N393BC
Registered owner: HYLIO 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, 2015-07-23 – 2015-12-03.
Part: FRAME — DENTED (BS 660) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 660, STR 23L-25L, FRAME DENTED SEVERAL PLACES. REJECTED DUE TO INCOMPLETE WORK, NO OPEN HOLE OR NEW STR CLIPS DOCUMENTED REF SRM 53-00-07, REPAIR 5, DETAIL III. COMPLIED WITH SRM 53-00-07, REPAIR 5, DETAIL III, HFEC OPEN HOLE INSPECTION PERFORMED ON ALL HOLES COMMON TO THE REPAIR AND STR CLIP ATTACHMENTS. REPLACED STR CLIPS. DOCUMENTATION OF THESE STEPS COMPLETE WORK REQUIRED ON NRC 100-164, REF ORIGINAL LOGPAGE 2182288.
Part: SKIN — DAMAGED (BS 1460-1480) · airframe 29,601 hrs · 17,657 cycles
AFTER REMOVAL OF ANTENNA MOUNT, FOUND SCRIBE MARKS AT ANTENNA MOUNT AREA, LWR EXT FUSELAGE SKIN BETW BS 1460 -1480, STR 29R-30. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN ANTENNA MOUNT AREA BS 1459-1480 BETWEEN STR 29R-30, REF ER/A 541036-14, REVISION ORIGINAL.
Part: FRAME — CORRODED (BS 1460) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO UNDER FLOOR FRAME BS 1460 HAVE 3 AREAS OF CORROSION AT RT SIDE OF STR S-30 AND OTBD OF STR S-29R. REMOVED CORROSION AT RT SIDE OF STR S-30, OTBD OF STR S-29R AND ACCOMPLISHED A PERMANENT REPAIR REF ER/A 538392-14, REV ORIGINAL AT BS 1460 FRAME.
Part: FRAME — DENTED (BS 660) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 660 STR 23-25R, FRAME DENTED 2 PLACES. TRIMMED-OUT 2 EA DENTS ON FRAME AT BS 660, STR 23R-25R, REF SRM 53-00-07, REPAIR 5. TRIMOUT NR 1 MEASURES 1.040" X 2.105" X 0.5" R, TRIMOUT NR 2 MEASURES 1.090" X 1.040" X 0.5"R. ACCOMPLISHED PERMANENT REPAIR CAT "B" ON FRAME 660 BS, STR 23R -25R, REF SRM 53-00-07, REPAIR 5. THRESHOLD INSPECTION REQUIRED AT 42657 F/C WITH REPEAT INSPECTION EVERY 11000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION. ACFT CURRENTLY AT 17657, F/C REF SRM 53-00-07, REP 5, FIG 201, TABLE II, PAGE 210. ACCOMPLISHED ER/A 539824-14, REV ORIGINAL FOR 2 EA STR CLIPS, R & R AT STA 660, BETWEEN STR 23R-25R.
Part: SKIN — DENTED (BS 1320) · airframe 29,601 hrs · 17,657 cycles
LOWER FUSELAGE- 1EA DENT BETWEEN RIVETS FOR FRAME ON SKIN AT BS 1320 AND 1" ABOVE S-27R. DENT MEASURED 1.0" X 0.9" X 0.012" DEEP, A/Y=75. ACCOMPLISHED PERMANENT REPAIR ON DENT FUSELAGE SKIN FOR FRAME AT BS 1320 & 1" ABOVE S-27R IAW ER/A 539852-14, REV ORIGINAL NO CRACK FOUND ON DENTED AREA & DENT WAS ALLOWED TO REMAIN AS-IS REF ER/A 539852-14, REV ORIGINAL INSTALLED ID TAG IAW PS 900-5-1, NR 04 & ESTABLISHED DENT DECAL MONITOR IAW TOPP 30-10-70, PAGE 13. ASSOCIATED ER/A 14-539852 ADDED FOR ACFT.
