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 96FDEA00887Clamp · looseAT 3,000 FEET ON DEPARTURE, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. RIGHT DUCT PRESSURE ROSE STEADILY AND NR 3 ENGINE BLEED TRIPPED. WING ANTI-ICE WAS CLOSED. FOLLOWED RED TABS AND WENT TO 1 PACK OPS (NR 2 PACK AND NR 2 AND NR 3 BLEED OFF). STRUT LOWMay 2, 1996 · N282FE · Boeing 727233 · Pneumatic Distribution SystemSDR 96FDEA00855Skin · dentedDENT IN EXTERIOR SKIN BS 450 BETWEEN STR 15 AND 16R. REPAIRED DENT AT BS 450 BETWEEN STR 15 AND 16R PER FEDEX SRM 53-30-03.Apr 26, 1996 · N270FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00854Stringer Splice · corrodedNR0246 AND 019 CORROSION (C53-113-01, -1) ON O/B FLANGE OF STR 27R BS 680 RBL 16.Apr 26, 1996 · N270FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00841Skin · dentedNR0183 004, BULGE IN SKIN BS 205 RBL 12 WL 168. *S/D* REPAIRED BULGE IN SKIN AT BS 205, RBL 12, WL 168 IAW SRM 53-30-3.Apr 25, 1996 · N270FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00817Stringer Splice · corrosionNRO238 001, CORROSION (C53-113-01, -1) AND MISSING LEVELING COMPOUND ON STR SPLICE BS 683 LB 15 WL 149. *S/D* REMOVED AND REPLACED STRINGER SPLICE BS 683, LBL 15, WL 149.Apr 22, 1996 · N270FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00816Gate Beam · crackedNR0150, 002 FWD ENTRY DOOR LWR GATE BEAM IS CORRODED FWD SIDE BS 314 WL 214 LBL 60.Apr 22, 1996 · N270FE · Boeing 727233 · Passenger/Crew DoorsSDR 96FDEA00808Skin · corrodedCORROSION BETWEEN SKIN LAP FROM STA 680 TO 685 AT STR 14R. CUT OUT CORRODED SKIN BEHIND LAPPED SKIN AND INSTALLED REPAIR PER SRM 53-30-03.Apr 22, 1996 · N222FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00806Doubler · corrodedCORROSION (C53-113-01, -1) ON DOUBLER AT BS 720 PLUS 6 WL 149 RBL 23. MECHANICALLY REMOVED CORROSION ON DOUBLER AT BS 720A PLUS 6 WL 149 RBL 23 IN AN AREA OF .7 INCH BY 1.3 INCH BY .021 INCH OF ORIGINAL THICKNESS OF .050, AREA WAS FOUND TO BE OUT OF LIMITS PEApr 22, 1996 · N270FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00791Tr Switch · failedAFTER T/O, ENG NR 1 REVERSER OPERATING LIGHT CAME ON NR 1 ENGINE, SHUTDOWN AS PER PROCEDURE. A/C RELEASED FOR SERV PER MEL 78-2A. CHECKED WIRING HARNESS AT SWITCH FOR CONDITION, FOUND GOOD. CHECKED SW ADJ, WITHIN LIMITS. DURING T/S HAD NR 1 T/R OPS LIGHT GApr 18, 1996 · N257FE · Boeing 727233 · Engine Thrust ReverserSDR 96FDEA00794Web · crackedLIGHTENING HOLE ON TORQUE BOX VERTICAL WEB IS CRACKED .5 INCH LONG BS 1330 RBL 20 WL 185. STOP DRILLED CRACK ON TORQUE BOX WEB AT BS 1330 RBL 20 WL 185. FABRICATED REPAIR AND INSTALLED REPAIR WORK IAW FEDEX SRM 51-10-1 AND 51-40-2.Apr 17, 1996 · N269FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00793Web · crackedLIGHTENING HOLE ON TORQUE BOX VERTICAL WEB IS CRACKED .5 INCH LONG BS 1230 LBL 20 WL 185. STOP DRILLED CRACK IN TORQUE BOX WEB AT BS 1230 LBL 20 WL 185. FABRICATED REPAIR DOUBLER AND INSTALLED IAW FEDEX 51-40-2 AND 51-10-1.Apr 17, 1996 · N269FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00788Skin · damagedWHILE REMOVING SCUFF PLATES FROM LT AFT SERVICE DOOR ON CARD NR 72C200-01, FOUND DAMAGED HOLE ON OUTER SKIN AFT UPPER CORNER WHERE SCUFF PLATE FASTENER ATTACH POINT. REPAIRED