N759DA
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.
66 reports on file, 1995-02-12 – 1998-12-06.
Part: ENGINE — FLAMED OUT (NR 1)
NR 1 ENG FLAMED OUT AT 39000 FT. SHUTDOWN ENG PER POM. RELIGHT NR 1 PER POM. REPLACED ENGINE DRIVEN FUEL PUMP.
Part: AIR DISTR — ODOR (CABIN)
A/C DIVERTED COS DUE TO ODOR SIMILAR TO SULPHUR SMELL AT SEATS 22 AND 23 DF. A/C LANDED OVERWEIGHT 38K. CONTRACT MAINT INSPECTED AREA AND PERFORMED OVERWEIGHT LANDING INSP PER MM 5-50-01. NO DISCREPANCIES NOTED.
Part: FUEL PUMP — FAILED (NR 1 ENGINE)
NR 1 ENG FLAME-OUT AT FL 31.0, OIL FILTER PRESSURE LIGHT NOT ON. N3 ABOVE 20 PERCENT OTHER PARAMETERS WIND MILL NORMAL. USING CROSSFEED NR 3 TO NR 1 AT TIME WITH NR 1 FUEL BOOST PUMP OFF FUEL PRESS LIGHT ON MOMENTERILY ON FE AND PILOTS ANNUNCIATOR PANEL. RELIGHT SUCCESSFUL. REPLACED ENGINE FUEL PUMP.
Part: COMPUTER — MALFUNCTIONED (E/E COMPT)
AUTO SPOILERS DEPLOYED AT FL280. REPLACED FCES COMPUTER.
Part: COMPRESSOR — STALLED (NR 3 ENGINE)
JUST AFTER LEVEL OFF AT FL 370, NR 3 ENGINE HAD A PRESUMED COMPRESSOR STALL AND THE TGT WENT TO 850. ENGINE SHUTDOWN PERPOM. ESTIMATE TIME AT 850 TGT AT 5 SECONDS. REPLACED VIGV CONTROLLER. BOROSCOPES REVEALED NO DAMAGE.
Earlier reports · 1995–1997 · 61 reports
1997
Part: LIGHT — INOPERATIVE (CABIN)
AFT CABIN EMERGENCY LIGHTS FAIL TEST.
1996
Part: POWER SUPPLY — FAILED (CABIN)
AFT LT CEILING EMERGENCY LIGHTS FAIL TO TEST. REPLACED AFT LT POWER SUPPLY, LIGHTS CHECK NORMAL.
Part: CHECK VALVE — FAILED (2L FUEL TANK)
AFTER TAKEOFF, TOWER INFORMED FUEL WAS VENTING FROM LEFT WING. PASSENGER INFORMED OF FUEL VENTING FROM LEFT WING TIP. CONFIRMED THIS. 2L TANK NOT FEEDING. TURNED OFF 2R PUMP AND 2L STARTED TO FEED. TRIED TO FEED OUT OF TANKS 1 AND 3 AND QUANTITY IN 2L STARTED TO INCREASE. FIRM CODE 28-24-43-14. REPLACED BYPASS CHECK VALVE MANIFOLD TO 2L BOOST PUMP BOX. OPERATION CHECKS OK.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
TWO EMERGENCY LIGHT POWER SUPPLIES HAVE CHARGE LIGHT INOP. REPLACED POWER SUPPLIES.
1995
Part: FUEL FLOW REG — FAILED (NR 1 ENGINE)
DURING CRUISE FL 370, NR 1 ENGINE DID NOT RESPOND TO THROTTLE THEN FLAMED OUT, RESTARTED ON SECOND ATTEMPT, THEN FLAMED OUT AGAIN ON SHORT FINAL AT ORY. PER FIM 71-80-00, REPLACED NR 1 FUEL FLOW REGULATOR, OPERATION NORMAL.
