Boeing 727-251

Service difficulty reports · 1,181

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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 = '727251'
  ORDER BY difficulty_date DESC"

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SDR GAIA02163OPConnector · looseFLT 715 - ELP-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS RE-CYCLED AND ALL THREE DOWN AND LOCKED LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHEDec 4, 2002 · N278US · Boeing 727251 · Landing Gear Position and WarningSDR GAIA02162OPAccessory Unit · intermittentFLT 715 - ELP-FWA - ON APPROACH TO FW, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RE-CYCLED AND THE RED LIGHT REMAINED ON. FIVE MINUTES Dec 3, 2002 · N278US · Boeing 727251 · Landing Gear Position and WarningSDR GAIA02159OPSign · inoperativeDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 20, 2002 · N278US · Boeing 727251 · Emergency LightingSDR GAIA02157OPConnector · looseFLT 516 - FWA-ELP, ON APPROACH WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WNov 20, 2002 · N278US · Boeing 727251 · Landing Gear Position and WarningSDR GAIA02158OPAccessory Unit · malfunctionedFLT - 215 - DEN-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENTNov 19, 2002 · N278US · Boeing 727251 · Landing Gear Position and WarningSDR GAIA02154OPHinge · crackedDURING ROUTINE INSPECTION OF THE MAIN CARGO DOOR HINGE, A CRACK WAS INDICATED ON THE FORWARD END OF BOTH HALVES, FUSELAGE/DOOR. ALSO, AT THE AFT END OF FUSELAGE HALF. NON DESTRUCTIVE INSPECTION CONFIRMED FINDING. REMOVED AND REPLACED HINGE IAW SB AEIO1-01 RNov 7, 2002 · N252US · Boeing 727251 · Fuselage, Door HingeSDR 0203792299Battery Pack · inoperativeEmergency escape path lighting inoperative at rows 1-7 as well as main cabin and galley door vertical signs. Maintenance replaced battery pack. Operational tests were satisfactory.Nov 2, 2002 · N299US · Boeing 727251 · Emergency LightingSDR 0203522299Lap Joint · crackedDuring special visit check found cracks in lap joints at BS 480-680 STR 26L. Repaired per EA 22-184425.Oct 16, 2002 · N299US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA02134OPLight · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 25, 2002 · N255US · Boeing 727251 · Emergency LightingSDR GAIA02128STSeat Track · corrodedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 25 WAS CORRODED OUT OF LIMITS. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 51-30-5, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA02127STStringer · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15L WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Longeron/StringerSDR GAIA02126STStringer · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15R WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Longeron/StringerSDR GAIA02125STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE PREVIOUS REPAIR AT FRAME BS 600, STRINGER S17R. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02124STFrame · dentedDURING LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S7R IS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02123STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT A PREVIOUS REPAIR TO A FRAME AT BS 540, STRINGER S17R HAD BEEN DENTED. ACCOMPLISHED REPAIR TO FRAME IAW 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02122STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 540, STRINGER S9R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02121STSkin · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING OUTBOARD AILERON TAB HAS A SHARP DENT. REMOVED AND REPLACED THE RIGHT OUTBOARD AILERON TAB IAW BOEING MM 27-10-41. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Aileron TabsSDR GAIA02120STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THE THE FUSELAGE FRAME AT BS 400, STRINGER S6R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02119STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 380 WAS DENTED AT STRINGER S5L. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02118STSkin · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO DOOR INNER SKIN IS CRACKED AROUND NR 3 LATCH HOOK ASSEMBLY FROM AFT CENTER ATTACH BOLT. ACCOMPLISHED REPAIR IAW COTNEY EDR03-1, 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Cargo/Baggage DoorsSDR GAIA02117STSeat Track · corrodedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 45.5 IS CORRODED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA02116STFrame · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FRAME AT BS 344, STRINGER S2L WAS CRACKED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-2, FIGURE 3 AND 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, FrameSDR GAIA02115STBeam · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE AFT PRESSURE BULKHEAD VERTICAL BEAM AT BS 1183, WL 240, RBL 36 IS CRACKED AT THE INBOARD CHORD. ACCOMPLISHED REPAIR IAW BOEING SERVICE BULLETIN 727-53-0192, REV 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Miscellaneous StructureSDR GAIA02114STFloorbeam · corrodedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FLOORBEAM AT BS 783, LBL 45.5 HAS CORROSION AT UPPER T-CAP. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA02112STSeat Track · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK WAS CRACKED AT BS 720D, RBL 45.5. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA0211STFloorbeam · damagedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 560, LBL 3 HAVE NUMEROUS HOLES THROUGH THE UPPER FLANGE AND RADIUS. ACCOMPLISHED A REPAIR IAW BOEING 727 SRM 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA02110STTorque Box · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIRS RIGHT LOWER TORQUE BOX HAS A CRACKED REPAIR CHANNEL AT BS 1263. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-2, FIGURE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Miscellaneous StructureSDR GAIA02130STStiffener · crackedDURING A LTC INSPECTION, IN WAS DISCOVERED THAT THE LEFT WING LEADING EDGE AT WS 62.4 HAS A BOTTOM STIFFENER CRACKED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 57-10-2, FIGURE 3 AND 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Wing Miscellaneous StructureSDR GAIA020129STRib · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIB CHORD AT FUSELAGE BS 760.95 LEFT WAS CRACKED AT THE FIRST TWO FORWARD HOLES. ACCOMPLISHED REPAIR IAW BOEING 727 SERVICE BULLETIN 727-57-0112, REV 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251 · Wing, Rib/BulkheadSDR 0202962202Csd · malfunctionedTAKEOFF WAS ABORTED AT 130 KNOTS AFTER THE NR 3 GENERATOR TRIPPED. RESET THE NR 3 GENERATOR AND IT TRIPPED AGAIN. RETURNED TO THE GATE. REPLACED THE NR 3 CSD. RAN ENGINE. OPERATIONAL CHECK OK.Sep 18, 2002 · N202US · Boeing 727251 · Alternator-Generator DriveSDR GAIA02099OPLight · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE CABIN EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2002 · N252US · Boeing 727251 · Emergency LightingSDR GAIA02096STSkin · gougedDURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS GOUGED FROM STATION 950C TO 990 BETWEEN STRINGER 28L-29. MAINTENANCE REPAIRED THE GOUGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-3 DATED 8/01/02. (M)Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA02097STSkin · damagedDURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DAMAGED FROM STATION 950C TO 990 BETWEEN STRINGER 26L-28L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-1 DATED 8/01/02. (M)Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA02098STSkin · gougedDURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DENTED AND GOUGED FROM STATION 970C TO 1009 BETWEEN STRINGER 26L-29L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING INC DRAWING NR 53-02463-2 DATED 8/01/02. (M)Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/SkinSDR 0202682287Power SupplyAFT CABIN SECTIO OF EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK OK.Aug 20, 2002 · N287US · Boeing 727251 · Emergency LightingSDR GAIA02079OPLight · dischargedDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. C/A: RECHARGED EMERGENCY LIGHT ASSEMBLY