Boeing 727-2S2F

Service difficulty reports · 842

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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 = '7272S2F'
  ORDER BY difficulty_date DESC"

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SDR 98FDEA00353Retract Mech · out of adjustL/MAIN GEAR LIGHT ILLUM'D ON BOTH FWD PANEL AND S/O PANEL DURING EACH GEAR HANDLE PLACED IN THE UP POS ON FOR 30 SECS. FOUND GEAR RLS MECHANISM OUT OF ADJ, ADJUSTED AND TESTED PER 32-34-21. NO GEAR SWING REQ BY MM.May 17, 1998 · N207FE · Boeing 7272S2F · Landing Gear Retraction/Extension SystemSDR 98FDEA00352Connector · dirtyLWR AFT BODY OVERHEAT ILLUM'D DURING CLIMB W/LEFT PACK SUPPLIED BY NR 2 ENG, SWP PACK TO NR 1 ENG AND LIGHT STAYED ON, CLOSED NR 1 BAV AND LWR AFT BODY LIGHT WENT OUT. INSPECTED LEFT AND RIGHT OVHT DETECTOR LOOPS, NO DEFECT, CLEANED PLUG SENSORS AND L/LOOP RAMay 16, 1998 · N203FE · Boeing 7272S2F · Overheat DetectionSDR 98FDEA00331Shutoff Valve · malfunctionAFTER TAKEOFF, DUCT OVERHEAT LIGHT ILLUM FOLLOW BY ZONE 4 MAIN CARGO SMOKE WARN LIGHT AND BELL. SMELL SMOKE IN COCKPIT LIGHTS AND BELL EXTINGUISH THEN CAME ON ANOTHER. THE NR 3 ENG DUCT TEMP WAS 220 DEG NR 1 ENG WAS APPROX 180. OPER CKD WING ANTI-ICE SYS, ALMay 6, 1998 · N212FE · Boeing 7272S2F · Airfoil Anti/De-ice SystemSDR 98FDEA00287Starter · failedWHEN TURNING ON NR 3 BLEED ON CLIMB-OUT, NR 3 FIRE LIGHT AND FIRE WARNING CAME ON. TURNING OFF THE BLEED, THE FIRE LIGHT AND HORN WENT OFF. FOUND STARTER CONTROL VALVE STUCK 25 PERCENT OPEN AND STARTER IN TOO MANY PIECES. REPLACED STARTER AND CONTROL VAApr 23, 1998 · N212FE · Boeing 7272S2F · Engine StarterSDR 98FDEA00081Indicator · inoperativeINBOARD INDICATED ASYMMETRIC AT 1 DEGREE UPON RETRACT. REPLACED INBOARD FLAP POSITION INDICATOR. REMOVED AND CLEANED BYPASS VALVE CANNON PLUG THEN REINSTALLED. LUBED JACK SCREWS, VISUALLY CHECKED JACK SCREWS FLAP TRACKS AND ROLLERS OPERATED WITH HYDRAULICS Feb 3, 1998 · N215FE · Boeing 7272S2F · Trailing Flap Position Indicating SystemSDR 98FDEA00079Doubler · damagedUPPER LOBE BS 540, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00078Doubler · damagedUPPER LOBE, BS 520, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00077Doubler · damagedUPPER LOBE, BS 500, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00076Doubler · damagedUPPER LOBE, BS 600, RBL 66, FRAME DAMAGED APPROXIMATELY 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00075Doubler · damagedFWD ENTRY DOOR CUTOUT UPPER HINGE AREA HAS BEEN CUTOUT PAST FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HINGE CUTOUT. INSTALL UPPER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00074Doubler · damagedFWD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT HAS BEEN CUTOUT BEYOND FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HINGE CUTOUT. INSTALLED LOWER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333.Feb 2, 1998 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 98FDEA00047Thermo Valve · malfunctionedON CLIMBOUT, GOT ANTI-ICE DUCT OVERHEAT LIGHT NR 1 AND NR 3 ENGINES WERE BOTH OFF THE TEMPERATURE SCALE. FOLLOWED RED TABS, LIGHT WENT OUT AFTER 1 TO 2 MINUTES ON LANDING. LIGHT CAME ON AGAIN WITH WINGS OFF AND ENGINE ANTI-ICE OPEN. REMOVED AND REPLACED NR Jan 23, 1998 · N212FE · Boeing 7272S2F · Air Intake Anti/De-Ice SystemSDR 98FDEA00022Floorbeam · gougedFLOORBEAM UPPER CHORD FWD SIDE LWR SURFACE GOUGED BS 880 RBL 55 WL 208. BLENDED OUT GOUGE, FABRICATED REPAIR STRAP FROM .071 7075-T6. INSTALLED STRAP PER AMERICAN AIRLINES REPAIR 53-10-07-2 FIG 1 3/20/96.Jan 9, 1998 · N212FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 98FDEA00005Duct · failedENGINE NR 3 FIRE WARNING LIGHT ON CLIMBOUT 100 AGL. FOLLOWED RED TAB PROCEDURES. WARNING LIGHT WENT OUT WHEN THRUST LEVER RETARDED. FIRE WARNING SYSTEM CHECKED OK. RETURNED TO STL. *S/D* REMOVED TUBE PART NUMBER 777790, DUCT PART NUMBER 1211318-002, FLANJan 6, 1998 · N216FE · Boeing 7272S2F · Air Intake Anti/De-Ice SystemSDR 98FDEA00001Control Unit · malfunctioned98-0001 FIRE WARNING LIGHTS AND BELL ON FOR 1 SECOND AT CRUISE, (ON FORWARD INSTRUMENT PANEL) NO FURTHER INDICATIONS. ENGINE INSTRUMENTS ALL NORMAL. FOUND PIN PUSHED BACK IN FIRE DETECTOR CONTROL UNIT REMOVED AND REPLACED UNIT OPERATIONAL CHECKED GOOD.Jan 1, 1998 · N210FE · Boeing 7272S2F · Detection SystemSDR 97FDEA00832Smoke Detector · failedAPPROX 4 TO 5 MIN AFTER T/O, NR 4 MAIN CARGO SMOKE ALARM SOUNDED AND ILLUMINATED. LIGHT REMAINED ILLUMINATED FOR A FEW MIN AND THEN WENT OUT. NO SECONDARY IND OF FIRE OR SMOKE. REMOVED AND REPLACED NR 4 SMOKE DETECTOR, OPERATIONAL CHECKS NORMAL PER B727 MAINov 14, 1997 · N208FE · Boeing 7272S2F · Smoke DetectionSDR 97FDEA00818Wire · looseENGINE NR 2 FIRE WARNING LIGHT AND BELL ILLUMINATED AND SOUNDED PERIODICALLY AT BEGINNING OF DESCENT - IDLE POWER SETTING. LIGHT AND BELL COULD BE CANCELED. ENGINE OPERATION WAS NORMAL. INSPECTED ALL DUCTING OK. SECURED LOOSE WIRING AND BRACKETS AT VARIOUSNov 11, 1997 · N210FE · Boeing 7272S2F · Fire DetectionSDR 97FDEA00793Connector · dirtyAFTER LOWERING LANDING GEAR, LEFT MAIN GEAR DOOR LIGHT ILLUMINATED ON SECOND OFFICER'S PANEL. RECYCLED GEAR AND LIGHT EXTINGUISHED. CHECKED DOOR SWITCH FOR SECURITY, NORMAL. CYCLED DOOR, INDICATION NORMAL. FOR PRECAUTION DEFERRED LEFT GEAR DOOR WARNING SYSOct 30, 1997 · N208FE · Boeing 7272S2F · Landing Gear Position and WarningSDR 97FDEA00780Connector · dirtyDURING TAKEOFF WITH LANDING GEAR IN UP AND OFF LEFT MAIN GEAR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL WITH CORRESPONDING RED DOORS LIGHT ILLUMINATED. FOLLOWING RED TABS, CYCLED LANDING GEAR WHICH CORRECTED PROBLEM. CHECKED AND CLEANED LEFT GEAR UP SWITCHOct 28, 1997 · N208FE · Boeing 7272S2F · Landing Gear Position and WarningSDR 97FDEA00775Fire Warn Bell · malfunctioned97-0211 - AFTER TAKEOFF, 2000FT FIRE WARNING BELL SOUNDED AND GLARE SHIELD LIGHT CAME ON FOR 1-2 SECONDS. NO OTHER INDICATION ALL ENGINE INSTRUMENTS NORMAL. OPERATIONAL CHECK ALL SYSTEM CHECK NORMAL COULD NOT DUPLICATE. OK FOR SERVICE.Oct 24, 1997 · N201FE · Boeing 7272S2F · Fire DetectionSDR 97FDEA00685Clamp · looseENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN CRUISE. CLOSED ENGINE NR 1, ANTI-ICE VALVE LIGHT WENT OUT. COMPLIED ENGINE STRUT OVERHEAT PROCEDURES IN CHECKLIST. TIGHTENED HIGH STAGE MODULATING VALVE CLAMP, OPERATIONAL CHECK. ON RUN GOOD, COWLING SECURED.Sep 25, 1997 · N215FE · Boeing 7272S2F · Engine Anti-Icing SystemSDR 97FDEA00662Bleed Valve · failedCLIMBING THROUGH FLIGHT LEVEL 200 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. AS PER RED TABS WE ISOLATED PROBLEM TO THE NR 1 BLEED VALVE AND OPERATED THE RIGHT PACK ONLY. OVERHEAT LIGHT EXTINGUISHED WITH THE REDUCTION OF THE NR 1 THROTTLE TO IDLE. ALSO SYSTSep 17, 1997 · N203FE · Boeing 7272S2F · Compressor Bleed ValveSDR 97FDEA00659Accessory Unit · malfunctionedON GEAR EXTENSION GEAR DOOR LIGHTS CYCLED CORRECTLY. NOSE AND LEFT GEAR LIGHTS INDICATED NORMAL EXTENSION. THE RIGHT RED GEAR LIGHT STAYED LIT. THE RIGHT GREEN GEAR LIGHT DID NOT COME ON, LIGHTS TESTED GOOD. RAN CHECKLIST, CYCLED GEAR, RED LIGHT STAYED ON,Sep 16, 1997 · N201FE · Boeing 7272S2F · Landing Gear Position and WarningSDR 97FDEA00594Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON DURING FLIGHT. LIGHT CAME ON WHILE CLIMBING PAST FL240. THE CONFIGURATION WAS NR 1 BLEED CLOSED, NR 2 BLEED OPEN, NR 3 BLEED OPEN WITH BOTH PACKS ON. AS PER RED TABS, OPENED NR 1 BLEED AND CLOSED NR 2 BLEED. AFTER THISAug 29, 1997 · N203FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 97FDEA00502Valve · leakingLOWER AFT BODY LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1 CABIN AIR MODULATING VALVE PER MAINTENANCE MANUAL 36-00. RAN ALL THREE ENGINES PER B-727 JET RUN HANDBOOK. THE OVERHEAT LIGHT DID NOT ILLUMINATE. NO LEAKS FOUND.Aug 5, 1997 · N212FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 97FDEA00495Clamp · failedDURING CLIMBOUT AFTER 10 MINUTES OF FLIGHT, THE LOWER AFT BODY HEAT LIGHT CAME ON. CONFIGURATION WAS 1 AND 3 BLEEDS OPEN. PER RED TABS SECTION 2-7-14, NR 1 PACK AND BLEED WERE TURNED OFF. BEFORE NR 1 ENGINE COULD BE RETARDED THE LIGHT WENT OUT. THE OVERHEAAug 1, 1997 · N203FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 97FDEA00472Detection Unit · malfunctionedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN CRUISE FLIGHT. (NO ANTI-ICE ON AT ALL). NR 2 ENGINE LEFT BLEED ON NR 3 BLEED ON, LEFT AND RIGHT PACKS ON. FOLLOWED RED TABS PROCEDURES. LIGHT WENT OUT AFTER NR 1 ENGINE BLEED TURNED OFF FOR SEVERAL MINUTES. RANJul 25, 1997 · N206FE · Boeing 7272S2F · Overheat DetectionSDR 97FDEA00471Clamp · looseIN CRUISE FLIGHT AT FL 270, LOWER AFT BODY OVERHEAT LIGHT CAME ON. OPERATING ENGINES 2 AND 3 BLEEDS AT THE TIME WITH BOTH PACKS. OVERHEAT LIGHT WENT OUT AFTER FOLLOWING ABNORMAL EMERGENCY RED TABS CHECKLIST. OVERHEAT LIGHT WENT OUT AFTER SHUTTING OFF NR 2 EJul 24, 1997 · N203FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 97FDEA00352Fire Light · illuminatedAFTER TAKEOFF, NR 4 FIRE LIGHT CAME ON. SILENCED BELL AND NR 5 CARGO FIRE LIGHT CAME ON SILENCED THAT LIGHTS STAYED ON. DID 180 AND LANDED. SMOKE CONTROL WAS ON AND AFTER ROLLOUT LIGHTS EXTINGUISHED. NEVER DETERMINED OR SMELLED SMOKE. REMOVED FREIGHT FROM Jun 18, 1997 · N207FE · Boeing 7272S2F · Fire DetectionSDR 97FDEA00325Floorbeam · corrodedNR 0358, MAIN CARGO CORROSION TOP AND BOTTOM OF FLOORBEAM AT 2 FAST HOLES RBL 5 TO RBL 15, FS 344. REMOVED CORROSION ON BEAM BY CUTTING OUT AFFECTED AREAS AND INSTALLING ANGLE REPAIR PER SRM 53-10-08 FIG 7.May 30, 1997 · N208FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 97FDEA00324Skin · crackedNR 0715, FUSELAGE SKIN CRACKED AT RIVET RBL 1, STA 1098 ONE INCH TO RIGHT OF STRINGER 1. GAINED ACCESS TO AREA. HFEC CHECK TO FIND AND MARK END OF CRACK. CUT OUT DAMAGED AREA. HFEC TO CONFIRM DAMAGE REMOVED. INSTALLED REPAIR PER SB 727-53A0204 REVISION 3;May 28, 1997 · N208FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 97FDEA00261Retract Mech · malfunctionedON TAKEOFF AT IND LEFT MAIN GEAR DOOR HAD TO BE RECYCLED BEFORE IT WOULD RETRACT. WORKED FINE AT JFK. INSPECTED LEFT DOOR ASSEMBLY AND OPERATED GEAR DOOR SEVERAL TIMES, GEAR LIGHT CHECKED NORMAL.May 1, 1997 · N208FE · Boeing 7272S2F · Landing Gear Door Retract SectionSDR 97FDEA00273Doubler · malfunctionNR 0384, 71C301-02, SKIN GOUGED AT LWR FUSELAGE STA 720F FWD OF GROUND AIR INLET. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3.Apr 30, 1997 · N206FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 97FDEA00202Fire Loop · failedNR 1 ENGINE FIRE WARNING BELL AND LIGHT ILLUMINATED. SHUT DOWN ENGINE PER RED TABS. NR 1 ENGINE COWL OPENED. TAPPED ON ENGINE LOOP ASSY, JUST AFT OF GENERATOR AND FIRE HANDLE AND DETECTOR LIGHTS FLICKERED. REMOVED AND REPLACED ENGINE FIRE LOOP. OPS CHECK Mar 30, 1997 · N209FE · Boeing 7272S2F · Fire DetectionSDR 97FDEA00187Switch · inoperativeRIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE LIGHT REMAINED ON THROUGH FLIGHT. RED DOOR LIGHT ON INSTRUMENT PANEL SAME INDICATION. CYCLED GEAR, NO CHANGE. FUEL BURN WAS NORMAL, NO ASYMMETRIC CONTROL INPMar 20, 1997 · N205FE · Boeing 7272S2F · Landing Gear Position and WarningSDR 97FDEA00155Lock Actuator · damagedNOSE GEAR FAILED TO RETRACT WHEN GEAR HANDLE WAS PLACED UP. FOLLOWED RED TAB PROCEDURES AND RETURNED TO BASE. FOUND NOSE GEAR LOCK ACTUATOR DAMAGED. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR PER MAINTENANCE MANUAL 32-33-11. OPERATIONAL CHECK OK. OK FORMar 12, 1997 · N213FE · Boeing 7272S2F · Landing Gear Retraction/Extension SystemSDR 97FDEA00101Windshield · crackedON TAKEOFF, CAPTAIN'S WIND SCREEN BEGAN ARCING, HEAT TURNED OFF AND WINDOW CRACKED 20 SECONDS LATER. REMOVED AND REPLACED L-1 WINDOW PER MAINTENANCE MANUAL 56-11-11. REPLACED L-1 WINDOW HEAT CONTROLLER AND SYSTEM OPERATES NORMAL PER MAINTENANCE MANUAL 30-41-Feb 13, 1997 · N205FE · Boeing 7272S2F · Flight Compartment WindowsSDR 97FDEA00038Fuel Tank · leakingNR 2 FUEL TANK LEAKING ONTO AIR CYCLE MACHINE, LEFT SIDE INSIDE PANEL 3351L. INSPECTED AREA AROUND LT AIR CYCLE MACHINE, FOUND NO EVIDENCE OF FUEL LEAKING. CLEANED AREA AND CHECKED FOR LEAKS, NONE FOUND.Jan 12, 1997 · N208FE · Boeing 7272S2F · Fuel StorageSDR 96FDEA01693Starter · failedNR 3 ENGINE FIRE WARNING CAME ON AT 2,500 MSL, LIGHT WENT OUT WHEN NR 3 POWER RETARDED. FOUND STARTER TURBINE SHEARED FROM SHAFT, STARTER DESTROYED. REPLACED NR 3 ENGINE STARTER PER MAINTENANCE MANUAL 80-10-01. REPLACED NR 3 ENGINE START VALVE PER MAINTENANCNov 26, 1996 · N212FE · Boeing 7272S2F · Engine StarterSDR 96FDEA01641Control Valve · inoperativeINBOARD TRAILING EDGE FLAPS FAILED TO EXTEND, INBOARD ALTERNATE FLAP CIRCUIT BREAKER POPPED WHEN ALTERNATE FLAP SWITCH ACTUATED. REPLACED INBOARD FLAP CONTROL VALVE PER 727-200 MAINTENANCE MANUAL CHAPTER 27-51-51. SERVICED HYDRAULIC SYSTEM, RIGGED SYSTEM PEROct 31, 1996 · N213FE · Boeing 7272S2F · Trailing Edge Flap Control SystemSDR 96FDEA01604Supply Duct · burnt smellBURNT OIL SMELL FROM AIR CONDITIONING WHEN NR 1 BLEED USED FOR PACK AIR SOURCE ON DESCENT. REPEAT GRIPE. RAN NR 1 AND NR 3 ENGINES TOGETHER AND SEPARATELY AS AIR SOURCE . RAN LEFT AND RIGHT PACKS TOGETHER AND SEPARATELY WITH BOTH PACKS ON. USING NR 1 BLOct 21, 1996 · N216FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 96FDEA01585Coalescer Bag · dirtyAFTER TAKEOFF, AGAIN STRONG SMELL FROM NR 1 ENGINE BLEED ON LEFT PACK. CHANGED TO NR 3 BLEED AND RIGHT PACK, SMELL WENT AWAY. AT 18,000 FT USING NR 2 BLEED AND LEFT PACK, SMELL CAME BACK BUT NOT AS STRONG. SELECTED WARMER TEMPERATURE LEFT PACK, SLOWLY SMELLOct 18, 1996 · N209FE · Boeing 7272S2F · Humidity Control SystemSDR 96FDEA01579Valve · malfunctionedAGAIN ON DEPARTURE STRONG ACRID SMELL, RETURNED LEFT PACK AND NR 1 BLEED SELECTED. RETURNED TO AIRPORT. REMOVED