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 02FDEA00156Floorbeam · corrodedCORROSION C53-111-01(3) LWR SURFACE OF UPPER CHORD OF FLOORBEAM BS 1166, RBL 3, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.Feb 28, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00146Skin · dentedSKIN DENTED AT BS 1279 TO 1282, BETWEEN STR 20R & 21R. REMOVED AND REPLACED SKIN WITH DOUBLER PER SRM 53-30-3.Feb 27, 2002 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00157Frame · crackedBS 580, RBL 2, WL 156 FRAME INNER CHORD CRACKED. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-20-001.Feb 26, 2002 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00149Stringer · crackedSTR 25L CRACKED AT BS 560. REMOVED AND REPLACED STR PER SRM 53-10-3.Feb 25, 2002 · N278FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 02FDEA00154Floorbeam · corrodedCORROSION (C53-224-01,1) ON FLOORBEAM UPPER CHORD BS 560, LBL 50. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.Feb 24, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00142Skin · corrodedCORROSION ON SKIN AND STRINGER AT BS 950D TO 950E, STR 28L. REMOVED AND REPLACED SKIN PER SRM 53-30-3.Feb 23, 2002 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00148Frame · dentedFRAME DENTED AT BS 420 BETWEEN STR 8L TO 9L. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.Feb 23, 2002 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00168Floorbeam · damagedFLOORBEAM UPPER CHORD ELONGATED HOLE BS 1030, LBL 18, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.Feb 23, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00155Floorbeam · corrodedCORROSION ON LOWER CHORD BS 1070 FLOORBEAM LBL 45, RBL 50, WL 200. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 53-10-1 FIG 4 & 53-10-8 FIG 2.Feb 21, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00186Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM BS 1070, RBL 35-41, WL 208 PER SRM 53-10-1 FIG 4. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-62765.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00194Floorbeam · corrodedCORROSION, BS 1050, RBL 27, WL 208 ON TOP OF FLOORBEAM. R&R FLOORBEAM PER SRM 53-10-1 FIG 4.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00164Shear Tie · corrodedCORROSION ON SHEAR TIE BS 970, LBL 8, WL 136. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 15 & EA 7-5310-62782.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, StructureSDR 02FDEA00163Shear Tie · corrodedCORROSION ON SHEAR TIE BS 970, RBL 8, WL 136. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 5 & EA 7-5310-62782.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, StructureSDR 02FDEA00160Shear Tie · corrodedCORROSION ON SHEAR TIE BS 950F, RBL 7, WL 137. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 15 & EA 7-5310-62782.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, StructureSDR 02FDEA00170Floorbeam · damagedHOLE ON FLOORBEAM BS 720F UPPER CHORD LBL 54, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00167Shear Tie · corrodedCORROSION C53-113-01(2) ON SHEAR TIE BS 1130, LBL 8-10, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4, 51-10-2.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, StructureSDR 02FDEA00165Floorbeam · corrodedCORROSION ON LOWER SURFACE OF BS 344 FLOORBEAM. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-6, 53-10-8.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00161Shear Tie · corrodedCORROSION C53-113-01(2) ON SHEAR TIE BS 1130, LBL 8-10, WL 148. REMOVED AND REPLACED SHEAR TIE PER THE SRM.