Boeing 727-232

Service difficulty reports · 6,539

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  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 05FDEA03036Keelbeam · damagedLT AC BAY, BS 740 TO 800 KEELBEAM LWR WEB, 4 LIGHTNING HOLES HAVE OUT OF ROUND HOLES AND ARE MISSING STRESS BEVELS. REPAIRED LOWER KEELBEAM WEB PER SRM 51-40-2.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, KeelSDR 05FDEA03035Frame · dentedAFT CARGO BAY, FRAME IS DENTED AT BS 950C BETWEEN STR 25R AND STR 26R. REPAIRED FRAME AT BS 950C, STR 25R-26R PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03034Frame · dentedFRAME DENTED AT BS 970, ABOVE STR 26L. REPAIRED PER SRM 53-10-1.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03039Shear Tie · corrodedAFT CARGO BAY, SHEAR TIE IS CORRODED AT BS 950B, RBL9, WL138. REPAIRED AFT CARGO BAY, SHEAR TIE AT BS 950B, RBL 9 WL 138 IAW SRM 51-10-2, 53-10-4.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Internal Mounting StructureSDR 05FDEA03032Frame · dentedFRAME DENTED IN 2 PLACES AT BS 1050, STR 23L AND 25L. REPAIRED FRAME AT BS 1050 STR 23L & 25L PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03031Frame · dentedFRAME DENTED AT BS 1050, BELOW STR 26R. REPAIRED FRAME AT B.S. 1050 BELOW STR 26R PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03030Frame · dentedFRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR 26L PER SRM 51-40-3Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03029Frame · dentedFRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR. 26L PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03028Frame · dentedAFT CARGO BAY, BS 950B FRAME BETWEEN STR 25R AND STR 26R HAS A DENT. REPAIRED FRAME AT BS 950B STR 26R PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03027Frame · dentedFRAME DENTED AT BS 1070, JUST BELOW STR 25R. REPAIRED FRAME AT B.S. 1070, STR 25R PER SRM 51-40-3.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA02994Keelbeam · crackedCRACK IN KEEL BEAM UPPER FLANGE AT FASTENER LOCATION ON STA 873 LBL 6. REPAIRED KEEL BEAM PER EA 7-5310-91372.Sep 19, 2005 · N499FE · Boeing 727232 · Fuselage Main, KeelSDR C7WA200400074Engine · damagedNR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACED, S/N OF INSTALLED ENGINE IS 654920. (M)Jan 11, 2005 · N511PE · Boeing 727232 · Engine (Turbine/Turboprop)SDR C7WA200400032Skin · dentedFOUND LEFT FUSELAGE SKIN DENTED FS 380 STRINGER 26 RT. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Plate/SkinSDR C7WA200400019Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Plate/SkinSDR C7WA200400020Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Plate/SkinSDR C7WA200400017Hinge · crackedFOUND MAIN CARGO DOOR UPPER AFT HINGE SECITON CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AE MM CHAPTER 52 PAGE 15. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Cargo/Baggage DoorsSDR C7WA200400018Stringer · corrodedFOUND STRINGER 28 RIGHT STATION 1050 EVIDENCE OF CORROSION. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 53-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400021Frame · corrodedFOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED STAITON 1148 STRINGER 25 RIGHT. INSTALLED INTERNAL FRAME REPAIR IAW 727 SRM 51-20-1 AND 51-30-2. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, FrameSDR C7WA200400022Stringer · corrodedFOUND AFT CARGO COMPARTMENT STRINGER 27 RIGHT STATION 950E HAS LIGHT CORROSION. INSTALLED STRINGER REPAIR IAW 727 SRM 51-40-4 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400023Stringer · corrodedFOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 720E CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400024Stringer · corrodedFOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 700 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400025Stringer · corrodedFOUND E/E COMPARTMENT STRINGER 28 LEFT STATION 720C CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-4 FIGURE 13. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400026Stringer · corrodedFOUND E/E COMPARTMENT STRINGER 27 LEFT STATION 450 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400027Stringer · corrodedFOUND E/E COMPARTMENT STRINGER 20 RIGHT STATION 460 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400028Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Center BoxSDR C7WA200400029Stringer · corrodedFOUND E/E COMPARTMENT STRINGER 28 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR C7WA200400030Frame · corrodedFOUND FUSELAGE FRAME UPPER CHORD CORRODED BS 950E AT STRINGER 27 RT. INSTALLED FRAME REPAIR IAW 727 SRM 53-10-4 FIGURE 2. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, FrameSDR C7WA200400031Stringer · corrodedE/E COMPARTMENT STRINGER 26 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S030300Control Valve · leakingSHORTLY AFTER T/O SYS-A HYD LOW PRESS LIGHT ILLUM. FOUND LANDING GEAR CONTROL VALVE LEAKING AT FITTING. REPLACED FITTING AND O-RING.Mar 29, 2003 · N533DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S030222Bulkhead · crackedINSPECTION OF THE FS 1183 BULKHEAD AFT ENTRY DOOR FRAME AT RBL 17.8 PER AD 99-18-05 REVEALED A CRACKED FASTENER HOLE AT WL 273. THE CRACKED HOLE WAS OVERSIZED TO REMOVE ALL CRACK INDICATIONS AND AN ADDITIONAL OVERSIZING INSURANCE CUT WAS MADE. AN OVERSIZE FMar 5, 2003 · N523DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S030211Mount · crackedINSPECTION OF THE NR 1 ENGINE FWD MOUNT SUPPORT FITTING ATTACH HOLES PER AD 97-05-08 REVEALED A CRACK INDICATION IN THE HOLE G-LOCATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION AND AN INSURANCE CUT APPLIED. AN OVERSIZE FASTENER WAS THEN INSTALLMar 5, 2003 · N523DA · Boeing 727232 · Engine Mount SectionSDR DL72S030185Light · malfunctionedCOCKPIT EMERGENCY LIGHT FAILS TO COME ON DURING EMERGENCY POWER CHECK. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK GOOD.Feb 24, 2003 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S030143Skin · damagedUPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD.Feb 11, 2003 · N410DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S030141Battery Pack · dischargedRT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.Feb 10, 2003 · N544DA · Boeing 727232 · Emergency LightingSDR DL72S030110Warning Light · illuminatedNR 1 ENG OIL FILTER BYPASS LIGHT PER POM SHUT ENGINE DOWN. CLEANED CONNECTOR FOR MASTER DIM AND TEST MODULE AND PERFORMED ENGINE WINDMILL INSP PER M/M.Jan 29, 2003 · N523DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S021479Engine · malfunctionedNR 3 ENGINE EGT LIMITED IN CLIMB POWER, EGT 590-595 AT 20 TAT CLIMB THRUST (ON T/O USING ALT 40 TAT CLIMB NR 3 EGT 610). AT 20 TAT CLIMB EPR = 1.88 HAD TO PULL NR 3 THROTTLE BACK TO 1.76 EPR TO KEEP EGT AT / BELOW 580. REPLACED NR 3 ENGINE PER 4T203AD.Dec 29, 2002 · N544DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S021457Actuator · leakingON APPROACH AFTER FLAPS 15 COMPLETE LOSS OF A SYSTEM QUANTITY AND PRESSURE. EMERGENCY PROCEDURES CHECKLIST FOLLOWED WITH MANUAL LANDING GEAR EXTENSION. A SYSTEM HYDRAULIC PUMPS WERE DEACTIVATED WITHIN 2 MINUTES CA_FOUND NBR 4 