM 51-10-08.CRACKINDICATION NOT FOUND. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC500D, S/N: 00X12101V022237, D/D: 26-JAN-24. THIS DENT ISCATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT F/C: 60000, F/H: 120000. WHICHEVER OCCURS FIRST AS PER A320SRM 53-00-11-205-050, STEP2(A). DECAL MONITOR STABLISHED (REFERENCE TO LOG PAGE 0068863) JOB COMPLETE. (LP: 0092595)
SHIP 3273 DISC: CORROSION LOWER SILL LOC. FR 16 R/H AT FWD GALLEY AREA C/A: REPLACED LOWER SILL LOC. FR 16 R/H AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53110339 RELEASE DATE 28-MAY-98 ISSUE G00. MEASURES OF CORROSION ARE P1 L: 1.613 IN W: 1.338 IN D: 0.030 IN P2 L: 3.484 IN W: 1.632 IN D: 0.042 INTOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N A21303945 DUE DATE 07/NOV/23 AND DEPTH GAUGE P/N 547-217S S/N 009401 DUE DATE 22/SEP/24. RII INSPECTION COMPLETE JOB COMPLETE. (LP: 0089303)
SHIP 3273 DISC: CORROSION FLOOR BEAM -Y765 LOC. FR 20 AT FWD GALLEY AREA C/A: REPLACED FLOOR BEAM -Y765 LOC. FR 20 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-44-11, SRM 51-21-11 DWG D53918123, RELEASE DATE: 28-MAY-98, ISSUE: COO DWG D53112814 RELEASE DATE: 14-MAR-03, ISSUE: E0O.DWG D53110984 RELEASE DATE: 25-JUN-05ISSUE : CO0, DWG D53110920 RELEASE DATE: 28-APR-21 ISSUE: E00 AND DWG D53112812 RELEASE DATE: 22-MAR-06 ISSUE: E00.TOOK MEASUREOF CORROSION ARE:L: 0.807 IN W: 0.165 IN D: 0.048 IN TOOL USED CALIPER P/N 500-197-30 S/N A21303945 DUE DATE 07-NOV-23, DEPTHGAGE P/N 547-217S S/N 009401 DUE DATE 22-SEP-24 RII INSPECTION COMPLETE 1942138 JOB COMPLETE. (LP: 0058848)
SHIP 3273 DISC: ORROSION FLOOR BEAM -Y1292 LOC. FR 20 AT FWD GALLEY AREA. C/A: REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOC. FR 20 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11 AND DWG: D53112812 ISSUE: E00 RELEASE DATE: 08-JAN-97 RII INSPECTION COMPLETE 2173360 JOB COMPLETE. (LP: 0057644)
SHIP 3273 DISC: CORROSION NUT SPIGOT PIN FWD POS. L/H PYLON C/A: REMOVED AND REPLACED NUT SPIGOT PIN FWD POS. L/H PYLONS AS PER AMDS CARD # 5450-1010-LT AND AMDS CARD # 5450-6010-LT STEP 9. LP 0044915
SHIP 3273 TRANSDUCER PUSH-ROD, BEARING SEIZED/CORRODED ON RUDDER SIDE. CORRECTIVE ACTION:R/R AND RIG PUSH ROD PER A320 AMM 27-25-04. OK FOR SERVICE. (2279876)
SHIP 3273 DURING TEST AFT FLIGHT ATTENDANT RIGHT HAND O2 PANEL FAILED TO OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8825269)
SHIP 3273 DURING TEST O2 PANELS DID NOT OPEN AT L/H SEATS ROWS 18 AND 23 AND R/H SEATS ROWS 11, 12, AND 27. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8825268)
SHIP 3273 RETURN TO MSP FOR FUMES IN COCKPIT AND CABIN. PERFORMED INSPECTION AND MAINTENANCE PER WORKCARDS AMDS 0550-2002, 0550-9001 AND AMDS 7900-2001. OK FOR SERVICE. (7816880)
SHIP 3273 DURING TEST PSU AT SEAT 2 LEFT DID NOT DROP. CORRECTIVE ACTION: R/R PSU PER A320 AMM 35-21-41. OPS CK GOOD. (1847080)
SHIP 3273 DURING TEST PSU AT 29 RIGHT DID NOT DROP. CORRECTIVE ACTION: R/R PSU AND OPS CK PER A320 AMM 35-21-41. OPS CK GOOD. (1847092)
SHIP 3273 PSU AT SEAT 22 LEFT DID NOT DROP. CORRECTIVE ACTION: R/R PSU PER A320 AMM 35-21-41. OPS CK GOOD. (1847091)
SHIP 3273 DURING TEST PSU AT SEAT 19 LEFT SIDE DID NOT DROP. CORRECTIVE ACTION: R/R PSU AND OPS CK PER A320 AMM 35-21-41. OPS CK GOOD. (1847086)
DURING TEST PSU OXY PANEL 4AB DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OK FOR SERVICE.
