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 03FDEA01572Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 1070, RBL 10.5, WL 208. **SD** COMINGSep 18, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01577Floorbeam · corrodedCORROSION ON FLOOR BEAM UPR SURFACE BS 328, LBL 29, WL 208. **SD** COMINGSep 18, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01556Precooler · crackedENG NR 1 STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF FROM PHX. ENG ANTI ICE WAS NOT ON. WITH REDUCTION OF POWER TO QUIET EPR LIGHT WENT OUT. LIGHT WAS ON FOR A TOTAL OF 15 SECONDS. SYSTEM TESTED GOOD. CONSULTED QRH. NO FURTHER ACTION TAKEN. FOUND LEAK ATSep 17, 2003 · N207FE · Boeing 727200 · Pneumatic Distribution SystemSDR 03FDEA01543Indicator · false indicationON DEPARTURE WHEN THE GEAR HANDLE WAS PUT UP THE GEAR CAME UP NORMAL THE RED GEAR DOOR LIGHT STAYED ON, GREEN GEAR LIGHTS OFF AND S/O PANEL ALL LIGHTS SHOWED NORMAL. CYCLE GEAR ONCE SAME INDICATION. PULLED GEAR INDICATION CB'S AND RECYCLED GEAR NORMAL INSep 16, 2003 · N499FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01544Accessory Unit · false indicationLANDING GEAR LEVER LATCH FAILED TO RELEASE DURING GEAR RETRACTION. THE QRH PROCEDURE ON PAGES 2-6-2-12 /13 COMPLIED WITH. LANDING GEAR FAILED TEST NR 1 OF THE PROCEDURE. WHEN THE FLAPS WERE RETRACTED FROM 5 TO 2 DEGREES. AN INTERMITTENT HORN SOUNDED. AN ESep 16, 2003 · N478FE · Boeing 727200 · Landing Gear Retraction/Extension SystemSDR 03FDEA01555Sensor · failedAT FL270 AND .84 MACK, THE RED AND GREEN RIGHT GEAR LIGHTS ILLUMINATED. THE LANDING GEAR HANDLE WAS PLACED UP. ALSO THE LEFT GREEN GEAR LIGHT WOULD NOT TEST INFLIGHT. PER FLIGHT CREW DEBRIEF: WHEN GEAR HANDLE WAS MOVED FROM "OFF" TO "UP" THERE WAS NO Sep 13, 2003 · N487FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01522Floorbeam · corrodedCORROSION ON FLOORBEAM BS 328 LBL 18 TO LBL 30 WL 208.Sep 12, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01521Floorbeam · corrodedCORROSION ON STRAP LOWER SURFACE OF UPPER FLANGE OF BS 950 FLOORBEAM RBL 45 WL 208.Sep 12, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01499Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1030 RBL 25-0 WL 208 INSTALLED REPAIR PARTS PER/ UPPER CHORD PER SRM 53-10-8Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01502Stringer · crackedSTR 15L CRACKED AT 720B 4. REPAIRED IAW SRM 53-10-3 FIG 5Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01501Stringer · crackedN01557 STR CRACKED B/S 720B 15 STR 15L. REPAIRED IAW SRM 53-10-3 FIG 5.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01504Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER CHORD UNDER NUTCLIP. REPAIRED IAW SRM 53-10-8.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01503Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE UPPER & LOWER SURFACE AT NUTCLIP HOLES STA 950D LBL 10 & 21 WL 208. CUT OUT FLOORBEAM & REPAIRED PER SRM 53-10-8.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01506Frame · crackedFRAME CRACKED BS 360 LBL 2 WL 155. CUT-OUT CRACK DAMAGE ON FRAME PER 727 SRM 51-10-1. FABRICATED REPAIR ANGLE FROM 7075T6 .050, LOT 508357 PER 727 SRM 51-40-3. LOCATED & DRILLED ANGLE PER 727 SRM 51- 40-3. ALODINED, PRIMED & PAINTED ANGLE PER 727 SRM 51-1Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01505Floorbeam · damagedSTA 950F LBL 97 TO 54 WL 208 FLOORBEAM HAS DAMAGE ON UPPER FLANGE. TOOLING MARKS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER SRM 51-30-5, 53- 10-1, & FED EX EA 7-5310-54997, BS 950F, LBL 35 - 65, WL 208.