KREUGDec 21, 2002 · N533DA · Boeing 727232 · Hydraulic System, MainSDR DL72S021449Skin · crackedFUSELAGE / SKIN / FS 681-740 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT BETWEEN FS 681 & 740 GAVE CRACK INDICATIONS. INTERNAL MFEC INSPECTIONS CONFIRMEDec 13, 2002 · N521DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S021436Skin · crackedFUSELAGE / SKIN / FS 481-681 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R LAP JOINT REVEALED CRACK INDICATIONS BETWEEN FS 481 & 681. INTERNAL MFEC INSPECTION CONFIRMED A TOTAL OFDec 10, 2002 · N521DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S021391Actuator · failedAFTER T/O AMBER LED LIGHT REMAINED ILLUMINATED AT FLAPS 2. POSITION TEST SHOWED NR 4 L/E DEVICE NOT RETRACTED. REPLACED NR 4 SLAT ACTUATOR.Nov 30, 2002 · N518DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S021389Light · damagedEMERGENCY FLOOR LIGHT DAMAGED AT SEAT ROW 22 DEF. REPLACED LIGHT ASSY, OPERATIONAL CHECKS GOOD.Nov 29, 2002 · N526DA · Boeing 727232 · Emergency LightingSDR DL72S021378Handle · brokenL2 DOOR UPPER CRANK BROKE WHILE CLOSING DOOR, ROD ALSO DAMAGED SHEET METAL ON DOOR. REPLACED DOOR.Nov 25, 2002 · N533DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S021376Shim · out of positionREPAIR FOR MIGRATED SHIM, INSPECTION OF LT WING INBD FLAP INBD FLAP TRACK REVEALED A MIGRATED LAMINATED SHIM. THE CONDITION IS TYPICAL OF THAT DOCUMENTED PER BAC S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS MIGRATED BEYOND THE ALLOWABLE LIMITS OF THE S/B ANNov 23, 2002 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S021302Torque Box · crackedFUSELAGE / VENTRAL STAIRWAY / RH TORQUE BOX STRUCTURE / FS 1263 : CRACK REPAIR THE VENTRAL STAIRWAY ACTUATOR ON THE RH TORQUE BOX AT FS 1263 WAS FOUND PULLED THROUGH THE UPPER WEB OF THE TORQUE BOX, RESULTING IN CRNov 5, 2002 · N523DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S021264Transceiver · malfunctionedATB, WX RADAR C/B POPPED TWICE. REPLACED WX RADAR R/T TEST PATTERN NORMAL - OPERATED IN WX MOD OBTAINED TARGETS, ALL OPS NORMAL.Oct 30, 2002 · N516DA · Boeing 727232 · Weather Radar SystemSDR DL72S021252Light · brokenSEAT 20DEF EMERGENCY LIGHT BROKEN, (FWD,RED) CA RPLD LIGHT.Oct 27, 2002 · N518DA · Boeing 727232 · Emergency LightingSDR DL72S021251Light · inoperativeEMERGENCY EXIT LIGHT AT ROW 16 INOP AND LENS MISSING. RELAMPED AND REPLACED LENS-OPS NORMAL.Oct 27, 2002 · N519DA · Boeing 727232 · Emergency LightingSDR C7WA200200034Oil Cooler · faultyAFTER TAEKOFF, NR 1 ENGINE OIL TEMPERATURE WENT INTO YELLOW ARC (APPROX 126) AND STAYED THERE. HIGH OIL TEMP ABNORMAL CHECKLIST ACCOMPLISHED. AFTER 15 MINUTES OF OIL TEMPERATURE IN YELLOW BAND PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED AS PER CHECKLIST. HIGOct 22, 2002 · N511PE · Boeing 727232 · Engine Fuel/Oil CoolerSDR C7WA200200033Ground Wire · looseCLIMBING THROUGH FL195 FOR FL280 CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 10.5. EMERGENCY DESCENT INITIATED AS PRESSURE COULD NOT BE MAINTAINED IN STANDBY, ONLY IN MANUAL DC. CABIN REACHED 12 BEFORE PRESSURE COULD BE CONTROLLED MARGINALLY Oct 22, 2002 · N511PE · Boeing 727232 · Air Conditioning System WiringSDR C7WA200200032Position Switch · failedFLT 41 - DURING TAKEOFF AT 80 KNOTS, THE FORWARD LEADING EDGE INTRANSIT LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 8 LEADING EDGE SLAT POSITION SWITCH IAW MM 27-81-11. OPS CHECK GOOD. (M)Oct 19, 2002 · N511PE · Boeing 727232 · Leading Edge Slat Position Indicating System
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