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"

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 04FDEA03273Beam · crackedMAIN CARGO DOOR LWR LONGITUDINAL FRAME / CAP IS CRACKED OUTSIDE PREVIOUS REPAIRED AREA AT NR 4 LATCH CAM. COMPLIED WITH EA 7-5230-55418, REF: WRI 52-30/8452.Nov 30, 2004 · N208FE · Boeing 727200 · Fuselage Main, StructureSDR XNOA1213Warning Light · false activationLOWER FORWARD CARGO FIRE LIGHT AND BELL ILLUMINATED IN FLIGHT DIVERTED TO BNA. PERFORMED OPS CHECK ON CDU, INDICATED FALSE ALARM S/N M13198. VISUALLY CHECKED LOWER BELLY. TRANSFER TO DMI 4771. MEL 26-19-1 CAT B. SWAPPED SENSOR FROM P-3 TO FWD CARGO FOR TRONov 24, 2004 · N79754 · Boeing 727200 · Fire DetectionSDR 04FDEA03169Seat Track · gougedMAIN DECK - SEAT TRACK STA 1150 - 1170, BL 0 - LUGS GOUGED. BLENDED GOUGED AREA IAW SRM 53-10-1, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-30-2, FABBED NEW SEAT TRACK FROM 60-5017/7178-T6511 BATCH 746883 AND INSTALLED IAW SRM 51-30-2.Nov 19, 2004 · N208FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03022Warning Light · false activationAFT AIRSTAIR LIGHT ILLUMINATED AFTER TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 15NOV04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. MEM R CHECK AFT AIRSTAIR UP POSITION FOR ADJUSTMENT, PER MM 52-70-001-5 NO FAULTSNov 5, 2004 · N204FE · Boeing 727200 · Door Warning SystemSDR 04FDEA03002Actuator · malfunctionedNR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM.Oct 30, 2004 · N219FE · Boeing 727200 · Leading Edge Slat ActuatorSDR 04FDEA02980Frame · damagedWHILE COMPLING WITH EA 7-5310-64946 A F/U FOUND FRAME REPAIR NOT TO BE DONE IAW SRM AT BS 680 STR 24R NEED TO COMPLY WITH EA 7-5310-55392 ** SD ** COMING REPAIRED IAW EA 7-5310-55392.Oct 22, 2004 · N461FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02928Solenoid · failedPDIS 245 32-10 0006358 12OCT04 LAX CLOSE R LOGPAGES: 00900921 LANDING GEAR LEVER LATCH FAILED TO RAISE ON TAKEOFF PAST OFF POSITION. RAN QRH. CHECK/RESET LEVER LATCH CB (IAW QRH) AND PULLED AURAL WARNING CB (QRH) AND RETURNED.Oct 13, 2004 · N245FE · Boeing 727200 · Main Landing GearSDR C7WA200400040Duct · brokenAIR RETURN, INTERMITTENT FIRE WARNING LIGHT ON NR 2 ENGINE AFTER TAKEOFF. FOUND NR 2 ENGINE Y-DUCT BROKEN. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE DUCT.Oct 7, 2004 · N902PG · Boeing 727200 · Engine Anti-Icing SystemSDR 04FDEA02881Pump · malfunctionedNR 2 B-PUMP LOW PRESS LIGHT ILLUMINATED WITH APPROX 1.4 GALS LOSS IN B-QTY. TURNED NR 2 B-PUMP OFF, GROUND CREW FOUND HYD LEAK IN B-PUMP AREA, B-SPOILER SWITCH TURNED OFF. REMOVED AND REPLACED CASE DRAIN FILTER REF 727-200 M/M 29-12-021-2. STILL NEEDS LEAK Oct 6, 2004 · N495FE · Boeing 727200 · Hydraulic Pump (Electric/Engine), MainSDR 04FDEA02838Beam · corrodedCOMPLY WITH EA 7-5710-82042 WINGS RIGHT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. COMPLIED WITH EA 7-5710-82042 REAMED HOLE, FLAP PEENED AND INSTALLED REPAIR BUSHING.Sep 28, 2004 · N240FE · Boeing 727200 · Wing, Landing Gear Attach FittingsSDR 04FDEA02837Skin · damagedCOMPLY WITH EA 7-5450-80610 PYLON STRUCTURE NR 1 ENG PYLON UPPER SKIN REPAIR. COMPLIED WITH EA 7-5450-80610, REPLACED SKIN SECTION AND INSTALLED EXT SPLICE DOUBLER.Sep 28, 2004 · N240FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 04FDEA02799Skin · corrodedCORROSION EXT SKIN, BS 470 WL 148 CORROSION WHERE MOD S ANT MOUNTS. *S/D* REPAIRED PER SRM 53-30-1 AND 53-30-3.Sep 22, 2004 · N462FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02803Floor Support · corrodedAFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMITS IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES (SPLICES). REPAIR ANSep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA02801Intercostal · crackedFWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3 .050,Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA02800Stringer · corrodedNUMEROUS AREAS OF CORROSION FOUND AT FWD PIT BILGE AREA FROM STA 560 TO STA 580 AT STR 28L. REMOVED DAMAGED AREA FROM STA 550 - 590 IAW SRM 51-10-3 FIG 1 PG 4. FABBED 2EA STRINGERS FROM BAC1498-142 7075-T62, BATCH 318127, FABBED 3EA SPLICES FROM BAC1498-132 Sep 22, 2004 · N240FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR LLM2004F00000Roll Pin · missingWHEN REMOVING NR 2 T/E TRANSMISSION IT WAS DISCOVERED THAT THE IB TORQUE TUBE DRIVE GEAR WAS NOT POSITIVELY ATTACHED TO THE FLAP TRANSMISSION SPLINES. THE TRANSMISSION WAS REMOVED AND INSPECTED. THE INSPECTION REVEALED THAT GEAR/SPLINE ATTACHMENT ROLL PIN NASep 21, 2004 · N117JB · Boeing 727200 · Trailing Edge Flap Control SystemSDR 04FDEA02723Door · corrodedCORROSION LT FWD OVERWING ESCAPE HATCH, ALONG LWR EDGE UNDER PRESSURE SEAL. BLENDED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1 & REPAIRED PER SRM 51-30-5 & 51-30-2.Sep 17, 2004 · N462FE · Boeing 727200 · Emergency ExitsSDR 04FDEA02721Frame · corrodedWHILE REMOVING CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGERS 28L AND 28R CORROSION WAS FOUND TO BE .100 PERCENT THROUGH THE FRAME. ALL WORK DONE PER E.A. 7-5310-55378Sep 17, 2004 · N462FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02719Stringer · corrodedCORROSION ON STR 28R, AROUND FASTENER HOLES ATTACHING KEELBEAM, STA 722, FWD CARGO BAY. CORROSION ON STR NR 28 RT AROUND FASTENERS HOLES ATTACHING KEELBEAM STA 727 FWD CARGO BAY. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER SRM 53-10-3 &Sep 17, 2004 · N462FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02686Smoke Detector · failedINFLIGHT AT FL330, THE MAIN CARGO SMOKE NR 1 (FORWARD) LT ILLUMINATED, FOLLOWED RED TABS AND PHASE ONES DIVERTED. WARNING LT WENT OUT ON FINAL APPROACH THREE CREW DETECTED A FAINT ABNORMAL ODOR AFTER LANDING AND CARGO DOOR OPEN. REMOVED AND REPLACED NR 1 SMOSep 15, 2004 · N207FE · Boeing 727200 · Fire DetectionSDR 04FDEA02573Frame · crackedRIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE.Aug 29, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02563Frame · crackedCOMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9.Aug 25, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02552Frame · damagedFRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3.Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02551Skin · chafedFUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING.Aug 23, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02530Skin · bentAFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02529Doubler · damagedNR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600 Aug 19, 2004 · N246FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02500Shear Tie · corrodedCORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM .063, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIAug 18, 2004 · N246FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA02493Frame · crackedCRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-10-1.Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02492Floorbeam · corrodedCORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM .090. LBL 4 4 X 2 X .0015 INCH. LBL 20 6 X 2 X .005 INCH, LAug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02490Frame · bentFRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3.Aug 17, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02474Floorbeam · corrodedCORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 04FDEA02473Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02472Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02471Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02470Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, StructureSDR 04FDEA02469Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, FrameSDR 04FDEA02468Stringer · crackedCRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02467Stringer · crackedCRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3.Aug 13, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02466Skin Panel · damagedC/W EA 7-5330-80590 FUSELAGE SKIN REPAIR AT BS 1009 AND STRINGER 30 P/N 65-13913-1. COMPLIED WITH EA 7-5330-80590, FUSELAGE SKIN REPAIR AT BS 1009 STRINGER 30.Aug 13, 2004 · N284FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 04FDEA02460Angle · corrodedN00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA02458Keelbeam · corrodedN00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING **Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02462Hose · leakingON GEAR RETRACTION, HYD SYSTEM A QUANTITY WENT TO ZERO. NUMEROUS SAFETY WIRES BROKEN IAW EMERG PROC. BOTH A PUMPS OFF IMMEDIATELY, HYD FLUID SHUTOFFS CLOSED 5 MINUTES LATER, NR 1 AND NR 2 ENGINES SHUT DOWN APPROX 45 MINUTES AFTER THAT. FOUND LEAKING RT GEAug 12, 2004 · N262FE · Boeing 727200 · Hydraulic System, MainSDR 04FDEA02461Stringer · corrodedCORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02459Keelbeam · corrodedCORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02457Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02456Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A.Aug 12, 2004 · N246FE · Boeing 727200 · Fuselage Main, KeelSDR 04FDEA02454Stringer · dentedBS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02453Stringer · dentedBS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02451Stringer · dentedSTRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358.Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 04FDEA02450Stringer · dentedSTRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358Aug 11, 2004 · N246FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
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