Part: SKIN — CORRODED (BS 535) · airframe 29,601 hrs · 17,657 cycles
CORROSION ON LOWER FUSELAGE SKIN, BS 535 BETWEEN STRINGER 28L AND 28R, ON ANTENNA MOUNTING AREA. REMOVED CORROSION ON LOWER FUSELAGE SKIN BS 535 BETWEEN STR 28L & 28R ON ANTENNA MOUNTING AREA, BLENDOUT MEASURE 6" X 2.5" X .050" MIN REM MATERIAL ACCOMPLISHED PERMANENT REPAIR IAW ER/A 538391-14, REV ORIGINAL.
Part: SUPPORT — GOUGED (L4 DOOR) · airframe 29,601 hrs · 17,657 cycles
L4 DOOR POWER ASSIST BOTTLE CABLE SUPPORT ASSY IS GOUGED. REMOVED AND INSTALLED NEW DOOR POWER ASSIST BOTTLE CABLE SUPPORT ASSY AT L-4 DOOR IAW AMM.
Part: SEAT TRACK — CORRODED (BS 365-418) · airframe 29,601 hrs · 17,657 cycles
MAIN CABIN, CORROSION ON SEAT TRACK SUPPORT BETWEEN BS 365 & 418, RBL 24. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02, PAGES 7, 21, DETAIL II & DWGS 141N5130, 141N5131, REV A.
Part: SEAT TRACK — CORRODED (BS 365-418) · airframe 29,601 hrs · 17,657 cycles
MAIN CABIN SEAT TRACK CORRODED BS 365 - 418, RBL 45. REMOVED ALL CORROSION IAW SRM 53-00-52, FIG 101 AND FOUND AREAS OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02, PAGE 7, PAR 8 & DWG 141N5130, REV E.
Part: SEAT TRACK — DAMAGED (BS 494) · airframe 29,601 hrs · 17,657 cycles
WHILE WORKING CARD 2021-2074 FOUND SEAT TRACK OUT OF LIMITS AT BS 494, RT INBD. CUTOUT AND PERMANENTLY REPAIRED DAMAGED SEAT TRACK SECTION FROM FS 440-569.5, RBL 24.5 IAW SRM REPAIR 3 PG 203, FIG 201 & SWPM 707, 727-787, INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: FLOOR SUPPORT — CORRODED (BS 360-377) · airframe 29,601 hrs · 17,657 cycles
CORROSION FOUND ON FLOORBEAM STRUCTURAL SUPPORT IN SEVERAL LOCATIONS BETWEEN BS 360 AND BS 377, BL0. REMOVED CORROSION ON FLOORBEAM STRUCTURAL SUPPORT IN SEVERAL LOCATIONS BETWEEN BS 360 & BS 377, BL 0 IAW SRM 53-00-51. GREATEST MATERIAL LOSS MEASURE 1.0" X 0.8" X .015" & FOUND OUT OF LIMITS ON ORIGINAL MATERIAL THICKNESS OF .063" IAW SRM 53-00-51, DETAIL III. R & R FLOORBEAM STRUCTURAL SUPPORT IAW SRM 51-40-02, PAGE 6-7 & DWG 141N5191.
Part: FRAME — DENTED (BS 660) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 660 STR 23-25L, FRAME DENTED SEVERAL PLACES. REPAIRED FWD CARGO FRAME AT STA 660, STR 23L-25L BY INSTALLING. REPAIR DOUBLER ON FRAME AT BS 660 BETWEEN STR 22L- 26L, REF SRM 53-00-07, REPAIR 5, FIG 201, PG 208, TRIMOUT 4 EA ON FRAME: 1.140" X 1.040" X 0.5"R, 1.140" X 1.040" X 0.5"R, 1.140" X 1.040" X 0.5" R, 4.140" X 1.040" X 0.5" R. REPAIR IS PERMANENT CAT "B" ON ZONE 2 WITH THRESHOLD INSPECTION TO START AT OR BEFORE 42657 F/C & REPEAT INSPECTION EVERY 11000 F/C. THEREAFTER USING, HFEC, HIGH FREQUENCY EDDY CURRENT & DETAILED INSPECTION IN REF SRM 53-00-07, REPAIR 5, FIG 201, TABLE II, PAGE 210. ACFT IS CURRENTLY AT 17657 F/C.
