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 DL72L992215Skin · wornDURING SHOP VISIT, THE OB LE UPPER SKIN WAS FOUND WITH WORN AREA APPROX 3 INCH LONG AT OB END. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 803 BY REMOVING THE DAMAGED SKIN AND INSTALLING A SKIN FILLER AND DOUBLER.Aug 9, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991929Rib · crackedAT HMV2, FOUND NR 6 L/E SLAT 10TH RIB FROM I/B END IS CRACKED IN TWO PLACES. REMOVED RIB, FABBED NEW PER SRM 51-00 AND INSTALLED.Aug 9, 1999 · N501DA · Boeing 727232 · Leading Edge DevicesSDR DL72L991852Rib · crackedAT HMV 2 FOUND VERT STAB INTERIOR-RIB CHORD HAS CRACK AT PREVIOUS STRINGER REPAIR-RT SIDE OF VERT AT STA 110.4 STR 10. STOP DRILLED CRACK PER MM 55-30-00 FIG 802. MADE REPAIR ANGLE PER SAME, INSTALLED.Aug 9, 1999 · N501DA · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR DL72K991766Hyd Sys · reqd serviceHYD 'A' FLUID LEVEL DROPPED TO 2.0 GAL DURING FLIGHT AND PASSENGERS REPORTED SMELLING FUMES NEAR/IN SEATS OVERWING AREA. ALT FLAPS AND MANUAL GEAR USED. A/C ARRIVED AT GATE WITH HYD QTY 3.75 GAL. SERVICED HYD TO FULL, 1 GAL ADDED. INSPECTED NOSE AND MAIN Aug 8, 1999 · N466DA · Boeing 727232 · Hydraulic System, MainSDR DL72K991765Switch · failedAFTER T/O, AFTER GEAR RETRACTION, RED DOORS WARNING LIGHT AND R GEAR DOOR WARNING LIGHTS ILLUMINATE WHEN GEAR. HANDLE PLACED TO OFF. INSPECTION AND REPLACED RT GEAR DOOR SWITCH AND SYS CKS OK.Aug 8, 1999 · N466DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S991779Skin · gougedTHE FUSELAGE SKIN WAS GOUGED AT FS 990 BETWEEN STRINGERS 24R AND 25R DUE TO GROUND DAMAGE. THE REPAIR WAS ACCOMPLISHED BYERA 333427-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991778Skin · crackedTHE FUSELAGE SKIN WAS DAMAGED DUE TO CONTACT WITH THE JETWAY AT FS 380 BETWEEN STRINGERS 17L AND 18L ON 9/13/93 AND A TEMPORARY REPAIR WAS INSTALLED. AT THIS HMV A PERMANENT REPAIR WAS INSTALLED PER ER/A 257628-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991777Skin · crackedTHE SKIN ON THE RIGHT SIDE OF THE VERTICAL STABILIZER WAS FOUND CRACKED BETWEEN FS 1203 AND 1211. THIS DAMAGE WAS REPAIRED PER ERA 333422-14.Aug 6, 1999 · N527DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S991776Shear Tie · crackedTHE FS 1283 FRAME WAS FOUND CRACKED BETWEEN STR 12L AND STR 13L. THIS DAMAGE WAS REPAIRED PER ERA 367856-14.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991775Hinge · wornTHE PIVOT HINGE ON THE REAR SPAR OF THE HORIZONTAL STABILIZER WAS WORN AT RBL 10. THIS DAMAGE WAS REPAIRED PER ER/A 367854-14 AT HMV.Aug 6, 1999 · N527DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72S991773Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT THE FRONT SPAR WHERE THE TORQUE BOX ATTACHES ON THE LEFT HAND SIDE. THE CRACK WAS FOUND AT HMV AND WAS REPAIRED PER ER/A 333420-14.Aug 6, 1999 · N527DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S991760Overheat Loop · out of positionAT APPROX 100 FEET AFE, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. REPLACED