N816AT
Registered owner: SEMINOLE AIRCRAFT LLC, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ATP Flight School | Operator | on 2024-01-07 | Operator named in NTSB report |
Accident & incident history
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.
19 reports on file, 1999-01-01 – 2002-03-23.
Part: WIRE — CUT (TAIL CONE)
CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK, EMERGENCY PATH LIGHT WIRES WERE CUT OFF. REPAIRED WIRES L9045-20, L9054-20N, L9049-20 AND L9057-20N AT CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK EMERGENCY PATH LIGHT IAW WDM 33-51-03 AND MM 20-50-1. OPS CHECK NORMAL IAW MM 33-50.
Earlier reports · 1999–2001 · 18 reports
2001
Part: ENGINE — FAILED (NR 2)
ON CLIMBOUT CAPTAIN REPORTED NR 2 ENGINE PARAMETERS ACCELERATED WITH N1/N2 CLIMBING THRU 99 PERCENT AND EGT AT 750C FOR 30 SECONDS. SHUT DOWN ENGINE AND SECURED AIRCRAFT FOR ENGINE OUT APPROACH. REMOVED AND REPLACED NR 2 ENGINE DUE TO EGT LIMITS EXCEEDING TEMPERATURE AND TIME LIMIT PER P&W 72-00-00.
2000
Part: LIGHT — INOPERATIVE (CABIN)
FOUND FLOOR PATH LIGHTS AND NACELLE EMERGENCY LIGHTS OUT. TIGHTENED TERMINAL B2 ON FORWARD ATT SWITCH. REMOVED AND REPLACED RIGHT BATTERY PACK AND CHARGED LEFT BATTERY PACK IAW DC9 MM 33-51-01.
Part: DOOR FRAME — CRACKED (FUSELAGE)
DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL, FOUND FORWARD ENTRANCE DOOR AFT TOP DOOR STOP BOLT HOLES CRACKED. INSTALLED REPAIR DOUBLER IAW RES 00-0408.
Part: KEELBEAM — CRACKED (FUSELAGE)
DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL., FOUND KEEL BEAM WEB CRACKED AT BS 700 AFT OF GEAR DOOR ACTUATOR. INSTALLED REPAIR IAW RES 00-00441.
Part: SKIN — DAMAGED (FUSELAGE)
DURING A SCHEDULED INSPECTION AT AVBORNE IN MIAMI FL., FOUND PREVIOUS REPAIR AT STATION 218 LEFT BELOW LONGERON 15. REPLACED PREVIOUS REPAIR IAW RES 00-0439.
1999
Part: INTERCOSTAL — MISDRILLED (BS 370-375)
SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT AT STA 370 TO STA 375 L-29R INTERCOASTAL UPPER FLANGE AND WEB HAS MISDRILLED FASTENER HOLES. FABRICATED NEW INTERCOASTAL, FIT, DRILLED, TREATED AND PRIMED. LOCATED NEW WEB, DRILLED, DEBURRED AND INSTALLED IAW DC9 SRM 51-10-2A, 51-10-4, 51-10-3, 51-30-2, AND RES NR 99258. INTERCOASTAL P/N OFF 1A-49049-1.
Part: SUPPORT — CRACKED (BS 351-370)
SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FORWARD CARGO COMPARTMENT STA 351 TO STA 370 L-29L INTERCOASTAL BENT, AND FLOOR SUPPORT WAS FOUND CRACKED. REMOVED AND FABRICATED NEW INTERCOASTAL, RECEIVED NEW SUPPORT, DRILLED, AND INSTALLED BOTH PARTS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-5, 53-10-2, AND RES NR 99337. LONGERON P/N OFF 1A-42075-1.
Part: SKIN — CREASED (BS 484 & 955)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CREASE OUT OF LIMITS AT STA 484 RIGHT SIDE L-19-20. ALSO, A COAX CABLE STAND OFF BROKEN AT STA 955 ABOVE L-20R. TRIMMED OUT CREASE, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 53-04 FIG 12B, AND RES NR 99293. ALSO, REMOVED, REPLACED AND FABRICATED NEW STAND OFF AT STA 955 (P/N 1A-42054) IAW DC9 SRM 51-10-4, 51-10-2, 51-30-2 AND RES NR 99255.
Part: SKIN — DENTED (VENTRAL STAIR)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUMEROUS DENTS IN AFT VENTRAL STAIRS LOWER AFT SKIN FROM SPLICE. REMOVED AND REPLACED EXISTING SKIN FROM PREVIOUS SPLICE IAW DC9 SRM 51-10-4, 51-30-2, AND RES NR 99221.
Part: CUSP — CORRODED (BS 945 & 965)
SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON CUSP MEMBRANE AT RIGHT OUTBOARD STA 945 AND STA 965 CUSP A7. REMOVED CORROSION AND FABRICATED DOUBLERS AND FILLER IAW DC9 SRM 51-30-2, 51-10-3, 53-20-1. DOUBLER (P/N 1A-42076-1) OFF.
