# N336US: Hood Tech Corp Mechanical HTMC-40

- Status: Valid registration
- Airframe: [Hood Tech Corp Mechanical HTMC-40](https://openairdocs.org/model/hood-tech-corp-mechanical-htmc-40) (registry code 06101WV)
- Serial number: HTMC-0034
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: December 2, 2024
- Expires: December 31, 2031
- Mode S code: A3ADEC
- Registered owner: [Hood Tech Corp Mechanical Inc](https://openairdocs.org/faa-owner/HOOD%20TECH%20CORP%20MECHANICAL%20INC)
- Location: [Hood River, OR](https://openairdocs.org/faa-place/OR/Hood%20River)
- Owner type: Corporation
- Owner's area on the map: 45.6068° N, 121.6023° W: Placed by OpenAirDocs at the center of ZIP code 97031, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=336US
- Page: https://openairdocs.org/aircraft/N336US

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): 0 in force

### Matched by airframe (Hood Tech Corp Mechanical HTMC-40)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N336US.

## FAA accident and incident reports

None matched to N336US.

## Reports on N336US not matched to an aircraft (2)

They name N336US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19981218043329I](https://openairdocs.org/incident/19981218043329I), Dec 18, 1998: Boeing 737301 (N336US), New York, NY. (-5)On 12/19/98, at 1928 EDT a us air Boeing 737-301, s/n 23233, reported a burning odor in the cabin during climbout, and master caution warning (air…
- [Incident 19910519021139I](https://openairdocs.org/incident/19910519021139I), May 19, 1991: Boeing 737301 (N336US), Kansas City, MO. Navigation problems on approach. Landed safely. Logbook entry stated both FMC failed in flight.

