Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR 01FDEA00207Gasper Fan · shortedAIR CREW SMELL SULFUR ODOR IN COCKPIT, DONNED 02 MASK AND SMOKE GOGGLES. FLT ENG THOUGHT ODOR WAS COMING FROM GASPER FAN. INSP AC AND CARGO WITH FIRE DEPT, NOTHING FOUND. AFT OFF LOAD PRESS AC HAD ELECTRICAL ODOR COMING OUT GASPER. GASPER FAN CIRCUIT BREAKMar 17, 2001 · N276FE · Boeing 727233 · Air Distribution FanSDR 01FDEA00191Floorbeam · corrodedCORROSION (C53-224-04) AT FASTENER HOLES IN FLOORBEAM BS 1130, RBL 36-42 AND BL 0 - LBL 25, WL 201. *S/D* REPAIRED PER FEDEX EA 7-5310-56290.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00197Frame · crackedFRAME IS CRACKED AT CEILING SUPPORT MOUNTING POINT BS 1030, RBL 33.5, WL 294. * S/D * FAB & R&R PER IAW FEDEX SRM 53-10-4 FIG 2 AND FEDEX EA 7-5310-56296.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00195Frame · crackedFRAME IS CRACKED AT CEILING SUPPORT BS 1030, LBL 33.5, WL 294. * S/D * CUT OUT CRACK AND REPAIRED PER IAW FEDEX EA 7-5310-56295.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00190Shear Tie · corrodedCORROSION (SPEC C53-111-01,3) ON FRAME SHEAR TIE BS AT BS 950D BETWEEN STR 29L AND STR 28L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1 FIG 1, 53-10-4 FIG 15.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, StructureSDR 01FDEA00192Floorbeam · corrodedCORROSION ON 720A FLOORBEAM UPPER SURFACE OF UPPER FLANGE AT RBL 5 & 11. *S/D* REMOVED AND REPLACED PER SRM 51-10-1 FIG 4, 53-10-8 FIG 3 AND EA 7-5310-56300.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00194Support · crackedCEILING SUPPORT IS CRACKED FRAME HAS A DOUBLE HOLE AT BS 1130, WL 294. *S/D* REPAIRED PER FEDEX SRM 51-20-1, 51-40-3 FIG 1 AND EA 7-5310-56294.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 01FDEA00193Frame · crackedFRAME IS CRACKED AT CEILING SUPPORT MOUNTING POINT BS 990, WL 294, RBL 33.5. *S/D* REMOVED AND REPLACED PER FEDEX EA 7-5310-56291 AND SRM 53-10-4, FIG 2.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00196Frame · crackedFRAME IS CRACKED AT CEILING SUPPORT CHANNEL ATTACH POINT BS 1070, RBL 33.5, WL 294. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-4 FIG 2 & EA 7-5310-56293.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00200Frame · dentedFRAME 500 DENTED RBL 67, WL 212. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00189Floorbeam · corrodedFWD LOWER FLANGE OF FLOORBEAM BS 1010 CORRODED BEYOND LIMITS. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-10-8.Mar 14, 2001 · N218FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00187Fire Detector · contaminatedDURING FLT (APU OFF) RED FIRE LIGHT IN APU FIRE HANDLE CAME ON. UPON ENTRY INTO E&E COMP. FOUND AREA EXTREMELY WET. REMOVED APU FIRE DET OPS PWR UNIT, CLEANED AND DRIED AND REINSTALLED. TEST SYS ALL CK GOOD. NO LIGHTS CAME ON REF B727-200 WDM.Mar 14, 2001 · N268FE · Boeing 727233 · Fire DetectionSDR 01FDEA00186Warning Light · illuminatedNR 2 OIL PRESSURE/FILTER BYPASS LIGHT STAY ON LONGER THAN NORM. INFLT ENGINE SHUTDOWN ACCOMPLISHED.Mar 