# N341UA: Verge X7

- Status: Valid registration
- Airframe: [Verge X7](https://openairdocs.org/model/verge-x7) (registry code 06102I0)
- Serial number: P8DR7FPJ7T
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: November 7, 2024
- Expires: November 30, 2031
- Mode S code: A3C2C8
- Registered owner: [Cape May Aerial Advertising LLC](https://openairdocs.org/faa-owner/CAPE%20MAY%20AERIAL%20ADVERTISING%20LLC)
- Location: [Rio Grande, NJ](https://openairdocs.org/faa-place/NJ/Rio%20Grande)
- Owner type: LLC
- Owner's area on the map: 39.0171° N, 74.8881° W: Placed by OpenAirDocs at the center of ZIP code 08242, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=341UA
- Page: https://openairdocs.org/aircraft/N341UA

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 (Verge X7)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N341UA.

## FAA accident and incident reports

None matched to N341UA.

## 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 N341UA not matched to an aircraft (55, newest 50)

They name N341UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2008UALA02589](https://openairdocs.org/sdr/2008UALA02589), May 2, 2008: CONTROL PANEL. NO TEST. AFT PIT A DET LIGHT DOES NOT ILLUMINATE WITH CARGO SYS FIRE TEST OR LIGHTS TEST. REPLACED FIRE TEST CONTROL PANEL, CHECKS NORMAL. AC OK FOR SERVICE.
- [SDR 2008UALA02588](https://openairdocs.org/sdr/2008UALA02588), May 2, 2008: CONTROL PANEL. NO TEST. FWD PIT A DETECTOR LIGHT DOES NOT ILLUMINATE WITH CARGO FIRE SYS TEST OR WITH LIGHTS TEST. REPLACED TEST PANEL SYSTEMS CHECK GOOD.AC OK FOR SERVICE.
- [SDR 2008UALA02418](https://openairdocs.org/sdr/2008UALA02418), Apr 25, 2008: WARNING LIGHT. ILLUMINATED. ABORTED TAKEOFF AT 100 KTS DUE TO A FUEL FILTER BYPASS LIGHT ON NR 2 ENGINE.
- [SDR 2008UALA00997](https://openairdocs.org/sdr/2008UALA00997), Feb 22, 2008: BRACKET. LOOSE. DOOR 1R BRACKET THAT HOLDS GIRT BAR ON DOOR LOOSE. GIRT BAR COMES OUT TOO EASILY. ADJUSTED BRACKET.
- [SDR 2008UALA00030](https://openairdocs.org/sdr/2008UALA00030), Jan 2, 2008: DUMP VALVE. OBSTRUCTED. FLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW. FOUND FOREIGN OBJECT IN DUMP VALVE ALLOWING FLUID TO BYPASS VALVE. REMOVED OBJECT.
- [SDR 2008UALA0030](https://openairdocs.org/sdr/2008UALA0030), Jan 2, 2008: LAVATORY. UNKNOWN. FLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW.
- [SDR 2007UALA04404](https://openairdocs.org/sdr/2007UALA04404), Oct 25, 2007: FIRE BOTTLE. LOW PRESSURE. FWD ENGINE FIRE BOTTLE PRESSURE AT LIMIT. REPLACED BOTTLE OF FWD ENG SYS. 
- [SDR 2007UALA04380](https://openairdocs.org/sdr/2007UALA04380), Oct 23, 2007: SKIN. CRACKED. NR 6 SLAT (RT WING) CRACKED, LOCATED ON BOTTOM SURFACE. REMOVED DAMAGED AREA AND PERFORMED A REPAIR TO THE NR 6 SLAT (BOTTOM SURFACE). 
- [SDR 2007UALA04352](https://openairdocs.org/sdr/2007UALA04352), Oct 21, 2007: CLAMP. BROKEN. AIRCRAFT UNABLE TO MAINTAIN PRESSURE WITH SINGLE PACK OPERATION. FOUND APU BELLOWS CLAMP WAS FOUND LOOSE/BROKEN AND LEAKING PRESSURE. REPLACED CLAMP. PERFORMED 