## 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 N336US not matched to an aircraft (39)

They name N336US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR USAASB02021](https://openairdocs.org/sdr/USAASB02021), Jan 25, 2002: A/C PACK. FAILED. CLT - FLT 2434 - FLIGHT DEPARTED DCA WITH THE LEFT PACK ON MEL 21-1A. EN ROUTE TO CLT, AT FL240, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN BEGAN CLIMBING
- [SDR USAA011360](https://openairdocs.org/sdr/USAA011360), Oct 29, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.625 INCH, STATION 740 1.5 INCH BELOW STRINGER 23R. CUT OUT DAMAGE, INSTALLED FILLER AT STRINGER, INSTALLED DOUBLER PER SRM 53-00-01 F
- [SDR USAA011335](https://openairdocs.org/sdr/USAA011335), Oct 29, 2001: SKIN. CRACKED. PIT - ON WALKAROUND FOUND SKIN CRACKED 1.625 INCH, STATION 740 .5 INCH BELOW STRINGER 23R. CUT OUT DAMAGE, INSTALLED FILLER AT STRINGER, INSTALLED DOUBLER PER B
- [SDR USAASB01290](https://openairdocs.org/sdr/USAASB01290), Oct 9, 2001: INDICATOR. SHORTED. CLT - FLT 997 - EN ROUTE FROM PHL TO MSY, ALL THREE FUEL QUANTITY INDICATORS WENT BLANK. CREW FOUND FUEL QUANTITY CIRCUIT BREAKER TRIPPED BUT ATTEMPTS TO RESET 
- [SDR USAASB01259](https://openairdocs.org/sdr/USAASB01259), Sep 19, 2001: CHARGER. INOPERATIVE. GSO - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS, IN THE AFT CABIN, THAT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) A
- [SDR USAASB00324](https://openairdocs.org/sdr/USAASB00324), Nov 22, 2000: CONTROL HANDLE. LACK OF LUBE. PHL - FLT 1091 - ON APPROACH INTO PHL, FROM BOS, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS WHEN GEAR HANDLE WAS SELECTED DOWN. CREW ACCOMPLISHED GO-AR
- [SDR USAASB00313](https://openairdocs.org/sdr/USAASB00313), Nov 13, 2000: VALVE. LEAKING. CLT - FLT 9228 - ON CLIMB-OUT FROM CLT, BETWEEN 13,000 - 14,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES FOR THIS AND THEN HAD
- [SDR USAASB00224](https://openairdocs.org/sdr/USAASB00224), Aug 19, 2000: SENSOR. FAILED. CLT - FLT 1448 - LANDING GEAR WOULD NOT COME UP AFTER TAKEOFF FROM CLT. CREW PULLED AIR GROUND RELAY LIGHTS CIRCUIT BREAKER PER QUICK REFERENCE HANDBOOK PROCEDU
- [SDR USAASB00162](https://openairdocs.org/sdr/USAASB00162), Jun 10, 2000: FEEL UNIT. FAILED. CLT - FLT 1050 - AFTER T/O FROM CLT, AT APPROX 1,000 FT, THE ELEVATOR FEEL DIFFERENTIAL LIGHT ILLUMINATED AND THE NR 1 AUTOPILOT WOULD NOT ENGAGE, THE NR 1 ATC 
- [SDR USAASB99309](https://openairdocs.org/sdr/USAASB99309), Dec 31, 1999: SELECTOR. LACK OF LUBE. PIT - FLT705 - ON APPROACH INTO PIT, AS LANDING GEAR WAS SELECTED DOWN, ALL THREE GEAR SHOWED SIMULTANEOUS RED AND GREEN INDICATIONS. CREW BROKE OFF APPROACH AN
- [SDR USAASB99289](https://openairdocs.org/sdr/USAASB99289), Dec 6, 1999: HANDLE. MALFUNCTIONED. PIT - FLT 705 - DURING LOWERING OF LANDING GEAR, INBOUND TO PIT, CREW RECEIVED ALL 6 GEAR INDICATION LIGHTS (3 RED AND 3 GREEN). CREW RECYCLED GEAR AND INDICATI
- [SDR USAASB99259](https://openairdocs.org/sdr/USAASB99259), Oct 26, 1999: WINDSHIELD. CRACKED. CLT - FLT 1217 - EN ROUTE FROM PIT TO DFW, AT FL350, CREW HEARD A LOUD POPPING NOISE. CAPTAIN NOTICED THE FIRST OFFICERS NR 1 WINDSHIELD HAD MULTIPLE CRACKS AND
- [SDR USAA990466](https://openairdocs.org/sdr/USAA990466), May 22, 1999: STRINGER. CRACKED. CLT - DURING CX CHECK, FOUND STRINGER 5 LT CRACKED 1 INCH AT STATION 1142. STOP DRILLED, USED .1875 HI-LOCK FOR REAMED HOLES FOR INSTALLED ANGLE PER SRM 51-10-0
- [SDR USAA990459](https://openairdocs.org/sdr/USAA990459), May 22, 1999: STRINGER. CRACKED. CLT - DURING Q-6 CHECK, FOUND 1 INCH CRACK IN RADIUS OF STRINGER AT STRINGER 5 LEFT AT STATION 1142. INSTALLED REPAIR ANGLE PER EA 64489. (M)
- [SDR USAA990434](https://openairdocs.org/sdr/USAA990434), May 12, 1999: FLOORBEAM. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 520 LBL 46 FLOORBEAM. FABRICATED REPAIRED PER EA 64448 AND S/B 737-53-1120. (M)
- [SDR USAA990421](https://openairdocs.org/sdr/USAA990421), May 12, 1999: ANGLE. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT LOWER END OF INBOARD CHORD ANGLE OF FRAME RBL 65 AT TOP OF WING CENTER SECTION FRAME. INSTALL
- [SDR USAA990420](https://openairdocs.org/sdr/USAA990420), May 12, 1999: SKIN. CORROSION. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AT BS 727 BL 0 SKIN. FABRICATED REPAIR PER SRM 53-00-01. (M)
- [SDR USAA990365](https://openairdocs.org/sdr/USAA990365), May 12, 1999: CLIP. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25O INCH CRACK AT BS 380 STRINGER 2L TIE CLIP. REPAIRED PER SRM 51-10-01. (M)
- [SDR USAA990359](https://openairdocs.org/sdr/USAA990359), May 12, 1999: ANGLE. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BL 0 AT BS 380 PLUS 3 AND BS 400 MINUS INTERCOSTAL WEB ANGLE. REMOVED AND REPLACED ANGLE PER S