Part: FUEL PUMP — FAILED (NR 1 ENGINE)
DURING CRUISE, HAD NR 1 ENGINE FUEL PRESSURE LIGHT ILLUMINATED, THEN ENGINE FLAMED-OUT, ALL AIR STARTS WERE UNSUCCESSFUL, DIVERTED TO KEF. REPLACED HP FUEL PUMP, OPERATION NORMAL.
Part: STRAP — CORRODED (BS 910)
AT HMV, FOUND CENTER STRAP TO BE CORRODED. INTERNAL CENTER STRAP AT STA 910 STR 33. REPAIRED PER SRM 53-31-00 FIG 825.
Part: STRAP — DISBONDED (FS 930)
AT HVM, FOUND TEAR STRAP DISBONDED AT FS 930 BETWEEN STR 31 AND 32. REPAIRED PER SRM 53-31-00 FIG 804.
Part: TEAR STRAP — DISBONDED (BS 930)
AT HMV,FOUND TEAR STRAP DISBONDED, STA 930 BETWEEN STRINGER 31 AND 32. PEELED TEAR STRAP BACK, NO CORROSION FOUND. INSTALLED REPAIR PER SRM 53-31-00 FIG 804.
Part: SPAR CAP — CRACKED (RT WING)
DURING HMV COMPLYING WITH AD 93-17-10 AND 94-05-01, CRACKS WERE FOUND IN THE RIGHT WING REAR SPAR UPPER CAP FASTENER HOLES AT IWS 293.58 AND IWS 346.109. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. REPAIR APPROVAL PER FAA AMC LETTER DATED 3/13/95.
Part: SKIN — CORRODED (BS 1605-1625)
AT HMV, FOUND FUSELAGE SKIN CORRODED UNDER TEARSTRAP BETWEEN STA 1605 AND 1625 AT STRINGER 29. REPAIRED PER SRM 53-31-00 PG 965.
Part: FAIL SAFE STRAP — DELAMINATED (C-1 COMPT)
AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 709-729 ABOVE STRINGER 40. REPAIRED PER SRM 53-31-00, PG 830.
Part: FAIL SAFE STRAP — DELAMINATED (C-1 COMPT)
AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED IN FWD CARGO AREA, FS 886-901 AT STRINGER 23, 30, AND 34. REPAIRED PER SRM 53-31-00 PG 830.
Part: SKIN — DENTED (FS 220)
AT HMV, FOUND FUSELAGE SKIN DENTED AT FS 220 BETWEEN STRINGERS 3 AND 4. REPAIRED PER SRM 53-31-0.
Part: SEAT TRACK — CORRODED (FS 1705/1725)
AT HMV, FOUND CABIN SEAT TRACK AT FS 1705 AND 1725, 4TH FROM LEFT SIDE, CORRODED. REPLACED TRACK, PER SRM 53-21-00.
Part: STRAP — CORRODED (C-2 COMPT)
AT HMV, C-2 STRAP COMMON TO STRINGER 33 IS CORRODED ON LEFT SIDE OF THE STRINGER, JUST AFT OF TEAR STRAP AT FS 1695. REPAIRED PER SRM 53-31-00.
Part: RIB CAPS — CUT (WS 293.38/319.83)
AT HMV, RIB CAPS AT IWS 293.38 AND 319.83 WERE CUT TO FACILITATE REMOVAL AND COLD WORK OF FASTENERS IN REAR SPAR REWORK. REF EO 7-59089-3. REPAIRED RIBS PER SRM 57-12-00.
Part: FAIL SAFE STRAP — DELAMINATED (C-1 COMPT)
AT HMV, FOUND C-1 FUSEALGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 889-869 BETWEEN STRINGERS 37 AND 30. REPAIRED PER SRM 53-31-00.
Part: LONGERON — CRACKED (FS 983)
AT HMV, FOUND LONGERON AT FS 983 BETWEEN STRINGERS 45 AND 46 CRACKED. REPLACED LONGERON.
