N865AA
Registered owner: ANDURIL INDUSTRIES INC, CA (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.
47 reports on file, 1995-08-05 – 2001-01-30.
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND CRACK INDICATED IN OUTERSKIN BETWEEN RIVET AND DOOR RADIUS LOWER AFT CORNER, 420. INSTALLED REPAIR DOUBLER AT FORWARD GALLEY DOOR CUTOUT LOWER AFT CORNER IAW SERVICE BULLETIN 727-53-018 FIG 2. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION IN STRINGER 28R STATION 965-973. INSTALED NEW STRINGER SECTION AND REPAIR SPLICE PER ESO 11697 DATED 1-25-01. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION IN CENTER OF STRINGER 27R STATION 738-739. CUT OUT DAMAGED AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION IN CENTER OF STRINGER 27R STATION 704-705. REMOVED STRINGER AND SPLICE. INSTALLED NEW STRINGER AND SPLICE PER SRM 53-10-03. (M)
Earlier reports · 1995–2000 · 43 reports
2000
Part: SMOKE — DETECTED (CABIN)
DFW - FLT 1184 - APPROXIMATELY 15 MINUTES AIRBORNE AND LEVEL AT FL190, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. DECLARED EMERGENCY, RETURNED DFW AND LANDED WITHOUT INCIDENT. SMOKE AND HAZE DISAPPEARED WHEN SMOKE IN CABIN/REMOVAL PROCEDURE EXECUTED AT TIME OF SMOKE BOTH WING AND ENGINE HEAT WERE ON. EXTENSIVE GROUND TEST PERFORMED. UNABLE TO DUPLICATE PROBLEM. PACK BURNOUT ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — BROKEN (CABIN)
DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHT AT A SEAT 14D INOPERATIVE. REPAIRED LIGHT STRIP AT SEAT 14D. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CONNECTOR — LOOSE (AFT AIRSTAIR)
DFW DURING OVERNIGHT MAINTENANCE AFT AIR STAIR EMERGENCY LIGHT INOPERATIVE. RECONNECTED CONNECTOR ON AFT AIRSTAIR EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION.
1999
Part: CASTING — CRACKED (HORIZ STABILIZER)
TUL - RIGHT STABILIZER HINGE CASTING CRACKED. ABOUT 1.50 INCHES LONG. REMOVED CRACKED AREA PER SRM 55-10-4. INSTALLED DOUBLER PLATE PER SRM 55-10-4. TST: 62,106 HOURS. CYCLES: 37,887. (X)
Part: SKIN — GOUGED (BS 320)
TUL - APPROXIMATE STA 320 CROWN SKIN GOUGED AT STR 4L. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-30-3 FIG 14. (DOUBLER AND FILLER). AUTHORIZED BY ESO 11697 DATED 12-14-99. TST: 62,106 HOURS. CYCLES: 37,884. (X)
Part: SKIN — CRACKED (VERT STABILIZER)
TUL - CRACK IN VERTICAL STABILIZER SKIN LEFT AT BOTTOM APPROXIMATE STA 1343. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 727-55-82 AND ESO 11697 DATED 12-10-99. TST: 62,106 HOURS. CYCLES: 37,884. (X)
Part: SPAR — CORRODED (VERT STABILIZER)
TUL - CORROSION AT LEFT REAR SPAR CAP 2 PLACES BETWEEN NR 4 AND NR 5 HINGES. INSTALLED REPAIR IAW ESO 11697 DATED 12-8-99. TST: 62,106 HOURS. CYCLES: 37,884. (X)
Part: STRINGER — CRACKED (BS 950)
TUL - STRINGER 18A CRACKED OUTBOARD SIDE OF LEFT MLG WHEELWELL. CUT STR 18A 36 INCHES FORWARD OF STA 950 AND REPAIRED PER SB 727-53-0172 IAW SRM 53-30-3 SB REPAIRS. TST: 62,106 HOURS. CYCLES: 37,884. (X)
Part: LIGHT — DEFECTIVE (AFT AIRSTAIRS)
TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ACTUATOR — BROKEN (NR 8 SPOILER)
ORD - FLT 515 - ON APPROACH TO ORD FROM EWR, AIRCRAFT ROLLS RIGHT WITH FLAPS AT 25 DEGREES. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED NR 8 GROUND SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SHEAR TIE — CORRODED (BS 1000-1020)
TUL - SHEAR TIE CORRODED BETWEEN STRINGER 29L AND STRINGER 30. CUT OUT CORRODED LEG SHEAR TIE. FABRICATED AND INSTALL REPAIR ANGLE SRM 53-10-4. (M)
Part: SKIN — CORRODED (BS 1000-1020)
TUL - SKIN CORRODED BETWEEN STRINGER 29L AND STRINGER 30 BOTH SIDES. CUT OUT CORRODED DAMAGED AREA. FABRICATED REPAIR DOUBLER SRM 53-30-3. (M)
Part: SHEAR TIE — CORRODED (BS 1130)
TUL - SHEAR TIE CORRODED STATION 1130 BETWEEN STRINGER 29 LEFT AND STRINGER 30 AFT CARGO REF E58-0132199. REMOVED AND REPLACED WITH NEW SHEAR TIE SUPPORT ANGLE IAW CH SRM 51-30-3. (M)
Part: SPLICE — CORRODED (BS 1000-1020)
TUL - SPLICE STRAP CORRODED BETWEEN STRINGER 29L AND STRINGER 30. CUTOUT CORRODED SPLICE STRAP AND REPAIRED PER ESO 11697 DATED 1/8/99.
Part: STRINGER — CORRODED (BS 1151-1156)
TUL - FOUND STRINGER 30 CORRODED FROM STATION 1151 TO STATION 1156. INSTALLED .090 J-DOUBLER OF 7075-T6 STRINGER 30 STATION 1148-1158 WITH 5 FASTENERS EACH SIDE OF DAMAGE PER 53-10-3 SRM. (M)
1998
Part: SKIN — CRACKED (BS 310)
TUL - SKIN CRACKED AT FOWARD ENTRY DOOR LOWER HINGE CUT OUT. CUT OUT CRACK, INSTALLED FILLERS AND DOUBLER IAW SB 727-53-0198. TST: 57,178 HOURS. CYCLES: 35,293. (X)
1997
Part: LENS — MISSING (GALLEY)
RDU - DURING OVERNIGHT CHECK, FORWARD GALLEY SERVICE DOOR EMERGENCY EXIT SIGN LENS COVER WITH ARROW MISSING. REPLACED FORWARD GALLEY SERVICE DOOR EMERGENCY EXIT SIGN LENS COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRINGER — CORRODED (BS 686)
TUL - STR 10 FOUND WITH CORROSION AT BS 686. STOP DRILLED CRACK IN WS 10 AND INSTALLED REPAIR PER SB 727-57A159, FIG 18. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: SKIN — CORRODED (BS 580/600)
TUL - CORROSION ON SKIN IN FORWARD CARGO. CUT OUT CORROSION AND INSTALLED .100 INCH DOUBLER PER 53-30-3. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: STRINGER — CORRODED (BS 680/694)
TUL - CORROSION INSIDE STR 27R. REMOVED CORROSION PER SRM 51-10-6 AND INSTALLED STRINGER REPAIR EPR SRM 53-10-3 PAGES 3 THROUGH 4B. TST: 54,635 HOURS. CYCLES, 33,952. (X)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER 15R CRACKED FORWARD RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-3. (M)
Part: BELL FRAME — CRACKED (BS 930)
TUL - BELL FRAME CRACKED STA 930, S14R. INSTALLED BELL FRAME REPAIR PER ESO 11697 DATED 12/30/96. TST: 54,635 HOURS. CYCLES, 33,952. (X)
Part: SKIN — CORRODED (BS 700/720)
TUL - CORROSION ON SKIN IN FORWARD CARGO. CUT OUT CORROSION AND INSTALLED DOUBLER PER 53-30-3. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: SKIN — CORRODED (BS 480-485)
TUL - FOUND CORROSION ON INNER FUSELAGE SKIN, STATION 480-485, STRINGER 27L-28L. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-13 PAGE 14D. (M)
