Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR CAL950156Support · corrodedDEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 320, RBBL 12. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)Feb 15, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL950155Support · corrodedDEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 344, BBL ZERO TO RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)Feb 15, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL950154Support · corrodedDEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 312, RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X)Feb 15, 1995 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954267Flap Track · corrosionTHE LEFT SIDE INBOARD TRACK FOR THE INBOARD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE, FORWARD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBOARD AND OUTBOARD SIDES OF THE TRACK. THE HOLES WERE BOTH OVERSIZED TO Feb 14, 1995 · N543DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S951435Rear Spar · crackedAT SHOP INSP, NR 3 MID FLAP WAS FOUND WITH BOTTOM REAR SPAR CRACKED AT 40 INCHES FROM I/B END. REPAIRED PER MM 57-52-0 PG 807.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951434Spar · crackedBOTTOM REAR SPAR CHORD CRACKED 54 INCHES FROM I/B END OF NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0. FOUND DURING SHOP INSPECTION.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951433Angle · crackedCHORD ANGLE REPAIR CRACKED AT I/B PUSH ROD CUTOUT NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951432Angle · crackedAT SHOP INSPECTION, NR 3 MID FLAP WAS FOUND WITH CHORD ANGLE CRACKED AT I/B AFT FLAP TRACK CUTOUT. REPLACED CHORD PER SRM 57-52-0.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951431Fitting · wornAT SHOP INSPECTION, NR 3 MID FLAP CARRIAGE SUPPORT FITTING INBOARD THRUST BEARING RETAINER BOLT HOLES ARE CORRODED. REAMED HOLE TO .312 TO REMOVE CORROSION HFEC, TREATED AND BUSH PER SRM 57-50-4.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950708Skin · delaminatedAT HMV, FOUND NR 14 SPOILER DELAMINATED. REPAIRED PER SRM 57-50-6.Feb 14, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950656Wire · looseDURING CRUISE, UNABLE TO MAINTAIN CABIN PRESSURE, INITIATED EMERGENCY DESCENT. REGAINED CONTROL AT FL 180 IN MANUAL MODE. FOUND INTERMITTENT WIRES AT RIGHT PACK FLOW CONTROL AND SHUT OFF VALVE. REPLACED 3 WIRES AT CANNON PLUG D870, WDM 21-61-02 PG.4. OPERAFeb 14, 1995 · N409DA · Boeing 727232 · Air Conditioning System WiringSDR DL72L950625Nose Rib · crackedFOUND DURING C-2 LETTER CHECK, NR 7 SLAT I/B ACTUATOR NOSE RIB CRACKED .1250 INCH. REPAIRED PER B727 MM 57-54-0 PG 803.Feb 14, 1995 · N502DA · Boeing 727232 · Leading Edge DevicesSDR DL72K950616Nose Cowl · wornDURING ROUTINE SHOP INSPECTION THE AFT LANDING STRIP BETWEEN 8-9 0'CLOCK POSITION WAS FOUND TO BE WORN. ON NR 1 ENGINE NOSE COWL, REPAIRED PER SRM 54-10-3 FIG 3.Feb 14, 1995 · N410DA · Boeing 727232 · Engine Cowling SystemSDR DL72S950714Rib · crackedAT HMV, FOUND NR 2 SLAT RIB MKD NR 2 CRACKED AT LWR T/E RADIUS. FABRICATED AND INSTALLED NEW REPAIR PER M/M 57-54-0 PG 819.Feb 13, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950713Rib · crackedAT HMV, FOUND NR 3 SLAT CLOSE OUT ATTACH RIBS NR 5 AND NR 17 CRACKED IN RADIUS. FABRICATED REPAIR PER MM 57-54-0.Feb 13, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951111Web · crackedDURING SERVICE CHECK INSPECTION, THE REPLACEMENT WEB PREVIOUSLY INSTALLED AS PART OF THE FRAME REPAIR KIT WAS FOUND CRACKED AT WL 216. IN ACCORDANCE WITH BAC S/B 727-53-0153, R.6., THE