Part: FLOORBEAM — CORRODED (BS 1460) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO UNDER FLOOR FRAME BS 1460 LOWER SUPPORT ANGLE HAS CORROSION AT LT OF STR S-30. AFT CARGO UNDER FLOOR FRAME BS 1460 LOWER SUPPORT ANGLE AT LT OF STR S-30. CORROSION OUT OF LIMIT IAW SRM 53-00- 53, FIG 101. R & R ANGLE PN 140N2002. BATCH 00028423304 IAW SRM 51-40-02, PG 2 AND DWG 146N1014, ORIGINAL MATERIAL .050", MATERIAL LOSS 1.0" X 1.0" X .015".
Part: SEAT TRACK — NOT REPORTED (BS 539) · airframe 29,601 hrs · 17,657 cycles
WHILE WORKING CARD 2021-2075 FOUND SEAT TRACK OUT OF LIMITS AT BS 539.2 RT OTBD. TRIMMED-OUT DAMAGED SECTION OF SEAT TRACK FROM BS 510-570, RT OTBD & SPLICED-IN A NEW SECTION BY ACCOMPLISHING A PERMANENT SPLICE REPAIR IAW SRM 53-00-52, REPAIR 3, FIG 201.
Part: SEAT TRACK — CORRODED (BS 1640) · airframe 29,601 hrs · 17,657 cycles
CABIN FLOOR SEAT TRACK FLANGE HAS CORROSION AT BS 1640, RBL 25. REMOVED CORROSION ON 2 EA AREAS AT MAIN CABIN FLOOR SEAT TRACK FLANGE BS 1640, RBL 25 IAW SRM 53-00-52, FIG 101 WITH DIMENSIONS AREA1 L=1"X .7" AREA 2 L=2.5"X .9" AND MATERIAL LOSS 0.016" AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. REMOVED, FABRICATED AND REPLACED SEAT TRACK SUPPORT SECTION ON MAIN CABIN FROM BS 1600-BS 1640 AT RBL 25 IAW DWG 146N5120 AND SRM 51-40-02, PAR 7, ORIG THICKNESS .070".
Part: SEAT TRACK — DAMAGED (BS 564) · airframe 29,601 hrs · 17,657 cycles
WHILE WORKING CARD 2021-2072, FOUND SEAT TRACK OUT OF LIMITS AT BS 564.8, LT OTBD TRACK. TRIMMED DAMAGED SECTION ON SEAT TRACK FROM BS 490 TO BS 570 LT OTBD LBL 45 IAW SRM 53-00-52, REP 3. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-52, REP 3 BY SPLICING-IN A NEW SECTION OF SEAT TRACK. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: CREASE BEAM — CORRODED (BS 729-740) · corrosion level 2 · airframe 29,601 hrs · 17,657 cycles
MAIN CABIN-CORROSION ON RT INNER CREASE CHORD BETWEEN BS 729.6 AND BS 740, RBL 65. REMOVED CORROSION AT RT INNER CREASE BEAM BETWEEN BS 729-740, RBL 65, MATERIAL ORIGINAL THICKNESS .080", MATERIAL LOSS .051", FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL III ALLOWABLE DAMAGE 1, W=0.50", L=0.50", D=0.051". R & R RT INNER CREASE BEAM CHORD FROM BS 664-, BS 756, RBL 65 IAW SRM 51-40-02, FIG 4, PG 20, PG 6. PARA 7.D AND DWG 143N8322.
Part: CREASE BEAM — CORRODED (BS 1323) · corrosion level 2 · airframe 29,601 hrs · 17,657 cycles
L3 DOOR LOWER SILL INBD CREASE BEAM HAS CORROSION AT BS 1323. BLENDED CORROSION AT BS 1326 ON L3 DOOR LWR SILL INBD CREASE BEAM. FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL III. R & R PART IAW SRM 51-40-02, FIG 8 & DWG 146N8326.
