N880AA
Registered owner: AEROCROP APPLICATORS LLC, OK (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.
61 reports on file, 1995-03-08 – 2001-08-24.
Part: SKIN — GOUGED (FUSELAGE)
TUL - FOUND GOUGE IN SKIN STATION 460 STRINGER 24L. CUTOUT DAMAGED AREA OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M)
Part: STRINGER — CORRODED (FS 460)
TUL - FOUND STRINGER 24L DENTED AT STATION 460. CUT AND REMOVED DAMAGED SECTION OF STRINGER. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-10-3. (M)
Part: WEB — CRACKED (FUSELAGE)
TUL - FOUND VERTICAL WEB OF RIGHT LOWER TORQUE BOX CRACKED APPROX STATION 1233 UPPER LIGHTENING HOLE. INSTALLED DOUBLER OVER DAMAGED AREA (AFTER ROUTING OUT CRACK) PER SRM 51-40-2. (M)
Part: LAMP — INOPERATIVE (R2 DOOR)
DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT R2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — INOPERATIVE (L1 DOOR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR DIM. REPLACED EMERGENCY EXIT LGIHT BATTERY PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 THROUGH 21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 55 reports
2000
Part: SKIN — DENTED (FUSELAGE)
TUL - FOUND FORWARD ENTRY DOOR CUT OUT FRAME DENTED AT LOWER HINGE. INSTALLED REPAIR DOUBLER AT LOWER HINGE IAW SB 727-0198. (M)
Part: SKIN — CORRODED (FUSELAGE)
TUL - FUSELAGE SKIN CORROSION AROUND RIVETS IN AFT CARGO STATION 1010-1020, STRINGER 28L-29R. REMOVED SECTION OF CORRODED SKIN AND INSTALLED DOUBLER AND PER RM 53-30-3 FIG 3A. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION 3 INCHES BY 2 INCHES, STRINGER 25R STATION 1148. REMOVED DAMAGE AREA OF STRINGER REPAIR PER SRM 55-10-3 FIG 1. 9M)
Part: BEAM — CORRODED (HORIZONTAL STAB)
TUL - FOUND LEFT HORIZ STABILIZER TRAILING EDGE BEAM HAD CORROSION AT STATION 160. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697, DATED 10/20/00. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON BOTTOM OF STRINGER 30 AT STATION 1013. REMOVED PREVIOUS STRINGER SECTION AND INSTALLED NEW SECTION, 11 INCHES, PER SRM 53-10-3. (M)
Part: SKIN — CORRODED (FUSELAGE)
TUL - FOUND CORROSION OUTBOARD OF STRINGER 27L ON SKIN. REMOVED CORROSION BY REMOVING DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
Part: LIGHT — INOPERATIVE (AFT AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED CONNECTOR ON AFT EMERGENCY EXIT FLOOR PATH LIGHTING SYSTEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1999
Part: CONNECTOR — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN INOPERATIVE. REPAIRED CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS BROKEN. REPAIRED FLAT WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: SKIN — CORRODED (BS 680-690)
TUL - FOUND CORROSION ON FUSELAGE SKIN OUTBOARD SIDE OF STRINGER 28R, STATION 680-690. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 .063 2024 PLUS 3, 21 INCHES BY 11 INCHES. (M)
Part: SKIN — DENTED (BS 1080)