DURING TEST PSU OXY PANEL 28ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OK FOR SERVICE.
DURING TEST PSU OXY PANEL 14ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OK FOR SERVICE.
FOUND PSU OXY PANEL 15ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXY PANEL 15ABC. OK FOR SERVICE.
FOUND PSU OXY PANEL 30 ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXY PANEL 30 ABC. OK FOR SERVICE.
FOUND PSU OXY PANEL 26ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXY PANEL 26ABC. OK FOR SERVICE.
FOUND PSU OXY PANEL 23ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED PSU OXY PANEL 23ABC. OK FOR SERVICE.
PAX DOOR SLIDE DISARM PIN POUCH DAMAGED. CORRECTIVE ACTION: REPLACED DISARM PIN POUCH ON 1R DOOR.
CRACK BRACKET TELESCOPIC DUCT OUTBOARD OB FIXED LEADING EDGE ON LT WING. CORRECTIVE ACTION: REPLACED TELESCOPIC BRACKET ON OUTBOARD FIXED LEADING EDGE ON LT WING, AS PER A320 SRM 51-42-11 AND 51-72-11 AND DRAWING D57449206 ISSUE C AND ERA 530598-14 MA REV A.
PDA PART DEPARTED AIRCRAFT. A/C 3273 CLOSED LOG 1003398. LEFT FUSELAGE HOIST POINT PLUG MISSING JUST FWD TO LEFT FWD OVERWING EMERGENCY EXIT DOOR. INSPECTED AND INSTALLED HOIST POINT COVER ON LEFT FWD EMERGENCY EXIT DOOR.
AFTER REWORK CORROSION EVALUATED SEAT TRACK -Y1292 FR41 TO FR47 AND FOUND OUT LIMITS AS PER JOB CARD 2500-02231IN PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DWG D53377500 AND PRI/ERA 5733335-14, REV O.
CORROSION FLOORBEAM +Y765 LOCATED FR12 TO FR24 IN PASSENGER CABIN. REPLACED IAW SRM 51-72-11 AND DWG D53112812.
CORROSION FLOORBEAM +Y1292 LOCATED FR12 TO FR24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG 53112812.
AFTER REWORK CORROSION EVALUATED SEAT TRACK-Y765 FR41 TO FR47 AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-72-11 AND DWG D53371112.
AFTER REWORK CORROSION EVALUATED SEAT TRACK -Y765 FR36 TO FR41 AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-72-11 AND DWG D53370500.
DENT EXTERNAL SKIN DOUBLER REPAIR ON LOWER FUSELAGE FROM FRAME 25 TO FRAME 26 BETWEEN STRINGER 43L TO 42R. REPLACED IAW SRM 51-42-11 AND DWG P19110-21115, REV C.
CORROSION FLOOR BEAM -Y1162.5 AT FR38 AFT GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53472780.
