N217US
Registered owner: DAVIS AVIATION INC, MS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CARVER AERO, LLC (XRRA) | Operator | 2021-01-28 – 2021-01-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DEN - DURING DEMONSTRATION, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM MANUAL ACTIVATION PER MM 35-21-00A AND CHECKED OKAY. TC: 88,247. (X)
DEN - FLT 546 - FLIGHT CREW REPORTED CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CLOSED OUTFLOW VALVE USING MANUAL DC AT 32,500 FEET. CABIN CONTINUED TO CLIMB AT 1,000 FPM AND A RAPID DESCENT WAS MADE TO 14,000 FEET. OXYGEN MASKS WERE AUTOMATICALLY DEPLOYED. REPLACED LT FLOW CONTROL VALVE, RESTOWED OXYGEN MASKS, AND PERFORMED PRESSURIZATION TEST, WITH NO DISCREPANCIES NOTED. CYCLES: 4,630. (X)
DEN - FLT 857 - DURING SERVICE CHECK, EO 71-20-737-002 WAS ACCOMPLISHED WHICH FOUND THE NR 2 ENGINE OUTBOARD LUG BEARING LOOSE AND DISPLACED. AN ULTRA SOUND INSPECTION REVEALED THE FORWARD ENGINE MOUNT BOLT CRACKED. MAINTENANCE REPLACED NR 2 ENGINE MOUNT ASSEMBLY AND CHECKED OKAY. CYCLES: 4,444. (X)
PHX - DURING SERVICE CEHCK, MAINTENANCE REPORTED .5 INCH CRACK ON WEB OF LEFT NLG WHEEL WELL STATION 285. ONE RIVET BORKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG WHEEL WELL AT LEFT AFT ACCESS PANEL. MAINTENANCE REPLACED NLG WHEEL WELL CHORD STATION 235-294 AND STANCHION PLR SRM 51-30-02 AND EA 737-5310-0001. (M)
LEFT NLG W/W STATIN 285, .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL.
LEFT NLG W/W STATION 285 HAS .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. (M)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M186, REF WDM 33.51.01) FAILED TO ILLUMINATE BRIGHT DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CHECKED OK. (M)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED CONTROL CABIN ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M185, REF WDM 33.51.01) FAILED TO ILLUMINATE DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CHECKED OK. (M)
DEN - UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 ENGINE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE HYDRAULIC PUMP AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE AT NR 2 ENGINE PYLON AFT SPAR AND SYSTEM CHECKED OK. (M)
SAN - UPON DESCENT INTO SAN, FLIGHT CREW REPORTED SULFUR/ELECTRICAL ODOR FROM AIR VENTS AT ROW 5 AND 6 ON LEFT SIDE OF AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACARDED GASPER FAN PER MEL 21-24. UPON ARRIVAL IN DEN, GASPER FAN WAS REPLACED AND SYSTEM CHECKED OK. (M)
FLT 658 - DEN - AIR TURN BACK, UPON CLIMB-OUT FROM DEN, FLIGHT CREW REPORTED NR 1 ENGINE START VALVE 'OPEN' LIGHT ILLUMINATED. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE START VALVE SOLENOID AND CHECKED OK. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 907 PLUS 15, RBL 13, WL 169. MAINTENANCE REMOVED DAMAGED AREA (1.5 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 53-10-1 AND 53-10-3. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, RBL 4.7, WL 212-213. MAINTENANCE REMOVED CRACKED AREA (2 INCH BY 3.5 INCH), FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN FORWARD GALLEY DOOR AFT FRAME, 4 INCHES DOWN FROM TOP CORNER OUTBOARD RADIUS. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER DRAWING 69-69887-3-4-5 AND SB 737-52-1070. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED LEFT WING FIXED LEADING EDGE SKIN DOUBLER CRACKED AT NR 3 SLAT OUTBOARD AUXILLIARY TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED DOUBLER AND REPAIRED PER ER 98-0483 AND SRM 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACKS ON UPPER SKIN SURFACE AT RIGHT WING, BL 103.5, TWO INCHES FORWARD OF AFT SPAR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-57-1144. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SKIN AND DOUBLER AT BS 980-1012, STRINGER 27R. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0478. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BAY STRINGER 27R, RBL 5, BS 912-947. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-30-5, 53-10-1 AND 53-10-3. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, LBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, RBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0476 AND SRM 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, LBL 4.7, WL 192.5 TO 193.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-11. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26L, BS 888-892, LBL 13, WL 163. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2 AND 53-10-3. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 1006, LBL 4 THROUGH RBL 4, WL 178. MAINTENANCE REMOVED CORRODED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL LEFT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA, 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL RIGHT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M)
