# N306DU: 2020 Airbus Canada LP BD-500-1A11 - Status: Valid registration - Airframe: [Airbus Canada LP BD-500-1A11](https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11) (registry code 1400015, 153 seats) - Engine: [Pratt & Whitney PW1521G SERIE](https://openairdocs.org/engine/pratt-whitney-pw1521g-serie) (registry code 51763) - Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership) (OpenAirDocs) - Serial number: 55085 - Year built: 2020 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 7, 2020 - Certificate issued: December 8, 2020 - Expires: December 31, 2027 - Mode S code: A335FA - Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=306DU - Page: https://openairdocs.org/aircraft/N306DU From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 71 in force ### Matched by airframe (Airbus Canada LP BD-500-1A11) - [AD 2026-15-14](https://openairdocs.org/ad/2026-15-14): Engine fuel and control · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 3, 2026 - [AD 2026-13-52](https://openairdocs.org/ad/2026-13-52): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 7, 2026 - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2026-10-12](https://openairdocs.org/ad/2026-10-12): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026 - [AD 2026-10-10](https://openairdocs.org/ad/2026-10-10): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026 - [AD 2026-10-07](https://openairdocs.org/ad/2026-10-07): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026 - [AD 2026-07-04](https://openairdocs.org/ad/2026-07-04): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 11, 2026 - [AD 2026-06-06](https://openairdocs.org/ad/2026-06-06): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2026 - [AD 2026-07-07](https://openairdocs.org/ad/2026-07-07): Air conditioning system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 17, 2026 - [AD 2026-04-04](https://openairdocs.org/ad/2026-04-04): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 8, 2026 - [AD 2025-20-08](https://openairdocs.org/ad/2025-20-08): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 30, 2025 - [AD 2025-19-07](https://openairdocs.org/ad/2025-19-07): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 6, 2025 - [AD 2025-19-01](https://openairdocs.org/ad/2025-19-01): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 23, 2025 - [AD 2025-17-01](https://openairdocs.org/ad/2025-17-01): Flight controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 29, 2025 - [AD 2025-16-01](https://openairdocs.org/ad/2025-16-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 18, 2025 - [AD 2025-12-04](https://openairdocs.org/ad/2025-12-04): Hydraulic Power · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 25, 2025 - [AD 2025-09-02](https://openairdocs.org/ad/2025-09-02): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 18, 2025 - [AD 2025-11-06](https://openairdocs.org/ad/2025-11-06): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective Jun 16, 2025 - [AD 2025-07-04](https://openairdocs.org/ad/2025-07-04): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective May 27, 2025 - [AD 2025-06-06](https://openairdocs.org/ad/2025-06-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 2, 2025 - [AD 2025-05-07](https://openairdocs.org/ad/2025-05-07): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 15, 2025 - [AD 2025-02-06](https://openairdocs.org/ad/2025-02-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 9, 2025 - [AD 2025-03-05](https://openairdocs.org/ad/2025-03-05): Stabilizers · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 21, 2025 - [AD 2024-24-08](https://openairdocs.org/ad/2024-24-08): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 13, 2025 - [AD 2024-23-05](https://openairdocs.org/ad/2024-23-05): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 6, 2025 - [AD 2024-22-01](https://openairdocs.org/ad/2024-22-01): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 31, 2024 - [AD 