Part: SEAT TRACK — DAMAGED (BS 630-632) · airframe 29,601 hrs · 17,657 cycles
WHILE WORKING CARD 2021-2069, FOUND SEAT TRACK OUT OF LIMITS AT BS 630-632 LT. TRIMMED OUT DAMAGED SECTION OF SEAT TRACK FROM BS 610.45 TO BS 640, LBL 24 IAW SRM 53-00-52. REPAIR 3 & ACCOMPLISHED A PERMANENT SPLICE REPAIR BY SPLICING-IN, INSTALLING, A NEW SEAT TRACK IAW SRM 53-00-52, REPAIR 3, FIG 201, OPTION 2.
Part: SEAT TRACK — DAMAGED (BS 1360-1362) · airframe 29,601 hrs · 17,657 cycles
WHILE WORKING CARD 2021-2080 FOUND SEAT TRACK OUT OF LIMITS AT BS 1360-1362 RT INBD. TRIMMED-OUT DAMAGED SECTION OF SEAT TRACK RT INBD BETWEEN BS 1320 TO BS 1370 IAW SRM 53-00-52, REPAIR 3. ACCOMPLISHED A PERMANENT SPLICE REPAIR & INSTALLED A NEW SECTION OF SEAT TRACK IAW SRM 53-00-52, REPAIR 3, FIG 201.
Part: FRAME — DENTED (BS 680) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 680 STRINGERS 23-25R, FRAME DENTED. REPAIRED IAW SRM 53-00-07, REPAIR 5.
Part: FRAME — DENTED (BS 1520) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO FRAME AT BS 1520 DENTED ABOVE S26L. REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.
Part: FRAME — DENTED (BS 1460) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO FRAME AT BS 1460 DENTED ABOVE S26L. REPAIRED IAW SRM 53-00-07, REPAIR 5.
Part: FRAME — DENTED (BS 1320) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO FRAME BS 1320 DENTED. REPAIRED IAW SRM 53-00-07, REPAIR 5 .
Part: FRAME — DENTED (BS 580) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 580, STR 22-24L, FRAME DENTED. TRIMMED-OUT DENTS & ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-07, REPAIR 5.
Part: FRAME — DENTED (BS 1420) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO FRAME AT BS 1420 HAS DENT ABOVE S26L. TRIMMED-OUT THE DENT AND REPAIRED IAW SRM 53-00-07, REPAIR 5, DET I.
Part: FRAME — DENTED (BS 1480) · airframe 29,601 hrs · 17,657 cycles
AFT CARGO FRAME AT BS 1480 HAS DENTS ABOVE S26L. DENTS WERE TRIMMED AND REPAIRED IAW SRM 53- 00-07, REPAIR 5, FIG 201.
Part: STRAP — DAMAGED (BS 540-560) · airframe 29,601 hrs · 17,657 cycles
FWD CARGO BS 540-560/LBL 25, FLOORBEAM STABILIZATION STRAP DAMAGED FROM CONTACT WITH CARGO CEILING PANEL ATTACH SCREWS. REMOVED DAMAGED SECTION OF FLOORBEAM STABILIZATION STRAP AT BS 540-560, LBL 25 & ACCOMPLISHED A PERMANENT SPLICE REPAIRS IAW SRM 53-00-51, REPAIR 13. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: SKIN — DENTED (RT WING LE SLAT) · airframe 29,601 hrs · 17,657 cycles
RIGHT WING, NR 8 SLAT T/E WEDGE UPPER SKIN HAS APPROXIMATELY 1" DENT MIDSPAN. MEASURED DENT AND FOUND DENT TO BE WITHIN LIMITS IAW SRM 57-43-02 ALLOWABLE DAMAGE 1, NOTE "J", DETAIL III. DENT, ON NR 8 SLAT T/E WEDGE UPPER SURFACE, MEASURES 1.544" WIDE AND .025" DEEP, A/Y=61.76. NO CRACK NOTED. INSTALLED ID TAG IAW PS 900-5-1, NR 04. ESTABLISHED DENT DECAL MONITOR IAW TOPPS 30-10-70, PAGE 13.