AUGUSTA AVIATION INC
Also recorded as: AUGUSTA AVIATION INC, Augusta Aviation Inc
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
82 reports on file — showing most recent 50.
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT EXPOSED. RE-SECURED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
TUL - FOUND CORROSION ON LOWER CHORD OF FRONT SPAR BELOW ACTUATOR FOR THE NR 2 SLAT, WS 629. REMOVED CORROSION AND INSTALLED DOUBLER STRAP PER SRM 57-30-00. (M)
TUL - FOUND 2ND FASTENER HOLE ABOVE CREASE ANGLE STATION 760.95 ELONGATED ESO REQUIRED. REPAIRED HOLE AT STATION 760.95 PER ESO 11697, DATED 3-14-2001. (M)
TUL - FOUND NR 6 L/E FLAP GAP PANEL SPAR CAP CORRODED. INSTALLED DOUBLER PER BOEING REPAIR DOCUMENT 57-30-00-2, PATES 1-3. (M)
TUL - FOUND WING CENTER SECTION, ABOVE LEFT PRIMARY HEAT EXCHANGER LOWER WING SKIN HAS HEAVY CORROSION 2 INCHES AFT OF S-5C SKIN BUTT JOINT LBL 18. BLENDED OUT CORROSION AND REPAIRED PER RM 57-30-3 PAGE 28. (M)
TUL - FOUND LOWER HINGE ON FORWARD ENTRY DOOR BODY SKIN CRACKED. ROUTED OUT CRACK ON LOWER HINGE OF FORWARD ENTRY DOOR, INSTALLED DOUBLER PER S/B 727-53-198. (M)
TUL - FOUND DENT IN SKIN, STATION 410 BELOW STRINGER 24L, ADL NR 0029. INSTALLED DOUBLER STATION 410 BELOW STRINGER 24L PER SRM 53-30-3. (M)
TUL - FOUND DEEP GOUGE AND DENT IN SKIN STATION 715 BELOW STRINGER 20R. INSTALLED DOUBLER PER SRM 53-30-1. (M)
TUL - FOUND DENT AND GOUGE IN SKIN STATION 501 BELOW STRINGER 28R DEPTH OF GOUGE OUT OF LIMITS DYE CHECKED GOUGE. NO CRACKS FOUND. INSTALLED DOUBLER AT STATION 501 BELOW STRINGER 28R PER SRM 53-30-3. (M)
TUL - FOUND STRINGER DAMAGED, FS 463, 12 INCHES BY 2 INCHES. REPAIRED STRINGER 27 LEFT STATION PER SRM 53-10-03. (M)
TUL - FOUND STRINGER CUT AND DAMAGED, FS 457, 12 INCHES BY 1 INCH. REMOVED AND REPLACED STRINGER PER SRM 51-10-1. (M)
TUL - FOUND BELL FRAME CUT INTO, STATION 460, 12 INCHES BY 1 INCH. REMOVED AND REPLACED BELL FRAME PER SRM 51-10-01. (M)
TUL - FOUND STRINGER 2L CUT INTO AT STATION 466. REPAIRED STRINGER 26L AT STATION 466 PER SRM 53-10-3. (M)
TUL - FOUND STATION 720E STRINGER 286 FRAME CRACKED. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER PER SRM 51-40-3. (M)
TUL - FOUND FRAME DAMAGED 1 INCH BY 3 INCHES, RIGHT SIDE OF E/E DOOR OPENING STATION 443, STRINGER 27 RT. DAMAGE CAUSED BY GROUND EQUIPMENT. REMOVED AND REPLACED DAMAGED FRAME PER SRM 51-10-1. (M)
TUL - FOUND STRINGER 25 LEFT CUT INTO STATION 471. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. SPLICED IN NEW SECTION OF STRINGER 25 LEFT AT STATION 471 PER SRM 53-10-3. (M)
TUL - FOUND FRAME CUT IN AFT AND OF E/E DOOR OPENING STATION 450 STATION 27 LEFT TO 27 RIGHT. REMOVED AND REPLACED FRAME PER SRM 51-10-1. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. (M)
TUL - FOUND CHANNEL DAMAGED STRINGER 28 LEFT TO BELLFRAME STATION 460. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. REMOVED AND REPLACED CHANNEL PER SRM 51-10-4. (M)
TUL - FOUND VERTICAL ANGLE DAMAGED ON WEB LEFT SIDE OF E/E DOOR OPENING STATION 460 BETWEEN STRINGER 27/28 LEFT. AIRCRAFT DAMAGED BY GROUND EQUIPMENT. REMOVED AND REPLACED VERTICAL ANGLE PER SRM 51-10-1. (M)
DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 14D THOUGHT 17D INOPERATIVE. REPAIRED WIRE AND RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MAIN ENTRY DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
