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 DL72S951521Stringer · corrosionFOUND DURING CV-2 CHECK, CORROSION AROUND RIVETS IN STRINGER 25L BETWEEN STA 950D AND 950E. REPAIRED PER MM 53-11-0.Apr 12, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951496Rib · crackedDURING SHOP, INSPECTION RT WING NR 5 L/E SLAT WAS FOUNED WITH RIB NR 12 CRACKED. REPAIRED PER MM 57-54-00.Apr 12, 1995 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951492Te Skin · crackedDURING SHOP INSPECTION, THE LEFT ELEVATOR WAS FOUND WITH CRACKS IN THE TRAILING EDGE. REPAIRS ACCOMPLISHED PER SRM 55-20-3.Apr 12, 1995 · N494DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S951490Skin · crackedAT HMV, LEFT ELEVATOR WAS FOUND WITH CRACKED SKIN AT THE TRAILING EDGE. REPAIRED PER SRM 55-20-3.Apr 12, 1995 · N494DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S952107Chord · crackedLOWER AFT CHORD IS CRACKED 55 INCHES FROM IB END OF NR 3 MID-FLAP. CHORD WAS REPAIRED PER MM 57-52-0. DAMAGE FOUND AND REPAIRED AT HMV SHOP VISIT.Apr 11, 1995 · N494DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S952105Skin · crackedAT HMV, SHOP INSPECTION, NR 3 MID-FLAP WAS FOUND WITH LOWER AFT SKIN PANEL (COVE SKIN) CRACKED AT CUT-OUT 32 INCHES FROM THE IB END. REPAIR DOUBLER WAS INSTALLED AND REPAIR WAS ACCOMPLISHED PER MM 57520, PAGE 819.Apr 11, 1995 · N494DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951695Frame · crackedAT HMV, FOUND NR 2 SLAT O/B END 2ND FRAME FROM END CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.Apr 11, 1995 · N494DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951694Frame · crackedAT HMV, FOUND NR 3 L/E SLAT NR 7 FRAME CRACKED INSIDE L/E. REPAIRED PER M/M 57-54-0 FIG 814.Apr 11, 1995 · N494DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951692Frame · crackedAT HMV, FOUND NR 3 L/E SLAT OB FRAME CRACKED. REPAIRED PER M/M 57-54-0 FIG 805.Apr 11, 1995 · N494DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951564Frame · corrodedDURING HMV, FOUND STA 380 FRAME AT R-1 DOOR CORRODED AT Z ANGLE JOINT. REPAIRED PER SRM 53-10-4 FIG 23.Apr 11, 1995 · N494DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S951561Rib · crackedDURING HMV, FOUND NR 1 SLAT I/B END 2ND FRAME CRACKED. REPLACED RIB PER MM 57-54-00.Apr 11, 1995 · N494DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951491Slat · crackedFOUND DURING A-2 LETTER CHECK, .5 INCH CRACK AT I/B STOP PAD NR 6 SLAT. REPAIRED PER MM 57-54-0.Apr 11, 1995 · N537DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951826Stringer · crackedDURING HMV, FOUND STR 8L CRACKED 3RD BAY UP FROM ACCESS HOLE INSIDE VERT STAB. REPAIRED PER M/M 55-30-00 PG 803.Apr 10, 1995 · N494DA · Boeing 727232 · Vertical StabilizerSDR DL72S951825Web · crackedDURING HMV, FOUND WEB CRACKED STA 1303 LWR RT CORNER INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 16.Apr 10, 1995 · N494DA · Boeing 727232 · Vertical StabilizerSDR DL72S951765Stringer · crackedDURING HMV, FOUND STRINGER CRACKED AT VERT STAB INTERIOR STR 7L, CRACKED LOC 3RD BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-0 PG 803.Apr 10, 1995 · N494DA · Boeing 727232 · Vertical StabilizerSDR DL72S951764Web · crackedDURING HMV, FOUND STA 1303 WEB CRACKED IN LOWER LT CORNER, INSIDE VERT STAB. REPAIRED PER M/M 53-11-0 PG 856.Apr 10, 1995 · N494DA · Boeing 727232 · Vertical StabilizerSDR DL72S951760Former · damagedDURING HMV, FOUND FS 560 FORMER UPPER RAIL BENT/DAMAGED ABOVE STR 25L TO STR 24L. REMOVED DAMAGE, REPAIRED PER SRM 53-10-4 PG 107.Apr 10, 1995 · N494DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951759Skin · gougedDURING HMV, FOUND EXTERIOR SKIN GOUGED AT STR 20R, STA 1343. REMOVED DAMAGE, REPAIRED PER SRM 54-30-3 FIG 7.Apr 10, 1995 · N494DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S951542Skin · crackedDURING SHOP INSPECTION, RT WING NR 4 FOREFLAP WAS FOUND WITH CRACKED SKIN AT BOTH TRACK CUTOUT PANS ON L/E. REPAIRED PER MM 57-50-4.Apr 10, 1995 · N527DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951758Support · corrodedDURING HMV, FOUND CENTER FLOOR SUPPORT CORRODED BETWEEN STA 700 TO 720 IN FWD B/B. REMOVED DAMAGE, REPAIRED PER SRM 53-10-5.Apr 9, 1995 · N494DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951697Hinges · corrodedAT HMV, FOUND HEAVY CORROSION BEHIND HINGES FOR ACCESS DOOR 3348L AC BAY. INSTALLED NEW REPAIR AND SPLICE PER M/M 53-30-1.Apr 9, 1995 · N494DA · Boeing 727232 · Air Conditioning DoorsSDR DL72S951648Floor Beam · corrodedFOUND AT HMV. FLOOR BEAM CORRODED AT STA 360 BETWEEN RBL AND LBL 25 AT FLOOR MOUNT HOLES. REPAIRED PER SRM 53-10-8 FIG 3.Apr 9, 1995 · N494DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S951563Floorbeam · corrodedDURING HMV, FOUND FLOORBEAM CAP CORRODED STA 400 FROM LBL 10 THROUGH RIGHT DOOR OPENING. REPAIRED PER SRM 53-10-8.Apr 9, 1995 · N494DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S951560Seat Track · crackedDURING HMV, FOUND LT O/B SEAT TRACK CRACKED IN VERTICAL SUPPORT WEB CUTOUT 3 INCHES FWD OF STA 760 FLOORBEAM. REPAIRED PER SRM 53-10-8.Apr 9, 1995 · N494DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CAL950263Hyd Motor · crackedIAH - FLT 0777 - THE A-HYDRAULIC SYSTEM QUANTITY WAS LOST ON LANDING AT IAH. MAINTENANCE FOUND THE INBOARD FLAP DRIVE POWER UNIT HYDRAULIC FLAP MOTOR HOUSING CRACKED. THE HYDRAULIC MOTOR WAS REMOVED AND REPLACED. IN ADDITION, BOTH THE NR 1 AND NR 2 ENGINE DApr 9, 1995 · N523PE · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S951691Skin · damagedAT HMV, FOUND UNIDENTIFIED REPAIR ON TOP SKIN OF RT ELEV BETWEEN NR 5 AND NR 6 HINGE. INSTALLED PERMANENT REPAIR PER SRM 55-20-3 FIG 4.Apr 8, 1995 · N494DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S951573Stringer · crackedAT HMV, FOUND STRINGER CRACKED AT RT LE FLOODLIGHT HOUSING. FABRICATED AND DRILLED REPAIR PER SRM 53-10-3 FIG 1.Apr 8, 1995 · N494DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951572Stringer · crackedAT HMV, FOUND STRINGER CRACKED AT FWD AND AFT SIDE OF L/E FLOODLIGHT HOUSING. DRILLED AND INSTALLED REPAIR PER SRM 53-10-3 FIG 2.Apr 8, 1995 · N494DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951645Beam · crackedFOUND AT HMV. UPPER T/E SUPPORT BEAM CRACKED AT NR 8 SPOILER ACTUATOR CUTOUT. REPAIRED BEAM PER MM 57-20-22 FIG 809.Apr 7, 1995 · N494DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S951562Stringer · crackedDURING HMV, FOUND STR 26L CRACKED AT FASTERNER HOLE STA 481. REPAIRED PER SRM 53-10-3 FIG 1.Apr 7, 1995 · N494DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951452Actuator · crackedON APPROACH, LOST SYSTEM A HYDRAULICS. LANDED ATL AND FOUND NR 7 SLAT ACTUATOR CRACKED. REPLACED ACTUATOR, OPERATION NORMAL.Apr 7, 1995 · N419DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S951423Angle · crackedTHE NR 8 L/E SLAT LWR FWD SKIN ATTACH ANGLE CRACKED AT ANTI-ICE AIR DUCT CUTOUT. REPAIRED PER SRM 57-54-0. FOUND DURING D-2 LTR CK TPAMM 4/6/95.Apr 7, 1995 · N406DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951578Sidewall · crackedTHE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1 INCH CRACK BET STA 294.5 AND 285.5 APPROX AT WL 170. THE WEB AT THIS LOCATION IS 0.040 INCH THK 2024-T3 CLAD. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND STRAP WILL BE INSTALLApr 6, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951455Bearings · wornDURING CRUISE, LEFT INBOARD AILERON WAS STUCK DOWN. NEEDS 20 DEGREE RIGHT AILERON INPUT FOR WINGS LEVEL AND 1.5 DEGREE RT RUDDER TRIM. FOUND RIGHT INBOARD AILERON LOWER QUADRANT BEARINGS FAILED. REPLACED BOTH BEARINGS PER MM 27-10-11. OPERATION NORMAL.Apr 6, 1995 · N542DA · Boeing 727232 · Aileron Control SystemSDR DL72S951427Bracket · crackedA .375 INCH CRACK NR 3 L/E FLAP ACT I/B ATTACH ANGLE. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-20-21 PG 811.Apr 6, 1995 · N406DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S951426Skin · crackedA .25 INCH CRACK AT PNL NR 9523 LT SIDE OF VERT STAB. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 54-30-0 PG 804.Apr 6, 1995 · N406DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72S951425Actuator Bracket · crackedA 2.5 INCH CRACK AT NR 1 SLAT ACTUATOR CASTING MOUNT BRACKET I/B SIDE. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-20-21 PG 812.Apr 6, 1995 · N406DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S951424Skin · crackedA .25 INCH CRACK IN FUSELAGE SKIN JUST AFT OF R-3 WINDOW. FOUND AT D-2 LETTER CHECK. REPAIRED PER SRM 53-30-3 FIG 8.Apr 6, 1995 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S951413Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 5 O/B RIB FOR ACTUATOR ROD END CRACKED. REPAIRED PER MM 57-54-0 PG 3, FOR RT WING NR 5 L/E SLAT.Apr 5, 1995 · N477DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951412Actuator Angle · crackedTHE NR 13 SPOILER OUTBD ACT ATTACH ANGLE CRACKED. FOUND AT D-1 LTR CK. INSTALLED TIME LIMITED REPAIR PER SRM 57-50-6 PG 57 TO 60.Apr 5, 1995 · N477DA · Boeing 727232 · Drag Control SystemSDR DL72S951411Actuator Support · crackedACTUATOR SUPPORT BOX CRACKED I/B AND O/B SIDES AT NR 1 L/E FLAP. FOUND AT D-1 LTR CK. REPAIRED PER MM 57-20-21 PG 811.Apr 5, 1995 · N477DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S951407Rib · crackedRIB NR 18 CRACKED NEXT TO NUTPLATE. INSTALLED DOUBLER PER MM 57-54-0 FIGURE 805. DURING SHOP INSPECTION OF RT WING NR 5 L/E SLAT.Apr 4, 1995 · N498DA · Boeing 727232 · Leading Edge DevicesSDR CAL950252Accessory Unit · inoperativeDEN - FLT 0759 - THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM DEN. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE GEAR SEVERAL TIMES, BUT WERE UNABLE TO DUPLICATE Apr 4, 1995 · N27783 · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S951598Cowling · damagedNOSE COWL NR 1 ENG WAS FOUND WITH TIME LIMITED REPAIR AT 6 O'CLOCK POSITION. THE COWL WAS REPAIRED PER SRM 54-30-3.Apr 3, 1995 · N416DA · Boeing 727232 · Engine Cowling SystemSDR DL72S951449Web · crackedFOUND ON CV2 CHECK .25 INCH CRACK LIGHTNING HOLE TORQUE BOX SIDE WEBB STA 1263 LT SIDE. REPAIR: ROUTE OUT DAMAGED AREA PER M/M 53-11-0.Apr 3, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951444Skin · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN BETWEEN STA 480 AND 500 AT BL 0. REPAIRED PER SRM 53-30-3 FIG 1.Apr 3, 1995 · N476DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S951495Stringer · corrodedFOUND ON CV2 CHECK, CORROSION AROUND RIVETS STRINGER 25L FROM 950A TO 950B. REPAIRED PER SRM 53-10-3 AND PER PS 900-5-1.Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951451Clip · crackedFOUND ON CV2 CHECK, ONE INCH CRACK IN SKIN CLIP BETWEEN STR 28L AND 29L FWD SIDE STA 990. REPAIR: REPAIRED PER M/M 53-11-0.Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951445Stringer · corrodedFOUND ON CV2 CHECK, CORROSION AROUND RIVETS STR 27L STA 1030 TO STA 1050. REPAIRED PER ERA 301506-14 CODE 4-53-14.Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S951647Frame · crackedAT HMV FROM SCHEDULED MTC SHEET. COMPLY WITH PERMANENT REPAIR PER 53-11-0 STA 913 AFT RT WHEEL WELL. REPAIRED PER MM 53-11-0 PG 814.Apr 1, 1995 · N494DA · Boeing 727232 · Fuselage Main, Frame
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