N902DL
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.
13 reports on file, 1995-06-22 – 2006-05-17.
Part: SKIN — GOUGED (FUSELAGE) · airframe 51,984 hrs · 42,512 cycles
THE FUSELAGE SKIN BELOW THE AFT CORNER OF THE C-3 CARGO DOOR CUTOUT WAS DAMAGED BY CONTACT WITH GSE. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 51,947 hrs · 42,480 cycles
LT HYD SYS LOST HYD PRESS FOLLOWED BY LT SYS HYD LOSS. FOUND FLEX PRESSURE LINE INBD OF LEFT PYLON LEAKING. REPLACED SAME. REPLACED NR 1 EDP. LEFT ENG LK CK OK PER MM. REPLACED CASE DRAIN AN PRESSURE FILTERS FOR LEFT ENGINE. LK CK GOOD. C/W IN FLIGHT FLUID LOSS CK PER M/M 29-00-01 PG 201.
Earlier reports · 1995–2004 · 11 reports
2004
Part: SKIN — DENTED (FUSELAGE) · airframe 45,980 hrs · 38,153 cycles
DENTS IN FUSELAGE STA 223 BETWEEN STR 17L & 18L. ALSO DENTS AT FS 218-227 BETWEEN STR 18L & 19L. ALL DENTS REPAIRED PER DRD 53-04D FIG 12B SHT 34 - 36 & 95 PG 60F. THE A/C RECEIVED THE FWD 2 REPAIRS AND THE UPPER AFT REPAIR AS ILLUSTRATED IN THE FIGURE.
2003
Part: GENERATOR — DEFECTIVE (NR 2 ENGINE) · airframe 44,696 hrs · 37,259 cycles
AS WE REACHED CRUISE ALT NOTICED RIGHT CSD OUTLET OIL TEMP ABOVE RED ARC FOLLOWED POM PROCEDURE. TURNED RIGHT GEN OFF, STABILIZED ABOUT 130 DEG. FREQ 394 398 WITH GEN SW OFF. CSD RISE IN CAUTION UNTIL GEN TURNED OFF/ T/S NR 2 ENGINE IAW MM 24-10-00-01 R/R TEMP SENSOR IAW MM RAN ENGINE FOR 5-7 MINS OPS CKS NORMAL.
2002
Part: APU — CONTAMINATED (APU BAY) · airframe 43,182 hrs · 36,204 cycles
JUST AFTER TAKE OFF FLT ATTENDENTS REPORTS HEAVY SMOKE ODOR THROUGH OUT CABIN. CREW RETURNED TO PNS. FOUND APU INLET CONTAMINATED WITH HYD FLUID. AIRCRAFT MTC FERRIED TO ATL. ATL MTC COMPLIED WITH OPN 5089 DUCT BURNOUT AND CLEANED APU INLET. ATL MTC UNABLE TO FIND ANY HYD LEAKS.
1999
Part: TIRE — WORN (NLG)
ON T/O, EXCESSIVE NOSE WHEEL SHIMMY FOLLOWED BY VIBRATION WHEN NOSE WHEEL SLOWED AGAINST SNUBBERS, BURNING RUBBER SMELL WAS EVIDENT FOR 3-5 MIN ON CLIMBOUT. CLEANED NOSE WHEEL SNUBBERS AND REPLACED NOSE WHEEL ASSY.
Part: SEPARATOR BAG — FAULTY (CABIN COOLING)
STRONG SMOKE ODOR IN AIRCRAFT. AFT SMOKE DET WENT OFF. REPLACED RT ACM PER M/M, PERFORMED DUCT BURN OUT. REPLACED WATER SEPARATOR BAG, LEAK CKS GOOD.
1997
Part: LENS — MISSING (CABIN)
EMERGENCY TRACK LIGHTING IS INOP BY DOOR 2L FRC335-04653. FOUND THAT LIGHTS DO OPERATE NORMALLY. HOWEVER,THEY NEEDED 2 EA RED LENS TO BE INSTALLED. INSTALLED SAME.
Part: SKIN — DENTED (BS 1360)
DENT FOUND IN FUSELAGE SKIN BETWEEN FS 1340 AND 1380, BETWEEN L22R AND 23R. DENT WAS APPROX 41 BY 1.5 WITH A DEPTH OF 0.100. DAMAGE WAS REPAIRED PER ERA 330856-14.
Part: FITTING — CORRODED (RT SPOILER)
RHS OUTB'D FLIGHT SPOILER CENTER HINGE FITTING WAS FOUND TO HAVE CORROSION IN THE BORE THAT ACCEPTS THE ASBY10-18 BEARING. REPAIRED PER ERA 330842-14.
Part: BOLT — SHEARED (LT MLG ACTUATOR)
LT MLG LWR ACT/BOTTOM BOLT SHEARED. FOUND DURING LUBE. REPLACED LWR BOLT ASSEMBLY AND LUBED PER M/M. VISUALLY INSPECTED UPPER BOLT, NO DAMAGE NOTED.
1996
Part: THRESHOLD — CORRODED (CARGO DOOR)
FOUND ON D1 LTR CHECK, CORROSION AT MID CARGO DOOR THRESHOLD. REPAIRED PER SRM 53-05 FIG 63.
1995
Part: FRAME — CRACKED (LT MLG WW)
FOUND DURING C-2 LETTER CHECK, 2 INCH CRACK AT MAIN WHEEL WELL FWD FRAME O/B END. REPAIRED PER SRM 53-05 FIG 78A.