CORROSION WEB LOCATED FR20 TO FR24 AT LEVEL STRINGER 23R AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53114332.
CORROSION FLOORBEAM -Y1292 LOCATED FR12 TO FR24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DRAWING D53112814.
AFTER REWORK CORROSION EVALUATED SEAT TRACK -Y765 FR36 TO FR41 AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-72-11 AND DWG D53370500.
(LP# 0842547) CRACK CROSS BEAM AT FR68 STRINGER 23R LEVEL, -Y1662 (SSI534147) REPLACED IAW SRM 51-72-11 AND DWG D53474250.
(LP# 0843109) CORROSION SPLICE UPPER AND INBOARD POSTION AT FLOOR BEAM -Y1165 AT AFT GALLEY AREA ON FRAME 68 (SSI 534147) REPLACED IAW SRM 51-72-11 AND DWG D53472780
AFTER REWORK CORROSION EVALUATED SEAT TRACK -Y1292 FR36 TO FR41 AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-72-11 AND DWG D5713-0300.
CORROSION FLOORBEAM -Y765 AT AFT GALLEY AREA ON FRAME 68+6INCHES. REPLACED IAW SRM 551-72-11 AND DWG D53472815.
CORROSION FLOORBEAM -Y765 LOCATED FR12 TO FR24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D5311-2812.
CORROSION FLOORBEAM +Y1162.5 UPPER FLANGE LOWER SURFACE AT AFT GALLEY AREA ON FRAME 67+8 INCHES. REPLACED IAW SRM 51-72-11 AND DWG D53472780.
CORROSION FLOORBEAM +Y254 LOCATED FR12 TO FR24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG 53112816.
(LP# 0837197) CORROSION RAIL DUMMY -Y189 LOCATED FR20 TO FR24 AT FORWARD GALLEY AREA. (SSI 531194) REPLACED IAW SRM 51-72-11 AND DRAWING D53111406.
HYD B RESERVOIR LOW LEVEL. FOUND BLUE SYSTEM HYDRAULIC RESERVOIR FULL, ACCUMULATOR CHARGE GOOD, HEAD PRESSURE GOOD, AND NO EXTERNAL LEAKAGE. REPLACED BLUE SYSTEM LOW LEVEL SWITCH, OPERATION AND LEAK CHECK GOOD. OK FOR SERVICE.
R2 DOOR EXIT LIGHT INOPERATIVE. FOUND WIRE HOOKED UP BACKWARDS, SWAP WIRES, TESTED NORMAL.
DENT FOUND ON THE EXTERNAL SKIN, DURING A WALK AROUND, UNDER AND JUST FWD OF L1 DOOR ON LOWER FUSELAGE, PERFORMED PERMANENT REPAIR BETWEEN FRAMES 12+3 AND 16 ABOVE THE LT UPPER STRINGER ON FUSELAGE IAW SRM 53-11-11-300-006, ITEM 2. A STEPS 1A TO R, FIGURE 20105, SHEET 3, AND ER/A 554943-14AD, REV ORIGINAL, AND PRI 554943-14.
CORROSION ON STR 42L BETWEEN FRAMES 56 AND 57. REMOVED DAMAGED SECTION OF STR 42L IAW SRM 53-00-13, FIG 201. ACCOMPLISHED NDT OF EXISTING FASTENER HOLES. NO CRACK NOTE IAW NTM 51-10-01, PB6, PROCEDURE B. ALODINE, PRIMED AND PAINTED IAW SRM 53-00-13, STEP 7, M & N.
CORROSION ON STR 43L BETWEEN FRAMES 56 AND 57. REMOVED DAMAGED SECTION OF 43L IAW SRM 53-00-13, FIG 201. ACCOMPLISHED NDT OF EXISTING FASTENER HOLE. NO CRACK NOTE. IAW STM 51-10-01 8B6 PROCEDURE B. QC 1988. FABRICATED REPAIR PARTS IAW SRM 53-00-13, FIG 201. ALODINE, PRIMED AND PAINTED IAW A32 SRM 53-00-13, STEP 7, M & N.
DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 23. MAINTENANCE REPAIRED WIRE TO LIGHT ASSY AND OPS CHECKED NORMAL.
DURING CHECK, FOUND SEAT 26C EMERGENCY LIGHT HARNESS DAMAGED. MX PULLED DAMAGED WIRE FROM CONNECTOR AND INSTALLED NEW PIN ON WIRE. FUNCTIONAL CHECKED NORMAL.
DURING INSPECTION, FOUND FWD CARGO BULKHEAD PANEL 131DW HAS FOUR BRACKETS LOOSE. REPAIRED FWD CARGO BULKHEAD PANEL IAW ER/A 512310-14 REV 'O' FINAL STEPS 1 THRU 6.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131BF PUNCTURED, GOUGED AND DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131CF PUNCTURED, GOUGED AND CRACKED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 132KF CREASED & GOUGED IN SEVERAL AREAS. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131GF PUNCTURED AND DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132JF PUNCTURED, GOUGED AND DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131KF GOUGED & PUNCTURED IN SEVERAL LOCATIONS. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131FF GOUGED AND CRACKED. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG. 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132GF PUNCTURED, GOUGED AND DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151NF DAMAGED 5" X 5". NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131EF MISSING INSERT. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 162BF DAMAGED 5" X 5". NEW FLOOR PANEL IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151EF DAMAGED. NEW SLOPE PANEL FABRICATED IAW DWG 3D25-37705 & SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF DAMAGED 5" X 5" N/R 150/45. NEW SLOPE PANEL FABRICATED IAW DWG 3D25-37705 SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND RT AFT PASSENGER & CREW DOOR SILL BEAM INBD FR68 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED THE DEEPEST DAMAGE LIMITS L=0.60" W=0.50" D=0.035 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. ACCOMPLISHED REPAIR IAW SRM 53-41-14, FIG 201 & ER/A 508987-14 REV.
DURING INSPECTION, FOUND TAILCONE EXTERNAL SKIN DENTED AT FR80 RT SIDE APPROX 8" FROM TOP CENTER LINE. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-11, FIG 108, DIA 104. L=.850 W=.850 IAW SRM 53-51-11, FIG 203. FABRICATED REPAIR DOUBLER IAW SRM 53-51-11, FIG 203. INSTALLED REPAIR DOUBLER IAW SRM 53-51-11, FIG 203.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D 25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151LF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG NR 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161BF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG NR 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151TF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG NR 3D 25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151BF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151RF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151RF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D 25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152NF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152QF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152QF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG NR 3D 25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152QF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG NR 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152EF DAMAGED. NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151HF DAMAGED 7" X 5". NEW FLOOR PANEL FABRICATED IAW DWG 3D25-37705, SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261BG DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37498 AND SRM 53-02-00, FIG 209. AND INSTALLED.
DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261PF INSERTS RUSTY AND BOTTOM LT AFT CORNER DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-37498, & SRM 53-02-00, FIG 209, INSTALLED FLOOR PANEL.
DURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR12 TO FR20, Y1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 101. REPLACED FLOOR SUPPORT IAW 51-42-11, AIPC 53-11-01, FIG 105 AND DWG NR D5110422.
DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R FLOOR SUPPORT WEB IAW SRM 51-42-11 & DWG D531143.
DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R FLOOR SUPPORT WEB IAW SRM 51-42-11 & DWG D531143 32.
DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA LT SIDE INDB FR16 UPPER SURFACE WEB HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 L=1.5" W=1.0" D-.006" NO ALLOWABLE LIMITS ESTABLISHED IN SRM. REPLACED FORWARD UTILITY AREA LT SIDE WEB BETWEEN FR12 TO FR16 IAW SRM 51-42-11 AND DWG NR 53114332.
