- Registered owners
- Mulhall Timothy PElsea George E
- Location
- Lampasas, TX
- Owner type
- Co-owned
- Serial number
- T-5703
- Year built
- 1940
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 1, 1969
- Certificate issued
- July 16, 2022
- Expires
- July 31, 2029
- Mode S code
- A6B2C5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QXEA2013091001346Seat Track · corrodedCORROSION FOUND ON RT INBD SEAT TRACK AT FS 373.15. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINESDR QXEA2013022100398Frame · corrodedFRAME FLANGES AT FR 176 STR 32-30P HAVE CORROSION. REMOVED 1 EA RIVET TO FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01, 53-00-00-02-09 REV 12 AND DISPLACED WIRES IAW AMM 20-30-26-910-801, REV 40. PRIOR TO CORROSION REMOVAL REMOVED AN ADDITIONAL 6 RIVETS ISDR QXEA2011083000767Stringer · corrodedSTRINGER 30S IS CORRODED, FRAME 1.00 TO 19.4. REMOVED CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3888, MINIMUM REMAINING THICKNESS .057", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8SDR QXEA2009102600842Skin · corrodedCORROSION FOUND AROUND ANTENNA MOUNT BETWEEN FS 295.00 - 310.00. REMOVED 2 RIVETS TO ACCESS CORROSION IAW SRM 51-42-06. BLENDED .002 DEEP BY 1 INCH WIDE AND 1 INCH LONG. ORIGINAL THICKNESS IS .050 INCH. REMAINING MATERIAL AFTER BLEND .048 INCH. BLEND WITHSDR ASAA0640001Frame · crackedFRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED FRAME IAW SRM. (K)SDR DHL2005782538Frame · bentAFT CARGO BENT FRAME STA 1070 RIGHT AROUND STR 27R. REMOVED DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6,0. .063 PO NR 9001660 DIMENSIONS 3 1/4' X 8 1/2', FILLER REPAIR FROM 7075-T6 0.063 PO #9001660 DIMENSIONS 1 3/8' BY 1 3/4' AND SHIM FROM 7075-T6 0
Reports on N5300 not matched to an aircraft · 3
They name N5300, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2022FA0000635Fuel · nonePISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANKSDR 2022FA0000634Fuel · nonePISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANKSDR DALA10295837303Sill · corrodedPSV14 FWD CARGO DOOR SILL WEB CORRODED. INSTALLED NEW WEB IAW SRM 51-40-02 AND DWG 143A8122 SHEET 5.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.