DAMAGED HOLE ON OUTER SKIN AFT UPPER CORNER WHERE SCUFF PLATE FASTENER ATTACH POINT Apr 16, 1996 · N269FE · Boeing 727233 · Service DoorsSDR 96FDEA00782Keel Beam · crackedRT KEEL BEAM CRACKED AT BS 990 PLUS 1 TO PLUS 4 W/L. REPAIRED RT KEEL BEAM AT BS 990 PLUS 1 TO PLUS 4, PER FEDEX EO 7-5310-7-2356C PT 5 AND EA 7-53-10-27778.Apr 15, 1996 · N269FE · Boeing 727233 · Fuselage Main, KeelSDR 96FDEA00815Intercostal · corrodedNR0710, FLT DECK FLOOR SUPPORT INTERCOSTAL CORRODED ON TOP SURFACE FROM STA 259.5 TO 277 LBL 18.Apr 13, 1996 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00814Floor Beam · corrodedNR0708, FLOOR BEAM BELOW F/E'S SEAT AFT TRACK CORRODED ON TOP SURFACE STA 268 LBL 5. *S/D* REMOVED CORROSION PER SRM 51-10-06, INSTALLED DOUBLER PER ESO 11782 AND EA 7-5300-28617.Apr 13, 1996 · N222FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 96FDEA00813Frame · corrodedNR0704, FRAME CORRODED AT STA 227.8 BELOW F/O'S SLIDING WINDOW NEAR FLOOR. *S/D* REMOVED AND REPLACED STA 227.8 RT FRAME WEB SRM 51-10-1.Apr 13, 1996 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00819Stringer · crackedSTR 3R CRACKED AND GOUGED BETWEEN STA 420 TO 440. *S/D* REPLACED STR FROM STA 430 TO 450 PER SRM 53-10-3.Apr 12, 1996 · N222FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 96FDEA00812Skin · corrodedNR0198, SKIN BULGED FWD LWR CORNER OF AFT LAV SERVICE PANEL STA 1160 STR 22L. *S/D* REMOVED RIVETS AS MARKED PER SRM 51-30-2, NO EVIDENCE OF CORROSION. INSTALLED FASTENERS PER SRM 51-30-2.Apr 12, 1996 · N222FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00811Channel · gougedNR0168, UPPER LOBE STA 640 STR 3R, 2 DEEP GOUGES IN CHANNEL AND FLANGE CUT. *S/D* INSTALLED STR REPAIR PER SRM 53-10-3.Apr 12, 1996 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00781Stringer · double drilledFOUND DOUBLE DRILLED HOLE IN STRINGER AT BS 540 STR 15R. REMOVED DAMAGE PER FEDEX SRM 53-10-03 FIG 1, DETAIL 1. FABRICATED AND REPAIRED SPLICES AND FILLER PER FEDEX SRM 53-10-03, FIG 1 DETAIL 1. ALODINE AND PRIMERED PER FEDEX SRM 51-10-2 AND INSTALLED FASTEApr 11, 1996 · N269FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 96FDEA00755Flap Assy · corrodedNR 0130 AND 003, DUE TO NUMEROUS CORROSION DISCREPANCIES, NR 5 K-FLAP ASSY REQUIRES REPLACEMENT.Apr 8, 1996 · N269FE · Boeing 727233 · Leading Edge DevicesSDR 96FDEA00754Hinge Lug · corrosionNR 0381 AND 004, NR 2 K-FLAP O/B HINGE LUG O/B UPPER BOLT HAS CORROSION AROUND IT. REPLACED NR 2 K-FLAP PER FEDEX MM 27-81-01, DUE TO CORROSION BEING EXCESSIVE.Apr 8, 1996 · N269FE · Boeing 727233 · Leading Edge DevicesSDR 96FDEA00753Skin · lightning strikeLIGHTNING STRIKE BS 650 STR 6R. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER PARTS AND INSTALLED. TREATED, PRIMED AND PAINTED REPAIR PARTS AND AREA AT BS 650 STR 6R, ALL WORK DONE IAW FEDEX SRM 53-30-3.Apr 8, 1996 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 96FDEA00752Pressure Pan · crackedUPON REMOVAL OF PRESSURE PAN, FOUND TWO CRACKS AT BS 757 RBL 65 TO 68 WL 207. REMOVED DAMAGE ON PRESSURE PAN, FABRICATED AND INSTALLED REPAIR PARTS AT BS 757 RBL 65 TO 68 WL 207 PER FEDEX SRM 51-40-2.Apr 8, 1996 · N269FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00707Frame · damagedDAMAGED