N368PA, cancelled Dec 5, 1997

Service difficulty reports · 22

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N368PA' AND deregistration_id = 'N368PA-1997-12-05'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR EISA97106Switch · inopL/E FLAP NR 5 FAILED TO RETRACT AFTER TAKEOFF. REPLACED L/E NR 5 FLAP SWITCH PER MM 27-80. (M)Jun 3, 1997 · N368PA · Boeing 727221 · Leading Edge Slat Control SystemSDR EISA97083O-Ring · damagedNR 3 ENGINE HAD OIL LOSS ON FINAL. INDICATIONS AT SHUT DOWN, QTY 0, PRESSURE IN YELLOW BAND AND YELLOW OIL LIGHT ILLUMINATED. REPLACED DAMAGED O-RING ON OIL RETURN LINE ABOVE OIL SCREEN. LEAK CHECKED OK PER CHAPTER 71. (M)Apr 23, 1997 · N368PA · Boeing 727221 · Turbine Engine Oil SystemSDR EISA96286Relief Valve · out of adjustDURING TAKEOFF, NR 2 OIL PRESSURE ROSE ABOVE RED LINE (APPROX 80 PSPSI). TROUBLESHOT ENGINE OIL PRESSURE RELIEF VALVE AND ADJUSTED PER MM, LEAK AND OPS CHECK GOOD. (M)Dec 23, 1996 · N368PA · Boeing 727221 · Engine Oil PressureSDR EISA96282Outflow Vlv · inoperativeCABIN PRESSURE CONTROL SYSTEM MALFUNCTIONED IN CLIMB. FAILED IN STANDBY MODE TO FULL CABIN DESCENT, SWITCHED TO MANUAL DC FAILED OPS PER AOM VOL 1. REMOVED AND REPLACED OUTFLOW VALVE PER MM. OPS CHECK GOOD PER GROUND OPS PROCEDURE. (M)Dec 1, 1996 · N368PA · Boeing 727221 · Pressure Regulator/Outflow ValveSDR EISA96196Fitting · looseENGINE NR 3 OIL QTY BEGAN RAPIDLY DROPPING ON APPROACH AND OIL TEMPERATURE ENTERED YELLOW BAND. ENGINE SHUTDOWN ACCOMPLISHED APPROXIMATELY 1/4 GALLON REMAINING UPON LANDING. OIL SYSTEM INSPECTED, BANJO FITTING ON SYSTEM RETURN FOUND LOOSE. THREAD PITCH CHECOct 22, 1996 · N368PA · Boeing 727221 · Turbine Engine Oil SystemSDR EISA95431Channel · dentedAFT CARGO LOWER BILGE HAT CHANNEL DENTED, AT STATION 967 ABOVE AND BETWEEN STRINGER 30 AND 29L. REMOVED HAT CHANNEL AND DENT, FABRICATED REPAIR PER SRM 51-40-1 TREATED AND PRIMED PER 51-10-2. INSTALLED HAT CHANNEL PER SRM 51-10-2. (M)Nov 20, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95437Stringer · crackedSTATION 990, STRINGER 29R HAS CORROSION ON OUTBOARD FLANGE. REMOVED CORROSION AND FOUND 2 INCH CRACK. STOP DRILLED CRACK PER SRM 51-10-1. HFEC CONFIRMS CRACK CONTAINED, FABRICATED REPAIR PARTS AND INSTALLED PER CA22026-5068. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Main, Longeron/StringerSDR EISA95436Rib · crackedINSIDE VERTICAL STAB THROUGH ACCESS PANEL 9504, FOURTH COMPARTMENT UP FROM ENTRANCE, THE EIGHTH RIB FROM THE TOP IS CRACKED. REPAIRED CRACK IN RIB PER SRM 55-30-4. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Vertical Stabilizer, Spar/RibSDR EISA95435Tie Clip · crackedDITCHING PAN CLIP CRACKED, STATION 1183, BL 37 LEFT. REMOVED TIE CLIP AND FABRICATED PER SRM 51-30-2. TREATED, PRIMED AND INSTALLED PER SRM 51-10-2 AND 51-10-5. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95434Channel · crackCORROSION AT HAT CHANNEL UNDER RIGHT LAV DOOR WAY, APPROXIMATELY STATION 303-320. CORRODED HAT CHANNEL, FABRICATED NEW SECTION, INSTALLED PER SRM 51-30-2. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95433Skin · crackedVERTICAL STABILIZER RIGHT SIDE, JUST BELOW NR 7 VORTEX GENERATOR FROM TOP, SKIN CRACKED AT RIVET HEAD. STOP DRILLED CRACK PER SRM 55-30-3. HFEC CONFIRMED CRACK CONTAINED BY STOP HOLE. EXTERNAL DOUBLER INSTALLED AND SEALED PER SRM 55-30-3. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Vertical Stabilizer, Plate/SkinSDR EISA95432Flange · corrodedFOUND CORROSION, AT STRINGER 950D LOWER FLANGE. REMOVED FLANGE PER SRM 51-10-1, FABRICATED NEW FLANGE AND INSTALLED PER SRM 51-10-6 AND 51-10-2. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95430Angle · corrodedPRESSURE BULKHEAD STATION 1183, FORWARD SIDE RBL HORIZONTAL ANGLE AND TIE CLIP CORRODED. INSTALLED ALL PARTS, REMOVED AND FABRICATED PER SRM 51-81-1. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95429Tie Clip · crackedDITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 47. FABRICATED NEW TIE CLIP AND INSTALLED PER SRM 51-40. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95428Tie Clip · crackedDITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 37. REMOVED CLIP, FABRICATED NEW CLIP PER SRM 51-30-2, INSTALLED CLIP PER SRM 51-10-1. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95427Tie Clip · crackedDITCHING PAN TIE CLIP CRACKED AT STATION 1183, BL 27L. FABRICATED NEW TIE CLIP PER SRM 51-30-2. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95426Doubler · damagedREPAIR DAMAGED ELONGATED HOLE, STATION 600, TOP OF FORWARD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER 51-10-1, TREATED AND PRIMED AND INSTALLED DOUBLER PER 51-10-1 AND 51-30-1. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Miscellaneous StructureSDR EISA95425Skin · damagedREPAIR BENT DAMAGED STATION 580 TOP OF FWD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER IAW 51-10-1. TREATED PRIMED AND INSTALLED DOUBLER PER SRM 51-10-1. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Fuselage Main, Plate/SkinSDR EISA95424Panel · corrosionRT WING PANEL AT NR 7 SLAT ACTUATOR HAS EXFOLIATING CORROSION. REMOVED RIGHT WING PANEL, NR 7 SLAT FROM AIRCRAFT FABRICATED NEW HORSESHOE BRACKET AND FACE PANEL. TREATED, PRIMED AND INSTALLED NEW PANEL AND HORSESHOE BRACKET PER SRM 51-10-4. (M)Nov 18, 1995 · N368PA · Boeing 727221 · Wing, Plate/SkinSDR EISA95439Le Rib · corrodedCORROSION AT RIB AND STIFFENER INSIDE LEFT WING LE AFT OF NR 2 LE FLAP AND 14 INCHES OUTBOARD OF ACTUATOR. FABRICATED REPAIR PARTS PER SRM 51-40-4. INSTALLED PER SRM 51-40-4. (M)Nov 16, 1995 · N368PA · Boeing 727221 · Wing, Rib/BulkheadSDR EISA95438Rib · crackedCRACK INDICATION, FORWARD 2 FASTENER HOLES, BS 760 LBL 70.5 RIB CHORD VERTICAL FLANGE. REMOVED ANGLE AND SUPPORT. REMOVED FASTENERS FOR NDT, ACCOMPLISHED HFEC TO FASTENER HOLES. NO OTHER CRACKS NOTED. FABRICATED REPAIR ANGLE REF BAC DRAWING 65-68492, COMPLNov 16, 1995 · N368PA · Boeing 727221 · Wing, Rib/BulkheadSDR EISA95290Fuel Control · failedNR 3 ENGINE QUIT AT 800 FEET AFTER TAKEOFF, NO WARNING, SHUTTERED AND QUIT. REMOVED AND REPLACED NR 3 ENGINE FUEL CONTROL IAW 73-21-1. OPS AND LEAK CHECK GOOD IAW 72-00. TRIMMED NR 3 ENGINE IAW 71-00-97. (M)Oct 7, 1995 · N368PA · Boeing 727221 · Fuel Control/Turbine Engines
Back to N368PA, cancelled Dec 5, 1997