N847AA
Registered owner: AB PROP PLAN I LLC, LA (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.
27 reports on file, 1995-05-27 – 2025-09-16.
Part: AIR BOX — CRACKED (ENGINE) · airframe 439 hrs
AIRBOX FAILURE. SEALS MISSING AND CRACKED WELD
Earlier reports · 1995–2000 · 26 reports
2000
Part: CONNECTOR — LOOSE (CABIN)
DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD AISLE LIGHT FORWARD STATION BS 350 INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY EXIT OVERHEAD AISLE LIGHT FORWARD STATION BS 350. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WEB — CRACKED (BS 950)
TUL - HFEC INDICATES CRACK IN UPPER PRESS DECK AT BEAD FORWARD OF STATION 950, OUTBOARD MOST BEAD. REPAIRED PER ESO 11697, DATED 7-21-99. (M)
Part: SKIN — CRACKED (BS 640-660)
TUL - FOUND CRACKS AT 2 FASTENER HOLES BELOW STRINGER 4R AT SKIN LAP BETWEEN 640-660. CUT OUT DAMAGE 653-660. HFEC'D CUT OUT AREA NO FURTHER CRACKS INSTALLED .080 2024T3 DOUBLER USING EXISTING FASTENER SPACING PER SRM 53-30-03 PAGE 2023. (M)
Part: SKIN — CRACKED (BS 507-512)
TUL - FOUND CRACKS AT TWO EACH FASTENER HOLES BELOW STRINGER 4R AT SKIN LAP BETWEEN 500-520. CUT OUT DAMAGE 507-512, HFEC'D AREA, NO FURTHER CRACKS. INSTALLED .080 2024 T-3 DOUBLER USING EXISTING FASTENER SPACING PER SRM 53-30-03 PAGE 20-23. (M)
Part: SKIN — CRACKED (BS 610-630)
TUL - FOUND CRACKS AT 2 FASTENER HOLES BETWEEN 600 PLUS 620 STRINGER 4R CRACKS AT 2 FASTENER HOLES BETWEEN 620 AND 640, STRINGER 4R. CUT OUT DAMAGE 610-630, HFEC'D AREA. NO CRACKS BEYOND CUTOUT. INSTALLED .080 2024T3 DOUBLER USING EXISTING FASTENER SPACING PER SRM 53-30-03 PAGE 20-23. (M)
Part: LIGHT — LOOSE (RT EMERG EXIT)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT RIGHT OVERWING EXITS INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY LOOSE. TIGHTENED LOOSE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: STRINGER — CORRODED (BS 1148-1160)
TUL - FOUND STRINGER 30 CORRODED ON RT SIDE AFTER STATION 1148 TO 1160. REMOVED CORRODED AREA OF STRINGER 30. INSTALLED FILLER AND STRINGER SPLICE AT STRINGER 30, STA 1148 TO 1160 PER SRM 53-10-3 PAGE 4B. (M)
Part: SPAR — CRACKED (BS 865)
TUL - FOUND CRACK IN REAR SPAR OF NR 2 FUEL TANK CENTER SECTION AT RBL 20 INCH IN RADIUS OF WEB AT TOP CHORD ANGLE. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 8-6-98. (M)
Part: FRAME — CRACKED (BS 1130)
TUL - TOP OF FRAME AT STATION 1130 CRACKED AREA 27R. SCREW DRIVER TURN FRAME AT STATION 1130 STRINGER 27R. CUT OUT DAMAGED AREA IN UPPER FLANGE OF 1130 FRAME. FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED IAW SRM 51-40-3 2653538. PREPARED AND PLUGGED HOLE IN FRAME IAW SRM 53-10-1. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY INOPERATIVE. REPLACED EMEREGNCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AFT STAIR)
DTW - DURING MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: WIRE HARNESS — DEFECTIVE (NLG)
DFW - FLT 2002 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT FLICKERED. VISUALLY CONFIRMED NLG DOWN AND LOCKED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NLG WIRE BUNDLE. ACCOMPLISHED NLG RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SPLICE — SEPARATED (NLG)
MCO - FLT 2010 - DURING APPROACH TO MCO AFTER LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT FLICKERED. VISUALLY CONFIRMED NLG DOWN AND LOCKED AND AIRCRAFT LANDED MCO WITHOUT INCIDENT. REPLACED NLG WIRE SPLICE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SPLICE — SEPARATED (NLG)
ORD - FLT 0448 - DURING APROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. VISUALLY CONFIRMED NLG DOWN AND LOCKED AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED SPLICE ON NLG DOWNLOCK SWITCH. ACCOMPLISHED NLG RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (CABIN)
ATL - DURING OVERNIGHT CHECK, AFT STAIRS OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRS OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: FRAME — CRACKED (BS 930)
TUL - FOUND CRACK IN FRAME STATION 930R AND STRINGER 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER WITH HI-LOC AND SEALER SRM 53-10-2 DOUBLER 7075-T6. (M)
Part: STRINGER — CRACKED (BS 656.5)
TUL - 5TH STRINGER AFT TANK STATION 656.5 TOP OF THE CHORD ANGLE FOUND CRACKED. INSTALLED 'Z' ANGLE REPAIR PER SRM 57-10-4. (M)
Part: SKIN — CORRODED (BS 460-1030)
TUL - FOUND CORROSION UNDER SKIN AT RIGHT STRINGER 14 LAP, FROM STATION 460-1030. REMOVED FASTENERS, CLEANED AND TREATED SKIN AND INSTALLED NEW FASTENERS PER 53-30-6 FIG 1, PAGE 11. (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION AROUND LEFT RAM AIR DOOR ACTUATOR SHAFT HOLE ON FUSELAGE SKIN AT STATION 720B INBOARD OF STRINGER 28L. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 PAGE 5 THROUGH 8 AND SRM 51-20-1, PAGE 12A. (M)
Part: STRINGER — CRACKED (WS 656.5)
TUL - FOUND TOP WING STRINGER 9 CRACKED AT RIB ATTACHMENT. REPAIRED DAMAGE AREA PER SRM 57-10-4 FIG 2, PAGE 4. (M)
Part: SKIN — CORRODED (BS 683)
TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER LEVELING COMPOUND OUTBOARD STATION 683, STRINGER 28R. INSTALLED OUTSIDE DOUBLER PER SRM 53-30-3 PAGE 14D. (M)
Part: FRAME — CRACKED (BS 930)
TUL - FOUND CRACK IN BELT FRAME AT STATION 930 BETWEEN STRINGER 13-12. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 2 PAGE 11. (M)
Part: FLOOR BEAM — CORRODED (BS 1130)
TUL - FOUND CORROSION ON TOP OF FLOOR BEAM STATION 1130 BETWEEN RIGHT, INBOARD AND OUTBOARD SEAT TRACK. REMOVED CORROSION PER SRM 51-10-6, REPAIRED FLOOR BEAM PER AARD/MS/MB CHAPTER 53-10-07-1 PAGE 1-3. (M)
Part: SHEAR TIE — CORRODED (BS 540)
TUL - FOUND SHEAR TIE CORRODED FORWARD OF STATION 540 OUTBOARD OF STRINGER 26R. REPLACED SHEAR TIE AT STATION 540, OUTBOARD OF STRINGER 26R. (M)
1995
Part: EEL STRIP — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS DIM AFT OF ROW 7. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT CLASS DIVIDER, REPLACED CENTER CAB CONTROL MODULE, AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)