N5300
Registered owner: MULHALL TIMOTHY P, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
9 reports on file, 2005-03-13 – 2021-06-28.
Part: FUEL — NONE (FUEL SECTOR)
PISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANK
Part: FUEL — NONE (FUEL SECTOR)
PISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANK
Part: SEAT TRACK — CORRODED (BS 373.15) · airframe 11,228 hrs · 12,175 cycles
CORROSION 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 ALODINE TREATMENT IAW SRM 51-21-10-02-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 10,385 hrs · 11,359 cycles
FRAME 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 IAW SRM 51-42-05-02-01, REV 12. VERIFIED AFFECTED AREAS TO BE CRACK FREE REF NDTM PART 6 TASK 51-00-01-250-801, REV 8. MIN THICKNESS NOTED .045" REF NDTM PART 1 TASK 51-00-04-910-801 REV 8. NOMINAL THICKNESS .040" REF DWG 85328142 FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15-00-01, REV 12. ALODINE AND PRIMED REWORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01 REV1 2. INSTALLED RIVETS IAW SRM 51-42-05-02-01, REV 12. APPLIED TOP COAT IAW SRM 51-25-15-02-01 REV 12. APPLIED CPC IAW AMM 51-25-01-390-801, REV 40. RESECURED WIRES IAW WM 20-12-10-201, REV 39.
Part: STRINGER — CORRODED (ZONE 200) · airframe 10,744 hrs · 11,707 cycles
STRINGER 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 8/4-53-3888. RESTORED SURFACE PROTECTION IAW RD 8/4-53-3888. APPLIED CPC IAW AMM 51-25-01-390-801.
Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 35,292 hrs · 15,613 cycles
PSV14 FWD CARGO DOOR SILL WEB CORRODED. INSTALLED NEW WEB IAW SRM 51-40-02 AND DWG 143A8122 SHEET 5.
Part: SKIN — CORRODED (BS 295-310) · airframe 21,304 hrs · 15,667 cycles
CORROSION 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 WITHIN LIMITS PER CRJ700 SRM 53-00-00. TREATED, PRIMED AND PAINTED IAW CRJ700 SRM 51-21-11, 51-25-06 AND 51-25-16.
Part: FRAME — CRACKED (FUSELAGE)
FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED FRAME IAW SRM. (K)
Part: FRAME — BENT (FUSELAGE) · airframe 59,330 hrs · 33,035 cycles
AFT 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 0.090 PO NR 9001777 DIMENSIONS 11/16' BY 8 1/2' IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-40-3 FIG 1.