Boeing 727-200

Service difficulty reports · 2,835

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 06FDEA1572Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1070, STR 21R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVE EXISTING REPAIR AND FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6Apr 24, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1567Repair · misinstalledFUSELAGE SKIN REPAIR AT FS 1140 & STR 19L DOES NOT COMPLY WITH SRM REPAIR. REMOVED AND REPLACED EXISTING REPAIR DOUBLERS IAW SRM 53-30-3 FIG 5.Apr 22, 2006 · N468FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1561Tie · corrodedFOUND RT FWD HORIZONTAL TENSION TIE O/B FITTING LUG, O/B FACE IS CORRODED. REPAIRED PER EA 7-5530-96626.Apr 20, 2006 · N485FE · Boeing 727200 · Vertical StabilizerSDR 06FDEA1493Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT FWD CARGO COMPT DOOR EXTERNAL SKIN IS NOT CONFORMED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 52-00-3, INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEApr 18, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1478None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 277 STR 20R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1477Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT AFT LOWER CARGO COMPT DOOR WAS NOT CONFORMED TO FAA APPROVED DATA, PERFORMED REPAIR IAW SRM 52-00-3 FIG 3 AND SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.Apr 16, 2006 · N491FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA1476None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 243 STR 20R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1475None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 320 STR 21R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX Apr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1474None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 675 STR 18R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1473Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 685 STR 29R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR ISApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1472Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT AFT EDGE OF AFT LOWER CARGO DOOR CUTOUT WAS ACCOMPLISHED IAW EA 7-5330-56260 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1471Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950D STR 29R WAS ACCOMPLISHED IAW EA 7- 5310-27736 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1470Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 970 STR 29R WAS ACCOMPLISHED IAW S/B 727-53-0179 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLAApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1469Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 27R WAS ACCOMPLISHED IAW EA 7- 5330-70493 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1468Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1130 STR 30 WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CApr 16, 2006 · N491FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1453Skin · puncturedUPPER RUDDER L/E SKIN HAS PUNCTURE AT LT SIDE AT RUDDER STA 160. REPAIRED PUNCTURE ON UPPER RUDDER L/E SKIN AT LT SIDE AT RUDDER STA 160 IAW EA 7-5530-96539.Apr 14, 2006 · N485FE · Boeing 727200 · Rudder, Plate/SkinSDR 06FDEA1424Skin · corrodedCORROSION ON FUSELAGE SKIN FROM BS 480-681 S4L &R. REPAIRED PER EA 7-5330-99457.Apr 12, 2006 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA1398Skin · dentedFORWARD LEFT FUSELAGE HAS DENT OUTER SKIN APPROX STA 196 STR 25L.Apr 12, 2006 · N468FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA1303Structure · dentedUPPER RUDDER TRAILING EDGE DENTED LEFT HAND LOWER 6 INCHES FROM BOTTOM. *S/D* REMOVED AND REPLACED FAIRING STRIP LOWER LT SIDE PER FED EX EA 7-5540-99063.Apr 3, 2006 · N492FE · Boeing 727200 · Rudder StructureSDR 06FDEA1302Structure · nickedUPPER RUDDER TRAILING EDGE HAS NUMEROUS NICKS LEFT HAND. *S/D* REMOVED AND