NTSB investigations · 1
Matched to this aircraft by N364PA and the event date: up to this one’s cancellation.
FAA incident reports · 6
FAA accident and incident reports matched to this aircraft by N364PA and the event date: up to this one’s cancellation.
Incident 20040117010689INormal Cruise · Kinston, NC(-23) On January 17, 2004 on a routine flight from bos to cancun mex at 31000, flight 8510 with 149 passengers and 8 crew members had a forward cargo compartment fire warning light come on. The flight crew followed the emergency checklist procedures. ATC was…Incident 20010320004809ITo Init Climb(1st Pwr Reduct) · Belleville, IL(-23) Upon departure from blv, during landing gear retraction, the crew heard a loud clunk and the nose gear would not fully retract. The gear was extended and the aircraft returned and landed at blv. Post landing inspection found the left forward nose gear…Incident 20001122021539IFinal Approach · Pittsburgh, PA(-23) On November 22, 2000, a B-727, s/n 21107, registered as N364PA, and operated as "riva" flight #63, landed at "pit" after reporting an anti-skid problem while inbound to landing. The a/c landed at "pit" and taxied to the gate without incident.…Accident 20000728008539ACharleston, SC(-23) Pan am flight 164 departed sanford (sfr), FL, at 2053Z destined for pittsburg (pit), PA. While maneuvering between cells 60 miles south fo the cae VORTAC, pan am flight 164 experienced severe turbulence. The PIC diverted into Charleston international…Incident 20000502019559INormal Cruise · Pittsburgh, PA(-23)While enroute from portsmouth, ma to Pittsburgh, PA over albany, PA, the #3 starter valve light illuminated. The power reduced and the light went out. After a short time the light illuminated again. The pilot shut down #3 engine, and declared an…Incident 19870608046289IInitial Approach-IFR · New York, NYThe NR1 leading edge flap failed to extend properly. A safe landing was made. Flap actuator was replaced.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2004F00407Housing · crackedDURING CHARGER FLT FROM CANCUN-BOS, B HYDRAULIC SYSTEM PRESSURE WENT TO ZERO, BOTH NR 1 AND NR 2 PUMP LOW PRESSURE LIGHTS ON. DUMPED 20,000 LBS OF FUEL AND DIVERTED TO MCO. FOUND B HYDRAULIC SYSTEM CASE DRAIN FILTER HOUSING CRACKED. REPLACED FILTER AND HOUSSDR RIV2004F00000Actuator · leakingFLIGHT CREW WAS UNABLE TO EXTEND THE RT MLG ON AC. DURING INITIAL APPROACH, THE APPROACH WAS ABORTED AND THE CREW ALLEGEDLY ACCOMPLISHED ALL APPROPRIATE CHECKLIST ITEMS. THE RT MLG WOULD STILL NOT EXTEND USING THE MANUAL EXTENSION SYSTEM, ( THE GEAR APPEAREDSDR RIVA0000013Regulator · activatedAFTER DEPARTURE FROM SFB, CREW FOUND OXYGEN WAS DEPLETED. AIRCRAFT RETURNED TO SFB WITHOUT INCIDENT. THE FLIGHT ENGINEERS REGULATOR SWITCH WAS FOUND TO BE IN THE ON POSITION. RETURNED THE FLIGHT ENGINEERS REGULTOR SWITCH TO THE OFF POSITION AND SERVICED THESDR RIVA0000012Starter · damagedWHILE EN ROUTE TO PIT, NUMBER 3 ENGINE START VALVE LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AS PER SUPPLEMENTARY PROCEDURES. THE AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE STARTER TO BE DAMAGED. THE STARTER AND START VALVE WERSDR RIVA0000009Fitting · corrodedDURING REPLACEMENT OF L1 DOOR PLATE GUIDE ASSEMBLY AND ARM ASSEMBLY, THE UPPER FUSELAGE SUPPORT FITTING FOR THE UPPER DOOR HINGE (BODY STATION 310, WATER LINE 260) WAS FOUND TO BE CORRODED. REPAIR BY REPLACEMENT OF UPGRADED PART (PART NUMBER 50-9327-5) IN ACCSDR RIVA0000007Angle · crackedNR 4 SLAT REAR LOWER ANGLE, WS 191 TO WS 198, CRACKED 7 INCHES ALONG PREVIOUS REPAIR. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3, FIG 1. REMOVED ANGLE IAW BSRM 51-30-2. FABRICATED REPAIR ANGLE USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED REPAIR ANGSDR RIVA0000006Rib · crackedNR 4 SLAT, OTBD RIB WS 198 CRACKED, 1 INCH LONG. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3. CUT OUT DAMAGED AREA OF RIB. FABRICATED DOUBLER USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED ANGLE USING .063 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TSDR RIVA0000005Skin · gougedRIGHT OTBD T/E FOREFLAP HAD GOUGE IN L/E AT WS 550. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 57-50-4, FIG 1. REMOVED DAMAGED AREA. FABRICATED DOUBLER FROM .050 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TREATMENT IAW BSRM 51-10-2. INSTALLED DOUBLER. RESDR RIVA0000004Skin · dentedDENT IN LOWER SKIN OF LT OTBD AILERON AT WBL 540.2 INCHES BEHIND FRONT SPAR. INSTALLED FLUSH PATCH REPAIR DOCUMENTED IN THE BOEING SRM 57-50-5. REMOVED DAMAGED SECTION OF SKIN. FABRICATED DOUBLER AND FILLER FROM .020 INCH 7075 T-6 ALUM. APPLIED PROTECTIVE SDR RIVA0000003Rib · crackedDAMAGE TO RT WING OTBD AFT FLAP, OTBD CONTROL ROD ATTACH BRACKET AND L/E RIB AT WBL 464. REPAIRED RIB AND BRACKET BY REPLACEMENT. USED REPAIR DOCUMENTED IN BOEING SRM 57-50-4 FOR L/E SECTION REMOVED TO GAIN ACCESS. REMOVED L/E SKIN SECTION, FABRICATED DOUBLSDR RIVA0000002Rib · crackedNR 5 LEADING EDGE SLAT INBOARD RIB, AT ACUATOR ATTACHMENT WS 234 IS CRACKED. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED DOUBLER FROM .050 INCH 2024-T3 ALUMINUM. APPLIED PROTECTIVE TREATMENT TO ALL PARTS AS REQUIRED. INSTALLED DOUBLER. REBALANCE
Other aircraft with N364PA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N364PA is registered now to the first aircraft listed.