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 CALA9600913Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 580 BETWEEN STRINGER 27R AND 28R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-4, FIG 15 AND MM 51-20-2, 51-20-15.Jun 10, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600901Stringer · corrodedINSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.Jun 5, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S961357Light · corrodedRT EXTERIOR EMERGENCY EXIT LIGHT AT OVERWING HATCH INOP. CLEANED CORROSION ON LIGHT SOCKET CONTACTS. CHECKS NORMAL.Jun 4, 1996 · N520DA · Boeing 727232 · Emergency LightingSDR DL72S961397Frame · crackedFOUND CRACKS AT THE LT AND RT FRAMES AT STA 784. REPAIRED BOTH CRACKS PER BAC S/B 727-53-0197, REV 2.Jun 3, 1996 · N522DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S961396Skin · corrosionFOUND CORROSION SLIGHTLY AFT OF C-3 DOOR OPENING BEAR STRAP. REPAIRED PER ER/A 303676-14.Jun 3, 1996 · N522DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600936Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.Jun 2, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9600764Bulkhead Web · crackedINSPECTION FOUND A 1 INCH CRACK IN STA 1183 PRESSURE BULKHEAD AT LBL 8, W.L. 162. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-01473 AND BOEING DRAWING 65C33041.Jun 2, 1996 · N27783 · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S961326Light · inoperativeEXIT LIGHT RT AFT INOP, LT WING EMER LIGHT INOP AND RT ENTRY EMER LIGHT INOP.May 31, 1996 · N400DA · Boeing 727232 · Emergency LightingSDR DL72S961371Floor Beam · corrodedFOUND CORROSION ON FLOOR BEAM, STA 1030 UPPER FLANGE FASTENER HOLES AT LBL 0 AND LBL 9. REPAIRED PER M/M 53-20-11 PG 811B.May 29, 1996 · N416DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S961370Floor Beam · corrodedFOUND CORROSION 0N TOP OF FLOOR BEAM AT STA 1070, RBL 44 TO RBL 58. REPAIRED PER M/M 53-20-11 FIG 804A.May 29, 1996 · N416DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S961358Torque Box · crackedAT MID-VISIT, THE AFT STAIRWELL RT TORQUE BOX WAS FOUND CRACKED AT THE UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0.May 29, 1996 · N522DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600938Angle · corrodedINSPECTION FOUND CORROSION ON SKIN ATTACH ANGLE AT STA 580, STRINGER 27L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2 AND MM 51-20-11.May 29, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600915Support · corrodedINSPECTION FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 535, S28L TO S29L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-4, 51-10-2, 53-10-1 AND 51-30-2.May 28, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961469Blkhd Stiffener · crackedCRACKS WERE FOUND EMANATING FROM THE BOTTOM OF THE FLANGE ON THE VERTICAL STIFFENERS LOCATED AT THE BOTH LBL AND RBL 8. REPAIRED PER B727 S/B 727-53-0175, REV 2.May 26, 1996 · N522DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S961284Bulkhead · crackedCRACKS EMANATING FROM VERTICAL STIFFENERS AT LBL AND RBL 8 ON STA 1183 BULKHEAD. REPAIRED PER EO 4-59275-3AD.May 26, 1996 · N522DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S961279Battery Pack · dischargedON L/O, FOUND RT AFT EMERGENCY SLIDE LIGHT FLASHING. REPLACED BATTERY PACK, CK'S GOOD.May 26, 1996 · N537DA · Boeing 727232 · Emergency LightingSDR CALA9600919Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 265, S25R. A REPAIR WAS PERFORMED IAW SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-21.May 26, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600914Skin · corrodedINSPECTION FOUND SKIN LAP CORRODED AT STA 720D TO 720E, STRINGER 27R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.May 26, 1996 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600935Angle · corrodedINSPECTION FOUND ATTACH ANGLE CORRODED AT STA 540, S29R. THE ATTACH ANGLE WAS REMOVED. A REPAIR PART WAS FABRICATED IAW SRM 53-10-4, 53-10-1 AND 51-20-4.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600934Frame · corrodedINSPECTION FOUND STA 540 FRAME ASSEMBLY CORRODED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, PAGE 43.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9600902Angles · corrodedINSPECTION FOUND SKIN ATTACH ANGLES(2) AT BILGE, STA 580, BL ZERO CORRODED. ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961273Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED 1 INCH AT ANTI-ICE TUBE CUTOUT, NR 2 SLAT. REPAIRED PER M/M 57-54-0.May 24, 1996 · N490DA · Boeing 727232 · Leading Edge DevicesSDR DL72L961281Door Frame · crackedTHE L-2 DOOR FORWARD FRAME HAS A .5 CRACK EMANATING FROM THE LOWER INBOARD CORNER OF THE UPPER HINGE CUTOUT. THIS DAMAGE IS ADDRESSED BY B727 SRM 52-40-2, FIGURE 4. THERE IS AN EXISTING REPAIR LOCATED APPROXIMATELY 2 INCHES ABOVE THE UPPER HINGE CUTOUT. THEMay 24, 1996 · N513DA · Boeing 727232 · Service DoorsSDR CALA9600900Floor Beam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT B.S. 1130, LBL 25. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-8, AND MM 51-20-11.May 24, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR MZZA96049Frame · corrodedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON C3 CARGO DOOR LOWER FRAME FORMED, SECTION. THE CORRODED FORMED SECTION WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806May 23, 1996 · N15790 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961300Trunnion Ftg · corrodedAT MID VISIT, THE NLG TRUNNION FITTING WAS FOUND TO BE CORRODED. REPAIRED PER MM 53-40-0.May 23, 1996 · N522DA · Boeing 727232 · Nose/Tail Landing Gear Attach SectionSDR DL72S961299Trunnion Ftg · corrodedAT MID VISIT, BORE OF NLG FITTING WAS FOUND TO BE PITTED. AREA SPOTFACED, BORED DYE CHECKED, ROTOPEENED AND BUSHING INSTALLED PER M/M 53-40-0.May 23, 1996 · N522DA · Boeing 727232 · Fuselage, Landing Gear Attach FittingsSDR DL72S961268Light · inoperativeL-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP CKS GOOD.May 23, 1996 · N405DA · Boeing 727232 · Emergency LightingSDR DL72L961267Fitting · crackedA .6875 INCH CRACK IN NR 5 SLAT AT ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-0.May 23, 1996 · N513DA · Boeing 727232 · Leading Edge DevicesSDR DL72L961266Beam · chafedAFT SIDE OF MLG LOWER SIDE STRUT CHAFING INTO FWD SIDE OF WALKING BEAM RT WING. REPAIRED PER M/M 57-43-0.May 23, 1996 · N513DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR CALA9600923Floor Beam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 30. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-4 AND MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600912Web · crackedINSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2 AND MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9600909Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Wing, Plate/SkinSDR CALA9600899Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1010-1030, RBL 65. A REPAIR WAS FABRICATED AND INSTALLED IAW 51-30-2, 51-10-2, AND 51-40-3.May 23, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600897Floor Beam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 380, RBL 28 TO 59. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.May 23, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR MZZA96048Skin · misdrilledTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO RIVET SPACING WAS FOUND BELOW THE SPECIFIED LIMIT ON BS 530, STRINGER 27L THE DAMAGED SKIN WAS REPAIRED PER B727 SRM 53-30-3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806835. (SEQ NR 01084) May 22, 1996 · N15790 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S961484Angle · crackedFOUND A CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DELTA ER/A 303623-14AD.May 22, 1996 · N537DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961470Skin · corrosionTHE SKIN AT STA 1044 AND ST 28L WAS FOUND CORRODED. REPAIRED PER B727 SRM 53-30-3, FIGURE 3.May 22, 1996 · N537DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S961311Fitting · corrodedAT MID VISIT, THE RT MLG FLAP TRACK ATTACH FITTING WAS FOUND CORRODED. THE FITTING WAS REMOVED, HOLES MACHINED TO REMOVE CORR, BUSHINGS INSTALLED AND FITTING REINSTALLED PER 57-42-0 AND 27-51-31.May 22, 1996 · N522DA · Boeing 727232 · Wing, Control Surface Attach FittingsSDR DL72S961291Transverse Beam · crackedCRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA IS SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDACE WITH THE S/B.May 22, 1996 · N537DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961287Skin · damagedAIRCRAFT STRUCK BY A GROUND SERVICE TRUCK, DAMAGE CONSISTED OF A DENTED SKIN, A BROKEN STRINGER AND A CRACKED SHEAR CLIP. THE DENT WAS REMOVED WITH A CUTOUT AT STA 1080, THE STRINGER HAS BEEN CUT AND WILL BE SPLICED IN THE BAYS FWD AND AFT OF THE DAMAGE. ALSMay 22, 1996 · N490DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S961286Skin · corrodedSKIN CORROSION AT STRINGER 28L, STA 1044 TO 1047, CUTOUT IS 3 BY 1.75 INCH. REPAIRED PER DAL ER/A 303626-14.May 22, 1996 · N537DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600937Floor Beam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328, LBL 30. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 9.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600928Floor Beam · corrodedINSPECTION FOUND UPPER FORWARD FLANGE OF FLOORBEAM CORRODED AT BS 1070, RBL 47.25 TO 50.25. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-8. AN UPPER CHORD, SUPPORT ANGLES, FILLERS, STRAPS AND WEB DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10May 22, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600922Floor Beam · corrodedINSPECTION FOUND UPPER FLANGES OF FLOORBEAM CORRODED AT BS 1070, RBL 9 TO 12. THE CORRODED AREA WAS REMOVED. AN UPPER CHORD, SUPPORT ANGLES, FILLER AND STRAPS WERE FABRICATED AND INSTALLED IAW 53-10-8, FIGURE 1.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600921Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 308 TO 312, LBL 30. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND MM 51-20-151.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600920Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 312 TO 340, RBL 55. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600898Floor Beam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110, BL ZERO TO RBL 66. ANGLES, STRAPS, AND CORDS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-30-2, AND 51-10-2.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600896Floor Beam · crackedINSPECTION FOUND A .3750 INCH CRACK AND A .50 INCH CRACK IN FLOORBEAM U-CHANNEL AT B.S. 335, LBL 25, WL 200. THE CHANNEL WAS REMOVED. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-40-3, AND MM 51-20-11.May 22, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S961414Torque Box · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF THE AD 94-07-08 WHICH REQUIRES INSPECTION PER SB 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDMay 21, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
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