Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA0859Frame · corrodedFRAME STA 950F STRINGER 29L, CORROSION. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR STA 950F AT S29L ALL IA FX B727 SRM'S 53-10-4 FIG 12,53-10-1,53-10-2 AND 51-10-2 SNRM N00990.Feb 27, 2006 · N494FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0858Shear Tie · corrodedFWD PIT SHEAR TIE STA 700 BETWEEN STRINGER 28L AND 27L IS CORRODED. REMOVED AND REPLACED WITH NEW SHEAR TIE AT STA 700 BETWEEN S28L AND 27L IAW SRM B727 51-30-5 AND 51-30-2. SNRM N01051.Feb 27, 2006 · N494FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0845Stringer · corrodedINTERIOR FUSELAGE, STR 4R HAS CORROSION FROM BS 620 TO BS 720E. *S/D* REPAIRED STRINGER AT BS 620 TO BS 720E STR 4R IAW SRM 53-10-3 FIG 3.Feb 26, 2006 · N488FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA0846Skin · unknownREMOVE AND REPLACE SKIN FROM BS 680 TO 740 STR 4L TO 4R. *S/D* REMOVED AND REPLACED SKIN AT BS 680 TO 740 STR 4L TO 4R IAW SRM 51-30-2, 51-10-2.Feb 26, 2006 · N488FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0840Failsafe · damagedFOUND FAIL SAFE SEVERED AT BS 950C FRAME, BL 0.Feb 24, 2006 · N492FE · Boeing 727200 · Fuselage Main, StructureSDR 06FDEA0838Shear Tie · corrodedAFT CARGO BAY, CORROSION ON SHEAR TIE BS 950C BETWEEN LEFT KEEL BEAM AND LBL 0.Feb 24, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0841Repair · unknownEXTERNAL DOUBLER REPAIR APPROX 8 X 12 INCHES. LT AFT FUSELAGE STA 1050 STRINGER 19L TO 20L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-96607Feb 24, 2006 · N492FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0839Sill · damagedBS 618-623 MCD CUTOUT I/B SILL UPPER SURFACE HAS HOLES WITH LESS THAN 2D EDGE MARGIN. COMPLIED WITH E.A. 7-5310-98572Feb 24, 2006 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA0815Floorbeam · corrodedCORROSION ON FLOORBEAM LWR FLANGE BS 720 LBL30-RBL37. REPLACED WITH NEW FLOOR BEAM PER SRM 51-10-2, SRM 51-30-5 & 51-30-2.Feb 23, 2006 · N492FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0817Shear Tie · corrodedBS 720 STR 28 LT TO STR 28 RT FRAME TO SKIN ATTACH STRUCTURE IS CORRODED. *S/D* REMOVED AND REPLACED FRAME TO SKIN ATTACH STRUCTURE STA 720 STR 28L TO STR 28R IAW SRM 53-10-4 AND SRM 51-30-2.Feb 23, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0816Stringer Clip · corrodedN00370 STRINGER CLIP AT BS 804 AND STR 4R HAS SURFACE CORROSION. REMOVED AND REPLACED STR CLIP BS 804 STR 4R IAW SRM 51-10-1.Feb 23, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0805Angle · damagedMAIN WHEEL WELL RBL-8 BS-870 WL-150 CORNER ANGLE ON AFT SIDE OF BS 870 DAMAGED. REPARIED DAMAGED ANGLE PER SRM 51-30-2.Feb 22, 2006 · N492FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA0804Stringer · corrodedN00364 STR 2R HAS SURFACE CORROSION BETWEEN BS 740- BS 826. REMOVED AND REPLACED STR 2R BS 740-870 IAW SRM 53-10-1, 51-30-2, 51-20-1 AND 51-10-2.Feb 22, 2006 · N488FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 72300253Warning Light · illuminatedFIRE WARNING LIGHT ILLUMINATED IN FLIGHT NR 1 ENG. FIRE PULLED, ENGINE FIRE SWITCH. RETURNED TO DAY.Feb 22, 2006 · N723CK · Boeing 727200 · Fire DetectionSDR 06FDEA0800Skin · corrodedFWD PIT STA 680 FROM STRINGER 27R TO 28R SKIN IS CORRODED. FABRICATED, ALODINED, PRIMED AND INSTALLED FUS SKIN REPAIR AT STA BS 680-690 AND STRINGER 27R TO 28R ALL IAW FX SRM'S 53-30-3 FIG 3, 53-30-1, 53-30-2,51-30-2 AND 51-10-2. SNRM N01070.Feb 21, 2006 · N494FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0782Stringer Clip · corrodedSTRINGER CLIP AT BS 784 AND STR 4R HAS SURFACE CORROSION. REPLACED STR CLIP PER SRM 51-30-2.Feb 20, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0781Stringer · corrodedINTERIOR FUSELAGE, STR 3R HAS CORROSION FROM BS 700 TO BS 740. *S/D* REPAIR TO STRINGER TO BE