N736DY
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.
26 reports on file, 1995-06-25 – 1999-11-03.
Part: SKIN — CORRODED (BS 1615)
FUSELAGE SKIN FS 1605-1625 STRINGER 33-35 HAS CORROSION REPAIR. THE FUSELAGE SKIN BETWEEN FS 1605 AND 1625 AND BETWEEN STRINGERS 33 (BL0) AND 35 WAS FOUND WITH AN AREA OF CORROSION UNDER AN EXISTING TEAR STRAP. THE CORROSION WAS CUTOUT OF THE SKIN WITH AN 8.25 BY 7.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368651-14, REV A.
Part: RETRACT MECH — INOP (LANDING GEAR)
LANDING GEAR WOULD NOT RETRACT INTRANSIT LIGHT REMAINED ON. REMOVED AND REPLACED 4-WAY 3 POSITION VLV. GEAR SWING COMPLETED ALL INDICATIONS NORMAL.
Part: ENGINE — FAILED (NR 2)
NR 2 ENGINE IFSD DUE TO FIRE WARNING. FIRED BOTTLES/DUMPED FUEL ATB TO ATL. TROUBLESHOT IN WORK. PREVIOUS DIVERSION F17/10JUL, ATL/DFW DUE TO SAME PROBLEM. REPLACED ENGINE.
Part: FIRE WARNING — ACTIVATED (NR 2 ENGINE)
NR 2 ENGINE IFSD DUE TO FIRE WARNING CLIMBING OUT OF ATL. FIRED BOTH BOTTLES. MTC IN WORK.
Part: SKIN — CORRODED (BS 703)
THE FUSELAGE SKIN WAS CORRODED AT FS 703 BETWEEN STRINGERS 33 AND 34. THE CORROSION WAS CUT OUT OF THE SKIN WITH A 4 X 8 CUTOUT. THE DAMAGE WAS ADJACENT TO AN EXISTING REPAIR DOUBLER INSTALLED TO REPAIR A SIMILAR CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS REPAIRED WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 367407-14, REV B.
Part: SKIN — CORRODED (BS 1545)
THE FUSELAGE SKIN ASSY WAS FOUND WITH CORROSION AT FS 1545 AND STRINGER 26. THE CORROSION WAS THROUGH THE C2 DOOR SURROUND TRIPLER AND SURROUND DOUBLERS AND INTO THE SKIN. THE CORROSION WAS REMOVED WITH A 6 CUTOUT THROUGH THE ENTIRE SKIN ASSY. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL DOUBLERS PER ER/A 367391-14, REV A.
Part: BATTERY PACK — DISCHARGED (L4 DOOR)
L-4 OUTSIDE EMERGENCY LIGHT STAYED ON. REPLACED EMERGENCY LIGHT BATTERY PACK, CKS OK.
Part: SKIN — CORRODED (BS 798)
THE FUSELAGE SKIN WAS FOUND WITH AREAS OF CORROSION BETWEEN FS 789 AND 809 AND BETWEEN STRINGERS 33 AND 35. THE CORROSION WAS REMOVED WITH TWO CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 367367-14, REV A.
Earlier reports · 1995–1998 · 18 reports
1998
Part: AIR DIST — ODOR (CABIN)
ON DESCENT, PAX IN 42AB SMELLED SMOKE. UPON FURTHER INVESTIGATION BY FLT ATTEND, ELECTRICAL SMELLING SMOKE CONFIRMED AT 42AB AND BY DOORS 3L AND 3R. THE SMELL DISSIPATED ON DESCENT BUT STILL LINGERED. INSPECTED LIGHTS, NO PROBLEMS FOUND.
Part: SPAR CAP — CRACKED (BS 1163)
CENTER WING, INTERMEDIATE SPAR, FS 1163, UPPER SPAR CAP: CAP SPLICE REPAIR. THE RT END OF THE UPPER SPAR CAP ON THE FS 1163 INTERMEDIATE SPAR WAS FOUND CRACKED BEYOND LIMITS. THE RT END OF THE CAP WAS CUT OFF AND A NEW SECTION WAS SPLICED IN PER ER/A 364821-14, REV A.
Part: BULKHEAD WEB — CORRODED (BS 328)
FUSELAGE, BULKHEAD FS 328 LBL 6 WL 126, REPAIR FOR WEB CORROSION. THE FS 328 BULKHEAD WEB WAS FOUND CORRODED AT LBL 6 AND WL 126A 6 BY 3 CUTOUT WAS MADE IN THE WEB TO REMOVE THE CORROSION THE WEB WAS REPAIR WITH AND ALUMINUM DOUBLER AND TRIPLER PER ER/A 364835-14AD, REV A.
Part: SKIN — CRACKED (BS 912)
THE FUSELAGE SKIN AT FS 912 BETWEEN STRINGERS 32 AND 33 WAS FOUND WITH A 2 INCH LONG CRACK DUE TO CORROSION. AN EXISTING SKIN DOUBLER REPAIR WAS ADJACENT TO THE DAMAGE. THE CRACK WAS CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED TO REPAIR THE CUTOUT AND TO TIE-IN TO THE EXISTING REPAIR. THE REPAIR WAS ACCOMPLISHED PER ER/A 364475-14, REV A AND IS TIME- LIMITED.
