N717AA
Registered owner: DOMFREMAN LLC, MT (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.
53 reports on file, 1995-12-24 – 2001-07-25.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTING FORWARD SECTION INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 52 reports
2000
Part: SPAR — CORRODED (HORIZONTAL STAB)
TUL - FOUND LEFT HORIZONTAL STABILIZER UPPER REAR SPAR CHORD CORRODED, 8 INCHES BY 2 INCHES, INBOARD OF ELEV PUC. INSTALLED REPAIR IAW ESO 11679 DATED 10/11/2000. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND OUTBOARD FACE OF STRINGER 20L HEAVY CORROSION BETWEEN STATION 1163 AND 1177, 10 INCHES BY 1 INCH. REMOVED AND REPLACED STRINGER PER SRM 51-10-1. (M)
Part: SKIN — CORRODED (FUSELAGE)
TUL - FOUND SKIN CORROSION, 10 INCHES BY 10 INCHES, ABOVE AFT LAVATORY DUMP. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND NEW STIFFENER IAW ESO 11692, 10-16-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND STATION 360 FRAME CORRODED BETWEEN STRINGER 17R AND 16R, 18 INCHES BY 4.5 INCHES. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 10/12/00. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND STRINGER 22L FLANGE DAMAGED AT STATION 1174 AND CORROSION 2 INCHES BY 7 INCHES, IN STRINGER ON FILLER AT STATION 1180. REMOVED DAMAGED AREA OF STRINGER. INSTALLED STRINGER SPLICE PER SRM 53-10-3. INSTALLED NEW FILLER. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND STATION 360 FRAME CORRODED 1 INCH BY 2 INCHES, BETWEEN STRINGER 17R-16R. INSTALLED REPAIR PER ESO NR 11697 DATED 10/12/2000. (M)
Part: SPAR — CORRODED (HORIZONTAL STAB)
TUL - FOUND LEFT HORIZ STAB UPPER REAR SPAR CHORD CORRODED OUTBOARD END, 9 INCHES BY .375 INCH. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11967, DATED 10/10/2000. (M)
Part: STRINGER — CRACKED (FUSELAGE)
TUL - FOUND STRINGER 4R CRACKED AT STATION 481. REMOVED CRACKED FACTORY STRINGER SPLICE. INSTALLED NEW SPLICE AT STRINGER 4R STATION 481 PER SRM 51-10-1. (M)
Part: LAP JOINT — CRACKED (FUSELAGE)
TUL - FOUND CRACK .125 INCH, IN SKIN AT SKIN LAP STRINGER 26L, STATION 488. INSTALLED STRAP DOUBLER AT STRINGER 26L LAP APPROX STATION 488 ESO 11697 10/10/2000. (M)
Part: WIRE — BROKEN (AFT STAIR)
MIA DURING OVERNIGHT MAINTENANCE AFT STAIRWELL OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN FIRST CLASS LAVATORY AND GALLEY INOPERATIVE. REPAIRED WIRE SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ABOVE DOOR L1 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ABOVE DOOR L1. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (AIRSTAIR)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BOTTOM OF AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT BOTTOM OF AFT AIRSTAIRS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMEGNCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHCKED NORMAL OPERATION. (M)
Part: RIB — CRACKED (WS 760)
TUL - HFEC INDICATES CRACK IN RIB CHORD RADIUS INBOARD SIDE AT STATION 760R AT EDGE OF REPAIR DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SB 727-57-0112, DWG 65C33202 AND ESO 11697 DATED 10-20-99. (M)
Part: SKIN — CORRODED (BS 680-695)
TUL - FUSELAGE SKIN BULGING BETWEEN FASTENERS ON SKIN LAP STRINGER 19R FS 680-695. CUTOUT CORRODED SKIN AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 1. (M)
Part: RIB — CRACKED (BS 760)