Part: FLOORBEAM — CORRODED (FS 1823-1842)
FLOORBEAM STA 1823 TO 1842 LBL 71 LBL 44 CORRODED AT FLOOR PANEL ATTACH HOLES, TWO PLACES. DAMAGE FOUND AT HMV. REPAIRED PER SRM 53-21-00 PAGES 866 TO 868.
Part: STRINGER — CORRODED (FS 953)
AT OVERHAUL STRINGER 32 AT LOWER SIDE OF SKIN ATTACH FLANGE (FS 953) WAS FOUND CORRODED. INSTALLED NEW SECTION OF STRINGER WITH SPLICE REPAIR PER SRM 53-13-00, FIG. 804.
Part: FLOORBEAM — CORRODED (FS 886)
DURING HMV, FOUND CORROSION ON CABIN FLOORBEAM FS 886 RBL 30. REPAIRED PER SRM 53-21-00 PG 866-868.
Part: SEAT TRACK — CORRODED (FS 1665-1725)
DURING HMV, FOUND CABIN SEAT ATTACH TRACK CORRODED AT FS 1665 TO 1725 AT RBL 42. REPLACED TRACK PER SRM 53-21-00 FIG 820.
Part: SKIN — CORRODED (FS 629-649)
DURING HMV, FOUND LOWER FUSELAGE SKIN CORRODED AT FS 629-649 BETWEEN STRINGER 32 AND 34. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 FIG 825.
Part: ACT FITTING — DAMAGED (LT MLG)
AT HMV, FOUND HOLES DAMAGED IN LMLG ACTUATOR FITTING. DRILLED HOLES 17 THROUGH 20 TO .628 TO REMOVE DAMAGE. CORROSION REMOVED. ALL REMAINING WORK DONE ON JPC 031255.
Part: ACT FITTING — CORRODED (LT MLG)
AT HMV, FOUND HOLES CORRODED HOLES 1, 2, 4, 6, IN LMLG ACTUATOR FITTING CORRODED. REF TASK C-32-730-01. REAMED HOLES 1, 2, 4, 5 AND 6 TP .688. REMOVED DAMAGE AND TO FACILATATE MAINT ON HOLE NR 5, REAMED NR 3 .719 TO REMOVE DAMAGE. CORROSION REMOVED, ALL REMAINING WORK DONE ON JPC 031255.
Part: STRAP — DELAMINATED (C-1 COMPT)
C-1 B/B FAILSAFE STRAP DELAMINATED, F/S 749-769, STRINGERS 30 AND 34. ACTUAL LOCATION F/S 860, STRINGERS 30 AND 34. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 816.
Part: TEAR STRAP — DISBONDED (FS 860)
FS 860 TEAR STRAP DISBONDED BETWEEN STR 27-29 AND STR 35-36. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-00 PG 830.
Part: STATIC WICK — FAILED CHECK (BASES 34/43)
AT HMV, FOUND STATIC WICK BASES 34 AND 43 FAILED MEG CHECK. REPLACED STATIC WICK BASES 34 AND 43. REQ PANELS INSTALLED ON AC STATIC ARRESTER BASES.
Part: BLKHD FRAME — CORRODED (PRESS DOME)
AT HMV, FOUND P-DOME FRAME CORRODED AT LOWER END OVER A 2FT SECTION. AT THE FORWARD SIDE OF P-DOME LEFT SIDE JUST AFT OF AFT CARGO AREA STRINGER 41. REPAIRED PER SRM 53-11-00 FIG 809.
Part: BLKHD FRAME — CORRODED (PRESS DOME)
AT HMV, FOUND FRAME CORRODED ON P-DOME LOWER INBOARD SIDE JUST AFT OF WHERE STRINGER 25 ENDS. REPAIRED PER SRM 53-11-00 FIG 809.
Part: DECK — CORRODED (BS 359)
AT HMV, FOUND CORROSION DAMAGE ON PRESSURE DECK AT FS 359 LEFT OF FORWARD LAV 18 INCHES. REPAIRED PER SRM 53-11-00 FIG 840.
