N4874
Registered owner: GOIN JEFF TRUSTEE, FL (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
No NTSB accidents or incidents on file for this aircraft.
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.
12 reports on file, 2020-03-11 – 2020-04-13.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
PERFORME ROTO INSP FND 2EA HOLE CRACK AT LH-FR68, DOOR STOP NO.1 LOWER INBOARD HOLE & LOWER OUTBOARD HOLE REF NON-ROUTINE NO.9407 207 - ORIGINATED EA 5340-01724 OP002 STEP 3.1. PERFORMED AT LH-FR68 DOOR STOP NO.1, 2EA CRACKED HOLES REPAIRED AS PER ECRA 5341-01224 AND SRM 53-41-12-300-011 REV 132 AND REQUIRE RE-INSPECTION AT OR BEFORE A/C REACHES 45358 TOTAL FC AND REPEAT THE INSPECTION AT 9000 FC INTERVAL, THEREAFT ER. FOR AREA 1 (SHOWN IN EN PAGE 16 OF THIS ECRA), AT OR BEFORE AT OR BEFORE A/C REACHES 100158 TOTAL FC. PLANNING MUST CONTACT FR68 R, FR68 L (EXCEPT AT STOP FIG NO.1). REQUIRE RE-INSPECTION ECRA) PER THIS ECRA PART 1.2).3) AND PART 2.B).C). FOR FR66 L/R INTERVAL, THEREAFTER. FOR AREA 2 (SHOWN IN EN PAGE 16 OF THIS A/C REACHES 45358 TOTAL FC AND REPEAT THE INSPECTION AT 4800 FC ENGINEERING AFT 99500 TOTAL FC BUT BEFORE 99800 TOTAL FC FOR INSPECTION INTERVAL & METHOD PER ECRA 5341-01224 PART 1 B).1) AND PART 2 A). RII BY TA620.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
FR68 LH DOOR SILL AREA FND CORROSION REF NON-ROUTINE NO.9406285 - ORIGINATED SPEC NO.A3NB-53-3-6187. PERFORMED FR 66-68 L/H DOOR SILL RPELACED AS PER DWG E53474250000 ISSUE AF D53480076000 ISSUE J AND D53480505006. ISSUE AF. RII
Part: BATTERY — FAILED (CABIN) · airframe 46,551 hrs · 29,558 cycles
DURING TEST FND ESPU BATT 12WL LOW VOLTAGE REF NON-ROUTINE NO. 9407438 - ORIGINATED SPEC NO.A3NB-33-3-6012. PERFORMED REPLACED THE BATT 12WL AND PERFORMED OPS CHK OF ESPU. THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000- 002A REV 107, AMM 33-51-38-400-002A REV 107, AMM 33-51-00-710-00 1A REV 107.
Part: BATTERY — FAILED (CABIN) · airframe 46,551 hrs · 29,558 cycles
DURING TEST FND ESPU BATT 10WL LOW VOLTAGE REF NON-ROUTINE NO. 9407440 - ORIGINATED SPEC NO.A3NB-33-3-6012. PERFORMED REPLACED THE BATT 10WL AND PERFORMED OPS CHK OF ESPU. THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000- 002A REV 107, AMM 33-51-38-400-002A REV 107, AMM 33-51-00-710-00 1A REV 107.
Part: BATTERY — FAILED (CABIN) · airframe 46,551 hrs · 29,558 cycles
DURING TEST FND ESPU BATT 11WL LOW VOLTAGE REF NON-ROUTINE NO. 9407439 - ORIGINATED SPEC NO.A3NB-33-3-6012. PERFORMED REPLACED THE BATT 11WL AND PERFORMED OPS CHK OF ESPU. THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000- 002A REV 107, AMM 33-51-38-400-002A REV 107, AMM 33-51-00-710-00 1A REV 107.
