# N136DQ: 2020 Airbus Canada Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [Airbus Canada Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10) (registry code 1400010, 133 seats)
- Engine: [Pratt & Whitney PW1519G](https://openairdocs.org/engine/pratt-whitney-pw1519g) (registry code 52315)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership), [TCDS E00090EN](https://openairdocs.org/tcds/E00090EN) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 50055
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 2020
- Certificate issued: October 28, 2020
- Expires: October 31, 2027
- Mode S code: A091D5
- 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=136DQ
- Page: https://openairdocs.org/aircraft/N136DQ

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): 75 in force

### Matched by airframe (Airbus Canada Ltd Ptnrsp BD-500-1A10)

- [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 2025-09-02](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 2025-06-06](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 2024-10-11](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 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 2023-07-05](https://openairdocs.org/ad/2023-07-05): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10. Effective May 30, 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
- [AD 2022-21-03](https://openairdocs.org/ad/2022-21-03): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 14, 2022
- [AD 2022-16-02](https://openairdocs.org/ad/2022-16-02): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 25, 2022
- [AD 2022-16-08](https://openairdocs.org/ad/2022-16-08): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 1, 2022
- [AD 2022-11-21](https://openairdocs.org/ad/2022-11-21): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 15, 2022

### Matched by engine (Pratt & Whitney PW1519G)

- [AD 2025-04-13](https://openairdocs.org/ad/2025-04-13): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 8, 2025
- [AD 2024-06-04](https://openairdocs.org/ad/2024-06-04): Turbine Engine Compressor Section; Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 11, 2024
- [AD 2022-27-04](https://openairdocs.org/ad/2022-27-04): Engine Controls · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Jan 31, 2023
- [AD 2022-15-03](https://openairdocs.org/ad/2022-15-03): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 19, 2022
- [AD 2022-02-05](https://openairdocs.org/ad/2022-02-05): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Jan 27, 2022
- [AD 2021-20-01](https://openairdocs.org/ad/2021-20-01): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 27, 2021
- [AD 2021-17-09](https://openairdocs.org/ad/2021-17-09): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 22, 2021
- [AD 2020-04-01](https://openairdocs.org/ad/2020-04-01): Turbine Engine Oil System · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Mar 27, 2020
- [AD 2019-16-15](https://openairdocs.org/ad/2019-16-15): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 1, 2019

### 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
- [AD 2021-14-06](https://openairdocs.org/ad/2021-14-06) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 12, 2021
- [AD 2020-07-02](https://openairdocs.org/ad/2020-07-02) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Apr 15, 2020
- [AD 2019-21-11](https://openairdocs.org/ad/2019-21-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 29, 2019
- [AD 2019-19-11](https://openairdocs.org/ad/2019-19-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 26, 2019

All 89: https://openairdocs.org/aircraft/N136DQ/ads.md

## Information bulletins (advisory) (2 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
- [SAIB NE-20-09](https://openairdocs.org/saib/NE-20-09): TURBINE ENGINE COMPRESSOR SECTION. Issued Apr 30, 2020

## NTSB investigations

None matched to N136DQ.

## FAA accident and incident reports

None matched to N136DQ.