- [SDR USAA990358](https://openairdocs.org/sdr/USAA990358), May 12, 1999: CLIP. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FASTENER TIE CLIP STRINGER 10R AND FRAME STATION 663.75. INSTALLED NEW TIE CLIP PER SRM 53-00
- [SDR USAA990357](https://openairdocs.org/sdr/USAA990357), May 12, 1999: CLIP. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK TIE CLIP STATION 663.75 STRINGER 10L FRAME. INSTALLED NEW TIE CLIP PER SRM 53-00-07. (M)
- [SDR USAA990356](https://openairdocs.org/sdr/USAA990356), May 12, 1999: STRINGER. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 685 STRINGER 7L. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAA990355](https://openairdocs.org/sdr/USAA990355), May 12, 1999: STRINGER. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 705 STRINGER 3L. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAA990354](https://openairdocs.org/sdr/USAA990354), May 12, 1999: STRINGER. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 685 STRINGER 6L. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAASB99065](https://openairdocs.org/sdr/USAASB99065), Mar 6, 1999: SWITCH. MALFUNCTIONED. BWI - FLT 218, ON TAKEOFF, CAPT HEAD A LOUD NOISE AND WAS UNABLE TO PRESSURIZE THE AIRCRAFT. AT ABOUT 10,000 FT, CREW ELECTED TO RETURN TO FIELD AT BWI WHERE TH
- [SDR USAASB99049](https://openairdocs.org/sdr/USAASB99049), Feb 22, 1999: POWER SUPPLY. FAILED. SYR - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M
- [SDR USAASB99007](https://openairdocs.org/sdr/USAASB99007), Dec 31, 1998: BATTERY PACK. DISCHARGED. IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE RIGHT FORWARD SIDE OF THE FUSELAGE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERA
- [SDR USAASB98332](https://openairdocs.org/sdr/USAASB98332), Dec 18, 1998: ACM. INOPERATIVE. LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE WAS NOTICED IN THE AIRCRAFT. FLIGHT RETURN
- [SDR 99ZZZM83](https://openairdocs.org/sdr/99ZZZM83), Dec 18, 1998: COALESCER. DIRTY. LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE WAS NOTICED IN THE AIRCRAFT. FLIGHT RETURN
- [SDR 99ZZZM82](https://openairdocs.org/sdr/99ZZZM82), Dec 18, 1998: PACK VALVE. FAILED. LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE WAS NOTICED IN THE AIRCRAFT. FLIGHT RETURN
- [SDR USAA980583](https://openairdocs.org/sdr/USAA980583), Nov 10, 1998: SKIN. CRACKED. CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 2 INCH LONG CRACK IN SKIN RIGHT SIDE AT BS 727D 1 INCH BELOW STRINGER 23R. INSTALLED DOUBLER PER TR 53-60-03. (M
- [SDR USAASB97283](https://openairdocs.org/sdr/USAASB97283), Oct 9, 1997: BATTERY PACK. DISCHARGED. IAH - EMERGENCY EXIT SIGN OVER LEFT MID-CABIN ESCAPE HATCH AND LIGHT OVER RIGHT WING WILL NOT ILLUMINATE ON EMERGENCY LIGHT TEST. MAINTENANCE REPLACED BATTERY P
- [SDR USAASB97087](https://openairdocs.org/sdr/USAASB97087), Mar 21, 1997: N1 SPEED SENSOR. FAILED. PIT - FL 1052 - DURING CLIMB-OUT FROM PIT, THE NR 2 ENGINE N1 FLUCTUATED3-5 PERCENT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTE
- [SDR USAA950574](https://openairdocs.org/sdr/USAA950574), May 30, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 15 INCH CORRODED AREA ON INTERCOSTAL AT BS 312 THROUGH BS 328. REPAIRED PER SRM 51-10-02. CORROSION T
- [SDR USAA950571](https://openairdocs.org/sdr/USAA950571), May 30, 1995: FLOORBEAM. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH TOTAL CORROSION, CORROSION AT SCREW HOLES ON FLOORBEAM AT BS 312 LBL 12 INCHES THROUGH RBL 2
- [SDR USAA950569](https://openairdocs.org/sdr/USAA950569), May 16, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH AREA OF CORROSION ON INTERCOSTALS BS 328 THROUGH BS 344 RBL 12 AND LBL 12. REPAIRED PER SRM 51-10-1. CORR
- [SDR USAA950572](https://openairdocs.org/sdr/USAA950572), May 15, 1995: FLOORBEAM. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AT STATION 328 RBL 48. REPAIRIED PER 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LE
- [SDR USAA950573](https://openairdocs.org/sdr/USAA950573), May 12, 1995: FLOORBEAM. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES OF CORROSION OF FLOORBEAM AT STATION 344 BL 0 TO LBL 12. REPAIRED PER TR 53-10-03. CORROSION TAS
- [SDR USAA950570](https://openairdocs.org/sdr/USAA950570), May 5, 1995: KEEL BEAM. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK, 5.25 INCH BY 2 INCH CORRODED AREA BS 540, RBL 6.5 (LOWER FLANGE OF KEEL BEAM). REPAIRED PER EA 

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Hood Tech Corp Mechanical HTMC-40 aircraft: https://openairdocs.org/model/hood-tech-corp-mechanical-htmc-40/aircraft.md

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