- [SDR UALA2008111304215](https://openairdocs.org/sdr/UALA2008111304215), Oct 14, 2007: SKIN. DAMAGED. FUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LT MAIN GEAR, FROM UPPER REAR SPAR CORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES
- [SDR 2007UALA04215](https://openairdocs.org/sdr/2007UALA04215), Oct 14, 2007: SUPPORT FITTING. DAMAGED. FUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LEFT MAIN GEAR, FROM UPPER REAR SPAR CHORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LEFT SUPPORT FITTING HAS 6 ELONGA
- [SDR 2007UALA03014](https://openairdocs.org/sdr/2007UALA03014), Aug 4, 2007: LIGHT. CONTAMINATED. FLOOR PROXIMITY LIGHTING INOP FROM ROW 16 AFT TO AFT GALLEY. CLEANED & DRIED PROXIMITY LIGHTS. TESTED GOOD.
- [SDR 2007UALA02220](https://openairdocs.org/sdr/2007UALA02220), Jun 25, 2007: DETECTOR. FAULTY. CARGO FIRE DETECTION FAIL LIGHTS ALL 4 ARE ILLUMINATED. REPLACED 3 DETECTORS IN AFT PIT A SYSTEM AND 3 IN FWD PIT 2 EACH FOR B SYSTEM AND 1 FOR A SYSTEM.
- [SDR 2007UALA02199](https://openairdocs.org/sdr/2007UALA02199), Jun 22, 2007: LIGHT. OUT OF POSITION. CREW REPORTS EEL LIGHTS COMING OFF THE LAST THREE FEET. LIGHTS INOP FROM ROW 16 BACK. REPLACE EEL AFT STRIP OPS CKS OK.
- [SDR 2007UALA00790](https://openairdocs.org/sdr/2007UALA00790), Mar 15, 2007: BEARING. FAILED. RECIRC FAN ABOVE 7 IS GRINDING & HAS A BURNING ODOR. [SUP 05-29-07] RECIRCULATION FAN INOP. REPLACED RECIRCULATION FAN AND FILTER. UNIT HAD BAD BEARINGS. REPLAC
- [SDR 2007UALA00544](https://openairdocs.org/sdr/2007UALA00544), Feb 19, 2007: FILTER. DIRTY. CREW REPORTS MAIN CABIN FLIGHT ATTENDANTS AND PASSENGERS HAVING DIFFICULTY BREATHING AND SNEEZING. SUPPLEMENTAL DATA UPDATE CAUSE: HEPA FILTER. REPLACED RIGHT P
- [SDR 2006UALA01302](https://openairdocs.org/sdr/2006UALA01302), Jul 2, 2006: WIRE. INOPERATIVE. FOUND AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL TRACK CABLE.
- [SDR 2006UALA01301](https://openairdocs.org/sdr/2006UALA01301), Jul 2, 2006: WIRE. INOPERATIVE. FOUND EEL LIGHTS INOP AT ROWS 1-2 AND EEL STRIP IN FRONT OF FWD GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL TRACK CABLE.
- [SDR 2006UALA01259](https://openairdocs.org/sdr/2006UALA01259), Jun 26, 2006: FAN. ODOR. BURNING ELECTRICAL ODOR OR ACRID SMOKE ODOR DETECTED IN CABIN DURING APPROACH. EMERGENCY DECLARED. REPLACED THE INSTRUMENT COOLING SUPPLY FAN. REPLACED BEARINGS
- [SDR 2006UALA00747](https://openairdocs.org/sdr/2006UALA00747), Apr 19, 2006: DOOR FRAME. CORRODED. AFT CARGO DOOR CUTOUT FWD FRAME HAS CORROSION AT STA 794 BETWEEN STR 24R & 27R. INSTALLED EXTERNAL ANGLE DOUBLER REPAIR PER SRM 51-70-11 FIG 1.
- [SDR 2006UALA00716](https://openairdocs.org/sdr/2006UALA00716), Apr 17, 2006: STRINGER. CORRODED. AFT CARGO COMPARTMENT STATION 847 STRINGER 22R HAS CORROSION ON STRINGER. CUT OUT DAMAGED STR AND REPLACED WITH NEW SECTION PER SRM 53-00-03.
- [SDR 2006UALA00660](https://openairdocs.org/sdr/2006UALA00660), Apr 7, 2006: STRINGER CLIP. CRACKED. DURING BELLY SKIN REPLACEMENT 4 EA STRINGER CLIPS WERE FOUND CRACKED AT STA 787 STR 21R, STA 787 STR 22R, STA 867 STR 20R & STA 887 STR 20R. REPLACED STRINGER C
