Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  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 95FDEA01148Angle · crackedRT WING WS 656.5 S13 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALL REPAIR ANGLES PER SRM 57-10-4 AND SB 57A 159 FIG 18.Aug 8, 1995 · N254FE · Boeing 727233 · Wing Miscellaneous StructureSDR 95FDEA01147Angle · crackedRT WING WS 656.5, S12 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. HFEC CONFIRMED CRACK RUNS FROM FASTENER HOLE TO AFT EDGE OF ANGLE. INSTALLED REPAIR ANGLES PER SRM 57-10-4 PG 37 FIG 11, REF SB 727-57A159.Aug 7, 1995 · N254FE · Boeing 727233 · Wing Miscellaneous StructureSDR 95FDEA01179Bracket · corrodedCORROSION ON STR TO FRAME BRACKET BS 950E, RBL 6, STR 29R, WL 138.5. REMOVED CORRODED BRACKET, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW FEDEX SRM 51-20-1, 51-30-2.Jul 28, 1995 · N264FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA01178Skin · gougedGOUGE IN SKIN AT STA 1030 AFT CARGO DOOR SKIN CUT OUT BETWEEN STR 23-24R (MARKED) OUT OF LIMITS PER FEDEX SRM 53-30-1 FIG 1. REPAIRED SKIN IAW FEDEX SRM 53-30-3.Jul 28, 1995 · N264FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA00860Hyd Fluid · lostON DEPARTURE FROM ROC, A/C LOST ALL A-SYSTEM HYD QTY.Jun 30, 1995 · N262FE · Boeing 727233 · Hydraulic System, MainSDR 95FDEAOO604Turbine · failedMAX T10 POWER, AFTER GEAR RETRACT. NR 2 ENGINE TURBINE FAILED HIGH N1, 700 DEGED EGT. REMOVED AND REPLACED NR 2 ENGINE.May 23, 1995 · N263FE · Boeing 727233 · Turbine SectionSDR 95ZZZW689Ps4 Line · brokenAFTER TAKEOFF DURING CLIMB NR 2 ENGINE FLAMED OUT, ENGINE RESTARTED BUT WOULD NOT ACCELERATE FROM IDLE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. AFTER TROUBLESHOOTING, FOUND PS4 LINE ON TOP OF ENGINE BROKEN. REPLACED LINE, OPS CHECK OK.Apr 21, 1995 · N395AJ · Boeing 727233 · Fuel Controlling SystemSDR 95FDEA00424Fire Loop · out of positionNR 1 ENG STRUT O/H LIGHT CAME ON. BLEED AIR WAS BEING USED FOR PACK. OPS AFTER AIR WAS TURNED OFF, O/H LIGHT EXTINGUISHED, ACCOMP ENG STRUT O/H LIGHT ON CKLST. ESTABLISH PACK OPS USING NR 2 BLEED. OPENED NR 1 STRUT ACCESS PANELS, FOUND AFT UPPER LOOP IN COApr 19, 1995 · N221FE · Boeing 727233 · Fire DetectionSDR 95FDEA00319Duct · leakingLOWER AFT BODY O/H LIGHT CAME ON DURING FLIGHT AT FL310. COMPLETED 'LWR AFT BODY O/H LIGHT ON' ABNORMAL/EMERG CKLIST. LIGHT REMAINED ON. DIVERTED TO FLL. ON LONG FINAL APPROACH W/ALL ENG AT IDLE FOR DESCENT, LIGHT WENT OUT. CKD KEEL BEAM LOOP M-367, AFT CAMar 22, 1995 · N281FE · Boeing 727233 · Pneumatic Distribution SystemSDR 95FDEA00213Window Post · crackedNDT PLEASE C/W E.O. 7-5330-7-3354 ( AD 93-05-17) X-RAY INSPECTION THE E-N WINDOW POST. E.O. 7-5330-7-3354 PART II X-RAY INSP E-N WINDOW POST RT HAND. PILOTS SLIDING WINDOW CRACK INDICATION APPX 1.125 INCH LONG. ENGINEERING NOTIFIED. REFERENCE PART 4 AND PMar 16, 1995 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA00227Airframe · vibrationINFO ONLY, AT 8,000, 220 KIAS, NOTICEABLE VIBRATION BEGAN UNDERNEATH THE COCKPIT, PRESS NORMAL WITH NR 2 PACKS IN OPERATION, CYCLED GEAR, VIBRATION REMAINED, SELECT MANUAL AC AT OPENED OUTFLOW VLV, AS CABIN PASSED THROUGH 6500, SELECTED AUTO, VIBRATION STOPPEDMar 11, 1995 · N264FE · Boeing 727233 · Fuselage Structure (General)SDR 95FDEA00215Flow Contl Valve · leakingLWR AFT BODY HEAT CAME ON DURING CLIMB-OUT PASSING THROUGH FL 320. NR 2 LEFT AND NR 3 BLEEDS OPEN BOTH PACKS ON, WENT THROUGH THE EMERGENCY PROCEDURE. THE LIGHT WENT OUT WHEN WE TURNED LEFT PACK OFF. CHECKED DUCTS AND CLAMPS IN AFT STAIRS WELL AREA FOUND OKMar 10, 1995 · N220FE · Boeing 727233 · Pneumatic Distribution SystemSDR 95FDEA00208Cadc · malfunctionedCAPTAIN'S AIRSPEED FAILED AND ALTITUDE FAILED ON TAKEOFF ROLL-CYCLED C.B. FOR ADC, MACH, AIRSPEED-NO HELP, ALT WARNING SYSTEM INOP ALSO. (RAIN DURING LOADING WATER IN E & E). FOUND WATER IN E & E COMPARTMENT (HEAVY RAINS DURING LOADING) REMOVED AND REPLACED AMar 7, 1995 · N271FE · Boeing 727233 · Air Data ComputerSDR 95FDEA00206Cadc · malfunctionedAFTER TAKEOFF, THE CAPTAIN'S AIRSPEED AND ALT FLAGS CAME IN VIEW. PROBABLE CASE FAILURE. THE AIR DATA CMPTR CB WAS POPPED AND WOULD NOT RESET. REMOVED AND REPLACED AIR DATA COMPUTER PER MM 34-12-01. OPS CHECK GOOD, NEEDS PITOT STATIC CK. A/C DOWNGRADED TOMar 7, 1995 · N257FE · Boeing 727233 · Air Data ComputerSDR 95FDEA00166Air Distr · odorDURING CLIMB THROUGH APPROX 20,000 AN ACRID ODOR BECAME EVIDENT IN THE COCKPIT. ODOR DISSIPATED WHEN PACKS SECURED ON LANDING. REMOVED AND REPLACED LEFT AND RIGHT CONDENSOR BAG & LEAK CHECKED GOOD. CHECKED ALL PNUEMATICS DUCTS LEAKAGE, NO LEAKS.Feb 24, 1995 · N178FE · Boeing 727233 · Air Distribution SystemSDR 95FDEA00153Radar · failedRADAR FAILURE WARNING ON CLIMB-OUT ANTENNA FAIL QUIT SWEEPING. CHECKED ALL WIRING FROM ANT TO R/T, BOTH POINT TO POINT, WIRE AND TO GND. ALL CKS GOOD, R/T MESSAGE ANNUNCIATED BRIEFLY. REMOVED AND REPLACED R/T FOUND ANTENNA WAVE GUIDE O-RING DETERIORATED REPFeb 17, 1995 · N276FE · Boeing 727233 · Weather Radar SystemSDR 95FDEA00163Stringer · crackedWHILE WORKING NR 0335, DISCOVERED STR 1 CRACKED AT BS 460. CUT FRAME TO FACILITATE STR REMOVAL, REMOVED PORTION OF DAMAGED STR, REPAIRED STR