FASTENER HOLE IN FRAME AT BS 20A LBL 10 STR 28L. REPAIRED PER FEDEX SRM 51-40-02.Mar 27, 1996 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00706Inner Skin · corrosionCORROSION (C53-111-02, 2) NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT EDGE 10 INCHES FROM THE BOTTOM. REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUT FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRMar 27, 1996 · N275FE · Boeing 727233 · Cargo/Baggage DoorsSDR 96FDEA00681Outer Skin · dentedMCD HAS 2 BULGES IN THE OUTER SKIN AT FWD AND AFT LIFT ACTUATORS. REWORKED BULGES ON MCD OUTER SKIN AT FWD AND AFT LIFT ACT TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEARANCES BETWEEN MCD OUTER SKIN AND FWD AND AFT LIFT ACT ROD ENDS IAW FEDEX MM 52Mar 25, 1996 · N275FE · Boeing 727233 · Cargo/Baggage DoorsSDR 96FDEA00680Fairing Formers · corrosionCORROSION (C53-132-01) ON FAIRING FORMERS BS 740 TO 846 WL 138.5 LBL TO RBL 10. REMOVED DAMAGED SECTION AND REPLACED WITH NEW PARTS USING OLD PARTS AS A TEMPLATE AT BS 740 TO 846 WL 138.5 LBL TO RBL 10 IAW PER FEDEX SRM 51-10-1.Mar 25, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00678Floor Beam · corrodedCORROSION ON BS 1130 FLOOR BEAM RBL 55 TO LBL 55 WL 200 AT NUTPLATE HOLES. REPAIRED DAMAGED AREA ON BS 1130 FLOOR BEAM RBL TO LBL 55 WL 200 AT NUTPLATE HOLES PER FEDEX EA NR 7-5310-28075.Mar 21, 1996 · N275FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 96FDEA00665Skin · gougedNR 1 CARGO DOOR OUTER SKIN IS GOUGED 20 INCHES FWD THE AFT EDGE, 2 INCHES UP FROM THE BOTTOM. REMOVED GOUGE WITH A .193 DRILL BIT AND INSTALLED RIVET WET WITH SEALANT.Mar 20, 1996 · N275FE · Boeing 727233 · Cargo/Baggage DoorsSDR 96FDEA00664Seat Track · corrodedCORROSION (C53-224-01, 2) ON EXPANSION LINK SEAT TRACK IS OUT OF LIMITS AT BS 850 TO 870 RBL 25 WL 208.5. REMOVED CORRODED EXPANSION LINK AND REPLACED REF SRM 51-10-1.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00663Seat Track · corrosionCORROSION ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 RBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK REF SRM 51-30-2.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00662Frame · corrodedCORROSION (C53-224-01) BS 460 BETWEEN STR 4 AND 5R FRAME HAS CORROSION. REMOVED CORROSION AND REPAIRED FRAME BS 460 BETWEEN STR 4 AND 5R PER FEDEX EA 7-5310-27747.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00661Angles · corrodedCORROSION ON LOWER 1183 RBL 25 VERTICAL BEAM ATTACH ANGLES UNDER DITCHING PAN. REMOVED ANGLE ATTACHED TO VERTICAL BEAM UNDER DITCHING PAN AND REPLACED WITH NEW ANGLE.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00634Frame · corrodedCORROSION (C53-224-01) BS 460 BETWEEN STR 4 AND 5R FRAME HAS CORROSION. REMOVED CORROSION AND REPAIRED FRAME BS 460 BETWEEN STR 4 AND 5R PER FEDEX EA 7-5310-27747.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00633Seat Track · corrodedCORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 25 WL 208. SEAT TRACK CORRODED OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 25 WL 208.