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01508Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 720B, STRINGER 7 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP AT BS 720B, STRINGER 7 RT.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01507Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 LBL 32 AND 37 WL 208. REMOVED DAMAGED AREA OF FLOORBEAM, FABRICATED REPAIR ALODINED, PRIMED, PAINTED & INSTALLED REPAIR IAW SRM 53-10-8 FIG 10 BS 1130 LBL 32-38 WL 208.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01510Stringer · damagedDAMAGED STRINGER BS 647 STR 21R. CUT OUT DAMAGE & REPAIRED PER SRM 51-10-3 FIG 1Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01509Skin · dentedCREASED & DENTED SKIN , BS 620 TO BS 640 STR 21. CUT OUT DAMAGED SKIN BS 620 TO 640 STR 21 RT 4.3 X 19.7 AND INSTALLED REPAIR DOUBLER TRIPLER AND FILLER IAW FEDEX EA 7-5330-70507.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01512Stringer Clip · crackedCRACKED STRINGER CLIP, BS 720F, STR 4 RT. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720F, STR 4R PER SRM 51-30-2.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01511Floorbeam · corrodedCORROSION BS 1070, WL 201, LBL 25-45 AROUND AND IN NUT CLIP HOLES. CORROSION ON FLOORBEAM BS 1070, WL 201, LBL 25-45 AROUND END IN NUT CLIP HOLES FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOOR BEAM IAW SRM 53-10-8.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01514Stringer Clip · crackedN1550 CRACKED STRINGER CLIP, BS 720, STR. 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720, STR. 5R PER SRM 51-30-02.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01513Stringer Clip · crackedSTA 950D, STRINGER 2L CLIP IS CRACKED. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950D, STR 2L PER SRM 51-30-2.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01516Stringer · crackedN01548 CRACKED STRINGER, BS 720B 4 STR 15R. REMOVED DAMAGED PORTION OF STR 15R AT BS 720B 4 IAW SRM 53-10-3 FIG 5. HFEC INSPECTION ON PERPHERY OF CUTOUT NO CRACKS NOTED. FABRICATED ALODINED, PRIMED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 FIG 5.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01515Stringer Clip · crackedN01551 CRACKED STRINGER BS 720 STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP, BS 720 STR 5R PER SRM 51-30-02.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01500Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CHORD, STA 340, RBL 4 WL 208.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01517Frame · dentedAFT CARGO FRAME DENTED BS 950F AT STR 23L.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01518Floorbeam · corrodedCORROSION ON FLOORBEAM UPR FLANGE UPR SURFACE STA. 1010 RBL 25-45 WL 208.Sep 11, 2003 · N221FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01472Skin · dentedDENT ON SKIN BS 359 BETWEEN STR 19-20 LT. REPAIR PER ER 03-3244 AND EA 7-5330-72319.Sep 9, 2003 · N220FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01468Door Frame · crackedMAIN CARGO DOOR STUB FRAME IS CRACKED AT O/B FLANGE THRU FASTENER HOLE, 69 INCHES AFT OF FWD FRAME 3 INCHES