AND FRAME PER SRM 53-10-4, 57-40-5, 53-10-3.Feb 16, 1995 · N284FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 95FDEA00152Window · crackedDURING CLIMB-OUT, R-1 WINDOW BEGAN ARCING FOLLOWED BY CRACKING OF THE OUTER PANE OF THE R-1 WINDOW. REMOVED R-1 WINDOW AND TAGGED PARTS, INSTALLED R-1 WINDOW PER MM 56-11-11. CHECK FOR CORRECT R-1 TERMINAL AND R-1 WINDOW CONTROL TO BE REPLACED. TERMINAL CK Feb 16, 1995 · N220FE · Boeing 727233 · Flight Compartment WindowsSDR 95FDEA00151Radar · failedRADAR FAILURE WARNING ON CLIMB-OUT ANTENNA FAIL, (QUIT SWEEPING). REMOVED AND REPLACED RADAR INDICATOR, RADAR ANTENNA AND RADAR RT UNIT. SYS OPS CK GOOD.Feb 16, 1995 · N276FE · Boeing 727233 · Weather Radar SystemSDR 95FDEA00146Seat Track · crackedSEAT TRACK IS CRACKED AT BS 1128 LBL 625 WL 208. REMOVED SEAT TRACK, INSTALLED FABRICATED TRACK BACK DRILLED, COUNTER SUNK HOLES, ALODINED AND PRIMED TRACK, INSTALLED FASTENERS.Feb 13, 1995 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00147Floor Beam · damagedTRAMCO RESPONSIBILITY 9502-30. MISDRILLED HOLE IN FLOOR BEAM AT BS 1110 LBL 25 WL 208. REPAIRED FLOOR BEAM AT BS 1110 LBL 25 WL 208 PER FEDEX SRM 53-10-8.Feb 12, 1995 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA00137Aux Spar · crackedLEFT WING AUXILIARY SPAR LOWER CHORD CRACKED AT INBD FWD (FWD OF NR 7 SPOILER FITTING). CUTOUT CRACKED LW-AUX-SPAR LWR CHORD. FABRICATED NEW CHORD AND REPAIR ANGLES AND INSTALLED PER FEDEX EA 75810-23728.Feb 10, 1995 · N284FE · Boeing 727233 · Wing Miscellaneous StructureSDR 95FDEA00136Shear Tie · corrodedCORROSION ON SHEAR TIE IN AFT BAY ON AFT SIDE OF FRAME BS 1166, LBL 1-4, WL 152. CORRODED SHEAR TIE FOUND TO BE OUT OF LIMITS. REMOVED OLD SHEAR TIE, FABRICATED INSTALLED NEW SHEAR TIE.Feb 10, 1995 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA00133Web · crackedBS 1303 WEB IS CRACKED LWR LEFT CORNER (MARKED). REPAIRED CRACK LWR LEFT CORNER BS 1303 IAW FEDEX DRAWING SR 27-53-015.Feb 9, 1995 · N284FE · Boeing 727233 · Empennage StructureSDR 95FDEA00132Fitting · damagedWHILE WORKING FEDEX CARD 75C051-00 FOUND I/B DRUM SUPPORT BACKUP FITTING HEAVILY GOUGED. REMOVED GOUGED FITTING IN L/W I/B MIDFLAP LOCATED AND DRILLED AND INSTALLED NEW FITTING.Feb 7, 1995 · N284FE · Boeing 727233 · Trailing Edge FlapsSDR 95FDEA00131Skin · dentedDENT IN SKIN OUT OF LIMITS 2 INCHES WIDE BY 3 INCHES BY .085 DEEP AT BS 187 WL 160 RBL 12. REPAIRED DAMAGED AREA BS 187 WL 160 RBL 12 PER FEDEX SRM 53-30-3.Feb 7, 1995 · N284FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA00112Retract Mech · malfunctionedAFTER T/O GEAR HANDLE WOULD NOT