11, 2001 · N220FE · Boeing 727233 · Engine Oil PressureSDR 01FDEA00183Line · leakingNR 2 LOW OIL PRESSURE BYPASS LIGHT CAME ON. FOLLOWED BY LOSS OF OIL QUANTITY SHUT DOWN NR 2 IN FLT PER CKLIST. *S/D* FOUND MAIN SCAVENGE OIL LINE LEAKING AT COUPLING NUT PACKINGS DETERIORATING. REMOVED AND REPLACED PACKINGS PER MM 79-20-002-2, MAIN OIL FILMar 10, 2001 · N220FE · Boeing 727233 · Turbine Engine Oil SystemSDR 01FDEA00182Relief Valve · stuckNR 2 OIL BYPASS LIGHT ILLUMINATED. SECURE ENG PER RED TAB PROC. REMOVED AND REPLACED MAIN OIL SCREEN, FOUND FILTER PRESSURE RELIEF VALVE STUCK. REMOVED AND REPLACED VALVE PER PW JT8D72-009G518C-518D. INSP OIL SCREEN PER MM 79-00-000-2. NONE NOTED. LEAK AMar 9, 2001 · N220FE · Boeing 727233 · Turbine Engine Oil SystemSDR 01FDEA00171Door · damagedFWD ENTRY DOOR LIGHT ILLUM AT 18,000. LOUD BANG AT 3000 ON DEP I FRONT AREA OF A/C. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR PER 727-200 MM 52-11-00-4. PERF RIG ADJUSTMENT TEST PER B727-200 MM 52-11-001-5. INSTALL DOOR LINER PER MM 52-11-001-5. REINSTALMar 1, 2001 · N222FE · Boeing 727233 · Passenger/Crew DoorsSDR 01FDEA00170Motor · leakingDURING CRUISE SYS HYD QUANTITY READ ZERO, PRESS ZERO TOO. RED TAB PROC PUMPS TURN OFF 20 MIN. FOUND FLAP PWR UNIT HYD MOTOR LEAKING FROM TOP OF MOUNTING FLANGE AT FLAP PWR UNIT GEARBOX. REMOVED AND REPLACED FLAP HYD MOTOR IN REF TO 727-200 MM 27-51-062-4. Mar 1, 2001 · N280FE · Boeing 727233 · Trailing Edge Flap ActuatorSDR 01FDEA00169Door · out of adjAT FL 250 340 KTS/84 GOT INTERMITTENT RED GEAR DOOR LIGHTS AND LOUD THUMP FROM NOSE GEAR. FOLLOW RED TAB AND RAISE GEAR HANDLE. LIGHT WENT OUT. ADJUSTED AND RETRACTED NOSE GEAR WHEEL WELL DOORS AS PER MM 32-22-001.Mar 1, 2001 · N282FE · Boeing 727233 · Landing Gear Door Retract SectionSDR 01FDEA00158Rib · crackedVERTICAL STAB, RT RIB CHORD IS CRACKED IN 3 PLACES AT FIN STA 133.8, STR 7 - 10R. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 55-30-5.Feb 22, 2001 · N275FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA00147Switch · failedON APPROACH WHEN SEL FLAPS 5 AMBER LIGHT ON FRONT PNL REMAIN ILLUM. NR 3 LEAD EDGE FLAP ON POS IND SHOW NOT DEPLOYED. REMOVED AND REPLACED NR 3 LEAD EDGE FLAP SWITCH PER MM 27-82-011-4, GOOD PER MM 27-81-000-5.Feb 20, 2001 · N281FE · Boeing 727233 · Leading Edge Slat Position Indicating SystemSDR 01FDEA00153Stringer · crackedCRACK IN STRINGER, BS 720B+4 INCH, STR 15R. *S/D* REMOVED, REPLACED AND FAB PER FEDEX 727 SRM 51-10-2 & 53-10-3 FIG 5.Feb 19, 2001 · N275FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00152Frame · misdrilledTWO DRILL STARTS IN I/B FLANGE OF FRAME BS 1010 ABOVE STR 16L. *S/D* REMOVED, REPLACED AND FAB OUT OF LIMITS DRILL STARTS PER FEDEX SRM 53-10-1. REPAIR PARTS AND STR CLIP PER FEDEX SRM 51-40-3 & 51-30-2.Feb 19, 2001 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00157Frame · gougedGOUGE IN O/B FLANGE OF FRAME BS 1148 ADJACENT TO STR 8L. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3 FIG 1.Feb 16, 2001 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00131Stringer · crackedCRACKED STR BS 720B+4, STR 15L. *S/D* REMOVED, REPLACED, FAB, ALODINED, AND PRIMED PER FEDEX SRM 51-10-2 AND 53-10-3.Feb 16, 2001 · N275FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00134Window · crackedCAPT L1 FRONT WINDOW IS CRACKED. WINDOW HEAT CAUSES ARCHING AND FURTHER CRACKING. OUTER PANE APPEARS TO BE MOST AFFECTED. WINDOW HEAT IS INOP. *S/D* REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER REF MM 30-41-013-5, 56-11-011-4. SEALED AND INSTALL WIFeb 16, 2001 · N281FE · Boeing 727233 · Flight Compartment WindowsSDR 01FDEA00130Stringer · corrodedCORROSION (C53-111-01,2) ON I/B SIDE OF STR 27 RT, BS 680. *S/D* REMOVED AND REPLACED STR CAP PER FEDEX SRM 51-30-2. CAP FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1.Feb 15, 2001 · N275FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00129Floorbeam · corrodedCORROSION (C53-224-01) ON BS 312 FLOORBEAM UPPER CHORD LBL 4, WL 208. *S/D* OUT OF LIMITS PER IAW FEDEX SRM 53-10-1. FAB ANGLE AND FILLER PER IAW FEDEX SRM DWG 27-53-017. INSTALLED ALL FASTENERS PER IAW FEDEX SRM 51-30-5, 51-30-2 AND MM 51-20-151.Feb 15, 2001 · N275FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00128Floorbeam · corrodedCORROSION (C53-224-01,1) ON BS 328 FLOORBEAM UPPER CHORD, LBL 4, WL 208. *S/D* OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED PER FEDEX DWG SR 27-53-017.Feb 15, 2001 · N275FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00127Frame · crackedWHILE WORKING NR-329 FOUND CRACK IN FRAME AT BS 540, RBL 3, WL 156. *S/D* REMOVED, REPLACED, FAB, ALODINED AND PRIMED PER FEDEX SRM 51-40-3 FIG 1 AND 51-20-1 FIG 3 & 7, 51-30-2, 51-10-2.Feb 15, 2001 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00112Frame · dentedFRAME DENTED AT BS 700 BETWEEN STR 22 LT AND 23 LT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3 AND EA 7-5310-56528.Feb 12, 2001 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00083Transformer · failedOUTPUT DIFFERENCE BETWEEN TR 1 & 2 VS ESSENTIAL TR. REMOVED AND REPLACED NR 1 T/R PER IAW MM 24-53-000 & SYS OPS CK NORMAL.Feb 8, 2001 · N267FE · Boeing 727233 · DC Generating SystemSDR 01FDEA00080Keelbeam · corrodedCORROSION ON STRAP ON LT KEEL BEAM BS 950E - 950E+16 IN AFT CARGO BAY. *S/D* REMOVED AND REPLACED OUT OF LIMIT CORROSION PER IAW FEDEX SRM 53-10-1, EA 7-5310-56529.Feb 6, 2001 · N275FE · Boeing 727233 · Fuselage Main, KeelSDR 01FDEA00073Cylinder · failedNOSE GEAR FAILED TO EXTEND NORMALLY ON FIRST ATTEMPT. OK WHEN CYCLED UP TO DOWN- REPEAT WRITE-UP. *S/D* REMOVED AND REPLACED NOSE GEAR HYDRAULIC TRANSFER CYLINDER AS PER MM 32-35-011-4. JACK AND LWR NOSE PER MM 07-11-000-2. ACCOMP EXT AND RETRACT PER 32-3Feb 3, 2001 · N222FE · Boeing 727233 · Nose/Tail Landing GearSDR 01FDEA00070Accessory Unit · malfunctionedNOSE GEAR UNSAFE. RECYCLE TWICE TO GET ALL DOWN. *S/D* REMOVED AND REPLACED PER MM 32-09-122-5, 32-33-000-5. JACKED AND LWR A/C PER MM 07-11-000-2.Feb 1, 2001 · N222FE · Boeing 727233 · Nose/Tail Landing GearSDR 01FDEA00069Wire · brokenRADAR