## Service difficulty reports (55, 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 DALA2026041002301](https://openairdocs.org/sdr/DALA2026041002301), Apr 8, 2026: HEATER. ODOR. DIVERTED TO OAK DUE TO DIRTY SOCK SMELL. DECLARING AN EMERGENCY. DEFERRED AFT GALLEY FAN AND GALLEY HEATER. LATER, AFT GALLEY HEATER WAS REPLACED. (LP 7963269, 
- [SDR DALA2026031801872](https://openairdocs.org/sdr/DALA2026031801872), Mar 15, 2026: SKIN. PUNCTURED. PUNCTURE TO LH SIDE FUSELAGE SKIN BETWEEN FR69-FR70 AND BETWEEN STR 33L AND 34L. REPAIRED DAMAGE SKIN ON L/H SIDE FUSELAGE BETWEEN FR69-FR70 AND BETWEEN STR 33L
- [SDR DALA2026031701847](https://openairdocs.org/sdr/DALA2026031701847), Mar 13, 2026: DOUBLER. CORRODED. WHILE PERFORMING DVI OF ER/A 610625-14 REV ORIGINAL SECTION II OF CC JOB#136-2882877 CORROSION WAS FOUND AT INTERNAL DOUBLER AFT EDGE CORNERS OF WASTE BOX CUTOU
- [SDR DALA2026041502390](https://openairdocs.org/sdr/DALA2026041502390), Mar 11, 2026: SKIN. CORRODED. ER/A 610625-14 REV A; A220 / LOWER AFT FUSELAGE / FR75-76 / WASTE SERVICE COMPARTMENT/CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 610625-14 
- [SDR DALA2026030901609](https://openairdocs.org/sdr/DALA2026030901609), Mar 8, 2026: ACCESS PANEL. CORRODED. CORROSION, FLOOR ACCESS PANEL AT THE R/H SERVICE DOOR AT FR76 NEAR RBL 43.5. REMOVED DAMAGED FLOOR ACCESS PANEL R/H SERVICE DOOR (ASD) AND REPLACED PER A220 AMP
- [SDR DALA2026030901610](https://openairdocs.org/sdr/DALA2026030901610), Mar 6, 2026: SUPPORT FITTING. CORRODED. CORRODED FLOOR PANEL SUPPORT FITTING AT RBL 23, FR 79. REMOVED AND REPLACED DOOR PANEL SUPPORT FITTING AT RBL 23 FR79 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A
- [SDR DALA2026030401493](https://openairdocs.org/sdr/DALA2026030401493), Mar 3, 2026: FLOOR PANEL. CORRODED. CORRODED FLOOR PANEL SUPPORT BETWEEN RBL 23 AND RBL 43.2 AT FR 76. REMOVED DAMAGED SUPPORT AND INSTALLED NEW FLOOR SUPPORT AT FR 76 -78 RBL 39" IAW BOMBARDIER D
- [SDR DALA2026030401487](https://openairdocs.org/sdr/DALA2026030401487), Mar 2, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK AT FR74, LBL44, WL151. REMOVED SEAT TRACK DAMAGED AND INSTALLED NEW SEAT TACK AT FR 74 TO FR61 LBL 44, WL 151 IAW A220 ASRP BD500-A-J51-
- [SDR DALA2026022601374](https://openairdocs.org/sdr/DALA2026022601374), Feb 22, 2026: SEAT TRACK. CORRODED. CORROSION FOUND ON FUSELAGE SEAT TRACK AT STA FR20 RBL 23. REMOVED DAMAGED SEAT TRACK AT STA FR20 TO FR30 RBL 23 AND INSTALLED NEW SEAT TRACK PER A220 ASRP BD50
- [SDR DALA2026022401322](https://openairdocs.org/sdr/DALA2026022401322), Feb 21, 2026: SUPPORT. CORRODED. LOWER FAIRING SUPPORT STRUCTURE AT FR 48 FROM BL0 TO LBL 13 WITH POSSIBLE CORROSION. REMOVED AND REPLACED LOWER FAIRING SUPPORT FRAME AT STA FR 48 FROM BL0 TO L
- [SDR DALA2026022401321](https://openairdocs.org/sdr/DALA2026022401321), Feb 20, 2026: SEAT TRACK. CORRODED. CORROSION FOUND ON FUSELAGE SEAT TRACK AT STA FR20 RBL 43.5. REMOVED AND REPLACED SEAT TRACK AT RBL 43.5 FROM STA FR 20 TO STA FR 30 IAW A220 ASRP BD500-A-J51-4
- [SDR DALA2026022401320](https://openairdocs.org/sdr/DALA2026022401320), Feb 18, 2026: FLOOR PANEL. CORRODED. CORROSION FWD SERVICE DOOR ENTRY FLOOR PANEL WITH CORROSION ON AFT I/B CORNER. REMOVED AND REPLACED FWD SERVICE DOOR ENTRY FLOOR PLANE IAW ASRP BD500-A-J51-40-0
- [SDR DALA2026010200036](https://openairdocs.org/sdr/DALA2026010200036), Jan 1, 2026: VALVE. FAULTED. AFTER ENGINE START, TRIM AIR WAS VERY HOT IN CKPT AND AFT DUCTS. 188+F IN CKPT, 184+F AFT. CYCLED TRIM AIR SWITCH AND FUNCTIONED NORMALLY. AT CRUISE, FA REPORTE
- [SDR DALA2025121209101](https://openairdocs.org/sdr/DALA2025121209101), Dec 8, 2025: LONGERON. CRACKED. CRACK IN WTB FAIRING LONGERON P/N 53-1111-501 AT LBL 40.0. CRACK SPREAD BETWEEN TWO NUT PLATES ON OUTBOARD SIDE OF LONGERON FORWARD OF FRAME AT FS 973. CRACK ME
