N707AA
Registered owner: STAHR JOHN C, FL (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.
40 reports on file, 1996-07-11 – 2001-11-04.
Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS)
ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M)
Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS)
ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON UNDERSIDE OF FLOORBEAM AT DOOR SILL AREA FRAME 62 INBOARD OF ROLLOUT DEVICE. CORROSION IS HALF WAY THROUGH FLOORBEAM. INSTALLED FABRICATED SECTION OF FLOORBEAM AT DOOR SILL AREA STATION 4097 (FRAME 62) PER SRM 51-72-10. (M)
Part: CHARGER — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER SYSTEM FOR LEFT OVERWING EMERGENCY EXIT LIGHT. (M)
Earlier reports · 1996–2000 · 36 reports
2000
Part: WIRE — DAMAGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHT AT SEAT 6D THROUGH 15D INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR LIGHT WIRE AT SEAT 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM ROW 6D TO 15D INOPERATIVE. RE-SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT BETWEEN 6D AND 15D INOPERATIVE. RE-SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOOR INOPERATIVE. REPLACED LIGHT SYSTEM GROUND CHECK NORMAL OPERATION.
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVERWING EXIT INOPERATIVE. REPAIRED BROKEN WIRE IN OVERWING LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 14-18 INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT ROW 14-18. SYSTEM GRUOND CHECK NORMAL OPERATION. (M)
1999
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGNCY EXIT FLOOR PATH LIGHTING FROM ROWS 25 TO 28 DEF INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOOR — CORRODED (BS 1183)
TUL - EXFOLIATED CORROSION ON FLOOR PAN EXTRUDING UNDER AND CAUSING BULGING TO FLOOR STRAP ON FORWARD SIDE OF STATION 1183 BULKHEAD, AT LOWER RIGHT CORNER OF VAULT DOOR FRAME, RBL 14 - RBL 24. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 AND FLOOR PAN ON FORWARD SIDE OF STATION 1183, LOWER RIGHT CORNER OF VAULT DOOR FRAME RBL 14 - RBL 24. (M)
Part: SKIN — CRACKED (BS 312)
TUL - HFEC INDICATES CRACK IN FUSE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER BSB 727-53-0198 PAGE 32, FIG 4 DETAIL IV. (M)
Part: FLOORBEAM — CORRODED (BS 380)
TUL - CABIN FLOORBEAM CORRODED TOP SIDE RBL 52-62. REMOVED CORROSION AND INSTALLED REPAIRED DOUBLER PER AARD 53-10-07-2. (M)
1998
Part: SPAR CAP — CORRODED (RT HORIZ STAB)
TUL - RIGHT HORIZONTAL STABILIZER T/E SPAR CAP HAS CORROSION UNDER DOUBLER, BETWEEN NR 6 AND NR 7 ELEVATOR HINGES. TREATED, PRIMED, AND PAINTED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 55-10-6 AND ESO 11-6-97, DATED 6-3-98. TST: 46,450. CYCLES: 24,085. (X)
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CLIP — OUT OF ADJUST (CABIN)
RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN VENTRAL STAIR INOPERATIVE. ADJUSTED CLIPS ON EMERGENCY EXIT CHARGER FOR VENTRAL STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT PASSENGER SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BROKEN WIRE AT EMERGENCY FLOOR LIGHT PASSENGER SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: FUEL CAP — DEPARTED A/C (LT OVERWING)
JFK - FLT 803 - AFTER TAKEOFF LGA DURING CLIMB-OUT, NR 1 FUEL QTY BEGAN DECREASING AT AN ABNORMAL RATE. ACCOMPLISHED ABNORMAL PROCEDURE FOR DECREASING FUEL QTY AND AIRCRAFT DIVERTED TO JFK, LANDING WITHOUT INCIDENT. REPLACED LEFT OVERWING FUEL CAP WHICH HAD DEPARTED THE AIRCRAFT. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)
Part: STRINGER — CORRODED (BS 676-680)
TUL - CORROSION STR 27L OUTBOARD SIDE AND INSIDE CHANNEL STA 676 - STA 680. REMOVED CORRODED SECTION OF STRINGER AND SPLICED IN NEW SECTION PER SRM 53-10-3, FIG 1. TST: 44,187 HOURS. CYCLES: 22,987. (X)