EXISTING WEB WAS REPLACED.Feb 12, 1995 · N407DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S950850Web · crackedAT HMV FOUND SUPPORT WEB CRACKED AT STA 357 STR 16 L AIR DUCT CUTOUT. FABRICATED DOUBLER PER ERA 301217-4. INSTALLED PER SRM 53-10-4.Feb 12, 1995 · N543DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950720Lt Box · corrosionAT HMV, FOUND CORROSION UNDER SEALANT AT RW L/E LT BOX AT STR 15R CABIN. FABRICATED REPAIR PER SRM 53-30-3.Feb 12, 1995 · N543DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S950719Stringer · crackedAT HMV, FOUND L/WING L/E LT BOX CRACK IN STR 15L FWD AND AFT OF BOX. DRILLED AND INSTALLED NEW REPAIR PER SRM 53-10-3 FIG 1.Feb 12, 1995 · N543DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950630Stringer · crackedFOUND AT HMV RT WING L/E LT BOX FWD SIDE HAS CRACK IN STR 15R. FABRICATED REPAIR PER SRM 53-10-3 FIG 2.Feb 12, 1995 · N543DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950852Stringer · damagedAT HMV FOUND HOLE IN STR 25L AT STA 580. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3.Feb 11, 1995 · N543DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950849Former · damagedAT HMV FOUND HOLE IN FORMER STA 540 STR 24L. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 26.Feb 11, 1995 · N543DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950814Stiffener · crackedDURING INSPECTION, THE RT UPPER TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS LOCATED AT F61273. THE STIFFENERS WILL BE REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4.Feb 11, 1995 · N534DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950712Skin · delaminatedAT HMV, FOUND NR 11 SPOILER PANEL DELAMINATED AT T/E. REPAIRED AS PER SRM 57-50-06.Feb 11, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72L950605Anti-Ice Valve · leakingDURING CLIMB, HAD NR 3 STRUT OVERHEAT LIGHT ON, LIGHT WENT OUT WITH REDUCTION OF POWER. RETURNED ATL. REPLACED NR 3 ENGINE ANTI-ICE VALVE AND UPPER ANTI-ICE DUCT ASSEMBLY AT VALVE, LEAK CHECK OK.Feb 11, 1995 · N510DA · Boeing 727232 · Air Intake Anti/De-Ice SystemSDR DL72S950851Support · crackedAT HMV FOUND SUPPORT STRIP CRACKED ON T/E OF STAB BELOW O/B ELEV ATTCH HNGE POINT. INSTALLED NEW T/E BEAM.Feb 10, 1995 · N543DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72S950717Skin · delaminatedAT HMV, FOUND NR 9 SPOILER DELAMINATED. BONDED REPAIR PER SRM 57-60-6.Feb 10, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950715Bracket · crackedAT HMV, FOUND NR 2 L/E FLAP ACT. BRACKET L/E CRACKED IB AND OB. FABRICATED AND INSTALLED NEW DOUBLER PER M/M 57-20-21.Feb 10, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950707Skin · delaminatedAT HMV, FOUND NR 12 SPOILER DELAMINATED. MADE BONDED NOTE PER SRM 51-50-6.Feb 10, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950631Bracket · crackedFOUND AT HMV IB/OB AT NR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED. REPAIRED BRACKETS PER M/M 57-20-21 FIG 807.Feb 10, 1995 · N543DA · Boeing 727232 · Wing, Attach FittingsSDR DL72S950584Skin · crackedFOUND DURING A-2 LETTER CHECK, 2 INCH VISIBLE CRACK AT LWR HINGE CUTOUT OF MAIN ENTRY DOOR ON FUSELAGE. REPAIRED PER MM 53-30-0 PG 820-836 PART 2.Feb 10, 1995 · N534DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950815Beam · crackedDURING INSPECTION, THE FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED IN THE ANGLE. THE BEAM WILL BE REPLACED IN ACCORDANCE WITH B727 S 53-0129 REV 4.Feb 9, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950716Panel · damagedAT HMV, FOUND NR 7 SPOILER PANEL HAS BOTTOM SURFACE