# N969DL: 2024 Bell Textron Canada 505

- Status: Valid registration
- Airframe: [Bell Textron Canada 505](https://openairdocs.org/model/bell-textron-canada-505) (registry code 1182166, 5 seats)
- Engine: [Safran ARRIUS-2R](https://openairdocs.org/engine/safran-arrius-2r) (registry code 59992)
- Data sheets: [TCDS R00008RD](https://openairdocs.org/tcds/R00008RD) (Bell Textron Canada Limited), [TCDS E34NE](https://openairdocs.org/tcds/E34NE) (Safran Helicopter Engines S.A.) (OpenAirDocs)
- Serial number: 65580
- Year built: 2024
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: May 6, 2024
- Certificate issued: April 26, 2024
- Expires: April 30, 2031
- Mode S code: AD7DEB
- Registered owner: [Dj Aviation LLC](https://openairdocs.org/faa-owner/DJ%20AVIATION%20LLC)
- Location: [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville)
- Owner type: LLC
- Owner's area on the map: 35.8605° N, 84.1005° W: Placed by OpenAirDocs at the center of ZIP code 37922, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=969DL
- Page: https://openairdocs.org/aircraft/N969DL

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): 18 in force

### Matched by airframe (Bell Textron Canada 505)

- [AD 2026-18-10](https://openairdocs.org/ad/2026-18-10): Rotorcraft tail boom · Bell Textron Canada 505. Effective Oct 22, 2026
- [AD 2026-16-02](https://openairdocs.org/ad/2026-16-02): Tail rotor system · Bell Textron Canada 505. Effective Sep 10, 2026
- [AD 2026-15-06](https://openairdocs.org/ad/2026-15-06): Vertical stabilizer structure · Bell Textron Canada 505. Effective Sep 3, 2026
- [AD 2026-05-51](https://openairdocs.org/ad/2026-05-51): Equipment/furnishings · Bell Textron Canada 505. Effective Apr 16, 2026
- [AD 2025-22-03](https://openairdocs.org/ad/2025-22-03): Equipment/Furnishings · Bell Textron Canada 505. Effective Nov 20, 2025
- [AD 2025-18-10](https://openairdocs.org/ad/2025-18-10): Engine Fuel/Oil Cooler · Bell Textron Canada 505. Effective Sep 25, 2025
- [AD 2025-09-01](https://openairdocs.org/ad/2025-09-01): Auto Flight System · Bell Textron Canada 505. Effective May 13, 2025
- [AD 2024-15-10](https://openairdocs.org/ad/2024-15-10): Fuel Storage · Bell Textron Canada 505. Effective Oct 21, 2024
- [AD 2023-12-26](https://openairdocs.org/ad/2023-12-26): Engine fuel and control · Bell Textron Canada 505. Effective Jul 21, 2023
- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2022-24-08](https://openairdocs.org/ad/2022-24-08): Main Rotor Control · Bell Textron Canada 505. Effective Dec 6, 2022
- [AD 2022-04-06](https://openairdocs.org/ad/2022-04-06): Main Rotor Control · Bell Textron Canada 505. Effective Apr 4, 2022
- [AD 2021-26-01](https://openairdocs.org/ad/2021-26-01): Tail Rotor Control System · Bell Textron Canada 505 with STC SR09758DS. Effective Dec 28, 2021
- [AD 2021-16-12](https://openairdocs.org/ad/2021-16-12): Instrument Panel · Bell Textron Canada 505. Effective Oct 13, 2021
- [AD 2021-11-19](https://openairdocs.org/ad/2021-11-19): Fuselage Main, Structure · Bell Textron Canada 505. Effective Jul 16, 2021
- [AD 2021-05-52](https://openairdocs.org/ad/2021-05-52): Main Rotor Control · Bell Textron Canada 505
- [AD 2020-19-05](https://openairdocs.org/ad/2020-19-05): Main Rotor Mast/Swashplate · Bell Helicopter Textron Canada 505. Effective Oct 8, 2020

