Boeing 727-200

Service difficulty reports · 2,835

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '727200'
  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 02FDEA00356Frame · dentedFRAME 600 DENTED AT OPEN HOLES 5R. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.May 21, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR C7WA200200002Windshield · brokenCRUISING AT 33,000 FEET FROM DAY TO BOS CAPTAINS L-1 WINDSHIELD OUTER AND INNER PANES SHATTERED. AIRSPEED WAS MACH .76. DONNEDE OXYGEN MASKES AND DESCENDNED TO 11,000 FEET AS INSTRUCTED BY ATC. FURTHER DESCENDED TO 10,000 FEET. REMOVED OXYGEN MASKS AND DIVEMay 21, 2002 · N902PG · Boeing 727200 · Flight Compartment WindowsSDR 02FDEA00360Frame · corrodedCORROSION ON FRAME BS 720F FWD FACE BETWEEN STR 4 & 5 RT.May 20, 2002 · N209FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00361Frame · dentedDENT IN FRAME AT BS 700, STR 25 RT. REMOVED AND REPLACED FRAME PER SRM 53-10-1.May 20, 2002 · N209FE · Boeing 727200 · Fuselage Main, FrameSDR 2003F00297Gearbox · leakingNR 1 ENGINE OIL QUANTITY DECREASED FORM 3 GALLONS TO ONE-FOURTH GALLON, IN ONE HOUR. PERFORMED AND IN FLIGHT PRECAUTIONARY ENGINE SHUTDOWN AS PER AFM PROCEDURES. PERFORMED BREATHER PRESSURE, INSPECTED FOR EXTERNAL LEAKAGE. BOTH CHECKS WERE SATISFACTORY. AIMay 19, 2002 · N906PG · Boeing 727200 · Accessory GearboxesSDR 02FDEA00359Floorbeam · corrodedCORROSION ON LOWER SURFACE OF FLOORBEAM FWD FLANGE AT BS 360, LBL 3.1, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.May 19, 2002 · N462FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00357Stringer · corrodedCORROSION ON STR 27L, BS 657 LOWER LOBE (C53-111-01-2). REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 51-20-2, 53-10-2, 53-10-3.May 18, 2002 · N462FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 02FDEA00351Position Switch · failedON FINAL AT DSM, EXTENDED LANDING GEAR GOT 3 GREEN LIGHTS, RED DOORS LIGHT ON FORWARD PANEL AND AMBER RT MAIN GEAR DOOR LIGHT ON S/O PANEL. CYCLED GEAR, ALL INDICATIONS NORMAL. ACN RELEASED FOR SERVICE PER MEL/CDL. RT MAIN GEAR DOOR POSITION SWITCH SHOWS NOMay 17, 2002 · N288FE · Boeing 727200 · Landing Gear Position and WarningSDR 02FDEA00336Gasper Fan · overheatedIN RANGE TO LAS DETECTED A SLIGHT SMELL LIKE OVERHEATED EQUIPMENT. SMELL SEEMED TO DISSIPATE AFTER LANDING. RELEASED FOR SERVICE PER MEL/CDL. GASPER FAN INOP. REMOVED AND REPLACED GASPER FAN PER MM 21-23-011-4, OPS CHECK NORMAL.May 16, 2002 · N210FE · Boeing 727200 · Air Distribution FanSDR 02FDEA00335Indicator · false activationRED DOOR INDICATOR ON AFTER GEAR RETRACTION DEPARTING DAY. RECYCLED GEAR PER RED TAB PROCEDURE AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES PER MM 32-62-01. NO DEFECTS NOTED. OK FOR SERVICE.May 16, 2002 · N288FE · Boeing 727200 · Landing Gear Position and WarningSDR 02FDEA00333Fire Warning · malfunctionedON DESCENT, RECEIVED ENGINE FIRE WARNING BELL AND ENGINE FIRE WARNING LIGHT WITH NO ASSOCIATED FIRE PULL HANDLE LIGHTS. ALL ENGINE PERFORMANCE PARAMETERS WERE NORMAL. FOLLOWED CHECKLIST. FIRE WARNING SYSTEM TEST SATISFACTORY. CONTINUED DESCENT TO LANDINMay 16, 2002 · N467FE · Boeing 727200 · Fire DetectionSDR 02FDEA00334Fire