# N606AW: 1985 British Aerospace BAE 146 SERIES 200A, registration cancelled 2011-11-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 15, 2011
- Status when cancelled: First renewal notice
- Airframe: [British Aerospace BAE 146 SERIES 200A](https://openairdocs.org/model/british-aerospace-bae-146-series-200a) (registry code 1500266)
- Engine: [Lycoming ALF-502 SER. series](https://openairdocs.org/engine/lycoming-alf-502-ser-series) (registry code 41580)
- Data sheets: [TCDS A49EU](https://openairdocs.org/tcds/A49EU), [TCDS E6NE](https://openairdocs.org/tcds/E6NE) (OpenAirDocs)
- Serial number: E2033
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 9, 1985
- Certificate issued: July 11, 2001
- Last registry action: June 6, 2006
- Mode S code: A7DD9E
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N606AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=606AW
- Page: https://openairdocs.org/deregistered/N606AW-2011-11-15

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the British Aerospace BAE 146 SERIES 200A: https://openairdocs.org/model/british-aerospace-bae-146-series-200a.md

## Service difficulty reports (76, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR A6WA200460055](https://openairdocs.org/sdr/A6WA200460055), Nov 11, 2004: ACM. MALFUNCTIONED. NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR
- [SDR A6WA200460021](https://openairdocs.org/sdr/A6WA200460021), Jun 7, 2004: WARNING LIGHT. ILLUMINATED. AFTER GEAR UP SELECTED LEFT MLG RED INDICATION STAYED ILLUMINATED WITH GEAR INTRANSIT IN GEAR HANDLE ILLUMINATED GEAR SELECTED DOWN ALL NORMAL INDICATIONS. MAIN
- [SDR A6WA200360041](https://openairdocs.org/sdr/A6WA200360041), Sep 29, 2003: BRACKET. IMPROPER. LEFT ELEVATOR NR 2 HINGE 'A' FRAME TOP MOUNTING BOLT HAS AN IMPROPER SAFETY BRACKET, POORLY MANUFACTURED. REPLACED WITH NWE PART NR HC551B0098-000. (M)
- [SDR A6WA200360040](https://openairdocs.org/sdr/A6WA200360040), Sep 27, 2003: SKIN. DAMAGED. DAMAGED RIGHT OUTBOARD FLAP TAB BOTTOM SKIN BETWEEN RIBS 21-22. REPAIR IAW BAE FAX BARA/AVR/6530/03-DC. (M)
- [SDR A6WA200360043](https://openairdocs.org/sdr/A6WA200360043), Sep 24, 2003: STRINGER. CORRODED. FOUND STRINGER 33 RIGHT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101 AVMAX NON-ROUTINE 2289 FOR REPAIR. REPAIRED STRINGER IAW BAE SRM 53-0
- [SDR A6WA200360042](https://openairdocs.org/sdr/A6WA200360042), Sep 24, 2003: STRINGER. CORRODED. FOUND STRINGER 33 LEFT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101. REV AVMAX NON-ROUTINE 1204 FOR REPAIR. REPAIRED STRINGER IAW SRM 53-0
- [SDR A6WA200360038](https://openairdocs.org/sdr/A6WA200360038), Sep 10, 2003: STRUCTURE. DAMAGED. DAMAGED BUSHING BORES AT LT WING FLAP STRUCTURE AT TRACK 2. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060005. (M)
- [SDR A6WA200360037](https://openairdocs.org/sdr/A6WA200360037), Sep 8, 2003: DOOR FRAME. GOUGED. AFT CARGO DOOR OUTSIDE DOOR SURROUND GOUGED AT TOP AFT RADIUS MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060004. (M)