TUL - PREVIOUSLY REWORKED AREA OF STRINGER 29L WORN BEYOND MM LIMITS. CUT OUT DAMAGED AND INSTALLED DOUBLER PER ESO 11697 DATED 1-14-00. (M)
TUL - FOUND CORROSION ON VERTICAL STIFFENER.. INSTALLED SERVICEABLE STIFFENER PER ESO 11697 DATED 01-11-00. (M)
TUL - FOUND STRINGER 27L CORRODED AT STATION 72A PLUS 12 INCH. CUTOUT CORROSION AT STATION 720A STRINGER 27L. INSTALLED STRINGER DOUBLER PER SRM 53-10-3. (M)
TUL - EMERGENCY LIGHT ASSY IN AFT ENTRY OVERHEAD LIGHT WILL NOT COME ON WHEN AFT ATTENDANTS LIGHT SWITCH IS TURNED ON. INSTALLED SERVICEABLE LIGHT LIGHT ASSY. (M)
TUL - FOUND SKIN EXFOLIATED AND CRACKED APPROX 3 INCHES LONG STATION 720 PLUS 14 TO STATION 720 PLUS 18 AT STRINGER 27L. REMOVED CORROSION BY CUTTING OUT EXFOLIATED SECTION OF SKIN. ALODINED AND PRIMED CUT OUT. INSTALLED SKIN REPAIR PER SRM 53-30-3 FIG 3. (M)
TUL - FOUND CORROSION ON FLOORBEAM STATION 344 LBL 40 TO RBL 60, TOP FLANGE. INSTALLED NEW T-ANGLE SECTION AND SPLICE PER SRM 53-10-8 FIG 9. (M)
TUL - FOUND CORROSION ON FLOORBEAM STATION 380 BL 0 TO RBL 65. REPAIRED PER SRM 53-10-08 FIG 9A AND 9B AT STATION 380 RBL 27. REPAIRED PER SRM 53-10-08 FIG 9A AND 9B AT STATION 380 RBL 39 TO RBL 71. (M)
TUL - FOUND RIGHT N/R TRUNNION AFT UPPER SUPPORT BEAM IN CUTOUT. TOP FLANGE CORRODED INBOARD AND OUTBOARD END. REMOVED STIFFENER MILL SHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED, PRIMED AND INSTALLED WITH HI-LOCKS AT ORIGINAL FASTENERS LOCATIONS SRM 51-10-1. (M)
TUL - FOUND RIGHT N/G TRUNNION FORWARD UPPER SUPPORT BEAM IN CUTOUT CORRODED AT INBOARD END TOP AND BOTTOM FLANGES. REMOVED STIFFENER , SHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED PRIMED AND INSTALLED WITH HI-LOCKS AT ORIGINAL FASTENER HOLES SRM 51-10-1. (M)
TUL - FOUND RIGHT N/G TRUNNION FORWARD UPPER SUPPORT BEAM CORRODED FORWARD SIDE OF CUTOUT FORWARD STIFFENER. REMOVED STIFFENER, MILLSHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED PRIMED AND INSTALLED WITH HI-LOCK AT ORIGINAL FASTENER HOLES SRM 51-10-1. (M)
TUL - FOUND LEFT GEAR FORWARD TRUNNION SUPPORT FITTING HAS PITTING INSIDE 4 EACH BUSHING BORES. REMOVED PITTING BY OVERSIZING BUSHING BORES AND INSTALLING NEW BUSHINGS. REPAIRED PER ESO 11697 DATED 11-24-98. (M)
TUL - FOUND BELLFRAME 720E SPOTTED WITH CORROSION FROM STRINGER 4L TO 8L. REMOVED DAMAGED AREA CUT TO SIZE FILLERS AND DOUBLERS DRILLED, ALODINED, PRIMED, SEALED AND INSTALLED FASTENERS PER SRM 53-10-4. (M)
TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 680 FROM STRINGER 24R TO STRINGER 25R. REMOVED DAMAGE, INSTALLED 14 INCH DOUBLER PER AARD 53-10-07-3 PAGE 1 OF 7075T6 .063 INCH THICK WITH 29 MS2040D .1875 INCH RIVETS, 4 MS2040D .25 INCH RIVETS. (M)
TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 660 FROM STRINGER 28L TO STRINGER 24L. REMOVED DAMAGE AREA, FROM 23L-24L, STATION 660. INSTALLED .063 DOUBLER 18 INCH LONG, 7075T6 COVERED TWO DAMAGE AREAS 1 INCH BY 1.5 INCH AND 1 INCH BY 2 INCH. USED 45 EACH MS20470D RIVETS AND 4 EACH MS 20470 D8 RIVETS. (M)
TUL - FOUND BELLFRAME DENTED IN SEVERAL PLACES, STATION 500 FROM STRINGER 22L TO 25L. REMOVED DAMAGED INSTALLED 19 INCH DOUBLER OF 7075T6 .063 INCH WITH 44 EACH .1875 D RIVETS, 2 EACH .25 INCH D RIVETS ALL UNIVERSAL HEADS PER SRM 51-40-3 FIG 1. (M)
