N309DU
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
53 reports on file, 2021-10-04 – 2026-08-14.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
UPPER AFT FUSELAGE CABIN, RT OTBD SEAT TRACK CORROSION LEVEL 2 NOTED AT THE AFT END, RBL 43.5, FR 74. SEAT TRACK FROM FR 61-FR 74, RBL 43.5 WAS REPLACED IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01342701 REV-G. (LP 1755837 - AIRCRAFT WAS GROUNDED)
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
CORROSION LEVEL 2 ON FLOOR SUPPORT BRACKET AT FR 79 RBL 24. REPLACED FLOOR SUPPORT BRACKET AT FR79 RBL 24 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01342700 REV-T. (LP 1751325- AIRCRAFT WAS GROUNDED)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
UPPER AFT FUSELAGE CABIN, LT OTBD SEAT TRACK CORRODED, NOTED AT THE AFT END, LBL 43.5, FR 74. REPLACED THE AFT FUSELAGE CABIN LT OTBD SEAT TRACK IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01342701, REV-G. (LP 1748894 - AIRCRAFT WAS GROUNDED)
Part: SUPPORT — WORN (ZONE 100) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
AFTER EVALUATING THE BARE METAL ON THE AFT FAIRING SUPPORT LOCATED AT FR61 BETWEEN RBL 10 TO LBL 10 FOUND CORROSION. NO DAMAGE IS ALLOWED IAW ASRP BD500-A-J53-82-08-00AAA-661A-A, FIG 2. REPLACED THE FAIRING SUPPORT IAW PL C01731500 REV-E AND ASRP BD500-A-J51-42-06-00AAA-078A-A. (LP 1747473 - AIRCRAFT WAS GROUNDED)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
UPPER AFT FUSELAGE CABIN, RT, INBD SEAT TRACK CORROSION NOTED AT THE AFT END, RBL 23, FR 74. REPLACED SEAT TRACK RBL 23 BTW FR 61 TO FR 74 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, ASRP BD500-A-J51-42-06-00AAA-078A-A AND DWG C01342701, REV G. (LP 1744624 - AIRCRAFT WAS GROUNDED)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
UPPER AFT FUSELAGE CABIN, LT INBD SEAT TRACK CORROSION NOTED AT THE AFT END, LBL 23, FR 74. REPLACED SEAT TRACK LBL 23, FR 74 - FR 60 IAW ASRP BD500-A-J51-42-20-00AAA-078A AND DWG C01342701, REV-G. (LP 1743757 - AIRCRAFT WAS GROUNDED)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,604 hrs · 6,844 cycles
FORWARD FUSELAGE FLOOR STRUCTURE, RT INBD SEAT TRACK CORROSION NOTED AT THE FORWARD END, RBL 23, FR 20. REPLACED SEAT TRACK FROM FR 20 - FR 30 RBL23 IAW ASRP BD500-J51-42-20-00AAA-078A-A AND DWG C02312600, REV-J. (LP 1743765 - AIRCRAFT WAS GROUNDED)
Part: SKIN — DAMAGED (ZONE 100) · airframe 15,604 hrs · 6,844 cycles
SEE LOG PAGE 8612918 FOR ERA 634635-14 REV ORIG SECT I STEP 9 RESTORE FINISHES TO EXTERNAL SURFACES . C/W REP INSP. OF FWD BELLY FAIRING DAMAGE PER ASRP 51-12-00-04AAA-661A-A. SPEED TAPE IN GOOD CONDITION OK. (LP# 8612921; AIRCRAFT WAS GROUNDED)
Part: FRAME — CRACKED (WNG-BDY FAIRING) · airframe 14,128 hrs · 6,257 cycles
DURING AIRFRAME VIBRATION INVESTIGATION FOUND WTBF FRAME ASSEMBLY INBD END THAT ATTACHED TO LONGERON DEVELOPED A 1.25" L-CRACK REF A220 IPD 53-82-84-10AAB-941A-D. ITEM -75 P/M C02382115-001. REMOVED FRAME 48 OF WTBF SUPPORT STRUCTURE IAW AMP 220 53-82. INSTALLED FRAME 48 WTBF IAW AMP A220- 53-82. (LP# 1424459)
Part: SPLICE PLATE — BROKEN (ZONE 100) · airframe 14,128 hrs · 6,257 cycles
FOUND SPLICE PLATE BROKEN P/N CO2386047-101 REMOVED DAMAGED SPLICE PLATE. INSTALLED SPLICE PLATE P/N C02386047-101 IAW A220 AMM 53-82. (LP# 1424461)
Earlier reports · 2021–2025 · 43 reports
2025
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 11,210 hrs · 5,054 cycles
LH SLAT TRACK NBR 4 PINION TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT LOG-PAGE UPDATED @ 01FEB25 1703 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 01943566 W C/W ERA 624035-14AD REV O AND PRI 624035-14AD REV 0 MATCHES ASSOCIATED ER/A 14-624035 ADDED FOR AC 8309. (LP# 0791010)
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 11,210 hrs · 5,054 cycles
LH SLAT TRACK NBR 4 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1655 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 02350989 W C/W ER/A 624035-14AD REV O AND PRI 624035-14AD REV 0 MATCHES. (LP# 0790998)
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 11,210 hrs · 5,054 cycles
LH SLAT TRACK NBR 7 PINION (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE NEXT FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1659 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 01943566 W C/W ERA 624035-14AD REV O AND PRI 624035-14AD REV 0 MATCHES. ASSOCIATED ER/A 14-624035 ADDED FOR AC 8309. (LP# 0791006)
Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 11,210 hrs · 5,054 cycles
LH SLAT TRACK NBR 7 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1701 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 02350989 W C/W ER/A 624035-14AD REV O AND PRI 624035-14AD REV 0 MATCHES. (LP# 0791008)
2024
Part: EROSION SHIELD — PEELING (ZONE 500) · airframe 11,143 hrs · 5,020 cycles
LH WINGLET LEADING EDGE EROSION TAPE PEELED UP AT LOWER EDGE. LH WINGLET LEADING EDGE WHERE EROSION TAPE IS DAMAGED AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 57-32-00-00AAA-662A-A. FWD TO MONITOR AND PERFORM REPETITIVE INSPECTIONS EVERY 150 FLIGHT HOURS AND TERMINATION ACTION AT 850 FLIGHT HOURS. REPLACED DIS BONDED SECTION OF ABRASION RESISTANT TAPE ON LEFT WINGLET REF A220 AMP 51-22-01-00AAA- 621A-A. OK TO CLOSE QC MON LOG. (00341696 23JAN25 10:41 UTC) (LP# 6687159)
Part: SLAT TRACK — WORN (LT NR 8) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 8 LOWER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER FWD I/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-605285 ADDED FOR AC 8309. (LP# 0445010)
Part: SLAT TRACK — WORN (LT NR 8) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 8 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445013)
Part: SLAT TRACK — WORN (LT NR 9) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445005)
Part: SLAT TRACK — CORRODED (RT NR 4) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14AD REV 0 MATCHED. (LP# 0445672)
Part: SLAT TRACK — CORRODED (LT NR 5) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444976)
Part: SLAT TRACK — WORN (RT NR 1) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 1 UPPER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14AD REV 0 MATCHED. (LP# 0445692)
Part: SLAT TRACK — WORN (LT NR 8) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 8 UPPER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 UPPER FWD I/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445007)
Part: SLAT TRACK — WORN (LT NR 7) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 7 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445002)
Part: SLAT TRACK — WORN (LT NR 8) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 8 UPPER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 UPPER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445011)
Part: SLAT TRACK — CORRODED (RT NR 5) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14AD REV 0 MATCHED. (LP# 0445676)
Part: SLAT TRACK — CORRODED (LT NR 2) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. (LP# 0444990)
Part: SLAT TRACK — WORN (LT NR 4) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444995)
Part: SLAT TRACK — WORN (LT NR 4) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444998)
Part: SLAT TRACK — CORRODED (LT NR 2) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444957)
Part: SLAT TRACK — WORN (RT NR 1) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 1 LOWER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082286-14AD REV 0 MATCHED. (LP# 0445675)
Part: SLAT TRACK — WORN (RT NR 3) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 3 LOWER AFT SURFACE (2 LOCATIONS) HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 3 LOWER AFT SURFACE (2 LOCATIONS) IAW ER/A 608286-14AD REV C AND PRI 608286-14AD REV 0 MATCHED. (LP# 0445685)
Part: SLAT TRACK — CORRODED (RT NR 4) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14AD REV 0 MATCHED. (LP# 04456663)
Part: SLAT TRACK — WORN (LT NR 4) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.MEASURED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444996)
Part: SLAT TRACK — CORRODED (LT NR 6) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0444984)
Part: SLAT TRACK — CORRODED (RT NR 5) · airframe 9,524 hrs · 4,311 cycles
RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14AD REV O MATCHED. (LP# 0445688)
Part: SLAT TRACK — WORN (LT NR 6) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. ASSOCIATED ER/A 14-608285 ADDED FOR AC 8309. (LP# 0445004)
Part: SLAT TRACK — CORRODED (LT NR 1) · airframe 9,524 hrs · 4,311 cycles
LH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 1 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AD REV 0 MATCHED. (LP# 0444988)
Part: SKIN — DENTED (FRM 30 S29L) · airframe 9,124 hrs · 4,138 cycles