STILL INOP. FOUND BROKEN WIRE BETWEEN F11 AT RT TO R68 U ON VERTICAL GYRO CONNECTOR D669. REMOVED AND REPLACED WIRE ACCORDANCE WITH BOEING WIRE STANDARD CHAPTER 20. OPS CK OK.Jan 29, 2001 · N218FE · Boeing 727233 · Inertial Guidance SystemSDR 01FDEA00030Circuit Breaker · failedTRAILING EDGE INBOARD FLAPS FAILED TO RETRACT DURING GO-AROUND. RED TABS ACCOMPLISHED. RESET INBOARD FLAP IND CIRCUIT BREAKER. CYCLED FLAPS 4 TIMES WITH NO DISCREPANCY. TEST PER 727-200 MM 27-51-000-1. OK TO CONTINUE.Jan 20, 2001 · N258FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 01FDEA00022Wire · failedDURING FLAP RETRACT (FROM 5 DEG TO 2 DEG) DID NOT GET A GREEN LEAD EDGE FLAP LIGHT, 2ND OFF. POSITION IND SHOW NR 7 INTRANSIT. *S/D* REPAIRED WIRES AS PER CHAP 20 WIRING DIAGRAM PER 27-81-01, 27-82-00-1.Jan 16, 2001 · N283FE · Boeing 727233 · Leading Edge Slat Control SystemSDR 01FDEA00018Skin · crackedCRACK IN SKIN, VERTICAL STAB, LEFT SIDE, STR 10, BOTTOM OF STAB. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 55-30-3 AND FEDEX EA 7-5510-56226.Jan 11, 2001 · N273FE · Boeing 727233 · Elevator, Plate/SkinSDR 01FDEA00014Frame · dentedFRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3.Jan 9, 2001 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00011Doubler · gougedMAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 51-30-2.Jan 8, 2001 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 01FDEA00003Stringer · damagedNR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-10-3.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00004Stringer · crackedCRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00005Stringer · crackedNR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00006Stringer · crackedNR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMINGJan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00002Keelbeam · corrodedCORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMINGJan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, KeelSDR 00FDEA00866Floorbeam · damagedNR 911 DOUBLE FASTENER HOLES IN FLOORBEAM AT BS 380, LBL 13, WL 208. ** S/D ** R&R PER FEDEX SRM 53-10-8, FIG 8.Dec 8, 2000 · N274FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 00FDEA00861Actuator · failed00-343 ON CLIMBOUT RETRACTED FLAPS FROM 5 DEG TO 2 DEG ON SCHELDULE NR 1 LEAD EDGE FLAP REMAIN IN TRANSIT. R&R PER 727-200 MM 27-81-22. OPS CK OK. AC OK FOR SERVICE.Dec 8, 2000 · N279FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 00FDEA00857Frame · dentedNR 339- DENTED FRAME BS 660, 2 INCHES ABOVE STRINGER 26R. ** S/D ** R&R PER FEDEX SRM 51-40-3.Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, FrameSDR 00FDEA00856Frame · dentedNR 333, DENTED FRAME BS 600, 2 INCHES ABOVE STR 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, FrameSDR 00FDEA00855Frame · dentedNR 332 DENTED FRAME BS 580, 2 INCHES ABOVE STRINGER 26L. ** S/D ** R&R PER FEDEX SRM 51-40-3, 51-30-2.Dec 5, 2000 · N274FE · Boeing 727233 · Fuselage Main, Frame
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