### Matched by engine (Safran ARRIUS-2R)

- [AD 2023-24-09](https://openairdocs.org/ad/2023-24-09): Engine Indicating System · Safran Helicopter Engines ARRIUS 2R. Effective Jan 17, 2024

### Historical (superseded or no longer in force)

- [AD 2025-06-51](https://openairdocs.org/ad/2025-06-51) (historical): Equipment/furnishings · Bell Textron Canada 505. Effective Apr 25, 2025
- [AD 2024-02-55](https://openairdocs.org/ad/2024-02-55) (historical): plates/skin · Bell Textron Canada 505. Effective Mar 14, 2024
- [AD 2021-24-04](https://openairdocs.org/ad/2021-24-04) (historical): Engine fuel and control · Bell Textron Canada 505. Effective Jan 13, 2022
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2021-06-06](https://openairdocs.org/ad/2021-06-06) (historical): Main Rotor Control · Bell Textron Canada 505. Effective Mar 31, 2021

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N969DL.

## FAA accident and incident reports

None matched to N969DL.

## Reports on N969DL not matched to an aircraft (2)

They name N969DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20040404008259I](https://openairdocs.org/incident/20040404008259I), Apr 4, 2004: Doug MD88 (N969DL), Norfolk, VA, Minor damage. (-23) At 1828E, delta airlines, flight 428, an MD88, experienced a sudden decrease in altitude and speed due to crosswinds. The aircraft landed hard on runway…
- [Incident 20010308005839I](https://openairdocs.org/incident/20010308005839I), Mar 8, 2001: Doug MD88 (N969DL), Pittsburgh, PA. (-23) On March 8, 2001, at 1330E, a MD-88, s/n 53172, registered as N969DL and operated as dala flight 1923, returned to "pt" after reporting a problem with…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N969DL not matched to an aircraft (210, newest 50)

