N848AA
Registered owner: AB PROP PLANE 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.
40 reports on file, 1997-01-02 – 2025-08-01.
Part: AIR BOX — CRACKED · airframe 249 hrs
AIRBOX SEALS BROKEN, WORN AND, CRACKED CAUSING BUTTERFLY VALVE TO FLUTTER AND CRACK WELD.
Earlier reports · 1997–2001 · 39 reports
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY AFT STAIRWELL LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN BETWEEN L1 AND R1 DOOR INOPERATIVE. RECONNECTED EMERGENCY SIGN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
TUL - FOUND AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE, STATION 1398. REPLACED LIGHT ASSEMBLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
TUL - AFT SLIDE LIGHTS INOPERATIVE, STATION 1143 EQUIP NR M983. REPLACED BATTERY PACK M983. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY SIGN BETWEEN L1 AND R1 INOPERATIVE. RECONNECTED EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (AFT AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SIGN AT AFT AIRSTAIRS DIM. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 3 EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 3 EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND STRINGER 26R HAS CORROSION ON SPLICE STATION 668-670. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND STATION 682-685 OUTBOARD SIDE STRINGER 26R CORRODED. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND STATION 700 FORWARD SIDE FRAME OUTBOARD STRINGER 26R SHEAR TIE CORRODED. REMOVED AND REPLACED CORRODED SHEAR TIE. (M)
Part: ANGLE — CORRODED (FUSLEAGE)
TUL - FOUND CORROSION ALONG LOWER AFT CARGO DOOR CUTOUT ANGLE, STRINGER 27 RT. REMOVED CORROSION BY BLENDING, INSTALLED STRAP REPAIR AS PER ESO 11697 DATED 1/6/2000. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND STATION 682-688 OUTBOARD SIDE STRINGER 26R SKIN CAP CORROSION. INSTALLED FUSELAGE SKIN DOUBLER PER SRM 53-30-3. (M)
Part: RIB — CRACKED (WING)
TUL - FOUND UPPER CHORD RIB CRACKED 1.5 INCH ABOVE OUTBOARD AILERON INBOARD HINGE CASTING, WBL 499. REPLACED UPPER T-CHORD PER BOEING SERVICE BULLETIN 727-57-16F. (M)
Part: SKIN — CORRODED (FUSELAGE)
TUL - FOUND OUTBOARD SIDE STRINGER 26R, SKINCAP CORRODED STATION 720D PLUS 8 TO 720E. CORROSION REMOVED BY CUTTING OUT AFFECTED AREA AND REPAIRED WITH STRINGER SPLICE AND DOUBLER PER SRM 53-30-3 AND 51-10-3. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT AFT OVERHEAD AIR STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT AFT OVERHEAD AIR STAIRS LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)
ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIR STAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — MISDRILLED (FUSELAGE)
TUL - FOUND A 1.5 INCH DIAMETER HOLE WAS MISDRILLED IN FLOORBEAM WEB AT RIGHT STATION 280. A REPAIR DOUBLER WAS INSTALLED PER ESO 11697, DATED 5/16/00. (M)
Part: TRUNNION — CORRODED (NLG)
TUL - FOUND LEFT AND RIGHT NLG TRUNNION FITTINGS (UPPER AND LOWER) AND CAPS CORRODED. REPAIRED TO FIRST OVERSIZE PER SRM 53-40-1 PAGE 1. (M)
1999
Part: RIB — CRACKED (WS 760)
TUL - LEFT 760.95 RIB CHORD ANGLE CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR KIT PER SB 57-0112. TST: 63,311 HOURS. CYCLES, 40,510. (X)
Part: LUG — CORRODED (HORIZONTAL STAB)
TUL - RIGHT OUTBOARD AND INBOARD LUGS FOR THE HORIZONTAL STABILIZER PIVOT BEARING CORRODED. BORED AND SPOT FACED, MANUFACTURED AND INSTALLED NEW BUSHINGS PER ESO 11697 DATED 11-11-99. TST: 63,321 HOURS. CYCLES: 40,522. (X)
