Boeing 727-224

Service difficulty reports · 2,252

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 = '727224'
  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 CALA9801312Sidewall · crackedTHE NLG WHEEL WELL RIGHT SIDEWALL AND TOP CENTER PANEL HAD CRACKS MEASURING .5 TO 1 INCH LONG. THE CRACKED AREAS WERE CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801311Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 400 AND 420, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED IAW SRM 51-30-2. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-2, AND 51-10-2.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801310Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO COMPARTMENT FRAME AT BS 680 BETWEEN STRINGER 23L AND 24L. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, FrameSDR CALA9801309Skin · corrodedINSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT BS 720 TO 720A, BL 0. A DOUBLER AND SHEAR TIE WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 53-30-4, AND 53-10-4.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9801308Stringer · crackedINSPECTION FOUND A 1.25 INCH CRACK IN STRINGER 15R AND A 2 INCH CRACK IN STRINGER 15L AT STA 720B. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 53-10-3, AND 51-10-2.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CALA9801307Housing · crackedINSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR CUTOUT UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED IAW SRM 51-10-1. A NEW HOUSING WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Jul 2, 1998 · N69735 · Boeing 727224 · Service DoorsSDR CALA9801306Floorbeam · corrodedINSPECTION FOUND FORWARD LAV FLOORBEAM AT STA 344, RBL 24 CORRODED. THE CORRODED AREA OF FLOORBEAM WAS REMOVED, A NEW FLOORBEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801305Web · crackedINSPECTION FOUND STA 700 SUPPORT WEBS CRACKED AT S22L, S23L, S23R, AND S25R. THE CRACKS WERE 1 TO 1.5 INCH LONG. THE CRACKED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801304Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORROSION AT STA 328, LBL 30 AND 45, STA 344, STA 380, RBL 32 TO 42. THE CORRODED AREAS OF FLOORBEAM WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801303Door · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO C-2 DOOR BOTTOM AFT CORNER. THE CORNER OF C-2 DOOR WAS REMOVED AND REPLACED IAW SRM 51-10-2.Jul 2, 1998 · N69735 · Boeing 727224 · Cargo/Baggage DoorsSDR CALA9801198Rib · crackedINSPECTION FOUND A .375 INCH CRACK IN UPPER OUTBOARD FLANGE OF RT WING RIB AT WS 171.5, STRINGER 16. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6.Jul 1, 1998 · N69735 · Boeing 727224 · Wing, Rib/BulkheadSDR CALA9801197Angle · crackedINSPECTION FOUND A CRACK IN AFT END OF LOWER ANGLE AT RT OUTBOARD MID-FLAP INBOARD END RIB. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INTALLED IAW SRM 51-40-2.Jul 1, 1998 · N69735 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801196Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 360, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 53-10-5.Jul 1, 1998 · N69735 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801195Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 5 LEADING EDGE FLAP INBOARD MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-40-3, AND 51-10-2.Jul 1, 1998 · N69735 · Boeing 727224 · Leading Edge DevicesSDR CALA9801194Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 18. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4.Jul 1, 1998 · N69735 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801193Skin · tornINSPECTION FOUND A 1 TEAR IN UPPER RUDDER RT SIDE TRAILING EDGE SKIN. THE TORN AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.Jul 1, 1998 · N69735 · Boeing 727224 · Rudder, Plate/SkinSDR GAIA9862AClamp · failedMKE - AFTER DEPARTING JUST PRIOR TO FLAP RETRACTION, THE NR 1 FIRE WARNING CAME ON. FIREWARNING LIGHT WENT OUT AFTER NR 1 THROTTLE WAS RETARDED. AIRCRAFT RETURNED TO MKE AND MADE UNEVENTFUL LANDING. FOUND 8TH STAGE BLEED VALVE, AFT CLAMP UNSECURED. SECUREDJun 15, 1998 · N69739 · Boeing 727224 · Pneumatic Distribution SystemSDR GAIA9861AIndicator · sticksAFTER FLAPS RETRACTED, RT INBOARD FLAP ASYMMETRY