- [SDR A6WA200360034](https://openairdocs.org/sdr/A6WA200360034), Sep 6, 2003: SKIN. DAMAGED. DAMAGE EXTERNAL SKIN TO THE FORWARD CARGO DOOR MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060001. (M)
- [SDR A6WA200360035](https://openairdocs.org/sdr/A6WA200360035), Sep 6, 2003: STRUCTURE. CRACKED. FOUND CRACK AT RIVET LOCATION JUST AFT OF FRAME 29 STRINGER 13 LT. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060002. (M)
- [SDR A6WA200360036](https://openairdocs.org/sdr/A6WA200360036), Sep 6, 2003: FRAME. CORRODED. FOUND CORROSION ON FRAME 18 MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060003. (M)
- [SDR A6WA200360028](https://openairdocs.org/sdr/A6WA200360028), May 13, 2003: A/C PACK. SMOKE. PACKS EMITTING SMOKE INTO CABIN MAINTENANCE REMOVED AND REPLACED APU, PERFORMED PACK BURNOUT IAW AWAC SUPP 96.31. (M)
- [SDR A6WA200260034](https://openairdocs.org/sdr/A6WA200260034), Aug 20, 2002: CLAMP. OUT OF POSITION. DAMAGE TO THE MAIN LANDING GEAR BAY SKIN AT FRAME 29 LEFT SIDE AS CAUSED BY DOWN LOCK ACTUATOR CLAMP. MAINTENANCE DAMAGE BLENDED OUT IAW SRM 51-10-2. (M)
- [SDR A6WA200100008](https://openairdocs.org/sdr/A6WA200100008), Jan 30, 2001: WEB. DAMAGED. DAMAGE TO WEBS ABOVE AND BELOW FORWARD PASSENGER DOOR DAMPER CAN. MAINTENANCE REMOVED AND REPLACED DAMPER CAN LOWER AND UPPER WED ASSEMBLIES IAW BAE 146 SRM.
- [SDR A6WA200100007](https://openairdocs.org/sdr/A6WA200100007), Dec 21, 2000: LONGERON. CRACKED. LONGERON ON THE RT SIDE, AT THE TOP OF SERVICE DOOR AFT OF FRAME 19 AT THE FRAME HAS A CRACK. MAINTENANCE FOUND CLEAT OF DIAPHRAM CRACKED AND REPAIRED BY PATCHI
- [SDR A6WA200100006](https://openairdocs.org/sdr/A6WA200100006), Dec 15, 2000: FRAME. CRACKED. FOUND SEVERE CORROSION AND CRACKING ON THE AFT SIDE OF FRAME 18, ON THE I/B FRAME FLANGE 8 INCHES ABOVE FLOOR LEVEL AND 4 INCHES TO 8 INCHES BELOW FLOOR LEVEL. 
- [SDR A6WA9900128](https://openairdocs.org/sdr/A6WA9900128), Dec 1, 1999: BRAKE. FAILED. FLT 5545 - ORD-MLI - AFTER CHOCKS WERE PULLED. AIRCRAFT STARTED ROLLING FORWARD, BRAKING DID NOT STOP AIRCRAFT. AIRCRAFT HIT TERMINAL BLDG. AIRCRAFT REMOVED FRO
- [SDR 99ZZZM607](https://openairdocs.org/sdr/99ZZZM607), Nov 3, 1998: STRINGER. DENTED. HAT STRINGER ON AFT WALL OF APU BOX IS DENTED. REPLACED HAT STRINGER ON AFT APU FIREWALL IAW BAE FAXES BARA/AVR/1885/98 AND DWC/RJ0002-98. (M)
- [SDR 99ZZZM606](https://openairdocs.org/sdr/99ZZZM606), Nov 3, 1998: CABLES. CORRODED. LEFT AND RIGHT MAIN ELEVATOR CONTROL CABLES ARE CORRODED AT VERTICAL STABILIZER REAR SPAR PULLEYS. REMOVED AND REPLACED ALL FOUR MAIN ELEVATOR CONTROL CABLES FR
- [SDR 99ZZZM604](https://openairdocs.org/sdr/99ZZZM604), Nov 2, 1998: FLOORBEAM. CRACKED. FOUND CRACK IN FLOORBEAM AT FRAME NR 37 UNDER FLOOR PANEL 241DF IN CENTER ON FWD SIDE OF BEAM ABOUT 8 INCHES LONG AND 1 INCH FROM TOP OF BEAM. REMOVED CRACKED A
- [SDR 99ZZZM610](https://openairdocs.org/sdr/99ZZZM610), Oct 28, 1998: DIAPHRAGM. CRACKED. NLG ACTUATOR AT UPPER ATTACHMENT POINT DIAPHRAGM IS CRACKED IN THE WEB AND BOSS. REPORTED TO BAE RDO. REF W/C 7025 FOR CORRECTIVE ACTION, DIAPHRAGM REPLACEMENT.