TEMPORARY. REPAIRED PER B727 SRM 51-40-6 FIG 35.Feb 9, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950607Engine · flamed outDURING DESCENT, NR 3 ENGINE FLAMED OUT UPON RETARD OF THROTTLES AT FL370. FUEL HEAT AND IGNITION ON AT THE TIME. HAD SUCCESSFUL AIR RESTART. INSPECTED AND REPLACED FUEL AND OIL FILTERS FOUND OK, RAN ENGINE PER PFHB, NO PROBLEMS FOUND, RETURNED TO SERVICE.Feb 9, 1995 · N532DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S950571Skin · crackedDURING LETTER CHECK, FOUND 2 CRACKS IN PANEL FWD OF SADDLE PLATE LEFT SIDE VERTICAL STABILIZER. REPAIRED PER MM 54-30-0 PG 801-802.Feb 9, 1995 · N409DA · Boeing 727232 · Vertical StabilizerSDR DL72S951201Flap · corrosionNR 2 MID FLAP DURING HMV WAS FOUND TO HAVE CORROSION IN ALL FOUR I/B THRUST BEARING RETAINER BOLT HOLES. THE HOLES WERE REPAIRED PER SRM 57-50-4 PAGE 34.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951200Flap · corrosionNR 2 MID FLAP DURING HMV WAS FOUND TO HAVE CORROSION IN ALL FOUR O/B THRUST BEARING RETAINER BOLT HOLES. THE HOLES WERE REPAIRED PER SRM 57-50-4 PAGE 34.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951199Flap · crackedNR 2 FLAP DURING HMV SHOP INSP WAS FOUND TO HAVE A CRACK IN DOULBER ON AFT SPAR 36 INCHES FROM I/B END. DOUBLER WAS REPLACED PER SMR 57-52-0 PAGE 807.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950963Skin · delaminatedDURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 46 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SMR 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950962Skin · delaminatedDURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 46 TO 59 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950961Skin · delaminatedDURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 21.5 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950960Skin · dentedDURING SHOP INSPECTION, FOUND TOP SKIN DENTED 89 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950959Skin · delaminatedDURING SHOP INSPECTION, BOTTOM SKIN DELAMINATED 15 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950958Skin · delaminatedDURING SHOP INSPECTION, BOTTOM SKIN FOUND DELAMINATED 19 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950957Skin · delaminatedDURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 19 INCHES FROM I/B END, RT WING NR 4 FOREFLAP. REPAIRED PER SRM 57-40-4, WITH REF TO SRM 51-40-6.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950921Skin · wornA TEMP REPAIR WAS FOUND 47 INCHES FROM THE OB END. AN AREA WAS WORN THROUGH BOTH THE REPAIR AND THE LE SKIN OF NR 4 FOREFLAP. CLEANED UP DAMAGE AND INSTALLED DOUBLER PER SRM 57-50-4 FIG 1.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950920Skin · wornTHE L/E WAS WORN 52.5 INCHES FROM THE O/B END OF NR 4 FOREFLAP. THE AREA WAS CLEANED UP AND AN EXTERNAL DOUBLER INSTALLED PER SRM 57 50 4 FIG 1.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950919Skin · wornA TEMP REPAIR WAS FOUND 74 INCHES FROM THE O/B END ON L/E SKIN OF NR 4 FOREFLAP. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER SRM 57 50 4 FIG 1.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950918Skin · wornTHE LT SKIN WAS WORN AT APPROX 7.5 INCHES AND 10.5 INCHES FROM THE I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4 FIG 1.Feb 8, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950816Stringer · corrodedDURING CV-2 CK, FOUND CORROSION AT STR 23R JUST FWD OF STA 520. REPAIRED PER SRM 53-10-3 ID PER PS 900-5-1 NR 4.Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
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