Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  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 03FDEA01683Stringer · crackedN01203 LT WING STA 656.5, STRINGER 12 UPPER TAB CRACKED (VENT BOX) REPAIRED IAW EA 7-5710-55011.Oct 2, 2003 · N468FE · Boeing 727200 · Wing, Longeron/StringerSDR 03FDEA01686Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950C STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950C STRINGER 4 LT IAW SRM 51-30-2 AND 51- 30-5.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01687Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950E STRINGER 4 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 950E STRINGE 4LH IAW SRM 51-30-2 AND SRM 51-30-5.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01688Skin · corrodedCORROSION ON FUSELAGE INNER SKIN BETWEEN STR 28L - STR 27L, STA 720D TO 720E. INSTALLED REPAIR IAW SRM 53-30-3 FIG 1.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01689Frame · gougedBS 1150 FRAME GOUGED AT LBL 13 & LBL 15 WL 163 IN RADIUS. REPAIRED FRAME FAIL SAFE BS 1150, LBL 13 & 15, WL 163. ALL IAW SRM 51-40-3.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01685Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C STRINGER 6RT. ** SD ** COMINGOct 2, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01684Stringer · crackedLT WING STR 10 UPPER CRACKED AT TAB WING STA 656.50 ** SD ** COMINGOct 2, 2003 · N468FE · Boeing 727200 · Wing, Longeron/StringerSDR 03FDEA01668Frame · crackedRT 930 FRAME CRACKED AT LWR SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 RT, PER SRM 53-10-4, EA 7-5310-55032.Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01665Frame · crackedLT 930 FRAME CRACKED AT LOWER SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 LT, PER SRM 53-10-4, EA 7-5310-55032.Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01680Frame · dentedSTA 680 FRAME IS DENTED BETWEEN STRS 24 - 25R. REPAIRED IAW SRM 51-40-3 AND EA 7-5310-70536Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01679Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 4 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 4 RT IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01678Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950B, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950B, STRINGER 6 RT IAW SRM 51-30-2 & 51-30-5.Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01677Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950D, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950D, STRINGER 6 RT IAW SRM 51-30-2.Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01676Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950C, STRINGER 9 LT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 9 LT IAW SRM 51-30-2Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01675Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 5 RT. REPLACED CLIP. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 5RH IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01674Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C STRINGER 7 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, 7RH IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01671Floorbeam · corrodedCORROSION ON LOWER FLANGE OF FLOORBEAM STA 720, WL 201, RBL 18. REMOVED 1 X 1 X .031 CORROSION ON LOWER FLANGE OF FLOORBEAM BS 720, WL 201, RBL 18. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLEOct 1, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01670Floor Support · corrodedCORROSION ON LONGITUDINAL BEAM AT STA 760 TO 850 LBL 29 WL 208. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208, AND INSTALLED NEW LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208. ALL WORK DONE PER SRM 5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01669Frame · damagedN01698, BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L, REPAIR AND FASTENERS NOT INSTALLED WITH SEALANT, MECHANICAL DAMAGE ON FAIL SAFE CHORD AT TOP HORZ FASTENER, LARGE GAP BETWEEN DOUBLER AND FRAME, 1 FASTENER TO SHORT WITH GAPPED COLLAR, 1 FASTENER WITH Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01666Structure · gougedNLG WHEEL WELL HAS NUMEROUS GOUGES AROUND RT AFT PRESSURE PANEL CUTOUT. REPAIRED AS PER SRM 51-40-2.Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01663Frame · gougedMAIN CARGO DOOR FWD SIDE FRAME GOUGED 12" FROM LWR CORNER .Oct 1, 2003 · N221FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA01662Frame · gougedMAIN CARGO DOOR FWD SIDE FRAME GOUGED 52 INCHES FROM LOWER CORNER. GOUGE IN MAIN CARGO DOOR FWD FRAME 52 INCHES ABOVE LOWER CORNER FOUND TO BE OUT OF LIMITS IAW SRM 52-00-1. REPAIRED IAW FED EX EA 7-5230-70516.Oct 1, 2003 · N221FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA01661Frame · gougedMAIN CARGO DOOR AFT SIDE FRAME GOUGED 12 INCHES FROM LOWER CORNER. REPAIRED GOUGED MAIN CARGO DOOR FRAME AFT SIDE 12 INCHES FROM LOWER CORNER IAW FED EX EA 7-5230-70516Oct 1, 2003 · N221FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA01660Smoke Detector · false activationNR 5 CARGO SMOKE ALARM SOUNDED, CLIMBING THROUGH 1500 AGL SILENCED ALARM SOUNDED 3 MORE TIMES PRIOR TO LANDING. INSPECTED A/C UPON ARRIVAL. NO EVIDENCE OF CARGO SMOKE. CARGO SMOKE TEST GOOD. FOR PRECAUTION REPLACE NR 5 CARGO SMOKE DETECTOR AND CHECKED GOct 1, 2003 · N215FE · Boeing 727200 · Fire DetectionSDR 03FDEA01673Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950D STRINGER 9 LT. ** SD ** COMINGOct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01672Skin · chafedEXTERNAL SKIN CHAFED BS 720D 13 INCHES, STR 19R ** SD ** COMINGOct 1, 2003 · N469FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01667Floorbeam · corrodedN01643, CORROSION ON UPPER SURFACE OF LOWER SECTION OF FLOORBEAM BS 1070 LBL 7 WL 200. ** SD ** COMINGOct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 2003F00596Strip · out of positionFLOOR EMERGENCY GLOW STRIP DISPLACED IN AFT GALLEY. INSTALLED DISPLACED PHOTO LUMINESCENT TRACK SEGMENT PER SAFTGLO MM 33-60-13. (M)Sep 28, 2003 · N910PG · Boeing 727200 · Emergency EquipmentSDR 03FDEA01648Stringer · corrodedCORROSION ON STRINGER AT BS 720F 18, STR 27R. CUT OUT DAMAGED STR B/S 720F 9 FABRICATED AND INSTALLED STR 27R. REPAIRED IAW SRM 53-10-3 FIG 1.Sep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01643Skin · corrodedCORROSION ON FUSELAGE INNER SKIN BETWEEN STR S26-R AND S27-R, STA 720E TO 720F, UNDER STRINGER S27-R. REPAIRED IAW EA 7-5330-55027.Sep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01649Floorbeam · corrodedCORROSION BS 1130, WL 201, LBL 38 - BL 0, IN AND AROUND NUTPLATE HOLES. REPAIRED BS 1130 FLOORBEAM LOWER CHORD, W.L 201, LBL 65 TO RBL 65. CORROSION ON FLOOR BEAM WAS FOUND TO BE OUT OF LIMITS. LOWER CHORD OF 1130 FLOOR BEAM WAS REMOVED AND REPLACESep 26, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01650Floorbeam · corrodedCORROSION / GOUGE ON FLOORBEAM BS 277, LBL 14 - LBL 10, WL 208. REPAIRED FLOORBEAM BS 277, LBL 10-14 PER EA 7-5310-54991.Sep 26, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01647Stiffener · crackedRT WING FUEL TANK RIB, OB VERTICAL STIFFENER CRACKED, UPPER END, WS 171.5 BETWEEN STR 9 AND STR 10. REMOVED DAMAGED VERTICAL RIB STIFFNER AT WS 171.5 BETWEEN STR 9 & 10 RIGHT. DRILLED UP & INSTALLED NEW STIFFNER (P/N 65-8338-30) IAW SRM 51-30-5, SRM 51Sep 26, 2003 · N469FE · Boeing 727200 · Wing Miscellaneous StructureSDR 03FDEA01646Floorbeam · corrodedCORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. REMOVED CORROSION ON FLOORBEAM BS 344, LBL 42, WL 208. AREA REMOVED 2 X 1 X .022 INCH. ORIGINAL THICKNESS .125 OUT OF LIMITS CUT OUT DAMAGED AREA. 2 X 1 INCH FABRICATED, ALODINED, PRIMED, PAINTED ANDSep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01645Floorbeam · corrodedCORROSION GOUGE IN UPPER SURFACE OF FLOOR BEAM B/S 328, LBL 33, WL 208. REPAIRED IAW SRM 53-10-8.Sep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01644Floorbeam · corrodedCORROSION ON BEAM BS 269, LBL 3, WL 208. REMOVED CORROSION IN A 3.0 X 3.0 AREA, .050 MATERIAL LOSS FROM AN ORIGINAL THICKNESS OF .125 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG. 1. REMOVED FE'S SEAT TRACK AT BS 268, REMOVED 4EA FLOOR SUPPORTS AT BS 26Sep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01640Stringer Clip · corrodedCORROSION AFT CARGO BAY ON STRINGER CLIP BS 1050, RBL 14, WL 163. REMOVED CORROSION FROMS TR CLIP. ORIGINAL THICKNESS .040. AREA REMOVED 1 X 1 X .010 INCH. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR. CLIP AT BS 1050, RBL 14, WL 163. IAW SRSep 26, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01642Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED BS 685 JUST BELOW STR 26 RT. EXTERNAL FUSELAGE SKIN DAMAGE B.S. 685 BELOW STR 26 RT REPAIRED PER EA 7-5330- 70519.Sep 26, 2003 · N469FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01638Switch · failedAFTER T/O NR 6 LED FAILED TO RETRACT. COMPLIED WITH QRH AND RETURNED TO MEM. REPEAT WRITEUP, NO DIRECTIONAL PROBLEMS. DURING CREW DEBRIEF, INDICATION WAS FOR NR 6 LEADING EDGE SLAT, NOT KRUEGER FLAP. AFTER TRANSLOAD, CYCLED FLAPS SEVERALTIMES AND FINALLY DSep 26, 2003 · N496FE · Boeing 727200 · Leading Edge Slat Control SystemSDR DHL2003749515Skin · corrodedDURING C-CHECK, WING CENTER SECTION LOWER SKIN CORRODED ABOVE RT PRIMARY HEAT EXCHANGER. REMOVED CORROSION IAW B-727 SRM 51-10-6 WITH A MAT LOSS OF .057 AREAS FOUND TO BE OUT OF LIMITS IAW B-727 SRM 57-30-1 FIG 4 TABLE I FIG 5, PARA 2 FABBED DOUBLER FROM 2024Sep 25, 2003 · N749DH · Boeing 727200 · Wing, Plate/SkinSDR 03FDEA01637Indicator · false indicationAFTER TAKEOFF NR 6 LED FAILED TO RETRACT, COMPLIED WITH QRH AND RETURNED TO MEM. JUMPER INSTALLED ON NR 6 KRUEGER FLAP. DETERMINED TO BE INDICATION PROBLEM, CYCLED FLAPS SEVERAL TIMES- INDICATIONS NORMAL, REF MM27-82-000-1. REMOVED JUMPER FROM NR 6 KRUEGER Sep 25, 2003 · N496FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 03FDEA01894Warning Light · activatedLOWER AFT BODY OVERHEAT LIGHT AT CRUISE. FOLLOWED QRH- RIGHT PACK SECURED, RIGHT (NR 3) BLEED SECURED, LIGHT WENT OUT. RAN ALL 3 ENGINES AT 40 PERCENT N1 FOR APPROX 25 MINUTES (WITH AIRSTAIRS RETRACTED) NO LEAKS DETECTED AND COULD NOT GET LIGHT. OK FOR CONTSep 24, 2003 · N492FE · Boeing 727200 · Overheat DetectionSDR 03FDEA01630Stringer Clip · crackedBS 440 STR 3 LT STRINGER CLIP CRACKED. REMOVED AND REPLACED STR CLIP AT BS 440 STR 3 LT PER SRM 51-30-2, 51-30-5.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01629Floorbeam · corrodedCORROSION ON BS 1130 FLOORBEAM LOWER SECTION LBL 2 - LBL 40 WL 200. REPAIRED FLOORBEAM BS 1130 LOWER CHORD, LBL 65 TO RBL 65 PER FED EX EA 7-5310- 55008.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01628Stringer Clip · crackedSTRINGER CLIP 7R CRACKED AT B.S 720B. REPLACED STR CLIP AT BS 720B STR 7R, PER SRM 51-30-2, 51-30-5.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01627Stringer Clip · crackedSTRINGER CLIP 5 RT CRACKED AT BS 720C. REMOVED AND REPLACED STRINGER CLIP AT BS 720C, STR 5R PER SRM 51-30-2, 51-30-5.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01622Frame · dentedDENT IN FRAME BS 600, ABOVE STR 25L. REPAIRED DENT IN FRAME BS 600 ABOVE STR 25L PER FED-EX E.A. 7-5310-70526A.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01616Floorbeam · corrodedCORROSION BS 950F FLOORBEAM LWR CHORD NUTPLATE HOLES LBL 45 - RBL 45 WL 200. REPAIRED IAW SRM 53-10-8Sep 24, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01624Frame · dentedAFT CARGO BAY, FRAME DENTED BS 1110 STR 26R. DAMAGE ON FRAME AT BS 1110, STR 26R (DENT) FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 1110, STR 26R IAW SRM 51-40-3 AND EA 7-5310-54986.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01626Frame · damagedBS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L. *S/D* DAMAGE ON FRAME AT BS 950F BETWEEN 25L & 27L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 950F FRAME BETWEEN STR 25L AND 27L IAW SRM 51-40-3.Sep 24, 2003 · N468FE · Boeing 727200 · Fuselage Main, Frame
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