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 DL72L951321Tube · crackedDURING CRUISE, B-SYSTEM HYDRAULIC QTY WENT TO 0. FOLLOWED ABNORMAL PROCEDURES LANDED SEA. FOUND LINE FROM NR 2 CASE DRAIN AT TEMP SWITCH CRACKED. INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE THEN SCHEDULED INSTALLATION OF REPLACEMENT LINE.Mar 16, 1995 · N509DA · Boeing 727232 · Hydraulic System, MainSDR DL72S951121Stiffener · crackedFOUND DURING B-2 LETTER CHECK, 1 INCH CRACK AT VERTICAL STIFFENER ON 1183 BULKHED LWR RADIUS BLOCK. INSTALLED DOUBLER PER N.N. 53-11-0 PG 811.Mar 15, 1995 · N469DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S951118Slat · crackedINNER SKIN CRACKED AT RIVET, O/B OF O/B ACTUATOR RIB. REPAIRED PER M/M 57-54-0 FIG 803A BY INSTALLING DOUBLER. NR 3 L/E SLAT, DAMAGE FOUND AT SHOP INSPECTION.Mar 15, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951117Angle · crackedFWD LEFT COWL LIP ON FIREWALL DAMAGED 8:00 POSITION. NBR 2 ENG. FOUND DURING B-2 LETTER CHECK.Mar 15, 1995 · N469DA · Boeing 727232 · Nacelle/Pylon, Bulkhead/FirewallSDR 95FDEA00279Coupling · leakingYMX: AFTER ABOUT 1 HR INTO FLT, LWR AFT BODY OVERHEAT LIGHT CAME ON PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. PROCEDURE STATED LEAK IS BETWEEN BLEED VALVE AND PACK VALVE. (PROBLEM NR 1 BLEED). REMOVED AND REPLACED COUPLING ASSY (ON LINE GOING TO PURGE Mar 15, 1995 · N498FE · Boeing 727232 · Pneumatic Distribution SystemSDR DL72S951147Door · crackedFOUND DURING CV-2 L/O CHK, .5 INCH CRACK IN FWD SVC DOOR FWD UPPER CORNER. REPAIRED PER MM 52-12-0 PG 808.Mar 14, 1995 · N468DA · Boeing 727232 · Service DoorsSDR DL72S951050Skin · crackedFOUND DURING F-1 LETTER CHECK, CENTER ENG INLET DUCT OUTER SKIN CRACKED .25 INCH RT SIDE FWD OF PNL 9501. REPAIRED PER M/M 54-30-0 FIG 801.Mar 13, 1995 · N493DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S951049Skin · crackedFOUND DURING F-1 LETTER CHECK, CRACK AT NBR 7 SLAT BELOW TAI TELESCOPING TUBE. REPAIRED PER MM 57-54-0 FIG 805A.Mar 13, 1995 · N493DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951046Skin · crackedFOUND ON F-1 LETTER CHECK, .375 INCH CRACK MAIN ENTRY DOOR SKIN. INSTALLED REPAIR PER MM 52-11-01 FIG 806.Mar 13, 1995 · N493DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S951422Skin · crackedTHE NR 3 SLAT 727, AFT LWR SKIN CRACKED 5 INCHES FROM O/B END. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION.Mar 11, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951421Skin · crackedTHE NR 3 SLAT 727, FWD EDGE OF SKIN CRACKED AT NUTPLATES ON RIB 9 AND 10. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION.Mar 11, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951410Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKS IN L/E RIBS NR 9 AND 10. CRACKING WAS ON THE INNER SKIN OUTBOARD OF THE OUTBOARD ACTUATOR ATTACH SUPPORT RIB, CRACK IN LOWER SKIN AT 5 FROM THE OUTBOARD END OF SLAT. ALSO, A CRACK IN THE UPPER CORNEMar 11, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951134Slat · crackedNR 3 SLAT, CRACK IN UPPER CORNER OF OPENING IN SPAR FOR TEE DUCT. INSTALLED DOUBLER PER M/M 57-54-0 FIG 810. FOUND DURING SHOP INSPECTION.Mar 11, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951094Skin · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN O/B SIDE STR 28L UNDER INNER COSTAL AFT OF STA 480. REPAIRED PER SRM 53-30-3 FIG 1.Mar 10, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950997Bearing Mount · corrodedLT MLG FWD TRUNNION BEARING MOUNT CORRODED ON INBD FACES AND ALL FOUR BORES.Mar 10, 1995 · N496DA · Boeing 727232 · Main Landing Gear Attach SectionSDR DL72L951042Rib · crackedUPPER CORNER OF BOTH ACTUATOR RIBS ON NR 6 SLAT WERE FOUND CRACKED. REPAIRS WERE COMPLETED PER THE MM 57-54-0. FOUND AT SHOP VISIT.Mar 10, 1995 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L951216Skin · crackedBAY NR 6 INNER SKIN, CRACKED AROUND RIVET. REPAIRED PER MM 57-54-0 FIG 803A. BAY NR 14 DOUBLER CRACKED .5 INCH LONG FWD TOP