Part: CONNECTOR — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR IN AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: WIRE — BROKEN (CABIN)
IAH - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR LIGHT WIRE AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FRAME — GOUGED (BS 783.95)
TL - HOLE AND GOUGE IN RADIUS OF BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: WEB — CORRODED (BS 1136-1166)
FIVE PLACES OF CORROSION ON RIGHT AFT LAVATORY FLOOR WEB, EACH BEING APPROXIMATELY 2 INCHES BY 6 INCHES IN A 20 SQUARE INCH AREA WITH 2 PLACES PASSED LIMITS. REMOVED CORROSION SECTION, REPLACED WITH SHIMMED DOUBLER PER SRM 51-40-2. ALODINED, PRIMED AND PAINTED. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 480-488)
TUL - CORROSION ON STR 28L, OUTBOARD SIDE. REMOVED CORROSION STA 28L STA 480 - STA 488. REPAIRED STR 28L, STA 484 PER SRM 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: SHEAR TIE — CORRODED (BS 720)
TUL - CORROSION ON SHEAR TIE, STA 720 FROM STR 28L - STR 28R. REPLACED WITH NEW SHEAR TIE. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: SKIN — CORRODED (BS 480-500)
TUL - FOUND CORROSION ON SKIN STATION 480 TO 500, STATION 28 LEFT. INSTALLED REPAIR PER SRM 53-30-3, STATION 480 TO 500, STRINGER 28 LEFT. (M)
Part: FRAME — MISDRILLED (BS 804.95)
TUL - HOLE DRILLED IN RADIUS OF FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STIFFENER — CORRODED (WS 245)
TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER, FSS 245. REPLACED VERTICAL STIFFENER PER SRM 51-10-4, PAGE 4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 680-710)
TUL - CORROSION ON STA 27R. REMOVED STA 27R, STA 680 - STA 710. INSTALLED NEW SECTION OF STRINGER PER 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: SHEAR TIE — CORRODED (BS 700)
REMOVED SHEAR TIE, REPLACED WITH NEW SHEAR TIE, STA 700, 28LT-28RT PER 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 495-500)
TUL - FOUND CORROSION ON STRINGER 27R . REPAIRED STRINGER PER SRM 53-10-3 PG 3-4. REMOVED CORROSION PER SRM 51-10-6. (M)
Part: STIFFENER — CORRODED (WS 255)
TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER FSS 255. REPLACED STIFFENER PER SRM 51-10-4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 680-720)
TUL - CORROSION ON STR 28R, STA 680 TO STA 720 PLUS 3 INCHES. REMOVED AND INSTALLED NEW STRINGER PER SRM 51-10-1, PAGE 4. ALODINED, PRIMED AND PAINTED PER MM 51-20-0. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: SKIN — CORRODED (BS 480-500)
TUL - CORROSION ON BELLY SKIN. INSTALLED DOUBLER PER SRM 53-30-3, PAGES 12-14A. REMOVED CORROSION. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: FRAME — CORRODED (BS 720)
TUL - CORROSION ON LOWER BELL FRAME, STA 720. INSTALLED REPAIR ON BELL FRAME PER SRM 53-10-4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: FRAME — DOUBLE DRILLED (BS 804.95)
TUL - DOUBLE HOLE DRILLED IN BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 704)
TUL - CORROSION ON STR 28L, STA 704. INSTALLATED NEW SECTION OF STR 28L, STA 680 TO STA 720. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRINGER — CORRODED (BS 950-1000)
TUL - HEAVY CORROSION ON STR 29R FROM STA 950E TO STA 1000. REMOVED AND REPLACED STR 29R, STA 950-STA 1000 IAW SRM 53-10-3, AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-30-3, FIGURE 3, AND ESO 11697, DATED 6-10-96. TST: 41,665 HOURS. CYCLES: 21,768. (X)
Part: STRAP — CORRODED (BS 610-620)
TUL - CORROSION ON STRAP. REMOVED CORROSION, INSTALLED NEW STRAP FRAME 610-620 PER SRM 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)