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 DL72S960838Battery Pack · dischargedEMERGENCY LIGHT OVER L1 DOOR INOP. REPLACED BATTERY PACK MFR NR 3106 DAL 334101877, BATTERY WEAK.Apr 11, 1996 · N538DA · Boeing 727232 · Emergency LightingSDR 96ZZZX3504Skin · corrodedLEVEL 2 CORROSION ON SKIN DOUBLER AND RAM AIR DOOR ACTUATOR CABLE ASSEMBLY AT STA 720B TO STA 720C LBL 4 - RBL 4. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER AND FILLERS, AND INSTALLED PER SRM 53-30-3, FIGURE 1, SRM 51-30-2, SRM 51-10-2.Apr 11, 1996 · N17789 · Boeing 727232 · Fuselage Main, Plate/SkinSDR 96ZZZX3509Panel · corrodedACCESSORY PANEL AT STA 700 TO STA 720, LEFT LBL 15, EXTERIOR PANEL HAS LEVEL 2 EXFOLIATION CORROSION AROUND NUTPLATES. REMOVED CORROSION AND TREATED. REINSTALLED PANEL PER SRM 51-10-6 AND SRM 51-30-2. MATERIAL LOSS WITHIN LIMITS PER SRM 53-10-1, FIGURE 1.Apr 10, 1996 · N17789 · Boeing 727232 · Fuselage Main, Plate/SkinSDR 96ZZZX3508Web · tornBOTTOM FACE OF LOWER RUDDER, SKIN TORN AWAY AT LEFT SIDE. REMOVED SKIN PANEL, ORDERED AND INSTALLED NEW SKIN PER SRM'S 51-10-1, 51-10-2, 51-30-2. INSTALLED RUDDER PER MM 27-20-1, AND TESTED RUDDER PER MM 27-20-1.Apr 10, 1996 · N17789 · Boeing 727232 · Rudder StructureSDR 96ZZZX3495Web · corrodedWEB AT STA 720F IS CORRODED BEYOND LIMITS - KEEL BEAM CBL. REMOVED WEB, FABRICATED AND INSTALLED NEW WEB PER SRM 51-20-2. CUT WEB, FABRICATED WEB DOUBLER, AND INSTALLED PER SRM 51-40-2.Apr 10, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3493Support · corrodedSUPPORT AT STA 700 TO STA 720 RBL HAS LEVEL 2 CORROSION. FABRICATED SUPPORT PER OLD PART PER SRM 51-10-2. INSTALLED SUPPORT PER SRM 51-30-2.Apr 10, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3492Support · corrodedSUPPORT AT STA 720E TO 740 LBL 6 HAS LEVEL 2 CORROSION. FABRICATED SUPPORT ANGLE PER SRM 51-10-2 AND SRM 51-20-2. INSTALLED SUPPORT ANGLE PER SRM 51-30-2.Apr 10, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3491Support · corrodedSUPPORT AT STA 720E TO STA 740 RBL 6 HAS LEVEL 2 CORROSION. FABRICATED SUPPORT PER OLD PER PART PER SRM 51-20-2. INSTALLED SUPPORT PER SRM 51-30-2.Apr 10, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960814Angle · crackedFOUND ON A-1 LETTER CHECK, 1.5 INCH CRACK IN NR 3 L/E SLAT LWR COVE SKIN ANGLE. REPAIRED PER M/M 57-54-0.Apr 9, 1996 · N544DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960976Blkhd Stiffener · crackedA CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE VERTICAL STIFFENER FS 1183 AT RBL 8. THE CRACK WAS APPROXIMATELY 0.25 INCH IN LENGTH. S/B 727-53-0175, REV 2, WHICH IS REQUIRED BY A.D. 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND REPAIApr 8, 1996 · N498DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960807Rod End · brokenWHEN SPEEDBRAKES APPLIED ON LANDING, AIRCRAFT ROLLED TO RIGHT. FOUND NR 2 LEFT OUTBD SPOILER NOT DEPLOYING. FURTHER INVESTIGATION FOUND ROD END BROKEN REF IPC 27-10-0- 22B ITEM 5. MAINT FROM ATL REPLACED ROD END AND OPS CHECK OK.Apr 8, 1996 · N520DA · Boeing 727232 · Drag Control SystemSDR DL72S960806Skin · crackedFOUND ON A2 LETTER CHECK, 1 INCH VISIBLE CRACK ON NR 7 SLAT COVE SKIN SUPPORT ANGLE. REPAIRED PER MM 57-54-0.Apr 8, 1996 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960805Skin · crackedFOUND ON A2 LETTER CHECK, L1 DOOR UPPER AND LOWER HINGE CUTOUTS CRACKED, UPPER .5 INCH LOWER .875 INCH. REPAIRED PER MM 53-30-0.Apr 8, 1996 · N543DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 96ZZZX3507Seat Track · corrosionSEAT TRACK STA 340 TO STA 460 RBL 24 HAS LEVEL 2 CORROSION ON FLANGES AT NUMEROUS LOCATIONS. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5, FIGURE 1. TREATED AND PRIMED PER SRM 51-10-2. REPAIRED SEAT TRACK STA 380 TO STA 460, REPLACEApr 8, 1996 · N17789 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZX3497Seat Track · corrosionEXFOLIATING CORROSION ON SEAT TRACK AT STA 344 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5, FIGURE 1. TREATED AND PRIMED PER SRM 51-10-2. REPAIRED SEAT TRACK STA 380 TO STA 480, REPLACED SEAT TRACK STA 344 TO STA 380 PER DRApr 8, 1996 · N17789 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZX3496Seat Track · corrosionLEVEL 2 SURFACE CORROSION THROUGHOUT SEAT TRACK AT STA 344 TO STA 440 RBL 45.5. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5, FIGURE 1. TREATED AND PRIMED SEAT TRACK PER SRM 51-10-2. REPAIR SEAT TRACK INSTALLED STA 380 TO STA 440. Apr 8, 1996 · N17789 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZX3494U-Channel · crackedSTA 720F UPPER CHORD OF INTERCOSTAL, STRAP CRACKED WITH LEVEL 2 CORROSION. ALSO, 2 EACH, U-CHANNELS CRACKED LBL 12 AND RBL 12 AND 1 EACH L-ANGLE. FABRICATED AND INSTALLED 1 EACH L-ANGLE AND 2 EACH CHANNELS PER SRM 51-30-2 AND SRM 51-20-2.Apr 8, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960791Light · inoperativeLEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND RACK OPN CHECKS NORMAL.Apr 7, 1996 · N420DA · Boeing 727232 · Emergency LightingSDR DL72S960778Actuator · failedSLOW LEAK OF HYDRAULIC SYSTEM-A AT F310 AFTER 2 HRS AT CRUISE. POM PROCEDURES FOLLOWED FOR LOSS OF SYSTEM-A. RT SLAT NR 6 DID NOT EXTEND WITH ALTERNATE FLAPS EXTENSION SWITCH. FOUND NR 6 SLAT ACTUATOR LEAKING. REPLACED ACT SERVICED HYD SYSTEM, OPERATIOApr 6, 1996 · N421DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960879Doubler · damagedAT MID-VISIT, A TEMP REPAIR WAS FOUND TO BE INSTALLED ON THE TOP AFT CORNER OF THE L1 DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND REPAIR INSTALLED PER MM 52-11-01 FIG 804.Apr 5, 1996 · N498DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960842Frame · crackedAT MID-VISIT, THE R2 DOOR FRAME WAS FOUND CRACKED JUST BELOW UPPER HINGE CUTOUT. THE DAMAGE WAS ROUTED OUT AND DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.Apr 5, 1996 · N498DA · Boeing 727232 · Service DoorsSDR DL72S960841Skin · crackedAT MID-VISIT, THE R2 DOOR UPPER HINGE ARM CUTOUT WAS FOUND TO BE CRACKED. THE DAMAGE WAS ROUTED OUT AND A DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.Apr 5, 1996 · N498DA · Boeing 727232 · Service DoorsSDR DL72L960773Press Blkhd · crackedADDITIONAL CRACKING OF .75 WAS FOUND ON PRESSURED DECK AT FS 289 RBL4.5. REPAIRS ACCOMPLISHED PER DL ERA 258994-14 REV A.Apr 5, 1996 · N502DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72L960768Vertical Web · crackedFOUND DURING D-2 LETTER CHECK, TWO .5 INCH CRACKS IN LT LOWER TORQUE BOX VERTICAL WEB UPPER END, APPROX STA 1214. REPAIRED PER SRM 53-11-0.Apr 4, 1996 · N502DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3500Shear Tie · corrodedPREVIOUS SHEAR TIE REPAIR ON STATION FRAME AT STA 720F HAS