- [SDR 99ZZZM609](https://openairdocs.org/sdr/99ZZZM609), Oct 27, 1998: DIAPHRAGM. CRACKED. NOSE SIDEWALL DIAPHRAGM REMOVED FOR CRACKED ACTUATOR ATTACH POINT. REPLACED NLG LEFT DIAPHRAGM PER BAE FAX REF NR JEN/RJO0505-98. GEN W/C FOR 60 CYC DV INSPECTI
- [SDR 99ZZZM608](https://openairdocs.org/sdr/99ZZZM608), Oct 16, 1998: CONTROL CABLE. CORRODED. ELEVATOR TRIM CABLE BETWEEN SCREWJACKS HAS SIGNS OF CORRISON AT CENTER PULLEY. ALSO, CENTER PULLEY BEARING WORN. REMOVED AND REPLACED CENTER PULLEY AND TRIM CAB
- [SDR 99ZZZM602](https://openairdocs.org/sdr/99ZZZM602), Sep 22, 1998: ENGINE. FAILED. NR 1 EGINE FAILE AND FIRE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM ANS AWAC GMM ENG CHANGE CHECKLIST VOLUME II SEC B CHAP 72, COMPLIED WI
- [SDR 98ZZZM928](https://openairdocs.org/sdr/98ZZZM928), Sep 22, 1998: ENGINE. FAILED. NR 1 ENGINE FAIL/SAFE AND FIRE INFLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM AND AWAC GMM ENGINE CHANGE CHECKLIST VOLUME II SEC B CHAP 72. COMP
- [SDR 98ZZZM927](https://openairdocs.org/sdr/98ZZZM927), Mar 28, 1998: POPPET VALVE. FAILED. NR 4 ENGINE READS 7 PERCENT BELOW N1 REF AT 904 DEGREES TGT, ABORTED TAKEOFF AT LESS THAN 60 KTS, RETURNED TO GATE AT DEN. REPLACED FCU POPPET VALVE ASY. ENGINE
- [SDR 98ZZZX1187](https://openairdocs.org/sdr/98ZZZX1187), Nov 11, 1997: GENERATOR. FAILED. DEN - FLT 587 - APU GENERATOR WENT OFF-LINE AND WOULD NOT RESET. FAILURE ACCOMPANIED BY ELECTRICAL SMELL WHEN APU AIR IS USED. INSPECTED APU, OIL LEVELS OK. INS
- [SDR 97ZZZX2990](https://openairdocs.org/sdr/97ZZZX2990), May 26, 1997: SPOILER LIGHT. ILLUMINATED. DEN - FLT 655 - AFTER TAKEOFF GEAR RETRACTED, SPOILER LOCK-UP LIGHT ILLUMINATED ALONG WITH MAIN SPOILER FAULT LIGHT. RETURNED FOR LANDING. UPON GEAR DOWN, MAIN 
- [SDR 97ZZZX2991](https://openairdocs.org/sdr/97ZZZX2991), May 21, 1997: SLIDE. DAMAGED. LEFT FORWARD EVACUATION SLIDE PACK-BOARD STRUCTURE WAS TORN AND SLIDE PARTIALLY PULLED FROM DOOR. REPLACED SLIDE.