AND REPLACED 3 HYD BLEED RESERVOIR CHECK VALVES. GROUND RAN NR 1 ENG WITH LT AND RT PACKS ON NR 1 BLEED AT H. POWER AND MAX HEAT, NO SMELL NOTEDOct 15, 1996 · N209FE · Boeing 7272S2F · Compressor Bleed ControlSDR 96FDEA01578Coalescer Bags · dirtyAFTER LIFT OFF STRONG ACRID SMELL IN COCKPIT ALONG WITH BURNING EYES (LEFT PACK #1 BLD) SWITCHED PACK/BLD SOURCE (RIGHT PACK #3 BLD) NO CHANGE IN SMELL. INTENSITY SEEMED TO CHANGE WITH PWR SETTINGS. INSPECTED INLETS & EXHAUST OF ALL ENGINES FOR FLUID NONE Oct 15, 1996 · N209FE · Boeing 7272S2F · Humidity Control SystemSDR 96FDEA01576Gasper Fan · failedCREW HAD AIR RETURN DUE SMOKE IN COCKPIT, ODOR POSSIBLY OIL/HYD CMA SMOKE AND FUMES. T/S A/C SYSTEM FOUND CONDENSOR/WATER SEPARATOR BAGS BLACK COLOR WITH BAD SMELL. GASPER FAN HAD OIL ON BLADES WITH BAD SMELL. REMOVED AND REPLACED CONDENSOR/WATER SEPARATOROct 15, 1996 · N216FE · Boeing 7272S2F · Air Distribution FanSDR 96FDEA01225Clamp · looseENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT AT 15,000 MSL. FOLLOWED APPROPRIATE CHECK LIST AND LIGHT WENT OUT CONTINUED TO GEG. TIGHTENED LEAKING CLAMPS BOTH SIDES OF MODULATING SHUTOFF VALVE IN NR 1 ENGINE STUB WING TO STOP LEAKS Jul 10, 1996 · N210FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 96FDEA01159Gasper Fan · failedFLIGHT CREW SMELLED ELECTRICAL INSULATION BURNING IN THE COCKPIT. WE NOTICED THE GASPER FAN CIRCUIT BREAKER OPENED. A FEW MINUTES LATER THE SMELL SUBSIDED. GASPER FAN CIRCUIT BREAKER WAS LEFT OPEN AND GASPER FAN SWITCH TURNED OFF. A/C RELEASED FOR SERVICE Jun 18, 1996 · N212FE · Boeing 7272S2F · Air Distribution FanSDR 96FDEA01072Overheat Unit · malfunctionedDISCREPANCY: ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED WHEN NR 1 THROTTLE WAS RETARDED, LIGHT WENT OUT. FINISHED CHECK LIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. CORRECTIVE ACTION: RAN ENGINE NR 1 AT IDLE POWER, CHECKED PYLON AREA FOR ANYJun 6, 1996 · N210FE · Boeing 7272S2F · Overheat DetectionSDR 96FDEA01070Valve · looseENGINE NR 1 STRUT OVERHEAT ILLUMINATED. WHEN NR 1 BLEED WAS CLOSED, LIGHT WENT OUT, FINISHED CHECKLIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. FOUND SENSE LINE ON NR 1 ENGINE BLEED AIR SHUTOFF VALVE LOOSE, (B-NUT WAS BACKED OFF). TIGHTENED SENSEJun 5, 1996 · N210FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 96FDEA01069Retract Mech · damagedUPON LDG AT 147K AND ROLLOUT TO 110K AT WHICH POINT A NOTICEABLE SHIMMY BEGAN AND GOT WORSE. A/C DIRECTION MAINTAINED WITH DIFFERENTIAL BRAKES AND REVERSE. NOSE WHEEL STEERING WAS COMPLETELY INEFFECTIVE. EMERGENCY EQUIPMENT REPORTED TO FLIGHT DECK, AND THAJun 4, 1996 · N206FE · Boeing 7272S2F · Landing Gear Retraction/Extension System
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