Part: DOUBLER — CORRODED (BS 937)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGED AT STA 937 L-26R. MECHANICALLY REMOVED CORROSION, FASTENERS AND DOUBLER. FABRICATED AND INSTALLED FASTENERS, DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 51-20-0, AND RES NR 99301.
Part: LONGERON — CORRODED (BS 237, 560, 579)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON LONGERONS AT STA 237 L-30 AND STA 560 TO STA 579 L-30. ALSO, CORRODED RIVETS AT T-CAP AT STA 598 L-24L TO L-24R. REMOVED AND REPLACED FASTENERS ON T-CAP, TREATED CORROSION, CUT OUT DAMAGE LONGERON SECTION, FABRICATED ANGLES, SPLICES, FINGER DOUBLERS AND INSTALLED IAW DC9 SRM 53-02 FIG 14, 51-10-3, 51-10-5, 53-02 FIG 2A, 51-30-2, 53-11-3, 51-10-2, AND 53-01 FIG 1. ANGLES AND SPLICE (P/N 1A-42057-1, 2) (P/N 1A-42056-1), (P/N 1A-42059-1).
Part: STRUCTURE — CORRODED (FUSELAGE)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FORWARD AND AFT CARGO COMPARTMENT. LOCATIONS ARE AS FOLLOW: CARGO DOOR FRAME LOWER EDGE AT STA 340 TO 427, FRAME STA 522 L-28L TO L-28R, AFT CARGO WEB STA 870 L-29R ON LEFT AND RIGHT SIDE, AFT CARGO FRAME (SHEAR TIE) AFT SIDE STA 887 L-27L TO L-29R, AND AFT CARGO FRAME STA 965 L-28L TO L-28R AFT SIDE. MECHANICALLY REMOVED CORROSION, FABRICATED AND FORMED DOUBLERS, FRAME, INTERCOSTAL, ANGLES, CLIPS, SPLICE AND PLATES. HEAT TREATED, DRILLED, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-10-3, 51-30-2, 51-30-5, 53-03 FIG 2A, 51-10-2A, 53-11-3 FIG 12. SPLICE (P/N 1A-42022-1) OFF, (P/N 1A-42021-1), (P/N 1A-42020-1).
Part: SKIN — CRACKED (BS 69.5)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON UPPER NOSE SKIN RIGHT SIDE AT STA 69.5 AT SECOND FASTENER JUST TO THE RIGHT OF PREVIOUS REPAIR. REMOVED EXISTING FILLER, FASTENERS, ENLARGED EXISTING CUTOUT TO REMOVED CRACK, FABRICATED, TREATED, PRIMED, AND INSTALLED FILLER WITH WET SEALER IAW DC9 SRM 51-10-4, DOUGLAS DRAWING SR09530239 REVISION A AND SERVICE BULLETIN 53-262.
Part: STRUCTURE — CORRODED (FUSELAGE)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION, DELAMINATION AND ELONGATED HOLES. FIRST, AT THE FORWARD CARGO SIDE WALL STRAPS (4 EACH) AND THRESHOLD DOOR STRAP (AFT SIDE) CORRODED AND ENLONGATED HOLES. SECOND, AT THE E/E COMPARTMENT AFT BULKHEAD LOWER FRAME L-28L TO L-28R. THIRD, AT THE RIGHT SIDE ELEVATOR GEAR TAB CORRODED AND DELAMINATED AROUND HINGE BRACKET HOLES. REMOVED, REPLACED, FABRICATED, LOCATED AND DRILLED STRAPS AND ANGLE, DEBURRED, TREATED, PRIMED, PAINT, INSTALLED ALL PARTS AND NEW ELEVATOR GEAR TAB IAW DC9 SRM 51-21-0, 51-10-2, 51-10-3, 53-21-0, 51-30-1, 53-01 FIG 1, 51-10-4 AND MM 27-30-4. GEAR TAB (P/N 5910414-502).
Part: FRAME — CRACKED (BS 718)
SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT MAIN FRAME LOWER FORWARD POCKET AND LOWER FLANGE IN THE WHEEL WELL AT STA 718 CRACKED. REMOVED AND REPLACED MAIN FRAME IAW EO 12-5511-29-B1044, EO 12-5511-29-B1044, AND SB 53-131 R4. FRAME (P/N 9919619-504N) OFF.
Part: FRAME — CRACKED (BS 718)
SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CRACK AT MAIN FRAME STA 718 RUNNING THROUGH 2 EA FASTENERS IN THE FORWARD INMEDIATE POCKET. REMOVED FITTING, DRILLED UP NEW FITTING, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5, MM 25-22-0, AND RES NR 9924 E/O 12-5311-29-B1044.
Part: SPLICE — CRACKED (WS 290)
SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WING STA XOS 290.0 LEADING EDGE SKIN SPLICE CRACKED. REMOVED AND REPLACED SPLICE PLATE, FABRICATED SPLICE PLATE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2 AND RES NR 99199.