FIRE/OVERHEAT DETECTION MODULE. REPLACED KEEL BEAM LOOP M367 REPOSITIONED LOOP M 365 NEAR RT PURGE SHUTOFF VALVE. RAN ALL 3 ENGS AT T/O EPR. AT T/O EPR AFT BODY OVERHEAT CHKS NAug 6, 1999 · N517DA · Boeing 727232 · Overheat DetectionSDR DL72S991758Battery · dischargedLT MID OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT RACK M654. OPS CHKS GOO.Aug 6, 1999 · N485DA · Boeing 727232 · Emergency LightingSDR DL72S991755Skin · crackedDURING HMV INSPECTIONS IT WAS NOTED THAT THE FUSELAGE SKIN WAS CRACKED AT STRINGER 1 BETWEEN FS 1090 AND FS 1110. THIS DAMAGED WAS REPAIRED PER ER/A 333417-14 AND APPROVED BY FAA 8110-3 FORM, DER DESIGNATION DERY-635273-NM.Aug 6, 1999 · N527DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991935Insulation · splitON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-0Aug 2, 1999 · N406DA · Boeing 727232 · Electrical Power System WiringSDR DL72S991711Fuel Control · malfunctionedNR 1 ENGINE STARTED FLUX PLUS OR MINUS .2 EPR WITH ALL OTHER ENGINE INSTRUMENTS ALSO. REPLACED NR 1 ENGINE FUEL CONTROL RAN ENG, OPS NORMAL.Jul 30, 1999 · N515DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR DL72S991708Battery Pack · dischargedON SVC CK, FOUND CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN AT ROW 21 INOP. REPLACED BATTERY PACK, OPS NML.Jul 30, 1999 · N421DA · Boeing 727232 · Emergency LightingSDR DL72S991693Engine · failedNR 2 ENG OIL PRESS SLOWLY DECREASED TO ZERO WITH ASSOCIATED LOW OIL PRESS LIGHT ON. GOOD QTY AND TEMP. REPLACED ENGINE.Jul 28, 1999 · N485DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S991676Rib · damagedLWR AFT EXTERNAL SKIN OPENED UP TO FACILITATE REPAIR OF NR 6 RIB. REPAIRED SKIN PER SRM 57-54-0 FIG 801.Jul 25, 1999 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72S991674Angle · damagedT ANGLE SUPPORT DAMAGED AT AFT HINGE OF DOOR 3348. REMOVED DAMAGED PORTION OF T ANGLE. BEGAN FABRICATING T ANGLE PER M/M 53-30-1 FIG 804. FABRICATED REPAIR PIECES PER M/M 53-30-1 FIG 804. INSTALLED ANGLE REPAIR PER M/M 53-30-4 FIG 804.Jul 25, 1999 · N527DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K991669Seal · leakingDURING CRUISE AT FL290, NR 2 ENG OIL QNTY DECREASED TO ZERO GAL. OIL PRESS LOW LIGHT ILLUMINATED OIL TEMP RAISE TO 130 OIL PRESS 17 PSI ENG SHUTDOWN PER CHECKLIST WINDMILLED FOR 22 MINS. PRIOR TO SHUTDOWN OTHER INSTRUMENTS NORMAL. MAINTENANCE T/S FOUND FUEJul 25, 1999 · N415DA · Boeing 727232 · Engine Fuel PumpSDR DL72S992233Skin · wornLWR L/E SKIN WORN ON I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803.Jul 24, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991663Light · damagedONE EMERGENCY LIGHT AT 20 DEF INOP. REPLACED SEAT ASSY AT ROW 20 DEF. OPS CHECK GOOD. MCO AND PLACARD REMOVED.Jul 23, 1999 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S991641Bushing · wornON DESCENT INTO BHM, NR 2 THROTTLE RETARDED TO IDLE NR 2 ENG WENT TO HIGH POWER SETTING AND DID NOT RESPOND TO THROTTLE MOVEMENT. ACCOM PRECAUTIONARY ENG SHUTDOWN. OPENED NR 2 ENG COWLING AT GATE AND FOUND THE BUSHING ON THE FUEL CONTROL ROD WORN OUT. REPLAJul 21, 1999 · N528DA · Boeing 727232 · Fuel Controlling SystemSDR DL72S991648Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INIDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN THE PANEL. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUJul 20, 1999 · N545DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991636Strap · out of positionDOOR 2L SAFETY WAS REPORTED BY F/A TO BE FLAPPING AGAINST OUTSIDE OF A/C AFTER T/O. INSPECTED AREA, NO APPRECIABLE DAMAGE NOTED. INSPECTED INTAKE NR 1 ENG, A-OK. REPLACED DAMAGED STRAP.Jul 20, 1999 · N494DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S991635Flap · brokeON APPROACH, RIGHT O/B TRAILING EDGE FOREFLAP BROKE IN HALF. DID NOT LEAVE AIRCRAFT. DID GO-AROUND. A/C LANDED WITHOUT INCIDENT.Jul 20, 1999 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991632Skin · crackLOWER SKIN CUT TO FACILITATE MAINTENANCE. REPAIRED PER M/M 57-54-0 FIG 801.Jul 20, 1999 · N544DA · Boeing 727232 · Trailing Edge Flap ActuatorSDR DL72S991631Rib · crackedRIB CRACKED. REPAIRED RIB PER M/M 57-54-0.Jul 20, 1999 · N544DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S991629Frame · damagedC-3 CARGO DOOR / DOOR STOP FITTING MODIFICATION / OMIT FRAME DOUBLER REPAIR: AD 90-06-09. DURING CURRENT SHOP VISIT, MTC ACCOMPLISHING DOOR STOP FITTING REPLACEMENT PER EO 4-59432-3AD. DAMAGE WAS FOUND TO FWD EDGE FRAME REQUIRING REPLACEMENT. EO REQUIRES TJul 20, 1999 · N494DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S992476Spar · crackedAFT SPAR LWR CAP ANGLE, CRACKED 19 FROM INBD END. REPAIRED PER MM 57-52-0, FIG 802.Jul 19, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991626Angle · crackedNR 5 SLAT LOWER COVE ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812.Jul 19, 1999 · N404DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72K991616Battery Pack · dischargedL2 EMERGENCY BATTERY PACK FAILED TO ILLUMINATE DURING TEST. REPLACED PACK.Jul 19, 1999 · N481DA · Boeing 727232 · Emergency LightingSDR DL72S991614Light · inopDURING L/O, FOUND RIGHT OVERWING SLIDE LIGHT INOP. REPLACED BATTERY PACK.Jul 18, 1999 · N539DA · Boeing 727232 · Emergency LightingSDR DL72S991603Detector · wornNR 1 ENG STRUT OVERHEAT. REPLACED S/O VALVE AND CLAMPS. FOUND OVERHEAT DETECTOR WORN. REPLACED SAME, RAN ENG AND CKS GOOD.Jul 17, 1999 · N515DA · Boeing 727232 · Overheat DetectionSDR DL72K991607Battery · dischargedFOUND FWD AISLE EXIT LIGHT INOP, T/S SYSTEM FOUND RACK ASSY AND BATTERY INOP. REPLACED BOTH SYSTEM, OPS NORMAL.Jul 17, 1999 · N412DA · Boeing 727232 · Emergency LightingSDR DL72S991599Fasteners · missingDURING SHOP INSPECTION, FOUND FASTENERS MISSING. THERE WAS NOT ENOUGH ROOM TO ADD FASTENERS, SO THE SPAR RAIL WAS SPLICED. ON SO 738482, N/R CARD 012493 & 012494.Jul 16, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L991624Spar · crackedSTABILIZER / LT ELEVATOR / REAR SPAR : CRACK REPAIR. THE L/H ELEVATOR WAS FOUND WITH CRACK