They name N969DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DALA2020030201502](https://openairdocs.org/sdr/DALA2020030201502), Mar 2, 2020: BATTERY. DISCHARGED. EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS. REPLACED BATTERIES AT B5-104. CKS GOOD. REF MD88 33-53. (LP6639438)
- [SDR DALA2020021001025](https://openairdocs.org/sdr/DALA2020021001025), Feb 10, 2020: CHARGER. FAILED. CEILING EMERG LIGHTS INOP AT ROW 22-25. R/R EMERG LIGHT BATTERY CHARGER BATTERIES (3E) REF MD88 AMM 33- 53. OPS CKS OK. (LP6896559)
- [SDR DALA2020020600935](https://openairdocs.org/sdr/DALA2020020600935), Feb 6, 2020: TRANSCEIVER. FAILED. WX RADAR SCREEN BECAME FUZZY THEN SMOKE APPEARED TO BE COMING OUT OF THE RADAR UNIT WX RADAR INOP. REPL DISPLAY PER MD88 AMM 34-41. CKS NML. ACCORDING TO THE MC
- [SDR DALA2019110406366](https://openairdocs.org/sdr/DALA2019110406366), Nov 3, 2019: ENGINE. OVERTEMP. SHIP 969 - IFSD & ATB - DUE TO LEFT ENGINE HIGH OIL TEMPERATURE. FLT CREW REPORTED AT 2000 FT THAT OIL TEMP WAS AT 165DEG AND WHEN POWER WAS ADDED, OIL TEMP WEN
- [SDR DALA2019072604414](https://openairdocs.org/sdr/DALA2019072604414), Jul 26, 2019: BATTERY. DISCHARGED. EMER. LIGHTS OUT ON OVERHEAD @ ROWS 18,21,24,25. R/R BATTERIES AT B5-103 PER AMM 33-53 AND WM 33-51-12. OPS CK GOOD. (LP5926683)
- [SDR DALA2019072604413](https://openairdocs.org/sdr/DALA2019072604413), Jul 26, 2019: CONNECTOR. BROKEN. EMER. LIGHT @ SEAT 16ED INOP. FOUND PLASTIC SEAT CONNECTOR BROKEN OFF RETERMINATED AS REQUIRED. OPS CHECK GOOD OK FOR SVC. (LP5926682)
- [SDR DALA2018091305576](https://openairdocs.org/sdr/DALA2018091305576), Sep 12, 2018: COWLING. CORRODED. CORROSION ON LIP OF NOSE COWLING BTW 1 TO 2 HRS AT LT ENGINE. REPLACED NOSE COWLING.
- [SDR DALA2018091305577](https://openairdocs.org/sdr/DALA2018091305577), Sep 11, 2018: TAB. DELAMINATED. DELAMINATED RUDDER CONTROL TAB LT/RT SIDE (MID HINGE AREA). DELAMINATED RUDDER CONTROL TAB LT/RT SIDE (MID HINGE AREA) WAS REPAIRED PER ERA 092613-14MA REV "A" 
- [SDR DALA2018091205575](https://openairdocs.org/sdr/DALA2018091205575), Sep 11, 2018: DOOR FRAME. CRACKED. CRACK ON RH AFT OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA. CRACK ON RT AFT OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA WAS REPAIRED PER SRM 53-05 FIG 32.
- [SDR DALA2018091305574](https://openairdocs.org/sdr/DALA2018091305574), Sep 11, 2018: DOOR FRAME. CRACKED. CRACK ON RH FWD OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA. ON RT FWD OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA WAS REPAIRED PER SRM 53-05 FIG 32.
- [SDR DALA2018090905502](https://openairdocs.org/sdr/DALA2018090905502), Sep 8, 2018: TAB. CRACKED. HIDDEN CRACKS: CRACKS ALONG T/E ON LT AILERON CONTROL TAB, DURING PAINT REMOVAL (IN REF NRC S/N 00017). ON REFERENCE OF NRC SERIAL NR 00325: CRACKS ALONG T/E ON
- [SDR DALA2018090405397](https://openairdocs.org/sdr/DALA2018090405397), Sep 2, 2018: DOUBLER. WORN. WORN EXTERNAL DOUBLERS (2 E/AS) AT FWD CARGO DOOR. EXTERNAL DOUBLERS WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL AND SRM 51-30-2.