- [SDR 2006UALA00657](https://openairdocs.org/sdr/2006UALA00657), Apr 6, 2006: FRAME. CRACKED. ROUND OVERWING FRAME STA 616 RT SIDE IS CRACKED. INSTALLED STIFFENING ANGLE PER MM53-11-89.
- [SDR 2006UALA00645](https://openairdocs.org/sdr/2006UALA00645), Apr 5, 2006: FRAME. CRACKED. LT WW BS 695 FRAME AT STR 18A IS CRACKED IN THE RADIUS. REPLACED ANGLE PER SRM51-4 0-02.
- [SDR 2006UALA00630](https://openairdocs.org/sdr/2006UALA00630), Apr 2, 2006: WEB. CRACKED. STRINGER 7L ATTACH WEB AT STA 294.5 IS CRACKED AT INBD CORNER. REPLACED WEB PER SRM51-40- 02.
- [SDR 2006UALA00272](https://openairdocs.org/sdr/2006UALA00272), Feb 10, 2006: LIGHT. INOPERATIVE. LEFT OVERWING EMERGENCY SLIDE LIGHT INOP.
- [SDR 2005UALA00257](https://openairdocs.org/sdr/2005UALA00257), Mar 21, 2005: OVERHEAT LOOP. MALFUNCTIONED. RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORME
- [SDR 2005UALA00078](https://openairdocs.org/sdr/2005UALA00078), Jan 19, 2005: SKIN. DENTED. STA 341-359 HAS 3 DENTS ABOVE STR 21R. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.
- [SDR 2005UALA00077](https://openairdocs.org/sdr/2005UALA00077), Jan 19, 2005: SKIN. DENTED. LT FUSE SKIN IS DENTED AT STA 897 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR DOUBLER, TRI
- [SDR 2003UALA00745](https://openairdocs.org/sdr/2003UALA00745), Oct 5, 2003: SWITCH. FAILED. UNABLE TO SELECT NOSE DOWN ELEVATOR TRIM FROM BOTH YOKES. MAINTENANCE TECHNICIANS DUPLICATED THE PROBLEM ON GROUND. THE PROBLEM WAS TRACED TO A FAULTY FLAPS UP 
- [SDR 2003UALA00746](https://openairdocs.org/sdr/2003UALA00746), Oct 5, 2003: AUTOPILOT SYS. MALFUNCTIONED. WITH EITHER AUTO PILOTS ENGAGED AND ATTEMPTING TO ACCELERATE THE AIRCRAFT PITCHES UP. UPDATE DURING BITE CHECK OF THE AUTOPILOT BITE, FOUND FCC-B FAULTED, DADC2
- [SDR 2002UALA01376](https://openairdocs.org/sdr/2002UALA01376), Aug 29, 2002: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE. DEFECTIVE EEL LIGHT ASSEMBLY. REPLACED EEL STRIP. OPERATIONAL CHECK GOOD.
- [SDR 2002UALA00773](https://openairdocs.org/sdr/2002UALA00773), Apr 27, 2002: CIRCUIT BREAKER. FAILED. DIVERTED TO DEN DUE TO LOSS OF GENERATOR. THE AIRCRAFT WAS DIVERTED TO DENVER WITHOUT INCIDENT. AMT CREW ISOLATED CAUSE OF FAILURE DUE TO NR 2 TRANSFER BUS NORM
- [SDR 2002UALA00584](https://openairdocs.org/sdr/2002UALA00584), Mar 28, 2002: KEELBEAM. WORN. RIGHT HAND KEEL BEAM LOWER FLANGE UPPER SURFACE WEAR AREA AROUND FASTENER HOLE BODY STATION 700-727. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.
- [SDR 2002UALA00535](https://openairdocs.org/sdr/2002UALA00535), Mar 25, 2002: FRAME. CRACKED. STATION 178 LEFT HAND VERTICAL SIDE CHORD CRACKED AT STRINGER 17. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE.
- [SDR 2002UALA00533](https://openairdocs.org/sdr/2002UALA00533), Mar 25, 2002: FRAME. CORRODED. AFT PIT FRAME UPPER SURFACE BODY STATION 727E STRINGER 25R TO STRINGER 26R HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.
- [SDR 2002UALA00532](https://openairdocs.org/sdr/2002UALA00532), Mar 25, 2002: FRAME. MISDRILLED. AFT STABILIZER COMPARTMENT STATION 1108 STRINGER 1R FORWARD FACE OF FRAME HAS MISDRILLED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOU
- [SDR 2002UALA00524](https://openairdocs.org/sdr/2002UALA00524), Mar 22, 2002: STRINGER. CRACKED. FUSELAGE STRINGER 16 LH IS CRACKED AT BODY STATION 500C + 18 INCHES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDINSTALLED NEW STRINGER AND SPLICE.
- [SDR 2002UALA00520](https://openairdocs.org/sdr/2002UALA00520), Mar 21, 2002: PRESSURE PANEL. CRACKED. MAIN LANDING GEAR WHEEL WELL HORIZONTAL BULKHEAD WEB IS CRACKED BS 665, LBL 32 WL 202. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.
- [SDR 2002UALA00513](https://openairdocs.org/sdr/2002UALA00513), Mar 20, 2002: FRAME. CRACKED. CABIN, BODY STATION 887 FRAME, BETWEEN S8R & S9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE-CHANNEL 
- [SDR 2002UALA00507](https://openairdocs.org/sdr/2002UALA00507), Mar 18, 2002: STRINGER. CRACKED. CABIN STATION 360 STRINGER 14L TAIL CRACKED AT FASTENER JUST FORWARD OF FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW U-CHANNEL.
- [SDR 2002UALA00506](https://openairdocs.org/sdr/2002UALA00506), Mar 18, 2002: STRINGER. CRACKED. FORWARD CABIN STATION 294.5 STRINGER 17R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.
- [SDR 2002UALA00472](https://openairdocs.org/sdr/2002UALA00472), Mar 18, 2002: BULKHEAD. CRACKED. STATION 178 BULKHEAD WEB AFT SIDE CRACKED AT BL 0 WL 188. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.
- [SDR 2002UALA00471](https://openairdocs.org/sdr/2002UALA00471), Mar 17, 2002: BULKHEAD. CRACKED. STATION 178 BULKHEAD AFT SIDE WEB CRACKED RBL 5 WL 200. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.
- [SDR 2002UALA00470](https://openairdocs.org/sdr/2002UALA00470), Mar 17, 2002: FRAME. CRACKED. CABIN, BODY STATION 867 FRAME, BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE 
- [SDR 2002UALA00466](https://openairdocs.org/sdr/2002UALA00466), Mar 16, 2002: FRAME. CRACKED. BODY STATION 887 FUSELAGE FRAME IS CRACKED BETWEEN STRINGER 8L AND STRINGER 9L AT UPPER FASTENER FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER 
- [SDR 2002UALA00439](https://openairdocs.org/sdr/2002UALA00439), Mar 13, 2002: FRAME. CRACKED. CABIN BODY STATION 867 FRAME, BETWEEN 8L & 9L FRAME IS CRACKED AT FASTENER HOLE FROM VENT BRACKET, AFT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED CHANNEL REPAIR
- [SDR 2002UALA00399](https://openairdocs.org/sdr/2002UALA00399), Mar 10, 2002: FRAME. CRACKED. CABIN BODY STATION 827 FRAME BETWEEN STRINGER 8R AND STRINGER 9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET (AFT SIDE). MAJOR REPAIR ACCOMPLISHED. INST
- [SDR 2002UALA00398](https://openairdocs.org/sdr/2002UALA00398), Mar 10, 2002: FRAME. CRACKED. CABIN BODY STATION 847 BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR CHANNEL (ANGLE
- [SDR 2002UALA00397](https://openairdocs.org/sdr/2002UALA00397), Mar 9, 2002: FLOORBEAM. DAMAGED. AFT CABIN STATION 947 LBL 5 AND LBL 15 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM UPPER CAP WITH SINGLE FLANGE BLEND OUT REPAIR.

All 55: https://openairdocs.org/aircraft/N341UA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Verge X7 aircraft: https://openairdocs.org/model/verge-x7/aircraft.md

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