Warning · malfunctionedON DESCENT, RECEIVED ENGINE FIRE WARNING BELL AND ENGINE FIRE WARNING LIGHT WITH NO ASSOCIATED FIRE PULL HANDLE LIGHTS. ALL ENGINE PERFORMANCE PARAMETERS WERE NORMAL. FOLLOWED CHECKLIST. FIRE WARNING SYSTEM TEST SATISFACTORY. CONTINUED DESCENT TO LANDING AMay 16, 2002 · N467FE · Boeing 727200 · Fire DetectionSDR 02FDEA00344Shear Tie · damagedHOLES IN SHEAR TIE AND SKIN AT BS 600 BETWEEN STR 27 & 28 L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & EA 7-5330-54321.May 14, 2002 · N462FE · Boeing 727200 · Fuselage Main, StructureSDR 02FDEA00346Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 312, LBL 27, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-1.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00342Frame · dentedDENT IN FRAME AT BS 1110 BETWEEN STR 25 - 26 L. REMOVED AND REPLACED FRAME PER SRM 51-40-3.May 13, 2002 · N209FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00338Skin · damagedEXTERIOR SKIN DAMAGED JUST AFT OF FWD E BAY DOOR AT BS 226, RBL 5. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00345Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER SURFACE BS 348, LBL 25-50, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00341Skin · dentedSKIN DENTED AT BS 1130 2 INCHES ABOVE STR 25 R.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00340Skin · dentedSKIN DENTED AT BS 1130 3 INCHES BELOW STR 23 R. REMOVED AND REPLACED SKIN PER SRM 53-30-1 & 53-30-3 FIG 3.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00339Skin · damagedHOLES IN SHEAR TIE AND SKIN AT BS 580 BETWEEN STR 27 & 28L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & EA 7-5330-54321.May 13, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00329Skin · gougedGOUGE IN EXTERNAL SKIN AT STR 17L, BS 400. REMOVED AND REPLACED SKIN PER SRM 53-30-3 & EA 7-5330-54245.May 12, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA0330Skin · corrodedCORROSION ON SKIN BS 720D+16, STR 26L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 5 & EA 7-5330-64102.May 12, 2002 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00326Clamp · looseLOWER AFT BODY OVERHEAT LIGHT FLICKERED SEVERAL TIMES THEN REMAINED ON STEADY FOR APPROX 20 SEC IN FLT WHILE EXECUTING PROC IN ORH LIGHT WENT OUT. PERFORMED RESISTANCE CHECKS OF OVERHEAT ELEMENTS. ALL RESISTANCE CHECKS ARE GOOD PER MM 26-14-001-2. GAIN ACCEMay 11, 2002 · N208FE · Boeing 727200 · Pneumatic Distribution SystemSDR 02FDEA00325Door · damagedON ARRIVAL INTO LAS FOUND HYD SERVICE DOOR TORN ABOUT 3/4 OFF. NO RESTRICTION HYD SERVICE DOOR MISSING (ON 2 CYCLE EA). FABRICATED AND INSTALLED TEMP REPAIR PER EA 7-5320. REMOVED AND REPLACED HYD ACCESS DOOR PER 12-30-000, OK FOR SERVICE.May 11, 2002 · N267FE · Boeing 727200 · Hydraulic Compartment DoorsSDR 02FDEA00323Warning System · false activationAFT AIRSTAIR LIGHT ON S/O PANEL ON AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AIRSTAIR UP UPON ARRIVAL. INSPECTED SYSTEM, HANDLE IN CORRECT LOCK POSITION. CYCLED AIRSTAIR ALL INDICATIONS NORMAL AT THIS TIME. MACH SHOWS NO HISTORY FOR LMay 11, 2002 · N212FE · Boeing 727200 · Door Warning SystemSDR 02FDEA00328Skin · chafedN 321 SKIN CHAFED AT SKIN LAP STR 19 RT, BS 