# N375TA: 2020 Cameron Balloons U S A-375 - Status: Valid registration - Airframe: [Cameron Balloons U S A-375](https://openairdocs.org/model/cameron-balloons-u-s-a-375) (registry code 1880198, 1 seats) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS B2GL](https://openairdocs.org/tcds/B2GL) (Cameron Balloons US) (OpenAirDocs) - Serial number: 6914 - Year built: 2020 - Type: Balloon - Engine type: None - Airworthiness: Standard, balloon - Airworthiness date: September 21, 2020 - Certificate issued: November 30, 2020 - Expires: November 30, 2027 - Mode S code: A44808 - Registered owner: [Arizona Balloons Inc](https://openairdocs.org/faa-owner/ARIZONA%20BALLOONS%20INC) - Location: [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix) - Owner type: Corporation - Owner's area on the map: 33.8225° N, 112.1304° W: Placed by OpenAirDocs at the center of ZIP code 85086, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=375TA - Page: https://openairdocs.org/aircraft/N375TA 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 (Cameron Balloons U S A-375) None in force. ### Matched by engine (NONE) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N375TA. ## FAA accident and incident reports None matched to N375TA. ## 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 N375TA not matched to an aircraft (47) They name N375TA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR W8PA971497](https://openairdocs.org/sdr/W8PA971497), Oct 15, 1997: LAMP. INOPERATIVE. DEN- R1 DOOR OUTSIDE EMERGENCY LIGHT IS INOP. REPLACED LAMP, OPS CHECK GOOD. - [SDR W8PA971125](https://openairdocs.org/sdr/W8PA971125), Jun 13, 1997: SEAL. TORN. AIRCRAFT WILL NOT HOLE PRESSURIZATION DESCENDED TO 17,000 FEET. REPLACED NR 2 CARGO DOOR SEAL. (M) - [SDR W8PA970179](https://openairdocs.org/sdr/W8PA970179), Apr 11, 1997: LAMP. FAILED. BULL NOSE EMERGENCY LIGHT AT ROW 23R IS INOP. REPLACED LAMP. (M) - [SDR W8PA970108](https://openairdocs.org/sdr/W8PA970108), Mar 12, 1997: COVER. MISSING. FLOOR TRACK LIGHT COVER MISSING AT ROW 6. INSTALLED FLOOR TRACK COVER. (M) - [SDR W8PA970052](https://openairdocs.org/sdr/W8PA970052), Jan 29, 1997: GALLEY MOUNTS. CORRODED. DURING C-CHECK, ALL FOUR OF THE G1 GALLEY MOUNTING FITTINGS ARE CORRODED, BS 273-288, RBL 13-42, WL 208. REMOVED CORROSION FROM THE GALLEY MOUNTS. ONE OF THE FO - [SDR W8PA970051](https://openairdocs.org/sdr/W8PA970051), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL AT BS 281-291, RBL 13, WL 208 IS CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CHANNEL, FABRICATED AND - [SDR W8PA970050](https://openairdocs.org/sdr/W8PA970050), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL AT BS 331-337, RBL 53, WL 208 IS CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED HAT CHANNEL, FABRICATED AND INS - [SDR W8PA970049](https://openairdocs.org/sdr/W8PA970049), Jan 29, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK, THE UPPER CHORD OF THE FLOOR BEAM IS CORRODED AROUND THE FASTENER HOLES AT BS 360, LBL 18.5 - RBL 60, WL 208. REMOVED CORROSION, FOUND TO BE OUT - [SDR W8PA970048](https://openairdocs.org/sdr/W8PA970048), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL IS CORRODED AT BS 336-345, RBL 10, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED HAT CHANNEL, FABRICATED - [SDR W8PA970047](https://openairdocs.org/sdr/W8PA970047), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL IS CORRODED AT BS 350, RBL 10-51, WL 208. FOUND CORROSION REMOVED, PART OUT OF LIMITS. REMOVED, FABRICATED NEW PART AND INSTALLE - [SDR W8PA970046](https://openairdocs.org/sdr/W8PA970046), Jan 29, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK, THE UPPER CHORD OF THE FLOOR BEAM IS CORRODED AROUND THE FASTENER HOLES AT BS 294, BL 0 - RBL 51, WL 208. REMOVED CORROSION, PART OUT OF LIMITS, - [SDR W8PA970045](https://openairdocs.org/sdr/W8PA970045), Jan 29, 1997: ATTACH FITTINGS. CORRODED. DURING C-CHECK, ALL FOUR ATTACH FITTINGS FOR THE G2 GALLEY ARE CORRODED, BS 336 - 347, RBL 10-53, WL 208. REPLACED FOUR ATTACH FITTINGS WITH NEW PARTS IAW SRM. - [SDR W8PA970044](https://openairdocs.org/sdr/W8PA970044), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL AT BS 289-294, RBL 42, WL 208 IS CORRODED. FABRICATED AND INSTALLED NEW PART IAW SRM. (M) - [SDR W8PA970043](https://openairdocs.org/sdr/W8PA970043), Jan 29, 1997: WEB. CRACKED. DURING C-CHECK, FOUND CRACK IN WEB, BS 294, RLB 14, WL 192. REMOVED AND FABRICATED NEW PART INSTALLED IAW SRM. (M) - [SDR W8PA970042](https://openairdocs.org/sdr/W8PA970042), Jan 29, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, THE HAT CHANNEL IS CORRODED AT BS 275-286, RBL 42, WL 208. REMOVED CORROSION, FOUND TO BE OUT LIMITS. FABRICATED AND INSTALLED PER SRM. (M) - [SDR W8PA970041](https://openairdocs.org/sdr/W8PA970041), Jan 29, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK, THE UPPER CHORD OF THE FLOOR BEAM IS CORRODED AROUND FASTENER HOLES AT BS 312 FROM LBL 8 - RBL 50, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF - [SDR W8PA970036](https://openairdocs.org/sdr/W8PA970036), Jan 27, 1997: STIFFENER. CORRODED. DURING C-CHECK, THE FLOOR SUPPORT AT BS 294-312, RBL 10, WL 208 IS CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED FLOOR SU - [SDR W8PA970035](https://openairdocs.org/sdr/W8PA970035), Jan 26, 1997: ANGLE. CORRODED. DURING C-CHECK, CORROSION ON R-1 DOORWAY THRESHOLD Z-ANGLE BS 298-347, RBL 60, WL 208. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACE - [SDR W8PA970034](https://openairdocs.org/sdr/W8PA970034), Jan 26, 1997: SEAT TRACK. CORRODED. DURING C-CHECK, THE LBL 22 SEAT TRACK IS CORRODED ON THE FLANGES BS 344-364, LBL 22, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND R - [SDR W8PA970033](https://openairdocs.org/sdr/W8PA970033), Jan 26, 1997: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION, THE LBL 42 SEAT TRACK IS CORRODED ON THE FLANGES BS 344-349 LBL 42, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOV - [SDR W8PA970027](https://openairdocs.org/sdr/W8PA970027), Jan 25, 1997: FRAME. CORRODED. DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 847, RBL 21, WL 161. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED WEB PER SRM. (M) - [SDR W8PA970025](https://openairdocs.org/sdr/W8PA970025), Jan 23, 1997: WEB. CRACKED. DURING C-CHECK, FOUND CRACK IN WEB ON FORWARD AIRSTAIR DOOR, BS 340, LBL 73, WL 180. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED IAW SRM. (M) - [SDR W8PA970040](https://openairdocs.org/sdr/W8PA970040), Jan 22, 1997: FLOOR TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO FLOOR TRACK, BS 847, RBL 14, WL 161. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW FLOOR T - [SDR W8PA970032](https://openairdocs.org/sdr/W8PA970032), Jan 22, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION ON HAT SECTION AND DOUBLER, INBOARD SIDE OF FWD LAV SERVICE PANEL, BS 280, RBL 50, WL 178. REMOVED CORROSION, FOUND TO BE OUT OF - [SDR W8PA970024](https://openairdocs.org/sdr/W8PA970024), Jan 21, 1997: FLOOR TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO FLOOR TRACK, BS 847, RBL 14, WL 161. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALL NEW FLOOR TRA - [SDR W8PA970026](https://openairdocs.org/sdr/W8PA970026), Jan 20, 1997: CARGO TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO TRACK AT BS 500C - BS 500D, RBL 18, WL 155. REMOVED DAMAGED SECTION, FABRICATED NEW PART AND INSTALL IAW SRM. (M) - [SDR W8PA970022](https://openairdocs.org/sdr/W8PA970022), Jan 20, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO FLOORBEAM, BS 825, RBL 8, WL 158. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED AREA, FABRICATE - [SDR W8PA970053](https://openairdocs.org/sdr/W8PA970053), Jan 19, 1997: FLOORSUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOORSUPPORT AT BS 312-328, LBL 11, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED FLOORS - [SDR W8PA970039](https://openairdocs.org/sdr/W8PA970039), Jan 19, 1997: ANGLE. CORRODED. DURING C-CHECK, THE ANGLE UNDER THE R1 DOOR WAY MOP SILL IS CORRODED, BS 312-328, RBL 57, WL 208. REMOVED AND INSTALLED NEW ANGLE PER SRM. (M) - [SDR W8PA970038](https://openairdocs.org/sdr/W8PA970038), Jan 19, 1997: WEB. CORRODED. DURING C-CHECK, FOUND WEB UNDER R1 DOOR MOP SILL TO BE CORRODED FROM BS 294.5 TO 328, RBL 61, WL 208. REMOVED, FABRICATED