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 08FDEA01442Panel · crackedLOWER PANEL 3456 RT IS CRACKED WITH ERODED AREA FLAME SPRAY. REPLACED CRACK AND FLAME SPRAY ON PANEL 3456 REF SRM 51-40-9 PARAGRAPHS 3D, 4E, 4F AND AMM 51-20-051-7. THIS IS CLASSIFIED AS A MINOR REPAIR.Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 08FDEA00341Support · crackedFORWARD ENTRY DOOR LOWER AND UPPER AFT LATCH TORQUE TUBE SUPPORT CASTING HAS PARTIALLY DETACHED FROM DOOR FRAME AND FRAME IS CRACKED ON BOTH UPPER AND LOWER ATTACH POINTS. REMOVED AND REPLACED L1 FORWARD ENTRY DOOR PER 727-200 MM 52-11-001-4/ADJUSTMENT TEST GFeb 1, 2008 · N498FE · Boeing 727232 · Passenger/Crew DoorsSDR 07FDEA05124Plate · crackedCRACKED ANGULAR PLATE INBD OF LT WING INBD TE FLAP O/B TRACK ALONG AFT SUPPORT FRAME REMOVED AND REPLACED CRACKED ANGULAR PLATE IAW SRM 51-40-3 PAINTED AREA IAW SRM 51-20-151-7.Dec 23, 2007 · N499FE · Boeing 727232 · Wing, Plate/SkinSDR 07FDEA00205Door · malfunctionedCREW ENTRY DOOR SHOWED CLOSED AND LOCKED WITH HANDLE FULL DOWN AND DOOR LIGHT OUT. AIRCRAFT WOULD NOT PRESSURIZE. RTB, UPON INITAL INSP FOUND ROLLERS ON AFT SIDE OF DOOR NOT IN TRACKS ON THE UPPER AND LOWER TRACK. UNABLE TO OPEN DOOR. AFTER OFF LOAD VISUJan 26, 2007 · N498FE · Boeing 727232 · Passenger/Crew DoorsSDR 06FDEA0184Repair · misinstalledEXISTING REPAIRS 2 AT AFT AIR STAIR CUT OUT FWD CORNERS DO NOT COMPLY WITH FAA DATA. REMOVED RT AND LT REPAIR DOUBLERS IAW SRM 51-30-2. PERFORMED HFEC INSPECTION PER NTM-PT6 51-00-00 TO MARK THE END OF CRACKS. NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED Jan 13, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0086Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 445, STR 17R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0085Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 23L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0084Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0083Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950E, STR 29R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0082Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1130, STR 22L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0081Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ABOVE AIRSTAIRS CONTROL PANEL WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIPJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0080Repair · unknownFOUND PREVIOUSLY 2 REPAIRS INSTALLED ON LT WING TIP LOWER SURFACE WAS ACCOMPLISHED IAW SRM 57-20-5 FIG 1, BASED ON EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AJan 8, 2006 · N498FE · Boeing 727232 · Wing StructureSDR 06FDEA0079Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT UPPER SURFACE OF LT WING TIP WAS ACCOMPLISHED IAW SRM 57-20-1 FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHJan 8, 2006 · N498FE · Boeing 727232 · Wing StructureSDR 06FDEA0078Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 370, STR 24L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 4, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0077Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 680, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 24, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASSJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0076Repair · unknownFOUND PREVIOUSLY 2 REPAIRS INSTALLED AT FWD CARGO DOOR WAS ACCOMPLISHED IAW SRM 52-00-3 FIG 3 AND 4, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0075Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 300 ABOVE RT NLG DOOR WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0074Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASSJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0073Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 970, STR 25L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0072Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050, STR 19L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0071Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 500, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0070Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 520, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0069Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 400, STR 22L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND RJan 8, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA0067Doubler · debondedFOUND INTERNAL DOUBLER DISBONDED ON FUSELAGE SKIN AT B.L. 0, STRINGER 30 AT STA 700 TO STA 720. REMOVED AND REPLACED DOUBLER IAW SRM 53-30-3 AND SRM 51-30-2.Jan 8, 2006 · N498FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 06FDEA00054Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 420, STR 8-9L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IJan 6, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA00053Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 25L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS CLAJan 6, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA00042Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 1 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 11, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA00041Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 4 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR 06FDEA00040Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 3 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, TYPE, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAIJan 5, 2006 · N498FE · Boeing 727232 · Aircraft StructuresSDR C7WA200500125Indicator · intermittentAIR RETURN. IB FLAP STUCK AT 15 DEGREES, AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. (K)Dec 21, 2005 · N511PE · Boeing 727232 · Trailing Flap Position Indicating SystemSDR C7W2006F00000Indicator · intermittentAIR RETURN. IB FLAP STUCK AT 15 DEGREES AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD.Dec 21, 2005 · N511PE · Boeing 727232 · Trailing Flap Position Indicating SystemSDR 05FDEA03591Fitting · brokenLEFT MLG LOWER TRAILING EDGE PANEL ATTACH BRACKET COMMON TO THE NR 7 SPOILER ACTUATOR FITTING IS BROKEN. REPAIRED L/H T/E CHORD PER FED-EX E.A. 7-5710-91398.Oct 30, 2005 · N499FE · Boeing 727232 · Wing, Attach FittingsSDR 05FDEA03331Rib · crackedR/W I/B MID FLAP TE RIB IS CRACKED AT IB AFT FLAP PUSHROD CUT OUT. REMOVED CRACKED SECTION & INSTALLED NEW SECTION IAW SRM 51-40-4.Oct 10, 2005 · N499FE · Boeing 727232 · Trailing Edge FlapsSDR 05FDEA03177Stringer Clip · crackedSTA 1110 STR 28R STRINGER CLIP CRACKED. REPLACED STRINGER CLIP AT B.S. 1110 STR 28R PER SRM 51-30-2.Sep 30, 2005 · N499FE · Boeing 727232 · Fuselage Main, Attach FittingsSDR 05FDEA03176Fitting · corrodedLEFT FWD EMERGENCY ESCAPE DOOR, ACCESS HANDLE CLOSURE FRAME CORRODED. REPLACED LT FWD EMERGENCY ESCAPE DOOR ACCESS HANDLE CLOSURE FITTING PER SRM 51-30-2.Sep 30, 2005 · N499FE · Boeing 727232 · Emergency ExitsSDR 05FDEA03144Floorbeam · corrodedCORROSION AT BS 950 LBL 48-53 WL 207 AT UNDERSIDE OF FLOORBEAM . ALL WORK ACCOMPLISHED IAW FED EX EA 7-5310-91391.Sep 27, 2005 · N499FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 05FDEA03143Floorbeam · corrodedCORROSION AT FLOORBEAM BS 950 RBL 48-54 WL 208 AT NUT PLATE HOLES. REPAIRED FLOORBEAM PER FED EX EA 7-5310-91395.Sep 27, 2005 · N499FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 05FDEA03142Floorbeam · corrodedREMOVAL OF BL 0 TENSION STRAP ON FED EX CARD, FOUND CORROSION ON LWR FLANGE OF FLOORBEAM AT B/S 1148, WL 200 BL 0. REPAIRED FLOORBEAM AT B.S. 1148, BL0, WL 200 PER SRM 53-10-8.Sep 27, 2005 · N499FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 05FDEA03121Skin · missingMAIN CARGO DOOR LOWER AFT CORNER HAS A PIECE OF EXTERIOR SKIN MISSING. REPAIRED MAIN CARGO DOOR SKIN PER FED EX EA 7-5230-93692ASep 26, 2005 · N499FE · Boeing 727232 · Cargo/Baggage DoorsSDR 05FDEA03073Floorbeam · corrodedCORROSION ON TOP FLOORBEAM BS 560 BL 0 TO RBL 50 AROUND NUT PLATES HOLES. REPAIRED FLOORBEAM IAW SRM 53-10-1.Sep 23, 2005 · N499FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 05FDEA03074Keelbeam · crackedFOUND CRACK IN THE DELTA KEELBEAM LWR FLANGE AT B/S 805 RBL 6 WL 148. REPAIRED DELTA KEELBEAM, BS 805, RBL6, WL 148 PER FED-EX EA 7-5310-91384.Sep 23, 2005 · N499FE · Boeing 727232 · Fuselage Main, KeelSDR 05FDEA03060Frame · corrodedCORROSION, FWD CARGO BAY (C53-111-01(2)) ON FRAME BS 660 BETWEEN BL 0 AND STRINGER 38RT (ON FWD SIDE OF FRAME). REPAIRED FRAME AT BS 660 BETWEEN BL0 AND STR 28RT IAW SRM 51-40-2.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03059Frame · dentedFORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 560 BETWEEN STRINGER 24 LT AND 25 LT. REPAIRED FWD CARGO BAY FRAME AT BS 560 BETWEEN STR 24LT & 25LT PER SRM 51-40-3.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03057Frame · dentedFWD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STR 22 LT AND 25 LT. REPAIRED PER SRM 53-10-1, 51-30-2, 51-40-3 FIG 1 MAJOR REPAIR.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03058Frame · dentedFORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STRINGER 24 RT AND 26RT. REPAIRED FRAME AT B.S. 520 STR 24R & 26R PER SRM 51-40-3.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03056Frame · dentedDENT IN FRAME BETWEEN STR 24R-25R BS 660. REPAIRED DENT IN FRAME AT B.S. 660, STR 24R-25R PER SRM 51-40-3.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03055Frame · dentedDENT IN FRAME AT BS 660 STR 24L. REPAIRED DENT IN FRAME AT B.S. 660 STR 24L PER SRM 51-40-3.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03054Frame · dentedFORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 680 STRINGER 25 RT. REPAIRED FRAME AT BS 680 STR 25R PER SRM 51-40-3.Sep 22, 2005 · N499FE · Boeing 727232 · Fuselage Main, FrameSDR 05FDEA03038Floorbeam · corrodedUPON REMOVAL OF BL "0" TENSION STRAP ON FEDEX CARD, FOUND CORROSION ON LOWER FLANGE OF FLOORBEAM AT BS 1148, WL200, BL'0'. REPAIRED FLOORBEAM AT B.S. 1148, BLO, WL 200 PER SRM 53-10-8.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 05FDEA03037Beam · corrodedCORROSION ON TOP LONGITUDINAL BEAM BS 760 TO 848.95 LBL 25 WL 208. REPAIRED PER SRM 53-10-1, 53-10-2.Sep 21, 2005 · N499FE · Boeing 727232 · Fuselage Miscellaneous Structure
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