720D+13. R&R SKIN PER SRM 53-30-3 FIG 14.May 10, 2002 · N209FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00322Frame · damagedHOLES IN FRAME AT BS 870, STR 9 RT. REMOVED AND REPLACED FRAME PER EA 7-5310-64105.May 9, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00321Keelbeam · corrodedCORROSION ON KEEL BEAM AT BS 950E+9, WL 139, LBL 6.May 9, 2002 · N462FE · Boeing 727200 · Fuselage Main, KeelSDR 02FDEA00318Frame · dentedFRAME DENTED AT BS 970 BETWEEN STR 25 & 26 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64087.May 7, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00319Frame · dentedN 653 FRAME DENTED AT BS 990 AT STR 26 LT. R&R FRAME PER SRM 51-40-3 & 51-10-2.May 7, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00317Frame · dentedN 329 FRAME DENTED AT BS 950F BETWEEN STR 26 & 25 LT. R&R FRAME IAW SRM 51-40-03 FIG 1.May 7, 2002 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00316Sensing Element · faultyIN CRUISE NR 1 ENGINE OVERHEAT FLICKERED ON/OFF. REDUCED PWR AND COMPLETED ENG STRUT OVERHEAT CHECKLIST. LIGHT REMAINED OUT. THEN FLICKERED AND CAME ON. SHUTDOWN NR 1 ON TAXI IN. REMOVED AND REPLACED OVERHEAT SENSING ELEMENT, BOOT & CLAMP ON DUCT.May 7, 2002 · N243FE · Boeing 727200 · Overheat DetectionSDR 02FDEA00311Warning System · false activationAFTER GEAR RETRACT, GEAR HANDLE IN UP POSITION, R/GEAR RED WARN LIGHT REMAIN ON. PERFORMED TEST OF R/GEAR UPLOCK IND PER MM 32-61-081-4. OPS CHECK NORMAL. OK FOR SERVICE.May 6, 2002 · N491FE · Boeing 727200 · Landing Gear Position and WarningSDR 02FDEA00310Torque Tube · disconnectedON DEPARTURE OUTBOARD FLAPS WENT ASYMMETRIC WITH ONE NEEDLE IND. RECONNECTED TORQUE TUBE PER MM 27-51-00-5. OPS CHECK GOOD.May 6, 2002 · N489FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 02FDEA00308Position Switch · failedRIGHT INBOARD LEADING EDGE FLAP NR 5 FAILED TO RETRACT WHEN FLAPS 2 SELECTED. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP POSITION SWITCH PER MM 27-80-001-4. OPS CHECK NORMAL.May 6, 2002 · N258FE · Boeing 727200 · Leading Edge Slat Position Indicating SystemSDR 02FDEA00305Sense Line · out of positionDURING DESCENT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON FOR APPROX 2 SECONDS THEN WENT OUT. THIS OCCURRED ONLY 1 TIME AND THE SYSTEM TESTED NORMALLY. ALL OTHER AIRCRAFT SYSTEMS/INDICATIONS NORMAL. INSPECTED AND FOUND SENSE LINE AT STATION 1243 LT SIDE OF AMay 2, 2002 · N208FE · Boeing 727200 · Overheat DetectionSDR V3E2002F00000Bolt · shearedBOLT ASSEMBLY - SIDE SPINDLE WAS FOUND WITH HEAD OF BOLT ASSEMBLY SHEARED OFF AND THE WAS BACKING OUT AFTER TOWING THE AIRCRAFT FROM STORAGE TO THE MAINTENANCE HANGAR. HEAD OF BOLT WAS FOUND ON FLOOR, THERE WAS NO MAINTENANCE BEING PERFORMED ON THE LANDING GEApr 25, 2002 · N876AA · Boeing 727200 · Main Landing GearSDR CA020402005Controller · failed(CAN) FLT 146 AFTER DEPARTURE, CABIN ALTITUDE WARNING HORN SOUNDED. CREW EXECUTED CABIN ALTITUDE WARNING / RADID DEPRESSURIZATION CHECKLIST & CABIN PRESSURE STABILIZED AT 12,000 FT. AIRCRAFT DESCENDED TO 26,000 FT, FLT ATTENDENTS DONNED PORTABLE OXYGEN MASKS Apr 2, 2002 · Boeing 727200 · Cabin Pressure ControllerSDR DHL2002749003Aileron · delaminatedDURING A CHECK FOUND