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 CALA9701170Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN E AND E COMPARTMENT ACCESS DOOR SKIN ALONG RIGHT EDGE. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 52-00-3.Jul 25, 1997 · N45793 · Boeing 727232 · Electrical/Electronic Compartment DoorsSDR CALA9701180Angle · crackedINSPECTION FOUND A 2.25 INCH CRACK IN ANGLE INSIDE LT WING FIXED LEADING EDGE AT NOSE RIB, SLAT STA 0. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.Jul 24, 1997 · N45793 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9701178Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LT ELEVATOR LOWER SKIN JUST AFT OF PANEL NR 9313. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-20-3.Jul 24, 1997 · N45793 · Boeing 727232 · Elevator, Plate/SkinSDR CALA9701177Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT RIVET HOLE OF LT ELEVATOR LOWER SKIN JUST AFT OF PANEL NR 9310. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-20-3.Jul 24, 1997 · N45793 · Boeing 727232 · Elevator, Plate/SkinSDR DL72S971517Frame · crackedFOUND ON MV1 CK, .5 INCH VISABLE CRACK RT FWD SERVICE DOOR FRAME FROM UNDER LOWER AFT DOOR STOP CASTING. ALSO, CASTING IS CRACKED. INSTALLED FRAME SPLICE AND REPLACED CASTING PER M/M 52-12-0 PG 806.Jul 22, 1997 · N540DA · Boeing 727232 · Service DoorsSDR DL72L971429Battery Pack · dischargedAFT FLOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK M9027, ALL OPS NORMAL.Jul 21, 1997 · N505DA · Boeing 727232 · Emergency LightingSDR DL72S971620Chord · crackedNR 3 MIDFLAP WAS FOUND TO HAVE A CRACKED AFT LOWER CHORD. THIS FLAP CHORD WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0.Jul 15, 1997 · N517DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971408Vert Stab · crackedAT MV2 FOUND STA 1303 CRACK, BULKHEAD, STA 1303 IN THE VERTICAL STAB, BOTH SIDES ARE CRACKED ON WEB. STOP DRILLED CRACKS AND FABRICATED DOUBLERS PER SRM 53-10-4 FIR 17. GOT OK TO INST DOUBLERS. REPAIRED BOTH SIDES PER SRM 53-10-4 FIG 17.Jul 15, 1997 · N477DA · Boeing 727232 · Vertical StabilizerSDR DL72S971381Battery Pack · dischargedFOUND FWD CABIN EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED FWD E-PATH POWER SUPPLY M9026 AND BATTERY PACK. EMERGENCY FLOOR TRACK LIGHTING CKS GOOD.Jul 15, 1997 · N489DA · Boeing 727232 · Emergency LightingSDR DL72S971375Power Supply · inoperativeEMERG EXIT SIGN LIGHTS DON'T ILLUMINATE OVER LT WING EXITS IN TEST. REPLACED PWR SUPPLY RACK AND BATTERY PACK.Jul 13, 1997 · N496DA · Boeing 727232 · Emergency LightingSDR DL72S971383Stringer · crackedTHE FUSELAGE STR 29R WAS FOUND WITH A CRACK AND CORROSION NEAR STA 950E. THE DAMAGED SECTION OF THE STRINGER HAS BEEN CUT OUT AND REMOVED BETWEEN STA 950D+10 AND 950E+10. A NEW SECTION WAS SPLICED IN AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-8Jul 11, 1997 · N527DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S971365Actuator · failedSYS-A HYD QTY WENT TO 0 AND BOTH LOW PRESS LIGHTS CAME ON WITH EXTENSION OF FLAPS ON TAXI OUT. FOUND NUMBER 4 SLAT ACTUATOR LEAKING. REPLACED ACTUATOR.Jul 11, 1997 · N408DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971362Skin · loose fastenersFASTENERS PULLING THROUGH UPPER SKIN. SPLICED SKIN PER SRM 57-50-5, RT AILERON.Jul 11, 1997 · N517DA · Boeing 727232 · AileronsSDR DL72S971360Downlock Sensor · malfunctionedAFTER GEAR RETRACTION RIGHT MAIN GEAR INDICIATION WAS BOTH THE RED AND GREEN RIGHT GEAR INDICATORS ILLUMINATED WITH GEAR HANLDE UP. WITH HANDLE DOWN ALL GEAR INDICATED DOWN AND LOCKED. REPLACED RT LANDING GEAR DOWN LOCK SENSOR.Jul 11, 1997 · N482DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72K971364Stiffener · crackedRIGHT WING L/E SPAR STIFFENERS CRACKED AT THREE LOCATIONS, INBD SPAR STIFFENER CRACKED AT NR 6 SLAT INBD TRACK AND INBD SPAR STIFFENER CRACKED AT NR 7 SLAT INBD TRACK, OTBD SPAR STIFFENER CRACKED AT NR 7 SLAT O/B TRACK. REPAIRED PER MM 57-20-21.Jul 11, 1997 · N479DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S971444Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX .5 INCH LONG AND IS LOCATED AT APPROX WL 249 IN THE INB'D RADIUS OF THE AFT CHORD. THIS AREA IS ADDRESSED IN EO 4-59821-3, WHICH INCORPOJul 10, 1997 · N468DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S971421Skin · wornNR 4 L/E SLAT INNER SKIN WORN AND GOUGED I/B OF ACTUATOR. REPAIRED PER B-727 M/M57-54-0, FIG 801.Jul 7, 1997 · N468DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971309Drive Motor · failedAT FL 310, LOSS QUANTITY AND PRESSURE ON HYD SYS-A. FOUND FLAP HYD POWER UNIT LEAKING FLUID. REPLACED RT OTBD FLAP DRIVE MOTOR.Jul 6, 1997 · N401DA · Boeing 727232 · Trailing Edge Flap ActuatorSDR DL72S971306Light · inoperativeROW 26 OVERHEAD EMER LIGHT INOP. REPLACED LIGHT, OPS NML.Jul 6, 1997 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S971304Hydraulic Line · leakingCLIMBING THROUGH FL310, TOTAL HYD LOSS DETECTED BEFORE A-SYS LOST PRESSURE. PUMPS OFF IMMEDIATELY NO CAVITATION QTY WENT TO ZERO. REPLACED A-SYSTEM RETURN LINE IN RT WHEEL WELL CHECKS GOOD.Jul 6, 1997 · N418DA · Boeing 727232 · Hydraulic System, MainSDR DL72L971298Hydraulic Line · crackedLOSS OF B-SYSTEM PRESSURE IN FLT. BRAKE PRESSURE RESTORED AFTER LANDING GEAR EXTENSION. ACCOMPLISHED SYSTEM-B LOSS PROCEDURES IAW 727-POM. REPLACED HYDRAULIC PRESSURE LINE FROM NR 2 B-PUMP QUICK DISCONNECT FILTER MODULE. LEAK AND OPERATIONAL CHECK NORMJul 5, 1997 · N508DA · Boeing 727232 · Hydraulic System, MainSDR DL72S971395Stop Pad · crackedDOUBLER CRACKED AT LWR COVER SKIN ANGLE AT NR 7 SLAT I/B STOP PAD. REPAIRED PER DELTA ER/A 362251-14.Jul 3, 1997 · N476DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971394Vert Web · crackedVERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 EA CRACKS ONE AT LWR RT CORNER AND ONE AT LWR LT CORNER. INSTALLED REPAIR PER SRM 53-10-4.Jul 3, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971344Spar Web · crackedTHE WING CENTER SECTION REAR SPAR WEB IS CRACKED AT RBL 20.5. THE CRACK IS 2.625 LONG IN A CHEM-MILL RADIUS JUST BELOW THE SPAR UPPER CHORD. INSTALLED DOUBLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DATED 7-3-97.Jul 3, 1997 · N528DA · Boeing 727232 · Wing SparSDR DL72S971311Skin · crackedA .25 INCH VISIBLE CRACK AT NR 2 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.Jul 3, 1997 · N476DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971310Web · crackedLT VERT TORQUE BOX WEB CRACKED AT LIGHTENING HOLE STA 1230. REPAIRED PER MM 53-11-0.Jul 3, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971284Skin · damagedRIVETS PULLING THROUGH SKIN SEVERAL AREAS. SPLICED SKIN PER SRM 57-50-5, FIG 3.Jul 3, 1997 · N527DA · Boeing 727232 · AileronsSDR DL72S971374Torque Box · crackedTORQUE BOX CHORD CRACKED STA 1273R. CRACK HORIZ TORQUE BOX ANGLE STA 1273. REPAIRED PER SRM 53-10-10.Jul 2, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971354Torque Box · crackedA .75 INCH CRACK IN UPPER LT TORQUE BOX WEB STA 1215 CRACKED AT CHORD ATTACH POINT, MARKED. STOP DRILLED CRACKS, DRILLED REPAIR DOUBLER PER M/M 53-11-0, INSTALLED REPAIR.Jul 2, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971280Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM STA 344 AND RBL 2. INSTALLED REPAIR PER SRM 53-10-8 FIG 11.Jul 1, 1997 · N476DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S971348Support · crackedTHE NR 7 SLAT ACTUATOR OUTBOARD SUPPORT BRACKET DOUBLER (P/N 66-19114-2) AT SLAT STA 288.60 IS CRACKED. THIS AREA WILL BE REPAIRED PER S/B 727-57-0130, REV 2.Jun 30, 1997 · N411DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971267Hydraulic Line · rupturedSYSTEM A HYDRAULICS TOTAL FAILURE 10 MIN INTO FLIGHT. BY POM ELECTRICALLY OPERATED FLAPS AND CRANKED NOSE GEAR DOWN. MAIN GEAR DOWN BY ALTERNATE METHOD. ALL HAPPENED AT 10,000 FT AND 250 KTS. REPLACED LOWER RUDDER POWER CONTROL UNIT PRESSURE LINE, SERVICEDJun 29, 1997 · N522DA · Boeing 727232 · Hydraulic System, MainSDR DL72S971434Flange · crackedSTA 1010 FRAME UPPER FLANGE, CRACK ABOVE STG 25R. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED REPAIR DOUBLER PER SRM 53-10-4 FIG 27. REPAIRED PER SRM 53-10-4 FIG 27.Jun 27, 1997 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971251Frame · crackedA 3 INCH CRACK IN FS 930 FRAME AT STR 14R. TRIMMED UPPER FRAME PER SRM 53-10-4 FIG 25. DYE CHECKED PER SRM 53-10-4, NO CRACKS FOUND. FORMED REPAIR ANGLE FROM 071. 7075-0 SENT TO HEAT TREAT PER SRM 53-10-4. COMPLETED REPAIR PER SRM 53-10-4.Jun 27, 1997 · N495DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971359Frame · dentedFRAME DENTED AFT B/B FS 950 B ABOVE STR 26R. REMOVED DAMAGE PER SRM 53-10-4 FIG 27. DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 27. TREATED AND PAINTED FRAME AND DOUBLER PER PS 900-3-6. OK TO INSTALL. INSTALLED DOUBLER PER SRM 53-10-4 FIG 27.Jun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971358Frame · dentedFRAME DENTED AFT B/B FS 950C ABOVE STR 26R. REMOVED DAMAGE AND CHECKED FOR CRACKS PER SRM 53-10-4 PG 110, NO CRACKS FOUND. DRILLED REPAIR PER SRM 53-10-4 FIG 27. TREATED AND PAINTED DOUBLER AND AREA PER PS 900-3-6. OK TO INSTALL. INSTALLED DOUBLER PER SRJun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971357Frame · dentedFRAME DENTED AFT B/B FS 950C FRAME ABOVE STR 26L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER DRILL HOLES AND ALODINED AND PRIMED IAW SRM 53-10-4 FIG 27. OK TO INSTALL. INSTALLED REPAIR PER SRM 53-10-4 FIG 27.Jun 26, 1997 · N527DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971356Angle · crackedCRACK STOP DRILLED INSIDE NR 5 SLAT AT OUTBD ACTUATOR ROD END ATTACH ANGLE. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED REPAIR PER M/M 57-54-1 FIG 804.Jun 26, 1997 · N527DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971349Frame · double drilledDURING THE PERFORMANCE OF SI 4-61904-12, THE SECOND FASTENER HOLE ABOVE THE FLOORBEAM ON THE INBOARD FLANGE WAS DISCOVERED TO HAVE BEEN LOCATED CLOSE ENOUGH TO A PILOT HOLE TO CREATE A DOUBLE DRILLED HOLE. THE DOUBLER DRILLED HOLE WAS OVERSIZED TO 0.403 THROUJun 25, 1997 · N467DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971350Doorframe · crackedTHE C-1 CARGO DOOR OPENING AFT FRAME AT STA 620 WAS FOUND CRACKED JUST BELOW THE CARGO FLOOR LINE. THE DAMAGE CONSISTED OF AN APPROX 3.0 CRACK IN THE WEB AND A SEVERED INBOARD CHORD. THIS AREA WAS REPAIRED WITH A DOUBLER AND STRAPS, APPROVED BY FAA/DER FORM Jun 24, 1997 · N516DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971239Stringer · corrodedSTRINGER 28R WAS CUT AT STA 980 IN ORDER TO REMOVE CORROSION. THE AFT SECTION OF THE STRINGER, TO STA 1010 WAS REPLACED AND A NEW STRINGER SECTION WAS SPLICED IN. THE STRINGER WAS TOO THICK TO BE REPAIRED PER THE SRM. THE REPAIR WILL CONSIST OF SPLICING IN Jun 23, 1997 · N495DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S971221Power Supply · inoperativeAFT CABIN FLOOR TRACK LIGHTING INOP. REPLACED POWER SUPPLY, CHECKS NORMAL.Jun 22, 1997 · N519DA · Boeing 727232 · Emergency LightingSDR DL72S971228Skin · crackedTHREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. EACH CRACK IS 4 INCHES IN LENGTH AND IS THROUGH THE SKIN, BONDED DOUBLER, AND BEAR STRAP. THE DAMAGE WAS CUTOUT AND AN EXTERNAL DOUBLER AND TRIPLERJun 21, 1997 · N520DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S971242Fitting · corrosionTHE DRAG BRACE FITTING WAS FOUND CORRODED ON THE FACE OF A SMALL LUG. THE CORROSION WAS LOCALLY BLENDED TO A MAX DEPTH OF 0.030. THE LUG BORE WAS OVERSIZED TO 2.858. THIS REPAIR WAS AUTHORIZED BY FAA/ DER FORM 8110-3, DER DESIGNATION NM-2256, DTD 6-20-97.Jun 20, 1997 · N517DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S971688Chord · crackedTHE NR 2 MIDFLAP BN242 WAS FOUND WITH A CRACK IN THE AFT CHORD 41 FROM OB END OF FLAP DURING SHOP INSPECTION. THIS CONDITION WAS REPAIRED BY STOP DRILLING CRACK AND INSTALLING A DOUBLER PER 727 MM 57-52-0.Jun 19, 1997 · N495DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971590Flap · damagedNR 2 MID FLAP BN242 AFT SPAR CRACKED 32 FROM I/B END OF SPAR REPAIRED PER M/M 57-52-0 FIG 802.Jun 19, 1997 · N495DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L971199Battery Pack · dischargedEMERGENCY LIGHT WOULD NOT ILLUMINATE ON AFT CARGO DOOR. REPLACED EMERGENCY LIGHT BATTERY RACK, CKS NORMAL.Jun 19, 1997 · N508DA · Boeing 727232 · Emergency LightingSDR DL72S971236Skin · separatedAT HMV, THE T/E OF RT ELEV WAS FOUND TO BE SEPARATED IN THREE DIFFERENT AREAS. THIS WAS REPAIRED PER MM 55-20-0 PG 801.Jun 17, 1997 · N495DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S971173Water Heater · overheatedSMOKE REPORTED IN AFT CABIN BY F/A, CONFIRMED BY SECOND OFFICER. BOTH AFT LAV SMOKE DETECTORS ALARMED, DID SMOKE CLEARANCE CHECKLIST. REPLACED AFT LAV WATER HEATER, CHECKS NORMAL.Jun 17, 1997 · N490DA · Boeing 727232 · LavatoriesSDR DL72S971244Skin · damagedLEADING EDGE SLAT DENTED 48 INBOARD OF OUTBOARD END. ALSO, 3, 4, 10 RIBS CRACKED. REPAIRED PER SRM 57-54-0.Jun 16, 1997 · N477DA · Boeing 727232 · Leading Edge Devices
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