- [SDR DALA2018071204450](https://openairdocs.org/sdr/DALA2018071204450), Jul 12, 2018: BATTERY PACK. DISCHARGED. FOUND EMERGENCY EXIT LIGHT SIGN INOP DURING LIGHT CKS AT ROW 24 BOTH SIDES. R&R BATTERY PACK AT ROW 24 IAW MM 33-53. EXIT SIGNS LIGHT CKS NORM. OK FOR SVC.
- [SDR DALA2018042202699](https://openairdocs.org/sdr/DALA2018042202699), Apr 20, 2018: WIRE. BROKEN. SMALL AMOUNT OF SMOKE AND ODOR DETECTED FROM UNDER CAPTAIN'S DASHBOARD. REDUCED LIGHTS. SMOKE STOPPED. FOUND WIRE TERMINALS FOR BACK LIGHTNING FOR LANDING LIGHT
- [SDR DALA2018022101017](https://openairdocs.org/sdr/DALA2018022101017), Feb 19, 2018: SMOKE DETECTOR. FALSE ACTIVATION. CREW VERBAL, F/C LAV SMOKE ALARM SOUNDED ON TAXI IN. FLIGHT NUMBER WAS NOT SPECIFIED. R&R DETECTOR.
- [SDR DALA2018020500635](https://openairdocs.org/sdr/DALA2018020500635), Feb 3, 2018: BATTERY PACK. DEFECTIVE. DURING SVC FOUND 5 OVERHEAD EMERGENCY LIGHTS INOP IN FIRST CLASS. RELAMPED. NO HELP. R&R BATTERIES IN BATTERY PACK B5-100. NO HELP. R&R BATTERY PACK ASSY B5-100
- [SDR DALA2017120408411](https://openairdocs.org/sdr/DALA2017120408411), Dec 1, 2017: BATTERY PACK. FAILED. DURING SVC CK- FOUND TWO CABIN EMERGENCY BATTERY PACKS BAD. REMOVED & REPLACED BATTERY PACKS AT SEAT ROWS 25 & 29 PER MD88 AMM 33-53. (LP3309106)
- [SDR DALA2017102307714](https://openairdocs.org/sdr/DALA2017102307714), Oct 20, 2017: PIN. PULLED. L1 DOOR SLIDE PINS PULLED. R & R L1 DOOR SLIDE IAW AMDS 2561-4964.
- [SDR DALA2017100907435](https://openairdocs.org/sdr/DALA2017100907435), Oct 7, 2017: BATTERY PACK. INOPERATIVE. COCKPIT AND ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017062905084](https://openairdocs.org/sdr/DALA2017062905084), Jun 28, 2017: FIRE WARNING. FALSE ACTIVATION. RIGHT ENGINE FIRE LOOP B LIGHT ILLUMINATED WITH OAP FIRE DETECTOR LOOP MESSAGE. IAW QRH, PERFORMED LOOP TEST ON SYSTEM A, TESTED NORMAL. COULD NOT DUPLICATE FAU
- [SDR DALA2017053104389](https://openairdocs.org/sdr/DALA2017053104389), May 30, 2017: BATTERY. DISCHARGED. CEILING EMERGENCY LIGHTS OUT AT SEATS 16, 17, 18, 19, 20, 26, 27, 28, 29, AND 30. REPLACED BATTERIES AT POWER UNITS SN-22713 AND SN-27406. REFERENCE AMM 33-53-0
- [SDR DALA2017052404149](https://openairdocs.org/sdr/DALA2017052404149), May 24, 2017: WIRE. DAMAGED. SEVERAL SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPAIRED THE WIRING IAW AMM 20-50.
- [SDR DALA2016121209788](https://openairdocs.org/sdr/DALA2016121209788), Dec 11, 2016: BATTERY. DISCHARGED. EMER CEILING LIGHTS ROW 17-19 INOP. REPLACED BATTERIES FOR B5-102 EMER LIGHTS REF AMM 33-53. OPS CHECK GOOD.
- [SDR DALA2016110408259](https://openairdocs.org/sdr/DALA2016110408259), Nov 4, 2016: BATTERY PACK. INOPERATIVE. BACK HALF OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY PACKS AT B5-106 & B5-103. CHECKS GOOD. ACFT OK FOR SERVICE.
- [SDR DALA2016081906102](https://openairdocs.org/sdr/DALA2016081906102), Aug 19, 2016: FRAME. CRACKED. TAIL INTERIOR CANTED FRAME WEB AT BS 1485 HAS 1/2 INCH CRACK. INSTALLED REPAIR IAW SRM 51-70-5.