Part: GROUND — LOOSE (CABIN)
ON L/O, FOUND RT SECTION D FLOOR TRACK LIGHTING INOP. SWAPPED BATTERIES AND CONTROLLER, NO HELP. SWAPPED CHARGERS, NO HELP. RANG OUT WIRES AND FOUND LOOSE GROUND STUDS, TIGHTENED. OPS CK GOOD.
1997
Part: COMPARATOR — FAILED (LE SLATS)
L/E SLATS LOCKED OUT AFTER T/O, SLATS WOULD NOT RETRACT. REPLACED SLAT COMPARATOR MONITOR.
Part: COUNTER BALANCE — WEAK (R-4 DOOR)
DURING ACCOMPLISHMENT OF OPN NR 68115 R/CARD 20 FOUND A WEAK COUNTERBALANCE ON THE R-4 DOOR. THE COUNTERBALANCE WOULD ONLY OPEN THE DOOR HALFWAY. MFG PART NR 1313T100-13 S/N 0371, REPLACED SAME.
Part: TRIPLER — CORRODED (FS 1545)
FUSELAGE C2 CARGO DOOR SURROUND, LOWER TRIPLER. REPAIR FOR CORROSION CUT OUT. THE C2 DOOR SURROUND TRIPLER WAS FOUND CORRODED JUST FWD OF FS 1545 AT STRG 29. TRIPLER CUTOUT RESULTED IN A 3.5 WIDE AREA REMOVED. REPAIR DOUBLER INSTALLED PER ER/A 363043-14.
1996
Part: POWER SUPPLY — INOPERATIVE (CABIN)
EMERGENCY LIGHTS AT L1/R1 DOOR INOP. REPLACED POWER SUPPLY, CK'S GOOD.
Part: ATTACH FITTING — CORRODED (LT MLG)
THE LT MLG RETRACT ACTUATOR RIB FITTING WAS FOUND WITH CORROSION. THE DAMAGE WAS CLEANED UP; SEVERAL FASTENER HOLES WERE SPOT-FACED. THE FITTING WAS EVALUATED AFTER CLEAN-UP AND IT WAS DETERMINED THAT IT COULD STILL CARRY THE INTENDED FLIGHT LOADS. *** REV A PROVIDES FAA APPROVAL TO REPAIR ***
Part: SKIN — CORROSION (FS 1363-1453)
THE BELLY SKIN FOR STA 1363 TO 1453 BETWEEN 31, 32, 34 AND 35 HAD CORROSION. THE REPAIR WAS ACCOMPLISHED PER SRM 53-31-00 FIG 827. REV A CHANGES INSTRUCTIONS AND ADDS DRAWING TO ALLOW DEVIATION FROM REFERENCE SRM.
Part: SKIN — CORROSION (BS 1361-1453)
DURING HMV, THE BELLY SKIN FROM FS 1363 TO 1453 BETWEEN STR 31 AND 32 AND BETWEEN STR 34 AND 35 WAS FOUND TO BE CORRODED. THE CORROSION WAS CUT OUT AND A REPAIR FILLER/DOUBER WAS INSTALLED.
Part: FAIRING SUPT — CRACKED (BS 1363-1443)
P/N 1518590-175 T, FOR FUSELAGE FAIRING SUPPORT STRUCTURE CRACKED AFT OF STA 1363. REPLACED.
Part: TRUCK POSITIONER — FAILED (LT GEAR)
AFTER TAKEOFF, GEAR HANDLE STUCK DOWN TRUCK LIGHT ON, OVERBD LIGHTS OUT. FLIGHT RETURNED ATL. REPLACED LT MLG TRUCK POSITIONER AND SERVICED HYD FUSE, OPERATION NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN)
FLOOR TRACK LIGHTING INOP IN AFT CABIN. REPLACED BATTERY PACK, OPERATION NORMAL.
1995
Part: EEL TRACK — MISSING (CABIN)
EMERGENCY TRACK LIGHT AT 12C IS MISSING. REPLACED TRACK AND LENS ASSEMBLY, CKS GOOD.
Part: MACH FEEL MOTOR — FAILED (AUTO FLT SYST)
DURING DEPARTURE APPROX 14,000 FT AND 280 KTS MACH FEEL, 1 AND 2 LIGHTS FAILED. LATER MACH TRIM 2 FAILED, RETURNED ATL. REPLACED BOTH MACH FEEL MOTORS, OPERATION NORMAL.
Part: TE CORNER — DAMAGED (RT WING)
DURING INSPECTION, RT WING SPOILER PANEL WAS FOUND WITH TRAILING EDGE CORNER DAMAGE APPROXIMATELY 6 INCH BY 6 INCH AREA TO TOP AND BOTTOM SKIN. ACCOMPLISHED BONDED REPAIRS PER SRM 57-52-00.