Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72S960562Skin · crackedFOUND ON E1 LETTER CHECK, 2 CRACKS IN OUTBD SURFACE OF NR 4 L/E FLAP, 1.5 INCH AND 2 INCH. REPAIRED AND REPLACED L/E FLAP.Mar 12, 1996 · N478DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960560Bracket · crackedFOUND DURING F-1 LETTER CHECK, CRACK EXTENDING FROM NR 2 SLAT ACTUATOR MOUNT BRACKET UPPER I/B BOLT HOLE. REPAIRED PER M/M 57-42-0.Mar 12, 1996 · N403DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S960559Web · crackedFOUND DURING E-1 LETTER CHECK, LIGHTENING HOLE AT RT FWD TORQUE BOX WEB CRACKED .1875 INCH. REPAIRED PER MM 53-11-0.Mar 12, 1996 · N478DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960558Bracket · crackedFOUND DURING F-1 LETTER CHECK, 1 INCH CRACK AT NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-54-21.Mar 12, 1996 · N403DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S960557Bracket · crackedFOUND DURING E-1 LETTER CHECK, NR 1 SLAT ACTUATOR SUPPORT BRACKET CRACKED I/B SIDE. REPAIRED PER MM 57-20-21 PG 812.Mar 12, 1996 · N478DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72K960561Battery · dischargedON PREFLIGHT, R-1 DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND OPERATION NORMAL.Mar 12, 1996 · N414DA · Boeing 727232 · Emergency LightingSDR DL72S960548Web · crackedVISIBLE CRACK IN STA 870 BULKHEAD WEB BELOW LOAD CONTROL VALVE BOX INSIDE PANEL 3455R. CRACK MEASURES 3 INCHES LONG ON AFT SIDE OF WEB FROM LOAD CONTROL VALVE BOX CUTOUT, EXTENDING DOWN AND OUTBOARD. REPAIRED PER SRM 53-10-9 FIG 13.Mar 11, 1996 · N470DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960546Former · crackedFOUND DURING C-2 LETTER CHECK, 1.25 INCH CRACK VERT STAB FORMER AT STRINGER ATTACH POINT, FIN STATION 110.4 AND STR 9 LEFT. REPAIRED PER M/M 55-30-3 PG 802.Mar 11, 1996 · N470DA · Boeing 727232 · Vertical StabilizerSDR DL72K961227Skin · corrosionCORROSION WAS REMOVED FROM THE FUSELAGE SKIN AT STATION 700 AND STRINGER 28L RESULTING IN A 3 INCH FWD, AFT BY 1.25 INCH I/B, O/B CUTOUT. THE SKIN IS MADE FROM .160 2024-T3 MILLED TO 0.050 LOCALLY.Mar 11, 1996 · N412DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960733Skin · damagedDURING INSPECTION, RT ELEVATOR WAS FOUND WITH T/E DAMAGED AT 27 TO 63 INCHES FROM THE O/B END. REPAIRED DAMAGED UPPER SKIN PER SRM 55-20-3 FIG 2.Mar 10, 1996 · N515DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72K960541Fuel Control · failedENGINE FAILURE, NR 3, AT LIFT-OFF - FUEL TO ZERO WITH NORMAL WIND DOWN INDICATIONS. REPLACED FCU AND ENGINE DRIVEN FUEL PUMP.Mar 10, 1996 · N491DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR DL72K961463Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 166.5. REPAIRED PER ER/A 303276-14.Mar 9, 1996 · N491DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72K960743Bulkhead · crackedA .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT LBL 8 AND WL 168 AS A RESULT OF INSPECTIONS PER SI 4-59275-12. ACCOMPLISHED REPAIRS PER DL ERA 303278-14AD.Mar 9, 1996 · N491DA · Boeing 727232 · Fuselage Main, BulkheadSDR CAL960288Wire · brokenEWR - FLT 0242 - INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT BETWEEN SERVICE DOORS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT WIRE BUNDLE CONNECTION. THE WIRE WAS REPINNED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (X)Mar 9, 1996 · N45793 · Boeing 727232 · Light System WiringSDR DL72L960580Snap Ring · failedFWD 1L DOOR WOULD NOT OPEN AT GATE, REPEATED ATTEMPS DOOR FINALLY OPENED. FOUND SNAP RING MISSING ON UPPER ARM OF DOOR GUIDE PIN. INSTALLED SNAP RING AND OPERATION NORMAL.Mar 8, 1996 · N502DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72K960531Blkhd Beam · crackedFOUND DURING A-2 LETTER CHECK - 1.50 INCH CRACK VERTICAL BEAM BS 1183 BLKHD AT RBL 8. REPAIRED PER MM 53-11-0, PG 811.Mar 8, 1996 · N491DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S961579Angle · crackedTHERE IS A ONE INCH CRACK IN THE ANGLE OF THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THE REPAIR REPLACES THE DAMAGED PARTS IN ACCORDANCE WITH