2024-22-04](https://openairdocs.org/ad/2024-22-04): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 17, 2024 - [AD 2024-22-03](https://openairdocs.org/ad/2024-22-03): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 14, 2024 - [AD 2024-15-06](https://openairdocs.org/ad/2024-15-06): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 15, 2024 - [AD 2024-17-04](https://openairdocs.org/ad/2024-17-04): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 20, 2024 - [AD 2024-12-02](https://openairdocs.org/ad/2024-12-02): Portable Oxygen System · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 13, 2024 - [AD 2024-09-01](https://openairdocs.org/ad/2024-09-01): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 2, 2024 - [AD 2024-10-11](https://openairdocs.org/ad/2024-10-11): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2024 - [AD 2024-10-03](https://openairdocs.org/ad/2024-10-03): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 28, 2024 - [AD 2024-07-11](https://openairdocs.org/ad/2024-07-11): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 6, 2024 - [AD 2024-05-10](https://openairdocs.org/ad/2024-05-10): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024 - [AD 2024-05-08](https://openairdocs.org/ad/2024-05-08): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024 - [AD 2024-04-08](https://openairdocs.org/ad/2024-04-08): Electrical power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 23, 2024 - [AD 2024-03-09](https://openairdocs.org/ad/2024-03-09): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Apr 16, 2024 - [AD 2023-24-01](https://openairdocs.org/ad/2023-24-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 2, 2024 - [AD 2023-20-01](https://openairdocs.org/ad/2023-20-01): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 9, 2023 - [AD 2023-16-03](https://openairdocs.org/ad/2023-16-03): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 25, 2023 - [AD 2023-16-02](https://openairdocs.org/ad/2023-16-02): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 22, 2023 - [AD 2023-12-09](https://openairdocs.org/ad/2023-12-09): Flight control system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 7, 2023 - [AD 2023-14-02](https://openairdocs.org/ad/2023-14-02): Navigation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 27, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2023-07-01](https://openairdocs.org/ad/2023-07-01): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 19, 2023 - [AD 2022-26-06](https://openairdocs.org/ad/2022-26-06): Placards and markings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Feb 2, 2023 - [AD 2022-25-19](https://openairdocs.org/ad/2022-25-19): Hardware, Engine Exhaust · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023 - [AD 2022-25-05](https://openairdocs.org/ad/2022-25-05): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023 ### Matched by engine (Pratt & Whitney PW1521G SERIE) None in force. ### Historical (superseded or no longer in force) - [AD 2025-06-01](https://openairdocs.org/ad/2025-06-01) (historical): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2025 - [AD 2024-04-11](https://openairdocs.org/ad/2024-04-11) (historical): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2024 - [AD 2024-04-06](https://openairdocs.org/ad/2024-04-06) (historical): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2024 - [AD 2023-05-08](https://openairdocs.org/ad/2023-05-08) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 12, 2023 - [AD 2022-25-51](https://openairdocs.org/ad/2022-25-51) (historical): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 27, 2022 - [AD 2022-19-09](https://openairdocs.org/ad/2022-19-09) (historical): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 27, 2022 - [AD 2021-09-03](https://openairdocs.org/ad/2021-09-03) (historical): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 4, 2021 - [AD 2021-04-05](https://openairdocs.org/ad/2021-04-05) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 30, 2021 - [AD 