R/H O/B AILERON UPPER SURFACE WITH DELAMINATED UPPER O/B SKIN APPROX 4 1/2 X 8 IN. AREA OF TAB.Mar 20, 2002 · N749DH · Boeing 727200 · AileronsSDR P9R2002F00002Light · loose(TRACK, BASE, EPL) EMERGENCY EXIT ILLUMINATION STRIP ON RT SIDE OF AIRCRAFT AT ROW 6 CAME LOOSE. REATTACHED EMERGENCY ILLUMINATION STRIP ON RIGHT SIDE AT ROW 6.Mar 19, 2002 · N906PG · Boeing 727200 · Emergency LightingSDR 2003F00060Strip · looseFLT 322 - MSP - AFT CABIN ESCAPE PATH ILLUMINATION STRIP IS NOT ATTACHED TO FLOOR BY AFT GALLEY LEFT SIDE. REINSTALLED SAFETY GLOW ESCAPE PATH STRIP AT LEFT AFT LAVATORY PER CHAPTER 25. (M)Mar 4, 2002 · N919PG · Boeing 727200 · Emergency EquipmentSDR 2003F00059Strip · looseFLT 322 - MSP - ESCAPE PATH ILLUMINATION STRIP HAS CAME LOOSE FROM FORWARD GALLEY FLOOR. REINSTALLED SAFETY GLOW ESCAPE PATH STRIP IN FORWARD GALLEY PER CHAPTER 25. (M)Mar 4, 2002 · N919PG · Boeing 727200 · Emergency EquipmentSDR 02FDEA00158Pump · failedNR 3 ENGINE QUIT ON TAKEOFF. REMOVED AND REPLACED ENGINE FUEL PUMP AND CONTROL UNIT PER 73-12-001-2, 73-21-000-4. CHECK OK.Feb 27, 2002 · N203FE · Boeing 727200 · Engine Fuel PumpSDR C1HA200296010Compressor · stalledAFTER STARTING TO APPLY T/O POWER WITH A CROSSWIND NR 2 ENGINE COMPRESSOR STALLED. INSPECTED NR 2 ENG INLET AND EXHAUST FOUND NO DAMAGE AS PER MM 71-00, OK FOR CONTINUED SERVICE.Feb 19, 2002 · N696CA · Boeing 727200 · Turbine Engine Compressor SectionSDR DHL2002749001Control Panel · faultyTAKEOFF ROLL GEN NR 2 BUS TIE LIGHT ILLUMINATED. REJECTED TAKEOFF. ACCOMPLISHED ABNORMAL CHECKLIST, SYSTEM RETURNED TO NORMAL. MOVE THRUST LEVERS AND SAME CONDITION RETURNED. S/O AUX PANEL INDICATED GEN OVER - EXCITED SYSTEM NR 2. REMOVED AND REPLACED NR Feb 5, 2002 · N749DH · Boeing 727200 · AC Power Distribution SystemSDR EISA20010137Trim Tab · damagedL/H ELEVATOR TRIM TAB HAS ELONGATED HOLES AT FWD HINGE POINT.FOUND DURING 'D' CHK.CORRECTIVE ACTION:FAB AND INSTALLED REPAIR DOUBLER IAW B727-55-20-2. WEIGH AND BALANCE IAW B727 SRM 51-80-9 FIG. 2.Dec 6, 2001 · N702NE · Boeing 727200 · Elevator, Tab StructureSDR EISA20010136Skin · corrodedR/H PLENUM CENTER WING SKIN HAS CORROSION AT ST 840, RBL 30.FOUND DURING 'D' CHECK.CORRECTIVE ACTION:REMOVED PREVIOUS REPAIR, FABRICATED DOUBLER AND TRIPLER AND INSTALLED IAW FLIGHT VEHICLES CONSULTING DRAWING 57-01600-3Dec 6, 2001 · N702NE · Boeing 727200 · Wing, Plate/SkinSDR EISA20010135Skin · corrodedL/H PLENUM CENTER WING SKIN HAS CORROSION AT STA. 850 LBL 30.FOUND DURING 'D' CHECK.CORRECTIVE ACTION: REMOVED CORROSION. FABRICATED REPAIR DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW FLIGHT VEHICLES CONSULTING DRAWING 57-01600-2Dec 6, 2001 · N702NE · Boeing 727200 · Wing, Plate/SkinSDR EISA20010148Support · crackedRT WING #7 FLAP TRACK FWD SUPPORT FITTING CRACKED.FOUND WHILE ACC. ROUTINE CARD 458, PLACED ON N/R CARD 3489.CORRECTIVE ACTION:REMOVED AND REPLACED FITTING IAW B727 MM 20-80-1Dec 5, 2001 · N702NE · Boeing 727200 · Trailing Edge FlapsSDR DHL2001749002Windshield Wiper · out of adjCAPT'S W/S WIPER INOP. SERVICEABLE ADJUSTED WIPER TENSION IAW B727 M/M 30-42-42, OPERATIONAL CHECK.Nov 30, 2001 · N749DH · Boeing 727200 · Windshield/Door Rain/Ice Removal
Back to Boeing 727-200