Part: LIGHT — DEFECTIVE (AIRSTAIRS)
TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EXIT LIGHT ASSEMLBY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT SECTION IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ABOVE AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ABOVE AFT STAIRS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: PUMP — DEFECTIVE ('B' HYD SYSTEM)
JFK - FLT 1195 - AFTER TAKEFF JFK, HYDRAULIC SYSTEM 'B' INDICATED A QUANTITY LOSS. AIRCRAFT AIR INTERRUPTED AND RETURNED TO JFK AND LANDED WITHOUT FURTHER INCIDENT. FOUND SYSTEM 'B' ELECTRIC PUMP LEAKING FROM SHAFT. REPLACED PUMP, CHANGED FILTERS AND SERVICED SYSTEM. SYSTEM GROUND AND LEAKED CHECKED NORMAL OPERATION. (M)
1997
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15L CRACKED AT AFT SIDE OF WING ICE LIGHT FS 720B-720C. REMOVED AND REPLACED CRACKED STRINGER 15L PER SRM 53-10-3 FIG 1. (M)
Part: PRESSURE DECK — CRACKED (BS 286)
TUL - FOUND LEFT NOSE W/W TOP PANEL BETWEEN BL 4-5, STATION 286, 2 FASTENER HOLES CRACKED. CUT OUT DAMAGED HOLES, (2 EACH) FABRICATED DOUBLER AND FILLER, ALODINED AND PRIMED, INSTALLED DOUBLER FILLER AND REINFORCEMENT STRAPS PER ECO H 4087 DX. (M)
Part: SEAT TRACK — CORRODED (BS 440)
TUL - FOUND CORROSION AROUND FASTENERS IN THE RIGHT OUTBOARD SEAT TRACK AT STATION 440. REMOVED AND REPLACED RIGHT OUTBOARD SEAT TRACK, FS 344 TO 480 PER SRM 53-0-5. (M)
Part: FLOORBEAM — CORRODED (BS 1130)
TUL - FOUND CORROSION ON STATION 1130 FLOORBEAM LOWER CHORD LBL 39 TO RBL 52, AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-6, REPAIR PER ESO 11697. (M)
Part: PRESSURE DECK — CRACKED (BS 270-272)
TUL - RIGHT NOSE W/W TOP PANEL BL 14, STATION 270-272, 3 EACH FASTENER HOLES CRACKED. CUT OUT DAMAGED HOLES (3), FABRICATED DOUBLER AND FILLER, ALODINED AND PRIMED, INSTALLED DOUBLER AND FILLER AND REINFORCEMENT STRAP PER ECO H 4087DX. (M)
Part: SKIN — DAMAGED (BS 950)
TUL - STA 950E TO STA 950F, BETWEEN STR 25L AND STR 26L, FAIRING SEAL HAS WORN INTO FUSELAGE SKIN. NOTE: NDT READING HAS SKIN ORIGINAL THICKNESS AT .063 INCH. SKIN WORN BEYOND LIMITS. INSTALLED FLUSH DOUBLER PER SRM 53-30-3. TREATED AND PRIMED WEAR SURFACE WITH TEFLON PAINT.
Part: SKIN — DENTED (BS 1090/1110)
TUL - DENT IN FUSELAGE SKIN BETWEEN STR 18L AND STR 19L BETWEEN STA 1090 AND STA 1110. CUT OUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-30-3. TREATED, PRIMED, AND SEALED EDGES. TST: 55,616 HOURS. CYCLES, 36,623. (X)
Part: SKIN — CORRODED (BS 1000)
TUL - GOUGE IN FUSELAGE SKIN BEYOND LIMITS, APPROXIMATELY 16 INCHES AFT OF AFT CARGO DOOR AT STR 24R. AREA PREVIOUSLY BLENDED, DAMAGE APPROXIMATELY 4 INCHES LONG. INSTALLED DOUBLER. REF: 53-30-03. TST: 55,616 HOURS. CYCLES, 36,623. (X)
Part: SKIN — DENTED (BS 400/420)
TUL - FUSELAGE SKIN, SMALL DENT IN SKIN WITH SMALL SCRATCH BETWEEN STA 400 - STA 420, STR 24R AND STR 25R. DYE CHECKED AREA AND FOUND CRACKS. INSTALLED DIAMETER FLUSH REPAIR IAW SRM 53-30-3. TST: 55,616 HOURS. CYCLES, 36,623. (X)
Part: SKIN — DENTED (BS 1050)
TUL - FUSELAGE SKIN DAMAGE, DENT WITH SHARP CREASE AND WITH CRACK, STR 23R - STA 1050. INSTALLED DOUBLER REF 53-30-3. TST: 55,616 HOURS. CYCLES, 36,623. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15L CRACKED AT WING ICE LIGHT, FS 720B AND 720C IN TWO PLACES, AFT OF LIGHT. REMOVED AND REPLACE CRACKED STRINGER PER SRM 53-10-3, FIG 1. (M)
Part: PRESSURE DECK — CRACKED (BS 262-274)
TUL - FOUND 6 FASTENER HOLES CRACKED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND STRAPS IAW ECOH4087 DX. (M)