TUL - DENT IN SKIN STATION 1080 STRINGER 19L. CUTOUT DENTED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M)
Part: SHEAR TIE — CRACKED (BS 600)
TUL - BELLFRAME SHEAR TIE CRACKED AND DEFORMED STA 600 ABOVE STRINGER 16R. REPAIRED SHEAR TIE PER SRM 53-10-4 AND SKIN PER 53-30-3. (M)
Part: SKIN — GOUGED (BS 415)
TUL - FOUND INNER SURFACE OF SKIN GOUGED STATION 415 BELOW STRINGER 9 LEFT. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 53-30-1 PAGES 1-8. (M)
Part: SKIN — CORRODED (BS 1082)
TUL - BULGE IN SKIN AT STRINGER 18L. CUT OUT BULGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M)
Part: FLOORBEAM — CORRODED (BS 1110)
FOUND CORROSION ON UNDERSIDE BS 1110 FLOORBEAM UPPER CHORD ADJ TO FASTENER COVERED BY GALLEY. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8 PAGE 9E. (M)
Part: STRINGER — CORRODED (BS 950-970)
TUL - FOUND CORROSION ON OUTSIDE OF STRINGER 29L STATION 950A TO 970. REMOVED CORROSION AND INSTALLED .071, 7075-T6 REPAIR STRAP PER ECO 11697 DATED 10-14-98. (M)
Part: SKIN — DAMAGED (HORIZ STABILIZER)
TUL - DEEP LIGHTNING BURN ON HORIZ STAB (LT) REAR SPAR AND SKIN. BLENDED SPAR AND REPAIRED PER SRM 55-10-3. (M)
Part: FLOORBEAM — CORRODED (BS 1070)
TUL - FOUND CORROSION ON FLOORBEAM AT STATION 1070, BL 0 - LBL 22. REMOVED CORRODED UPPER PORTION OF FLOORBEAM AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8. (M)
Part: STRINGER — CRACKED (BS 344)
TUL - FOUND STRINGER 5 RT CRACKED IN TWO PLACES UPPER FLANGES WHERE CLIP ATTACHES STATION 344. STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER SRM 53-10-3 PAGE 4C-6. (M)
Part: STRINGER — CORRODED (BS 687)
TUL - FOUND CORROSION INSIDE STRINGER CHANNEL BETWEEN RIVITS. INSTALLED STRINGER SPLICE SAME AS ORIGINAL MATERIAL PRODUCTION SPLICE EXCEPT EXTENDED THE SAME NR FASTENERS PAST DAMAGE PER ESO 11697 DATED 10/15/98. (M)
Part: SKIN — GOUGED (BS 1083)
TUL - DEEP GOUGE IN SKIN STRINGER 174. BLENDED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M)
Part: STRAP — CORRODED (HORIZ STAB)
TUL - FOUND CORROSION ON HORIZ STAB REAR UPPER SRM FAIL/SAFE STRAP RIGHT SIDE. REPAIRED PER ESO 11697, DATED 10/15/98. (M)
Part: STRINGER — CORRODED (BS 680-683)
TUL - FOUND 28R STRINGER FORWARD OF STATION 690 FOUND TO BE CORRODED. FABRICATED NEW STRINGER SPLICE EXTENDED TO PICK UP SAME NUMBER OF FASTENERS PAST DAMAGE CUTOUT PER ESO 11697, DATED 10/21/98. (M)
Part: SPAR — CORRODED (HORIZ STABILIZER)
TUL - HORIZ STABILIZER FRONT SPAR CENTER SECTION LEFT UPPER AND LEFT LOWER 'A' FRAME ATTACH LUGS CORRODED. REPAIRED PER ESO 11697, DATED 10/15/98. (M)
Part: SKIN — CORRODED (BS 1148-1150)
TUL - FOUND INNER SKIN CORRODED JUST ABOVE STRINGER 26R, STATION 1148-1150. INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M)
Part: STRINGER — CRACKED (WS 686)
TUL - FOUND STRINGER AFT OF VENT TOP OF TANK CRACKED AT STATION 686.50. INSTALLED REPAIR PER BOEING S/B 727-57-A155. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15R CRACKED FORWARD OF ICE LIGHT AT STATION 720B PLUS 4 INCHES. REPAIRED CRACKED STRINGER IAW SRM 53-10-3 PAGE 3-4B. (M)
