Boeing 727-222

Service difficulty reports · 1,723

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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 = '727222'
  ORDER BY difficulty_date DESC"

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SDR 99UAL900537Stringer · corrodedCORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010 THAT WAS BEYOND ALLOWABLE LIMITS. UAL REPAIR PROCEDURES CUT OUT THE BELLY SKIN TO ALLOW ACCESS TO REPLACE STRINGER 29. DURING THE CUTTING OF THE SKIN THE EDGE MARGIN OF THE FASTENER ROW Oct 18, 1999 · N7458U · Boeing 727222 · Fuselage Main, Longeron/StringerSDR 99UAL900536Power Supply · failedEEL STRIPS INOPERATIVE IN CENTER PORTION OF CABIN. ALSO, WALL MOUNTED EXIT SIGNS ON LOWER LEFT SIDEWALL BY THE OVERWING DOORS INOPERATIVE. *S/D* REPLACED POWER SUPPLY AND 2 LIGHT SEGMENTS.Oct 18, 1999 · N7279U · Boeing 727222 · Emergency LightingSDR 99UAL900533Wire · looseEMERGENCY LIGHT OUT ABOVE FORWARD GALLEY DOOR. *S/D* LOOSE GROUND CONNECTION. REPAIRED LOOSE GROUND GD352. WD 33-51-02. OPS CKS GOOD.Oct 16, 1999 · N7257U · Boeing 727222 · Light System WiringSDR 99UAL900535Seat · looseAFTER TAKOFF FROM FLL SEAT ROW 14 DEF CAME OUT OF THE TRACK. MOVED PASSENGERS AND CREW WAS ABLE TO PUT ROW OF SEATS BACK INTO THE TRACK. SUPPLEMENTAL DATA UPDATE SECURED SEATS AT ATTACH POINTS.Oct 16, 1999 · N7285U · Boeing 727222 · Passenger Compartment EquipmentSDR 99UAL900534Unknown · odorUPON ROTATION EXPERIENCED HAZE IN THE COCKPIT ALONG WITH A BURNING RUBBER SMELL. SMELL WOULD GO AWAY AND COME BACK. RETURNED TO ORD AND DID A FLY-BY TO DETERMINE IF THERE WAS A PROBLEM WITH THE GEAR BEFORE MAKING A NORMAL LANDING. *S/D* MAINTENANCE SPECULOct 16, 1999 · N7287U · Boeing 727222 · Air Distribution SystemSDR 99UAL900513Valve · crackedAFTER DEPARTURE FROM BDL, AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE. DIVERTED TO BOSTON. *S/D* FOUND RT MLG LOCK OPERATED DOOR SEQUENCE VALVE ASSY CRACKED. REPLACED VALVE. JACKED AIRCRAFT, ACP'D GEAR SWING FIVE COMPLETE CYCLES AND CYCLED ALL FLIGHT CONTROOct 10, 1999 · N7269U · Boeing 727222 · Landing Gear Door Retract SectionSDR 99UAL900512Tailskid · damagedPOSSIBLE TAIL STRIKE ON TAKEOFF FROM BDL. TAIL STRIKE ILLUMINATION LIGHT ON. OVER SYR UNABLE TO MAINTAIN PRESSURE. DIVERTED TO CLE. *S/D* REPLACED CYLINDER AND SKID STRIKE PAD, OPERATIONALLY CHECKED OK. ALSO, PERFORMED CABIN PRESSURIZATION SYSTEM CHECK, Oct 8, 1999 · N7277U · Boeing 727222 · Auxiliary Gear (Tail Skid)SDR 99UAL900515Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON BOTH THE RIGHT AND LEFT SIDES WERE FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREAS WERE BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAOct 7, 1999 · N7452U · Boeing 727222 · Vertical Stabilizer, Spar/RibSDR 99UAL900509Frame · crackedA CRACK WAS FOUND IN THE BODY STATION 760.95 FRAME STUB WEB (P/N 65-16325-18) AT THE CORNER OF AN EXISTING ACCESS HOLE CUTOUT. THE CRACK WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DEROct 5, 1999 · N7452U · Boeing 727222 · Fuselage Main, FrameSDR 99UAL900504Access Panel · loosePASSENGER REPORTED FUEL DRAINING FROM LEFT WING TIP. CREW REPORTED QUANTITY DECREASING. RETURNED TO ABQ. *S/D* TORQUED NR 15 LEFT HAND WING ACCESS PANEL.Oct 1, 1999 · N7451U · Boeing 727222 · Wing, Plate/SkinSDR 99ZZZM759Clamp · looseFLT 308 - EN ROUTE TO JFK, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. RAN CHECKLIST, LIGHT EXTINGUISHED WITH NR 1 BLEED PACK VALVE CLOSED. FOUND AIR LEAK AT CLAMP ON DUCTING BEHIND PANEL OF THE RIGHT KEEL BEAM IN THE RIGHT WHEEL WELL. SECURED SAME.Sep 28, 1999 · N7642U · Boeing 727222 · Pneumatic Distribution SystemSDR 99UAL900499Skin · crackedFUSELAGE SKIN AFT OF FORWARD LAVATORY SERVICE PANEL FOUND WITH CRACKS AROUND AREA FASTENERS DUE TO CORROSION. 2024-T3 O.O40 INCH FUSELAGE SKIN AT STATION 312 RT SIDE, BETWEEN STRINGERS S-19 AND S-21 CORRODED. UNDERLYING BEAR STRAP, FRAME AND STRINGERS NOT AFSep 27, 1999 · N7279U · Boeing 727222 · Fuselage Main, Plate/SkinSDR 99UAL900493Battery · dischargedEMERGENCY LIGHT AT DOOR 2R INOPERATIVE. *S/D* REPLACED BATTERIES.Sep 27, 1999 · N7260U · Boeing 727222 · Emergency LightingSDR GAIA99144BStrut · leakingTOL- ATL - FLT 518 - DURING TAKEOFF, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS SELECTED UP. THE LIGHT ON THE FLIGHT ENGINEERS DOOR WARNING PANEL. THE CREW CARRIED OUT AOM PROCEDURES, AND RETURNED TO TOL MAKING A ROUTINE AND SAFE LANDINGSep 23, 1999 · N90AX · Boeing 727222 · Nose/Tail Landing Gear Strut/AxleSDR GAIA99142Light · inoperativeDURING ROUTINE INSPECTION, COCKPIT EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Sep 21, 1999 · N90AX · Boeing 727222 · Emergency LightingSDR 99ZZZM760Bulb · failedFLT 215 - DAY - NR 6 SMOKE DETECTOR IS INOPERATIVE. RELAMPED BEACON LAMP ON NR 6 SMOKE DETECTOR. (M)Sep 21, 1999 · N7645U · Boeing 727222 · Smoke DetectionSDR 99UAL900486Switch · out of adjustAFTER DEPARTURE FROM SYRACUSE, CREW RECEIVED AN AMBER LIGHT INDICATION ON THE AFT STAIR/DOOR. RETURNED TO SYR. ADJUSTED UPLOCK SWITCH. ACTUATED AIRSTAIR SEVERAL TIMES. GROUND CHECKS NORMAL.Sep 18, 1999 · N7282U · Boeing 727222 · Door Warning SystemSDR GAIA99141Switch · out of adjustFLT 518 - TOL-ATL, AFTER TAKEOFF, THE CREW RETRACTED THE GEAR AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO TOL AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIES. ADJUSTED THE NOSE LANDING GEAR DOOR SWITCHES AND PERFORMED A RETSep 17, 1999 · N90AX · Boeing 727222 · Landing Gear Position and WarningSDR 99UAL900481Connector · failedGALLEY HOT PLATE SMOKING AND SPARKING. HOT PLATE CORD FRAYED AND EXPOSED. *S/D* REMOVED HOT PLATES, INSPECTED WIRING FROM GALLEY WALL TO PLATES AND NO DAMAGE, NO OPEN INSULATION, NO BRITTLENESS. INSTALLED NEW CONNECTORS, CLEANED AREA, RECONNECTED HOT PLATESep 16, 1999 · N7459U · Boeing 727222 · Buffet/GalleysSDR 99UAL900480Light · inopEMERGENCY AISLE LIGHT