N895AA
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.
20 reports on file, 1996-02-20 – 2000-11-02.
Part: BEAM — CRACKED (LT MLG)
DURING C-CHECK INSPECTION, FOUND A .75 INCH CRACK IN THE WEB AREA AFT SIDE OF THE LEFT MAIN LANDING GEAR SUPPORT BEAM. PART TOTAL TIME AND CYCLES ARE UNKNOWN, BUT AIRCRAFT TT 53,763.0 HOURS. TC: 26,653. (X)
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AIRSTAIR OVERHEAD LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT AIRSTAIR OVERHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1996–1999 · 17 reports
1999
Part: SWITCH — FAILED (RT MLG)
PHL - FLT 0274 - AFTER TAKEOFF, MIA/PHL, RIGHT GEAR DURING RETRACTION INDICATED UNSAFE INDICATION. RIGHT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL WAS ILLUMINATED. RECYCLED GEAR, STILL HAD GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL ILLUMINATED. 25 MINUTES INTO FLIGHT, LIGHT EXTINGUISHED. REPLACED RIGHT GEAR DOOR SWITCH. ACCOMPLISHED SUCCESSFUL GEAR SWING. GROUND CHECKED, NORMAL OPERATION. (X)
Part: SWITCH — FAILED (RT MLG)
TPA - FLT 1486 - DURING LANDING WHEN GEAR WAS EXTENDED, THE LEFT GEAR DOOR ANNUNCIATED ON THE FLIGHT ENGINEER'S PANEL AND THE RED DOOR LIGHT REMAINED ILLUMINATED. REPLACED LEFT GEAR DOOR SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: STRINGER — CORRODED (BS 481-486)
TUL - FOUND CORROSION ON STRINGER 26L AT STATION 481 TO 486. CUT OUT CORRODED END OF STRINGER AND INSTALLED EXTENDED PRODUCTION SPLICE PER ESO11697 3/17/99. (M)
Part: ANGLE — CORRODED (NLG WW)
TUL - FOUND CORROSION ON UPPER AFT SUPPORT ANGLE IN RIGHT TRUNNION BOX (MARKED) INBOARD OF SWIVEL VALVE REF E58 NR 3146190. REMOVED CORROSION ON UPPER AFT SUPPORT ANGLE. INSTALLED EXTRUDED SECTION REPAIR PER SRM 51-40-4 PAGE 5. (M)
Part: FRAME — CRACKED (BS 910)
TUL - FOUND STATION 910 UPLOCK FRAME CRACKED ON FORWARD FLANGE. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-2 PAGE 28. (M)
Part: SKIN — DENTED (BS 1090)
TUL - FOUND STATION 1090, 3 INCH BELOW STRINGER 17 LT HAS DEEP DENT IN FUSE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3, AFTER CUT OUT DAMAGED AREA. (M)
Part: STRINGER — CORRODED (BS 560)
TUL - FOUND CORROSION ON STRINGER 28R AT STATION 560. INSTALLED STRINGER REPAIR AT STATION 554 AND STATION 566 IAW SRM 53-10-3. (M)
Part: STRINGER — CORRODED (BS 495)
TUL - FOUND CORROSION ON STRINGER 27L AT STATION 495. CUT AND REMOVED DAMAGED SECTION OF STRINGER 27L FROM STATION 491 TO 509 MANUFACTURED AND INSTALLED REPAIR FILLER AND SPLICE IAW SRM 53-10-3. (M)
Part: FRAME — DENTED (BS 1050)
TUL - FOUND BELL FRAME AT BS 1050 DENTED. REMOVED DENTED PORTION OF BELL FRAME AND INSTALLED REPAIR SECTION PER SRM 53-10-4. (M)
Part: SPAR — CORRODED (WS 468)
TUL - FOUND CORROSION ON FRONT SPAR LOWER CHORD, LOWER WING L/E PANEL LAND AT NR 3 SLAT INBOARD TRACK. BLENDED OUT CORROSION. INSTALLED REPAIR STRAP PER B727 AARD 57-30-00-2 PAGE 1 AND 2 AND 3. TREATED, PRIMED AND PAINTED AREA. (M)
1998
Part: WIRE — FAILED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN COACH CABIN INOPERATIVE. REPAIRED WIRING IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BOTTOM OF AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT THE BOTTOM OF AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: STRINGER — CORRODED (BS 1113)
TUL - CORROSION INSIDE STR 29L AT BS 1113. REMOVED CORROSION PER 51-10-06 AND REPLACED PER SRM 53-10-3 FIG NR 1. TST: 46,083 HOURS. CYCLES: 23,083. (X)
Part: SHEAR TIE — CORRODED (BS 720)
TUL - FOUND CORRODED SHEAR TIE AT BS 720. REMOVED SHEAR TIE AND CORROSION FROM SURROUNDING AREA PER SRM 51-10-6 AND INSTALLED FABRICATED SHEAR TIE PER SRM 53-10-4. TST: 46,083 HOURS. CYCLES: 23,083. (X)
Part: CONNECTOR — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS INOPERATIVE THROUGH OUT MAIN CABIN. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS BY AFT LAVATORY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: HARNESS — DEFECTIVE (NLG)
DFW - FLT 1528 - AFTER TAKEOFF MEX WHEN LANDING GEAR RETRACTED, NO RED NOSE LANDING GEAR INDICATION ON INSTRUMENT PANEL AS GEAR RETRACTED. ALL INDICATIONS ON F/E PANEL NORMAL. AIRCRAFT PROCEEDED TO DFW AND ALL LANDING GEAR INDICATIONS NORMAL WHEN GEAR EXTENDED. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR LOCK AND POSITION WIRE HARNESS. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 16D AND 22D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)