Boeing 727-233

Service difficulty reports · 3,034

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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 = '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 95FDEA01333Motor · failedA/P AND CRUISE STABILIZER TRIM ACTUATOR CIRCUIT BREAKER TRIPPED IN DESCENT. DISCONNECTED A/P. RESET CIRCUIT BREAKER, IT TRIPPED SECOND TIME. REMOVED AND REPLACED CRUISE TRIM MOTOR. OPS CK GOOD.Sep 13, 1995 · N258FE · Boeing 727233 · Stabilizer Control SystemSDR 95FDEA01326Shear Tie · corrosionCORRODED SHEAR TIE AT BS 1010 RBL 9 WL 138. REMOVED DAMAGE IN A .5 INCH BY 6 INCH AREA AND FABRICATED REPAIR PART ALODINED, PRIMED AND INSTALLED REPAIR IAW FEDEX SRM 53-10-4.Sep 12, 1995 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA01325Skin · dentedDENT ON EXTERNAL SKIN SURFACE, BS 1195 TO 1205 STR 24R. REPAIRED DENT, REF SRM 53-30-2.Sep 12, 1995 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01273Stringer · crackedCABIN, STR END CRACKED 15R BETWEEN 720B AND 720C FWD OF LIGHT ASSY NR 1401. STOP DRILLED CRACK PER SRM 53-10-2, INSTALLED REPAIR PART PER SRM 53-10-3.Sep 8, 1995 · N223FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 95FDEA01260Seat Track · corrodedCORROSION (72C207-00), ON SEAT TRACK BS 870 TO 893 RBL 45 WL 208.5. THE CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER FEDEX SRM 53-10-1.Sep 5, 1995 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01259Seat Track · corrodedCORROSION (72C207-00), ON LONG BEAM FLANGE AND FASTENER HOLES AT BS 758 TO 852 RBL 25 WL 208.1. CORROSION REMOVAL WAS OUT OF LIMITS ON SEAT TRACK. REPLACED SEAT TRACK, REPAIRED SEAT TRACK FLANGE, ALL WORK DONE IAW EA NR 7-5310-25652.Sep 5, 1995 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01258Floorbeam · corrodedWHILE ACCESSING FOR REPAIR ON CARD NR O102, DISCOVERED THE UPPER CHORD OF 344 BEAM TO BE CORRODED BEYOND LIMITS AT RBL 30 LBL 45 WL 208. THE CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED ENTIRE UPPER CHORD, FABRICATED NEW CHORD AND INSTALLED ALL WORK PER FEDESep 5, 1995 · N263FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01257Floorbeam · corrodedCORROSION (71C709-02), ON LOWER FLANGE OF FLOORBEAM AT BS 1070 RBL 7 WL 200. CORROSION WAS FOUND TO BE OUT OF LIMITS ON LOWER FLANGE OF FLOORBEAM AT BS 1070, RBL 1 TO 16 AND RBL 50, PER FEDEX SRM 53-10-1. REPAIRED LOWER FLANGE OF FLOORBEAM AT BS 1070 LBL 27 Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01256Skin · gougedLWR 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM BS 950 TO 1010, STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND INSTALLED NEW AT BS 950 TO 1010 STR 25 LT AND RT, IAW FEDEX SRM 51-30-Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01255Skin · gougedLOWER 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM 1010 TO 1183 STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 26 LT AND RT, IAW FEDEX SRM 5Sep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01254Skin · gougedFUSELAGE SKIN PANEL IS SEVERELY NICKED AND GOUGED FROM BS 1010 TO 1090 STR 20 TO 26R, REQUIRING REPLACEMENT OF PANEL. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 20 TO 26R, IAW FEDEX SRM 51-30-2, BASep 5, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01246Floorbeam · corrodedCORROSION ON TOP AND BOTTOM OF FLOORBEAM AROUND MOUNT HOLES AT STA 1070 BETWEEN RBL 22.5 AND RBL 46. REPAIRED PER SRM 53-10-8.Sep 1, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01245Floorbeam · corrodedCORROSION ON BOTTOM OF CABIN FLOORBEAM AROUND FLOOR BOARD ATTACH HOLES AT STA 1110 BETWEEN RBL 22.5 AND RBL 46. REPAIRED PER SRM 53-10-8.Sep 1, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01244Floorbeam · corrodedSTA 1110 FLOORBEAM IS CORRODED ON TOP AND BOTTOM OF UPPER CAP AREA, WHERE FLOOR BOARDS MOUNT BETWEEN NR 5 AND NR 6 SEAT TRACKS. REPAIRED PER SRM 53-10-8.Sep 1, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01243Floorbeam · corrodedCORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 1110 FROM 3 TO 20 RBL. REPAIRED PER SRM 51-10-6.Sep 1, 1995 · N233FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01242Floorbeam · corrodedTOP FLANGE OF FLOORBEAM AT STA 600 CORRODED BEYOND SRM LIMIT RBL 46.5 APPROX. CUT OUT DAMAGE, REPAIRED PER SRM 53-10-8 PG 44 TO 48. DAMAGE CUT OUT WAS 1 BY 1.5.Sep 1, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01241Floorbeam · corrodedFLOORBEAM UPPER CAP WHERE FLOORBEAM MOUNTS IS CORRODED AROUND SCREW HOLES BETWEEN 5 AND 6 SEAT TRACKS STA 1070. REPAIRED PER SRM 53-10-8.Sep 1, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01239Seat Track · corrodedCORROSION (72C207-00), ON SEAT TRACK BS 752 TO 852 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK PER FEDEX SRM 51-30-2, 51-10-1, 51-30-4, 51-10-2.Sep 1, 1995 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01238Seat Track · corrodedCORROSION (72C207-00), ON SEAT TRACK FLANGE BS 741.5 TO 757.5 LBL 25 WL 208. REMOVED CORRODED SEAT TRACK EXPANSION LINK, POSITIONED AND INSTALLED NEW SEAT TRACK EXPANSION LINK, LOCATED HOLES AND SECURED WITH FASTENERS IAW FEDEX SRM 53-10-1, 51-10-1, 51-10-2 ASep 1, 1995 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01237Seat Track · corrodedCORROSION (72C207-00), ON SEAT TRACK BS 890 LBL 45 WL 208.5 IN WELL OF SEAT TRACK. REPLACED EXPANSION LINK SEAT TRACK BS 852 TO 870. REMOVED CORROSION AT STA 870 TO 890, .004 TO .005 MATERIAL IN AREA 1 BY 20 ORIGINAL THICKNESS, .100 WITHIN LIMITS IAW FEDEX SSep 1, 1995 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01232failedABORTED T/O DUE TO SEVERE VIBRATION FROM NR 2 ENG, LOUD BANG FOLLOWED BY ENG FAIL LIGHT AND NR 2 LOW OIL PRESSURE BYPASS LIGHT. NR 2 FIRE HANDLE PULLED AND BOTH FIRE BOTTLES USED. ALSO, LOSS OF OIL PRESSURE, PER CONVERSATION WITH CREW AT SITE. DISCONNECTED Sep 1, 1995 · N285FE · Boeing 727233 · Turbine SectionSDR 95FDEA01231Floorbeam · crackedBS 380 RBL 26 TO 32, MAIN CARGO FLOORBEAM UPPER FLANGE IS CRACKED AND CORRODED. REMOVED CRACKED AND CORRODED SECTION OF UPPER FLANGE OF BS 380 RBL 16.75 AND 35.25 RBL, FLOORBEAM. FABRICATED DOUBLER PER SRM 53-10-8 PG 2A. INSTALLED FLOORBEAM REPAIR PER SRM 5Aug 31, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01240Floorbeam · corrodedCORROSION STA 620 LBL 12 CABIN FLOORBEAM. INSTALLED DOUBLER ASSY PER SRM 53-10-6 FIG 8.Aug 30, 1995 · N223FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01225Skin · punctureLARGE PUNCTURE AT RIVET LOCATION ON NR 3 CARGO DOOR INTERNAL SKIN, BS 1138 WL 169 RBL 86. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 52-00-3.Aug 30, 1995 · N263FE · Boeing 727233 · Cargo/Baggage DoorsSDR 95FDEA01224Cowl · dentedNR 1 ENG NOSE COWL DENTED AT 6 O'CLOCK POSITION. DENT OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 54-10-3.Aug 30, 1995 · N263FE · Boeing 727233 · Engine Cowling SystemSDR 95FDEA01222Skin · damagedWHILE WORKING NR 0412, FOUND LIGHTNING STRIKES AND DEEP GOUGES TO BE OUT OF LIMITS AT BS 490 STR 27R WL 149. REPAIRED DAMAGE AT BS 490 STR 27R WL 149, PER FEDEX SRM 53-30-3.Aug 30, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01210Floorbeam · corrodedCORROSION (72C237-02), ON TOP CHORD OF BS 1030 FLOORBEAM RBL 9 TO 22 LBL 51.5 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1030 RBL 9 TO 22 LBL 51.5 AREA WAS OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED TOP CHORD OF FLOORBEAM AT Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01209Floorbeam · corrodedCORROSION ON TOP CHORD OF BS 1110 FLOORBEAM RBL 8 TO 55 LBL 47 TO 55 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1110 RBL 8 LBL 55 WL 208. TOP CHORD WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED TOP Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01208Skin · lightning strikeBS 620 STR 24R AND 25R THERE IS A LIGHTNING STRIKE ON EXTERIOR SKIN. BLENDED OUT LIGHTNING STRIKE, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-30-1. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER AND FILLER, ALL WORK WAS DONE IAW FEDEX SRM 53-30-3, 53-30-1.Aug 28, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01207Gate Beam · crackedFWD ENTRY DOOR LOWER GATE BEAM IS CRACKED AT FWD CORNER STOP FITTING, APPROX 1 INCH LENGTH. REPAIRED CRACK IN FWD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-3210-25602.Aug 28, 1995 · N271FE · Boeing 727233 · Passenger/Crew DoorsSDR 95FDEA01211Floorbeam · corrodedCORROSION ON TOP CHORD OF FLOORBEAM BS 1070 AT LBL 13 LBL 47.5 TO 54 RBL 15 TO 52 WL 208. CUT OUT DAMAGED UPPER CHORD OF FLOORBEAM FROM LBL 65 RBL 65 AND REPAIRED PER SRM 53-10-08 FIG 3.Aug 26, 1995 · N271FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 95FDEA01196Doubler · gougedMAIN CARGO DOOR SIDE FRAME IS GOUGED ON AFT LOWER FRAME. REPAIRED MAIN CARGO AFT LOWER SIDE FRAME IAW FEDEX SR 27-52-009.Aug 24, 1995 · N271FE · Boeing 727233 · Cargo/Baggage DoorsSDR 95FDEA01185Stringer · damagedDRILL STARTS IN STR 4-5R, BS 804. REPAIRED IAW FEDEX SRM 53-10-3, STR 4-5R, BS 804.Aug 23, 1995 · N271FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 95FDEA01212Seat Track · corrodedCORROSION ENTIRE LENGTH OF I/B FLANGE OF SEAT TRACK BS 1050 TO 1090 WL 208 LBL 45. FOUND CORROSION TO GO ALL THE WAY THROUGH THE SEAT TRACK. REMOVED CORRODED TRACK, INSTALLED NEW TRACK.Aug 22, 1995 · N271FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA01160Clip · crackedCRACKED STR CLIP AT BS 910 STR 5R. REMOVED AND REPLACED STR CLIP AT BS 910 STR 5R.Aug 22, 1995 · N271FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 95FDEA01156Skin · lightning strikeLIGHTNING STRIKE AT BS 491 STR 17R. REPAIRED LIGHTNING STRIKE AT BS 491 STR 17R IAW FEDEX SRM 53-30-3, FILLET SEALED PATCH AND PAINTED.Aug 21, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01144Skin · dentedSKIN DENTED INWARD AT BS 324, BETWEEN STR 3L AND 4L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 