- [SDR DALA2025121209100](https://openairdocs.org/sdr/DALA2025121209100), Dec 8, 2025: LONGERON. DAMAGED. FOUND LONGERON DAMAGED. REMOVED LONGERON PER A220 DWG C02382100 REV A. INSTALLED LONGERON PER A220 DWG C02382100 REV A. ONE FASTENER STILL REQUIRED. (HR 259148)
- [SDR DALA2025121009037](https://openairdocs.org/sdr/DALA2025121009037), Dec 4, 2025: SEAL. FAILED. DIV TO LAX DUE TO A "L PACK LEAK". FOUND FAULT CODE 3621F0024. FOUND LEAK ON LT UROSEAL UNDER BLUE INSULATION OVER FORWARD END OF SEAL. R/R LT DUCT UROSEAL, ITE
- [SDR DALA2025111208279](https://openairdocs.org/sdr/DALA2025111208279), Nov 11, 2025: ENGINE. MAKING METAL. LEFT ENGINE IFSD INTO SLC, DECLARED EMERGENCY. LEFT ENGINE OIL TEMP BEGAN TO RISE AND OIL PRESSURE STARTED TO DROP. CREW THEN RECEIVED AN OIL DEBRIS OVER LIMIT 
- [SDR DALA2025090206508](https://openairdocs.org/sdr/DALA2025090206508), Aug 26, 2025: EGT INDICATION. ILLUMINATED. RIGHT ENGINE AUTO SHUTDOWN ON DESCENT WITH EGT EXCEEDANCE. RT ENGINE REPLACED. (LP# 7823306)
- [SDR DALA2025061804588](https://openairdocs.org/sdr/DALA2025061804588), Jun 14, 2025: CIRCUIT BREAKER. TRIPPED. AFTER C/B CDC5-7-6 TRIPPED, FA REPORTED BURNING PLASTIC SMELL FUMES IN AFT GALLEY. FUMES DISSIPATED AFTER AFT GALLEY HEATER/ FAN WAS TURNED OFF BY FA. C/W AMDS 
- [SDR DALA2025061704573](https://openairdocs.org/sdr/DALA2025061704573), Jun 11, 2025: HEATER. ODOR. MUSTY SMELL REPORTED IN THE AFT GALLEY BY FA'S AFTER TURNING GALLEY HEATER ON. ODOR DISSIPATED ABOUT 15-20 MINUTES AFTER TURNING HEATER BACK OFF. C/W NO GO ODI.
- [SDR DALA2025060304235](https://openairdocs.org/sdr/DALA2025060304235), Jun 2, 2025: SEAT TRACK. CORRODED. AIRCRAFT 8136, CORROSION ON SEAT TRACK LBL 23 AFT OF FRAME 72. CORRECTIVE ACTION: CUTAWAY DAMAGE SEAT TRACK LBL 23 TO CUT LOCATION PER ER/A#623168-14TR REV O. A
- [SDR DALA2025060304234](https://openairdocs.org/sdr/DALA2025060304234), Jun 2, 2025: SEAT TRACK. CORRODED. AIRCRAFT 8136, CORROSION ON SEAT TRACK RBL 23 AFT OF FRAME 72. CORRECTIVE ACTION: CUT & REMOVED DAMAGED SEAT TRACK RBL 23.0 AT LOCATION A PER ER/A 623169-14TR R
- [SDR DALA2025060104196](https://openairdocs.org/sdr/DALA2025060104196), Jun 1, 2025: SEAT TRACK. CORRODED. AIRCRAFT 8136, CORROSION ON SEAT TRACK LBL 43.5 AFT OF FRAME 72. CORRECTIVE ACTION: CUT AND REMOVED DAMAGED SEAT TRACK LBL 43.5 AT LOCATION B PER ER/A 623167-14
- [SDR DALA2025020300800](https://openairdocs.org/sdr/DALA2025020300800), Jan 27, 2025: BATTERY PACK. INOPERATIVE. L2 DOOR EMERGENCY EXIT SIGN INOP. R/R EPSU BATTERY PACK PER A220 AMP 33-51. OPS CHECK PASSED. A/C OK FOR RETURN TO SERVICE. (LP# 6384381)
- [SDR DALA2024010800263](https://openairdocs.org/sdr/DALA2024010800263), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024010800262](https://openairdocs.org/sdr/DALA2024010800262), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 6 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024010800261](https://openairdocs.org/sdr/DALA2024010800261), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024010800260](https://openairdocs.org/sdr/DALA2024010800260), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 5 LWR FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024010800259](https://openairdocs.org/sdr/DALA2024010800259), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR5 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800258](https://openairdocs.org/sdr/DALA2024010800258), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024010800257](https://openairdocs.org/sdr/DALA2024010800257), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024010800256](https://openairdocs.org/sdr/DALA2024010800256), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 3 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024010800255](https://openairdocs.org/sdr/DALA2024010800255), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 2 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024010800254](https://openairdocs.org/sdr/DALA2024010800254), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 