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"

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SDR FDEA201107202863Floorbeam · corrodedSURFACE CORROSION ON FLOORBEAM BS 950D, LBL 20. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 1. CUTOUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107202857Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 480 - STA 530, RBL 25. REMOVED SEAT TRACK & SPLICE SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK AND SPLICE ANGLES AND SPLICE STRAP IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1 AND INSTALLED NEW SEAT TRACK AND SPLICE PARTS Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202848Seat Track · corrodedMULTIPLE AREAS OF CORROSION ON SEAT TRACK FLANGE LBL 50 BS 780-870. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7 AND 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202840Skin · damagedRT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 580, STRINGER 7R. CUT OUT DAMAGED AREA OF FUSELAGE SKIN IAW SRM REV.103 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG. 2. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107202838Skin · damagedRT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 690, STRINGER 7R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED DOUBLER IAW SRM 51-30-4 FIG. 6 AND 53-30-3 FIG. 1Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107202827Skin · damagedRT SIDE OF FUSELAGE HAS LIGHTING STRIKE DAMAGE AT BS 265 BELOW STR 4R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG. 3 AND 53-30-2 FIG. 1.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107202826Floorbeam · corrodedMAIN CABIN BS 1110 FLOORBEAM HAS CORROSION ON UPPER SURFACE BETWEEN BL0 AND LBL26. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG. 3, FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG. 3, AND INSTALLED REPAIR PARTS IAW B727 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107202858Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 370-480, LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A & SRM 53-10-2 FIG 7, INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 & 51-10-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202867Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 383 - 480, LBL 45. REMOVED SEAT TRACK AND SPLICE PARTS AND WEB FOR ACCESS IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, SRM 51-30-5 & 53-10-2 FIG 7, TREATED AND PRIMED, AND INSTALLED SEAT TRACK SECTJul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202866Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 380 - 480, RBL 45. REMOVED SEAT TRACK SECTION AND FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-2 FIG 7A.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202861Seat Track · corrodedCORROSION SEAT TRACK SPLICE PLATE BS 480-498, LBL 45. FOUND SEAT TRACK SPLICE AND SEAT TRACK SECTION OUT OF LIMITS IAW SRM REPORT 2489. REMOVED SEAT TRACK SECTION AND SPLICE PARTS IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION AND SPLICE ANGLES, AND Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202860Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 480 - 550, RBL 45. REMOVED SEAT TRACK SECTION AND SPLICE PARTS AFTER FOUND OUT OF LIMITS IAW SRMR 2489 & SRM 51-30-2. FABRICATED NEW SEAT SECTION AND SPLICE PARTS IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1. INSTALLED NEW SEJul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202856Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 600 - 720, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM REPORT 2489 AND SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202854Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 344-390, RBL 25. REMOVED SEAT TRACK SECTION AFTER FOUND OUT OF LIMITS IAW SRM 51-30-2 & SRM REPORT 2489, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202853Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 480-600, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM 51-30-2 AND SRM 2489. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107202865Beam · misinstalledAFT PIT BS 1183 VERTICAL BEAM LBL 17.8 SEVERAL FASTENERS HAVE LOW SPACING. TRIMMED OFF BEAM AFT FLANGE AND WEB, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED IAW EA 7-5310-136787.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201107202846Skin · corrodedBS 510 BL 0 IN FWD CARGO BAY FUSELAGE SKIN HAS CORROSION AROUND ANTENNA DOUBLER. REMOVED ANTENNA STRUCTURAL DOUBLER BS 510, BL 0 IAW SRM 51-30-2. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-01, FIG 1, FABRICATED REPAIR DOUBLER IAW EA 7-5330-1541Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107202841Stringer · corrodedSTR 28L AT BS 510 HAS CORROSION INSIDE HAT CHANNEL. CUT OUT DAMAGED AREA IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3 FIG 1 AND 53-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201107202839Frame · dentedBS 500 FRAME DENTED BTWN STR 24R-25R AT UPPER FLANGE. FOUND AREA DENTED AND OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. TRIMMED OUT DAMAGE, FABRICATED REPAIR FILLER AND REPAIR DOUBLER SPLICE AND INSTALLED IAW EA 7-5310-152426.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107202824Seat Track · corrodedSURFACE CORROSION ON SEAT TRACK BL 0 BS 1140 TO 1180. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2, FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107192823Floorbeam · corrodedSURFACE CORROSION ON TOP OF FLOORBEAM BS 950, RBL 50. REMOVED UPPER TEE CAP IAW SRM 51-30-2. FABRICATED NEW TEE CAP IAW SRM 53-10-2 FIGURE 7 AND SRM 51-30-5. INSTALLED TEE CAP IAW SRM 51-30- 2 AND SRM 51-30-5.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107192818Floorbeam · corrodedSURFACE CORROSION ON FLOORBEAM, LOWER SIDE LBL58, BS 950. FLOORBEAM REPLACED ON NR NOO538.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107192815Frame · damagedRT FRAME BS 783.95, SECOND AND THIRD HOLE ABOVE FLOOR HAVE DOUBLE DRILLED HOLES. REPAIRED RIGHT HAND FRAME BS 783.95 IAW EA 7-5310-152422.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107192804Keelbeam · crackedRT KEELBEAM IS CRACKED AT SECOND HAND, THIRD FASTENER, BS 880, RBL 6. REPAIRED RT KEELBEAM AT BS 880 RBL 6 IAW EA 7-5310-152421.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, KeelSDR FDEA201107192805Keelbeam · crackedLT KEEL BEAM IS CRACKED AT SECOND FASTENER BS 880 LBL 6. REPAIRED LT KEELBEAM BS 880 LBL6 IAW EA 7-5310-152421.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, KeelSDR FDEA201107192802Floorbeam · corrodedCORROSION TOP TEE ON FLOORBEAM STA 620, LBL 45 - 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG.3. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG.3. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107192807Skin · damagedLT SIDE OF FUSELAGE SKIN IS DENTED AND CHAFED AT LAP SEAM BS 950, PLUS 10", STRINGER 26L. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIG.14. FABRICATED REPAIR PARTS DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG.14 AND 53-30-2 FIG.2. INSTALLED DOUBLER AND STRUCJul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107192811Spar · crackedCENTER TANK REAR SPAR UPPER WEB BL 0 TO LBL 2 HAS UT SHEAR WAVE CRACK INDICATION AND BL 0 TO RBL HAS HFEC CRACK INDICATION. STOP DRILLED HOLES AT CENTER TANK REAR SPAR UPPER WEB LBL 0-2 AND RBL 0-2 IAW SRM 51-10-1. LOCATED AND DRILLED HOLES AT REPAIR KIT AND Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107192810Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620, STR 8L. REMOVED DAMAGED INNER SKIN, FABRICATED AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2. FIG 3A AND SRM 51-30-2.Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107192809Skin · corrodedSKIN BULGE STA 440, STR 20R. CUTOUT DAMAGED SKIN -DAMAGED AREA, FABRICATED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER AND INSTALLED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER IAW SRM 53-30-3 FIG 12.Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107192803Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM STA 380, RBL 25 - RBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 4B. FABRICATED REPAIR PARTS AND REPAIRED TOP TEE CAP OF FLOORBEAM BS 380 IAW SRM 53-10-8 FIG. 3 AND 51-30-2.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107192999Skin · damagedRT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 198, STR 13 R. CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 13, FABRICATED DOUBLERS & FILLERS IAW SRM 53-30-3 FIG 13 & 53-30-2 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AT RT SIDE OF FUSELAGE AT BS 198 ANDJul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107192821Floorbeam · corrodedSURFACE CORROSION TOP OF FLOORBEAM, BS 950F, LBL 18. CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3 AND FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107192819Seat Track · corrodedSURFACE CORROSION ON SEAT TRACK RBL 26, BS 870 AND 950. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7 & SRM 51-30-5, AND INSTALLED NEW Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107192806Seat Track · corrodedCORROSION SEAT TRACK SPLICE PLATE M/C STA 480 - STA 500, LBL 24. REMOVED SEAT TRACK SPLICE PLATE & FOUND OUT OF LIMITS IAW SRM 51-30-2, FABRICATED NEW SPLICE PLATE IAW SRM 53-10-2 FIG 7A AND 51-30-5, INSTALLED NEW SPLICE PLATE IAW SRM 51-30-2.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107192820Structure · corrodedSURFACE CORROSION AROUND FASTENERS LOWER SIDE OF FLOORBEAM TOP TEE , BS 930, RBL 60. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 4, FABRICATED REPAIR ANGLES IAW EA 7-5310-154104, AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND EA 7-5310-154104.Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201107182784Frame · damagedAFT PIT BS1130 FRAME UPPER FLANGE HAS TRIPLE DRILLED HOLE BETWEEN STR 27L AND 28L. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR IAW SRM 51-40-3 FIG 1. INSTALLED FRAME REPAIR IAW SRM 51-30-2 AND 51-40-3 FIG 1.Jul 18, 2011 · N257FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107162731Frame · puncturedAFT PIT BS 1070 FRAME IS PUNCTURED IN UPPER FLANGE ABOVE STR 27L. CUT OUT DAMAGE AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PARTS AND FITTING IAW SRM 51-30-2Jul 16, 2011 · N257FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107152717Torque Box · crackedAFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1223. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 51-40-2.Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201107152716Torque Box · crackedAFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1233. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201106212370Turbine Blades · damagedSETTING T/O POWER HAD LOUD BANG AND ALL ENG NR 1 INSTRUMENTS DROPPED. REPEATED T/O PRIOR TO T/O. REJECTED T/O PRIOR TO T/O POWER BEING SET. ENG NR1 WAS RUNNING ROUGH AND SMOOTHED OUT AS ENG WOUND DOWN. OPEN COWLING FOUND MASSIVE AMOUNT OF OIL IN COWL. INSPJun 21, 2011 · N286FE · Boeing 727233 · Turbine SectionSDR FDEA201106022096Slide · dislodgedBIRD WAS A LAYOVER. WALKING UP CREW STAIRS DURING LINE INSPECTION, FOUND EMERGENCY ESCAPE SLIDE LYING ON CREW STAIRS. REPLACED WITH A "NEW" SLIDE.Jun 2, 2011 · N263FE · Boeing 727233 · Escape SlideSDR FDEA201105251983Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620 STR 15 - 16L ACCOMPLISHED REPAIR AT MCD INNER SURROUND SKIN IAW EA 7-5310-123597.May 25, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201105241973Skin · damagedINNER SKIN STA 540 STR 3L DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 540 STR 3L INNER SKIN IAW EA 7-5310-123595.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201105241972Support Fitting · damagedMAIN CARGO DOOR BS 620 AFT O/B SUPPORT FITTING HAS ELONGATED FASTENER HOLES REMOVED DAMAGED BS 620 TENSION ANGLE (SUPPORT FITTING), FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-2, 51-10-2, AND DRAWING 53FX1286.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201105241971Frame · damagedMAIN CARGO DOOR CUT-OUT BS 620 FRAME WEB HAS DOUBLE DRILLED FASTENERS REMOVED AND REPLACED BS 620 FRAME WEB IAW EA 7-5310-123595.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105191922Frame · damagedAFTER FRAME REMOVAL AND CLEAN UP FOUND DOUBLE DRILL HOLES STA 620 BETWEEN STR 10L TO STR 13L. CUTOUT DAMAGED AREAS (3) AT BS 620 STR 10L, STR 11L, AND STR 13L AND FABRICATED FILLERS (3). INSTALLED FILLERS (3) AND FABRICATED REPAIR DOUBLER AND REPAIR TRMay 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105191921Frame · damagedDOUBLE DRILLED HOLES FOUND UPON REMOVAL OF INNER SKIN GOING THROUGH SHIM AND FRAME STA 620, STR 9L AT 2 EACH LOCATIONS.May 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105161871Web · damagedBS 1183 HORIZONTAL CHORD & WEB WL 190 HAS FASTENERS WITH NO SPACING & DAMAGED FASTENER HOLES. ACCOMPLISHED REPAIR AT BS 1183 HORIZONTAL CHORD & WEB IAW EA 7-5310-123591.May 16, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201105111799Skin · damagedSKIN STA. 590 STR 3L HAS DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 590 STR 3L IAW EA 7-5310-123595.May 11, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
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