N338BC
Registered owner: BURKE JOHN W JR, KY (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, 2015-06-19 – 2015-09-29.
Part: LATCH — CORRODED (NR 1 NACELLE) · airframe 25,839 hrs · 15,429 cycles
NR 1 ENG OTBD FAN COWL HAS COMPOSITE DAMAGE AROUND AFT LATCH. REPAIRED NR 1 ENGINE OTBD FAN COWL IAW PRI 536955-14, REV 0, AND ER/A 536955-14, REV. ORIGINAL.
Part: RIB — CRACKED (NR 1 NACELLE) · airframe 25,839 hrs · 15,429 cycles
NR 1 PYLON OTBD AFT FLUID BARRIER RIB CRACKED AT APPROXIMATELY STA 135. COMPLIED WITH ERA536952-14, REV A ON NR 1 PYLON OTBD-AFT FLUID BARRIER RIB AT APPROXIMATELY BS 135 ID IAW TOPP 30-10-70 AND PS 900-5-1, NR 4.
Part: STRAP — CRACKED (BS 370) · airframe 25,839 hrs · 15,429 cycles
DURING ACCOMPLISHMENT OF ER/A 535454-14, REV A, SECT I: SECTION 41, REPAIR SURVEY, FOUND CABIN FLOORBEAM STABILIZATION STRAP AT BS 370 LBL 24 CRACKED UNDER PREVIOUS REPAIR DOUBLER. REMOVED THE REPAIR, TRIMMED-OUT DAMAGED SECTION OF STABILIZATION STRAP AT BS 379 - 345 AT LBL 24 AND ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-51, REPAIR 12 AND ER 42.
Part: FRAME — CORRODED (BS 1540) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
CORROSION IN SEVERAL LOCATIONS ON FRAME BS 1540 BETWEEN S28-29R. REMOVED CORROSION ON FRAME IAW SRM 53-00-07, AD1 DETAIL II. REPLACED THE FRAME IAW SRM 51-40-02, 51-40-05 & DWG 146N1018.
Part: FRAME — DAMAGED (BS 580) · airframe 25,839 hrs · 15,429 cycles
FRAME DAMAGED BS 580, ACCOMPLISHED PERMANENT MAJOR REPAIR ON FWD CARGO LT FRAME AT BS 580 BETWEEN STR 22 - 26L IAW ER/A 536959-14AD REVISION ORIGINAL SECTION I.
Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
R1 DOOR GATE, LOWER GATE HAS CORROSION ALONG BOTH LOWER EDGES IN ONE 14" LONG AREA AND SEVERAL SPOTS IN A 19" LONG AREA FROM FWD TO AFT CORNERS. REMOVED AND INSTALLED NEW R-1 DOOR LOWER GATE IAW AMM 52-11-38-004-001 AND IAW AMM 52-11-38-404-009.
Part: CREASE BEAM — CORRODED (BS 730-742) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
CORROSION ON RT CREASE BEAM INBD CHORD BETWEEN BS 730 - 742. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15. R & R THE CREASE BEAM ANGLE IAW SRM 41-40-02, PAGE 2, PAR B AND PAGE 6, PAR D, DWG 143N8328.
Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
L1 DOOR, LOWER GATE HAS CORROSION ALONG LOWER EDGE IN 8 PLACES FROM FWD TO AFT CORNER. REMOVED CORROSION ON L-1 DOOR LOWER GATE FROM FWD TO AFT IAW SRM 52-10-02. ORIGINAL MATERIAL DIMENSION ON LOWER EDGE OF LOWER GATE IS 4.92" IAW DWG 141N6206, MATERIAL LOSS IS .110" FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. R & R L-1 LOWER GATE, PN 141N6120-29 IAW AMM 52-11-38-404-009.
Part: FLOOR SUPPORT — CORRODED (BS 376-678) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
CORROSION ON MAIN CABIN FLOOR SUPPORT, BS 376 - 378, BL0. REMOVED CORROSION ON MAIN CABIN FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 AD1, DETAIL III. R & R MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02, PG 6, 7 REF DWG 141N5191, REV A.
Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 25,839 hrs · 15,429 cycles
L1 DOOR, GIRT BAR MECHANISM, FWD & AFT GIRT BAR CRANKS HAVE PLAY AT HINGE. REMOVED CRANK, PN 140N2769-1, FOUND TO BE OUT OF LIMITS IAW DWG 140N2769, DIAMETER 0.5009, MAX ALLOWABLE 0.5006, INSTALLED NEW CRANK, PN 140N2769-1 IAW CMM 52-11-07. REMOVED CRANK, R & R BUSHINGS IAW AMM 20-10-02 AND SOPM 20-50-02. INSTALLED THE CRANKIAW CMM 52-11-07. GIRT BAR ADJUSTMENT TO BE ACCOMPLISHED ON CARD NR 2040-0057-1L.
Part: FLOOR SUPPORT — CORRODED (BS 1200-1344) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
AFT CARGO BAY HAS SEVERAL AREAS OF CORROSION ON CARGO FLOOR SUPPORT BOTH UPPER AND LOWER SURFACES BETWEEN BS 1200 - 1344, RBL 10.45. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, PG 7 & 21, DWG 146N5390, AND ER/A 491157-14MA, REV A.
Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 25,839 hrs · 15,429 cycles
LIGHT CORROSION ON MAIN CABIN FLOOR SUPPORT BETWEEN BS 1660 - 1680, BL0. R & R THE FLOOR SUPPORT IAW SRM 51-40-05, 51-40-02, PARA 4 & PARA 7 AND DWG 146N5230.