CORNER (MKD). REPAIRED PER MM 57-54-0 FIG 804 SLAT NR 5. FOUND DURING SHOP INSPECTION.Mar 9, 1995 · N506DA · Boeing 727232 · Leading Edge DevicesSDR DL72L951076Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH CRACKED RIBS AT LOCATIONS NR 17, 18, 19. REPAIRED PER MM 57-54-0.Mar 9, 1995 · N506DA · Boeing 727232 · Leading Edge DevicesSDR CAL950186Hyd Trans Cyl · inoperativeFLT NR 0777 - IAH - THE NLG TOOK APPROXIMATELY 10 SECONDS LONGER TO EXTEND THAN THE MLG, ON APPROACH TO IAH. WHEN THE NOSE GEAR DID EXTEND IT WAS ACCOMPANIED BY A BANG. MAINTENANCE FOUND THE NLG HYDRAULIC TRANSFER CYLINDER AT FAULT. THE TRANFER CYLINDER WASMar 9, 1995 · N523PE · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S951380Angle · crackedLOWER AFT ANGLE CRACKED 2 INCHES O/B OF O/B STOP. REPAIRED PER MM 57-54-0 FIG 812. DURING SHOP INSPECTION OF NR 5 L/E SLAT.Mar 8, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951083Rib · crackedDURING SHOP INSPECTION NR 6 L/E SLAT WAS FOUND WITH L/E RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0 FIG 814.Mar 8, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951082Rib · crackedDURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIBS NR 7 AND NR 12 CRACKED. REPAIRED PER MM 57-54-0 FIG 814.Mar 8, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951080Rib · crackedDURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIB NR 4 CRACKED. (I/B RIB OF THE O/B TRACK). REPAIRED PER MM 57-54-0 PG. 813.Mar 8, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951078Rib · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE 2ND RIB FROM THE O/B END OF SLAT CRACKED. REPAIRED PER MM 57-54-0.Mar 8, 1995 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950971Frame · crackedFOUND ON LTR CK, FRAME CRACKED STA 913.5 IN WW. REPAIRED PER MM 53-11-0 PG 834.Mar 8, 1995 · N528DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S950970Torque Box Web · crackedFOUND ON LTR CK, RIGHT FWD TORQUE BOX WEB CRACKED ALONG CHORD ANGLE RIVET ROW CRACK LENGTH 1.75 INCHES TO 2.25 INCHES. CRACK AT FWD LOWER TORQUE BOX WEB EXTENDING FROM LIGHTNING HOLE. REPAIRED PER MM 53-11-0 PG 833 AND 828.Mar 8, 1995 · N528DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951055Skin · crackedFOUND ON CV2 CHECK, SKIN DAMAGED AT STR 27L BETWEEN 720A AND 720B. REPAIRED PER SRM 53-30-3 FIG 3.Mar 7, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S951084Slat · crackedDURING SHOP INSPECTION, FOUND RT WING NR 5 SLAT WITH CRACKED PREVIOUSLY INSTALLED REPAIR DOUBLER. INSTALLED NEW REPAIR PER MM 57-54-0.Mar 6, 1995 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950943Spar Stiffener · crackedFOUND DURING F-1 LETTER CHECK, NR 6 SLAT I/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED 2 INCHES. REPLACED STIFFENERS PER MM 57-20-21 PG 813.Mar 6, 1995 · N489DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950942Stiffener · crackFOUND DURING F-1 LETTER CHECK, NR 6 L/E SLAT O/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED. REPLACED STIFFENERS PER MM 57-20-21 PG 813.Mar 6, 1995 · N489DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950938Web · crackFOUND DURING F-1 LETTER CHECK, .75 INCH CRACK IN LT TORQUE BOX WEB FROM FWD LWR LIGHTENING HOLE STA 1227. REPAIRED PER MM 53-11-0 PG 828.Mar 6, 1995 · N489DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950931Fairing · crackedFOUND ON F-1 LETTER CHECK, CRACK AT NR 5 SLAT INBD TRACK FAIRING. REPAIRED PER MM 57-40-0 PG 820-821.Mar 6, 1995 · N489DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951113Transverse Beam · crackedDURING LETTER CHECK INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED. PER THE B727 S/B 53-0129, REV 4, THE PART WILL BE REPLACED.Mar 4, 1995 · N485DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA9520Exit Sign · crackedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK FOUND ON PASSENGER CABIN AFT ENTRY DOOR EXIT SIGN COVER. THE DAMAGED EXIT SIGN ASSEMBLY REMOVED AND REPLACED WITH PN BR9279-105 ASSEMBLY PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTOMar 3, 1995 · N15781 · Boeing 727232 · Emergency LightingSDR DL72S951112Plate Web · crackedDURING INSPECTION AT CV-2, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 270. IN ACCORDANCE WITH BAC S/B 727-53-145, THE DAMAGED PORTION OF THE WEB WAS TRIMMED OUT, AND A DOUBLER AND 4 REPAIR STRAPS WERE INSTALLED.Mar 3, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL950172Door · out of adjustFLT NR 0702 - EWR - THE NLG WOULD NOT EXTEND WHEN GEAR WAS LOWERED FOR LANDING ON APPROACH TO EWR. THE NOSE GEAR DOOR LIGHT DID NOT INDICATE OPEN AND THE NOSE GEAR DOWN AND LOCKED INDICATION DID NOT ILLUMINATE. THE GEAR WAS CYCLED AND THE NOSE GEAR EXTENDED Mar 3, 1995 · N523PE · Boeing 727232 · Landing Gear Door Retract SectionSDR CAL950171Switch · crackedIAH - FLT 148 - THE RT MLG DOOR DID NOT INDICATE UP AND LOCKED DURING GEAR RETRACTION AFTER TAKEOFF FROM IAD. THE GEAR WAS CYCLED AND THE RT MLG DOOR INDICATED UP AND LOCKED. MAINTENANCE FOUND THE S399 RT GEAR DOOR SWITCH CRACKED. THE GEAR DOOR SWITCH WAS RMar 3, 1995 · N33785 · Boeing 727232 · Landing Gear Position and WarningSDR DL72S950905Chord · crackedFOUND ON C2 LTR CK, LOWER CHORD CRACKED BELOW TAI DUCT NR 7 SLAT. REPAIRED AND INSTALLED DOUBLER PER MM 57-54-0 PG 807A.Mar 2, 1995 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950901Rib · crackedNOSE RIB CRACKED .25 INCH I/B SIDE NR 6 SLAT AT ACT ATTACH. CRACK WAS FOUND DURING C-2 LETTER CHECK TPAMM 3-2-95. STOPPED DRILLED PER MM 57-54-0 PG 803.Mar 2, 1995 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953634Skin · wornFASTENERS PULLED THROUGH SKIN AT 2ND TAB HINGE FITTING FROM INBRD, UPPER SKIN OF LEFT OUTBOARD AILERON. REPAIRED DURING SHOP VISIT`PER SRM 57-50-5 FIG 3.Mar 1, 1995 · N418DA · Boeing 727232 · AileronsSDR DL72L950987Cowl · wornDURING INITIAL INSPECTION OF NR 1 ENGINE NOSE COWL. FOUND FORWARD BULKHEAD OUTER ANGLE AT THE 9 O'CLOCK POSITION WITH ELONGATED BOLT HOLES. REPAIRED PER SRM 54-10-3 FIG. 3.Mar 1, 1995 · N506DA · Boeing 727232 · Engine Cowling SystemSDR 95FDEA00196Press Controller · failedLOSS OF PRESSURIZATION AT FL 310. UNABLE TO MAINTAIN CABIN PRESS IN AUTO, MANUAL, OR STANDBY MODE. REMOVED AND REPLACED CABIN PRESS CONTROLLER PER MM 21-31-0. CABIN PRESSURE FUNCTION TEST NORMAL PER JRH 7-23.Mar 1, 1995 · N498FE · Boeing 727232 · Cabin Pressure ControllerSDR DL72S951098Skin · corrodedFOUND ON CV2 CHECK, CORROSION LEFT SIDE OF STRINGER SPLICE STR 28L STA 480. REPAIRED SKIN PER SRM 53-30-3 FIG 3. REPLACED FACTORY SPLICE WITH SAME.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S951097Z Angle · corrodedFOUND ON CV2 CHECK, CORROSION FOUND ON 'Z' ANGLE ABOVE STR 27R JUST FWD OF STA 620. REPAIRED PER ERA 301345-14 CODE 4-53-21-04.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951096Floor Support · corrodedFOUND ON CV2 CHECK, FLOOR SUPPORT 'Z' CHANNEL CORRODED AT FASTNER HOLES ABOVE STR 27R STA 620-640. REPAIRED PER ERA 301345-14 CODE 4-53-21-04.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951095Stringer · corrodedFOUND ON CV2 CHECK, STR 27L AT STA 720D TO FWD OF STA 720C, WITH CORROSION DAMAGE, REPAIRED PER ERA 30133744.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950978Stringer · corrodedFOUND ON CV2 CK, CORROSION BOTTOM SIDE OF O/B LEG UNDER NUTPLATE STR 28R FWD OF STA 540. REPAIRED PER SRM 53-10-3 FIG 2.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950977Seat Track · corrodedFOUND ON CV2 CK, CORROSION AT GALLEY SUPPORT TRACK BS 1070 PLUS 6. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950976Seat Track · corrodedFOUND ON CV2 CK, CORROSION AT LEFT O/B SEAT TRACK BS 1010. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950975Seat Track · corrodedFOUND ON CV2 CK, CORROSION AT SEAT TRACK FROM STA 344 TO STA 440BL 24R. REPLACED TRACK SECTION BS 344 TO 400 PER SRM 53-10-5 FIG 7.Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
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