AT STATION 680 IS INOPERATIVE.Sep 16, 1999 · N7442U · Boeing 727222 · Emergency LightingSDR 99ZZZM761Hose · pluggedFLT 319 - OMA - NR 2 ENGINE OIL PRESSURE EXCEEDED NORMAL LIMITS (61 PSI) AND WOULD NOT RETURN TO NORMAL PRESSURE RANGE, NR 2 ENGINE WAS SHUT DOWN IN ACCORDANCE PROCEDURES AND CHECKLISTS. REPLACED OIL PRESSURE RELIEF VALVE, REPLACED OIL PRESSURE TRANSMITTER. Sep 14, 1999 · N7635U · Boeing 727222 · Engine Oil PressureSDR 99UAL900474Spar · corrodedTHE VERTICAL STABLE MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS RSep 10, 1999 · N7454U · Boeing 727222 · Vertical Stabilizer, Spar/RibSDR 99UAL900469Sill · corrodedCORROSION DAMAGE WAS FOUND ON THE OUTBOARD CHORD OF THE AFT CARGO DOOR LOWER SILL. THE DAMAGED AREA WAS CUT OUT AND REPAIRED WITH A STRIP AND ANGLE REPAIR PER TIMCO REO-06703 REPAIR INSTRUCTIONS. THE REPAIR WAS APPROVED BY FAA FORM 8110-3.Sep 3, 1999 · N7445U · Boeing 727222 · Fuselage Miscellaneous StructureSDR 99UAL900455Battery · dischargedEMERGENCY EXIT LIGHT IN CABIN TO OVERWING IS INOPERATIVE. REPLACED ROW 7 BATTERYS IN EMERGENCY LIGHT. OPERATIONALLY CHECKS GOOD.Aug 28, 1999 · N7281U · Boeing 727222 · Emergency LightingSDR 99UAL900454Air Dist · odorRETURNED TO GATE DUE TO ARCING ODOR IN COCKPIT. CLICKING STATIC ON RADIO. WINDSHEAR INOPERATIVE FAILURE LIGHT STARTED TO FLICKER. ON WAY BACK TO GATE SMOKE BEGAN TO COME FROM UNDER THE INSTRUMENT PANEL. RAN ENGINES WITH ALL SYSTEMS OPERATING, LOOKED BEHINDAug 20, 1999 · N7466U · Boeing 727222 · Air Distribution SystemSDR 99UAL900440Floorbeam · corrodedCORROSION WAS DISCOVERED ON THE UPPER CHORD OF THE STATION 1070 FLOORBEAM (P/N 65-20821-21), CENTERED ABOUT RBL 26. THE DAMAGE COVERS A SPAN OF SIX (6) FASTENER ROWS LOCATED BETWEEN THE RBL 24.75 SEAT TRACK AND THE GALLEY RAIL INBOARD OF THIS LOCATION. A REPAug 20, 1999 · N7445U · Boeing 727222 · Fuselage Main, Floor BeamSDR 99UAL900439Floorbeam · misdrilledA .1562 INCH DIAMETER HOLE WAS MISDRILLED ON THE UPPER CHORD OF THE STATION 360 FLOORBEAM AT ABOUT RBL 54. THE HOLE GOES THROUGH THE HORIZONTAL FLANGE AND EXTENDS INTO THE VERTICAL WEB OF THE FLOORBEAM. THE DAMAGE WAS REPAIRED PER THE INSTRUCTIONS GIVEN IN TAug 20, 1999 · N7445U · Boeing 727222 · Fuselage Main, Floor BeamSDR 99UAL900438Keel Beam · misdrilledA DOUBLE DRILLED HOLE WAS FOUND ON THE LOWER FLANGE OF THE STRINGER 29 RIGHT KEEL BEAM CHORD AT STATION 950C. THE HOLE WAS TRIMMED OUT AND A REPAIR STRAP INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY FAA FORM 8110-3.Aug 20, 1999 · N7445U · Boeing 727222 · Fuselage Main, KeelSDR 99UAL900434Hook · failedNR 3 LEADING EDGE SLAT DID NOT RETRACT. VERIFIED BY VISUAL CHECK. *S/D* FOUND SLAT HOOK CRACKED. REPLACED SLAT.Aug 19, 1999 · N7291U · Boeing 727222 · Leading Edge Slat Control SystemSDR 99UAL900430Stringer · corrodedCORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010. CORROSION WAS BEYOND ALLOWABLE LIMITS. THE ADJACENT STRINGER 29 RIGHT HAD BEEN