Part: SPAR — CORRODED (HORIZ STABILIZER)
TUL - HORIZ STABILIZER FRONT SPAR CENTER SECTION RIGHT UPPER 'A' FRAME MOUNT LUGS AND LOWER 'A' FRAME MOUNT LUGS CORRODED. REPAIRED PER ESO 11697 DATED 10/15/98. (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND CORROSION AROUND LEFT ICE LIGHT STATION 720B-720C BETWEEN STRINGER 16 LEFT AND 19 LEFT. PERFORMED FUSELAGE SKIN REPAIR AT LEFT WING SCANNING LIGHT CUTOUT PER SRM 53-30-3, ALODINED AND PRIMED PER MM 51-20-0. (M)
Part: FLOORBEAM — CORRODED (BS 1050)
TUL - FOUND CORROSION FLOORBEAM STATION 1050 LB 10 TO LB 55. REMOVED CORROSION, CUTOUT, BEYOND LIMITS, AREA AND INSTALLED REPAIR PER SRM 53-10-8 PAGE 9A AND 9B. (M)
Part: ANGLE — CORRODED (BS 340-344)
TUL - FOUND STATION 340-344 RIGHT SKATE ANGLE HAS CORROSION, FOUND UNDER LEVELING COMPOUND WHICH WAS REMOVED TO ACCOMPLISH WORK ON E58 NR 2736701. REMOVAL OF CORROSION WAS BEYOND LIMITS, INSTALLED 12.75 INCH LONG 'L' ANGLE REPAIR PER ESO 11697, DATED 14 OCT 98 OVER FLANGE OF CHORD AT STATION 377-350 RIGHT SIDE. (M)
Part: SKIN — CORRODED (BS 834)
TUL - FOUND LOWER WING SKIN CORRODED ABOVE RIGHT PRIMARY HEAT EXCHANGER STATION 834 RBL 30. REMOVED CORROSION, REMOVED NECESSARY FASTENERS, CLEANED, TREATED, PREPARED AREA AND INSTALLED DOUBLER PER SRM 57-30-3, SEALED AREA WITH 1422A/B. (M)
Part: FRAME — CORRODED (BS 375)
TUL - FOUND CORROSION ON BELL FRAME AT STATION 375 RIGHT WL 209.1 JUST ABOVE FLOOR LEVEL. CUT OUT DAMAGE INSTALLED TYPICAL FORMED SECTION. REPAIR PER SRM 51-40-3 FIG 1 SHEET 3, L-ANGLE DOUBLER 7075 T-6 .090, 1.375 INCH BY 2 INCH BY 8.75 INCH, 29 HI-LOCKS TOTAL .1875 INCH DIAMETER. (M)
Part: SKIN — GOUGED (FUSELAGE)
TUL - FOUND DEEP GOUGE IN FUSE SKIN AT AFT LOWER CORNER OF LEFT AFT GALLEY DOOR CUTOUT. BLENDED AREA AND INSTALLED DOUBLER PER 53-30-3 FIG 4. (M)
Part: CASTING — CORRODED (NLG)
TUL - NOSE LANDING GEAR DRAG BRACE CASTING HAS CORROSION IN BORE AND ON FACE. REPLACED DRAG BRACE CASTING WITH NEW PART. (M)
Part: SHEAR TIE — CORRODED (BS 1166)
TUL - AFT SIDE OF SHEAR TIE IS CORRODED. REPLACED SHEAR TIE STRINGER 28L-29L, STATION 1166. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND CRACK AT END OF STRINGER LAST RIVIT. CUT OUT BAD SECTION OF STRINGER AND SPLICED IN NEW SECTION PER SRM 53-10-3 FIG 5 ESO 11697. (M)
Part: WEB — CORRODED (BS 351)
TUL - FOUND STATION 351 HAS CORROSION AROUND SEVERAL FASTENERS AT LOWER END OF WEB, FORWARD SIDE. REPAIRED WEB IAW ESO 11697 AND SRM 53-10-9. ENGINEER APPROVED ACCEPTABLE TO NT TRIM OUT BLEND AREA. (M)
Part: FRAME — DENTED (BS 520)
TUL - BELLFRAME DENTED STATION 520 TOP SIDE INTO RADIUS, WEB STRINGER 22 AREA. REMOVED DAMAGED AREA AND INSTALLED REPAIR, SRM 51-40-3 .050 7075-T6, REPAIR MATERILA AND .1875 FLUSH AND PAN 'D' RIVETS. (M)
Part: FRAME — DENTED (BS 660)
