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 CALA9600738Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 480, RBL 44 TO 60. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-1, FIGURE 4.Apr 17, 1996 · N16784 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S961731Rib · crackedRIB NR 18 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961730Rib · crackedRIB NR 12 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961729Rib · crackedRIB NR 12 WAS CRACKED. INSTALLED REPAIR PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961727Rib · damagedRIB NR 11 WAS CRACKED. INSTALLED RIB REPAIR PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961726Rib · crackedRIB NR 8 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960899Skin · crackedFOUND ON B1 LETTER CHECK, UPPER RUDDER OUTER SKIN CRACKED 3 INCH RT SIDE, 1 FT FROM TOP CENTER. INSTALLED DOUBLER PER SRM 55-40-2 FIG 1.Apr 16, 1996 · N485DA · Boeing 727232 · Rudder, Plate/SkinSDR DL72S960890Batteries · dischargedEMERGENCY EXIT LIGHT AT L1 DOOR INOP. REPLACED BATTERIES, CKS GOOD.Apr 16, 1996 · N497DA · Boeing 727232 · Emergency LightingSDR DL72S960886Stiffener · crackedFOUND ON B-1 LETTER CHECK, VERT SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK O/B SIDE. REPLACED PER M/M 57-20-21.Apr 16, 1996 · N485DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S960885Act Mount Box · cracked angleFOUND ON B-1 LETTER CHECK, NR 5 L/E FLAP ACT MOUNT BOX I/B LWR ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PG 811.Apr 16, 1996 · N485DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960884Stiffener · crackedFOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT SPAR STIFFENER AT NR 7 O/B SLAT TRACK O/B ANGLE. REPLACED STIFFENER PER M/M 57-20-21 PG 813.Apr 16, 1996 · N485DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S960883Act Attach Box · crackedFOUND ON B-1 LETTER CHECK, 1 INCH CRACK NR 2 L/E FLAP ACT ATTACH BOX O/B SIDE. REPAIRED PER M/M 57-20-21.Apr 16, 1996 · N485DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S960882Skin · crackedFOUND ON B-1 LETTER CHECK, THREE .5 INCH CRACKS EXTENDING FROM FASTENERS FWD OF PANEL 9501 RT SIDE AND TWO .5 INCH CRACKS EXTENDING FROM FASTENERS BELOW PANEL 9501 RT SIDE. REPAIRED PER M/M 54-30-0 PG 801 AND 802.Apr 16, 1996 · N485DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S960880Skin · crackedFOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT WEB OF TORQUE BOX TOP ROW OF RIVETS LT SIDE AT STA 1233. REPAIRED PER M/M 53-11-0 PG 832.Apr 16, 1996 · N485DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960874Rib · crackedRIB MARKED NR 14 WAS FOUND CRACKED IN THE LOWER RADIUS NEAR ATTACH ANGLE. THE NOTED RIB WAS REPAIRED IN COMPLIANCE WITH MM 57-54-0 FIGURE 805, FOR NR 2 L/E SLAT.Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960873Slat · crackedTHE INNR SKIN WAS FOUND CRACKED BY THE TELESCOPING ANTI-ICE DUCT. REPAIRED INNR SKIN PER SRM 57-50-3, FOR NR 2 L/E SLAT.Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960872Rib · crackedTHE 3RD RIB WAS FOUND CRACKED. REPAIRED RIB PER MM 57-54-0, FOR NR 2 L/E SLAT.Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960878Light · inoperativeFWD ENTRY OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.Apr 16, 1996 · N505DA · Boeing 727232 · Emergency LightingSDR CALA9600755Skin · crackedINSPECTION FOUND TWO .50 INCH CRACKS IN RT DOOR SIDE SKIN NEXT TO LOWER DOOR STOP FITTINGS. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-3, 51-10-2, AND 57-40-2.Apr 16, 1996 · N16784 · Boeing 727232 · Service DoorsSDR CALA9600752Stringer · corrodedINSPECTION FOUND STRINGER 27R IN FAR AFT SECTION OF FORWARD CARGO COMPARTMENT CORRODED NEAR ATTACH ANGLE AT STA 740. THE OLD SPLICE WAS REMOVED. A NEW SPLICE AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9600739Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 340, RBL 6 TO LBL 31. A REPAIR WAS INSTALLED IAW SRM 53-10-8.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600736Floorbeam · puncturedINSPECTION FOUND A HOLE IN CABIN FLOORBEAM AT STA 480, RBL 2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600733Floor Suppt · corrodedINSPECTION FLOOR SUPPORT CORRODED AT STA 418, RBL 24 TO 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600732Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 44 TO 60. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 5.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600731Angle · corrodedINSPECTION FLOOR ATTACH ANGLE CORRODED AT FS 303, LBL 42. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1.Apr 16, 1996 · N16784 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960863Light Panel · smokingPRIOR TO DEPARTURE WITH PSGRS ON BOARD, B-SYS STBY HYD PANEL WAS SMOKING. PSGRS WERE DEPLANED IN A NORMAL MANNER. FOUND BACKGROUND LIGHTING PANEL DAMAGED. REPLACED PANEL ASSEMBLY.Apr 15, 1996 · N532DA · Boeing 727232 · Flight Compartment LightingSDR CALA9600743Skin · corrodedINSPECTION FOUND SKIN CORRODED IN FORWARD CARGO COMPARTMENT AT STA 700 TO 720, BL 0. THE CORROSION WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.Apr 15, 1996 · N16784 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600742Str Splice · crackedINSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO COMPARTMENT STRINGER SPLICE AT STRINGER 28R, BS 625, RBL 15. THE CRACKED SPLICE WAS REMOVED, A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND MM 51-20-11.Apr 15, 1996 · N16784 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600760Door Frame · corrodedINSPECTION FOUND THE C-2 DOOR FORWARD FRAME CORRODED. A NEW WEB AND T-CAP WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3.Apr 14, 1996 · N16784 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600751Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN UPPER SKIN OF LEFT OUTBOARD MID-FLAP AT WBL 442. THE CRACK WAS LOCATED SEVEN INCHES FROM AFT TRAILING EDGE. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.Apr 14, 1996 · N16784 · Boeing 727232 · Trailing Edge FlapsSDR CALA9600741Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT STA 620. THE CORROSION WAS REMOVED AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 1.Apr 14, 1996 · N16784 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9600740Doubler · corrodedINSPECTION FOUND DOUBLER CORRODED IN FORWARD CARGO PIT AT FS 720D, STRINGER 27L TO 24L. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND MM 51-20-15.Apr 14, 1996 · N16784 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3501Shear Tie · corrodedFORWARD CARGO, STA 720F, STATION FRAME BETWEEN 28L-27L HAS LEVEL 2 CORROSION ON FORWARD SIDE. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-10-4.Apr 14, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX3488Shear Tie · corrosionLEVEL 2 CORROSION ON SHEAR TIE AT STA 720C BETWEEN STR 27 AND STR 28R. REMOVED AND REPLACED SHEAR TIE ANGLE PER SRM 53-10-4 AND SRM 51-10-2. FABRICATED SHEAR TIE PER SRM 53-10-4, TREATED PER SRM 50-10-2. (X)Apr 14, 1996 · N17789 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600757Skin · loose fastenersINSPECTION FOUND FASTENERS LOOSE AND PULLING THROUGH EXTERNAL FUSELAGE SKIN AT STA 1342 TO 1348, LT SIDE. A REPAIR CHANNEL AND SKIN WERE INSTALLED IAW SRM 54-30-3, FIGURE 7.Apr 13, 1996 · N16784 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600756Skin · loose rivetsINSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN WITH RIVETS LOOSE AND PULLING THROUGH FROM STA 1342 TO 1348, RT SIDE. BULB ANGLES AND A DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND 51-40-4.Apr 13, 1996 · N16784 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600748Stringer · corrodedINSPECTION FOUND STRINGER 29R CORRODED AT F.S. 730 TO 740. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-10, AND 51-10-7.Apr 13, 1996 · N16784 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 96ZZZX3505Channel · gougedLOWER EDGE OF FORWARD CARGO DOOR HAS 4 EACH HEAVY GOUGES (BEYOND LIMITS). FABRICATED REPAIR CHANNEL PER SRM 51-20-2 AND INSTALLED LOWER BEAM CHANNEL PER SRM 52-30-1 AND SRM 51-30-2.Apr 13, 1996 · N17789 · Boeing 727232 · Cargo/Baggage DoorsSDR 96ZZZX3498Stringer · corrodedLEVEL 2 CORROSION ON STRINGER SPLICE AT STA 675, STR 27R. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE PER SRM 53-10-1 AND SRM 53-10-3.Apr 13, 1996 · N17789 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 96ZZZX3489T-Angle · crackedT-ANGLE, 5TH RIB, FORWARD CARGO DOOR IS CORRODED AND CRACKED. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-30-1 AND SRM 51-30-2.Apr 13, 1996 · N17789 · Boeing 727232 · Cargo/Baggage DoorsSDR DL72S961145Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECITON AREA SPECIFIED BY BOEING SERVICE BULLApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960881Skin · damagedAT MID-VISIT, THE HORIZ STAB PANEL NR 9215 WAS FOUND TO HAVE A HOLE IN THE TOP SURFACE. THE HOLE WAS REPAIRED PER SRM 55-10-2.Apr 12, 1996 · N498DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72S960876Skin · corrosionCORROSION DAMAGE WAS REMOVED FROM AROUND THE HOLE CUTOUT FOR THE RADIO ALTIMETER ANTENNA BETWEEN STATION 520 AND STATION 540, BETWEEN STRINGER 28 LEFT AND STRINGER 29 RIGHT. THE SKIN IS MACHINED CLAD 2024-T3 SHEET WITH A LOCAL THICKNESS OF 0.090 THICK. AN INApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960875Skin · corrosionCORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING STRINGER SPLICE AT BS 490 AND A NEW SPLICE BEING INSTALLED AT BS 510 PER B727 SRM. THE SKIN IS MANUFACTURED FROM MACHINED CLAD 2024-T3 WITH AApr 12, 1996 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960851Web · crackedLOWER LT TORQUE BOX VERTICAL WEB CRACKED BEYOND ROUTED OUT REPAIR, UPPER LIGHTENING HOLE STA 1228. REPAIRED PER M/M 53-11-0 PG 828.Apr 12, 1996 · N533DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960850Web · crackedA .375 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB UPPER FWD END STA 1213. REPAIRED PER M/M 53-11-0.Apr 12, 1996 · N533DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960849Stringer · crackedA .75 INCH CRACK IN VERT STAB STR 7 AT 3RD BULKHEAD ABOVE OPENING TO CRAWLWAY. REPAIRED PER M/M 55-30-0.Apr 12, 1996 · N533DA · Boeing 727232 · Vertical StabilizerSDR DL72S960848Skin · crackedA 1 INCH CRACK IN NR 2 ENG INLET OUTER SKIN LT SIDE 8 O'CLOCK POSITION APPROX 36 INCHES AFT OF L/E. INSTALLED DOUBLER PER SRM 55-30-0.Apr 12, 1996 · N533DA · Boeing 727232 · Nacelle/Pylon StructureSDR 96ZZZX3499Stringer · corrodedSTRINGER 28R FROM STA 720F TO STA 740 HAS LEVEL 2 CORROSION ON INSIDE. REMOVED AND REPLACED CORRODED STRINGER SECTION AND REPAIRED PER SRM 53-10-3.Apr 12, 1996 · N17789 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S960843Angle · crackedFOUND ON E-2 LETTER CHECK, LWR T-ANGLE CRACKED AT AFT HINGE FOR LWR FUS PANEL 3448R. REPAIRED PER M/M 53-30-1 PG 807.Apr 11, 1996 · N407DA · Boeing 727232 · Fuselage Miscellaneous Structure
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