N785DL
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.
12 reports on file, 1995-04-19 – 1996-06-27.
Part: SKIN — CORROSION (BS 699/729)
THE BELLY SKIN AT FS 669 AND FS 729 AND STR 33 TO 35 WERE FOUND WITH SEVERAL AREAS OF CORROSION DURING RETIREMENT IN ATL. THE CORROSION WAS CUT OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
FLOOR TRACK LIGHTS INOP IN D-ZONE. REPLACED POWER SUPPLY (P/N 337001090), OPS CHECK NORMAL.
Part: BULB — BROKEN (L3 DOOR)
ON LAYOVER, FOUND EXTERIOR LIGHT ON L-3 DOOR EMERGENCY LIGHTING SYSTEM INOP. RELAMPED LIGHT, OPERATION NORMAL.
Part: FRAME — DAMAGED (FS 1343)
DURING ACOMPLISHMENT OF S.I. 7-69903-12, FOUND TWO EXISTING FASTENER HOLES IN THE FRAME WEB AT FS 1343 WERE DAMAGED. THE TWO HOLES WERE O.S. TO .437 INCH PER DL ERA 271920-14AD.
Part: RIB — CRACKED (WS 555)
THE LT WING WAS FOUND WITH 4 CRACKS ON CASTELLATION OF THE IWS 555 UPPER RIB CAP, FOUND AT HMV. REPAIRS ACCOMPLISHED PER DL ERA 270733.
Part: PANEL — DELAMINATED (NR 4 SPOILER)
DURING SHOP INSPECTION, NR 4 SPOILER PANEL WAS FOUND WITH DELAMINATION. REPAIRED PANEL PER LAC DWG 1529104190.
Part: FAN — FAILED (GALLEY)
DURING DESCENT, HAD STRONG ELECTRICAL BURNING ODOR MID CABIN AND LOWER GALLEY AREA. FOUND GALLEY EXHAUST FAN C/B C-11 TRIPPED WILL NOT RESET. REPLACED GALLEY EXHAUST FAN, OPERATION NORMAL.
Part: VANE — CRACKED (NR 2 TE FLAP)
NR 2 LT FLAP VANE, UPPER SKIN CRACKED. REPAIRED PER SRM 57-53-00 FIG 806, FOUND AT LETTER CHECK.
Part: TR ANGLE — CRACKED (NR 2 ENGINE)
T/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802. UNDERLYING BULKHEAD REPAIR SPLICE ANGLE DAMAGE PER RB-211-22B ENGINE MANUAL 78-32-07 FIG 78-32-07-990-012.
Part: SKIN — CRACKED (FUSELAGE)
SKIN CRACKED AT HINGE CUTOUT FWD OF ACS GROUND SERVICE DOOR. REPAIRED PER SRM 53-31-00 FIG 828.
Part: PANEL — CRACKED (LT ELEVATOR)
DURING INSPECTION, FOUND LEFT ELEVATOR LOWER SURFACE WITH NUMEROUS RIVETS LOOSE AT T/E PANEL O/B END. ALSO, AFT O/B CORNER OF SAME PANEL IS CRACKED. REPAIRED PER SRM 55-22-00.
Part: SLEEVE — DAMAGE (NR 2 ENGINE)
T/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802 PG 803 AND UNDER LYING BULKHEAD. REPAIRED SPLICE ANGLE DAMAGE PER 222B ENG MANUAL 78-32-07 FIG 990-012.