Boeing 727-227

Service difficulty reports · 5,082

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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 = '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 06FDEA1315Skin · corrodedFOUND CORROSION ON FUSELAGE SKIN BS 680 -740 FROM STRINGER 4 LEFT TO STRINGER 10 LEFT. REMOVED AND REPLACED SKIN PANEL BS 680-740 STR 4 LT, STR 10 LT IAW SRM 51-30-2.Apr 5, 2006 · N485FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA1314Skin · corrodedFOUND CORROSON ON FUSELAGE SKIN FROM BS 740 - 870 FROM STRINGER 4 LEFT TO STRINGER 4 RIGHT. REMOVED AND REPLACED SKIN BS 740-870 STR 4L-4R IAW SRM 51-30-2.Apr 5, 2006 · N485FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA1267Connector · damagedHAD OVER VOLTAGE SYS 1 UNDER VOLTS SYS 1, OVER EXCITED SYS 1, UNDEREXCITED SYS 1, IF EXTINGUISH LIGHTS, WARNING LIGHTS PANEL WILL NOT OPERATE CORRECTLY. ONLY APU AND APU BLEED LIGHTS WILL TEST. INSPECTED NR 1 GCU FOUND ELECTRICAL RECEPTACLE AND GCU PINS BURNMar 29, 2006 · N241FE · Boeing 727227 · Electrical Power System WiringSDR 06FDEA1269Floorbeam · damagedAFT CARGO BAY BS 1130 FLOORBEAM VERTICAL WEB CUT INTO A BL 0 VERTICAL ATTACH BRACKET. REPAIRED PER FED EX EA 7-5310-99474.Mar 29, 2006 · N492FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 06FDEA1208Skin · corrodedFOUND BS 680 ABOVE STR 27 RT FUSELAGE SKIN BUT SPLICE IS CORRODED INSIDE FWD CARGO BAY. REPAIRED SKIN AT BS 680, AT STA 27RT PER FED EX EA 7-5310-99057.Mar 23, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2006782001Battery · lowEMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATT, OPS CK GOOD IAW M/M 33-50-101 P/N MISC-062.Mar 22, 2006 · N782DH · Boeing 727227 · Emergency LightingSDR 06FDEA1186Skin · dentedDENT IN EXTERNAL FUSELAGE SKIN IN LEFT HAND UPPER TORQUE BOX AT BS 1344 JUST BELOW VERTICAL STABILIZER. *S/D* INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.Mar 21, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA1189Hinge · wornFOUND LT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE RIB, I/B LUG, O/B FACE IS WORN. I/B FACE IS WORN. REPAIRED LT HOR. STAB. THRUST HINGE RIB, I/B LUG, I/B & O/B FACES PER FED EX EA 7-5510- 96625.Mar 21, 2006 · N485FE · Boeing 727227 · Elevator StructureSDR 06FDEA1188Hinge · wornLT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE FITTING BUSHINGS ARE WORN. LT HORIZONTAL STAB. ELEVATOR THRUST HINGE FITTING BUSHINGS REPLACED PER FED EX EA 7- 5510-96625.Mar 21, 2006 · N485FE · Boeing 727227 · Elevator StructureSDR XN0A1311Strut · lowON TAXI OUT, KNOCKING SOUND FROM NOSE GEAR. SERVICED NOSE STRUT WITH NITROGEN IAW B727 MM CHAPTER 12-20-00.Mar 17, 2006 · N73751 · Boeing 727227 · Nose/Tail Landing Gear Strut/AxleSDR 06FDEA1122Attach Fitting · corrodedRIGHT WING, NR 7 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED.Mar 16, 2006 · N488FE · Boeing 727227 · Trailing Edge FlapsSDR 06FDEA1111Skin · misrepairedEXTERNAL DOUBLER REPAIR APPROX 35" BY 8" RT LWR FUSE STA 565 TO STA 600 STRINGER 26R TO 27R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INVESTIGATED EXTERNAL REPAIR BS 565 TO 600 STRMar 15, 2006 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20060005Quick Disconnect · disconnectedFLT 716 FROM TOL TO MEM. DURING TAKEOFF, CAPTAINS AIR SPEED INDICATOR FROZE AT 70 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. FOUND CAPTAINS MACH AIRSPEED INDICATOR QUICK DISCONNECT NOT FULLY ENGAGED. RESECURED QUICK DISCONNEMar 15, 2006 · N308AS · Boeing 727227 · Outside Air Temperature Indicator/SensorSDR 06FDEA1086Skin · damagedEXTERNAL DOUBLER REPAIR APPROX 8.5" BY 6.5", FUSELAGE STA 365 WL 218. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 53-30-3, SRM 51-30-2 MAJOR REPAIR.Mar 14, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA0886Repair · unknownFOUND 2 REPAIRS LOCATED ON THE RIGHT L/E WING UPPER SURFACE STA 450 AND 460. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIRS WERE DETERMINED TO BE IAW SRM 57-30-4 FMar 2, 2006 · N275FE · Boeing 727227 · Standard Practices/StructuresSDR 06FDEA0884Frame · corrodedFOUND FRAME AT STA 950E AND STRINGER 29L IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR AT STA 950E BETWEEN S28L AND S29L ALL IAW FX B727 SRM'S 53-10-4 FIG 12, 53-10-1, 53-10-2, 51-30-2, 51-10-6 AND 51-10-2, SNRM N00986.Mar 1, 2006 · N494FE · Boeing 727227 · Fuselage Main, FrameSDR XN0A1307Warning Light · illuminatedNR 2 OIL PRESSURE LIGHT ON AFTER START. REMOVED AND REPLACED OIL PRESSURE SWITCH, NR 2 POSITION, OPS CHECKS GOOD ON GROUND IAW B727 MM CHAPTER 79-33-00.Mar 1, 2006 · N793A · Boeing 727227 · Engine Oil Indicating SystemSDR XN0A1306Switch · malfunctionedNR 5 L/E FLAP DISAGREES WITH POSITION LIGHT (NO GREEN L/E FLAP LIGHT). REMOVED AND REPLACED L/E FLAP SWITCH, OPS CHECKS GOOD ON GROUND IAW A300 AMM CHAPTER 27-34-00.Feb 24, 2006 · N793A · Boeing 727227 · Leading Edge Slat ActuatorSDR XN0A1303Rudder · malfunctionedRUDDER SYSTEM -A- LADDER LIGHT ON. NO RUDDER INDICATION. CYCLED RUDDER LOWER HYDRAULIC UNIT, PERFORMED OPS CK IAW B727 AMM 27-20-121, OPS CHECKED GOOD.Feb 23, 2006 · N79754 · Boeing 727227 · Rudder Control SystemSDR XN0A1301Actuator · failedDISCREPANCY: DURING CLIMBOUT, RETRACTING FLAPS TO 5 DEGREES, TOOK LONG TIME TO GET GREEN LE LITE. RETRACTED TO FLAPS 2 DEGREES, GOT AMBER LITE AND NR 5 FLAP INTRANSIT LITE. EXTENDED FLAPS TO 5 DEGREES AND GOT ALL GREEN LITES. RETRACTED FLAPS TO 2 DEGREES AND HFeb 21, 2006 · N793A · Boeing 727227 · Leading Edge Slat ActuatorSDR 06FDEA0714Stringer · corrodedFOUND INTERIOR FUSELAGE, STR 2L HAS CORROSION FROM BS 660 TO 740.Feb 17, 2006 · N488FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 06FDEA0689Stringer Clip · damagedSTRINGER CLIP AT BS 400 STR 7 LT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRINGER CLIP AT BS 400 STR 7 LT PER SRM 51-30-2, 51-30-5, 51-30- 6.Feb 15, 2006 · N492FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 06FDEA0685Shear Tie · damagedTRANSFERED FROM CARD N01315, ITEM 7 OF JPF. UPON INSTALLATION OF FASTENERS FOUND DAMAGE ON AFT SIDE OF SHEAR TIE. REMOVED & REPLACED SHEAR TIE, BS 1148 BETWEEN STR 25R & 26R PER SRM 51-30-2.Feb 15, 2006 · N492FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 06FDEA0684Skin · gougedEXTERNAL SKIN AFT OF AFT CARGO DOOR GOUGED 21" UP FROM LWR CORNER 1.5" FROM SKIN EDGE.Feb 14, 2006 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR XN0A1299Relay · failedALL CAPTAIN INSTRUMENT FLAGS IN VIEW. REMOVED