Part: SKIN — CORRODED (BS 351-360)
TUL - FOUND CORROSION AT ANGLES, BRACKETS FASTENERS AND SKIN ON AFT OF NLG SHELF, STATION 351-360, LWR EXT RECESS ANGLES CORROSION OUT OF LIMITS. REMOVED CORROSION FROM SHELF TREATED AND PRIMED AREA. REPLACED ANGLES. (M)
Part: STRINGER — CORRODED (BS 680/690)
TUL - CORROSION INSIDE STR 26R, FS 680 TO FS 690. CUT OUT DAMAGED SECTION OF STRINGER REPAIR AT STR 26R STA 680 - STA 690 PER SRM 53-10-3. TST: 54,657 HOURS. CYCLES, 33,951 (X)
Part: SKIN — CORRODED (BS 710)
TUL - CORROSION ABOVE STR 26R, STA 710 AT SKIN LAP. INSTALLED DOUBLER PER SRM 53-30-3. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: SHEAR TIE — CORRODED (BS 720)
TUL - CORROSION ON SHEAR TIE STA 720 BETWEEN STR 25 - STR 26R. REMOVED CORRODED SHEAR TIE AND REPLACED. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: STRINGER — CORRODED (BS 620-630)
TUL - CORROSION IN AND ON STRINGER 27R FROM STATION 620 TO STATION 630. REMOVED CORROSION, REPAIRED FUSE STRINGER PER SRM 53-10-3 FIG 1. (M)
Part: STRINGER — CORRODED (BS 580/600)
TUL - STR 28L BETWEEN STA 580 - STA 600 HAS CORROSION ON OUTBOARD LEG. REMOVED CORROSION. REPAIRED PER SRM 53-10-3, FIGURE 2. TST: 54,657 HOURS. CYCLES, 33,951. (X)
Part: DOOR FRAME — CORRODED (BS 378)
TUL - FORWARD GALLEY DOOR FRAME CORRODED. REMOVED AND REPLACED INSTALLED REPAIR PER SRM 51-40-3. (M)
1996
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER CRACKED ON FLANGE. REPAIRED STRINGER PER SRM 53-10-31. (M)
Part: FLOORBEAM — CORRODED (BS 344)
TUL - CORROSION ON TOP OF FLOORBEAM. REMOVED CORROSION AND REPAIRED PER SRM 53-10-8. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER CRACKED AT FLANGE AREA. REPAIRED STRINGER PER 53-10-31. (M)
Part: HAT CHANNEL — CORRODED (BS 1135)
TUL - HAT CHANNEL FLANGES CORRODED THROUGHOUT LENGTH OF CHANNEL 4 INCH BY 39 INCH PIECE CHANNEL. REPLACED HAT CHANNEL. (M)
Part: HAT CHANNEL — CORRODED (BS 1135)
TUL - HAT CHANNEL FLANGES CORRODED THROUGHOUT LENGTH OF CHANNEL, 4 INCH BY 39 INCH PIECE CHANNEL. REPLACED HAT CHANNEL. (M)
Part: FLOORBEAM — CORRODED (BS 380)
TUL - CORROSION TOP OF MAIN FLOORBEAM, STATION 380 RBL 40 AND RBL 65. REMOVED CORROSION, REPAIRED AFFECTED AREAS WITH DOUBLERS PER SRM 53-10-07-2. (M)
Part: SKIN — CORRODED (BS 720)
TUL - SKIN BELOW STRINGER 26L BETWEEN STA 720E-720F CORRODED, LEVEL 2 DEGREE. INSTALLED DOUBLER PER SRM 53-30-3. (M)
Part: CONNECTOR — BROKEN (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT FORWARD PART AND MID PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: DUCT — RUPTURED (NR 2 ENGINE)
DFW - FLT 0471 - DURING MAXIMUM POWER TAKEOFF FROM ATL, AFT BODY OVERHEAT LIGHT ILLUMINATED. WHEN POWER WAS REDUCED, LIGHT EXTINGUISHED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE NOSE COWL ANTI-ICE DUCT. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
Part: CONNECTOR — LOOSE (ROW 17D)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 17D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL STRIP — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION (M)