Part: STRAP — DISBONDED (C-2 COMPT)
TEAR STRAP DISBONDED - C-2 F/S 1735 BETWEEN STR 34 AND 35. REPAIRED PER SRM 53-31-00 PAGE 830. DAMAGE FOUND AT HMV.
Part: TEARSTRIP — DISBONDED (FS 1695/1635)
DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1695 STR 30-29, FS 1635 STR 38-39, FS 1635 STR 40-41.
Part: FLOORBEAM — CORRODED (FS 281)
DURING HMV, FOUND CABIN FLOOR SUPPORT BEAM AT FS 281 WITH CORROSION DAMAGE AT LBL 74 TO RBL 74. REPAIRED PER SRM 53-21-00 PG 823-824.
Part: FLOORBEAM — CORRODED (FS 901/923)
DURING HMV, FOUND CABIN FLOORBEAM AT FS 923 CORRODED AT LBL 31. REPAIRED PER SRM 53-21-00 PG 866-868,_AND FLOORBEAM AT FS 901 CORRODED AT LBL 42 AND 47. REPAIRED PER SRM 53-21-00 PG 849-852.
Part: FLOORBEAM — CORRODED (BS 1725)
DURING OVERHAUL, FOUND FLOORBEAM CORRODED AT STA 1725, LBL 34-58. REPAIRED PER SRM 53-21-00.
Part: TEARSTRIP — DISBONDED (FS 1735)
DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1735 STR 29-31. REPAIR PER SRM 53-31-00 FIG 804.
Part: FAIL SAFE STRAP — DELAMINATED (C1 COMPT)
AT HMV, FOUND FUSELAGE SKIN FAILSAFE TEAR STRAP DELAMINATED AT FS 809-829 AT STRINGERS 27, 31, AND 23. REPAIRED PER SRM 53-31-00 PG 830.
Part: FAILSAFE STRAP — DISBONDED (FS 1443/1535)
DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1443 BETWEEN STRINGESR 30 AND 31, AND FS 1535 BETWEEN STRINGERS 33-34. REPAIRED PER SRM 53-31-00 PG 830.
Part: FAIL SAFE STRAP — DELAMINATED (C-1 COMPT)
ITEM NR 1 C1 B/B-FAILSAFE STRAP DELAMINATED-F.S.729-749, STRINGERS NR 37 AND NR 34. ITEM NR 2 SAME AREA AT STRINGERS NR 31 AND NR 32, N.R. 484, CONT. ON N.R. 1514. CORRECTION: REMOVED CORROSION AT STRINGERS NR 32 AND NR 31 F.S. 729-749. THICKNESS OF STRINGERS NR 31 AND NR 32 STA. 749, .062 INCH, REMOVED EXPOSED ADHESIVE AT STR. 34, CUT STRAP AT STR 37, FABRICATED SPLICE. PAINTED ALL AREAS, DRILLED ATTACH PATTERN IN TEAR STRIP AT STR. 31-32. INSTALLED REPAIR AT STR. 37. INST. TACT PAT. AT STR 31-32 & INSTALLED SPLICE AT STR. 34 PER SRM 53-31-00 PG. 830.
Part: TEARSRTAP — DISBONDED (FS 1585-1605)
DURING OVERHAUL, FOUND TEARSTRAP DISBONDED AT STA 1585-1605 BETWEEN STR 29-31. REPAIRED SRM 53-31-00 FIG 816.
Part: TEARSTRIP — DISBONDED (FS 1605/809)
DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1605-1625 STR 32-33, FS 1605-1625 STR 33-34, FS 809-829 STR 31.
Part: FAILSAFE STRAP — DISBONDED (FS 1545-1565)
DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1545 TO FS 565 BETWEEN STRINGERS 30 TO 37. REPAIRED PER SRM 53-31-00 PG 830.
Part: ANGLE — CRACKED (NR 2 NACELLE)
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-00 PG 808.
Part: ANGLE — CRACKED (NR 2 NACELLE)
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP AND AFT). REPAIRED PER SRM 54-12-00 FIG 803.