DURING INSPECTION, FOUND FORWARD LT PASSENGER DOOR LWR ENTRANCE MID FWD UPPER SURFACE FITTING AROUND NUTPLATES HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, NO ESTABLISHED LIMITS ON SRM 53-11-14. REPLACED FITTING IAW SRM 51-42-11 & DWG D53112109.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 64 TO FR 66,Y1292 HARD POINT SURFACE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.50"W=1.50"D=0.060" FOUND TO BE OUT LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 & DWG D53472000.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68 TO FR 69,Y1292 UPPER SURFACE FLANGES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 & DWG D53472000.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BTW FR 66 TO FR 68 Y1292 UPPER SURFACE FLANGES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.0 W= 1.00"D=0.055" FOUND TO BE OUT LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 & DWG D53472000.
DURING INSPECTION, FOUND FWD UTILITY AREA FLOOR PANEL 222FF LOWER SURFACE DELAMINATED AND CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-00.
DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT RT SIDE STRG 23R FR20 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. L=1.5 W=.200 D=.005 NO ESTABLISHED LIMITS IN SRM. REPLACED -Y1792 WEB FR16-FR20 IAW SRM 51-42-11 & DWG 53112783 & D53114332 & REPLACED CRACKED ANGLE FITTING IAW SRM 51-42-11.
DURING INSPECTION, FOUND L-1 DOOR FWD & AFT PLANKING PLATES HAVE CORROSION. REMOVED CORROSION IAW SRM 51-74-00, CHECKED DIMENSIONS AS FOLLOWS: AFT L=1.0", W=0.80", D=0.005"; FWD L=1.20", W=1.0", D=0.004", NO ALLOWABLE DAMAGE LIMITS IN SRM. REPLACED FWD & AFT BLANKING PLATES TO BE INSTALLED ON W/C 2500-6601.
DURING INSPECTION, FOUND FWD UTILITY AREA FLOOR PANEL 221FF LOWER SURFACE DELAMINATED AND CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-00.
DURING INSPECTION, FOUND LT AFT PASSENGER/CREW DOOR SILL AT AFT FR66 AROUND ANCHOR NUT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0 W=.500 D=.053 OUT OF LIMITS IAW SRM 53-41-14 FIG 101. REPLACED DOOR SILL IAW DWG 53480020.
DURING INSPECTION, FOUND AFT CABIN FLOOR SUPPORT RT SIDE BTW FR 65-66, Y-1732 UPPER SURFACE FLANGES & AROUND HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0" W=1.0" D=.050" NO LIMITS IAW SRM 53-41-14, FIG 101. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND DWGS D53472035 & D53472075.
DURING INSPECTION, FOUND AFT CABIN FLOOR SUPPORT LT SIDE BTW FR 65 TO FR 66, Y1732 UPPER SURFACE FLANGES & AROUND HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.73" W=1.20" D=.043NO ALLOWABLE LIMITS FOR THIS AREA. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND DWG 10 D53474250, PN D5347207500000.
DURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR18-20 Y-254, UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=3.40" W=0.03" D=0.057 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 105. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 TRM 53-21-01 & DWG NR D53110422.
DURING INSPECTION, FOUND R1 DOOR FWD AND AFT BLANKING PLATES CORRODED. REMOVED CORROSION IAW SRM 51-74-00, DIMENSIONS AS FOLLOWS: FWD L=1.5" W=1.0"D=.006", AFT L=1.0" W=1.0" D=.005" NO ALLOWABLE DANAGE LIMITATION IN SRM, REPLACED FWD & AFT BLANKING PLATES TO BE INSTALLED ON W/C 2500-6602.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 64 TO FR 66 Y-1292 HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AREA MEASURES L:1" W:1" D:.075" ORIG MAT. .100". FOUND OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT Y-1292 FROM FR 64-66 IAW SRM 51-42-11.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68-69 Y-1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AREA MEASURES L:4" W:3" D:.108" ORIG MAT. .155". FOUND OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOOR SUPPORT Y-1292 FROM FR 68-69 IAW SRM 51-42-11.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT RT SIDE BETWEEN FR 66-68, Y-1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AREA MEASURES L:2" W:1" D:.080" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOOR SUPPORT Y-1292 FROM FR 66-68 IAW SRM 51-42-11.