REPLACED AT A PREVIOUS VISIT AND THE REPAIR TO THE SKIN FOR THAT REPLACEMENT ALSO INCORPORATED DAMAGE TO TAug 17, 1999 · N7445U · Boeing 727222 · Fuselage Main, Longeron/StringerSDR 99UAL900429Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THAug 16, 1999 · N7457U · Boeing 727222 · Vertical Stabilizer, Spar/RibSDR 99UAL900428Elbow · crackedDURING CLIMB, FEEDING FUEL FROM NR 2 TANK, TANK NR 1 DROPPED 1,000 LBS. CONDITION CORRECTED WITH CROSSFEED. *S/D* FOUND CRACKED ELBOW OF THE NR 1 FUEL VENT SYSTEM. REPLACED ELBOW.Aug 16, 1999 · N7260U · Boeing 727222 · Aircraft Fuel Distribution SystemSDR GAIA99136Overheat Light · illuminatedFLT 202 - TYS-DFW - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED PROCEDURE IN AOM AND LIGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER DIFFICULTY. RAN NR 3 ENGINE AT 80 PERCENT EPR AND COULD NOT DUPLICATEAug 15, 1999 · N90AX · Boeing 727222 · Overheat DetectionSDR GAIA99135Overheat Light · illuminatedFLT 202 - DFW-SEA - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. ACCOMPLISHED PROCEDURE AS PER AOM VOL 1 AND LIGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED NR 3 ENGINE AND STRUT FIRE LOOPS Aug 13, 1999 · N90AX · Boeing 727222 · Overheat DetectionSDR 99UAL900423Bulb · failedEMERGENCY EXIT LIGHT SIGN AT DOOR 2L INOPERATIVE. RELAMPED EXIT LIGHT, OPERATIONALLY CHECKED OK.Aug 12, 1999 · N7280U · Boeing 727222 · Emergency LightingSDR GAIA99134Overheat Light · illuminatedFLT 302 - DFW-TYS - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED KHA PROCEDURE AND CONTINUED OPERATION ON NR 2 BLEED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED ALL BLEED AIR PLUMBING, FITTINGS, OAug 7, 1999 · N90AX · Boeing 727222 · Overheat DetectionSDR 99UAL900416Sequence Valve · leakingON GEAR EXTENSION AIRCRAFT LOST HYDRAULIC SYSTEM A. BOTH PUMPS RAN TO ZERO HYDRAULIC FLUID QUANTITY. *S/D* REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND REPLACED LT MLG LOCK OPERATED SEQUENCE VLV PER MAINTENANCE MANUAL. PERFORMED NORMAL RETRACTIAug 7, 1999 · N7251U · Boeing 727222 · Landing Gear Retraction/Extension SystemSDR 99UAL900414Coffemaker · smokingLOWER COFFEEMAKER IN AFT GALLEY SMOKING AND SPARKING. *S/D* REPLACED COFFEEMAKER. INSPECTED WIRING, LEFT UNIT ON FOR SEVERAL HOURS, NO DEFECTS NOTED.Aug 7, 1999 · N7449U · Boeing 727222 · Buffet/GalleysSDR GAIA99115Hat Section · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE HAT SECTION AT STATION 344 TO 360, RBL 19 IS CORRODED. HAT SECTION REMOVED PER ATS DRAWING 2000-0373. FABRICATED A NEW FLOOR PANEL IAW B727 SRM 53-20-2. THIS Aug 6, 1999 · N90AX · Boeing 727222 · Fuselage Miscellaneous StructureSDR GAIA99114Skin · misinstalledDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT AT STATION 610 AND STRINGER 3L, A FASTENER IS INSTALLED ON TOP OF A BUCKTAIL. REPAIRED IAW ATS DRAWING 2000-0193. THIS DRAWING WAS DER RECOMMENDED AND ACO APPROVEDAug 6, 1999 · N90AX · Boeing 727222 · Fuselage