S/B 53-0129.Mar 7, 1996 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K960545Skin · crackedDURING A MID-VISIT, A CRACK WAS FOUND IN THE FUSELAGE SKIN AT STA 1250 NEAR STRINGER 23R. THERE WAS AN EXISTING REPAIR DOUBLER IMMEDIATELY FORWARD OF THE DAMAGE. INSTALLED PER ER/A 233656-14. AFT TERMINATION POINT OF THE EXISTING DOUBLER IS ROUGHLY AT STA 1Mar 7, 1996 · N412DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K960517Position Switch · malfunctionedUPON NOSE GEAR EXTENSION, HAD AN UNSAFE NOSE GEAR INDICATION. INDICATED WERE TWO GREEN MAIN GEAR LIGHTS AND ONE RED NOSE GEAR LIGHT. NO DOOR LIGHTS WERE ILLUMUMINATED. PERFORMED EMERG CK LIST IAW POM INCLUDING AN ATTEMPT AT MANUAL GEAR EXTENSION TO NO AVAILMar 7, 1996 · N471DA · Boeing 727232 · Landing Gear Position and WarningSDR MZZA96012Aoa Sensor · failedGUM - FLT 873 - STICK SHAKER CAME ON RIGHT AFTER TAKEOFF, FLAPS 15 FEET, 5 FEET, 2 FEET, STAYED ON CONSTANTLY. IT CAME ON AFTER 2 FOOT FLAPS FOR EXTENSION ON LANDING. MAINTENANCE FOUND WIRE LOSE ON NLG GROUND/AIR SENSE SWITCH. MECHANIC SECURED WIRE AND REPLMar 6, 1996 · N15790 · Boeing 727232 · Stall Warning SystemSDR DL72S960522Bracket · misinstalledDURING MID-VISIT, THE NR 2 AND NR 7 SLAT ACTUATOR MOUNT BRACKETS WERE FOUND WITH GAPS EXCEEDING THE 0.01 INCH LIMIT SET BY S.I. 4-59271-12. GAPS ARE SUBJECT OF S/B 727-57-1030. SHIMS WERE INSTALLED IN ACCORDANCE WITH THE SERVICE BULLETIN. BRACKETS WERE NOT Mar 6, 1996 · N546DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960508Angle · crackedFOUND DURING C-2 LETTER CHECK - 2 INCH CRACK NR 4 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.Mar 6, 1996 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960524Accessory Unit · malfunctionedON GEAR RETRACTION, THE RIGHT GEAR RED LANDING GEAR DISAGREEMENT LIGHT REMAINED ILLUMINATED AND REMAINED ILLUMINATED UNTIL GEAR EXTENDED FOR LANDING. PERFORMED OPERATION TEST OF UPLOCK SENSORS PER MM 32-61-811, REPLACED LANDING GEAR ACCESSSORY UNIT PER 32-09-Mar 6, 1996 · N511DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72K960520Floor Beam · corrodedFOUND ON CV-1 CHECK CORROSION ON FLOOR BEAM STA 380 RBL 55. REPAIR: REPAIRED PER M/M 53-20-11.Mar 6, 1996 · N412DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S960509Frame · crackedDURING A MID-VISIT, THE FRAME AT STATION 950F WAS FOUND WITH A DENT LOCATED NEAR STRINGER 25L AND A .25 INCH CRACK EMANATING FROM A TOOLING HOLE OUTBOARD OF STRINGER 27L. FRAME WAS SPLICED FROM THE FACTORY SPLICE AT STRINGER 25L TO JUST OUTBOARD OF STRINGER 2Mar 5, 1996 · N546DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L960500Angle · crackedFOUND ON D1 LETTER CK, NR 7 SLAT LOWER ANGLE CRACKED AT THE ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960499Angle · crackedFOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR SUPPORT BOX CRACKED INBD END. REPAIRED PER MM 57-20-21.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L960498Casting · crackedFOUND ON D1 LETTER CK, NR 2 SLAT ACTUATOR MOUNT CASTING/ANGLE CRACKED O/B UPPER EAR. REPAIRED PER MM 57-42-0.Mar 5, 1996 · N505DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960512Light · looseON PRE-FLIGHT, FOUND SECTION OF TRACK LIGHTING LOOSE WITH EXPOSED WIRING. REPAIRED WIRING SECURED TRACK, OPERATION NORMAL.Mar 4, 1996 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S960542Skin · crackedHMV/ATL - NR 4 SLAT TOP SKIN - CRACK AT OUTBOARD SIDE OF STALL FENCE MID-AREA SCREW ATTACH POINT. CORRECTION: REMOVED FENCE. INSTALLED DOUBLER REPAIR PER MM 57-40-0.Mar 3, 1996 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960491Wire · brokenON PREFLIGHT, EMERGENCY TRACK LIGHTING ON RT SIDE AT SEAT ROW 12 TO FIRST CLASS DIVIDER INOP. REPAIRED BROKEN WIRE AT SEAT ROW 12.Mar 3, 1996 · N401DA · Boeing 727232 · Light System WiringSDR DL72S960530Skin · wornDURING A ROUTINE HANGAR INSPECTION, NR 637 WAS WRITTEN DUE TO A GROOVE WORN IN INNER SKIN OF NR 5 SLAT. THE DAMAGE WAS REPAIRED PER MM 57-54-0.Mar 1, 1996 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960502Web · crackedFOUND ON C1 