PAE - DURNIG C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON STRINGER 26R, BS 1006-1014. MAINTENANCE FABRICATED REPLACEMENT STRINGER AND REPAIR PARTS AND REPAIRED PER SRM 51-20-1, 53-10-1 AND 53-10-2. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON SHEAR TIE AT BS 727A, WL 149, RBL 13. MAINTENANCE FABRICATED REPLACEMENT SHEARTIE AND REPAIRED PER SRM 53-10-1, 51-30-2 AND 53-10-4. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, RBL 4.7, WL 190-191.5. MAINTENANCE REMOVED DAMAGED AREA (1 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, FIG 1, DETAIL IV AND SRM 51-30-2. (M)
PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AT BS 440, BL0, WL 148. MAINTENANCE REMOVED DAMAGED AREA (4.6 INCH BY 1.1 INCH). FABRICATED REPAIR DOUBLER AND REPAIRED PER SRM 51-30-2 AND 53-10-4. (M)
PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, LBL 6.7, WL 212-213. MAINTENANCE STOP DRILLED CRACK, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, PATE 2, DETAIL III AND PAGE 6, FIG 1. (M)
DEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED .625 INCH CRACK SIX INCHES FORWARD OF L-1 DOOR IN FUSELAGE SKIN AT STRINGER 7. MAINTENANCE REPAIRED CRACK PER SRM 53-30-3, PAGES 7 AND 8. (M)
DEN - FLT 43 - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD92-25-09), INSPECTION REPORTED BULGING OF SKIN (CORROSION) AT STATION 901, S23R AND S24R, AND STATION 895, STRINGER 25R. MAINTENANCE REPAIRED CORRODED AREAS PER SRM 53-30-1, PAGE 3 (FIG 1) AND PAGE 5. (M)
DEN - FLT 780 - FLIGHT CREW REPORTED NR 1 ENGINE WAS SHUT DOWN DUE TO LOW OIL QTY AND AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED O-RING ON FUEL CARBON SEAL IN STL. DURING FLT NR 217 STL TO DEN, NR 1 ENGINE OIL QTY DECREASED AND AIRCRAFT DIVERTED TO MCI AS PRECAUTIONARY MAINTENANCE. REPLACED NR 1 ENGINE N2 GEARBOX, PERFORMED A TEST FLT AND SYSTEM CHECKED OK. (M)
CLT - ONE INCH CRACK IN RIB AROUND RIVET HOLES BS 800, S19R TO S27R. INSTALLED NEW FRAME AND WEBS PER BOEING DRAWINGS 65-C35243 AND 69-42945, AND EA 59494. (M)
CLT - FOUND CRACK IN THE NR 2 ENGINE PYLON SCREW HOLE. INSTALLED NEW ANGLE, DOUBLERS AND FILLERS PER EA 57446, EA 57462, SRM 51-40-01 AND SRM 54-10-3. (M)
CLT - FOUND SURFACE CORROSION AT SEAT TRACK MOUNT AT STATION 294, RBL 45.5. REMOVED SURFACE CORROSION ALODINED AND PRIMED. (M)
CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 987, LBL 5. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-0. (M)
CLT - FOUND CORROSION AROUND SCREW HOLES AND ADJACENT AREAS, BS 947, RBL 3 THROUGH RBL 22 ON FLOOR BEAM. REMOVED SURFACE CORROSION BY BURNISHING THE TOP SURFACE. (M)
CLT - FOUND CORROSION AROUND SCREW HOLE BS 947, RBL 40. REMOVED SURFACE CORROSION ON FLOOR BEAM PER SRM 51-10-06. (M)
CLT - FOUND CORROSION (C53-107-02) ON AFT LAV FLOOR SUPPORT, STATION 1006-966, LBL 10-10. REMOVED NUT PLATES ON THE FLOOR BEAM SUPPORT, REMOVED LIGHT CORROSION BY BURNISHING PER SRM 51-10-6. (M)
CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 986, RBL 50 THROUGH LBL 21. REMOVED SURFACE CORROSION PER SRM 51-10-6. ALODINED AND PRIMED THE AREA. (M)
CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 967, RBL 42. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-6. (M)
CLT - FOUND CORROSION (C53-107-02) ON AFT GALLEY SEAT TRACK AT STATION 986-1016, RBL 20. REMOVED CORROSION PER SRM 51-10-6 AND ALODINED AND PRIMED THE AREA. (M)
ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY AISLE PATH LIGHTING AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OKAY.
FLT NR 546 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE LANDING GEAR WARNING HORN SOUNDED WITH THROTTLES RETARDED TO IDLE AND FLAPS UP. WARNING HORN DID NOT SOUND AT FLAP SETTINGS 1 OR 5 WITH THROTTLES RETARDED TO IDLE. LANDING GEAR WAS UP IN BOTH CASES. MAINTENANCE PEFORMED LANDING GEAR WARNING TEST PER MM 31-26-0 AND FLAP SETTINGS 1 AND 5 CHECKED NORMAL. LUBED FLAP SWITCH AS PRECAUTIONARY. (M)
FLT NR 465 - DEN -UPON ARRIVAL, FLIGHT CREW REPORTED RUDDER TRIM REQUIRED ONE FULL UNIT OF RIGHT RUDDER ADJUSTMENT TO ESTABLISH ZERO DEGREE DRIFT. MAINTENANCE REPLACED THE RUDDER POWER CONTROL UNIT AND SYSTEM CHECKED OK. (M)
BZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHECK. SYSTEM CHECKED OK. A FAULT WAS FOUND ON THE ANTI-SKID MODULE TEST AND THE LEFT OUTBOARD ANTI-SKID BRAKE SYSTEM WAS PLACARDED PER MEL 32-2. S/D MAINTENANCE REPLACED THE ANTI-SKID CONTROL UNIT ON THE LEFT OUTBOARD ANTI-SKID BRAKE AND SYSTEM CHECKED OK. (M)
FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. PLACARDED PER MEL 33-14. UPON ARRIVAL IN DEN, MAINTENANCE REPAIRED CANNON PLUG AND CHECKED OKAY. (X)
OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR 95ZZZX785. (X)
OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR F3LA95002.