NTSB investigations · 1
Matched to this aircraft by N319NE and the event date: up to this one’s cancellation.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR I5PA2015102631902Line · unknownNUMBER 3 ENG EXPERIENCED OIL LOSS. OIL PRESS AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOOTING IN PROGRESS. ENG HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL. FOUND OIL SUPSDR I5PA2015102631901Engine · leakingNR 3 ENG EXPERIENCED OIL LOSS. OIL PRESSURE AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOT NR ENG OIL LOSS, ENG INITIALLY HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL FOR TRSDR FY4Y201307180003Bulkhead · corroded8C CHECK. DURING CPCP INSPECTION, CORROSION WAS FOUND. THE CORROSION DAMAGE THROUGH THE PART ON THE NOSE WHEEL WELL BS 294.5 BULKHEAD WEB.SDR FY4Y20130718197Frame · corroded8C CHECK. DURING CPCP INSPECTION, PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON LOWER ANGLE OF BS 950 CANTED BULKHEAD BETWEEN S22-23L. BLENDED OUT CORROSION, PENETRATION DEPTH WAS OVER LIMITS IAW SRM 53-10-1, FIG 1.SDR FY4Y20130718002Skin · corroded8C CHECKK. DURING PERFORMED CPCP INSPECTION, CORROSION WAS FOUND ON THE UPPER SKIN UPPER SURFACE OF THE WING CENTER SECTION, AT BS 783.95, BETWEEN RBL 63.0 AND RBL 65.5. CORROSION BLENDED OUT. THE DAMAGE CONDITION HAD EXCEEDED THE ALLOWABLE LIMITATION IAWSDR FY4Y197M20110919Beam · corrodedDURING PERFORM THE MAINTENANCE WORK (7C CHECK CARD NO.:C53-300-10 PART 1 OF 2), CORROSION WAS FOUND ON THE AFTER FLANGE OF THE LT HORIZONTAL STABILIZER T/E LOWER BEAM AT ELEV STA 156~160 AND ELEV STA 186.5~190. THE DEPTH AFTER BLENDOUT IS OUT OF LIMIT. THE ASDR FY4Y197M20100129Spar · corrodedTHE ACFT INPUT FOR 6C CHECK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE THICKNESS OF CORROSION REMOVED IS 0SDR FY4Y197M20100201Spar · crackedACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL: 0.370"; THICKNESS OF CORROSION REMSDR 2010FA0000078Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING VISUAL INSP BY INSPECTOR, THE LEVEL 2 CORROSION WAS FOUND ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE CHORD THICKNESS OF CORROSION REMOVED IS 0.040". PHOTO SDR 2010F00009Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL:0.370"; THICKNESS OF CORROSION REMOVEDSDR 2010F00008Skin · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON SKIN OF FWD CARGO DOOR CUTOUT AFT LOWER CORNER STA: BS620 S26R. AFTER APA (OWNER) VERIFY AS A MAJOR REPAIR ON JAN 29, 2010, THE SKIN CORROSION HAS BEEN REPAIRED IAW DER APPRSDR 2010F00007Skin · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON SKIN OF FWD CARGO DOOR CUTOUT AFT LOWER CORNER STA: BS 620 S26R. AFTER APA (OWNER) VERIFY AS A MAJOR REPAIR ON JAN 29, 2010, THE SKIN CORROSION HAS BEEN REPAIRED IAW FAA DERSDR 2010F00000Spar · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON RT WING FRONT SPART LOWER CHORD PLATE AT WS 482. AFTER REPAIRING TO THE FRON SPAR LOWER CHORD PLATE, FORM 337 WILL BE SUBMITTED TO FAA FOR FINAL RESULT OF CORRECTIVE ACTIONS DETAIL.SDR I5PA030809Transceiver · malfunctionedAIRCRAFT, AIR RETURNED DUE TO NR 1 AND NR 2 HF'S WOULD NOT TRANSMIT OR RECEIVE. CLEANED AND RESEATED BOTH TRANSCEIVERS, OPS CHECK WITH SFO NORMAL. OK FOR SERVICE NO FURTHER PROBLEMS