LEVEL 2 CORROSION BETWEEN STR 29R AND STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-3.Apr 4, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZM1095Shear Tie · corrodedLEVEL 2 CORROSION ON SHEAR TIE AT STATION 720A STRINGER 28L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15.Apr 4, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZM1094Doubler · corrodedLEVEL 2 CORROSION ON SKIN DOUBLER AT STATION 724A TO 728A BL0. REMOVED EXISTING DOUBLER AND REPLACED WITH NEW PER SRM 53-30-3 FIG 1. (M)Apr 4, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960775Skin · corrodedDURING THE ACCOMPLISHMENT OF THE AFT LAV SERVICE PANEL REWORK PER EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND CORRODED. ALSO, THE LOWER CORNER OF THE OVERLAPPING SKIN AT APPROX STA 1183 STR 20L HAS TOOLING DAMAGE ON THE SKIN. ACCOMPLISHED REPAIRS PApr 3, 1996 · N520DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960760Web · crackedFOUND ON A2 LETTER CHECK, .375 INCH CRACK IN LT TORQUE BOX WEB STA 1263. REPAIRED PER MM 53-11-0.Apr 3, 1996 · N492DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960754Stringer · crackedFOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0.Apr 2, 1996 · N419DA · Boeing 727232 · Vertical StabilizerSDR DL72S960753Angle · crackedFOUND ON C-2 LETTER CHECK, NR 1 SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0.Apr 2, 1996 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960732Seal · tornAT FLIGHT LEVEL 290 LOUD RUMBLE FOLLOWED BY RAPID RISE IN CABIN ALT. BOTH OUTFLOW VALVES CLOSED AND FLT LEVEL 220, CABIN STILL CLIMBING SLOWLY. DESCENDED TO 10,000 FT TO MAINTAIN PRESS. FOUND FWD CARGO DOOR SEAL DAMAGE AND OUT OF RETAINER. REPLACED DOOR SEApr 1, 1996 · N416DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S960723Track Lights · inoperativeFIRST CLASS TRACK LIGHTS INOP. REPAIRED WIRING AT 3B AND REPLACED FUSE AT PWR SUPPLY, OPS OK.Mar 31, 1996 · N470DA · Boeing 727232 · Emergency LightingSDR DL72S960721Circuit Breaker · crackedON FINAL, ALL 3 BUS TIE BREAKERS TRIPPED, PHASE UNBALANCE, OVER EXCITED NR 2 AND NR 3, NR 1 TR UNIT C/B POPPED. FOUND APU GEN BREAKER CRACKED WITH LOOSE CONNECTIONS. REPLACED SAME. ALSO, REPLACED NR 1 ENG GEN BREAKER. RAN ENGS PARALLELED, ALL CHECKS NORMALMar 31, 1996 · N467DA · Boeing 727232 · AC Power Distribution SystemSDR DL72L960833Slide · torn webbingON PREFLIGHT, FOUND RT AFT SERVICE DOOR EMERGENCY SLIDE WEBBING AT GIRT BAR TORN. REPLACED SLIDE.Mar 31, 1996 · N505DA · Boeing 727232 · Escape SlideSDR CAL960429Tire · rupturedGYE - FLT 0777 - THE NR 2 TIRE RUPTURED ON TAKEOFF FROM UIO RESULTING IN DAMAGE TO HYDRAULIC LINES WITH FLUID LOSS FROM 'A' AND 'B' HYDRAULIC SYSTEM. THE AIRCRAFT WAS DIVERTED TO GYE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO THE LT INBD TMar 31, 1996 · N59792 · Boeing 727232 · TireSDR DL72S960702Fence · crackedUPON ROUTINE INSPECTION, FOUND CRACKS IN MOUNTING HOLES OF FENCE. REPAIRED AS PER SRM 57-54-0 PG 817, FOR NR 5 L/E SLAT.Mar 29, 1996 · N527DA · Boeing 727232 · Leading Edge DevicesSDR DL72K960708Skin · crackedFOUND DURING A-2 LETTER CHECK, .5 INCH CRACK IN LT AFT SERVICE DOOR FWD FRAME AT LOWER I/B CORNER OF UPPER HINGE/GUIDE ARM CUTOUT. REPAIRED PER SRM 52-40-2.Mar 29, 1996 · N481DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K960707Skin · crackedFOUND