N148AS
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.
29 reports on file, 2014-07-30 – 2016-04-11.
Part: SKIN — CRACKED (LEFT ELEVATOR) · airframe 55,483 hrs · 33,640 cycles
LEFT ELEVATOR HAS A 1.0" CRACK ON THE LOWER SURFACE AT BS 154, WL 260. REMOVED DAMAGE IAW CIN-16-0012-016, ACCOMPLISHED BOND TEST IAW NDT PART 4, PROCEDURE 1, NO DEFECTS NOTED. CLEANED AREA IAW EO-16-028-WO001. INSTALLED REPAIR PLIES IAW EO-16-028-WO001. PRIMED AND TOPCOAT IAW AMM 51-21-21 AND 51-21-73. PERFORMED WEIGHT AND BALANCE CHECK IAW MANUAL 51-60-04 FOUND TO BE WITHIN PREFERRED RANGE SBHM, NEW 100.4". REINSTALLED TAB MECHANISM IAW AMM 27-11-31.
Part: FRAME — CRACKED (BS 312) · airframe 55,483 hrs · 33,640 cycles
ELECTRONIC ENGINE COMPARTMENT LOWER FRAME, AT BS 312, RBL 32, WATERLINE 199. HAS A 0.50" CRACKED. REMOVED ALL FASTENERS COMMON TO CRACK IAW SRM 51-40-02, AND SRM 53-10-51. STOPPED DRILLED A .250 HOLE AT END OF CRACK IAW SRM 53-10-51, REPAIR 4. FABRICATED REPAIR PLATE IAW SRM 53-10-51. ALODINE, PRIME AND TOPCOAT IAW SRM 51-21-72 AND 51-21-73. INSTALLED REPAIR PLATE IAW SRM 53-10-51 AND 51-40-02. REPAIR SIZE, 4.00" X 2.40".
Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 55,483 hrs · 33,640 cycles
LEFT ELEVATOR HAS PUNCTURE OF 0.490 ON UPPER SURFACE AT ELEVATOR BS 109, WL 264. REMOVED DAMAGE ON LT ELEVATOR AND PREPPED FOR LAYUP IAW SRM 51-70-17, MATERIAL ID BMS 9-8 3K-70-PW BATCH/LOT 985149, GRAPHITE CLOTH EA9390A/B, ADHESIVE PO KLX15123087013 IAW SRM 51-70-17, LAYED UP AND CURED REPAIR, IAW SRM 51-70-17, ACCOMPLISHED TAP TEST, NO DEFECTS NOTED. REPAIR 5.0" X 5.0".
Part: SKIN — CRACKED (BS 727D) · airframe 55,483 hrs · 33,640 cycles
DURING SB 737-53-1287-01, TWO CRACKS WERE FOUND AT BS 727D, LBL 1 - RBL 1, WL 148.5. LBL CRACK IS 1.13 INCHES & RBL CRACK IS 1.42. HF ANTENNA AND HARDWARE WERE REMOVED IAW SRM 51-40-02 AND SB 737-53-1287. PERFORMED CUTOUT IAW DWG 65C37049-3 AND SB 737-53-1287. PERFORMED HFEC INSPECTION IAW B737-53-1287, PG 139, STEPS I, M, AND N. NO DEFECTS. FABRICATED REPAIR DOUBLER & TRIPLER IAW SB 737-53-1287. PERFORMED HFEC INSPECTION, NO DEFECTS. FABRICATED, LOCATED, & DRILLED IAW DWG 65C37049, REV ORIGINAL AND SB 737-53-1287, REV 1. INSTALLED REPAIR IAW SRM 51-40-02 AND SB 737-53-1287 & DWG 65C37044.
Part: SKIN — CRACKED (BS 951-965) · airframe 55,483 hrs · 33,640 cycles
FUSELAGE SKIN AT BS 951, RBL 45, WL 260, THERE IS A 1.00" CRACK AFT GALLEY DOOR UPPER HINGE CUTOUT. REMOVED WEB FORWARD OF GALLEY DOOR, IAW SRM 51-40-02. REMOVED ALL EXISTING FASTENERS IAW SRM 53-60-01, REPAIR 5. REMOVED DAMAGED AREA IAW SRM 53-60-01, REPAIR 5, STEP 3. PERFORMED HFEC INSPECTION OF THE CUTOUT IAW SRM 53-60-01, STEP 4. ACCOMPLISHED 0.040" INSURANCE CUTOUT IAW SRM 51-60-01, REPAIR 5. FABRICATED REPAIR FILLER FROM 2024 T3 0.080, PO AVIM16031700043 IAW SRM 53-60-01, REPAIR 5. TREATED AND PRIMED IAW SRM 51-20-01. FABRICATED REPAIR PLATE 0.063, 1,2 HARD AMC5518, PO. AVIM16040400045, IAW SRM 53-60-01, REPAIR 5. LOCATED, AND DRILLED REPAIR PLATE IAW SRM 51-60-01. REPAIR 5. ALODINE AND PRIMED REPAI
Part: FRAME — CRACKED (BS 312) · airframe 55,483 hrs · 33,640 cycles
ELECTRONIC EQUIPMENT COMPARTMENT AT BS 312, LBL 12, WL 199, THERE IS A CRACK 0.750 IN THE FRAME STRAP. REMOVED ALL FASTENERS COMMON TO THE STRAP IAW SRM 51-40-02 AND 51-10-51, REPAIR 4, STOPPED DRILLED END OF CRACK 0.250, IAW SRM 53-10-51, FABRICATED REPAIR PLATE FROM 2024, T3, 0.040, PO AVIM16040400045 IAW SRM 53-10-51. REPAIR 4 ALODINE AND PRIMED REPAIR PLATE IAW AMM 51-21-72 AND AMM 51-21-73. INSTALLED REPAIR PLATE IAW SRM 53-10-51 AND 51-40-02. REPAIR DEMENTIONS 2.40" X 7.15".