TUL - FOUND BELLFRAME DENTED ONTOP FLANGE STATION 700 FROM STRINGER 22R TO STRINGER 24R. REMOVED DAMAGED INSTALELD 17.5 INCH DOUBLER OF 7075T6 .063 INCH WITH 37 MS20470 D .1875 FASTENERS PER SRM 51-40-3 FIG 1. (M)
TUL - FOUND BELLFRAME DENTED SEVERAL PLACES ON TOP FLANGE STATION 520, FROM STRINGER 22L TO 25L. REMOVED DAMAGE INSTALLED 28 INCHES DOUBLER OF 7075T6 .063 INCH WITH 71 EACH .1875 INCH D RIVETS, 4 EACH .25 INCH RIVETS ALL UNIVERSAL HEADS AND TWO FLUSH .1875 RIVETS, PER SRM 51-40-3 FIG 1. (M)
TUL - FOUND BELL FRAME BENT INTO FORWARD RADIUS STATION 1130 AND STRINGER 26R TOP LEG. REPAIRED DAMAGE AREA WITH DOUBLER PER 53-10-4. (M)
TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 660 BETWEEN STRINGER 23R AND 25R. REMOVED AND REPLACED BELLFRAME SPLICE DOUBLER AT STRINGER 25R PART REPLACEMENT. CUTOUT DAMAGE AREAS (TWO PLACES) AND INSTALLED REPAIR DOUBLER AT STRINGER 23R TO STRINGER 24R PER SRM 51-40-3 SSI REPAIR. (M)
TUL - FOUND BELLFRAME BENT INTO RADIUS FORWARD STATION 1110 AND STRINGER 26R TOP LEG. MADE OUTSIDE DOUBLER, REPAIR PER 51-40-3 SRM INSTALLED WET, ALODINED AND PRIMED. (M)
TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 620 FROM STRINGER 23L TO STRINGER 25L. DENTS AT STRINGER 25L AND 23L WITHIN LIMITS PER AARD 53-10-07-3 PAGE 1, CUTOUT DAMAGE AT STRINGER 24L AND INSTALLED REPAIR DOUBLER PER 51-40-3. (M)
TUL - FASTENER HOLE DAMAGED AT STATION 1070 STRINGER 28L. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1 PAGE 5. (M)
TUL - FOUND STRINGER 27R AT BS 990, LOWER FLANGE CORRODED FROM APPROX BS 985 TO BS 993. BLENDED CORROSION OUT, DAMAGED AREA WAS BEYOND LIMITS. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER AND DOUBLER PER ESO 11697 DATED 12-1-98 AND SRM 51-40-4. (M)
TUL - FOUND SHEAR TIE CORRODED AFT SIDE STATION 1148, BETWEEN STRINGER 30R AND 29R. REMOVED CORROSION PER SRM 51-10-6 ALODINED AND PRIMED. (M)
TUL - FOUND BELLFRAME BEN AND DEFORMED AT BS 990 BETWEEN STRINGER 27L AND 26L. CUTOUT DAMAGED AREA, INSTALLED OUTSIDE DOUBLER SRM 53-10-4. BELLFRAME WAS ALODINED AND PRIMED AND INSTALLED WET WITH SEALANT USED H6426 HI-LOCKS. (M)
TUL - FOUND STRINGER 2R GOUGED AT END FASTENER TO END FITTING UNDER HAT SECTION STATION 740 STRINGER 2R. CUT OUT DAMAGED FLANGE AND INSTALLED EXTENDED LENGTH END FITTING PER ESO 11697, DATED 12/7/98. (M)
TUL - FOUND STRINGER 15L AFT OF WING ICE LIGHT, CRACKED AT FORWARD FASTENER STATION 720C. REMOVED DAMAGED SECTION OF STRINGER 15L. INSTALLED SPLICE REPAIR PER SRM 53-10-3. (M)
TUL - FOUND CORROSION UNDER SEALER AROUND LIGHT PAN STATION 720 B - 720C STRINGER 15L. REMOVED CORROSION, REPAIRED SKIN AT WING ICE LIGHT CUT OUT PER SRM 53-30-3. (M)
TUL - FOUND STRINGER 15L CRACKED AT FORWARD FASTENER STATION 720B. CUT OUT DAMAGED SECTION STRINGER 15L. INSTALLED SPLICE REPAIR PER SRM 53-10-3. (M)
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N329GS | BEECH C90A | 1992 | Valid Registration | Matched by certificate designator |
| N377P | BEECH C90 | 1984 | Valid Registration | Matched by certificate designator |
| N80931 | CESSNA 172M | 1976 | Valid Registration | Operator named in NTSB report |
| N891AA | BEECH C90A | 1989 | Valid Registration | Matched by certificate designator |