Boeing 727-227

Service difficulty reports · 5,082

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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 aircraft_model_key = '727227'
  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 95ZZZX3957Oil Cap Packing · failedAIRCRAFT DIVERTED TO FLL DUE TO INDICATED LOSS OF OIL IN NR 3 ENGINE. OIL QUANTITY INDICATOR STABILIZED AT 1.5 GA., TEMP AND PRESS OK (NO ENGINE SHUT-DOWN). FOUND PACKING BLOWN OUT AT SERVICE CAP AND REPLACED. LEAK CK OK.Jun 24, 1995 · N307AS · Boeing 727227 · Turbine Engine Oil SystemSDR CAL950521Seal · brokenMCO - FLT 1978 - AIRCRAFT RETURNED TO AIRPORT DUE TO NLG DOOR INDICATION AND AIR NOISE. MAINTENANCE FOUND SEAL AT LEADING EDGE OF DOOR LOOSE AND JAMMING UNDER DOOR WHEN CLOSED. RESECURED SEAL AND PERFORMED EXTENSION AND RETRACTION TEST OF DOOR AND GEAR, OPERJun 23, 1995 · N76752 · Boeing 727227 · Landing Gear DoorsSDR 95ZZZX4051Eel · inoperativeGUM - THE R-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING B-CHECK. THE R-2 DOOR EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED PER MM 33-50-101 AND OPERATION CHECKED GOOD.Jun 21, 1995 · N86426 · Boeing 727227 · Emergency LightingSDR CAL950496Eel Battery Pack · dischargedEWR - FLT 0623 - INSPECTION FOUND EMERGENCY EXIT LIGHT AT LEFT AFT SERVICE DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (X)Jun 16, 1995 · N76753 · Boeing 727227 · Emergency LightingSDR SCNA95127Switch · failedTAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED. AIRCRAFT RETURNED TO GATE, FOUND UPPER STABILIZER TAKEOFF WARNING SWITCH S532 BAD. REMOVED AND REPLACED SWITCH PER MM 31-26-24 PAGE 401. SYSTEM OPS CHECKED GOOD.Jun 5, 1995 · N275AF · Boeing 727227 · Stabilizer Position IndicatingSDR 95ZZZX5195Fire Loop · out of positionMCD - ON CLIMB-OUT GOING THROUGH FL 290, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, C/W ABNORMAL PROCEDURES. CLEANED ELECTRICAL CONNECTOR ON FIRE LOOP (AFT BODY). RESPOSITIONED AFT BODY FIRE LOOP. TESTS OK.Jun 1, 1995 · N769AT · Boeing 727227 · Fire DetectionSDR AALA950978Eel Strip · defectiveDFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED 10 FEET OF EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)May 30, 1995 · N729AA · Boeing 727227 · Emergency LightingSDR CAL950461Floorbeam Brace · crackedGSO - INSPECTION FOUND A 1.3 INCH CRACK IN FORWARD LAVATORY FLOORBEAM BRACE. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-21 AND 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, Floor BeamSDR CAL950460Le Structure · crackedGSO - INSPECTION FOUND THE LEFT WING LEADING EDGE CAVITY NR 1 SLAT ACTUATOR INBOARD ATTACH AREA CRACKED AT MOUNT BOLT. THE CRACK WAS .5 INCH LONG. A SUPPORT RIB REPAIR WAS INSTALLED IAW ECRA 557C187. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing Main, Frame StructureSDR CAL950459Angle · crackedGSO - A .25 INCH CRACK WAS FOUND IN THE RT WING LEADING EDGE CAVITY AT STATION 118 WEB LOWER ATTACH ANGLE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing Miscellaneous StructureSDR CAL950458Skin · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN RT WING FIXED LEADING EDGE ABOVE CUTOUT FOR NR 6 SLAT OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing, Plate/SkinSDR CAL950456Web · crackedGSO - INSPECTION FOUND THE RT OUTBOARD MID-FLAP INBOARD END WEB CRACKED AT TWO PLACES. BOTH CRACKS WERE .5 INCH LONG. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Trailing Edge FlapsSDR CAL950455Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN WEB LOWER ATTACH ANGLE OF RT WING LEADING EDGE CAVITY AT STATION 119. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing Miscellaneous StructureSDR CAL950454Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN FRAME AT UPPER LIP IN AFT CARGO HOLD STATION 990, BETWEEN S27L AND S28L. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-3. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, FrameSDR CAL950453Stringer · corrodedGSO - INSPECTION FOUND STRINGER 28L CORRODED UNDER FLOOR SUPPORT IN FORWARD PIT AT STATION 570. THE CORRODED AREA OF STRINGER WAS CUT OUT IAW SRM 53-10-3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR CAL950452Angle · crackedGSO - A .80 INCH CRACK WAS FOUND IN THE LOWER FUSELAGE INTERCOSTAL SUPPORT ANGLE AT BS 720. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-20-4. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CAL950451Floorbeam · corrodedGSO - INSPECTION FOUND THE FLOORBEAM CORRODED AT FS 1110, RBL 20-RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS CUTOUT IAW ECRA 5310-01102. A SPLICE T-CHORD, FOUR ANGLE SPLICES, AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5310-01102 AND SRM 51-30-2. (MMay 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, Floor BeamSDR CAL950450Floor · corrodedGSO - THE FLOORBOARD SUPPORTS, FLOORBEAM, AND ATTACHING WEB IN AFT GALLEY AREA AT STATION 1130-1140 WERE FOUND CORRODED. THE CORRODED SECTIONS WERE REMOVED IAW ECRA 5310-01508. REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-01508 AND SRM 51-30-2. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Floor PanelSDR CAL950449Skin · crackedGSO - INSPECTION FOUND RT WING LEADING EDGE CAVITY INTERIOR OF LEADING EDGE SKIN CRACKED AT RIVET HOLES AT STATION 90. THE CRACK WAS .25 INCH LONG. THE CRACK WAS STOP DRILLED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED PER ECRA 5720-01064. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing, Plate/SkinSDR CAL950448Stringer · crackedGOS - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING UPPER STRINGER S10 AT WS 656.50. THE STRINGER WAS REPAIRED IAW EA 5762-01050. (M)May 24, 1995 · N70755 · Boeing 727227 · Wing, Longeron/StringerSDR CAL950447Chord · corrodedGSO - THE MAIN CABIN BS 1183 BULKHEAD REINFORCEMENT CHORD AT BS 1176.9 AT RT CUSP TO AFT ENTRY DOOR CUTOUT HAD CORROSION AND BLUE WATER STAINS. THE REINFORCEMENT CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-1. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, BulkheadSDR CAL950446Skin · corrodedGSO - INSPECTION FOUND ACTUATOR ACCESS PANEL AND LOWER FUSELAGE BL 0, BS 720 SKIN CORRODED AT RT RAM AIR SCOOP. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. THE ACCESS PANEL WAS REPLACED WITH A NEW PANEL IAW SRM 51-10-1. (M)May 24, 1995 · N70755 · Boeing 727227 · Fuselage Main, Plate/SkinSDR SCNA95104Eel Assy · inoperativeAFT AIRSTAIR OVERHEAD EMERGENCY LIGHT FOUND TO BE INOPERATIVE. REPLACED BATTERIES IN LIGHT ASSEMBLY OPS CHECK GOOD.May 20, 1995 · N275AF · Boeing 727227 · Emergency LightingSDR CAL950408Duct · rupturedFLT NR 0238 - SFO - THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF FROM SFO. WHEN THE THROTTLE WAS REDUCED THE WARNING CEASED, BUT UPON INCREASING POWER THE WARNING WOULD ACTIVATE AGAIN. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WMay 19, 1995 · N15774 · Boeing 727227 · Pneumatic Distribution SystemSDR CAL950397Hyd Pump · leakingFLT NR 0693 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 HYMay 18, 1995 · N17773 · Boeing 727227 · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZM218Switch · failedMDW - SMOKE AND ELECTRICAL SMELL IN THE COCKPIT BELOW 10,000 FEET INTO MDW, COMING FROM OVERHEAD PANEL. FOUND RT RUNWAY TURNOFF SWITCH BAD SECURED WIRES. COLLAR CIRCUIT BREAKER SWITCH WAS REPLACED 5-10-95 SYSTEM OPS CEHCK GOOD. (M)May 15, 1995 · N766AT · Boeing 727227 · Exterior LightingSDR CAL950385Rib · corrodedGSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-2. (W)May 10, 1995 · N17773 · Boeing 727227 · Leading Edge DevicesSDR CAL950384Floorboard · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK AT MLG PRESSURE FLOOR, STATION 940R. THE CRACK WAS APPROXIMATELY 12 INCHES INBOARD OF OUTSIDE EDGE OF THE FLOOR. THE CRACKED FLOORBOARDS WERE REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. May 10, 1995 · N17773 · Boeing 727227 · Fuselage Floor PanelSDR CAL950383Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT SLAT TRACK ATTACH FITTING AREA OF NR 2 SLAT INBOARD SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-02. (W)May 10, 1995 · N17773 · Boeing 727227 · Leading Edge DevicesSDR CAL950382Skin · crackedGSO - INSPECTION FOUND A .9 INCH CRACK IN LEFT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUTOUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (W)May 10, 1995 · N17773 · Boeing 727227 · Wing, Plate/SkinSDR CAL950381Intercostal · crackedGSO - INSPECTION FOUND THE NR 6 SLAT INTERIOR WITH A CRACK IN EACH OF TWO INTERCOSTALS AT INBOARD SLAT TRACK ATTACH FITTING. THE CRACKS WERE 1.2 INCHES LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (W)May 10, 1995 · N17773 · Boeing 727227 · Leading Edge DevicesSDR CAL950380Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF RT RIB LOWER FORWARD ATTACH HOLE AT WS 738. THE CRACK WAS STOP DRILLED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W)May 10, 1995 · N17773 · Boeing 727227 · Wing, Rib/BulkheadSDR CAL950379Web · crackedGSO - INSPECTION FOUND RIGHT WING CENTER INBOARD OF STATION 139 WITH CRACKS IN WEBBING AROUND FASTENER HOLES. THE CRACKS WERE .8 INCH IN LENGTH. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-6. (W)May 10, 1995 · N17773 · Boeing 727227 · Wing Miscellaneous StructureSDR CAL950378Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN AFT ENTRY DOOR SILL ANGLE AT STATION 1183 (BELOW FLOOR) ON BOTH SIDES, RBL 15 AND LBL 15. THE DOOR SILL ANGLE WAS REMOVED, A NEW DOOR SILL ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (W)May 10, 1995 · N17773 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CAL950377Shear Tie · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT STATION 400 BETWEEN STRINGERS 27-28L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (W)May 10, 1995 · N17773 · Boeing 727227 · Fuselage Miscellaneous StructureSDR MZZA95029Csd · malfunctionFLT NR 954 - ROR - WITH NR 1 ENGINE GENERATOR ALREADY ON MEL DEFERAL, AFTER AIRCRAFT DEPARTURE OUT OF ROR, NR 2 GENERATOR TRIPPED AND UNABLE TO RESET, PERFORMED APPROPRIATE ABNORMAL CHECKLIST. AIRCRAFT DIVERTED BACK TO ROR. MAINTENANCE TROUBLESHOT AND FOUNDMay 2, 1995 · N86426 · Boeing 727227 · Alternator-Generator DriveSDR 95ZZZX3067Beam · corrodedBFM - RT AND LT KEEL BEAMS, STA 950 - STA 1010, HAS CORROSION AROUND FASTENERS HOLES, ENTIRE LENGTH (AFT CARGO BAY). REMOVED AND REPLACED LT/RT KEEL BEAM CHORDS PER SB 727-53-0179.Apr 28, 1995 · N768AT · Boeing 727227 · Fuselage Main, KeelSDR CAL950337Corner · crackedFLT NR 0610 - EWR - FOUND CRACK IN UPPER FORWARD CARGO DOOR CORNER. REPAIRED PER ECRA 