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 DL72L953408Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH L/E SUPPORT RIBS NR 7 AND NR 10 CRACKED AT THE LOWER END AND LOWER ATTACH ANGLE CRACKED 38 INCHES FROM I/B END. REPAIRED PER MM 57-54-0.Jul 27, 1995 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953334Shim · migratedDURING INSPECTION, A LAMINATED SHIM INSTALLED ON THE LEFT WING, INBD T/E FLAP, INBD TRACK WAS FOUND TO HAVE MIGRATED GREATER THAN THE 0.25 LIMIT SPECIFIED PER DAL SI 4-58662-12AD. IN COMPLIANCE WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED AND THE ATTJul 27, 1995 · N509DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953197Angle · crackedCRACK UNDER NR 3 SLAT I/B STOP PAD. FOUND AT B-2 LTR CHECK, REPAIRED PER MM 57-54-0.Jul 26, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953196Angle · crackedA .25 INCH CRACK COVE SKIN ATTACH ANGLE UNDER ANTI-ICE DUCT AT NR 8 SLAT. FOUND AT B-2 LTR CHECK, REPAIRED PER SRM 57-54-0.Jul 26, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953195Act Bracket · crackedA .75 INCH CRACK AT NR 3 L/E FLAP ACTUATOR MOUNT BRACKET. FOUND AT B-2 LTR CHECK, REPAIRED PER MM 57-20-21.Jul 26, 1995 · N421DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72K953212Eel Battery · dischargedON LAYOVER HAD RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL.Jul 26, 1995 · N410DA · Boeing 727232 · Emergency LightingSDR DL72S953333Panel Support · corrodedPANEL SUPPORT CORRODED BETWEEN STA 780 TO 800 LBL 8.0. FABRICATED NEW SECTION PER M/M 53-30-1 PG 807 TO 808. INSTALLED REPAIR PER MM 53-30-1 PG 807 AND FIG 804, FOUND AT HMV.Jul 25, 1995 · N493DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953190Skin · cracked2.25 INCH CRACK IN WING L/E SKIN AT WS 463.0 AFT OF NR 5 SLAT ABOVE REFUELING PANEL. FOUND AT B2 LTR CK. REPAIRED PER MM 57-20-21.Jul 25, 1995 · N416DA · Boeing 727232 · Wing, Plate/SkinSDR DL72S953189Web · cracked1) 1 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 LT. 2) .50 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 RT. FOUND AT B-2 LTR CK. REPAIRED PER MM 53-11-0.Jul 25, 1995 · N416DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953188Skin · crackedNR 7 SLAT DOUBLER CRACKED BELOW I/B STOP PAD. FOUND DURING B-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.Jul 25, 1995 · N416DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953187Skin · crackedNR 3 L/E SLAT COVE SKIN LOWER ATTACH ANGLE CRACKED BELOW THERMAL ANTI-ICE (TAI) DUCT. FOUND AT LTR CHECK. REPAIRED PER MM 57-54-0.Jul 25, 1995 · N416DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953186Bracket · crackedATTACH BRACKET CRACKED - NR 1 L/E FLAP ACTUATOR, LOWER CORNER. FOUND AT LTR CHECK, REPAIRED PE MM 57-20-21.Jul 25, 1995 · N416DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953524Aft Spar · crackedNR 3 MID-FLAP DURING HMV. SHOP INSPECTION WAS FOUND TO HAVE AFT SPAR CORD CRACKED 56 INCHES FROM INBOARD END. REPAIRED PER MM 57-52-0.Jul 24, 1995 · N493DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953523Doubler · crackedNR 3 MID-FLAP DURING HMV. SHOP INSP WAS FOUND TO HAVE AFT CORD SPAR DOUBLER CRACKED IN TWO PLACES, 19 INCHES AND 22 INCHES, FROM INBOARD END. REPAIRED PER MM 57-52-0.Jul 24, 1995 · N493DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S953177Skin · crackedFOUND DURING F-1 LETTER CHECK - NR 4 L/E FLAP CRACKED OUTBD HINGE CUTOUT. REPAIRED PER MM 57-53-0 PG 802.Jul 24, 1995 · N517DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L953176Window · missingMOMENTARY SHUDDER AT FL 350 IN CRZ. SUSPECT NR 1 ENG COMPRESSOR STALL. CHECKED INLET AND EXHAUST. BORESCOPED NR 1 ENG PER MM. RAN ALL 3 ENGS PER PFHB, OPERATION NORMAL. POST-INSPECTION FOUND THE LEFT SIDE OVERWING AFT EMERGENCY EXIT DOOR WITH THE OUTER PANJul 24, 1995 · N505DA · Boeing 727232 · Passenger Compartment WindowsSDR DL72S953175Separator Assy · burstON CLIMBOUT AT FL 2,500, HEARD LOUD BANG FOLLOWED BY VIBRATION AND RISING CABIN ALTITUDE, RETURNED ATL. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY BURST. REPLACED SAME, OPERATION NORMAL.Jul 22, 1995 · N482DA · Boeing 727232 · Humidity Control SystemSDR DL72S953162Eel Battery Pack · dischargedDURING PREFLIGHT, L-1 DOOR EMERGENCY EXIT SIGN FOUND INOP. REPLACED BATTERY, OPERATION NORMAL.Jul 22, 1995 · N525DA · Boeing 727232 · Emergency LightingSDR DL72S953390Floorbeam · corrosion1070 FLOORBEAM RBL 40 TO 60 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6, FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED DAMAGED SECTION, REPAIRED PER SRM 53-10-8 PG 1. FOUND AT HMV.Jul 21, 1995 · N493DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S953332Channel · wornTOP OF VERT U-SUPPORT CHANNELS, UNDER CABIN FLOOR, ARE WORN AT TOP AND ATTACH BOLT WASHERS AT RBL 24 AND 52 STA 720D AND 24 LBL. SUPPORTS CAME FROM B/B. INSTALLED PER SRM 53-10-9.Jul 21, 1995 · N493DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953223Inlet · crackedTEMP REPAIR OF .8750 INCH CRACK IN NR 2 ENG INLET. REPAIR LOCATED AT 12:20 JUST AFT OF FWD INLET. INSTALLED PERMANENT REPAIR PER MM 54-30-0 PG 801 TO 802.Jul 21, 1995 · N493DA · Boeing 727232 · Engine Cowling SystemSDR DL72S953140Web · crackedLT VERTICAL WEB OF NWW HAS 2.0 CRACK BETWEEN STA 294.5 AND STA 285.5, APPROX WL 170. REPAIRED PER DL ERA 302166-14AD.Jul 21, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L953355Skin · corrodedDURING CV-2 INSPECTION, CORROSION WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 700 AND OUTBD OF STRINGER 28L. DAMAGE REMOVAL RESULTED IN A 2 BY 2 CUTOUT. DUE TO THE PROXIMITY TO AN EXISTING REPAIR, THE FACT THAT THE SKIN IS A SSI ITEM AND THE PROXIMITY TO Jul 21, 1995 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953330Stringer · crackedSTR CRACKED BETWEEN STA 720B AND 720C STR 15L FWD AND AFT OF LIGHT BOX. REPAIRED PER SRM 53-10-3.Jul 20, 1995 · N493DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S953277Frame · crackedFRAME CRACKED IN HALF, STATION 312 RT SIDE AT STR 13 RT. REPAIRED PER SRM 53-10-4, FOUND AT HMV.Jul 20, 1995 · N493DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S953171Fitting · corrosionNOSE LANDING GEAR, ATTACH FITTING RIGHT SIDE AFT HOLE IS CORRODED. REAMED HOLE TO .890 TO REMOVE CORROSION PER M/M 53-40-0.Jul 20, 1995 · N493DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953125Skin · crackedDURING ROUTINE SHOP INSPECTION, NR CARD 7904 WAS WRITTEN DUE TO CRACK IN LOWER SKIN, 9 INCHES FROM O/B EDGE ON NR 6 SLAT. CRACK WAS REPAIRED PER MM 57-54-0 FIG 801.Jul 20, 1995 · N542DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953130Web · crackedFOUND DURING A-1 LETTER CHECK, .3125 INCH CRACK AT LIGHTNING HOLE LT SIDE TOP 2ND HOLE FROM FWD SIDE AFT STAIRWELL WEB. REPAIRED PER SRM 53-11-0 828.Jul 20, 1995 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953219Angle · stop drilledNR 5 SLAT ACTUATOR SUPPORT ANGLE ON O/B SIDE HAS CRACK STOP DRILLED. INSTALLED DOUBLER PER M/M 57-54-0 PG 805.Jul 19, 1995 · N493DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S953170Fitting · corrodedFITTING CORRODED, NLG LT ATTACH FITTING IS CORRODED ON BEARINGS ON FACE AND ON PADS. MACHINED BORE TO 2.625 FOR CORROSION REMOVAL. MACHINED SPOTFACES OF FITTING AND CAP TO REMOVE CORROSION LUG THICKNESS, FITTING 1.499 INCH, CAP 1.434 INCH WITHIN LIMITS OF M/Jul 19, 1995 · N493DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953169Fitting · corrodedFITTING CORRODED NLG RT ATTACH FITTING IS CORRODED ON BEARING ON FACE AND PADS. MACHINED RT BORE TO 2.556 TO REMOVE CORROSION. MACHINED SPOTFACES OF FITTING AND CAP TO REMOVE CORROSION LUG THICKNESS. FITTING 1.508 INCH, CAP 1.455 INCH WITHIN M/M 53-40-0 FIGJul 19, 1995 · N493DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953168Bearings · corrodedBEARINGS, CORRODED NLG LT AND RT ATTACHMENT BEARINGS REPITTED. ACCOMPLISHED REPAIRS PER MM 53-40-0.Jul 19, 1995 · N493DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S953120Sensor · out of adjustAT 31,000 FT RIGHT MAIN GEAR DISAGREEMENT LIGHT ILLUMINATED RED ON FORWARD PANEL, NO OTHER INDICATIONS. FLT CONTINUED WITH GEAR HANDLE UP AS PER POM. PASSED TO MCO DDM AT 0255Z LIGHT EXTINGUISHED PASSING 6000/220 KTS. ADJUSTED RT GEAR