Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  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 DL72S954450Battery · dischargedAFT BULLNOSE EMERGENCY LIGHT DIM. C/A REPLACED BATTERIES, OPS CHECK GOOD.Nov 20, 1995 · N545DA · Boeing 727232 · Emergency LightingSDR DL72S954444Skin · dentedDURING ROUTINE SHOP INSPECTION, AN AREA ON THE OUTER SKIN 11 INCHES FROM THE I/B END WAS FOUND TO BE DENTED AND OIL CANNED. THE DAMAGED AREA WAS CUT OUT AND REPAIRED PER SRM 57-50-3 FIG 1 FOR NR 8 L/E SLAT PANEL.Nov 20, 1995 · N401DA · Boeing 727232 · Leading Edge DevicesSDR DL72L954440Battery Pack · dischargedEMERGENCY LIGHTS INOP 2R AND AFT AISLE. REPLACED BATTERY PACK, OPERATION NORMAL.Nov 19, 1995 · N510DA · Boeing 727232 · Emergency LightingSDR DL72L954439Panel · delaminatedFOUND NR 2 SPOILER PANEL DELAMINATED. REPLACED PANEL, ROUTED TO SHOP FOR REPAIRS.Nov 19, 1995 · N514DA · Boeing 727232 · SpoilersSDR DL72S954687Spar Chord · crackedDURING SHOP VISIT, THE NR 2 MIDFLAP AFT CHORD WAS FOUND CRACKED AT CUTOUT FOR INBOARD AFT FLAP DRIVE ROD. THE CHORD WAS REPAIRED PER MM 57520.Nov 18, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954686Spar Chord · crackedDURING SHOP VISIT, THE NR 2 MIDFLAP AFT LOWER CHORD WAS FOUND CRACKED AT INBOARD AFT FLAP TRACK. THE CHORD WAS REPAIRED PER MM 57520.Nov 18, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954685Spar Chord · crackedDURING SHOP VISIT, NR 2 MIDFLAP AFT LOWER CHORD WAS FOUND TO BE CRACKED 55 INCHES FROM INBOARD END. THE CHORD WAS REPAIRED PER MM 57520.Nov 18, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954416Flow Contl Vlv · failedUNABLE TO MAINTAIN CABIN ALTITUDE IN CLIMB, REGAINED PRESSURIZATION BY CHECK LIST, FL 180 CABIN ALT CLIMBING OFF, LANDING PIT. REPLACED LEFT FLOW CONTROL VALVE AND RETURNED TO SERVICE.Nov 17, 1995 · N523DA · Boeing 727232 · Cabin Pressure Control SystemSDR DL72L954540Skin · corrosionCORROSION WAS FOUND IN THE FUSELAGE SKIN APPROXIMATELY 2 INCHES AFT OF STA 950F, AT S-28R. DAMAGE REMOVAL RESULTED IN A 4.125 INCH INBD/OUTBD BY 6.0 INCH FWD/AFT CUT-OUT. THE SKIN IS FABRICATED FROM CLAD 2024-T3 AND WAS MEASURED AT 0.150 INCH THICK. REPAIRENov 17, 1995 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K954419Web · crackedFOUND DURING A-2 LETTER CHECK, .25 INCH CRACK AT LIGHTENING HOLE AT TORQUE BOX VERTICAL WEB STA 1183. REPAIRED PER MM 53-11-0 PAGE 15.Nov 17, 1995 · N414DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K954418Skin · crackedFOUND DURING A-2 LTR CHK, NR 2 ENG NOSECOWL SKIN CRACKED .75 INCH AT 1ST RIB AFT OF LIP. REPAIRED PER MM 54-30-0 PAR 1.Nov 17, 1995 · N414DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72K954417Skin · crackedITEM FOUND DURING A-2 LTR CHK, 1.25 INCH CRACK AT FASTENERS AFT LWR CORNER PANEL 9516 RT SIDE NR 2 ENG DUCT HOUSING. REPAIRED PER B727 MM 54-30-0 PAR 1.Nov 17, 1995 · N414DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72K954415Angle · crackedRT W/W STA 913 SHELF ANGLE