53-30-03.Aug 18, 1995 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 95FDEA01143Skin · lightning strikeLIGHTNING STRIKE ON RT ELEVATOR ON TRAILING EDGE AT THE OUTBOARD STATIC WICK BASE. REPAIRED LIGHTNING STRIKE ON RT ELEVATOR ON TRAILING EDGE AT THE OUTBOARD STATIC WICK BASE, IAW FEDEX SRM 52-00-03 AND 51-80-7.Aug 18, 1995 · N271FE · Boeing 727233 · Elevator, Plate/SkinSDR 95FDEA01142Skin · dentedNR 3 CARGO DOOR OUTER SKIN IS DENTED 5.5, AFT OF FWD EDGE 21.5 UP FROM LOWER EDGE. REPAIRED NR 3 CARGO DOOR OUTER SKIN DENT, BY INSTALLING EXTERNAL REPAIR IAW FEDEX SRM 52-00-03.Aug 18, 1995 · N271FE · Boeing 727233 · Cargo/Baggage DoorsSDR 95FDEA01137Frame · dentedFOUND DENTS ON FRAME BS 700 BETWEEN STR 23 TO 25L. REMOVED DAMAGE AND REPAIRED PER SRM 51-40-03.Aug 17, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01134Frame · dentedFOUND DENTS ON FRAME STA 680 LT BETWEEN STR 22-25. CUT OUTDAMAGE AND REPAIRED PER SRM 51-40-03.Aug 16, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA11127Frame · dentedFOUND DENT ON FRAME, STA 660 LT BETWEEN STR 23-25L. TRIMMED OUT AND REMOVED DENT ON FRAME STA 660L STR 23-25L. REPAIRED FRAME PER FEDEX SRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01131Stringer · dentedFOUND DENT ON FRAME, STA 600 LT BETWEEN STR 23-25L. REPAIRED DENT ON FRAME BS 600 BETWEEN STR 23-25L PER FEDEX SRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 95FDEA01130Frame · dentedFOUND DENT ON FRAME STA 520 LT BETWEEN STR 23-24L. REPAIRED DENT ON FRAME STA 520 LT BETWEEN STR 23-24L IAW FEDEX SRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01129Frame · dentedFOUND DENT ON FRAME STA 500 RT BETWEEN STR 22-23R. REPAIRED DENTED FRAME BS 500 RT BETWEEN STR 22-23R IAW FEDEX SRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01128Frame · dentedFOUND DENT ON FRAME, STA 680 RT BETWEEN STR 20-25R. REMOVED DAMAGE FROM FRAME STA 680R STR 20-25R. REPAIRED PER FEDEXSRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01126Frame · dentedFOUND DENT ON FRAME STA 660 BETWEEN STR 23-25R. REMOVED AND REPLACED DAMAGE TO FRAME STA 660 STR 23-25R PER FEDEX 51-40-3, REPAIRED PER FEDEX SRM 51-40-3.Aug 15, 1995 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 95FDEA01095Detection Unit · failedFSD - ON CLIMBOUT PASSING 15,000 MSL, THE LOWER AFT BODY OVERHEAT LIGHT STARTED FLASHING. BLEEDS WERE NR 1 ON, LT PACKON, NR 2 RT ON, RT PACK ON, NR 3 OFF, OVERHEAT LIGHT EXTINGUISHED WITHIN 5 SECONDS OF TURNING NR 3 BLEED ON AND SYSTEM TESTED GOOD. NO FURTHAug 12, 1995 · N220FE · Boeing 727233 · Overheat DetectionSDR 95FDEA01081Overheat Warning · malfunctionedDURING CLIMB, AFTER SETTING CLIMB POWER, LOWER AFT BODY OVERHEAT LIGHT CAME ON. RAN CHECKLIST 'C'. LIGHT EXTINGUISHEDWITH RETARD OF NR 1 THROTTLE, RETURNED TO MEM. REMOVED ANDREPLACED APU KEEL BEAM FIRE LOOP. MEG BOTH LOOPS, CHECK OK. INSTALL APU, OPS CHECAug 10, 1995 · N278FE · Boeing 727233 · Overheat DetectionSDR 95FDEA01149Angle · crackedRT WING WS 656.6 S14 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED END OF CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALLED REPAIR ANGLES PER SRM 57-10-4 AND SB 727-57A 159 FIG 18.Aug 8, 1995 · N254FE · Boeing 727233 · Wing Miscellaneous Structure
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