1 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024010800253](https://openairdocs.org/sdr/DALA2024010800253), Jan 4, 2024: NOT REPORTED. NOT REPORTED. R/H SLAT TRACK NBR 1 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024010800252](https://openairdocs.org/sdr/DALA2024010800252), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 9 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024010800251](https://openairdocs.org/sdr/DALA2024010800251), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 8 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024010800250](https://openairdocs.org/sdr/DALA2024010800250), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 6 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800249](https://openairdocs.org/sdr/DALA2024010800249), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 4 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800248](https://openairdocs.org/sdr/DALA2024010800248), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 3 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800247](https://openairdocs.org/sdr/DALA2024010800247), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 3 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024010800246](https://openairdocs.org/sdr/DALA2024010800246), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 2 LWR FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800245](https://openairdocs.org/sdr/DALA2024010800245), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 2 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024010800244](https://openairdocs.org/sdr/DALA2024010800244), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 2 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024010800243](https://openairdocs.org/sdr/DALA2024010800243), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024010800242](https://openairdocs.org/sdr/DALA2024010800242), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 1 LOWER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024010800241](https://openairdocs.org/sdr/DALA2024010800241), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 1 LOWER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024010800240](https://openairdocs.org/sdr/DALA2024010800240), Jan 4, 2024: NOT REPORTED. NOT REPORTED. L/H SLAT TRACK NBR 1 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2023081506641](https://openairdocs.org/sdr/DALA2023081506641), Aug 10, 2023: UNKNOWN. UNKNOWN. SHIP 8136 -DIV- DIVERTED TO SFO DUE TO LEFT ENGINE OPERATION DEGRADED MESSAGE WITH LEFT ENGINE FAULT. CORRECTIVE ACTION: REPLACED EEC, PERFORMED GROUND TEST AND
- [SDR DALA2023073106173](https://openairdocs.org/sdr/DALA2023073106173), Jul 29, 2023: UNKNOWN. UNKNOWN. WASTE BOX CORRODED AT LOWER FWD CUT OUT AREA. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0085:5360-2017/001 00102 COMPLIED WITH ER/A 610625-14 PRI REV 0, ER/

All 55: https://openairdocs.org/aircraft/N136DQ/reports.md

## STCs that may be installed (OpenAirDocs) (15)

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 Ltd Ptnrsp BD-500-1A10)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST02570LA](https://openairdocs.org/stc/ST02570LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [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 ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [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
- [STC ST00149IB](https://openairdocs.org/stc/ST00149IB) (historical): Installation of a Cabin air exhaust muffler, to reduce this noise to a more comfortable level by installing a valve cap and sound damping system. DOA21 LIMITED

## Related

- Other Airbus Canada Ltd Ptnrsp BD-500-1A10 aircraft: https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10/aircraft.md
- The Pratt & Whitney PW1519G engine: https://openairdocs.org/engine/pratt-whitney-pw1519g.md

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