ACCOMPLISHED ON NRC N00880 PER SRM 53-10-1.Feb 20, 2006 · N488FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA0780Rib · chafedNR 2 SLAT I/B END RIB HAS CHAFING DAMAGE. *S/D* REPAIRED I/B RIB IAW SRM 51-30-2.Feb 20, 2006 · N488FE · Boeing 727200 · Leading Edge DevicesSDR 06FDEA0779Floorbeam · corrodedCORROSION ON FLOORBEAM BS 720 RBL 10 LWR FLANGE AT NUT PLATE HOLES. *S/D* REPAIRED PER FED EX SRM SR27-53-034.Feb 20, 2006 · N488FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0783Skin · unknownFILLED PILOT HOLES IN HAYES DOUBLER EXTERNAL SKIN, BS 620-720, STR 26L-27L. REPAIRED PER EA 7-5330-99479.Feb 20, 2006 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0736Web · crackedWHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. REPAIRED PER FED EX EA 7-5530-96598.Feb 19, 2006 · N488FE · Boeing 727200 · Vertical Stabilizer Miscellaneous StructureSDR 06FDEA0735Frame · dentedBS 1010, STR 25 - STR 26L FRAME AT BS 1010, STR 25L-26L IS DENTED. REPAIRED FRAME WITH DOUBLER PER SRM 51-40-3.Feb 19, 2006 · N492FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0734Stringer Clip · crackedSTA 400 STR 7L, STR CLIP IS CRACKED. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 400 STR 7L PER SRM 51-30-2. ITEM INSPECTED NOT ACCEPTED, SEE N01412 MAJOR REPAIR.Feb 19, 2006 · N492FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0718Sill · damagedBS 481 MCD CUTOUT I/B SILL UPPER SURFACE FILLER HAS FASTENER HOLE WITH NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5310-98583.Feb 17, 2006 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA0717Skin · gougedFUSELAGE EXTERIOR SKIN HAS 1 INCH GOUGE AT STA 380 AND STRINGER 15L. FABRICATED, ALODINED, PRIMED AND INSTALLED FUS EXTERIOR DOUBLER AT STA 380 AND S15L ALL IAW FX B727 SRM REF'S 53-30-3 FIG 3A, 53-30-2, 53-10-1 AND 51-10-2.Feb 17, 2006 · N494FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0716Stringer · corrodedFWD PIT AT STA 490 STRINGER 26L HAS CORROSION AT SPLICE. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER 26L REPAIR AT STA 490 ALL IAW FX B727 SRM REF'S 53-10-3 FIG 1, 51-10-6, 51-10-2 AND 51-30-2.Feb 17, 2006 · N494FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA0701Floorbeam · corrodedAFT CARGO BAY, CORROSION ON BS 1148 FLOORBEAM LWR CHORD AT NUT PLATE HOLES RBL 25 - LBL 45, WL 200. *S/D* REPAIRED BS 1148 FLOORBEAM LWR CHORD RBL 3 - RBL 20 AND LBL 1 - LBL 32 IAW SRM 53-10-8 FIG 2.Feb 16, 2006 · N492FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0696Floorbeam · corrodedAFT CARGO BAY, CORROSION IN AND AROUND NUT PLATE HOLES ON LWR CHORD OF BS 950D FLOORBEAM, BL 0 - LBL 45, WL 200. *S/D* REPAIRED BS 950D FLOORBEAM LWR CHORD BL 0 - LBL 45 IAW SRM 53-10-8 FIG 2.Feb 16, 2006 · N492FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0700Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIP 4R HAS CORROSION BS 720A. REMOVED CORRODED STR CLIP & WILL BE REPLACED ON N00343.Feb 16, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0699Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 720B STR 4 RT. REPLACED STR CLIP PER SRM 51-30-2.Feb 16, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0698Stringer · corrodedCORROSION ON STR 4 RT BS 700 TO BS 720C. REMOVED CORROSION FROM STR 4 R/H BS 700 TO 720C, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. STRINGER SECTION TO BE REPLACED ON N00343 BS 620-720E.Feb 16, 2006 · N488FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA0697Repair · unknownEXISTING EXTERNAL REPAIR AT BS 393 WL 228 APPROX 16.5 X 9.5 INCH REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER EA 7-5330-98567Feb 16, 2006 · N492FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0693Stringer · crackedLEFT WING INTERNAL FUEL CELL, UPPER STIFFENER 9 IS CRACKED AT WS 656.50. REPAIRED PER FED EX EA 7-5710-96588.Feb 15, 2006 · N488FE · Boeing 727200 · Wing, Longeron/StringerSDR 06FDEA0694Unknown · misdrilledBS 600 STR 18 LT HAS ONE DRILL START AND ONE MISSING FASTENER. *S/D* CUT OUT DAMAGED STR 18 LT BS 651 - 670, REPAIRED STR PER SRM 53-10-3.Feb 15, 2006 · N492FE · Boeing 727200 · Fuselage Main, StructureSDR 06FDEA0692Frame · misdrilledSTA 660 STR 25 LT TWO DOUBLE DRILLED HOLES THROUGH FRAME AND DOUBLER. *S/D* REMOVED DAMAGED DOUBLER AND DAMAGE ON FRAME AT STA 660 STR 25 LT, FABRICATED NEW DOUBLER, INSTALLED IAW SRM 51-40-03, 51-20-02 AND FED-EX MM 51-20-151 MAJOR REPAIR.Feb 15, 2006 · N488FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0657Shear Tie · corrodedBS 680 BETWEEN STR 28RT AND STR 28LT SHEAR TIE IS CORRODED. *S/D* REPAIRED SHEAR TIE BS 680 BETWEEN STR 28 RT AND STR 28 LT IAW SRM 53-10-4.Feb 13, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0674Flap Track · corrodedLEFT WING, NR 3 FLAP TRACK IS CORRODED AT THE SPOILER BEAM MOUNT AND THE MAIN MOUNT PADS. *S/D* REMOVED AND REPLACED CORRODED LT WING NR 3 FLAP TRACK IAW CARD 27X5705-01 AND CARD 27X5705-03.Feb 13, 2006 · N488FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA0673Shear Tie · corrodedBS 700 STR 28 RT SHEAR TIE IS CORRODED. *S/D* REPLACED SHEAR TIE AT BS 700 STR 28 RT IAW SRM 51-30-2 AND 51-30-5.Feb 13, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0655Flap Track · crackedRIGHT WING NR 6 FLAP TRACK CORRODED AT SPOILER BEAM PAD, MAIN MOUNTING PAD AND CRACKS EMMITTING FROM FAILSAFE BOLT HOLE. *S/D* REMOVED & REPLACED NR 6 FLAP TRACK PER FED EX CARD 27X5708-01 & 27X5708-03.Feb 13, 2006 · N488FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA0654Flap Track · corrodedNR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REPLACED PER CARD 27X5706-03.Feb 13, 2006 · N488FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA0656Skin · chafedCHAFE AT BS 720E RBL 48 WL 178 EXT SKIN JUST FWD OF RT LANDING LIGHT.Feb 13, 2006 · N488FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0646Repair · unknownEXTERNAL FLUSH REPAIR APPROX 2.5 X 2.5 INCH RT LWR FUSE STA 302 STRINGER 24R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED PER SRM 53-30-3, 51-30-2 MAJOR REPAIR.Feb 10, 2006 · N488FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA0645Shear Tie · corrodedCORROSION ON SHEAR TIE BS 1050, STR 26L - 27L. *S/D* REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-2 AND SRM 51-10-2.Feb 10, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA0644Skin · dentedSKIN FWD OF TAIL STAND JACK ACCESS DOOR DENTED. *S/D* REMOVED AND REPLACED SKIN IAW SRM 51-30-02.Feb 10, 2006 · N488FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA0580Floorbeam · corrodedFLOORBEAM IS CORRODED ON LWR FLANGE AT NUT PLATE HOLE BS 640 RBL 48. REPAIRED PER SRM 53-10-8 MAJOR REPAIR.Feb 7, 2006 · N488FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0582Frame · misdrilledSTA 400 STR 8L, DRILL STARTS ON FRAME WEB. DRILL STARTS STA 400 STR 8L ON FRAME WEB FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, INSTALLED REPAIR ON FRAME REF SRM 53-10-4 FOUND TO BE A MAJOR REPAIR.Feb 7, 2006 · N492FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0592Repair · unknownFOUND REPAIR LOCATED ON NR 2 L/E SLAT. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA (LEFT WING).Feb 7, 2006 · N487FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA0591Repair · unknownFOUND REPAIR LOCATED AT STATION 188, FORWARD OF NOSE ACCESS DOOR REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA0590Repair · unknownFOUND REPAIR LOCATED AT STA 660, STR 30. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA0589Repair · unknownFOUND REPAIR AT STA 259.5 STR 17L, REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Feb 7, 2006 · N487FE · Boeing 727200 · Standard Practices/Structures
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