N751UP
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.
19 reports on file, 1995-07-31.
Part: LONGERON — CRACKED (FS 190-390)
WHILE IN DALFORT FOR C-CHECK, LONGERON 35L TWO CRACKS, 28 INCHES LONG OUTBD SIDE AND 18 INCHES ON INBD SIDE, FS 190 TO 390. REPLACED LONGERON SECTION PER SRM 51-1-20D.
Part: LONGERON — CORRODED (FS 1620-1660)
WHILE IN DALFORT FOR C-CHECK, HEAVY CORR AT LONGERON 30R, FS 1620 TO 1660. REPLACED LONGERON SECTION PER 51-1-20D.
Part: LONGERON — CRACKED (FS 1140)
WHILE IN DALFORT FOR C-CHECK, LONGERON 21L HAS 3 CRACK AT RADIUS FS 1140. REPAIRED LONGERON PER SRM 53-2-5.
Part: SUBFLOOR — CORRODED (FS 16)
WHILE IN DALFORT FOR C-CHECK, COCKPIT SUBFLOOR WEB CORROSION REMOVAL OUT OF LIMITS, FS 16 LBL 48. REPAIRED PER UPS EO DC8-53-1417.
Part: LONGERON — CRACKED (FS 340-360)
WHILE IN DALFORT FOR C-CHECK, LONGERON 36 RT SECTION CRACKED FS 240 TO 360 AND LT SIDE FS 340 TO 360. REPLACED LONGERON SECTION PER SRM 51-1-20D.
Part: SUBFLOOR — CORRODED (FS 16)
WHILE IN DALFORT FOR C-CHECK, HEAVY CORR ON COCKPIT SUBFLOOR WEB UNDER F/E'S INSTRUMENT PANEL FS 49 TO 15 OUTBD CORNER. REPAIRED PER UPS EO DC8-5310-7208A.
Part: FITTING — CRACKED (RT TE FLAP)
WHILE IN DALFORT FOR C-CHECK, RT FLAP STA 98 FITTING ON INBD SIDE HAS A 1 INCH CRACK. REPLACED FITTING PER SRM 51-1-20D.
Part: LONGERON — CRACKED (FS 390)
WHILE IN DALFORT FOR C-CHECK, LONGERSON 34R HAS 4 INCH CRACK INBD SIDE FS 390 AND A 15 INCH CRACK FS 200 TO 250. REPLACED LONGERON SECTION PER SRM 51-1-20D.
Part: SKIN — CORRODED (FS 70-140)
WHILE IN DALFORT FOR C-CHECK, CORR BULGE ON BELLY SKIN FS 70 TO 140 BETWEEN LONGERONS 35L AND 34R. REPLACED BELLY SKIN PANEL FS 70 AND 190 PER SRM 51-1-21.
Part: LONGERON — CORRODED (FS 1558)
WHILE IN DALFORT FOR C-CHECK, LONGERON 23L HAS HEAVY CORROSION AT FS 1558. REPAIRED LONGERON PER SRM 53-2-2, FIGURE 10.
Part: LONGERON — CRACKED (FS 120)
WHILE IN DALFORT FOR C-CHECK, LONGERON 33R CRACKED 1 INCH LONG AT FS 120. REPLACED LONGERON SECTION FS 70 TO 180 PER SRM 51-1-20D.
Part: LONGERON — CRACKED (FS 120-180)
WHILE IN DALFORT FOR C-CHECK, LONGERON 32R CRACKED 7 INCHES LONG AT FS 120, 140, 160, AND 180. REPLACED LONGERON SECTION FS 20 TO 190 PER SRM 51-1-20D.
Part: DOUBLER — CRACKED (FS 1350)
WHILE IN DALFORT FOR C-CHECK, FINGER DOUBLER CRACKED AT FS 1350 LONGERON 32R. REPLACED FINGER DOUBLER PER SRM 51-1-20D.
Part: JAMB — CRACKED (FS 1360)
WHILE IN DALFORT FOR C-CHECK, X-RAY REVEALS 1 CRACK IN RT T3 DOOR UPPER AFT CORNER FS 1360, UPPER AFT RADIUS OF DOOR JAMB. REPAIRED JAMB PER SRM 53-2-0.
Part: SPLICE — CORRODED (FS 1560)
WHILE IN DALFORT FOR C-CHECK, AFT ASSY COMPT HAS HEAVY CORR ON LONGERON SPLICE FS 1560, LONG 30R. REPAIRED PER SRM 53-2-2 FIG 10.
Part: LONGERON — CRACKED (FS 390)
WHILE IN DALFORT FOR C-CHECK, LONGERON 35R INBD SIDE HAS 8 INCH CRACK AT FS 390. REPLACED LONGERON SECTION FS 100 TO 390 PER SRM 51-1-20D.
Part: SPLICE — CORRODED (FS 1540-1560)
WHILE IN DALFORT FOR C-CHECK, MODERATE CORR AT LONGERON 32L SPLICE BETWEEN FS 1540 TO 1560. REPAIRED SPLICE PER SRM 53-2-2 FIG 10.
Part: DOUBLER — CORRODED (FS 1620-1680)
WHILE IN DALFORT FOR C-CHECK, INNER DOUBLERS HAVE HEAVY CORR BELOW AFT SERVICED AIR ENTRY DOORS. REPLACED DOUBLERS PER SRM 51-1-20D, AND SRM 51-1-21.
Part: FITTING — CRACKED (FS 420)
WHILE IN DALFORT FOR C-CHECK, BELT FRAME END FITTING CRACKED AT FS 420 FWD SIDE, LONGERSON 21L LOWER. REPLACED FITTING PER SRM 51-1-20D.