AND REPLACED ESS RADIO AC RELAY AND RADIO DC RELAY IAW B727 MM CHAPTER 24-50-00. SYSTEM OPS CHECKS GOOD IAW B727 MM CHAPTER 24-50-00. NO DEFECTS NOTED.Feb 14, 2006 · N793A · Boeing 727227 · Navigation System WiringSDR CA060213006Manifold · cracked(CAN) AFTER DEPARTURE, THE NR 2 FIRE WARNING CAME ON THROUGH CLIMB, POWER LEVER REDUCED WITH SUBSEQUENT WARNING EXTINGUISHING AND AIRCRAFT RETURNED. INSPECTION CARRIED OUT AND FOUND THE NR 2, 13TH STAGE FUEL HEAT DUCT RUPTURED AT BOTH ENDS. THE DUCT WAS THEN Feb 9, 2006 · Boeing 727227 · Engine Anti-Icing SystemSDR 06FDEA0632Floorbeam · corrodedFOUND BS 480 RBL 65 TO LBL 65 FLOORBEAM IS CORRODED AT NUT PLATE HOLES. REPAIRED FLOORBEAM AT BS 480 LBL 65 TO RBL 65 IAW SRM 53-10-8.Feb 9, 2006 · N488FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 06FDEA0631Repair · unknownEXTERNAL DOUBLE REPAIR APPROX 5" BY 7" RT LWR FUSE STA 1152 TO STA 1160 STRINGER 29R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED & REPLACED EXTERNAL DOUBLER AT STA 1060 TO STFeb 9, 2006 · N488FE · Boeing 727227 · Aircraft StructuresSDR 06FDEA0630Skin · chafedFOUND CHAFING ON EXTERNAL FUSELAGE SKIN LAP STR 19R BS 720D PLUS 13. REPAIRED CHAFING ON EXTERNAL FUSELAGE SKIN LAP STR 19R BS 720D PLUS 13 IAW SRM 53-30-3.Feb 9, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA0619Spar · chafedRT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED PER FED EX EA 7-5530-96609.Feb 9, 2006 · N488FE · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR 06FDEA0618Spar · chafedLT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED THE LT VERTICAL FIN MIDSPAR AT FIN STA 225 IAW FED-EX EA 7-5530-96609.Feb 9, 2006 · N488FE · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR 06FDEA0617Sill · wornCUTOUT I/B SILL UPPER SURFACE HAS HOLES WITH LESS THAN 2D EDGE MARGIN. COMPLIED WITH E.A. 7-5310-98582Feb 9, 2006 · N485FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 06FDEA0608Skin · tool damageFOUND STA 365 ABOVE STR 3R, DRILL START ON INTERIOR SKIN.Feb 9, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA0607Skin · tool damageFOUND STA 365 ABOVE STR 5R (2) DRILL STARTS ON INTERIOR SKIN.Feb 9, 2006 · N492FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 06FDEA0606Floorbeam · corrodedAFT CARGO BAY, CORROSION ON BS 1130 FLOORBEAM LWR CHORD AT NUT PLATE HOLES RBL 65 - LBL 65, WL 200. REPAIRED DAMAGED AFT CARGO BAY FLOORBEAM, BS 1130, LOWER CHORD, RBL 45 TO LBL 45, WL 200 PER FED-EX EA 7-5310-99474Feb 9, 2006 · N492FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 06FDEA0605Support Fitting · corrodedWHILE WORKING N01255 FOUND SUPPORT FITTING CORRODED AT FWD CARGO DOOR THRESHOLD BS 607.Feb 8, 2006 · N492FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 06FDEA0604Support Fitting · crackedFOUND FITTING AT FWD CARGO DOOR SILL BS 600, BELOW FLOOR SUPPORT IS CRACKED.Feb 8, 2006 · N492FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 06FDEA0603Web · corrodedFOUND CORROSION ON WEB BS 720A-720B LBL 67 WL 208. REMOVED CORROSION ON WEB ON 720A-B BY 8"X4"X .007". FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, ALODINED, PRIMED, AND INSTALLED IAW SRM 53-10-1, SRM 53-30-02 SRM 51-10-2 USING LOT# 664728 7075-T6. MINFeb 8, 2006 · N492FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 06FDEA0602Frame · damagedFOUND BS 660 ABOVE STR 26 LT FRAME HAS DOUBLED HOLE. REPAIRED FRAME IAW SRM 51-40-03.Feb 8, 2006 · N492FE · Boeing 727227 · Fuselage Main, FrameSDR 06FDEA0601Structure · damagedFOUND LOWER RUDDER RT, T/E HAS SEVERAL AREAS OF NICK DAMAGE. REPAIRED PER FED EX EA 7-5530-96603.Feb 8, 2006 · N492FE · Boeing 727227 · Rudder StructureSDR 06FDEA0600Floorbeam · corrodedFOUND BS 1070 FLOORBEAM IS CORRODED AT NUT PLATE HOLES LBL 65 - RBL 65, WL 201. REPAIRED OUT OF LIMITS AREA AT STA 1070 W/L 201 RBL 48 IAW SRM 53-10-8, ALL OTHER AREAS FOUND TO BE IN LIMITS IAW SRM 53-10-1.Feb 8, 2006 · N492FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 06FDEA0599Tee Fitting · corrodedFOUND TEE FITTING CORRODED STA 740 RBL 4 CORROSION ON LOWER EDGE OF BULKHEAD. REPLACED BULKHEAD LOWER CHORD PER SRM 51-30-5 AND 51-30-2.Feb 8, 2006 · N492FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 06FDEA0597Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1158, STR 30 WAS DETERMINED TO BE ACCOMPLISHED IAW EO 7-2500-7-2348, ITEM 12, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERFeb 8, 2006 · N487FE · Boeing 727227 · Aircraft StructuresSDR XN0A1295Transceiver · inoperativeNR 1 VHF WOULD NOT TRANSMIT OR RECEIVE. REMOVED AND REPLACED VHF TRANSCEIVER IAW B727 M/M 23-21-31.Feb 7, 2006 · N79754 · Boeing 727227 · VHF Communications SystemSDR XN0A1195Transceiver · failedNR 1 VHF WOULD NOT TRANSMIT OR RECEIVE. REMOVED AND REPLACED VHF TRANSCEIVER IAW B727 M/M 23-21-31.Feb 7, 2006 · N79754 · Boeing 727227 · VHF Communications SystemSDR 06FDEA0549Repair · unknownEXISTING DOUBLER REPAIR APPROX 11" BY 19", RT LWR FUSELAGE STA 680 TO 692 STRINGER 27R TO 28R REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53Feb 6, 2006 · N492FE · Boeing 727227 · Aircraft StructuresSDR XN0A1294Flap System · malfunctionedNR 1 LED LOCKED UP & WOULD NOT EXTEND FOR 10 MINUTES ON FLAP EXTENSION. NR 4 LED INTRANSIT FOR 15 MINUTES ON FLAP EXTENSION. VERIFIED NR 1 LED IS AN INDICATION LIGHT, TRANSFERED TO DMI 6127 IAW ENA MEL 27-6, CAT -C-, SPECIAL PROCEDURES 27-6 COMPLIED WITH. PFeb 6, 2006 · N79754 · Boeing 727227 · Trailing Edge Flap Control SystemSDR 06FDEA0536Warning Horn · false activationDURING T/O ROLL AT APPROX 65 KIAS (ON CAPT'S A/S IND) THE MACH A/S WARN CLACKER SOUNDED. REJECTED T/O AND COMPLIED WITH RTO CHECKLIST IN QRH. RETURNED TO GATE. PERFORMED MACH AIRSPEED WARN CHECKS IAW 727-200 M/M 34-14-002-5, BOTH NR 1 AND NR 2 OVERSPEED WFeb 2, 2006 · N482FE · Boeing 727227 · Central WarningSDR XN0A1298Shear Tie · corrodedDURING REMOVAL OF STR 30, (FROM FS 1150 TO FS 1183), FOUND SHEAR TIE FITTING CORRODED (JACK FTG). REMOVED CORRODED JACK FITTING AND BULKHEAD STIFFENER AND INSTALLED SERVICEABLE LIKE UNITS PER B727 SRM 51-20-4 AND SRM 51-30-2.Jan 30, 2006 · N79754 · Boeing 727227 · Fuselage Internal Mounting StructureSDR XN0A1297Stringer · corrodedDURING CPCP INSPECTION FOUND STR 30 CORRODED FROM FS 1150 TO FS 1183. REMOVED CORRODED SECTION OF STRINGER FROM FS 1150 TO FS 1183 AND REPAIRED SAME PER B727 SRM 53-10-3.Jan 30, 2006 · N79754 · Boeing 727227 · Fuselage Main, Longeron/Stringer
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