NEW WEB AND INSTALLED PER SRM. (M) - [SDR W8PA970031](https://openairdocs.org/sdr/W8PA970031), Jan 19, 1997: SUUPORT. CRACKED. DURING C-CHECK, FLOOR TO SIDE WALL SUPPORT WEB CRACKED AROUND NUT PLATE AT BS 847, RBL 18, WL 160. REMOVED DAMAGED PART FABRICATED AND INSTALLED IAW SRM. (M) - [SDR W8PA970030](https://openairdocs.org/sdr/W8PA970030), Jan 19, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, THE UPPER CHORD OF BS 328 FLOORBEAM IS CORODED AROUND FLOORBOARD FASTENER HOLES FROM BL 0 TO RBL 59, WL 208. REMOVED CORROSION, FOUND TO BE OUT - [SDR W8PA970029](https://openairdocs.org/sdr/W8PA970029), Jan 19, 1997: FLOOR SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT BS 328-344, LBL 11, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND INSTALLED NEW SUP - [SDR W8PA970028](https://openairdocs.org/sdr/W8PA970028), Jan 19, 1997: FLOOR SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 312-328, RBL 10, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED FLOOR - [SDR W8PA970023](https://openairdocs.org/sdr/W8PA970023), Jan 19, 1997: SKIN. CRACKED. DURING C-CHECK, FORWARD CARGO DOOR INNER SKIN HAS 1 INCH CRACK AT FORWARD CENTER LIGHTING HOLE. STOP DRILLED HOLE. FABRICATED DOUBLER AND INSTALL ALL WORK DONE - [SDR W8PA970021](https://openairdocs.org/sdr/W8PA970021), Jan 19, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO FLOORBEAM BS 860, RBL 13, WL 162. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED AREA, FABRICATE - [SDR W8PA970018](https://openairdocs.org/sdr/W8PA970018), Jan 19, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON CARGO FLOORBEAM BS 860, RBL 8 WL 162. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED AREA, FABRICATED - [SDR W8PA970037](https://openairdocs.org/sdr/W8PA970037), Jan 17, 1997: MOP SILL. CORRODED. DURING C-CHECK, THE R1 DOORWAY MOP SILL IS CORRODED, BS 286-372, RBL 61, WL 208. REMOVED, AND INSTALL NEW CHORD, PER SRM. (M) - [SDR W8PA970020](https://openairdocs.org/sdr/W8PA970020), Jan 17, 1997: STRAP. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOOR STRAP BS 860 RBL 20 TO LBL 20 WL 162. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. FABRICATED NEW STRAP PER SR - [SDR W8PA970019](https://openairdocs.org/sdr/W8PA970019), Jan 17, 1997: SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 947 TO 867 RBL 18. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED SU - [SDR W8PA970006](https://openairdocs.org/sdr/W8PA970006), Jan 14, 1997: BULB. BURNED OUT. AFTER SELECTING 'GEAR DOWN' ON APPROACH, RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN. SWAPPED BULBS, DETERMINED FAULTY LIGHT BULB. DID FLYBY. RELAMPED GEAR DO - [SDR W8PA970005](https://openairdocs.org/sdr/W8PA970005), Jan 13, 1997: SOCKET. LOOSE. FOUND EMERGENCY TRACK LIGHT WILL NOT ILLUMINATE, LAST ROW. RECONNECTED LIGHT SOCKET. (M) - [SDR W8PA960187](https://openairdocs.org/sdr/W8PA960187), Dec 12, 1996: BATTERY CHARGER. FAILED. EMERGENCY LIGHTS WILL NOT ILLUMINATE, ROWS 19 THROUGH 22. REPLACED BATTERY CHARGER. (M) - [SDR W8PA960147](https://openairdocs.org/sdr/W8PA960147), Oct 3, 1996: LENS. MISSING. RIGHT AFT EMERGENCY EXIT LIGHT LENS IS OFF. RE-INSTALLED LENS. (X) - [SDR W8PA960146](https://openairdocs.org/sdr/W8PA960146), Oct 3, 1996: BATTERY. DISCHARGED. FLOOR TRACK LIGHTING INOP FROM ROWS 14 THROUGH 20. REMOVED AND REPLACED BATTERY ASSY. (X) - [SDR W8PA960141](https://openairdocs.org/sdr/W8PA960141), Sep 26, 1996: BULB. FAILED. LEFT AFT BODY FAIRING EMERGENCY LIGHT INOP. REPLACED BULB. (M) - [SDR W8PA960056](https://openairdocs.org/sdr/W8PA960056), Jul 15, 1996: BULB. FAILED. FOUND EXTERNAL EMERGENCY EXIT LIGHT INOPERABLE FOR R-1 DOOR. RELAMPED LIGHT ASSEMBLY. (X) ## STCs that may be installed (OpenAirDocs) (1) 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 (Cameron Balloons U S A-375) - [STC SB04407AT](https://openairdocs.org/stc/SB04407AT): Installation of the DBI-III Omega. Balloonacy, Ltd. LLC ## Related - Other Cameron Balloons U S A-375 aircraft: https://openairdocs.org/model/cameron-balloons-u-s-a-375/aircraft.md - The NONE engine: https://openairdocs.org/engine/none.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.