CRACKED. REPAIRED PER MM 53-11-0, FOUND DURING A-2 LTR CK TPAMM.Nov 17, 1995 · N414DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954564Angle · crackedDURING SHOP INSPECTION, THE LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ACTUATOR RIB. THE CRACK WAS REPAIRED PER THE B-727 M/M 57-54-0 FOR NR 5 L/E SLAT.Nov 16, 1995 · N518DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954563Skin · crackedDURING SHOP INSPECTION, A CRACK WAS FOUND IN THE EXTERIOR SKIN 37.5 INCHES FROM THE OUTBOARD END AT THE FENCE ATTACH POINT. THE DAMAGE WAS REPAIRED PER THE B-727 M/M 57-54-0, PG 817 FOR NR 5 L/E SLAT.Nov 16, 1995 · N518DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954562Rib · crackedDURING SHOP INSPECTION, RIB NR 17 WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER B-727 M/M 57-54-0 FOR NR 5 L/E SLAT.Nov 16, 1995 · N518DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954434Eel Pwr Supply · failedDURING POWER TRANSFER FWD CABIN EMERGENCY FLOOR TRACK LIGHTS FAILED TO LIGHT. REPLACED POWER SUPPLY, OPERATION NORMAL.Nov 16, 1995 · N408DA · Boeing 727232 · Emergency LightingSDR DL72S954410Angle · crackedFOUND DURING A-1 LETTER CHECK, 4 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.Nov 16, 1995 · N494DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954406Skin · corrosionCORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT AT THE FWD LT CORNER. THE CORROSION WAS CUT OUT. REPAIARED PER DL ERA 302764-14.Nov 15, 1995 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954494Doubler · crackedDURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH CRACKED DOUBLER AT AFT CLOSE OUT RIB LOWER AFT CORNER. REPAIRED PER MM 57-52-0.Nov 14, 1995 · N490DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954399Skin · corrosionTHE FUSELAGE SKIN WAS FOUND CORRODED AND CRACKED AT STA 870 STRINGER 10R. ONE CRACK WAS .25 INCH LENGTH AND THE OTHER 1.50 INCH LENGTH. DAMAGE WAS LOCATED IN OVERLAPPED SKIN PANELS FORWARD AND AFT OF THE BUTT SPLICE AND DAMAGE REMOVAL RESULTED IN TWO 2.75 BYNov 14, 1995 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954383Winshield · delaminatedCAPT WINDSCREEN DELAMINATED, RETARDS VISION. REPLACED WINDSCREEN.Nov 14, 1995 · N416DA · Boeing 727232 · Flight Compartment WindowsSDR DL72S954378Stringer · crackedFOUND DURING E-2 LETTER CHECK, VERT STAB STRINGER CRACKED AT FIN STA 110.4 AND STR 10 LEFT. REPAIRED PER M/M 55-30-0 PAR 3.Nov 14, 1995 · N523DA · Boeing 727232 · Vertical StabilizerSDR DL72S954377Angle · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB FORMER ATTACH ANGLE CRACKED AT FIN STA 157.2 AND STR8 LEFT. REPAIRED PER M/M 55-30-0 PAR 2.Nov 14, 1995 · N523DA · Boeing 727232 · Vertical StabilizerSDR 95FDEA01754Flap · corrosionDUE TO EXCESSIVE CORROSION (C57-562-01-2) NR 5 K-FLAP REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 5 K-FLAP IAW FEDEX MM 27-81-1. C/A ADDITION.Nov 14, 1995 · N498FE · Boeing 727232 · Leading Edge DevicesSDR 95FDEA01728Support · corrodedCORROSION (C53-111-01-1) ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. CORROSION REMOVED AROUND NUTPLATES ON SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. IN FOUR PLACES, 1.50 INCH BY 1.50 INCH BY .004 INCH Nov 14, 1995 · N490FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954368Fuel Tank · fuel leakIN FLIGHT RT WING WAS LEAKING FUEL 3 TO 6 FT INBD FROM WINGTIP. FOUND SEVERAL SCREWS MISSING FROM TANK ACCESS PANEL NR 5. REMOVED PANELS 3, 4 AND 5, CLEANED SEALS, INSTALLED NEW SCREWS, LEAK CHECK NORMAL.Nov 13, 1995 · N545DA · Boeing 727232 · Fuel StorageSDR DL72S954364Angle · crackedFOUND ON A2 LETTER CK, .5 INCH VISIBLE CRACK ON COVE SKIN ATTACH ANGLE BELOW THE OUTBOARD STOP PAD NUMBER 5 SLAT. REPAIRED PER MM 57-54-0.Nov 13, 1995 · N541DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954363Web · crackedFOUND ON A2 LETTER CK, TORQUE BOX WEB CRACKED .5 INCH AT FASTENER UPPER ROW OF RIVETS LT SIDE STA 1223. REPAIRED PER MM 53-11-0.Nov 13, 1995 · N541DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954355Duct · crackedUNABLE TO MAINTAIN PRESSURIZATION DURING CRUISE. FOUND LEFT WATER SEPARATOR FWD CLAMP SEPARATED AND WATER SEPARATOR TO MIZ VALVE DUCT CRACKED IN SEVERAL PLACES. REPLACED DUCT AND SEPARATOR, OPERATION NORMAL.Nov 12, 1995 · N533DA · Boeing 727232 · Humidity Control SystemSDR DL72L954349Eel Harness · damageCENTER CARGO EMERGENCY LIGHT INOP. REPLACED RACK AND REPAIRED DAMAGED WIRE HARNESS, OPERATION NORMAL.Nov 12, 1995 · N511DA · Boeing 727232 · Emergency LightingSDR DL72S960162Rib · crackedNR 5 RIB CRACKED ON FORWARD FLANGE. REPAIRED PER M/M 57-54-0 FIGURE 809. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Nov 11, 1995 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954343Bolt · missingON DEPARTURE, NR 2 SLAT FAILED TO RETRACT, AIL WAS DISPLACED 30 UNITS, NR 2 SLAT SHOWED GREEN ON S/O PANEL, NR 2 SLAT FINALLY STOWED WITH SPEED REDUCTION. FOUND NR 2 SLAT LWR INBRD BOLT MISSING FROM TRUNNION BRACKET, INTERMITTENTLY BINDING SLAT RETRACTION REPNov 11, 1995 · N536DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S954340Fuel Pump · failedON TAKEOFF ROLL WITH ALT POWER SET, NR 2 ENG ROLLED BACK AND SHUTDOWN ACCOMPANIED BY AUTO PACK TRIP. TAKEOFF ABORTED AND RETURNED TO GATE. INSPECTED NR 2 ENG INLET AND EXH FOR VISIBLE DAMAGE, NONE FOUND. REPLACED ENG DRIVEN FUEL PUMP, LEAK CKS GOOD. PERFORNov 11, 1995 · N478DA · Boeing 727232 · Engine Fuel PumpSDR DL72S954332Seat Track · crackedTHE INBOARD LT SEAT TRACK IS CRACKED AT FLANGE STA 1110, JUST FWD OF FLOORBEAM. REPAIRED TRACK BY SPLICING IN NEW SECTION OF SEAT TRACK PER 727 M/M 53-20-11 FIG 802.Nov 11, 1995 · N408DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S954384Rod · sheared rivetAIRFRAME VIBRATION AT 300 KNOTS. FOUND RIVET SHEARED AT RT OUTBOARD AFT FLAP OUTBOARD DRIVE ROD. REPLACED ROD, OPERATION NORMAL.Nov 10, 1995 · N420DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S954331Batteries · dischargedAFT AISLE EMERGENCY FLOOD LIGHT INOP. REPLACED BATTERIES IN AFT AISLE EMERGENCY FLOOD LIGHT, CHECKS NORMAL.Nov 10, 1995 · N524DA · Boeing 727232 · Emergency LightingSDR CAL951101Floor Beam · corrodedINSPECTION FOUND CORROSION ON FLOOR BEAM AT BS 460, RBL 45. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M)Nov 10, 1995 · N77780 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954729Le Skin · wornL/E EDGE SKIN WORN AT I/B END OF NR 1 MIDFLAP. REPAIRED PER MM 57-53-00.Nov 9, 1995 · N490DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954315Hyd Pump · leakingHYD PRESSURE LOSS IN FLT FOUND NR 2 B-HYD PUMP LEAKING. REPLACED NR 2 B-HYD PUMP, OPS NORMAL.Nov 9, 1995 · N522DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72S954308Skin · crackedINNER DOOR SKIN CRACKED AT LIGHTNING HOLE. REPAIRED CRACK PER SRM 52-00-3 FIG 3. FOUND DURING SHOP INSPECTION NR 1 CARGO DOOR.Nov 9, 1995 · N516DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S954304Battery Pack · dischargedLT FWD OVERWING EMERGENCY LIGHT INOP IN TEST. REPLACED BATTERY PACK, CHECKS GOOD.Nov 9, 1995 · N408DA · Boeing 727232 · Emergency LightingSDR DL72L954402Stiffener · crackedFOUND ON CV-2 CK, .125 INCH VISABLE CRACK EXTENDING FROM LOWER O/B RADIUS BLOCK AT VERTICAL STIFFENER STA 1183 LBL 8. REPAIRED PER M/M 53-11-0 PAR 9.Nov 9, 1995 · N509DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951084Doubler · corrodedINSPECTION FOUND SKIN DOUBLER CORRODED AT STRINGER 14R AND BS 714. THE CORRODED SECTION OF SKIN DOUBLER WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M)Nov 9, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954301Battery · dischargedCENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CKS NORMAL.Nov 8, 1995 · N484DA · Boeing 727232 · Emergency LightingSDR DL72S954282Skin · crackedDURING SHOP INSP, A CRACK WAS FOUND AT THE LOWER HINGE CUTOUT. THE CRACK WAS ROUTED OUT AND A STEEL DOUBLER WAS INSTALLED AS PER SRM 52-40-2 FIG 4, FOR LT AFT SERVICE DOOR.Nov 8, 1995 · N520DA · Boeing 727232 · Service DoorsSDR DL72L954401Frame · crackedFOUND ON CV-2 CK, LT AFT SERVICE DOOR (S/N 593) HAS A .5 INCH CRACK IN THE UPPER HINGE CUTOUT OF THE FWD FRAME. REPAIRED PER SRM 52-40-2 FIG 4.Nov 8, 1995 · N509DA · Boeing 727232 · Service DoorsSDR DL72L954400Mount · crackedFOUND ON CV-2 CHECK, NR 2 SLAT ACTUATOR MOUNT CRACKED AT UPPER O/B LOBE. REPAIRED PER M/M 57-42-0 PG 812.Nov 8, 1995 · N509DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72L954305Battery Pack · dischargedFOUND LT CENTER OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.Nov 8, 1995 · N508DA · Boeing 727232 · Emergency LightingSDR DL72K954283Actuator · failedLOST A-SYST HYD, ON CLIMBOUT. PERFORMED ABNORMAL PROCEED CK LIST, ELECT EXT FLAPS, MANUALLY EXT GEAR, FOUND NR 7 L/E SLAT ACTUATOR CASE SPLIT. REPLACED ACTUATOR, OPERATION NORMAL.Nov 8, 1995 · N414DA · Boeing 727232 · Leading Edge Slat Actuator
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