Main, Plate/SkinSDR GAIA99113Floorbeam · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE FLOORBEAM AT STATION 620 IS CORRODED BETWEEN LBL 24.75 AND RBL 24.75 SEAT TRACKS. REPAIRED IAW ATS DRAWING 2000-0276. THIS DRAWING WAS DER RECOMMENDED AND ACO Aug 6, 1999 · N90AX · Boeing 727222 · Fuselage Main, Floor BeamSDR GAIA99112Keel Beam · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE KEEL BEAM (STRINGER 27R) AT STATION 950E HAD EXFOLIATED CORROSION. THIS IN THE AREA OF THE NR 2 LOWER CARGO DOOR FRAME. REPAIRED IAW DRAWINGS 53-99296-1 AND 53Aug 6, 1999 · N90AX · Boeing 727222 · Fuselage Main, KeelSDR 99ZZZM741Smoke Detector · looseFLT 307 - JFK - NR 5 CARGO COMPARTMENT SMOKE DETECTOR FAILS TO TEST. FOUND SOCKET LOOSE ON TEST BULB, RE-SECURED SOCKET OPERATIONAL CHECKS NORMAL. (M)Aug 4, 1999 · N7635U · Boeing 727222 · Smoke DetectionSDR 99UAL900424Bulkhead Chord · corrodedTHE FORWARD EDGE OF THE CHORD AT STATION 1183 BULKHEAD LBL 24, WL 209 WAS CORRODED BEYOND THE SRM ALLOWABLE LIMIT. DAMAGE WAS TRIMMED OUT AND AREA WAS REPAIRED WITH STRAP AND FILLER PER TIMCO INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110Aug 2, 1999 · N7451U · Boeing 727222 · Fuselage Main, BulkheadSDR 99UAL900405Battery · dischargedMID CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY.Jul 31, 1999 · N7273U · Boeing 727222 · Emergency LightingSDR 99UAL900408Rib · crackedDURING INSPECTION AND INSTALLATION OF THE PREVENTIVE MOD PER SERVICE BULLETIN727-57-0012 AS MANDATED BY AD94-07-08 AND AD90-06-09 ON THE LBL 70.5 RIB CHORD AT STATION 760.5 TWO CRACKED FASTENER HOLES WERE FOUND. FATIGUE. C0RRECTION, BOTH HOLES WERE OVERSIZEJul 30, 1999 · N7451U · Boeing 727222 · Wing, Rib/BulkheadSDR 99UAL900406Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIJul 30, 1999 · N7451U · Boeing 727222 · Vertical Stabilizer, Spar/RibSDR 99UAL900404Spar Web · misdrilledDURING ACCOMPLISHMENT OF THE CENTER WING BOX REAR SPAR WEB MODIFICATION AS MANDATED BY AD97-25-15, EIGHTY THREE HOLES WERE MISDRILLED COMMON TO THE REAR SPAR CENTER WEB ACCESS PLATE AND THE REAR SPAR WEB. OVERSIZED FASTENERS OF THE SAME TYPE WERE INSTALLED. Jul 27, 1999 · N7268U · Boeing 727222 · Wing SparSDR 99UAL900393Fire Loop · defectiveNR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO STRUT OVERHEAT. RETURNED TO DEN. *S/D* DEFLECTIVE FIRE LOOP AT STUB WING CAUSED THE STRUT OVERHEAT LIGHT TO ILLUMINATE. AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF FIRE LOOP AND ENGINE RUN UP VERIFICATION.Jul 25, 1999 · N7446U · Boeing 727222 · Fire DetectionSDR 99UAL900394Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. SHUT OFF BLEED AND ANTI-ICE. LIGHT WILL NOT GO OUT. DIVERTED TO CLE. *S/D* TIGHTENED LOOSE CLAMP ON THE 13TH STAGE VALVE AND ONE CLAMP ON THE CHECK VALVE. RAN ALL THREE ENGINES TO TAKEOFF POWER WITH NO STRUT OVERJul 23, 1999 · N7446U · Boeing 727222 · Pneumatic Distribution System
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