2019-23-15](https://openairdocs.org/ad/2019-23-15) (historical): Time Limits/ Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 16, 2020 - [AD 2018-25-04](https://openairdocs.org/ad/2018-25-04) (historical): Cargo and accessory compartment · C Series Aircraft Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 14, 2019 All 81: https://openairdocs.org/aircraft/N306DU/ads.md ## Information bulletins (advisory) (1 in force) - [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019 ## NTSB investigations None matched to N306DU. ## FAA accident and incident reports None matched to N306DU. ## Service difficulty reports (98, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2026081404650](https://openairdocs.org/sdr/DALA2026081404650), Aug 12, 2026: SEAL. LEAKING. IN FLIGHT LIGHT ODOR DETECTED AROUND ROWS 17,18,19,20. FOUND OIL IN NR 2 ENGINE SPINNER, REPLACED FAN SHAFT COVER SEAL PER A220 AMP 72-15. AMDS W/C'S 0550-2001 - [SDR DALA2026080404485](https://openairdocs.org/sdr/DALA2026080404485), Aug 3, 2026: ENGINE. VIBRATION. DIVERTED TO ATL DUE TO NBR 2 ENGINE VIBES. NR 2 ENG VIBS 1.25 FOR 38 SEC. MAINTENANCE IN PROGRESS. - [SDR DALA2026070904025](https://openairdocs.org/sdr/DALA2026070904025), Jul 7, 2026: STRUT. FOD. ATB - WOW FAIL ON TAKE OFF. REMOVED LT MLG SHOCK STRUT. FOUND CHEESE CLOTH WRAPPED AROUND BEARING AND SEALS. REMOVED ALL DEBRIS, RE-PACKED LEFT MLG SLIDING TUBE - [SDR DALA2026062903853](https://openairdocs.org/sdr/DALA2026062903853), Jun 24, 2026: ANTI-ICE VALVE. FAULTED. DIV - TO SLC DUE TO "R WING A/ICE FAIL" MESSAGE. R & R RT WAI VALVE AND PRESSURE SENSOR HARNESS. (LP# 8948718; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062303731](https://openairdocs.org/sdr/DALA2026062303731), Jun 20, 2026: LIGHT. INOPERATIVE. MULTIPLE EMERGENCY EXIT EXTERIOR LIGHTS OUT. REPLACED EMERGENCY EXTERNAL LIGHTS (FWD RT, AFT LT AND AFT RT) IAW AMP BD500-A-J33-55-02-01AAA-520A-A, BD500-A-J33- - [SDR DALA2026062303730](https://openairdocs.org/sdr/DALA2026062303730), Jun 19, 2026: LIGHT. INOPERATIVE. BOTH LT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE, NEED TO REPLACE. REPLACED BOTH LT OVERWING EXTERNAL EMERGENCY LIGHT IAW AMP BD500-A-J33-55-02-02AAA-720A- - [SDR DALA2026061703626](https://openairdocs.org/sdr/DALA2026061703626), Jun 15, 2026: FLOOR SUPPORT. CORRODED. CORROSION AT REAR BARREL FLOOR EDGE SUPPORT AT FR 76 RBL 49 WL 147 . REMOVED AND REPLACED SILL FLOOR WEB AT STA FR76 RBL 49 WL 147 PER A220 ASRP BD500-A-J51-42- - [SDR DALA2026061703625](https://openairdocs.org/sdr/DALA2026061703625), Jun 12, 2026: FLOOR PANEL. CORRODED. FORWARD CABIN FLOOR PANEL 221 KLF (L1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 221 KLF AT L1 DOOR PER AMP BD500-A-J53 -00-47-12AAA - [SDR DALA2026061503586](https://openairdocs.org/sdr/DALA2026061503586), Jun 12, 2026: FLOOR PANEL. CORRODED. CORROSION ON FORWARD CABIN FLOOR PANEL 222 KRF (R1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 222 KRF AT R1 DOOR IAW AMP BD500-A-J53 - [SDR DALA2026061503585](https://openairdocs.org/sdr/DALA2026061503585), Jun 12, 2026: FLOOR PANEL. CORRODED. AFT SERVICE DOOR FLOOR PANEL 242MRF CORRODED ON AFT INBD CORNER. REMOVED AND REPLACED FLOOR PANEL 242MRF AT AFT SERVICE DOOR IAW AMP BD500-A-J53-00-47-14AAA-720 - [SDR DALA2026061503584](https://openairdocs.org/sdr/DALA2026061503584), Jun 12, 2026: FLOOR SUPPORT. CORRODED. CORROSION AT REAR BARREL FLOOR EDGE SUPPORT BETWEEN FR 74 TO FR 76 LBL 49 WL147. REMOVED AND REPLACED FLOOR PANEL SUPPORT FROM FR74 TO FR76 LBL 49 WL 147 IAW A2 - [SDR DALA2026060903489](https://openairdocs.org/sdr/DALA2026060903489), Jun 4, 2026: SEAT TRACK. CORRODED. CORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342722-009S1 LOT 5196527-3 AT REAR BARREL FROM FR - [SDR DALA2026060903488](https://openairdocs.org/sdr/DALA2026060903488), Jun 4, 2026: SEAT TRACK. CORRODED. CORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342723-0095 LOT 5194663-1 OF REAR BARREL FROM FR61 - [SDR