- [SDR DALA2016061704760](https://openairdocs.org/sdr/DALA2016061704760), Jun 16, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY OVERWING LIGHTS INOPERATIVE, R & R EMERGENCY POWER SUPPLY AND BATTERY IAW AMM 33-53. OPS CK NORMAL. AIRCRAFT OK FOR SERVICE. EMERGENCY POWER SUPPLY.
- [SDR DALA2016052704215](https://openairdocs.org/sdr/DALA2016052704215), May 27, 2016: SWITCH. INOPERATIVE. ALL EMERGENCY LIGHTS INOPERATIVE. R & R FWD ATTEND SWITCH S1-387. OPS CK GOOD, REF WDM 33-51-11.
- [SDR DALA2016041802996](https://openairdocs.org/sdr/DALA2016041802996), Apr 15, 2016: BATTERY PACK. INOPERATIVE. MSP MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 25 AND 31. THE BATTERY PACK WAS REPLACED AND GROUND WIRE L1844B16N WAS FOUND LOO
- [SDR DALA2016032102142](https://openairdocs.org/sdr/DALA2016032102142), Mar 18, 2016: CONNECTOR. DAMAGED. FWD LAV WATER HEATER CONNECTOR P1-385 HEAT DAMAGE. REPLACED P1-385 IAW SWPM CH20 AND R & R WATER HEATER AMM 38-11, OPS AND LEAK CK GOOD.
- [SDR DALA2016031802069](https://openairdocs.org/sdr/DALA2016031802069), Mar 18, 2016: HEATER. ODOR. AFTER TAKEOFF, A F/A REPORTED THAT THE CABIN FILLED WITH A WHITE COLORED HAZE WITH AN ELECTRICAL ODOR. THE QRH WAS FOLLOWED AND THE GALLEY AND SIDEWALL LIGHTS W
- [SDR DALA2016010500023](https://openairdocs.org/sdr/DALA2016010500023), Jan 5, 2016: BATTERY PACK. INOPERATIVE. FLL MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 1 THROUGH 10. AN EMERGENCY BATTERY PACK WAS REPLACED AND THE LIGHTS CHECKED OK.
- [SDR DALA2015110106629](https://openairdocs.org/sdr/DALA2015110106629), Nov 1, 2015: BATTERY PACK. INOPERATIVE. MAINTENANCE FOUND CABIN EMERGENCY LIGHT INOPERATIVE. THE OVERWING BATTERY PACK RELAY R2-271 AND BATTERY PACK B5-49 WAS REPLACED.
- [SDR DALA2015080304808](https://openairdocs.org/sdr/DALA2015080304808), Jul 31, 2015: AXLE. CORRODED. EVIDENCE OF CORROSION ON RT NLG AXLE SHAFT, REF CRD 3200-01207-0101. RT AXLE SHAFT IAW AMDS 6221-6192.
- [SDR DALA2015080304807](https://openairdocs.org/sdr/DALA2015080304807), Jul 31, 2015: AXLE. CORRODED. EVIDENCE OF CORROSION ON LT NLG AXLE SHAFT. R & R LT NLG AXLE SHAFT IAW AMDS 3221-6192.
- [SDR DALA2015050403069](https://openairdocs.org/sdr/DALA2015050403069), May 1, 2015: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THE CEILING MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 17-20. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES AND THE 
- [SDR DALA2015010700132](https://openairdocs.org/sdr/DALA2015010700132), Jan 7, 2015: LANYARD. MISINSTALLED. MAINTENANCE FOUND THE R1 DOOR SLIDE RELEASE LANYARD INSTALLED IMPROPERLY. THE LANYARD WAS REMOVED AND REINSTALLED.
- [SDR DALA2015010700131](https://openairdocs.org/sdr/DALA2015010700131), Jan 7, 2015: PIN. PULLED. MAINTENANCE FOUND L1 DOOR SLIDE PIN PULLED. SLIDE WAS REPLACED.
- [SDR DALA2015010700130](https://openairdocs.org/sdr/DALA2015010700130), Jan 7, 2015: CONNECTOR. DISCONNECTED. EMERGENCY LIGHTS INOPERATIVE AT 22D AND 28D. CONNECTED THE CONNECTOR AND REPLACED LIGHT ASSY AT 22D, OPS CHECKED GOOD AMM 33-53.
