Boeing 727-225

Service difficulty reports · 4,226

Newest first. General aviation reporting is voluntary.

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 = '727225'
  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 FDEA201003180904Spar · crackedRT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB USING 7075T-6 .032 DIMS 12.1250" X 9.5" PO 9009201, FABRICATED NEW INBD LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO 2911884 DIMS 20.5" X 3", FABRICMar 18, 2010 · N464FE · Boeing 727225 · Wing SparSDR FDEA201003180900Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 635 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180899Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 600 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180897Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING, SKIN FWD PIT STA 580, BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180895Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 560 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180893Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 557 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180892Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 540 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180890Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 530 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180888Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD SKIN PIT STA 520 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180887Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT SKIN STA 518 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180885Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 510 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180883Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 500 BELOW STR 25L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180882Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 490 BELOW STR 25L. CUT OUT DAMAGED AREAS, FABRICATED FILLER USING 2024T-3 .125 DIMS 63.75" X 7.40", DOUBLER USING 2024T-3 .080 DIMS 62" X 13", TRIPLER USING 2024T-3 .125 DIMS 60" X 9.30", 3 SHEAR TIES USING BAC150Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180879Attach Fitting · crackedRT INBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 224, SKIN FWD OF FITTING CRACKED.Mar 18, 2010 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201003180878Seat Track · corrodedSEAT TRACK CORRODED STA 783-804 RBL 45.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003110971Rib · crackedLT WING NR 4 L/E SLAT INBD RIB IS CRACKED WHERE ACTUATOR MOUNTS TO RIB. REMOVED CRACKED RIB IN NO. 4 L/E SLAT WHERE ACTUATOR MOUNTS IAW FED EX B727 SRM, REV102, 51-30-2 AND COVE PANEL FOR ACCESS IAW B727 SRM 51-30-2. LOCATED AND DRILLED TWO RIBS IAW B727 SRMar 11, 2010 · N479FE · Boeing 727225 · Leading Edge DevicesSDR K11A2010022772401Nut · looseON CLIMBOUT NOTED OXYGEN HAD DEPLETED FROM 1750 LBS TO 1000 LBS VERIFIED ALL REGULATORS / VALVES IN NORMAL FLIGHT POSITIONS ATTEMPTED TO TEST SYSTEM AND AFTER SEVERAL SHORT BREATHS OXYGEN SYSTEM DROP TO 0 PSI AND NO FLOW. UPON INSPECTION FOUND REGULATOR NUT LFeb 27, 2010 · N724CK · Boeing 727225 · Crew Oxygen SystemSDR CA091106006Bearing · seized(CAN) TO MAINTAIN STRAIGHT FLIGHT IN CLIMB (HAND FLYING), REQUIRED AILERON TRIM 3 1/2 UNITS, CONTROL COLUMN AT 18 DEG. MX FOUND CABLE ROD END BROKEN AT SPOILER MIXER MECHANISM. BRG IN ROD END SEIZED. ROD END REPLACED.Nov 5, 2009 · Boeing 727225 · Aileron Control SystemSDR FDEA200910213627Floor Splice · corrodedAFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1330 FOUND CORRODED. FOUND OUT OF LIMIT IAW SRM 53-00-53 REV 98 AFTER CORROSION REMOVAL. CORRODED STRAP REPLACED IAW SRM 20-11-00 REV 5. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910163595Rib · crackedNR 3 SLAT HAS 2 CRACKED RIBS, INBD AND OTBD OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIBS, FABRICATED NEW RIBS, HEAT TREATED RIBS TO T4 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLED IAW SRM 51-30-2 AND 51-20-1.Oct 16, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910143576Angle · crackedNR 1 SLAT LWR AFT CHORD ANGLE IS CRACKED BELOW ACTUATOR. REMOVED ACCESS PANEL IAW SRM 51-30-2, CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED NEW LOWER CHORD, AND 1 EACH SPLICER IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1 REV 101, TREATED AND PRIMED Oct 14, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910143588Structure · crackedR/WING INBD MIDFLAP T/E CHORD CRACKED AT NR 2 AFT FLAP HINGE CUTOUT. REMOVED LOWER CHORD SECTION IAW SRM 51-30-2 LOCATED AND DRILLED NEW LOWER CHORD, INSTALLED NEW CHORD IAW SRM 51-30-2 REV 101 INSTALLED LOWER MIDFLAP PANEL IAW SRM 51-30-2 REV 101.Oct 14, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA200910133624Shear Tie · corrodedAFT PIT CORROSION AT SHEAR TIE STA 950E STR 29R REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT SHEAR TIE, FABRICATED REPAIR ANGLE USING 7075-0 .080 PO NR 9008557 DIMS 6" X 2", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLEOct 13, 2009 · N465FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA200910133553Skin · gougedLT INBD MIDFLAP UPPER SURFACE IS GOUGED WBL 80. MIDFLAP REMOVED AND REPLACED DUE TO DAMAGE BEING OUT OF LIMITS AND BEYOND ECONOMICAL REPAIR.Oct 13, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA200910123625Frame · corrodedE AND E COMPARTMENT BS 400 STR 19R CORROSION NEXT TO TOOLING HOLES. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1" DIAMETER, FABRICATED NEW FRAME REPAIR USING 7075-0 .050 PO NR 29016223, DIMS 9 3/4" X 5 1/2", HEAT TREATED PART TO T6Oct 12, 2009 · N465FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA200910123546Skin · gougedRT OTBD FOREFLAP, GOUGED AND CHAFED AT OTBD L/E. GOUGE OUT OF LIMITS IAW SRM 51-30-2, FABRICATED REPAIR DOUBLER, IAW SRM 57-50-4, FIG 1 REV 101, TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REV 101.Oct 12, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR K11A2009100972410Skin · dentedSKIN DENTED 1 X 1 INCH.Oct 10, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972409Skin · dentedSKIN DENTED 1 X 1 INCH.Oct 10, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972407Skin · dentedSKIN HAS DENT 1 X 2 INCHES.Oct 10, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972406Skin · dentedSKIN DENTED 1.3 X 1.5 INCHES.Oct 10, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910103545Lap Joint · damagedSTA 620, STR 27L, LAP SEAM LWR ROW, NO DISTANCE BETWEEN RIVETS. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED REPAIR AND FASTENERS IAW SRM 51-30-2, 53-30-3, 51-30-8 AND 51-10-2.Oct 10, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972414Skin · dentedSKIN DENTED .5 X .5 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972413Skin · dentedSKIN DENTED 2 X 2 INCHES.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972412Skin · dentedSKIN HAS DENT, 1 X 1 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972411Skin · dentedSKIN DENTED 1 X 1 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972408Skin · dentedSKIN DENTED 1 X 1 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972405Skin · dentedSKIN HAS DENT.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972404Skin · dentedSKIN HAS DENT 1 X 1 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972403Skin · dentedSKIN HAS DENT AND CREASE 1 X 4 INCHES.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972402Skin · dentedSKIN HAS DENT 1 X 1 INCH.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100972401Skin · dentedSKIN DENT.Oct 9, 2009 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910093552Floor Support · corrodedL-1 ENTRANCE WALK WAY BS 300-340, LBL 56- RBL 30, FLOOR SUPPORTS LWR SURFACES HAVE CORROSION AT N/P HOLES AS MARKED. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 2" X 1", FABRICATED 2 EACH REPAIR ANGLES USING 7075-0 .063 PO 9008655 DOct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910093531Angle · crackedAFT AIRSTAIR RT LOWER TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1273 ON FWD SIDE RADIUS. REMOVED ANGLE SUPPORT IAW SRM 51-30-2, LOCATED AND DRILLED NEW ANGLE SUPPORT IAW SRM 51-30-5 REV. 101. INSTALLED NEW UPPER WEB SUPPORT ANGLE IAW SRM 51-30-2 Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910093533Vertical Beam · misinstalledFUSELAGE STA 1183 LWR CHORD LT INBD 17.8 VERT BEAM FASTENERS SPACING SHORT. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851.Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA200910093532Frame · crackedAFT AIRSTAIR RT LWR TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1263 ON AFT SIDE RADIUS. REMOVED WEB DOUBLER, REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE USING 7075-0 .090 PO 9008486 DIMS 18" X 5 7/8", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI FOct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910083518Skin · corrodedSKIN BULGE STA 1050, STR 27L. FOUND EXFOLIATED CORROSION OUT OF LIMITS ON SKIN, CUT OUT DAMAGED AREA, CUT OUT DAMAGED STRINGER SECTION, FABRICATED REPAIR DOUBLER AND FILLERS, FABRICATED STRINGER REPAIR AND SPLICES, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2, Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910083519Stringer · damagedMAIN CARGO AREA, STA 450, STR 3L NO EDGE DISTANCE BETWEEN RIVET AND HOLE. REMOVED FASTENERS AND CUT OUT DAMAGED AREA, FABRICATED ONE FILLER, ONE PLATE, TWO PLATES, TWO PLATES AND INSTALLED IAW SRM 51-30-2, 53-10-3 AND 51-10-2.Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2009100872401Seat Track · corrodedSEAT TRACK HAS CORROSION ON TOP SIDE.Oct 8, 2009 · N724CK · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910083517Keelbeam · crackedLT KEELBEAM CHORD IS CRACKED AT BS 870, LBL 4. CUT OUT DAMAGE AREA DIM 2" IAW FEDEX 727 EA 7-5310-135501, FAB REPAIR DOUBLER MAT USED 15-5 PH .071" PO # 290342001 DIM (85/8" X 4") IAW EA 7-5310-135501. ACCOMPLISHED HARDNESS TEST VERIFICATION OF FABRICATEOct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, KeelSDR FDEA200910083516Vertical Beam · damagedAFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM WEB HAS SEVERAL DOUBLE DRILLED HOLES AT WL 190. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851, REFERENCE SDR 09-3493.Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Structure
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