REPLACED FAIRING STRIP UPPER LT SIDE PER FED EX EA 7-5540-99063.Apr 3, 2006 · N492FE · Boeing 727200 · Rudder StructureSDR 06FDEA1301Structure · nickedUPPER RUDDER TRAILING EDGE HAS NUMEROUS NICKS RIGHT HAND. REMOVED AND REPLACED FAIRING STRIP RT SIDE PER FED EX EA 7-5540-99063.Apr 3, 2006 · N492FE · Boeing 727200 · Rudder StructureSDR 06FDEA1272Floorbeam · corrodedMAIN DECK FLOORBEAM AT STA 620 BETWEEN LBL 45 TO RBL 24.5 HAS CORROSION. REMOVED DAMAGED FLOORBEAM IAW SR 27-53-034, FABRICATED FILLER PLATE, ANGLES, BRACKET AND FLOORBEAM IAW SR 27-53-034, REINSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND SR 27-53-034, REPAIRMar 30, 2006 · N266FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA1271Floorbeam · corrodedMAIN DECK FLOORBEAM AT STA 560, LBL 62 TO RBL 24.5 HAS CORROSION, AFTER CORROSION REMOVAL FOUND OUT OF LIMITS. REMOVED FLOORBEAM IAW SRM 51-30-2 AND SRZ 27-53-034, FABRICATED FLOORBEAM SECTION IAW SR 27-53-034 AND REINSTALLED ALL REPAIR PARTS IAW SRM 51-30-2,Mar 30, 2006 · N266FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA1265Clamp · out of positionAT FLT LEVEL 320 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, WENT TO QRH TURNED RIGHT PACK SWITCH OFF, LIGHT STILL ON. CLOSED NR 3 BLEED LIGHT STILL ON. CLOSED CARGO HEAT SWITCH LIGHT STILL ON. WHEN NR 3 THRUST LEVER RETARDED LIGHT WENT OUT. WING ANTI-ICE WMar 29, 2006 · N275FE · Boeing 727200 · Pneumatic Distribution SystemSDR 06FDEA1264Fuel Control · unknownON TAKEOFF ROLL, AFTER TAKEOFF POWER WAS SET, N1 AND EPR INCREASED WITHOUT ANY PILOT INPUT. THE NUMBER 3 THROTTLE WAS ADVANCED AHEAD OF OTHER THROTTLES BY 1 KNOB WIDTH. COMPLETED INSTALL OF FUEL CONTROL AND PUMP IAW 727-2 00AMM AND PWMM 73-11-01.Mar 25, 2006 · N467FE · Boeing 727200 · Fuel Control/Turbine EnginesSDR 06FDEA1229Attach Fitting · corrodedNR 1 FLAP TRACK FWD FITTING I/B FACE IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-7-96574.Mar 24, 2006 · N492FE · Boeing 727200 · Wing, Attach FittingsSDR 06FDEA1228Attach Fitting · corrodedNR 8 FLAP TRACK FWD FITTING IS CORRODED. *S/D* REPAIRED PER FED EX EA 7-5710-96574.Mar 24, 2006 · N492FE · Boeing 727200 · Wing, Attach FittingsSDR 06FDEA1227Spar · chafedVERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, LT SIDE. *S/D* REPAIRED PER FED EX EA 7-5530-96617.Mar 24, 2006 · N492FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 06FDEA1226Spar · chafedVERTICAL STAB JACKSCREW COMPARTMENT LWR MID SPAR CHORD CHAFED JUST FWD OF STAB SLIDING SEAL, FIN STA 230, RT SIDE. *S/D* REPAIRED PER FED EX EA 7-5330-96617.Mar 24, 2006 · N492FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 06FDEA1225Indicator · reads lowDURING TAKEOFF, S/O NOTED NR 3 ENG OIL PRESSURE INDICATED LOW 32 PSI. T/O WAS REJECTED AT 80 KIAS, BRAKE COOLING CHART RAN AT 151000 LBS WEIGHT 1000PA 80 KTS EQUAL 16 MIN COOLING TIME. REMOVED AND REPLACED NR 3 OIL PRESS IND IAW 727-200 MM 79-32-000-5, RAN Mar 24, 2006 · N282FE · Boeing 727200 · Engine Oil PressureSDR 06FDEA1266Wire · brokenDURING FLAP RETRACTION AT FLAPS 2 DEG UNSAFE LED INDICATION FOR NR 5 LED. COMPLIED WITH QRH, DIVERTED TO INDY. T/S AND FOUND BURNT/BROKEN WIRE AT WIRE LOOM AFT OF NR 5 KRUEGER FLAP SWITCH ASSY. REPAIRED BROKEN WIRE REF B-727-200 SWP'S CH 20. SYSTEM OPERATEMar 23, 2006 · N499FE · Boeing 727200 · Flight Control System WiringSDR 06FDEA1210Skin · gougedREWORK ON N00140 REQUIRED. LWR LOBE EXTERNAL SKIN, SKIN AFT OF FWD CARGO DOOR HAS GRAVEL GOUGES BETWEEN STR 23R AND 25R. REWORK REQUIRED BECAUSE BLENDING EXTENDS OVER FASTENERS AND FASTENER HOLES. THIS IS NOT ALLOWED PER SRM 53-30-1. *S/D* REPAIRED PER FEMar 23, 2006 · N492FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA1209Skin · damagedEXTERNAL DOUBLER REPAIR APPROX 12.75 X 26.75 INCHES, RT FUSELAGE STA 1010 STRINGER 26R TO 26L REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED PER FED EX EA 7-5330-96615.Mar 23, 2006 · N492FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA1192Skin · dentedWHILE WORKING LWR RUDDER CARD N01322 FOUND DENT AT 2 INCHES FROM LOWER END AT RT CENTER SKIN AREA. *S/D* REPAIRED LOWER RUDDER PER SRM 55-40-1.Mar 22, 2006 · N492FE · Boeing 727200 · Rudder, Plate/SkinSDR 06FDEA1187Beam · damagedWHILE WORKING N01478, FOUND MECHANICAL DAMAGE AROUND UPPER I/B BRACKET ATTACH FASTENER ON FWD FACE OF LT MLG BEAM, JUST AFT OF THE MAIN GEAR STRUT. *S/D* REPAIRED PER FED EX EA 7-5710-96608.Mar 21, 2006 · N492FE · Boeing 727200 · Wing, Landing Gear Attach FittingsSDR 06FDEA1190Rib · corrodedLT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE RIB, O/B LUG, I/B & O/B FACES HAVE FRETTING CORROSION. REPAIRED LT HORIZ STAB, ELEV THRUST HINGE RIB, O/B LUG, I/B AND O/B FACES PER FED EX EA 7-5510-96625.Mar 21, 2006 · N485FE · Boeing 727200 · Horizontal Stabilizer, Spar/RibSDR 06FDEA1185Shear Tie · damagedWHILE WORKING CARD 73C023-00, FOUND VERT FIN AFT SHEAR TIE FITTING TO HAVE MECHANICAL DAMAGE ON LOWER SURFACE AT LEFT AFT VERT BOLT HOLE. *S/D* REPAIRED VERT FIN AFT SHEAR TIE FITTING LWR SURFACE IAW FEDEX EA 7-5530-96604.Mar 21, 2006 · N488FE · Boeing 727200 · Vertical StabilizerSDR 06FDEA1184Shear Tie · corrodedAFT CARGO BAY SHEAR TIE IS CORRODED BS 1166 RBL 3. *S/D* REMOVED AND REPLACED SHEAR TIE BS 1166, RBL 3 IAW SRM 53-10-4 FIG 13.Mar 21, 2006 · N492FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 06FDEA1142Web · crackedCRACK ON BEADED WEB BS 895 RBL 45 WL 203. REPLACED CRACKED BEADED PRESSURE WEB AT BS 895 RBL 45, WL 203 IAW FED EX EA 7- 5310-96584.Mar 17, 2006 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA1048Floorbeam · misdrilledWHILE WORKING ON ATTACHING L-ANGLE FOUND FLOOR BEAM AT BS 720D,WL 208, LBL 64 WITH MISDRILLED HOLE. REMOVED DAMAGE ON FLOORBEAM BS 720D, WL 208, LBL 64 AND REPAIRED IAW FED-EX SR 27-53-034.Mar 14, 2006 · N492FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA1047Repair · noneN01048 LOWER FWD CARGO COMP. FLOOR FRAME REPAIR FUSELAGE STA. 560 LBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ** SD ** COMING REPAIRED FRAME PWR SRM 51-40-3.Mar 14, 2006 · N492FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1046Web · corrodedCORROSION ON WEB BS 720C PLUS 13 LBL 67 WL 208. REMOVED AND REPLACED WEB PER SRM 53-10-02.Mar 14, 2006 · N492FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA1054Shear Tie · corrodedFOUND VERT FIN TENSION TIE RIB, AFT SHEAR FITTING, LWR SURFACE HAS CORROSION. *S/D* REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200 · Vertical StabilizerSDR 06FDEA1053Rib · gougedVERTICAL FIN TENSION TIE RIB, RIGHT FWD VERTICAL BOLT HOLE IS GOUGED. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200 · Vertical StabilizerSDR 06FDEA1052Rib · corrodedVERTICAL FIN TENSION TIE RIB, LT AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIRMar 14, 2006 · N488FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 06FDEA1051Rib · corrodedN00716 VERTICAL FIN TENSION TIE RIB, R/H AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 06FDEA1050Rib · gougedVERTICAL FIN TENSION TIE RIB, LT FWD VERTICAL BOLT HOLE IS GOUGED. COMING REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 06FDEA1049Shear Tie · corrodedWHILE WORKING CARD NO. N00718, FOUND VERT. FIN AFT SHEAR TIE FITTING, UPPER SURFACE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-96604 REPAIR CONSIDERED A MAJOR.Mar 14, 2006 · N488FE · Boeing 727200 · Vertical StabilizerSDR 06FDEA1010Repair · noneEXTERNAL DOUBLER REPAIR LEFT HORIZONTAL STAB UPPER T/E PANEL, APPROX 4 X 4 INCHES. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Mar 12, 2006 · N492FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1009Skin · puncturedWHILE WORKING FEDEX CARD N01048 FOUND SKIN PUNCTURE BS 680 PLUS 10 INCHES ABOVE STR 25L. *S/D* REMOVED DAMAGE FROM SKIN BS 680 PLUS 10 INCHES ABOVE STR 25L, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 1.Mar 12, 2006 · N492FE · Boeing 727200 · Fuselage Main, Plate/Skin
Back to Boeing 727-200