N886AA
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.
42 reports on file, 1995-08-18 – 2001-07-30.
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE CEILING EMERGENCY LIGHT AT SEAT ROW 8 DIM. REPLACED CEILING EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 8. 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: LIGHT — INOPERATIVE (AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 39 reports
2000
Part: DOUBLER — CRACKED (FUSELAGE)
TUL - FOUND SMALL CRACK 1 INCH BY 1 INCH EMANATING FROM RADIUS OF BEARSTRAP. ROUTED OUT CRACK AND INSTALLED DOUBLER AND TRIPLER PER BOEING S/B 727-53-0188 AUTHORIZED BY ESO 11697 DATED 10-31-2000. (M)
Part: LIGHT — MALFUNCTIONED (AFT AIRSTAIR)
TUL - FOUND AIRSTAIRS AFT OVERHEAD EMERGENCY EXIT LIGHT DIM. INSTALLED SERVICEABLE LIGHT ASSY PER MM 33-50-061-4, OPS CHECK OK, COMPLETED MRR. (M)
Part: LIGHT — INOPERATIVE (ESCAPE SLIDE)
TUL - FOUND RIGHT FORWARD DOOR SLIDE LIGHT INOPERATIVE. INSTALLED SERVICEABLE LAMP PER MM 33-50-041-21, OPS CHECK OK. (M)
1999
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: VALVE — DEFECTIVE (RT WING)
BNA - FLT 1750 - EN ROUTE DFW-PHL, NR 2 CROSSFEED VALVE FAILED TO OPEN. AIR INTERRUPTED AND LANDED BNA WITHOUT INCIDENT. CHECKED AND DEFERRED ACCORDING TO MEL. REPLACED NR 2 FUEL MANIFOLD VALVE. PERFORMED OPERATIONAL CHECK WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: FLOORBEAM — CORRODED (BS 344)
TUL - STATION 344, LBL 15 INCH TO RBL 12 INCH CORROSION IN AND AROUND FASTENERS HOLES FLOORBEAM. REMOVED CORROSION AND CRACKED TOP CHORD FROM RBL 16 TO LBL 30. REPAIR PER SRM 53-10-8 FIG 9 AT RBL 16 AND ATTACHED TOP CHORD OF FLOORBEAM TO EXISTING SPLICE AT LBL 30. (M)
Part: FRAME — CRACKED (BS 303)
TUL - FOUND CRACK IN FRAME AT STATION 303.9 EXTENDING FROM EXISTING WEB CUTOUT AT STA 16L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 11697, DATED 10-22-98. (M)
Part: SKIN — GOUGED (BS 720)
TUL - FOUND STATION 720D OUTBOARD STRINGER 2R OUTER SKIN GOUGED. INSTALLED DOUBLER AT STATION 720D STRINGER 2R OUTER SKIN PER SRM 53-30-3 FIG 1 PAGE 5, .061 THICKNESS WITH 72 FASTENERS. (M)
Part: FRAME — DENTED (BS 600)
TUL - BELL FRAME STATION 600 BETWEEN STRINGER 24L AND 23L DENTED. CUT OUT DENTED AREA AND INSTALLED DOULER PER SRM 51-40-3 FIG 1 PAGE 3-5 9.5 INCH LONG 7075T-6 .063 DOUBLER, 3 ROWS OF RIVETS PASS DAMAGE, 24 .1875 MS2047D6 RIVETS USED. (M)
Part: SKIN — CORRODED (BS 1050)
TUL - FOUND CORROSION ON BELLY SKIN FORWARD SIDE OF STATION 1050 BELL FRAME AT STRINGER 28L. CUT OUT DAMAGED INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 3. (M)
Part: SKIN — CORRODED (WS 815)
TUL - FOUND CORROSION ON LOWER WING SKIN IN RIGHT PRIMARY HEAT EXCHANGER AREA, STATION 815, RBL 30. INSTALLED DOUBLER PER SRM 57-30-3 FIG NR 8. (M)
Part: FRAME — CRACKED (BS 620)
TUL - BELL FRAME CRACKED AT FASTENER, STATION 620 ABOVE STRINGER 14R. REPAIRED CRACK AT BELL FRAME AT STATION 620 ABOVE STRINGER 14R PER SRM 51-40-3 FIG 1 SHEETS 1-6, 2024 T3 .071 MATERIAL, INSTALLED WITH .1875 FIRST OVER HI-LOCKS. (M)