Part: FAIL SAFE STRAP — DELAMINATED (FS 729-849)
AT OVERHAUL FOUND C-1 BAG BIN FAIL SAFE STRAP DELAMINATED AT FS 729-849, STR 37 AND 34 (SAME CONDITION AT STR 31-32). REMOVED CORROSION AND FABRICATED NEW SPLICE PER SRM 53-31-00 PG 830.
Part: TEAR STRAP — DISBONDED (FS 1605-1625)
AT HMV, FOUND TEAR STRAP DISBONDED C2 BIN BETWEEN 1605 TO 1625, STRINGER 29 AND 30. LIFTED TEAR STRAP AND REMOVED CORROSION, TREATED AND PAINTED AREA. FABRICATED AND INSTALLED REPAIR SPLICES PER SRM 53-31-00.
Part: STRAP — DISBONDED (BS 1605-1625)
AT HMV, FOUND TEAR STRAP DISBONDED AT FS 1605 AND 1625 BETWEEN STRINGER 29 AND 30. REPAIRED PER SRM 53-31-00 FIG 804.
Part: TEAR STRAP — DISBONDED (FS 1585-1605)
AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED IN C-2 STA 1585-1605, STR 35-37. REPAIRED PER SRM 53-31-00.
Part: TEAR STRAP — DISBONDED (FS 1565-1585)
AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED WITH CORROSION BETWEEN 1565-1585, AT STRINGERS 31-32. CLEANED CORROSION AND REPAIRED PER SRM 53-31-00 FIG 801.
Part: TEAR STRAP — DELAMINATED (FS 860)
C1 BB FAIL STRAP DELAMINATED AT STRINGER 23, 26 AND 28, FS 860. REPAIRED PER SRM 53-31-00 PG 830.
Part: TEAR STRAP — DISBONDED (FS 1585-1605)
AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT C-2 STA 1585-1605 STR 32-33. REPAIRED PER SRM 53-31-00 PG 801.
Part: TEAR STRAP — DISBONDED (FS 619)
TEAR STRAP AT FS 619 BETWEEN STR 29-30 IS DISBONDED. REPAIRED PER SRM 53-31-00 FIG 804. DAMAGE FOUND AT HMV.
Part: SKIN — CRACKED (LT TE FLAP VANE)
AT HVM, FOUND LEFT WING FLAP VANE WITH CRACK IN UPPER SKIN. DAMAGED WAS REMOVED AND REPAIRED PER SRM 57-53-00 FIG 806.
Part: SKIN — DENTED (FS 323)
DURING INSPECTION, FOUND LT FUSELAGE SKIN AT FS 323 DENTED BEYOND LIMITS. CUT OUT DAMAGE AND DYE CHECKED, FOUND NO CRACKS. C/W STEPS 3 AND 4 OF ERA 270330-14.
Part: SKIN — GOUGED (FS 182)
FUSELAGE SKIN GOUGED STA 182 BELOW L-2 COCKPIT WINDOW. FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 811. DAMAGE FOUND AT HMV.
Part: FAILSAFE STRAP — DISBONDED (FS 639/689)
DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 639 AND 689 BETWEEN STRINGERS 29, 30 AND 31 TO 35. REPAIRED PER SRM 53-31-00 PG 830.
Part: TEAR STRAP — DISBONDED (FS 619)
TEAR STRAP AT FS 619 BETWEEN STR 31-32 IS DISBONDED. REPAIRED PER SRM 53-31-00 FIG 804. DAMAGE FOUND AT HMV.
Part: BUSHING — MIGRATED (RT AILERON)
AT HMV, FOUND RT WING O/B AILERON, O/B PCA ATTACH POINT TO AILERON BUSHING IS MIGRATED. REPAIRED WORN LUGS AND REPLACED BUSHINGS PER SRM 57-55-00.
Part: TEAR STRAP — DISBONDED (FS 579)
AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 579 BETWEEN STRINGER 29 AND 30. REPAIRED PER SRM 53-31-00 PG 830.