GO ABOVE OFF POSITION. ACCOMPLISHED CKLIST, ELECTED TO RETURN TO MEM WITH GEAR DOWN. REMOVED AND REPLACED R-92 RELAY PRECAUTIONARY SWUNG GEARS SEVERAL TIMES, FOUND NO DEFECTS A/C OK FOR SERVICE AS PER MM 32-31-11.Feb 7, 1995 · N270FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 95FDEA00130Skin · oil canDENT IN SKIN OUT OF LIMITS 1 INCHE WIDE BY 7 INCHES LONG BY .080 DEEP AT BS 1095 WL 134.5 LBL 24. REWORKED DENT AT BS 1095 WL 134.5 LBL 24 TO WITHIN LIMITS FOUND SKIN TO OIL CAN. REMOVED DAMAGE FABRICATED PARTS AND INSTALLED ON A/C ALL WORK DONE IAW SRM 53-3Feb 6, 1995 · N284FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA00085Transmitter · failedDURING FLAP RETRACTION ON T/O O/B FLAPS SHOWED AS ASYMMETRICAL. O/B FLAPS WERE LOCKED OUT. COMPLIED WITH EMERGENCY PROCEDURES AND RETURNED TO AIRPORT. LANDED WITH NO OTHER PROBLEMS. REPLACED LEFT O/B FLAP POSITION TRANSMITTER ASYMMETRICAL. CHECKS OK PER MJan 26, 1995 · N222FE · Boeing 727233 · Trailing Flap Position Indicating SystemSDR 95FDEA00026Structure · crackedCRACK INDICATIONS NOTED IN HOLES 1-6 BELOW FLOOR AT BS 783.95 LT. REPAIRED HOLES 1-6 BELOW FLOOR AT BS 783.95 LT PER EA 7-5310-23485.Jan 15, 1995 · N278FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA00011Skin · crackedCRACKED AND DENTED SKIN AT BS 1347, LBL 30, WL 200. REPAIRED DAMAGED SKIN AT BS 1347, LBL 30, WL 200 IAW FEDEX SRM 54-30-7.Jan 11, 1995 · N278FE · Boeing 727233 · Fuselage Structure (General)SDR 95FDEA00009Engine · flamed outNR 3 ENG FLAMED OUT ON T/O PASSING 4000 FT AGL 220 KIAS. ATTEMPTED RESTART UNSUCCESSFUL, ENG SHUTDOWN CHECKLIST COMPLIED WITH. CHECKED NR 3 ENG, IGN SYS CK'D NORMAL, OPS CK'D NR 3 FUEL HEAT VALVE CK'D NORMAL. REPLACED NR 3 ENG MAIN FUEL FILTER. RAN ENG LEAJan 11, 1995 · N254FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 95FDEA00003Bypass Switch · malfunctionedNR 1 ENG LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON AT APPROX 0450Z FL240 CRUISE. OIL PRESS WAS 47 PSI QUAN AND TEMP NORMAL RANGE RETARDED NR 1 THRUST LEVER TO IDLE LIGHT REMAINED ON SHUTDOWN NR 1 ENG IAW CHECK LIST. LIGHT STAYED ON ABOUT 4 MINS AFTER ENG STAJan 4, 1995 · N274FE · Boeing 727233 · Engine Oil PressureSDR 95FDEA00001Spring · frozenAFTER TAKEOFF UPON FLAP RETRACTION, ASYMMETRIC OUTBOARD FLAPS, FLAPS IND DOESN'T MATCH DETENT, FLAP HANDLE IS DIFFICULT TO MOVE FROM 0 TO 2 DEGREES. FOUND LT OTBD FLAP TRANSMITTER RETRACT SPRING STIFF FROM COLD - FREED SPRING WITH HEAT - OPS CKS GOOD NOW.Jan 4, 1995 · N222FE · Boeing 727233 · Trailing Edge Flap Control System
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