N880DP
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.
10 reports on file, 2004-06-26 – 2013-07-31.
Part: ANGLE — DAMAGED (RT WING)
DURING SCHEDULED INSPECTION, FOUND ELONGATED HOLE IN LOWER RT WING ANGLE FITTING AT XRS 69 BETWEEN S15-16R.
Part: CUSP WEB — CRACKED (BS 1338)
DURING SCHEDULED INSPECTION, FOUND AFT CABIN BS 1338, LT CUSP WEB LIGHTNING HOLE CRACKED AT TWO AREAS.
Part: FLOOR SUPPORT — CRACKED (ZONE 100)
DURING SCHEDULED INSPECTION, FOUND UPPER FLANGE OF CABIN FLOOR SUPPORT CRACKED AT BS 796 BL 0.
Part: STRUCTURE — LOOSE (WING TIP)
DURING SCHEDULED INSPECTION, FOUND RT WING TIP (LOWER SIDE, AFT, INBD) HAS LOOSE/SMOKING RIVETS.
Part: FRAME — CRACKED (ZONE 600)
DURING SCHEDULED INSPECTION, FOUND RT OVERWING FRAMES STA 886.0 FOUND CRACK APPROX .300 IN LENGTH. CRACK TIP OUTSIDE SHADOW OF FASTENER HOLE, CRACK FALLS UNDER CONDITION 3 OF THE SB MD80-53A01, PAGE 16.
Part: FRAME — CRACKED (PAX DOOR) · airframe 36,183 hrs · 30,376 cycles
INTERCOSTAL FRAME CRACKED IN RADIUS FORWARD END OF FORWARD PASSENGER DOOR VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REPAIRED INTERCOSTAL IAW DC-9 SRM 52-05. REINSTALLED DOOR STOP IAW DC-9 SRM 51-30-1.
Part: SUPPORT — CRACKED (RT WING SLAT) · airframe 36,183 hrs · 30,376 cycles
LEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.
Part: FRAME — CRACKED (PAX DOOR) · airframe 36,183 hrs · 30,376 cycles
INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM THIRD LIGHTENING HOLE FROM TOP. STOP DRILLED CRACK AND REPAIRED PASSENGER DOOR NR 2 BEAM AFT END IAW DC-9 MM.
Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 36,183 hrs · 30,376 cycles
INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REMOVED FITTING AND STOP FOR REPLACEMENT AND REPAIR, FABRICATED PART IAW REA D952-50078. PRIMED AND PAINTED REINSTALLED IAW DC-9 SRM 52-05.
Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 36,183 hrs · 30,376 cycles
PYLON LEADING EDGE LOWER ATTACH ANGLE ON FUSELAGE CRACKED. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-2.