DURING INSPECTION, FOUND FORWARD CABIN FLOORBEAM BETWEEN FR16 TO FR23 Y254 UPPER SURFACE FLANGE HAS CORROSION. REPLACED FLOORBEAM Y254V FROM FR14-FR24 IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W=1.0" D=0.079". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOORBEAM BETWEEN FR64 TO FR66, Y765 UPPER SURFACE FLANGE & HARD PT. HOLES HAS CORROSION. REPLACED FLOORBEAM Y765 IAW SRM 51-42-11. BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS IAW TRM 53-41-15. L=1.5" W=.5" D=.050".
DURING INSPECTION, FOUND AFT UTILITY AREA FLOORBEAM BETWEEN FR 65 TO FR 66 Y-465 UPPER FLANGE AND HARD PT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS, L=2"W=1"D=.035", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOORBEAM AT -Y465 FROM FR 64 TO FR 67 IAW SRM 51-42-11 AND TRM 53-21-01.
DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 231 QF DAMAGED 3.0"X 4.0". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOORBEAM AT FR 68 Y765 UPPER FLANGE HAS CORRODED. BLENDED CORROSION IAW SRM 51-74-00; FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, L 2.0" W= 2.2 "D= 0.065"; REPLACED FLOORBEAM IAW SRM 51-42-11 & TRM 53-21-01.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR67 TO FR68 Y-254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.0" W=1.5" D=0.050" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOOR SUPPORT IAW DWG D53472000 & SRM 51-42-11.
DURING INSPECTION, FOUND FORWARD CABIN FLOORBEAM BETWEEN FR 20-21 Y-189 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW 53-11-14, FIG 105. REPLACED FLOORBEAM Y-189 IAW SRM 51-42-11.L=1.244"X W=1. 050"X D=0.070".
DURING INSPECTION, AFT CABIN RT SIDE BETWEEN FR 69 TO 70 FRAME SUPPORT OF SHEAR PLATE CORRODED ON UPPER & LOWER SURFACE. REMOVED CORROSION IAW SRM 51-74-00; CHECKED LIMITS DIMENSIONS L=1.0"W=0.900"D=0.017" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-17; REPLACED FRAME SUPPORT IAW SRM 51-42-11. APPLIED TOP COAT TO FASTENERS IAW SRM 51-75-12.
DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF IS CORRODED ON UNDERSIDE. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS, NO ALLOWABLE DAMAGE IN SRM. REPLACED FLOOR PANEL.
DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 12-16 Y503.2 UPPER SURFACE FLANGE HAS CORROSION. FLOORBEAM Y503.2 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED FLOORBEAM IAW SRM 51-42-11. LOCATED AND DRILLED NEW BEAM IAW SRM 51-44-11. INSTALLED NEW BEAM IAW TRM 53-20-01.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOORBEAM LT SIDE AT FR68, Y465 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.6" W=W=1.0" D=.055" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOORBEAM IAW SRM 51-42-11 & DWG D53472000.
DURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 66 TO FR69 Y-765 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=4.0" W=1.0" D=.025" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, ORIG MAT .157". R & R FLOOR SUPPORT Y-765 BTW FR66 - FR70 IAW SRM 51-42-11 & DWG D53472000.
DURING NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 ABC INOPERATIVE. MAINTENANCE REPLACED SEAT HARNESS AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 5/6 INOP. SECURED CONNECTOR IN SIDE WALL AND TESTS OK.