5230-01008. NO FURTHER INCIDENT AIRCRAFT DEPARTED. (W)Apr 27, 1995 · N10756 · Boeing 727227 · Cargo/Baggage DoorsSDR AALA950744Wire · brokenDFW - FLT 0371 - DURING DESCENT INTO DFW, RT MLG RED AND GREEN LIGHTS ILLUMINATED WITH NO HORN OR DOOR WARNING AND THEN EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPAIRED BROKEN/SHORTEDApr 27, 1995 · N728AA · Boeing 727227 · Landing Gear System WiringSDR SCNA95113Skin · dentedDURING C-CHECK, FOUND A DENT IN FUSELAGE SKIN AT STATION 1338, FOUR INCHES FROM VENTRAL STAIR CUTOUT ON RIGHT SIDE. DENT MEASURES 2.5 BY .75 BY .065. CUT OUT DAMAGED SKIN, REPAIRED WITH FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 1.Apr 26, 1995 · N275AF · Boeing 727227 · Fuselage Main, Plate/SkinSDR SCNA95112Floorbeam · corrodedDURING C-CHECK, FOUND AFT CARGO CEILING STRUCTURE TO HAVE CORROSION AT STATION 1130, RBL 45. CUT OUT CORRODED SECTION AND REPAIRED PER SRM 51-40-03.Apr 26, 1995 · N275AF · Boeing 727227 · Fuselage Main, Floor BeamSDR SCNA95111Skin · disbondingDURING C-CHECK, FOUND DISBONDING OF PREVIOUS REPAIR ON RIGHT HAND SIDE OF HORIZONTAL STABILIZER. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 55-10-03 FIGURE 2.Apr 26, 1995 · N275AF · Boeing 727227 · Horizontal Stabilizer, Plate/SkinSDR CAL950320Windshield · crackedFLT NR 693 - EWR - FOUND FLIGHT OFFICER WINDSHIELD OUTER PANE CRACKED. REMOVED AND REPLACED NR 1 WINDOW IAW MM 56-11-11 PAGE 401-412. (W)Apr 25, 1995 · N10756 · Boeing 727227 · Flight Compartment WindowsSDR SCNA95116Skin · crackedDURING C-CHECK, FOUND RIGHT WING, FIXED LEADING EDGE UPPER SURFACE AFT OF NUMBER 5 SLAT, WING STATION 436.5 IS CRACKED IN 4 PLACES ALONG RIVET ROW. CRACKS BLEND TOGETHER MEASURING A TOTAL OF 8.25 INCHES LONG, AND 6 RIVET HEADS ARE SHEARED. HIGH FREQUENCY EDDApr 22, 1995 · N275AF · Boeing 727227 · Wing, Plate/SkinSDR SCNA95114Fitting · corrodedDURING C-CHECK, FOUND PITTING CORROSION AROUND FASTENERS OF GEAR DOOR UPPER RADIUS ROD ATTACH CASTING. REMOVED AND REPLACED FITTING PER SRM 53-30-03.Apr 22, 1995 · N275AF · Boeing 727227 · Fuselage, Landing Gear Attach FittingsSDR MZZA95031Latch Cable · brokenTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON R2 ENTRY DOOR ESCAPE SLIDE LATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727-MM 25-60-15. HANGAR NON ROUTINE REPAIR ITEM CARD NApr 22, 1995 · N89427 · Boeing 727227 · Passenger/Crew DoorsSDR 95ZZZW690Fuel Pump · failedDURING CRUISE NR 1 ENGINE FLAMED OUT AND WOULD NOT RESTART. AIRCRAFT LANDED AT DESTINATION AIRPORT. AFTER TROUBLESHOOTING FOUND ENGINE DRIVED FUEL PUMP DEFECTIVE. REPLACED PUMP, OPS CHECK OK.Apr 22, 1995 · N794AJ · Boeing 727227 · Engine Fuel PumpSDR SCNA95115Skin · dentedDURING C-CHECK, REPAIRED FUSELAGE DENT AT STATION 344 STRINGER 23 R, 2.5 BY 1.5 BY .076. REPAIRED DAMAGED AREA BY INSTALLING FILLER AND DOUBLER REPAIR PER SRM 53-30-03 FIGURE 3.Apr 21, 1995 · N275AF · Boeing 727227 · Fuselage Main, Plate/SkinSDR 95ZZZX5187Engine · damagedIND - NR 1 ENGINE REQUIRES REPLACEMENT DUE TO BURNER CAN SHIFT AND DAMAGE. NR 1 ENGINE REMOVED AND REPLACED.Apr 19, 1995 · N779AT · Boeing 727227 · Engine (Turbine/Turboprop)SDR CAL950266T1 Blade · failedNAS - FLT 1901 - A LOUD BANG WAS HEARD AND THE NR 2 ENGINE EPR DROPPED TO ZERO WHILE CLIMBING THROUGH 1,100 FEET. FUEL WAS DUMPED AND ACFT RETURNED TO NAS WHERE IT LANDED WITHOUT INCIDENT. NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FApr 10, 1995 · N88770 · Boeing 727227 · Turbine Section
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