Earlier reports · 2014–2015 · 23 reports
2015
Part: WINDOW — CRACKED (COCKPIT) · airframe 54,936 hrs · 33,248 cycles
ENROUTE, ON CLIMBOUT- APPROXIMATELY FL220, F/O'S WINDOW CRACKED, SHATTERED. OPS IAW QRH, OK TO CONTINUE LAND W/NO FUTURE ISSUE. REMOVED NR 1 WINDOW IAW AMM 56-11-11. INSPECTED WINDOW FRAME AND HARDWARE AS REQUIRED. INSTALLED F/O WINDOW IAW AMM 56-11-11. PERFORMED PRESSURE LEAK CHECK, NO LEAKS NOTED. R & R RT FRONT WINDOW HEAT CONTROLLER AND PERFORMED, OPS CHECK AMM 30-41-11, CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,757 hrs · 33,145 cycles
THE R2 DOOR EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED THE LAMP IAW 33-51-31.
Part: SKIN — DENTED (ZONE 100) · airframe 53,692 hrs · 32,789 cycles
FOUND DAMAGE TO FUSELAGE SKIN FORWARD OF THE FWD LWR CARGO DOOR BELOW SKIN SPLICE.
2014
Part: CHANNEL — CORRODED (BS 857) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
AFT CARGO BAY TRANSITION PANEL SUPPORT AT LBL 20 BS 857 HAS CORROSION ON OLD REPAIR. REPAIRED ON FAS N148AS-01-01, NR 61224.
Part: SKIN — DENTED (BS 892) · airframe 53,210 hrs · 32,594 cycles
DENT FOUND IN SKIN ABOVE S26L, APPROXIMATELY BS 892. REPAIRED ON FAS N148AS-01-01, NR 61159.
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT BS 990, LBL 32 TIE DOWN FITTING HAS LIGHT CORROSION. REPLACED IAW FAS N148AS-01-01.
Part: FRAME — CRACKED (ZONE 200) · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT FRAME BS 380, BELOW STRINGER 8L CRACKED. REPAIRED IAW FAS N148AS-01-01.
Part: FRAME — CRACKED (BS 400) · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT FRAME BS 400 BELOW STG 8R AROUND RIVET CRACKED. REPAIRED ON FAS WO N148AS-01-01.
Part: FRAME — CRACKED (ZONE 200) · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN FRAME, BS 907 BELOW STRINGER 8R CRACKED. REPAIRED IAW FAS W/O N148AS-01-01.
Part: FRAME — CRACKED (BS 400) · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT FRAME BS 400 BELOW STG 8L AROUND RIVET CRACKED.
Part: FLOORBEAM — CORRODED (BS 986.5) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN ON FLOORBEAM 986 BL 0 - LBL 45 HAS LIGHT CORROSION. REPAIRED IAW N148AS-01-01.
Part: FRAME — CRACKED (BS 827) · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN FRAME BS 827 BELOW STRINGER 8L CRACKED AROUND RIVET. REPAIRED ON FAS WO N148AS-01-01.
Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT BS 328 FLOORBEAM BETWEEN LBL 49 AND LBL 56 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01, NR 60853.
Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN BETWEEN BS 327-333, RBL 60 CHANNEL CORRODED. REPAIRED ON FAS N148AS-01-01, NR 60860.
Part: FLOORBEAM — CORRODED (BS 366) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN AT FLOORBEAM BS 366 BETWEEN BL 0 - LBL 20 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CABIN FLOORBEAM AT BS 360 BL 0 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01.
Part: FLOORBEAM — CORRODED (BS 907) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
MAIN CARGO AT FLOORBEAM, BS 907, BL0 HAS LIGHT CORROSION. REPAIRED FLOORBEAM.
Part: WEB — CORRODED (BS 494) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
AFT/LOWER CARGO DOOR FRAME BS 494 STRINGER 28R UPPER WEB IS CORRODED AND GOUGED IN SEVERAL PLACES. REPAIRED ON FAS N148AS-01-01.
Part: DOOR SILL — CORRODED (BS 807-845) · corrosion level 2 · airframe 53,210 hrs · 32,594 cycles
AFT CARGO LOWER DOOR SILL CORRODED INSIDE AROUND FASTENERS BETWEEN BS 807-845. REPAIRED ON FAS N148AS-01-01.
Part: SKIN — DENTED (BS 907-947) · airframe 53,210 hrs · 32,594 cycles
LEFT FUSELAGE SKIN HAS SEVERAL DENTS BETWEEN BS 907 - 947.5 STRINGERS 17 - 19 LT. REPAIRED IAW FAS N148AS-01-01.
Part: SKIN — DENTED (ZONE 100) · airframe 53,210 hrs · 32,594 cycles
EXT FUSELAGE RT SIDE AT STA 495, BETWEEN 20R & 22R HAS MULTIPLE DENTS. REPAIRED ON FAS WO N148AS-01-01, NR 60228.
Part: SKIN — DENTED (BS 251) · airframe 53,210 hrs · 32,594 cycles
SKIN BS 251 BETWEEN 23-24R HAS PROTRUDING DENT. REPAIRED IAW FAS N148AS-01-01.
Part: SKIN — DENTED (BS 460-500) · airframe 53,210 hrs · 32,594 cycles
FUSELAGE BELLY BS 490 DENTED. REPAIRED IAW N148AS-01-01.