- [SDR DALA2014120406417](https://openairdocs.org/sdr/DALA2014120406417), Dec 1, 2014: WIRE. BROKEN. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE FOUND BROKEN TERMINALS AT THE AFT STAIRWAY 
- [SDR DALA2016110908558](https://openairdocs.org/sdr/DALA2016110908558), Jul 24, 2014: RETAINER. CRACKED. CORROSION AND A CRACK ON LOWER SECTION OF PRESSURE SEAL RETAINER OF RT FWD OVER WING EMERGENCY EXIT DOOR. THE SEAL RETAINER WAS REMOVED DRILLED AND INSTALLED IA
- [SDR DALA2014072504211](https://openairdocs.org/sdr/DALA2014072504211), Jul 24, 2014: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB REPAIR DOUBLER X=54 TO X=60 BETWEEN BS 930 - 936. NEW REPAIR INSTALLED IAW SRM 53-05 FIG 131A-1.
- [SDR DALA2014072504212](https://openairdocs.org/sdr/DALA2014072504212), Jul 24, 2014: BATTERY PACK. INOPERATIVE. DURING CHECK, MAINTENANCE FOUND MULTIPLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROW 27, 28 LT AND 30B. MAINTENANCE R & R THE BATTERY PACK LOCATED AT 29DE AND 
- [SDR DALA2016110908587](https://openairdocs.org/sdr/DALA2016110908587), Jul 9, 2014: WEB. CORRODED. CORROSION ON FWD WEB BS 363-370, LONGERONS 24 -28R AT FWD CARGO DOOR FRAME. CORRODED AREA WAS TRIMMED OUT, FILLER AND DOUBLER FABRICATED AND INSTALLED PER ER/A.
- [SDR DALA2016110908586](https://openairdocs.org/sdr/DALA2016110908586), Jul 9, 2014: RETAINER. CRACKED. CORROSION AND A CRACK WAS FOUND ON LOWER SECTION OF PRESSURE SEAL RETAINER OF FWD OVER WING EMERGENCY EXIT DOOR. REMOVED DAMAGED AREA, REWORKED, TREATED, PAINTE
- [SDR DALA2014071004023](https://openairdocs.org/sdr/DALA2014071004023), Jul 9, 2014: HEATER BLANKET. DAMAGED. DURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 23.6% ON RT WING HEATER BLANKET AREA REPAIRED IAW ER/A N./ 527365-14 REV ORIG.
- [SDR DALA2014071004022](https://openairdocs.org/sdr/DALA2014071004022), Jul 9, 2014: HEATER BLANKET. DEBONDED. NINE DEBONDED AREAS ON RT WING HEATER BLANKET WERE FOUND AT INBD AREA . DAMAGE WAS REPAIRED IAW ERA 527365-14 REV ORIG..
- [SDR DALA2014071004021](https://openairdocs.org/sdr/DALA2014071004021), Jul 9, 2014: HEATER BLANKET. DEBONDED. DBONDED AREAS ON LT WING HEATER BLANKET WERE FOUND AT INBD EDGE. REPAIRED IAW ERA 52736514 REV ORIG.
- [SDR DALA2014071004020](https://openairdocs.org/sdr/DALA2014071004020), Jul 9, 2014: HEATER BLANKET. DEBONDED. DURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 37 PERCENT ON LT WING HEATER BLANKET. AREA WAS REPAIRED IAW ERA 527365-14 REV ORIG.
- [SDR DALA2014071004019](https://openairdocs.org/sdr/DALA2014071004019), Jul 9, 2014: STRUCTURE. DELAMINATED. DELAMINATION ON LT MID BUTTE DOOR MID SECTION UPPER AND LOWER FACE AT LT WING. NEW BUTTE DOOR WAS ADJUSTED DRILLED INSTALLED IAW SRM 51-30-1,51-30-2.
- [SDR DALA2014071004018](https://openairdocs.org/sdr/DALA2014071004018), Jul 9, 2014: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PLATE 1365C COUNTERSINK AREA ON LEFT WING. CORROSION REMOVED, FOUND OUT OF LIMITS. REPLACED ACCESS PANEL.