DALA2026053003280](https://openairdocs.org/sdr/DALA2026053003280), May 29, 2026: SEAT TRACK. CORRODED. CORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 43.5 WL147. REPLACED SEAT TRACK AT LBL=43.5, WL=147 BTW FR=60 TO FR=75 PER A220 ASRP BD500-A-J51- - [SDR DALA2026053003279](https://openairdocs.org/sdr/DALA2026053003279), May 29, 2026: SEAT TRACK. CORRODED. CORROSION LEVEL 2 AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 43.5 FR 20 WL 147. REPLACED SEAT TRACK RBL 43.5 FR20 - FR30 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A A - [SDR DALA2026052703196](https://openairdocs.org/sdr/DALA2026052703196), May 26, 2026: SEAT TRACK. CORRODED. CORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 43.5 WL147. REPLACED SEAT TRACK RBL 43.5 FR61 - FR74 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A - [SDR DALA2026052703195](https://openairdocs.org/sdr/DALA2026052703195), May 26, 2026: SEAT TRACK. CORRODED. CORROSION AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 23 FR 20 WL 147. REPLACED FWD CABIN RIGHT SIDE SEAT TRACK RBL23 BTW FR19 TO FR31 WL 147 IAW ASRP BD500-A-J51- - [SDR DALA2026011400342](https://openairdocs.org/sdr/DALA2026011400342), Jan 12, 2026: SLIDE. WARNING MESSAGE. ON FINAL APPROACH, WING SLIDE CAUTION COME ON INTERMITTENTLY. DOORS PAGE SHOWED LEFT SLIDE YELLOW DOOR INDICATION IN AFT. INTERMITTENT INDICATION CONTINUED ON T - [SDR DALA2025111708376](https://openairdocs.org/sdr/DALA2025111708376), Nov 14, 2025: SKIN. PUNCTURED. HOLE IN FUSELAGE, AFT OF DOOR 1L. ACCESSED TO DAMAGE IS FWD BB, SUBMITTED DIMENSIONS OF DAMAGE TO ENGINEERING. ALL REPAIR WORK COMPLETED IAW ER/A 630504-14 REV. - [SDR DALA2025070204957](https://openairdocs.org/sdr/DALA2025070204957), Jun 25, 2025: ENGINE. ODOR. DIRTY SOCK SMELL IN AFT GALLEY DURING DESCENT. T/S PER AMDS W/C 0550-2001. FOUND OIL ODOR COMING FROM LT ENG DURING HIGH POWER OP (+80% N1). C/W AMDS W/C 0550-6 - [SDR DALA2025052003863](https://openairdocs.org/sdr/DALA2025052003863), May 16, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 RACK TEETH 1 AND 2 HAS EVIDENCE OF CORROSION WITH EVIDENCE OF PREVIOUS REWORK. LIAISON ENGINEERING SUPPORT WILL BE REQ BEFORE FURTHER FLIGHT. C - [SDR DALA2025010800175](https://openairdocs.org/sdr/DALA2025010800175), Jan 5, 2025: UNKNOWN. ODOR. ON DESCENT THROUGH 8000 FT WE SMELLED A STRONG ODOR SIMILAR TO OIL BURNING FOR APPROXIMATELY TWO MINUTES IN BOTH THE FLIGHT DECK AND CABIN. NO SMOKE WAS PRESENT - [SDR DALA2024093009542](https://openairdocs.org/sdr/DALA2024093009542), Sep 28, 2024: VALVE. LOCKED. SHIP 8306 - ATB - DUE TO TRIM AIR INDICATION WITH TRIM AIR VALVE LOCKED CLOSED. CORRECTIVE ACTION: REMOVED AND REPLACED TRIM AIR PRESSURE REGULATING VALVE. OPS - [SDR DALA2024021302039](https://openairdocs.org/sdr/DALA2024021302039), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR - [SDR DALA2024021302038](https://openairdocs.org/sdr/DALA2024021302038), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 11 LOWER FORWARD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302037](https://openairdocs.org/sdr/DALA2024021302037), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021302036](https://openairdocs.org/sdr/DALA2024021302036), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302035](https://openairdocs.org/sdr/DALA2024021302035), Feb 7, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK NBR 1 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2A. LIAISON ENGINEERING SUPPORT WIL - [SDR DALA2024021302034](https://openairdocs.org/sdr/DALA2024021302034), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH - [SDR DALA2024021302033](https://openairdocs.org/sdr/DALA2024021302033), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021302032](https://openairdocs.org/sdr/DALA2024021302032), Feb 7, 2024: SLAT TRACK. CORRODED. 