Part: STRINGER — CRACKED (BS 730)
TUL - STRINGER 15L CRACKED AFT SIDE OF THE ICE LIGHT 730B PLUS 10 INCHES. CUT OUT DAMAGED STRINGER END AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-3 FIG 5 PAGE 12. (M)
Part: STRINGER — CORRODED (BS 735-738)
TUL - STRINGER 24L CORRODED INSIDE STATION 735-738. INSTALLED FILLER AND DOUBLER PER SRM 53-10-3 FIG 1 (SHEET 4). (M)
Part: BULKHEAD — CORRODED (BS 351)
TUL - FOUND CORROSION ON LOWER WEB OF FUSELAGE STAITON 351.2 BULKHEAD APPROX 16 INCH LEFT AND RIGHT OF CENTER LINE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 PAGES 10-11. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - FOUND STRINGER 15R CRACKED JUST FORWARD OF ICE LIGHT. REPAIRED STRINGER 15R JUST FORWARD OF ICE LIGHT PER SRM 53-10-3, FIGURE 5, PAGES 12-17. (M)
Part: SKIN — CORRODED (WS 845)
TUL - FOUND CORROSION ON LOWER SKIN AT LEFT PRIMARY HEAT EXCHANGER AREA AFT OF EXISTING REPAIR (3 AREAS) STATION 845 LBL 36 APPROX. INSTALLED REPAIR PER SRM 57-30-3 PAGE 25 FIG 10. (M)
Part: SKIN — GOUGED (BS 720)
TUL - STATION 720D PLUS 10 INBOARD STRINGER 2R SKIN DENTED. INSTALLED DOUBLER AT STATION 720D PLUS 10 INBOARD STRINGER 2R OUTER SKIN PER SRM 53-30-3 FIG 1 PAGE 5, .061 THICKNESS WITH 72 FASTENERS. (M)
Part: SKIN — GOUGED (BS 720)
TUL - FOUND GOUGE IN CROWN SKIN AT FS 720D PLUS 10 INCH INBOARD OF STRINGER 2R. BLENDED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. (M)
Part: FRAME — DENTED (BS 660)
TUL - STATION 660 BELL FRAME DENTED THREE PLACES BETWEEN STRINGER 25R-23R. REPAIRED BELL FRAME AT STATION 660 PER SRM 51-40-3, FIG 1, PAGE 3. REMOVED DAMAGE AREA BETWEEN STRINGER 23 AND 24. (M)
Part: FRAME — CORRODED (PAX DOOR)
TUL - FORWARD GALLEY DOOR ENTRY, DOOR CUTOUT FRAME CORRODED 3 INCHES ABOVE FLOOR LINE STATION 377, ALL SIDES OF FRAME. CUT OUT DAMAGED AREA, INSTALLED TYPICAL FORMED SECTION. REPAIR PER SRM 51-40-3 FIG 1. (M)
Part: FRAME — DENTED (BS 1030)
TUL - FRAME DENTED AT STATION1030 ABOVE STRINGER 25L. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53-4-3. (M)
Part: SKIN — CORRODED (WS 825)
TUL - FOUND CORROSION ON LOWER WING SKIN IN LEFT PRIMARY HEAT EXCHANGER AREA STATION 825 APPROX LBL 36 INCHES FORWARD OF EXISTING REPAIR. INSTALLED REPAIR PER SRM 57-30-3 PAGE 19 FIG 8. (M)
Part: STRINGER — CRACKED (WS 686)
TUL - CRACK IN WING STRINGER NR 10 AT RIB W/W 686.5 (UPPER STRINGER). INSTALLED STRINGER DOUBLER REPAIR PER SB727-57A159. (M)
Part: STRINGER — CORRODED (BS 970-1010)
TUL - FOUND CORROSION ON STRINGER 29 LEFT STATION 970-1010. REPLACED STRINGER 29 LEFT STATION 960-1010 PER SRM 53-10-3. (M)
Part: FLOORBEAM — CRACKED (BS 344)
TUL - FOUND STATION 344 RBL 15 INCHES FLOORBEAM UPPER FLANGE CRACKED. CUT OUT DAMAGED AREA OF FLOORBEAM. ACCOMPLISHED REPAIR IAW 53-10-8 FIG 9. (M)
Part: FLOORBEAM — CRACKED (BS 760)
TUL - FLOORBEAM WEB CRACKED TWO PLACES STATION 760 AT RBL 58 - RBL 62. STOP DRILLED CRACKS AND REPAIRED FRAME WEB PER SRM 51-40-2 PAGE 1-3 AND 51-40-2 PAGE 5 FIG 1 SHEET 5. TWO ROWS OF .25 INCH HI-LOCK UPPER AND LOWER, TWO ROWS .1875 HI-LOCKS INBOARD AND OUTBOARD .050.5H 301 REPAIR DOUBLER 4.5 INCH BY 8 INCH. (M)