- [SDR 97ZZZM395](https://openairdocs.org/sdr/97ZZZM395), Nov 21, 1996: RELAY. FAILED. UNABLE TO RAISE GEAR UNLESS OVERRIDE IS SELECTED. GEAR SELECTED DOWN NORMAL EXTENSION. REMOVED AND REPLACED RELAY GF4 SYSTEM CHECKS GOOD. (M)
- [SDR 97ZZZM396](https://openairdocs.org/sdr/97ZZZM396), Nov 10, 1996: ANGLE. CRACKED. MACHINED ANGLE ATTACHED TO SEAT RAIL 5 INCHES AFT OF FRAME 28 TO 6 INCHES AFT OF FRAME 29 LEFT OUTBOARD CRACKED. REPLACED ANGLE, REF FAX FOR HI-LOKS IN LIEU OF 
- [SDR 97ZZZM463](https://openairdocs.org/sdr/97ZZZM463), Nov 7, 1996: SUPPORT. CRACKED. CABIN FLOOR SUPPORT AT FRAME 20A CRACKED AT CENTER GUSSET PLATE. REPAIRED FRAME 20A FLOOR SUPPORT IAW AVRO FAX REF NR DJR/R J1269-96.
- [SDR 97ZZZM462](https://openairdocs.org/sdr/97ZZZM462), Nov 7, 1996: SKIN. CHAFED. REF FAX JM/RJ0927-6 DATED 8/14/96, LT FLAP TAB UPPER SKIN CHAFES AT RIBS 19 AND 21, FORWARD OF THE SPOILER RIB STRIP. REQUIRE REPAIR BY 34682 TCA. AWAC FAX LM18
- [SDR 97ZZZM464](https://openairdocs.org/sdr/97ZZZM464), Nov 6, 1996: SEAT RAIL. CORRODED. FORWARD VESTIBULE FRAME 18 RIGHT INBOARD SEAT RAIL CORRODED IN SEVERAL SPOTS, REF SRM 53-00-32 PAGE 203 AND 51-31-11 PAGE 22. REPAIRED FORWARD VESTIBLE RT INBOA
- [SDR 97ZZZM466](https://openairdocs.org/sdr/97ZZZM466), Nov 5, 1996: FLOORBEAM. CRACKED. CRACK INDICATIONS FOUND ON THREE PRESSURE FLOORBEAMS OVER FRAME NR 32 LEFT SIDE. VERIFIED WITH ET INSPECTION. REPAIRED 3 CRACKS AT FRAME 32 IAW AVRO REPAIR DRAW
- [SDR 97ZZZM465](https://openairdocs.org/sdr/97ZZZM465), Nov 5, 1996: FLOORBEAM. CRACKED. ELEVEN CRACK INDICATIONS ON FORWARD END OF PRESSURE FLOORBEAMS AT FRAME 29. CRACKED BEAMS ARE NR 2, 3, 4, 5, 6, 7, 9, 13, 15, 19 AND 20 NUMBERED L TO RT. REPAIR
- [SDR 97ZZZM454](https://openairdocs.org/sdr/97ZZZM454), Nov 1, 1996: RIB. CHAFED. RIB ABOVE LEFT NR 1 FLAP TRACK IS CHAFED WHERE IT CONTACTS ACCESS PANEL 285FT. BLENDED AND REPROTECTED THE CHAFE MARK ON THE SIDE OF RIB 2 TRAILING EDGE EXTENSI