EXTENDING.125 INCH BEYOND THE 2ND FROM I/B END HINGE BRACKET. THE CRACK IS TYPICAL OF B727 S/B 55-0089 AND AD 96-06-05. THE CRACK WAS STOP DRILLED PER ER/A 367822-14Jul 16, 1999 · N512DA · Boeing 727232 · Elevator, Spar/RibSDR DL72S992332Angle · crackedDURING SHOP INSPECTION THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 56 INCHES FROM I/B END OF FLAP. A SECTION OF ANGLE WAS REPLACED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992331Angle · crackedDURING SHOP VISIT, THE AFT LOWER SPAR/CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. A REPLACEMENT SECTION OF ANGLE WAS INSTALLED ALONG WITH A DOUBLER PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992330Angle · crackedDURING SHOP VISIT, THE AFT LOWER SPAR/ANGLE WAS FOUND CRACKED 19 INCHES FROM THE I/B END. A REPLACEMENT SECTION OF ANGLE WAS INSTALLED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802.Jul 15, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991594Brake · failedAFTER TAXI TO RUNWAY, A/C REQUIRED APPROX 1.4 EPR TO INITIATE TAXI. WHEN A/C MOVED A VERY LOUD SHUDDER WAS FELT ON LT SIDE OF A/C. MAINT TOW BACK TO GATE. REPLACED NR 1 BRAKE AND TIRE ASSY DUE NR 1 BRAKE FAILUR.Jul 15, 1999 · N519DA · Boeing 727232 · BrakeSDR DL72S992289Skin · wornAPPROXIMATELY 3 INCH LONG WEAR AREA, LWR L/E SKIN O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803.Jul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992288Skin · wornLWR L/E SKIN WORN I/B END OF FLAP. REPAIRED OER MM 57-52-0 FIG 803.Jul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991647Mount · corrodedON HUSHKIT MOD, FOUND NR 2 AFT ENG MOUNT CORRODED. REPLACED MOUNT.Jul 14, 1999 · N490DA · Boeing 727232 · Engine Mount SectionSDR DL72S991617Spar · damagedNR 2 MIDFLAP/ UPPER SPAR CHORD / WBL 124.2: ALT FASTENER INSTALLED --- AD 94-07-08. DURING PREVENTATIVE MODIFICATION OF THE UPPER SPAR CHORD PER EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED UPPER SPAR CHORD FASTENER COLLAR DUE TO PROXIMITY OF THJul 14, 1999 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991587Spar · crackedWING CENTER SECTION, REAR SPAR, WEB RBL 10.75 AND LBL 14 CRACK REPAIR. THE CENTER WING REAR SPAR WAS FOUND WITH TWO SMALL TYPICAL CRACKS NEAR THE UPPER SPAR CAP AT RBL 10.75 AND LBL 14.5. THE CRACKS WERE REMOVED WITH A .25 HOLE AND .625 SLOT RESPECTIVELY. TJul 14, 1999 · N515DA · Boeing 727232 · Wing SparSDR DL72S991586Skin · crackedFUSELAGE SKIN FS 660-680, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEJul 14, 1999 · N540DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991580Rib · crackedLOWER SKIN CUT TO FACILITATE REPAIR OF RIBS. REPAIRED SKIN PER M/M 57-54-0.Jul 14, 1999 · N418DA · Boeing 727232 · Leading Edge DevicesSDR DL72S991579Frame · crackedFOUND AT F-1 LETTER CK, AFT ENTRY WALL LT FRAME HAS .5 INCH VISIBLE CRACK APPROX 6 INCHES BELOW UPPER STOP CASTING. REPAIR PER SRM 53-10-9.Jul 14, 1999 · N418DA · Boeing 727232 · Fuselage Miscellaneous Structure
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