DURING A-2 LETTER CHECK, .3750 INCH VISIBLE CRACK IN SKIN AT L5 WINDOW CUTOUT UPPER AFT CORNER. REPAIRED PER SRM 53-30-3.Mar 29, 1996 · N481DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K960706Blkhd Clip · crackedFOUND DURING A-2 LETTER CHECK, FS 1342 BULKHEAD AND UPPER ATTACH CLIP CRACKED 1.5 INCH AT RT SIDE AND CRACKED BEYOND STOP DRILL ON LT SIDE. REPAIRED PER MM 53-11-0.Mar 29, 1996 · N481DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960752Skin · corrosionTHE FUSELAGE SKIN (2024-T3 CLAD) WAS FOUND TO HAVE CORRODED JUST O/B OF STR 28L, FROM STA 708 TO 720. THIS DAMAGE WILL REQUIRE A CUTOUT MEASURING 12 INCHES LONG BY 1.5 WIDE EXTENDING FROM STA 708 TO 720. THIS DAMAGE IS 9.5 TO THE LEFT OF AN EXISTING EXTERNALMar 27, 1996 · N520DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960727Closing Mech · brokenON ARRIVAL AT GATE, THE FWD LT ENTRY DOOR WOULD NOT OPEN. FOUND SEVERAL BROKEN PARTS JAMMING UPPER HINGE AND LOWER CAM PLATE, UPPER HINGE WAS LOOSE IN AT FUSELAGE. REPLACED BROKEN SNAP RING AND TIGHTENED CAM PLATE, OPERATION NORMAL.Mar 27, 1996 · N524DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960667Rib · wornDURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGED INTERNAL SUPPORT RIB. ACCOMPLISHED REPAIRS PER SRM 57-50-3.Mar 27, 1996 · N469DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960660Switch · failedON INSPECTION, FOUND LT SIDE OF AIRCRAFT EMERGENCY EXIT SIGN ILLUMINATION LIGHTS INOP. REPLACED NO SMOKING SW ON PILOTS O/H PNL.Mar 26, 1996 · N401DA · Boeing 727232 · Emergency LightingSDR DL72S960659Overheat Sensor · out of positionLOWER AFT BODY OVERHEAT LIGHT ILLUM. C/W PROM LIGHT WENT OUT WHEN LT PACK AND BLEED TURNED OFF. REPOS OVERHEAT SENSOR IN 48 SECTION. RAN ENGINE WITH NO OVERHEAT IND.Mar 26, 1996 · N532DA · Boeing 727232 · Overheat DetectionSDR MZZA96026Support Plate · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 6 INCH LONG CRACK WAS FOUND ON R1 GALLEY DOOR LOWER FORWARD DOOR STOP BOLT FITTING SUPPORT PLATE. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. HANGAR NON ROUTINE REPAIR ITEM CARD NRMar 25, 1996 · N15781 · Boeing 727232 · Galley DoorsSDR MZZA96024Ball Nut · nickedTNN - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, NLG MANUAL EXTENSION BALL NUT AND SCREW ASSEMBLY PATH WAS FOUND NICKED. THE DAMAGED BALL NUT AND SCREW ASSY, PN 10-60744-1, WAS REMOVED AND REPLACED PER B727 MM 32-35-0, AND OPERATIONAL CHECK FOUNDMar 25, 1996 · N15781 · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S960746Skin · crackedTHE L-1 PASSENGER DOOR WAS FOUND WITH TWO CRACKS IN THE UPPER FWD CORNER. THESE CRACKS RESULTED IN TWO CUT OUTS, 2 INCH BY 1.25 INCH AND 2.5 INCH BY 1.5 INCH, EIGHT INCHES APART. ONE DOUBLER REPAIR WILL BE USED FOR BOTH CRACKS. THE DOOR SKIN IS MADE FROM 0.Mar 25, 1996 · N520DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960657Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE TAIL CRAWLWAY ONE AND ONE HALF BAYS DOWN. REPAIRED PER M/M 55-30-0.Mar 25, 1996 · N534DA · Boeing 727232 · Vertical StabilizerSDR DL72S960656Stringer · crackedFOUND DURING B-2 LETTER CHECK, STRINGER CRACKED IN TAIL CRAWLWAY BETWEEN 2ND AND 3RD BAY RT SIDE. REPAIRED PER M/M 55-30-0.Mar 25, 1996 · N534DA · Boeing 727232 · Vertical Stabilizer
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