LETTER CK, TORQUE BOX WEB CRACKED .50 INCH AT STA 1235, LT, AND .1250 INCH AT STA 1263 RT. REPAIRED PER MM 53-11-0.Mar 1, 1996 · N416DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960501Angle · crackedFOUND ON C1 LETTER CK, FOUND 1.25 INCH CRACK AT NR 7 SLAT I/B TRACK BOX INBD ANGLE. REPAIRED PER MM 57-20-21.Mar 1, 1996 · N416DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960555Rib · crackedTHE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960554Rib · crackedTHE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960553Rib · crackedTHE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960470Angle · crackedA .25 INCH CRACK AT NR 2 SLAT COVE SKIN ANGLE BELOW I/B TRACK. FOUND DURING C-1 LTR CK TPAMM AND REPAIRED PER MM 57-54-0.Feb 29, 1996 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960465Skin · corrodedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED ALONG THE S-26L LAP JOINT AT STA 700. REMOVAL OF THE CORROSION RESULTED IN A 3 INCH WIDE BY 10 INCH LONG CUT OUT IN THE OVERLAPPING SKIN ONLY. A PREVIOUS REPAIR DOUBLER IS LOCATED WITHIN 2 INCHES OF THIFeb 29, 1996 · N468DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960464Skin · crackedDURING INSPECTION, THE SKIN AT STA 312 AND S-22R WAS FOUND TO HAVE TWO CRACKS EMANATING FROM FASTENERS. ALSO, A PREVIOUS REPAIR WAS INSTALLED JUST BELOW THE TWO CRACKS. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3, BOTH DAMAGE LOCATIONS WERE INCORPORATED UNDER Feb 29, 1996 · N468DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K960468Actuator · crackedNR 4 L/E SLAT ACTUATOR CRACKED IN FLT CAUSING A-SYSTEM HYD FLUID LOSS. REPLACED ACTUATOR.Feb 29, 1996 · N479DA · Boeing 727232 · Leading Edge Slat ActuatorSDR 96ZZZM1097Skin · delaminatedUPPER RUDDER TAB HAS DELAM AT UPPER TRAILING EDGE AND AT LOWER FACE. INSTALLED FILLER/DOUBLER AND HONEY COMB TO UPPER RUDDER TAB. INSTALLED HONEY COMB TO LOWER RUDDER TAB PER SRM 51-40-6. FIBERGLASS HOT BOND REPAIRS. (M)Feb 29, 1996 · N17789 · Boeing 727232 · Rudder, Tab StructureSDR DL72S960467Skin · crackedDURING INSPECTION, THREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. ALL CRACKS GO THROUGH THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. CRACK LENGTH VARIED FROM 1 TO 2 INCH LENGTH. IN ACCORDANCE WFeb 28, 1996 · N467DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960466Bear Strap · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL SKIN DOUBLER OF THE R-2 DOOR CUTOUT AT STATION 1070. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 2-8-96, THE DAMAGE WAS CUT OUT AND A DOUBLER AND TRIPLER INSTALLED.Feb 28, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960461Skin · crackedTHE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A .25 INCH CRACK IN THE UPPER FORWARD CORNER OF THE L-1 DOOR CUTOUT. A TIME LIMITED REPAIR HAS BEEN INSTALLED AND A PERMANENT REPAIR WILL BE INSTALLED PER SB 727-53-0186, REV 1.Feb 28, 1996 · N476DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960456Skin · crackedMAIN ENTRY DOOR OUTER SKIN CRACKED .25 INCH AT RIVET TOP AFT CORNER. FOUND AT D-2 LTR CHECK. REPAIRED PER MM 52-11-01 FIG 804.Feb 28, 1996 · N468DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960453Skin · wornLOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232 · AileronsSDR DL72S960452Spar · crackedSPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232 · AileronsSDR DL72K960488Rib · crackedFOUND ON MV1 CHECK, REFERENCE EO 04-05512-12 OPN 0304, WHILE BORESCOPING SLAT TRACK BOLT HOLES, FOUND .75 INCH CRACK IN L/E RIB NR 4 SLAT AT I/B TRACK I/B RIB. REPAIR: REPAIRED PER M/M 57-54-00, FIG 813A.Feb 28, 1996 · N415DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961607Web · crackedTHE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 2.5 INCH CRACK BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE WEB AT THIS LOCATION IS 0.040 CLAD 2024-T3. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND TWO STRAPS WILL BFeb 27, 1996 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
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