UPLOCK SENSOR. CHECKSJul 19, 1995 · N470DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S953419Frame · corrodedTHE UPPER LEG OF THE C-3 DOOR CUTOUT FORWARD FRAME WAS FOUND CORRODED AT STA 1090, OUTBOARD OF STRINGER 27R. THE DAMAGE WAS REMOVED AND REPAIRED PER B727 SRM 51-40-3, FIGURE 1.Jul 18, 1995 · N515DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S953252Frame · wornTHE NR 2 ENGINE STA 1352 FWD COWLING MATING SURFACE RING FLANGE IS BADLY WORN. REMOVED RING LOCATED, DRILLED NEW RING AND INSTALLED NEW RING PER MM 53-11-0, FOUND AT HMV.Jul 18, 1995 · N493DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L953193Skin · corrodedFOUND ON CV2 CK. CORROSION ON SKIN LAP JOINT OUTBOARD OF STR 26R FROM STA 720C-STA 720F. REPAIR: REPAIRED PER ERA 302175-14.Jul 18, 1995 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L953182Firewall Panel · crackedFOUND ON CV2 CK, NR 2 ENG FIREWALL, NR 1 PANEL CRACKED .75 INCH, LT SIDE OF INLET, AND .50 INCH, RT SIDE OF INLET. REPAIR: REPAIRED PER SRM 54-10-3, FIG. 1.Jul 18, 1995 · N503DA · Boeing 727232 · Nacelle/Pylon, Bulkhead/FirewallSDR DL72L953108Rib · crackedFOUND DURING C-2 LETTER CHECK - SLAT RIB CRACKED .3750 INCH FOR NR 6 ACTUATOR RIB UPPER FLANGE. REPAIRED PER MM 57-54-0.Jul 18, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953107Angle · crackedFOUND DURING C-2 LETTER CHECK - NR 2 L/E SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED 1 INCH. REPAIRED ANGLE PER MM 57-54-0,Jul 18, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953106Angle · crackedFOUND DURING C-2 LETTER CHECK - COVE SKIN ANGLE CRACKED FOR NR 8 L/E SLAT UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.Jul 18, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L953105Web · crackedFOUND DURING C-2 LETTER CHECK, .1250 INCH CRACK AT LOWER LIGHTNING HOLE AT STA 1250 LT SIDE, ACCOMPLISHED REPAIRS PER M/M 53-11-0.Jul 18, 1995 · N507DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K960413Skin · crackedINNER TAI SKIN CRACKED BETWEEN RIBS 11 AND 12 AFT RIVET TAIL. REPAIRED PER MM 57-54-0 FIG 803A, FOR NR 2 L/E SLAT. FOUND DURING SHOP INSPECTION.Jul 18, 1995 · N481DA · Boeing 727232 · Leading Edge DevicesSDR CAL950616Floorbeam · corrodedSTATION 31J - CORROSION WAS FOUND ON THE MAIN CABIN FLOORBEAM AT BS 410. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-8 AND 51-10-1. (M)Jul 18, 1995 · N45793 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72L953198Angle · crackedFOUND ON CV2 CK, CRACK INBD OF ACTUATOR NR 5 SLAT. REPAIR: REMOVED SLAT PER OPN 7005, PEPAIRED PER MM 57-54-0, FIG 804.Jul 17, 1995 · N503DA · Boeing 727232 · Leading Edge DevicesSDR CAL950617Skin · crackedSTATION 31J - INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT BS 445, S19L AND THERE WAS CORROSION AT THE FASTENERS. THE CRACKED AND CORRODED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M)Jul 15, 1995 · N45793 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S953077Nose Rib · crackedFOUND DURING D-2 LETTER CHECK, NR 4 L/E SLAT ACT ATTACH RIB CRACKED 1.75 INCH I/B SIDE. REPAIRED PER MM 57-54-0.Jul 14, 1995 · N524DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953075Eel Battery Pack · dischargedDURING LAY OVER, FOUND FWD DOOR ESCAPE SLIDE LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL.Jul 14, 1995 · N517DA · Boeing 727232 · Emergency LightingSDR DL72L953065Angle · crackedFOUND DURING A-2 LETTER CHECK, CRACK IN ANGLE BL 8 LEFT STATION 1183 ON I/B RADIUS AT BOTTOM OF BULKHEAD SUPPORT ANGLE. REPAIRED PER MM 53-11-0.Jul 13, 1995 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L953064Rib · crackedFOUND DURING A-2 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT ACT ATTACH I/B RIB. REPAIRED PER MM 57-54-0.Jul 13, 1995 · N511DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72L953063Angle · crackedFOUND DURING A-2 LETTER CHECK, 1 INCH CRACK NR 11 SPOILER ACTUATOR SUPPORT FITTING I/B ATTACH ANGLE BELOW SUPPORT FITTING MOUNT BOLT. REPAIRED PER SRM 57-50-6 FIG 7.Jul 13, 1995 · N511DA · Boeing 727232 · Wing Miscellaneous Structure
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