FROM THE GROUND POWER UNIT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 9, 2002 · N255US · Boeing 727251 · Emergency LightingSDR 0202472275Nut · crackedWHILE PERFORMED SCHEDULED MAINTENANCE IN DTW, THE RIGHT MAIN LANDING GEAR FORWARD TRUNNION FITTING ATTACH BOLT OUTBOARD NUT WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE NUT PER IAW MM 32-11-51.Jul 30, 2002 · N275US · Boeing 727251 · Main Landing Gear Attach SectionSDR GAIA02076OPSmoke Detector · malfunctionedFLT 3706 - FWA-ELP - AFTER TAKEOFF, THE NR 1 SMOKE DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETUREND TO SERVICE. (M)Jul 24, 2002 · N255US · Boeing 727251 · Smoke DetectionSDR GAIA02072OPHydraulic System · failedDURING CRUISE THE AIRCRAFT STARTED TO LOOSE BOTH A AND B SYSTEM HYDRAULIC SYSTEM FLUID. BOTH SYSTEMS WERE SECURED AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED, USING MINIMUM BRAKING AND REVERSE THRUST. THE AIRCRAFT WAS STOPPED ON THE RUNWAY, THE Jul 20, 2002 · N278US · Boeing 727251 · Hydraulic System, MainSDR 0202242275Valve · damagedDURING TAKEOFF ROLL AT 100 KNOTS, THE NR 2 ENGINE FLAMED OUT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 ENGINE PRESSURE AND DUMP VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jul 2, 2002 · N275US · Boeing 727251 · Fuel Controlling SystemSDR 0201762296Clamp · brokenAFTER TOUCHDOWN ON LANDING, LOST -A- SYSTEM HYDRAULICS. AIRCRAFT WAS ABLE TO CLEAR RUNWAY BEFORE HAVING TO BE TOWED TO THE GATE DUE TO DEPLETION OF HYDRAULIC FLUID. ORD MAINTENANCE REPLACED THE BROKEN CLAMP FOUND ON MAIN RETURN FILTER. ALSO REPLACED COMPLETMay 31, 2002 · N296US · Boeing 727251 · Hydraulic Filter, MainSDR SQ7A182002Clamp · looseIND - #3 engine strut overheat warning light came on.Reduced power and light went out. Maintenance found loose starter supply duct clamps. Replaced same.Ops checked normalMay 7, 2002 · N282 · Boeing 727251 · Engine Bleed Air SystemSDR 0201442288Hydraulic Line · failedAPPROACHING TOP OF DESCENT INTO DTW, BOTH -B- PUMP LOW PRESSURE LIGHTS ILLUMINATED. -A- SYSTEM SHOWED 2.5 GALLONS, -B- SYSTEM QUANTITY SHOWED 1.7 GALLONS. -B- SYSTEM PRESSURE FELL TO ZERO AFTER SOME FLUCTUATIONS. COMPLIED WITH COM PROCEDURE FOR FLUID LOSS May 4, 2002 · N288US · Boeing 727251 · Hydraulic System, MainSDR GAIA02039OPBleed Valve · leakingFLT 734- FWA-DFW - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THEN RN 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISH THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPLACED CLAMPS ON NR 3 Apr 19, 2002 · N278US · Boeing 727251 · Compressor Bleed ValveSDR GAIA02038OPClamp · out of positionFLT 874 - LAX-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. ADJUSTED SHIMS AND REPApr 19, 2002 · N278US · Boeing 727251 · Pneumatic Distribution SystemSDR GAIA02036OPClamp · out of positionFLIGHT 863 - EWR-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPOSITIONED CLAMP ON HIGH PRESSURE BLEED DUCApr 18, 2002 · N278US · Boeing 727251 · Pneumatic Distribution SystemSDR GAIA02037OPClamp · out of positionFLT 875 - FWA-LAX - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT LAX WAS UNEVENTFUL. REPOSITIONED CLAMP ON Apr 18, 2002 · N278US · Boeing 727251 · Engine Bleed Air SystemSDR GAIA02035OPClamp · looseFLT 864 - FWA-EWR - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT EWR WAS UNEVENTFUL. FOUND AIR LEAK AT THE NR 3 BLEApr 17, 2002 · N278US · Boeing 727251 · Pneumatic Distribution SystemSDR GAIA02034OPClamp · looseFLT 879 - FWA-SJC - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT SJC WAS UNEVENTFUL. FOUND SEVERAL LOOSE CLAMPS ANDApr 16, 2002 · N278US · Boeing 727251 · Pneumatic Distribution SystemSDR 2002F00644Regulator · malfunctionedDURING CLIMB-OUT OF PHL, GEN 1 BTB, GB AND FIELD LIGHTS ILLUMINATED FOLLOWED ABNORMAL PROCEDURES DUMPED 22,000 LBS RETURNED TO AIRPORT ONE GENERATOR ALREADY ON DMI SWAPPED RN 1 AND NR 2 VOLTAGE REGULATOR. OPS CHECK GOOD PER MM 24-20. AIRCRAFT RETURNED TO SERApr 12, 2002 · N266US · Boeing 727251 · AC Regulator
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