SPLIT. ONE IS AT 15 DEGREES, AND THE OTHER AT ZERO. ON APPROACH, FLAPS LOCKED OUT AT 4 DEGREES ON INBOARD AFTER FLAPS MOVED TO 15 DEGREES. INBOARD FLAPS RE-SYNCED AND FLAPS OPERATED NORMALLY. AIRCRAFT MADE AJun 12, 1998 · N69739 · Boeing 727224 · Trailing Flap Position Indicating SystemSDR CALA9801051Fitting · crackedINSPECTION FOUND A 2 INCH CRACK ON L-1 DOOR UPPER HINGE FITTING. THE CRACKED AREA WAS CUT OUT, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-5.Jun 11, 1998 · N79750 · Boeing 727224 · Passenger/Crew DoorsSDR CALA9801050Fitting · corrodedINSPECTION FOUND LT MLG TRUNNION FITTING CORRODED. THE TRUNNION FITTING WAS REPAIRED IAW ECRA 5340-01320.Jun 11, 1998 · N79750 · Boeing 727224 · Fuselage, Landing Gear Attach FittingsSDR CALA9801000Seal · failedTHE AIRCRAFT LOST A-SYSTEM HYDRAULICS AFTER TAKEOFF. THE HYDRAULIC SWITCHES WERE TURNED OFF BEFORE ALL PRESSURE WAS LOST. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OUTBOARD FLAP HYD DRIVE MOJun 10, 1998 · N69736 · Boeing 727224 · Trailing Edge Flap ActuatorSDR MZZA98176Window · crackedGUM - FLT 956 - AIR RETURN DUE TO PILOT WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED L-1 WINDOW PER MM 56-11-11. RESTORED AIRCRAFT TO ORIGINAL CONFIGURATION. RELEASED AIRCRAFT FOR SERVICE. (M)Jun 8, 1998 · N79743 · Boeing 727224 · Flight Compartment WindowsSDR GAIA9859Light · inoperativeDURING ROUTINE 'A' CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE LT FORWARD ENTRANCE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY IAW BOEING 727 MM 33-50. SYSTEM OPERATIONAL TEST CARRIED OUT SATISFACTORY. ACJun 8, 1998 · N69740 · Boeing 727224 · Emergency LightingSDR CALA9800995Skin · delaminatedINSPECTION FOUND A 4 X 2 AREA OF RT WING TRAILING EDGE INBOARD FOREFLAP LOWER SURFACE DELAMINATED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-12.Jun 5, 1998 · N79750 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98162Ps4 Line · rupturedFLT 956 - KSA - DURING STAGE 2 CLIMB SEGMENT AT POWER REDUCTION TO CLIMB POWER, EPR DROPPED .30, FUEL FLOW DROPPED TO 1000 PPH, AND EGT ROSE TO NEAR REDLINE. AIR RETURN TO KSA. MAINTENANCE FOUND PRBC PS-4 LINE LEAKS 1PC 75-30-0-1, ITEM 30 PG-0/FIG-1. REMOVEJun 3, 1998 · N79743 · Boeing 727224 · Fuel Controlling SystemSDR CALA9800948Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 27R-28R. THE CORRODED AREA WAS CUT OUT, A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-4, FIGURE 15, REPAIR 3.Jun 2, 1998 · N79750 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9800930Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD BAGGAGE BIN AT STA 500, RBL 9. THE INTERCOSTAL WAS REMOVED AND CORRODED STRINGER WAS CUT OUT IAW SRM 53-10-3. NEW STRINGER AND SPLICES WERE FABRICATED IAW SRM 53-10-5 AND 51-10-2. THE STRINGER, SPLICES AND INJun 1, 1998 · N79750 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9800929Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.Jun 1, 1998 · N79750 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9800928Wire · brokenINSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 22 AND AFT. BROKEN WIRING WAS REPAIRED AND A FUSE WAS REPLACED IAW MM 33-50-00 AND OPERATION OF THE LIGHTS CHECKED GOOD.Jun 1, 1998 · N79750 · Boeing 727224 · Light System WiringSDR CALA9800927Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AND 51-10-2.Jun 1, 1998 · N79750 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9800926Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT LOWER INBOARD AND OUTBOARD CORNERS OF LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.Jun 1, 1998 · N79750 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9800925Cowling · corrodedINSPECTION FOUND NR 2 ENGINE INLET COWLING RING CORRODED. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, 51-10-2, 51-40-5 AND 51-30-2.Jun 1, 1998 · N79750 · Boeing 727224 · Engine Cowling SystemSDR MZZA98159Switch · malfunctionedFLT 956 - GUM - AFTER AIRBORNE, CREW CALLED TO ADVISED AIR RETURN DUE TO NR 1 LEADING EDGE FLAPS PROBLEM. NR 1 LE FLAPS DISAGREEMENT WITH FLAP HANDLE POSITION, RED INTRANSIT LIGHT STAYS ON. S/O PANEL SHOWS NR 1 LE FLAPS SHOWS DISAGREEMENT WITH FLAP HANDLE. May 22, 1998 · N69742 · Boeing 727224 · Leading Edge Slat Control SystemSDR CALA9800894Skin · crackedINSPECTION FOUND A .25 INCH CRACK COMING FROM SCREW HOLE TO ACCESS CUTOUT IN RT ELEVATOR SKIN. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-20-03.May 19, 1998 · N79749 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9800893Spar · crackedINSPECTION FOUND A 1.5 INCH CRACK ON OUTBOARD SIDE AND A 1.5 INCH CRACK ON INBOARD DOUBLER OF NR 8 SLAT INBOARD ACTUATOR MOUNT AREA OF FRONT SPAR. THE INBOARD DOUBLER WAS REMOVED AND REPLACED AND THE OUTBOARD CRACK WAS STOP DRILLED IAW SRM 51-10-1.May 19, 1998 · N79749 · Boeing 727224 · Wing SparSDR CALA9800892Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 5 LEADING EDGE FLAP AFT INBOARD ACTUATOR MOUNT BRACKET BELOW ACTUATOR TRUNNION. THE MOUNT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.May 19, 1998 · N79749 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9800891Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1145, STRINGER 24L. A REPAIR WAS FABRICATED AND DOUBLERS WERE INSTALLED IAW SRM 51-30-1 AND 51-10-2.May 19, 1998 · N79749 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9800837Beam · corrodedLEFT MLG SUPPORT BEAM LOWER ATTACH BORE FOR SWING LINK FORWARD AND AFT FACES CORRODED. REMOVED CORROSION, PEENED AREA, ALODINED AND PRIMED AREA, FABRICATED AND INSTALLED BUSHINGS PER EC/RA 5740-01841.May 11, 1998 · N69741 · Boeing 727224 · Main Landing Gear Attach SectionSDR CALA9800840Trunnion · corrodedLEFT MLG FWD TRUNNION I/B SIDE OF FITTING INNER SIDE CORRODED. REPAIRED PER EO 97-871 AND EC/RA 5740-01840.May 9, 1998 · N69741 · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR CALA9800839Panel · stainedAFT CARGO COMPARTMENT FS 950 TO 1183, LBL 60 TO RBL 60 STAINED WITH BLUE WATER. FABRICATED AND INSTALLED NEW CEILING AND SIDE WALL PANELS PER EC/RA 2550-01040 AND EC/RA 2011-01000.May 9, 1998 · N69741 · Boeing 727224 · Cargo CompartmentsSDR CALA9800838Fitting · corrodedLEFT MLG FWD TRUNNION ATTACH ANGLE FITTING ON LEG CORRODED. REPAIRED PER EO 98-871 AND EC/RA 5740-01840.May 9, 1998 · N69741 · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR CALA9800836Swing Link · corrodedLEFT MLG SWING LINK ATTACH LUGS ARE CORRODED ON FACES AND BORE HOLES. COMPLIED WITH REWORK PER EO 98-0847 AND EC/RA 5740-01842.May 9, 1998 · N69741 · Boeing 727224 · Main Landing Gear Attach SectionSDR CALA9800835Skin · corrodedCOMPLY WITH FWD DRAIN HOLE EA 5330-01463. REMOVED BELLY SKIN AND VERIFIED DOUBLERS INSTALLED. CLEANED AND REINSTALLED EXISTING DOUBLERS PER EA 5330-01463.May 9, 1998 · N69741 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA98008340ownlock · wornLEFT MLG DOWNLOCK CRANK HOLES ARE OVERSIZED. FABRICATED AND INSTALLED TWO BUSH INGS PER OHM 32-01-02.May 9, 1998 · N69741 · Boeing 727224 · Landing Gear Retraction/Extension SystemSDR CALA9800833Stringer · corrodedAFT CARGO PIT STR 29R STA 950 CORRODED. REMOVED AND REPLACED STRINGER PER DWGS 65C20489 AND 65C13913.May 9, 1998 · N69741 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CALA9800832Skin · corrodedAFT CARGO PIT STR 29R STA950 CORRODED. REMOVED AND REPLACED NR 4 BELLY SKIN PER DWGS 65C20489 AND 65C13913.May 9, 1998 · N69741 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9800831Angle · crackedAFT FUSELAGE AT FS 950 RT ELEPHANT EAR FAIRING ATTACH ANGLE CRACKED (3). CUT OUT CRACKED PORTION OF FAIRING ATTACH ANGLE. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4.May 9, 1998 · N69741 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9800841Panel · crackedLT UPPER INBOARD T/E PANEL HAS SURFACE CORROSION AND CRACK. REMOVED SURFACE CORROSION. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-10-1, 51-10-6, AND 51-40-2.May 8, 1998 · N69741 · Boeing 727224 · Wing, Plate/SkinSDR CALA9800830Hyd Line · leakingDURING CLIMB, B-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. FOUND LEAKING HYDRAULIC LINE. REPLACED LINE.May 8, 1998 · N69735 · Boeing 727224 · Hydraulic System, MainSDR CALA9800819Pan · corrodedAFT LAV SERVICE PAN HAS CORROSION THROUGH OUT. REMOVED SERVICE PAN WEB FRAME. FABRICATED REPAIR ANGLE. INSTALLED NEW WEB FRAME. NEW SUPPORT HINGES PER SRM 51-30-2, 51-20-1, AND 51-10-2.May 7, 1998 · N69741 · Boeing 727224 · Fuselage Miscellaneous Structure
Back to Boeing 727-224