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 FURT - [SDR DALA2024021302031](https://openairdocs.org/sdr/DALA2024021302031), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021302030](https://openairdocs.org/sdr/DALA2024021302030), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR - [SDR DALA2024021302029](https://openairdocs.org/sdr/DALA2024021302029), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 9 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR - [SDR DALA2024021302028](https://openairdocs.org/sdr/DALA2024021302028), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302027](https://openairdocs.org/sdr/DALA2024021302027), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302026](https://openairdocs.org/sdr/DALA2024021302026), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302025](https://openairdocs.org/sdr/DALA2024021302025), Feb 7, 2024: SLAT TRACK. CORRODED. 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 FURT - [SDR DALA2024021302024](https://openairdocs.org/sdr/DALA2024021302024), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 LOWER FORWARD O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302023](https://openairdocs.org/sdr/DALA2024021302023), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021302022](https://openairdocs.org/sdr/DALA2024021302022), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021201919](https://openairdocs.org/sdr/DALA2024021201919), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR - [SDR DALA2024021201918](https://openairdocs.org/sdr/DALA2024021201918), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021201917](https://openairdocs.org/sdr/DALA2024021201917), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2B. LIAISON ENGINEERING SUPPORT WILL - [SDR DALA2024021201916](https://openairdocs.org/sdr/DALA2024021201916), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 9 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021201915](https://openairdocs.org/sdr/DALA2024021201915), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021201914](https://openairdocs.org/sdr/DALA2024021201914), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021201913](https://openairdocs.org/sdr/DALA2024021201913), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT - [SDR DALA2024021201912](https://openairdocs.org/sdr/DALA2024021201912), Feb 7, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE - [SDR DALA2024021201911](https://openairdocs.org/sdr/DALA2024021201911), Feb 7, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT All 98: https://openairdocs.org/aircraft/N306DU/reports.md ## STCs that may be installed (OpenAirDocs) (13) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Airbus Canada LP BD-500-1A11) - [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects - [STC ST04818NY](https://openairdocs.org/stc/ST04818NY): Installation of a Passenger Seat Re-Pitch. ALOFT AeroArchitects - [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF - [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc - [STC ST04803NY](https://openairdocs.org/stc/ST04803NY): Installation of a Panasonic Avionics In-Flight Entertainment System. Delta Engineering Coporation - [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST04792NY](https://openairdocs.org/stc/ST04792NY): Update of Intelsat 2Ku. Delta Engineering Corporation - [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation - [STC ST04483AT](https://openairdocs.org/stc/ST04483AT): Installation of the Avionics Support Group Constant Friction Mount (cfMount) with Cradle. Avionics Support Group Inc - [STC ST03972NY](https://openairdocs.org/stc/ST03972NY): Installation of Honeywell Satcom SBB Upgrade and WiFi Network Activation. UMLAUT ENGINEERING GMBH - [STC ST04073NY](https://openairdocs.org/stc/ST04073NY): Installation of navAero Electronic Flight Bag provisions. Delta Engineering Corporation ## Related - Other Airbus Canada LP BD-500-1A11 aircraft: https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11/aircraft.md - The Pratt & Whitney PW1521G SERIE engine: https://openairdocs.org/engine/pratt-whitney-pw1521g-serie.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.