All 210: https://openairdocs.org/aircraft/N969DL/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (32)

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 (Bell Textron Canada 505)

- [STC SR11256DS](https://openairdocs.org/stc/SR11256DS): Installation of 2nd GIA. Bell Textron Inc
- [STC SR04842NY](https://openairdocs.org/stc/SR04842NY): Installation of RMCI Inc. Expandable Rotorcraft Diagnostic System (XRDS). Sterling Helicopter
- [STC SR11896AC](https://openairdocs.org/stc/SR11896AC): Installation of EMS equipment sled and equipment mount provision. HELIFAB
- [STC SR11253DS](https://openairdocs.org/stc/SR11253DS): Installation of Auxiliary Fuel System. Bell Textron Inc
- [STC SR00147IB](https://openairdocs.org/stc/SR00147IB): Installation of the Heli-Utility-Basket. Dart Aerospace
- [STC SR02774SE](https://openairdocs.org/stc/SR02774SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR04567AT](https://openairdocs.org/stc/SR04567AT): Installation of Crew and Cabin Floor Protectors. Helifab East LLC
- [STC SR02804LA](https://openairdocs.org/stc/SR02804LA): Installation of Airfilm Utility Mount. Airfilm Camera Systems
- [STC SR04522NY](https://openairdocs.org/stc/SR04522NY): Installation of an Accessory Fitting. AeroBrigham LLC
- [STC SR04691NY](https://openairdocs.org/stc/SR04691NY): Installation of the Cabin Floor Protection Kit. Alpine Aerotech LP
- [STC SR01961WI](https://openairdocs.org/stc/SR01961WI): Installation of a Garmin GFC 600H Flight Control System. Garmin International Inc
- [STC SR11249DS](https://openairdocs.org/stc/SR11249DS): Installation of Flitestep. Bell Helicopter Textron Inc
- [STC SR11244DS](https://openairdocs.org/stc/SR11244DS): Installation of Expanded Instrument Panel. Bell Helicopter Textron Inc
- [STC SR11246DS](https://openairdocs.org/stc/SR11246DS): Installation of Accessories Package. Bell Helicopter Textron Inc
- [STC SR09758DS](https://openairdocs.org/stc/SR09758DS): Installation of an S-TEC HeliSAS Stability Augmentation System / Autopilot. S-TEC Corporation
- [STC SR11243DS](https://openairdocs.org/stc/SR11243DS): Installation of Expanded Avionics Shelf. Bell Helicopter Textron Inc
- [STC SR04387NY](https://openairdocs.org/stc/SR04387NY): Installation of the Skidtubes. Dart Aerospace Ltd
- [STC SR11242DS](https://openairdocs.org/stc/SR11242DS): Installation of Avionics Rain Shield. Bell Helicopter Textron Inc
- [STC SR09899AC](https://openairdocs.org/stc/SR09899AC): Installation of Night Vision Goggle (NVG) Compatible Lighting System. Aero Dynamix Inc
- [STC SR04355CH](https://openairdocs.org/stc/SR04355CH): Installation of Med-Pac 505 EMS-Lite RC505 Medical Unit. Med-Pac Inc
- [STC SR11239DS](https://openairdocs.org/stc/SR11239DS): Installation of High Skid Landing Gear. Bell Helicopter Textron Inc
- [STC SR11238DS](https://openairdocs.org/stc/SR11238DS): Installation of Nightscanner. Bell Helicopter Textron Inc
- [STC SR09618RC](https://openairdocs.org/stc/SR09618RC): Installation of Headliner. Bell Helicopter Textron Inc
- [STC SR11237DS](https://openairdocs.org/stc/SR11237DS): Installation of Tinted Windows. Bell Helicopter Textron Inc
- [STC SR04158NY](https://openairdocs.org/stc/SR04158NY): Upgrade for Bell 505 VIP interiors P/N 685J0000X001001. Mecaer Aviation Group S.p.A
- [STC SR04133NY](https://openairdocs.org/stc/SR04133NY): Installation of Emergency Float System. Dart Aerospace Ltd
- [STC SR04124NY](https://openairdocs.org/stc/SR04124NY): Installation of Bear Paw kits. Alpine Aerotech LP
- [STC SR04120NY](https://openairdocs.org/stc/SR04120NY): Installation of the Bearpaws. Dart Aerospace Ltd
- [STC SR09616RC](https://openairdocs.org/stc/SR09616RC): Installation of Floor Protectors. Bell Helicopter Textron Inc
- [STC SR09615RC](https://openairdocs.org/stc/SR09615RC): Installation of Cargo Mirror Kit. Bell Helicopter Textron Inc
- [STC SR09612RC](https://openairdocs.org/stc/SR09612RC): Installation of a Cowling Access Door Kit. Bell Helicopter Textron Inc
- [STC SR09613RC](https://openairdocs.org/stc/SR09613RC): Installation of an Automatic Door Opener Kit. Bell Helicopter Textron Inc

## Related

- Other Bell Textron Canada 505 aircraft: https://openairdocs.org/model/bell-textron-canada-505/aircraft.md
- The Safran ARRIUS-2R engine: https://openairdocs.org/engine/safran-arrius-2r.md

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