- [SDR 97ZZZM453](https://openairdocs.org/sdr/97ZZZM453), Nov 1, 1996: FLAP TRACK. WORN. NR 1 FLAP TRACK LEFT SIDE HAS .020 INCH WEAR ON SIDE OF LOWER AND UPPER RAILS, FROM SLIPPER PLATES. BLENDED THE OUTBOARD SIDE OF THE LEFT NR 1 FLAP TRACK UPPER 
- [SDR 97ZZZM449](https://openairdocs.org/sdr/97ZZZM449), Oct 30, 1996: BOLTS. TOO LONG. FUSELAGE BOLT LOOSE AT RIGHT WING FORWARD SPAR. CHECK TORQUE ON THREE OTHER IN THAT SAME ROW. REPLACED 2 BOLTS FOUND TO BE TOO LONG. CHECK TORQUE ON REMAINING 3
- [SDR 97ZZZM452](https://openairdocs.org/sdr/97ZZZM452), Oct 29, 1996: ANGLES. BROKEN. AFT CARGO BAY AT FRAME NR 35, RT BELLY TIE DOWN AREA, SURROUND PLATE BENT AND ANGLES TO FRAME BROKEN. ALSO, MISSING RIVETS IN FRAME. STRAIGHTEN PLATE AND REPLAC
- [SDR 97ZZZM386](https://openairdocs.org/sdr/97ZZZM386), Oct 29, 1996: CABLES. CORRODED. PERFORMED AILERON INTERCONNECT CABLE CHECK. FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED IAW AMM GENERATED W/C FOR FUNC
- [SDR 97ZZZM385](https://openairdocs.org/sdr/97ZZZM385), Oct 29, 1996: CABLES. CORRODED. LEFT AND RIGHT AILERON INTERCONNECT CABLES COVER SLEEVES ARE WORN IN TWO AT CABLE GUIDES. REMOVED AND REPLACED LEFT AND RIGHT AILERON INTERCONNECT CABLES IAW AM
- [SDR 97ZZZM384](https://openairdocs.org/sdr/97ZZZM384), Oct 29, 1996: FLAP TRACKS. WORN. LEFT WING NR 2 FLAPTRACK WEARMARKS LOWER RAIL OUTBOARD EDGE FRM SLIP P/PLATE. WEARMARKS 94) BOTH SIDES TOP OF LOWER RAIL FROM ROLLERS AND 1, UPPER RAIL OUTBOARD
- [SDR 97ZZZM461](https://openairdocs.org/sdr/97ZZZM461), Oct 23, 1996: RAIL. CORRODED. FORWARD VESTIBULE INBOARD AIRSTAIR RAIL NEEDS TO BE REPLACED DUE TO CORROSION. RAIL IS REMOVED. REPLACED FORWARD INBOARD AIRSTAIR RAIL.
- [SDR 97ZZZM459](https://openairdocs.org/sdr/97ZZZM459), Oct 23, 1996: BOLTS. FAILED. LEFT WING INBOARD LIFT SPOILER JACK BOLTS, FORWARD AND AFT, FAILED NDT. INSTALLED NEW FORWARD AND AFT JACK BOLTS ON LEFT INBOARD LIFT SPOILER.