BELOW UPR FRAME. REPLACED PER SRM 51-30-2.Sep 9, 2003 · N220FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01469Structure · corrodedCORROSION ON STRUCTURE IN NLG BAY AT BS 284 RBL 18 INSIDE TORQUE BOX O/B OF STRUT DOOR FWD HINGE. REMOVED AND REPLACED PER SRM 51-30-2.Sep 9, 2003 · N220FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01470Door Frame · crackedMAIN CARGO DOOR STUB FRAME IS CRACKED AT O/B FLANGE THRU FASTENER HOLE 49 INCHES AFT OF FWD FRAME, 3 INCHES BELOW UPPER FRAME. REMOVED AND REPLACED PER SRM 51-30-2.Sep 9, 2003 · N220FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01471Rib · crackedCRACK INDICATION NOTED AT BS 760 WL 208 RBL 70.5 IN THE FWD UPPER HOLE COMMON TO THE RIB CHORD UPPER VERTICAL FLANGE IN THE RIB CHORD LAYER AT THE 12 O'CLOCK POSITION. REPAIRED PER EA 7-5710-54691 AND EO 7-5710-7-2308 I PT 3.Sep 9, 2003 · N220FE · Boeing 727200 · Wing Main, Frame StructureSDR 03FDEA01467Switch · false indicationENGINE NR 3 OVERHEAT LIGHT ILLUMINATED ON CLIMB OUT REFRENCED JRH AND CLOSED THE RIGHT WING ANTI-ICE SWITCH. LIGHT WENT OUT AND STAYED OUT FOR REMAINDER OF FLIGHT. CHECKED DUCTS AND CLAMPS ON NR 3 ENGINE OPS CHECK SYSTEM USING APU POWER IAW SMP. COULD NOT Sep 9, 2003 · N463FE · Boeing 727200 · Overheat DetectionSDR 03FDEA01461Attach Fitting · corrodedNR 5 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED AT BORE COMMON TO THE TRUNNION STUD. CLEANED AREA AND REINSPECTED AREA IAW BOEING SOPM 20-30-03. NO CORROSION NOTED AFTER CLEANING.Sep 8, 2003 · N233FE · Boeing 727200 · Trailing Edge FlapsSDR 03FDEA01462Tee Fitting · gougedRT MLG I/B FORWARD TRUNNION MOUNT FITTING GOUGED. REPAIRED FORWARD TRUNNION MOUNT IAW FEDEX EA 7-5740-54980 DATED 09/17/03. REFERENCE SNRM N00419 / WO 00023911Sep 8, 2003 · N233FE · Boeing 727200 · Wing, Landing Gear Attach FittingsSDR 03FDEA01453Warning Light · illuminatedDURING CLIMBOUT AT FL180, LIGHT CHOP, AFT AIRSTAIR AMBER LIGHT ILLUMINATED, AND REMAINED ON, COMPLIED WITH QRH. INSPECTED AFT AIRSTAIR WARNING INDICATION AND STAIR POSITION MICROSWITCHES IAW M/M 52-62-001-6-1, A (11). NO DEFECTS FOUND. FLIGHT CREW REPORTESep 6, 2003 · N209FE · Boeing 727200 · Door Warning SystemSDR 03FDEA01452Clamp · leakingON CLIMBOUT, FROM MEM NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH. LIGHT EXTINGUISHED. FOUND CLAMP BETWEEN SHUTOFF VALVE AND PRECOOLER LEAKING. REMOVED AND REPOSITIONED CLAMP IAW SMP PERFORMED ENGINE IAW JRH. LEAK CK. GOOD. RE-INSTALL LOSep 4, 2003 · N207FE · Boeing 727200 · Pneumatic Distribution SystemSDR 03FDEA01439Accessory Unit · false activationDURING CONFIGURATION TO LAND AFTER PLACING LANDING GEAR LEVER DOWN ALL LIGHTS REMAINED ILLUMINATED ON GEAR ANNUNCIATOR PANEL, REDS AND GREENS. RECYCLED GEAR IAW QRH AND AGAIN ALL LIGHTS REMAINED ILLUMINATED. RECYCLED AGAIN AND GOT A SAFE 3 GREEN INDICATION ASep 4, 2003 · N216FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01438Position Switch · inoperativeNOSE GEAR UNSAFE LIGHT CAME ON AND FLICKERED DURING T/O ROLL WITH A STEADY GREEN. NOSE GEAR DOWN AND LOCKED LIGHT DOORS LIGHT AND S/O NOSE GEAR DOOR LIGHT REMAINED OFF ALL LIGHTS WENT OUT NORMALLY DURING GEAR RETRACTION. OKAY ON LANDING. REMOVED NOSE GSep 4, 2003 · N479FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01437Clamp · looseWHILE DEPARTING LAS, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED FOR (TEMP 37C) APPROX 15 SECONDS DURING INTIAL TAKE-OFF/ CLIMBOUT AT 180 KTS PRIOR TO FLAP RETRACTION, THEN EXTINGUISHED. SYSTEM TESTED OK REFERRED TO QRH AND CONTINUED. FOUND CLAMPS ON ENGINE BSep 4, 2003 · N207FE · Boeing 727200 · Pneumatic Distribution SystemSDR 03FDEA01407Stiffener · chafedAFT STIFFNER IS CHAFED AT NR 6 LT NACELLE, ATTACH POSITION ABOVE NR 2 ENGINE BS 1456. REMOVED AFT STIFFENER, FABRICATED, DRILLED, ALODINED, PRIMED AND RE-INSTALLED RIBS AND STIFFENER AT BS 1456 AND 1459 AT NR 6 LT COWL ATTACH POSITION ABOVE NR 2 ENGINE.Sep 3, 2003 · N220FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR 03FDEA01406Keelbeam · damagedLT KEEL BEAM AT STA 740 HAS DAMAGED HOLE DUE TO A SEIZED FASTENER IN KEELBEAM. REMOVED AND REPLACED DAMAGED LT KEELBEAM STA 740 IAW FED EX EA 7-5330-54955, DWG 65-54577-21, AND SRM 53-30-3 FIG. 3. LEAK CHECK GOOD ON DISTRIBUTION DUCTS. REMOVED FOR ACCESSep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01405Frame · corrodedCORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 THRU LBL 7 WL 156 REMOVED CORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 TO LBL 7, WL 156. CORROSION BLEND-OUT OUT OF LIMITS IAW SRM 53-10-1 FIG 1. ORIGINAL THICKNESS .112 MATERIAL REMAINING = .052Sep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01403Warning Light · false activationBOTH FIRE WARNING MASTER LIGHTS ON FORWARD GLARESHIELD ILLUMINATED TWICE FOR ABOUT 1 SECOND EACH TIME DURING CRUISE AT F270. MOMENTARY BELL WITH EACH ILLUMINATION. NO OTHER WARNINGS AND ALL ENGINE INSTRUMENTS NORMAL. FIRE TEST IN BOTH LOOPS OK BOTH INFIGHTSep 3, 2003 · N478FE · Boeing 727200 · Detection SystemSDR 03FDEA01401Packing · leakingAFTER T/O NR 1 ENG EPR LOW WITH A HI FF AT FL200 NR 1 ENG THROTTLE LEVER 3 INCHES FWD OF NR 2 & 3 THROTTLE LEVERS W/ ALL EPR'S MATCHING & NR 1 FF GAUGE 3000 LBS/HR MORE THAN NR 2 & 3 FF GAUGES. ALL ENG INST IN GREEN. CL THRU FL230, NR 1 EPR INDIC 0 & NR 1 FFSep 1, 2003 · N240FE · Boeing 727200 · Turbine Engine Reduction GearSDR 03FDEA01400Skin · damagedSIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS. BS 400 SKIN AREA BETWEEN STR 14-15 LT WITH PLUGGED HOLES WAS REPAIRED PER FED EX EA 7-5330-70501.Aug 29, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01399Floorbeam · corrodedCORROSION ON BS 1130 FLOORBEAM UPPER CHORD AROUND HOLES AND UNDER NUT PLATES, LBL 48, WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM AT BS 1130, LBL 48, WL 208 FWD UPPER FLANGE PER SRM 53-10-8.Aug 29, 2003 · N220FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01397Floorbeam · corrodedA/C BAY LT SIDE, ABOVE PANEL 3355L, CORROSION ON TORQUE BOX LWR FLANGE NUT CLIPS FOUND DAMAGE TO LOWER FLANGE TO BE .066 MATERIAL LOSS ORIGINAL THICKNESS .125. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CHORD. DRILLED UP NEW CHORD. ALODINED, PRIMED & INSTAAug 28, 2003 · N220FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01398Floorbeam · corrodedCORROSION AT NUT PLATES BS 351 TO 341, LBL 18 TO RBL 18, W/L 152. REMOVED CORROSION ON T-CHORD AT VARIOUS LOCATIONS 1 X 1 X .077 INCH FROM ORIGINAL THICKNESS OF .097 INCH AT BS 341-351, LBL 18, RBL 18, WL 152 AND IS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1Aug 28, 2003 · N220FE · Boeing 727200 · Fuselage Main, Floor Beam
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