TUL - LEFT RIB CHORD CRACKED IN RADIUS UNDER DOUBLER STATION 760L. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SB 727-57-0112 DWG 65C3302 ESO 11697 DATED 10-20-99. (M)
Part: SKIN — CORRODED (LT WING)
TUL - FOUND LOWER WING SKIN ABV LEFT PRIMARY HEAT EXCHANGER HAS AREA OF CORROSION. INSTALLED DOUBLER/TRIPLER PER SRM 57-30-3. (M)
Part: SKIN — CORRODED (RT WING)
TUL - LOWER WING SKIN ABV RT PRIMARY HEAT EXCHANGE HAS AREA OF CORROSION FORWARD OF PREVIOUS REPAIR. INSTALLED DOUBLER/TRIPLER PER SRM 57-30-3. (M)
Part: SPAR CHORD — CORRODED (HORIZ STABILIZER)
TUL - SKIN BULGED AT AFT SPAR RT HORIZONTAL STABILIZER UPPER SURFACE JUST FORWARD OF ACTUATOR ACCESS PANEL. FABRICATED AND INSTALLED DOUBLER PER ESO 11697 DATED 10-19-99. TST: 74,272, HOURS. CYCLES: 49,986. (X)
Part: LIGHT — DEFECTIVE (CABIN)
TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT STAIRWELL INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: FRAME — CRACKED (BS 560)
TUL - FOUND FS 560 FRAME WEB CRACKED AT NR 2 AND NR 3 DOOR STOP ATTACH HOLES. CUTOUT FRAME WEB FROM STRINGER 24R TO STRINGER 21R 20 INCH OVERALL, SPLICED REPLACEMENT WEB PER TYPICAL WEB REPAIR SRM 51-40-2. (M)
Part: LIGHT — INOPERATIVE (AFT GALLEY)
DFW - DURING OVERNIGHT MAINTENANCE, THE AFT GALLEY SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT GALLEY SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: SKIN — CORRODED (BS 517)
TUL - CORROSION UNDER LAP SPLICE STRINGER 26L, STATION 517. REPAIRED CORRODED AREA PER SRM 53-30-3 FIG 5. (M)
Part: FITTING — CORRODED (BS 1183)
CORROSION ON STRINGER END FITTING 18R, AT STATION 1183. REMOVED AND REPLACED STRINGER END FITTING. (M)
Part: BEAM — CORRODED (RT HORIZ STAB)
TUL - CORROSION ON RIGHT UPPER TRAILING EDGE FROM TIP TO 48 INCHES INBOARD, INBOARD OF PCU, 86 INCHES FROM OUTBOARD END, 70 INCHES FROM OUTBOARD END. REMOVED OLD BEAM AND REPLACED WITH SERVICEABLE BEAM IAW SRM 51-10-1 PAGE 4. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER IS CRACKED AT STATION 720B, 3 INCHES AFT OF STATION. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 2, PAGE 4C AND 4E. (M)
Part: STRINGER — CRACKED (BS 720)
TUL - STRINGER 15R CRACKED 4 INCHES FORWARD OF STATION 720C. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 2, PAGE 4C AND 4E. (M)
Part: STRINGER — CORRODED (BS 720)
TUL - CORROSION ON STRINGER 16R, 3 INCHES FORWARD OF STATION 720E. REPAIRED STRINGER IAW SRM 51-10-3. (M)
Part: STRINGER — CRACKED (FUSELAGE)
TUL - STRINGER 15L CRACKED FORWARD AND AFT SIDES OF ICE LIGHT. INSTALLED STRINGER REPAIRS PER SRM 53-10-3 FIG 2. (M)
Part: STRINGER — CORROSION (BS 995)
TUL - INTERGRANULAR CORROSION IN BOTTOM OF STRINGER 28R. CUT OUT STRINGER SECTION FROM 977 AND 1007 AND INSTALLED REPAIR SECTION PER ESO 11697, DATED 9-19-97. (M)
Part: ANGLE — CORRODED (WS 517-523)
TUL - UPPER CHORD ANGLE ABOVE NR 6 SLAT ACTUATOR HAS HEAVY CORROSION FROM FS 517 TO FS 523, FRONT SPAR. INSTALLED DOUBLER AND FASTENERS PER ESO 11697. APPLIED BRUSH COAT AND TOP COAT SEALER AFTER REMOVING CORROSION. (M)
Part: SHEAR TIE — CRACKED (BS 500)
TUL - SHEAR TIE CRACKED STATION 500 BETWEEN STRIGNER 25 LEFT AND 26 LEFT. REMOVED CRACKED SHEAR TIE AND INSTALLED NEW SHEAR TIE PER 53-10-3. (M)
Part: STRINGER — CORRODED (BS 533)
TUL - FOUND CORROSION ON STRINGER 14 RT, STATION 533. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-4. (M)
Part: STRINGER — CORRODED (BS 531-537)