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, StructureSDR 02FDEA00159Floorbeam · corrodedCORROSION C53-224-08 ON BS 1176 CHORD LBL 36 TO LBL 65, WL 208. REMOVED AND REPLACED CHORD PER SRM 53-10-1, 51-30-2.Feb 20, 2002 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00136Switch · faulty02-51 ON RETRACT OF FLAPS AMBER LED LIGHT ON. R&R #1 L/E FLAPS POSITION SWITCH PER IAW MM 27-82-001-4. OPS CHECK GOOD.Feb 20, 2002 · N274FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 02FDEA00212Spar · wornVERT FIN MID SPAR AT FIN STA 230-231 WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MIDSPAR PER EA 7-5510-62791.Feb 19, 2002 · N278FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 02FDEA00197Frame · dentedFRAME IS DENTED AT BS 720 BETWEEN STR 24 & 25 LT. REMOVED AND REPLACED FRAME PER SRM.Feb 19, 2002 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00192Frame · dentedFRAME IS DENTED AT BS 720A BETWEEN STR 24 AND 25 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1.Feb 19, 2002 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00151Frame · corrodedCORROSION ON BS 950F FRAME ON LWR REPAIR ANGLE STR 30. REMOVED AND REPLACED ANGLE PER SRM 53-10-4.Feb 19, 2002 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00162Skin · corrodedCORROSION OF BELLY SKIN BS 965, LBL 8, WL 137. REMOVED AND REPLACED CORRODED SKIN PER SRM 53-30-3, 53-30-1.Feb 19, 2002 · N284FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00213Spar · wornVERT FIN MID SPAR IS WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MID SPAR PER SRM 55-30-6 FIG 3.Feb 18, 2002 · N278FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 02FDEA00166Frame · damagedMECHANICAL DAMAGE TO FRAME BS 804 BELOW STR 6L. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1.Feb 18, 2002 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00183Frame · dentedDENT ON FRAME AT BS 950F BETWEEN STR 26L AND 27L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-62760.Feb 18, 2002 · N278FE · Boeing 727233 · Fuselage Main, FrameSDR 02FDEA00178Intercostal · corrodedCORROSION C53-113-01(2) ON INTERCOSTAL WEB I/B AND O/B SIDES BS 1070-1090 RBL 2, WL 135-137. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-20-01, 51-10-3, 51-30-2.Feb 18, 2002 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 02FDEA00152Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER CHORD LBL 55 - RBL 55. REMOVED AND REPLACED FLOORBEAM.Feb 16, 2002 · N278FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00150Floorbeam · corrodedFLOORBEAM AT BS 720A, RBL 48 - RBL 56, WL 208 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8.Feb 16, 2002 · N278FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 02FDEA00147Skin · corrodedN 327 CORROSION ON SKIN & STRINGER AT BS 950D TO 950E, STR 28L (C53-113-01-(2)). ** S/D ** COMINGFeb 15, 2002 · N278FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 02FDEA00054Flap · out of adjON CLIMB NR 5 L/E FLAP POS IND WITHIN SHOW RETRACTED (GREEN) WITH FLAPS 2 DEG SELECTED. ACFT HANDLED AS IF SLAT WAS FULLY AND CORRECTLY RETRACTED. QRH DIRECT RECYCLING TO 5 DEG POS (EXTENDED) POS AND IND CORRECT THEN FLAPS 2 AND FLAPS UP. LIGHTS WERE OUT TIJan 17, 2002 · N275 · Boeing 727233 · Leading Edge Slat Control SystemSDR 02FDEA00033Actuator · failedAFTER RETRACT FLAPS AND SLATS 5-6 MIN LATER AMBER LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP SWITCH AND ACTUATOR PER MM 27-82-001-4, 27-81-022-4.Jan 9, 2002 · N284FE · Boeing 727233 · Leading Edge Slat ActuatorSDR PCS2002F00004Fire Detector · false activationCAPTAIN REPORTED DURING CLIMB OUT, FIRE INDICATION IN AFT CARGO ILLUMINATED. CREW NOTED THE INDICATION OCCURRED AFTER SELECTING ON THE WING ANTI-ICING. AIRCRAFT RETURNED BACK WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AFT CARGO COMPARTMENT PNEUMATIC DUCTDec 28, 2001 · N395AJ · Boeing 727233 · Fire DetectionSDR PCS2002F00009Relief Valve · defectiveCREW REPORTED NR 1 ENGINE OIL PRESSURE AT IDLE READS 37 PSI. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACE NR 1 OIL PRESSURE RELIEF VALVE MM. OPS CHECK NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE.Dec 21, 2001 · N994AJ · Boeing 727233 · Turbine Engine Oil SystemSDR PCS2002F00008Relief Valve · defectiveCREW REPORTED ENGINE NR 1 HAD 80 PSI ON CLIMB 1.85 EPR. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR OIL PRESSURE RELIEF VALVE. OPS CHECK NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE.Dec 21, 2001 · N994AJ · Boeing 727233 · Turbine Engine Oil SystemSDR 01FDEA01072Stringer · chafedVERTICAL STAB NR 7 STR LT IS CHAFED 3 INCHES FRONT OF SLIDING SEAT TRACK. REPAIRED CHAFFED AREA OF VERTICAL FIN STR 7 MID SPAR STA 229 PER SRM 55-30-06 FIG 3 PER FEDEX EA NR 7-5530-54129.Dec 17, 2001 · N285FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA01073Smoke Detector · inoperative1-398 IN CLBOUT #6 MAIN CARGO SMOKE DETECTOR LIGHT CAME ON. R&R #6 SMOKE DETECTOR PER MM 26-16-011-4.Dec 15, 2001 · N218FE · Boeing 727233 · Fire DetectionSDR 01FDEA01066Strap · corrodedCORROSION (C53-111-01, 3) ON LOWER SURFACE OF TENSION STRAP AT BS 1130, RBL 45, WL 201. REMOVED AND REPLACED PER SRM 53-10-1, 53-10-2.Dec 12, 2001 · N285FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 01FDEA01034Frame · dentedDENT IN UPPER FLANGE OF FRAME BS 970 AT STR 26L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-62617.Dec 5, 2001 · N285FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA01026Angle · corrodedCORROSION (C53-224-01, 1) UNDER MOPSILL AROUND FWD DRAIN FITTING BS 310, LBL 54, WL 208. REMOVED AND REPLACED MOPSILL REINFORCEMENT ANGLE BS 274 - 312 LBL 54 WL 208 PER SRM 51-3-2.Dec 4, 2001 · N285FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 01FDEA01035Skin · wornBS 720D+12, STR 19L SKIN PITTED AND WORN FROM FAIRING (C53-100-01). REMOVED AND REPLACED SKIN PER SRM 53-30-3 PER FIG 14.Dec 4, 2001 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA01025Solenoid · inoperative1-386 AFT T/O LG HANDLE WOULD NOT RAISE PAST OFF POS. R&R LG CONTROL LEVER SOLENOID PER MM 32-31-016-4.Dec 4, 2001 · N221FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 01FDEA01024Loop · faulty1-385 DUR CLB LWR AFT BODY OVERHEAT LIGHT CAME ON. REPOSITIONED LOOP IN LEFT SIDE OF CENTRAL STAIRS PER MM 26-14-001-2.Dec 4, 2001 · N270FE · Boeing 727233 · Overheat DetectionSDR PCS2002F00001Clamp · failedCREW REPORTED NR 1 STRUT OVERHEAT LIGHT ILLUMINATED PASSING FL220. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CLAMP AT STARTER DUCT CONNECTION NEAR 13TH STAGE BLEED VALVE, OPERATED ENGINE AT HEIGHT POWER FOR 15 MINUTES. OPSDec 3, 2001 · N395AJ · Boeing 727233 · Pneumatic Distribution SystemSDR 01FDEA01011Skin · corrodedCORROSION ON SKIN FWD CARGO BAY BS 700-720, STR 28R. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3 & EA 7-5310-62617.Nov 25, 2001 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA01005Skin · corrodedCORROSION ON SKIN FWD CARGO BAY BS 705-717 O/B OF STR 28L. REMOVED AND REPLACED DOUBLER PER SRM 53-30-3.Nov 23, 2001 · N285FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA01010Frame · dentedDENT IN FRAME UPPER FLANGE AT BS 1050, STR 26R. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-30-2 & EA 7-5310-62617.Nov 21, 2001 · N285FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA01009Frame · dentedDENT IN FRAME UPPER FLANGE AT BS 1090, STR 25L. REMOVED AND REPLACED FLANGE PER SRM 51-40-3 FIG 1 & EA 7-5310-62617.Nov 21, 2001 · N285FE · Boeing 727233 · Fuselage Main, Frame
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