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00632Fairing Former · corrosionCORROSION (C53-122-01) ON FAIRING FORMER AROUND NUTPLATES AT BS 740 WL 138.5 RBL TO LBL 11 TO 32 PER FEDEX SRM 51-40-3.Mar 20, 1996 · N275FE · Boeing 727233 · Aerodynamic FairingsSDR 96FDEA00631Floor Beam · corrodedCORROSION (C53-224-01, 3, 4) AND BARE METAL ON UPPER CHORD OF FLOOR BEAM BS 1070 RBL 25 TO 55 WL 208. REMOVED DAMAGE OF UPPER CHORD OF FLOOR BEAM BS 1070 RBL 10 TO SKIN RT, REPAIRED PER FEDEX SRM 53-10-8 FIG 3.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 96FDEA00630Seat Track · corrodedSEAT TRACK CORRODED OUT OF LIMITS AND CRACKED ALONG FLANGE BS 950D TO 1070 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK AT BS 950D TO 1070. DRILLED HOLES, ALODINED, PRIMED AND INSTALLED.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00629Clip · corrodedCORROSION BS 720E STR CLIPS 3 AND 4 RT HAVE CORROSION. REMOVED AND REPLACED STR CLIP AT BS 720E 3 RT PER FEDEX 51-10-1. STR CLIP 4 AT BS 720E RT FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00627Angle · corrodedCORROSION ON FAIRING FORMER BS 920E WL 138.5 LBL TO RBL 10. REMOVED AND REPLACED T-ANGLE AT BS 920E WL 138.5 LBL TO RBL 10 PER FEDEX SRM 51-30-2.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00626Seat Track · corrodedCORROSION ON THE RIGHT SIDE OF SEAT TRACK AT BS 1160 RBL 45 WL 208. REMOVED SECTION OF SEAT TRACK FROM BS 1130 TO 1173 RBL 45 AND REPLACED WITH NEW SEAT TRACK.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00625Clip · corrodedCORROSION BS 700 STR CLIP NR 5L HAS CORROSION ON IT. REMOVED STR CLIP AT BS 700 STR CLIP NR 5L. REPLACED WITH NEW STR CLIP PER FEDEX SRM 51-30-2.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00624Web · crackedCRACK IN WEB AT BS 950A PLUS 17 BL 0 WL 203.5. REMOVED DAMAGED AREA, FABRICATED REPAIR WEB AND INSTALLED PER FEDEX SRM 51-10-2.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00623Angle · crackedCRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B PLUS 10 RBL 14 WL 155. REMOVED CRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B PLUS 10 RBL 14 WL 155, FABRICATED REPAIR PART, DRILLED, ALODINED, PRIMED AND INSTALLED IAW FEDEX SRM 51-20-1.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 96FDEA00622Seat Track · corrodedCORROSION (C53-224-01) ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK AT BS 480 TO 680 LBL 45 WL 208 PER FEDEX SRM 53-10-5.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00621Frame · dentedDENT ON TOP FLANGE OF FRAME AT BS 680 RBL 39 WL 163. REPAIRED DENT ON FRAME AT BS 680 RBL 39 WL 163 IAW FEDEX SRM 51-40-3.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00620Frame · dentedDENT ON TOP FLANGE OF FRAME AT BS 660 RBL 33 WL 160. REPAIRED DENT ON TOP FLANGE PER FEDEX SRM 53-40-03.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00618Seat Track · corrodedCORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 845 LBL 45 WL 208. SEAT TRACK CORRODED BEYOND LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 45 WL 208.Mar 20, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00617Seat Track · corrosionSEAT TRACK CORRODED (C53-224-01, 3, 4) OUT OF LIMITS ALONG FLANGE AT BS 1158 RBL 25 WL 208. REMOVED SECTION OF SEAT TRACK FROM BS 1130 TO 1175 RBL 25 WL 208 AND INSTALLED NEW SEAT TRACK.Mar 19, 1996 · N275FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
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