N134AS
Registered owner: SKYLINE AVIATION INC, 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
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.
8 reports on file, 2014-09-16 – 2016-04-28.
Part: SUPPORT CHANNEL — CORRODED (BS 727D) · corrosion level 2 · airframe 56,044 hrs · 25,711 cycles
NR 3 VHF SUPPORT CHANNEL IS CORRODED AT FS 727D, LBL1-RBL1, WL.148.5, BLENDED AREA ON SUPPORT CHANNEL, L=2", W=1.5", D=.020" ORIGINAL MATERIAL 0.050" FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-53. MATERIAL ID TO FABRICATE NEW NR 3 VHF SUPPORT CHANNEL IS BAC1498-168. PO. AER016042783353. 0.050. IAW DWG 65-65710, REV CHECK FABRICATED, LOCATED, DRILLED AND DEBURRED NEW SUPPORT CHANNEL IAW DWG 65-65710, REV CHECK. TREATED AND PRIMED NEW SUPPORT IAW SRM 51-20-01. INSTALLED NEW CHANNEL IAW SRM 51-40-02 DWG 65C37049, REV ORIGINAL.
Part: SKIN — CRACKED (BS 727D) · airframe 56,044 hrs · 25,711 cycles
FUSELAGE SKIN HAS A 1.25" CRACK UNDER THE NR 3 VHF ANTENNA. FOUND WHILE ACCOMPLISHING HFEC INSPECTION AT BS 727D, LBL1-RBL1. WL.148. REMOVED ALL FASTNERS COMMON TO SB B737-53-1287. FABRICATED REPAIR DOUBLER AND TRIPLER FROM 2024-T3 0.071 PO AVIM15101500030 AND A 2024-T3 FILLER FROM 0.063, PO AVIA15062400021 IAW SB 737-53-1287, FIG 20. CUT OUT CRACKED CONDITION AND PREFORMED A HFEC INSPECTION IAW SB 737-53-1287 AND DWG 65C37049-3 FABRICATED, LOCATED, DRILLED AND DEBURRED ALL REPAIR PARTS IAW SB 737-53-1287 AND DWG 65C37049-3. ALODINE AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLED REPAIR IAW SB 737-53-1287 DWG 65C37049-3AND SRM 51-40-02.
Part: LIGHT — FAULTY (CABIN) · airframe 56,044 hrs · 25,711 cycles
DURING A GENERAL VISUAL INSPECTION OF THE EMERGENCY LIGHTING SYSTEM, A 13.5" AREA FAILED AN ILLUMINATION CHECK. THE DISCRIPENT AREA WAS REMOVED IAW CMM 33-51-06. A NEW SECTION OF PN PL88-9 WAS CUT AND INSTALLED USING TESAFIX 4965, IAW CMM 33-51-06 SEC.3 PAGE 601. OPS CHECK WAS COMPLETED, WITH NO DISCREPINCES NOTED.
Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 59,461 hrs · 36,890 cycles
CABIN PASSENGER OXYGEN MASKS DEPLOYED WITH 5 OXYGEN GENERATORS USED. REPACED ALL CABIN OXYGEN MASKS IAW AMM 35-22-31. REPLACED 5 EA OXYGEN GENERATORS IAW AMM 5-22-11.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 59,364 hrs · 36,810 cycles
CAPTAIN'S WINDSHIELD HAS MULTIPLE CRACKS.
Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 58,640 hrs · 36,434 cycles
AFT CARGO DOOR FRAME INTERIOR FWD EDGE HAS MULTIPLE AREAS OF CORROSION INCLUDING EXFOLIATION.
Part: GATE — CORRODED (R1 DOOR) · airframe 58,640 hrs · 36,434 cycles
R1 DOOR LOWER GATE CASTING CORRODED.
Part: KEELBEAM — CRACKED (ZONE 100) · airframe 58,640 hrs · 36,434 cycles
DURING MAINTENANCE CHECK, FOUND A CRACK ON THE LT KEELBEAM WEB BETWEEN BS 620 AND BS 630. OPEN