TUL - FOUND CORROSION ON STRINGER 16R FROM STATION 531 TO 537. FABRICATED AND INSTALLED STRINGER REPLACEMENT SECTION. SPLICED AS PER SRM 53-10-3. (M)
Part: BEAM — CORRODED (LT HORIZ STAB)
TUL - FOUND CORROSION ON LEFT TRAILING EDGE UPPER FALSE SPAR BEAM (INBOARD OF PCU). REPLACED UPPER FALSE SPAR BEAM. (M)
Part: SKIN — CORRODED (WS 520)
TUL - SKIN BULGED UP FROM CORROSION WHERE L/E OF TOP WING SKIN MEETS TRAILING EDGE OF L/E SKIN. CORROSION WAS REMOVED, INSTALLED FILLER DOUBLER AND REINFORCEMENT STRAP PER ESO NR 11697. (M)
Part: SPAR CAP — CORRODED (LT HORIZ STAB)
TUL - FOUND CORROSION AFT SPAR CAP BULGED TOP LEFT HORIZ STAB, FORWARD AND INBOARD OF NR 6 HINGE BEARING. REPAIRED CORROSION AREA PER ESO 11697. (M)
Part: BEAM — CORRODED (LT HORIZ STAB)
TUL - FOUND CORROSION ON LEFT HORIZ STABILIZER TRAILING EDGE BEAM, 76 INCHES FROM OUTBOARD END. REPLACED UPPER FALSE SPAR BEAM. (M)
Part: ANGLE — CORRODED (BS 487-490)
TUL - UPPER CHORD ABOVE NR 6 SLAT DE-ICE TUBE HAS CORROSION IN 2 PLACES FROM FS 487 TO FS 490 FRONT SPAR. INSTALLED DOUBLER AND FASTENERS PER ESO 11697. APPLIED BRUSH COAT AND TOP COAT SEALER AFTER REMOVING CORROSION. (M)
Part: STRINGER — CORRODED (BS 1166-1183)
TUL - FOUND CORROSION ON STRINGER 18R BETWEEN STATION 1166 AND 1183. CUT OUT CORRODED SECTION OF STRINGER AND INSTALLED NEW SECTION AND REPAIRED SPLICE PER SRM 53-10-3. (M)
Part: DOOR FRAME — CORRODED (BS 410)
TUL - CORROSION AROUND FORWARD E/E DOOR LOCK ON FUSELAGE. INSTALLED NEW FORWARD E/E DOOR FRAME STATION 420, STRINGER 28R TO 28L. (M)
1996
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 25 INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOOR — CORRODED (BS 1170-1176)
TUL - FOUND CORROSION ON LEFT AFT LAV FLOOR AT STATION 1170 TO STATION 1176. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-40-2 PAGES 1-6. (M)
Part: ANGLE — CORRODED (BS 1060-1170)
TUL - FOUND LEFT CREASE ANGLE CORRODED STATION 1060 TO 1170. CUT OUT CORRODED AREA AND INSTALLED ANGLE PER SRM 51-10-1 FIG 4. (M)
Part: SKIN — DAMAGED (BS 683)
TUL - FOUND DAMAGED SKIN AT BS 683. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
Part: SKIN — DENTED (BS 640)
TUL - FOUND DENT IN FUSELAGE SKIN STATION 640, STRINGER 25L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M)
Part: SPLICE PLATE — CRACKED (RT WING)
TUL - SPLICE PLATE CRACKED ABOVE NR 5 LEFT FLAP ACT. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-02 R8-12. (M)
Part: OPERATING ROD — DEFECTIVE (NLG DOOR)
DFW - FLT 1503 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. RECYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED NORMALLY. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED AND RIGGED NOSE LANDING GEAR DOOR OPERATING ROD. ALSO, LUBRICATED NOSE LANDING GEAR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: DOOR FRAME — CORRODED (BS 377)
TUL - FOUND CORROSION ON FRAME 377 ABOVE FLOOR LINE, FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER SECTION OF DOOR FRAME FORWARD SIDE OF GALLEY DOOR PER SRM 51-30-2. (M)
1995
Part: LIGHT PLATE — SHORTED (F/E PANEL)
MIA-MSY - FLT 1060 - DURING CRUISE, SMOKE NOTED COMING FROM AC POWER SELECTOR LIGHT PLATE PANEL. AIRCRAFT PROCEEDED TO MSY AND LANDED WITHOUT INCIDENT. PLACARDED AC POWER SELECTOR LIGHT PLATE INOPERATIVE. SUBSEQUENTLY, REPLACED AC POWER SELECTOR LIGHT PLATE PANEL AT ORD/24. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (M)