N69603
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.
17 reports on file, 1997-05-21 – 2009-07-26.
Part: BUTTSTRAP — CORRODED (BS 907 S22-24L)
DURING SCHEDULED INSPECTION, FOUND AFT PIT LT SIDE SKIN BUTT JOINT STRAP CORRODED AND BULGED UP FROM SKIN AT BS 907 BETWEEN S-22L TO S-24L.
Part: STRINGER — CORRODED (BS 967 S25L)
DURING SCHEDULED INSP, FOUND AFT LWR FUSELAGE HAD 2 EACH RIVETS PULLING IN SKIN LAP BS 967, S-25L. UPON REMOVAL OF FASTENERS FOUND CORROSION ON LT S-25L AT BS 967.
Part: SKIN — DENTED (HORIZONTAL STAB)
DENT ON RT HORIZ STAB UPPER SURFACE SKIN 8 INCHES FROM FWD SPAR AND 80 INCHES FROM INBD END.
Part: ANGLE — CORRODED (L-1 DOOR)
DURING SCHEDULED INSP, FOUND CORROSION AT SEVERAL AREAS ON CUSP ANGLE L-1 DOOR BS 303-360.
Part: FLOORBEAM — GOUGED (BS 663)
GOUGE IN FLOORBEAM BETWEEN BS 639 AND BS 663.75 BL 25R.
Part: INTERCOSTAL — CRACKED (BS 346-360)
DURING SCHEDULED INSP, FOUND CABIN FLOOR INTERCOSTAL CRACKED AT BS 346 TO BS 360 BL 0.
Part: CABLE — FRAYED (EVAC SLIDE) · airframe 42,525 hrs · 22,221 cycles
R-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED R-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE PER MM 25-61-35.
Part: CIRCUIT CARD — DEFECTIVE (LANDING GEAR) · airframe 42,395 hrs · 22,159 cycles
ON TAKEOFF LANDING GEAR DID NOT RETRACT IN THE WHEEL WELL, GEAR LIGHTS 3 GREEN 3 RED. FOUND M1112 CIRCUIT CARD DISCOLORED (BURNT). REMOVED AND REPLACED M1112 CIRCUIT CARD REF AMM 32-09-20. PERFORMED GEAR SWING NO ANOMALIES NOTED. REMOVED AND REPLACED M983 AND M986 AS PRECAUTIONARY.
Earlier reports · 1997–2007 · 9 reports
2007
Part: ATTACH FITTING — CRACKED (BS 344-360) · airframe 37,079 hrs · 19,325 cycles
INSPECTION FOUND A 1 INCH CRACK I/B OF AFT END OF STRINGER 11L ATTACHMENT CLIP AFT OF L-1 DOOR CUTOUT, STA 344-360. THE CLIP WAS REPLACED IAW ECRA 5311-01301. A DIP WAS INITIATED TO REINSPECT THE AREA AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES.
Part: FRAME — CRACKED (BS 400) · airframe 37,079 hrs · 19,325 cycles
INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FORWARD FRAME AT LOWER STOP PAD FITTING AT STA 400. THE FRAME WAS REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65C33514.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,079 hrs · 19,325 cycles
ABB DOOR CUTOUT FWD FRAME CRACKED AT SECOND STOP FROM THE BOTTOM. REPLACED FRAME IAW BOEING DRAWING 65-47959.
2004
Part: FRAME — CUT (STA) · airframe 30,423 hrs · 15,909 cycles
INSPECTION FOUND A 3 INCH CUT IN WEB ON FRAME AT STA 219.8, RBL 20. A DOUBLER WAS INSTALLED IAW SRM 51-70-13.
Part: ANGLE — CORRODED (BS) · airframe 30,423 hrs · 15,909 cycles
INSPECTION FOUND L-2 DOOR ZEE ANGLE CORRODED IN SEVERAL AREAS FROM BS 910-1016. THE ZEE ANGLE WAS REPLACED IAW SRM 51-10-2.
2002
Part: SKIN — CRACKED (STA 215) · airframe 25,319 hrs · 13,209 cycles
INSPECTION FOUND A 1/8" CRACK IN CAPTAIN'S WINDOW POST SKIN AT STA 215. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.
2001
Part: WIRE — BROKEN (CABIN) · airframe 23,061 hrs · 11,908 cycles
INSPECTION FOUND EMERGENCY LIGHT AT ROW 21ABC HAD BROKEN WIRES. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED.
1997
Part: FLAP TRANS — INOPERATIVE (NR 7 POSITION)
WHEN FLAPS WERE SELECTED TO 40 DEGREES ON APPROACH TO EWR, THE FLAPS WOULD ONLY EXTEND TO 30 DEGREES. THE AIRCRAFT LANDED NORMALLY WITH FLAPS AT 30 DEGREES. MAINTENANCE FOUND THE NR 7 FLAP TRANSMISSION AT FAULT. THE NR 7 FLAP TRANSMISSION WAS REMOVED AND REPLACED. THE FLAPS WERE CYCLED SEVERAL TIMES AND OPERATION CHECKED GOOD. IN ADDITION, THE NR 4, 5, AND 6 FLAP TRANSMISSIONS WERE SERVICED.
Part: AIR DATA COMP — INOPERATIVE (E/E COMPT)
THE FLAPS WOULD NOT EXTEND TO 40 DEGREES WHILE ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 AIR DATA COMPUTER WAS REMOVED AND REPLACED. NO DEFECTS WERE NOTED WITH AIRCRAFT IN FLIGHT MODE. THE FLAPS WERE CYCLED SEVERAL TIMES BETWEEN 30 AND 40 DEGREES WITH NO PROBLEMS.