Part: SKIN — CORRODED (BS 720)
TUL - OUTBOARD SIDE STRINGER 27L STATION 720C, 10 INCHES TO 720C PLUS 3 INCHES FUSELAGE SKIN CORRODED UNDER LEVELING COMPOUND. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL REPAIR PER SRM 53-30-3 FIG 1 PAGE 8. (M)
Part: FRAME — CORRODED (BS 600)
TUL - FOUND STATION 600 FORWARD SIDE OF FRAME WEB AND SHEAR TIE CORRODED BETWEEN STRINGER 26 RT AND 27 RT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 58-60, INSTALLED NEW SHEAR TIE. (M)
Part: FRAME — GOUGED (BS 950)
TUL - AFT EXTRUDED FRAME AT CARGO DOOR OPENING HAS DEEP GOUGES WITH ALUMINUM PEELING ON 90 DEGREES EDGE 10 INCHES ABOVE LOWER FORWARD CORNER. BLENDED GOUGES AND INSTALLED DOUBLER PER ESO 11677, DATED 10-22-98, DOUBLER 8.5 INCH LONG, 2 INCHES WIDE, 17-7 PH .050 THICK HEAT TREATED T0160-180 RSI CAD PLATE. (M)
Part: SKIN — CORRODED (BS 576-580)
TUL - FUSELAGE SKIN CORRODED OUTBOARD STRINGER 27L STATION 576-580. REMOVED CORROSION AND REPAIRED PER SRM 53-30-3 PAGE 8, FIG 1. (M)
Part: FLOORBEAM — CORRODED (BS 380)
TUL - FLOORBEAM 380 HAS CORROSION ON TOP SURFACE STATION 380 RBL 49 INCH TO RBL 65 INCH, EXTENDING BELOW FLOORBOARD OUTBOARD SUPPORT CHANNEL. REPAIRED FLOORBEAM AT STATION 380, RBL 42-RBL 66 PER SRM 53-10-08, PAGES 9A AND 9B. (M)
Part: SKIN — GOUGED (BS 720)
TUL - FOUND GOUGE IN SKIN AT 720D STRINGER 2R. REPAIRED WITH DOUBLER AFTER BLENDING PER SRM 3-30-3. (M)
Part: FRAME — DENTED (BS 620)
TUL - BELL FRAME STATION 620 ABOVE STRINGER 24L DENTED. INSTALLED A DOUBLER ON BELL FRAME PER SRM 51-40-3 PAGE 3-5, USING 8 INCH DOUBLER OF 7075T-6 .063 USING TWENTY .1875 INCH MS 20470D6 AND TWO .25 INCH MS20470D8 RIVETS. (M)
1997
Part: SKIN — CORRODED (BS 720)
TUL - REMOVED AIR DOOR ACT ACCESS PANEL, FOUND CORROSION AROUND EDGES, BULGING AT LT FWD CORNER, STR 28L, STA 720B + 4 INCHES. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-30-3, FIGURE NR 4, PAGES 1 THROUGH 4, AND ESO 11697 9-23-97. TST: 50,816 HOURS. CYCLES, 30,951. (X)
Part: SKIN — CORRODED (BS 830/840)
TUL - WING CENTER SECTION, LOWER SKIN, CORRODED WING, STR 1 - STR 3, ABOVE PRIMARY HEAT EXHANGER, RT SIDE, RBL 16 - RBL 32, STA 380 - STA 840. REMOVED CORROSION, FLAT PEENED AREA. COLD WORKED HOLES AND INSTALLED DOUBLER AND TRIPLER PER ESO 11697, DATED 9-23-97. TST: 51,239 HOURS. CYCLES, 31,088. (X)
1996
Part: SKIN — CORRODED (BS 680)
TUL - FOUND BUTT SPLICE CORRODED STATION 680 AT STRINGER 28R TO STRINGER 28L. CORROSION AREA CUT AND DOUBLER INSTALLED PER SRM 53-30-3 FIG 3A PG 14B. (M)
Part: SKIN — CORRODED (BS 660)
TUL - FOUND FUSELAGE SKIN CORRODED 2 INCHES BY 8 INCHES STATION 660, STRINGER 28R TO 27L. CORROSION AREA CUT OUT AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M)
1995
Part: EEL ASSEMBLY — DEFECTIVE (GALLEY)
RDU - DURING OVERNIGHT CHECK, FOUND THE FORWARD AND AFT GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)