TUL - BELLFRAME DENTED TOPSIDE FORWARD RADIUS STATION 660 STRINGER 24R. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER SRM 51-40-3 USING .050, 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M)
Part: FRAME — DENTED (BS 660)
TUL - BELLFRAME DENTED TOPSIDE, RADIUS AND INTO WEB STATION 660 STRINGER 22L AREA. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-40-3, USING .050 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M)
Part: FRAME — DENTED (BS 660)
TUL - BELLFRAME DENTED TOP SIDE, RADIUS AND INTO WEB STATION 660 STRINGER 20L AREA. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 51-40-3 USING .050, 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M)
Part: LIGHT — INOPERATIVE (ROW 29-30)
ORD - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 29 AND 30 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: SKIN — CORRODED (BS 1050-1060)
TUL - BULGE IN FUSELAGE SKIN STA 1050 - STA 1060, STR 27R. CUT OUT AND REMOVED DAMAGED SECTION OF SKIN AND STR 27R. INSTALLED DOUBLER AND STRINGER REPAIR PER SRM 53-30-3 AND SRM 53-10-3. TST: 51,239 HOURS. CYCLES, 31,088. (X)
Part: STRINGER — CORRODED (BS 990)
TUL - CORROSION FOUND ON STR 29R AT STA 990. REPAIRED PER ESO 11697 DATED 9-9-97. TST: 51,239 HOURS. CYCLES, 31,088. (X)
Part: SKIN — CORRODED (BS 825/826)
TUL - WING CENTER SECTION, LOWER SKIN, INSIDE HEAT EXCHANGE PLENUM AFT END, SKIN CORRODED. SKIN DOUBLER REPAIR PER SRM 57-30-3. TST: 51,239 HOURS. CYCLES, 31,088. (X)
Part: STRINGER — CORRODED (BS 683)
TUL - CORROSION ON OUTBOARD SIDE OF STR 27R AT STA 683. REPAIRED STR 27R AT STA 683 PER SRM 53-10-3, FIG 1. TST: 51,239 HOURS. CYCLES, 31,088. (X)
Part: STRINGER — CORRODED (BS 990)
TUL - CORROSION IN AFT CARGO BILGE STA 990A, STR 29R. FABRICATED REPAIR PARTS, CUT, FIT, AND DRILLED NEW SECTION OF STR 29R. INSTALLED NEW SECTION OF STRINGER WITH REPAIR PARTS IAW SRM 53-10-3, FIG 1. TST: 51,239 HOURS. CYCLES: 31,088. (X)
Part: LIGHT — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF MAIN CABIN HAD 8 FOOT SECTION INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: SKIN — DENTED (BS 420)
TUL - FOUND DENT IN FUSELAGE SKIN. CUTOUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-30-3 PG 5-8. (M)
Part: SKIN — CORRODED (BS 830)
TUL - FOUND CORROSION ON LEFT PLENNUM CHAMBER SKIN. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATE 10-1-96. (M)
Part: WING TIP — DAMAGED (RT WING)
TUL - FOUND RIGHT WING TIP DAMAGED. REMOVED DAMAGED PARTS AND REPLACED WITH NEW PER SRM 51-10-1 PG 1-15. (M)
1995
Part: EEL RELAY — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ILLUMINATED WHEN SYSTEM ARMED. REPLACED EMERGENCY EXIT LIGHT RELAY R70. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)
Part: SENSE LINE — BROKEN (NR 3 ENGINE)
SJC - FLT 2143 - EN ROUTE MIA-CCS DURING CRUISE, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED. ACFT DIVERTED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 3 ENGINE MODULATING VALVE SENSE LINE. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)