DAMAGE FOUND- EXTERNAL DENT LEFT FWD FUSELAGE. 4 INCH X 3 INCH ABOVE STRG 29L AND AFT OF FR30A. TWO PANELS FWD CARGO OPENED FOR MTC(975849) REMOVED PAINT FROM EXTERNAL DENT FOR INSPECTION PER ENGINEERING REQUEST(249846) C/W HFEC OF DAMAGED AREA PER A220 ANDTP BD500-A-J51-01-08-01AAA- 353A-A. NO CRACKS NOTED(QC2028,017441) C/W SEC I TIME-LIMITED REPAIR PER ER/A 618348-14 REV ORIG STEPS 1-2(535412) C/W ERA 618348-14 REV ORIG SEC I STEP 3. NO CRACKS NOTED(QC 2028, 017441 ) C/W SEC I STEP 4, COPY OF ER/A 618348-14 PLACED IN FRONT OF LOGBOOK(535412). ALL REPAIRS COMPLETED PER ER/A 618361-14 REV A( 491375) RII COMPLETED(QC5367,327476) ASSOCIATED ER/A 14-618361 ADDED FOR AC 8309. (LP# 5970980)
Part: LEVER — DAMAGED (DOOR ARMING) · airframe 8,797 hrs · 3,982 cycles
CREW REPORTS 1L DOOR WILL NOT ARM AFTER CLOSURE. REMOVED SLIDE BUSTLE + PANEL SLIDE + SAFE TIED DOOR ASSIST BOTTLE . REMOVED SLIDE FROM DOOR + INNER DOOR LINER. REF. A220 AMP 52- 11, NO VISIBLE DAMAGE. GIRT BAR MAY BE BENT, DOOR WILL NOT CLOSE PROPERLY + "ARM DISARM" LEVER WILL NOT MOVE. CONDUCTED SPECIAL IMPACT INSPECTION REF A220 AMP 51-13, WILL NEED FURTHER INSPECTION + TROUBLESHOOTING. WIP 810751. FOUND TRIGGER LEVER FOR EOAM OVER CENTER. RESET IT DOOR ARMING LEVER OPS NORMAL. (WIP 416340) FOUND DOOR NOT LIFTITNG ENOUGH TO ENGAGE INTO LOWER ROLLER GUIDES. ADJUSTED LIFT, ALL NOW WITHIN LIMITS. REF A220 AMP 52-11-00. SLIDE REINSTALLED PER AMDS W.C. 2563-4001 RII STAMPED IN W.C. ALL CLOSEUP AND CHECKS COMPLETE. A/C OK FOR SVC. (LP# 5332452)
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 7,997 hrs · 3,680 cycles
SEAT TRACK LBL 23 CORRODED AFT OF LAV C2 (203) SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/117 00234 PERFORMED SPLICE REPAIR PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND ER/A 615104-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/117 00234 PERFORMED SEAT TRACK SPLICE REPLACEMENT PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND E R/A 615104-14 REV ORIGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00738862. (LP# 0182740)
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 7,997 hrs · 3,680 cycles
SEAT TRACK LBL 43.5 CORRODED AFT OF LAV C2 (203). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/118 00235 PERFORMED SPLICE REPAIR PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND ER/A 615104-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/118 00235 PERFORMED SEAT TRACK SPLICE REPLACEMENT PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND E R/A 615104-14 REV ORIGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00738862. (LP# 0182744)
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 7,997 hrs · 3,680 cycles
SEAT TRACK RBL 23 CORRODED AFT OF LAV D4 (204). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/120 00237 PERFORMED SEAT TRACK SPLICE REPLACEMENT PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND E R/A 615104-14 REV ORIGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00738862. (LP# 0182747)
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 7,997 hrs · 3,680 cycles
SEAT TRACK RBL 43.5 CORRODED AFT OF LAV D4 (204). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/119 00236 PERFORMED SPLICE REPAIR PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND ER/A 615104-14 REV ORIGINAL. (LP# 0182746)
Part: SERVICE PANEL — DELAMINATED (LAVATORY) · corrosion level 2 · airframe 7,997 hrs · 3,680 cycles
LAV SERVICE PANEL - PROTECTIVE SEALANT DELAMINATING INSIDE LAV SERVICE PANEL. EVIDENCE OF CORROSION NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2021-2015/005 00005 REPAIRED PER PRI 614826-14 REV. 0, REV 1AND REV 2 AND ER/A 614826-14 REV. ORIGINAL. (LP# 0180743)
Part: PIN — INOPERATIVE (OVERWING SLIDE) · airframe 7,981 hrs · 3,672 cycles
UNABLE TO INSTALL R/H OVER WING SLIDE SAFETY VALVE PIN. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0204:2561-9101/001 00014 ACCOMPLISHED SAMPLING FUNCTIONAL DEPLOYMENT CHECK AND REPLACED SLIDE REF AMDS 2561-9006 AND AMDS 2563-4005. (LP# 0178916)
Part: DOOR — CORRODED (AFT LAV SERVICE) · corrosion level 2 · airframe 7,981 hrs · 3,672 cycles
AFT TOILET SERVICE DOOR CORRODED AFT RIGHT CORNER. "MARKED".SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2021-2015/008 00258 REMOVED AND REPLACED TOILET SERVICE DOOR. PER A220 ASRP 52-47-06. (LP# 0168084)
Part: SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 7,981 hrs · 3,672 cycles
FWD CARGO SILL REQUIRES REPLACEMENT DUE TO CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0251:5321-2015/002 00260 REPAIRED PER PRI 614834-14 REV 0 AND ER/A 614834-14 REV. ORIGINAL (LP# 0160460).