Part: BATTERY — FAILED (CABIN) · airframe 46,551 hrs · 29,558 cycles
DURING TEST FND ESPU BATT 13WL LOW VOLTAGE REF NON-ROUTINE NO. 9407437 - ORIGINATED SPEC NO.A3NB-33-3-6012. PERFORMED REPLACED THE BATT 13WL AND PERFORMED OPS CHK OF ESPU. THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000- 002A REV 107, AMM 33-51-38-400-002A REV 107, AMM 33-51-00-710-00 1A REV 107.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
DOOR 2R DOOR SILL FND CORROSION UNDER AFT GIRT BAR FITTING AREA REF NON-ROUTINE NO.9407205 ORIGINATED SPEC NO.A3N B-53-3-6299. PERFORMED, 2R DOOR SILL REPLACED AS PER DWG D5348 0078 ISSUE G AND E53474250000 ISSUE AF AND D53480505006 ISSUE EQ . RII BY TA620
Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
BULK CARGO COMPT BILGE AREA FR63-64 ST43L CORROSION. BULK CARGO COMPT BILGE AREA FR63-6 STR43L REPAIRED AS PER EC/RA 5341-01219. NO FURTER ACTION REQUIRED. SEE HAECO N/R 9406508 & EC/RA 5341-01219. LOG CLEARED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
BULK CGO COMPT BILGE AREA FR64-65 STGR 42L STRINGER FND CORROSION REF NON-ROUTINE NO.9406486 - ORIGINATED BY EMP, SPEC NO.A3NB-53-3-6179.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
CORROSION BULK CARGO BILGE AREA STR42 BETWEEN FR62 & FR63. CORROSION REMOVED AS PER SRM 51-74-00. DAMAGED AREA REMOVED AND REPAIR INSTALLED AS PER SRM 53-00-13-300-001. NDT CHECK PER NTM 51-10-08 CONFIRMS NO CRACKS. REQUIRES REPEAT INSPECTION AT 60,000 FLIGHT CYCLES OR 120,000 FLIGHT HOURS WWHICHEVER IS ACHIEVED FIRST AS PER 53-00-13-205-001. REF HAECO N/R 9406507. REQUESTING DIP CARRY AS PER ABOVE REQUIREMENTS. NOTE: REPEAT INSPECTION LIMIT IS 120,000 FLIGHT HOURS OR 60,000 FLIGHT CYCES FROM REPAIR EMBODIMENT. CORROSION BULK CARGO BILGE AREA STR42 BETWEEN FR62 & FR63. CORROSION REMOVED AS PER SRM 51-74-00. DAMAGED AREA REMOVED AND REPAIR INSTALLED AS PER SRM 53-00-13-300-001. NDT CHECK PER NTM 51-10-08 CONFIRMS NO CRACKS. REQUIRES REPEAT INSPECTION AT 60,000 FLIGHT CYCLES OR 120,000 FL
Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
CORROSION BULK CARGO BILGE AREA STR44 BETWEEN FR63 & FR64. CORROSION REMOVED AS PER SRM 51-74-00. DAMAGED AREA REMOVED AND REPAIR INSTALLED AS PER SRM 53-00-13-300-001. NDT CHECK PER NTM 51-10-08 CONFIRMS NO CRACKS. REQUIRES REPEAT INSPECTION AT 60,000 FLIGHT CYCLES OR 120,000 FLIGHT HOURS FROM REPAIR EMBODIMENT, WHICHEVER IS ACHIEVED FIRST. AS PER SRI 53-00-13-205-001. REF HAECO N/R 9406480. REQUESTING DIP CARRY AS PER ABOVE REQUIREMENTS. CORROSION BULK CARGO BILGE AREA STR44 BETWEEN FR63 & FR64. CORROSION REMOVED AS PER SRM 51-74-00. DAMAGED AREA REMOVED AND REPAIR INSTALLED AS PER SRM 53-00-13-300-001. NDT CHECK PER NTM 51-10-08 CONFIRMS NO CRACKS. REQUIRES REPEAT INSPECTION AT 60,000 FLIGHT CYCLES OR 120,000 FLIGHT HOURS FROM REPAIR EMBODIMENT, WHICHEVER IS ACHIEVED FIRST. AS PER SRI
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,551 hrs · 29,558 cycles
FWD CGO COMPT BILGE AREA FR 30-34 STGR 44-43R DOUBLER UPPER SURF ACE FND CORROSION - REF NON-ROUTINE NO.9407101 ORIGINATED, SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP, FWD CGO COMPT BILGE AREA FR 30-34 STGR 44-43R DOUBLER REPLACED AS PER SRM 51-42-11 REV 130 AND DWG 5323 3523 ISSUE A.