- [SDR 97ZZZM458](https://openairdocs.org/sdr/97ZZZM458), Oct 23, 1996: BLKHD DOUBLER. CRACKED. IN HYD BAY AT FRAME 29 BULKHEAD, THE TWO MOST OUTBOARD STIFFENERS LEFT AND RIGHT WERE FOUND TO HAVE CRACKED DOUBLERS AT BOTTOM BOLT HOLE. THESE STIFFENERS ARE N
- [SDR 97ZZZM457](https://openairdocs.org/sdr/97ZZZM457), Oct 23, 1996: BLKHD STIFFENERS. CRACKED. PERFORMED ET AT FRAME 29 BULKHEAD TO C/W EO E95/003/653 ITEM NR 3. FOUND CRACKS AT STIFFENER STATION 36.62, 31.13, 25.94 LEFT AND 36.62, 31.13, 25.94 RT. REPAIR
- [SDR 97ZZZM456](https://openairdocs.org/sdr/97ZZZM456), Oct 23, 1996: SUPPORT. CORRODED. FRAME 20 LEFT SIDE FLOOR SUPPORT BEAM HAS CORROSION WHERE BOTH FORWARD AIRSTAIR RAILS ATTACH. NEEDS TO BE CLEANED AND MEASURED FOR DEPTH. REPAIR OR REPAINT AS N
- [SDR 97ZZZM377](https://openairdocs.org/sdr/97ZZZM377), Oct 22, 1996: HI-LOK. SHEARED. SIGHTING ATTACHMENT ON (BELLY) LONGERON FITTING OF FRAME NR 29 HAS HI-LOK SHEARED. REPLACED BROKEN HI-LOK IAW BAE 146MM (SAME PART AS ORIGINAL). (M)
- [SDR 97ZZZM378](https://openairdocs.org/sdr/97ZZZM378), Oct 21, 1996: RAIL. CORRODED. REAR AIRSTAIR, INBOARD RAIL CORRODED NEEDS TO BE REPLACED. REMOVED AND REPLACED AFT INBOARD AIRSTAIR RAIL. (M)

All 76: https://openairdocs.org/deregistered/N606AW-2011-11-15/reports.md

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI00IA037](https://openairdocs.org/ntsb/CHI00IA037), Dec 1, 1999: British Aerospace BAE 146-200A (N606AW), Chicago, IL, incident, minor damage. Probable cause: An undetermined failure in the hydraulic system, which resulted in the airplane's entire braking system becoming temporarily inoperative. A factor associated with the incident was the airport…
- [NTSB FTW97LA070](https://openairdocs.org/ntsb/FTW97LA070), Dec 21, 1996: British Aerospace BAE 146-200A (N606AW), Denver, CO, no damage. Probable cause: an inflight encounter with unreported and unanticipated clear air turbulence during landing descent.

## FAA accident and incident reports (7)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 19961220047279A](https://openairdocs.org/incident/19961220047279A), Dec 20, 1996: N606AW, Denver, CO, No damage. (-16) Two flight attendants injured due to in-flight turbulence.
- [Incident 19940802047679I](https://openairdocs.org/incident/19940802047679I), Aug 2, 1994: Bag BAE146200A (N606AW), Milwaukee, WI. Fire light NR2 engine on climbout. Used bottles. Returned. Engine fire caused by cracked fuel manifold.
- [Incident 19940204006869I](https://openairdocs.org/incident/19940204006869I), Feb 4, 1994: Bag BAE146200A (N606AW), Rifle, CO, Minor damage. Narrative: after landing at Rifle, Colorado, the aircraft ran off the west end of the runway. Two (2) pilot reports, approximately one (1) hour prior to…
- [Incident 19940106001329I](https://openairdocs.org/incident/19940106001329I), Jan 6, 1994: Bag BAE146200A (N606AW), Aspen, CO, Minor damage. Narrative: the flight was normal until touchdown. Shortly after the nose wheels were on the ground the aircraft began moving to the right of runway centerline.…
- [Incident 19911018056609I](https://openairdocs.org/incident/19911018056609I), Oct 18, 1991: Bag BAE146200A (N606AW), Fort Wayne, IN, Minor damage. NR2 engine fire warning. Fired bottle. Diverted and landed. Turbine failed,tailpipe separated from engine.
- [Incident 19900730040879I](https://openairdocs.org/incident/19900730040879I), Jul 30, 1990: Bac 146200A (N606AW), Huntsville, AL. Unable to get an up gear indication. Returned. Found a leak in the hydraulic system.
- [Incident 19881007059069I](https://openairdocs.org/incident/19881007059069I), Oct 7, 1988: Bac 146200A (N606AW), Fort Wayne, IN. Received bird strike to leading edge of left wing during takeoff. Continued flight. No damage to wing.

## Other aircraft with N606AW

- [Registered now](https://openairdocs.org/aircraft/N606AW): Textron 680A, S/N 680A0281, built 2021

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