Part: DOOR SILL — NOT REPORTED (ZONE 100) · airframe 15,171 hrs · 6,652 cycles
ERA 614834-14 ISSUED FOR FWD CARGO SILL REPAIR. FOLLOW ON ACTION IS REQUIRED AS SECTION I REPAIR IS CONSIDERED TIME-LIMITED. SECT.I ACCOMPLISHED @ CCK VISIT MSP 16JAN24. SECT.II REPEAT INSPECTIONS TBA @ EVERY 1000FHAFTER SECT. I. SECT. III PERMANENT REPAIR REQUIRED PRIOR TO 10000FH AFTER SECT.I. FOLLOW ON ACTION IS REQUIRED. ERA REVISION REQUIRED FOR SERVICE BEYOND 10000FH. (LP# 0157524)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,981 hrs · 3,672 cycles
ERA 614826-14 SECTION I ISSUED TO MTC IN MSP DURING CCK FOR CORROSION ON THE WASTE BOX DOUBLER. FOLLOW ON ACTION IS REQUIRED. W ACCOMPLISH ERA 614826-14 SECTION II EVERY 1000 FH AFTER SECTION I. SECTION I IS TIME LIMITED TO 10000 FH. THIS RESTRICITON IS TRACKED PER SECTION III. THIS IS A MAJOR REPAIR. ASSOCIATED ER/A 00-614826 ADDED FOR AC 8309. (LP# 0150446)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 7,981 hrs · 3,672 cycles
AFT DRAIN MAST INTERNAL SUPPORT STRUCTURE FOUND CORRODED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0241:3833-2001/004 00253 REPLACED SUPPORT ANGLES REF. A220 ASRP 51-42-06. (LP# 0145763)
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 7,981 hrs · 3,672 cycles
RH MLG WHEEL WELL- FWD LOWER LEG OF LONGERON IS SEVERED JUST O/B OF THE RAT, AFT SIDE OF WHEEL WELL. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0328:2090-2065-RH/004 00162. COMPLETE: REMOVED AND REPLACED LONGERON REF A220 ASRP 51-40-00. (LP# 0144074)
2022
Part: ENGINE — VIBRATES · airframe 4,330 hrs · 2,085 cycles
A/C 8309 DIVERTED TO DEN DUE TO RIGHT ENGINE N2 VIBS. QRH REQUIRED TO REDUCE THRUST UNTIL VIBS WITHIN LIMITS. REDUCED THRUST VIB INDICATION CLEARED PER QRH OK TO CONTINUE WITH NORMAL ENGINE OPERATION. ALL OTHER INDICATIONS NORMAL. CORRECTIVE ACTION: PER AMP THIS IS A TRANSIENT N2 VIBRATION. CHECKED MCD'S AS PRECAUTION PERFORMED VISUAL INSPECTION A/C RTS. (LP# 9610434)
2021
Part: NONE — NONE · airframe 857 hrs · 362 cycles
SHIP 8309 - DIV - TO BUF DUE TO EQUIPMENT BAY SMOKE FAIL MESSAGE. CORRECTIVE ACTION: REPLACED FIDEX CONTROLLER, AVIONICS SMOKE DETECTORS 1 AND 2, AND CDC-2 LRM 15 POWER MODULE. (LP#7981640)