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 06FDEA2630Skin · misrepairedEXTERNAL FLUSH REPAIR ON LT LWR FUSELAGE APPROX 3 X 2.5 INCHES STA 220, S21L TO S22L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* FLUSH REPAIR ON LT LWR FUSELAGE STA 220, STR 21LJul 19, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2620Skin · corrodedWHILE WORKING NR N01047 FOUND CORROSION IN FWD CARGO BAY SKIN AT BS 596, LBL 9. *S/D* REMOVED CORROSION FWD CARGO BAY SKIN BS 596 LBL 9 AND REPAIRED IAW SRM 53-30-3, 51-30-2.Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2618Skin · dentedDENT IN SKIN AT BS 227, WL 178, 3 INCHES BELOW STR 19 LT. *S/D* REMOVED EXISTING REPAIR BS 700 PLUS 10 TO 720 STR 28R AND INSTALLED REPAIR IN SKIN IAW SRM 53-30-3 FIG 1.Jul 18, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2624Splice · corrodedFWD PIT, FS 620-640, APPROX LBL 2 FLOOR TRACK SPLICE CORRODED.Jul 18, 2006 · N242FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2622Floor Support · crackedFLOOR SUPPORT AT LBL 1 STA 751 IS CRACKED.Jul 18, 2006 · N262FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2621Splice · corrodedFWD PIT, FS 620-640, APPROX RBL 2, FLOOR TRACK SPLICE CORRODED.Jul 18, 2006 · N242FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2619Unknown · unknownEXTERNAL DOUBLER REPAIR APPROX 12 X 8 INCHES ON RIGHT HAND LOWER FUSELAGE STA 720 STR 2R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR BS 700 PLUS 10 - 720 STR 28Jul 18, 2006 · N281FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2617Clamp · looseNR 3 ENG STRUT OVERHEAT LIGHT ILLUM IN FLIGHT. C/W WITH CFM RED TABS, WAS ABLE TO GET LT EXTINGUISHED & RETURNED TO MEM. FOUND 2 CLAMPS ON THE 8TH STAGE CHECK VLV & 3 JOINTS NEAR THE STRUT LOOP LEAKING. REMOVED AND REPLACED THE 2 CLAMPS AND REMOVED SHIMS FRJul 18, 2006 · N489FE · Boeing 727200 · Engine Bleed Air SystemSDR 06FDEA2597Frame · dentedDENT ON I/B FRAME FLANGE BS 970 LT AT STR 26L IN AFT CARGO BAY. *S/D* REPAIRED DENT ON I/B FRAME FLANGE BS 970 STR 26L IAW SRM 51-40-3.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2596Frame · dentedDENT ON I/B FRAME FLANGE BS 970 LT BETWEEN STR 23L AND STR 24L IN AFT CARGO BAY. *S/D* REPAIRED DENT ON I/B FRAME FLANGE BS 970 BETWEEN STR 23L AND 24L IAW SRM 51-40-3.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2595Frame · dentedDENT ON INBOARD FRAME AT BS 990 LEFT AT STR 26L IN AFT CARGO BAY. *S/D* REPAIRED DENT IN FRAME BS 990 STR 26L IAW SRM 51-40-3.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2594Frame · dentedDENT ON INBOARD FRAME AT BS 1010 LT AT STR 26L IN AFT CARGO BAY.Jul 17, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2568Unknown · unknownEXTERNAL DOUBLER REPAIR APP. 8" X 6" ON R/H LOWER FUSELAGE STA 1156 STRINGER 29R TO 30R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AT BS 1156 STR 29R TO 30RJul 14, 2006 · N281FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2567Skin · dentedA 3 INCH DIAMETER BLENDED AREA WITH ASSOCIATED DENT AND CREASE STA 1270 STRINGER 21L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED BLEND AT STA 1270 STR 21L IAW SRM 53-30-1Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2566Frame · dentedDENT ON I/B FRAME FLANGE BS 950F LT BETWEEN STR 23L AND STR 24L IN AFT CARGO BAY. REPAIRED DENT IN FRAME IAW SRM 51-30-5Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2565Frame · dentedDENT ON I/B FRAME FLANGE BS 950F LT BETWEEN STR 25L AND STR 26L IN AFT CARGO BAY. REPAIRED FRAME IAW SRM 51-30-5, 51-30-8, 51-10-2Jul 14, 2006 · N281FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2552Skin · chafedFUSELAGE SKIN UNDER WING TO BODY FAIRING, IS CHAFED AT LT FWD L/E, BS 720D PLUS 11, STR 19L. *S/D* REPAIRED SKIN UNDER WING TO BODY FAIRING BS 720D 11 STR 19L IAW SRM 53-30-3, 51-30-2, 51-20-1.Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2551Skin · chafedFUSELAGE SKIN UNDER WING TO BODY FAIRING, IS CHAFED AT RT FWD L/E, BS 720D PLUS 11 TP 720E, BELOW STR 17R TO STR 19R. *S/D* REPAIRED SKIN UNDER WING TO BODY FAIRING BS 720D 11 TO BS 720D STR 17R-19R IAW SRM 53-30-3, SRM 51-30-2, SRM 51-20-1.Jul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2550Floorbeam · unknownFLOORBEAM UPPER TEE REPAIR APPROX 12 INCHES LONG ON MAIN CABIN FLOORBEAM STA 1070 RBL 31 TO RBL 42 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED FLOORBEAM T-CAP BS 1070 RBLJul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2549Skin · misrepairedEXTERNAL DOUBLER REPAIR APP 27 X 11 INCHES ON RIGHT HAND LOWER FUSELAGE STA 720 STR 22R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER BS 720 STR 22R WAS NOT INSTALLED PEJul 12, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2540Unknown · unknownFLOORBEAM AT STA 344, UPPER CAP HAS AN EXISTING SPLICE THAT INTERFACES WITH INSTALLATION OF MOD PARTS PER EO 7-5340-7-5002. REMOVED AND REPLACED T-CHORDS SPLICES IAW SRM 27-53-007 & SRM 51-30-2. MAJOR REPAIR.Jul 11, 2006 · N262FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2539Floorbeam · corrodedFLOORBEAM CAP CORRODED FS 1110 AT LBL 67 MAIN CABIN. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM CAP REPAIR ALL IAW FX B727-200 SRM 53-10-1 FIG 4A, 53-10-8 FIG 3, 51-10-2, 51-30-2.Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2538Stringer · corrodedFWD PIT STR 27L HAS CORROSION AT STA 740. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR IAW FX B727-200 SRM 53-10-1, 53-10-3 FIG 1, 51-10-6, 51-30-2 AND 51-10-2.Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2537Stringer · corrodedFWD LOWER CARGO COMPT S28L SPLICE CORRODED AT FS 680. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR ALL IAW FX B727-200 SRM 53-10-1, 53-0-3 FIG 4, 53-10-3 FIG 1, 51-10-6, 51-10-2 AND 51-30-2.Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2536Skin · corrodedFWD LOWER CARGO AT STA 535 BETWEEN STR 28L AND STR 28R SKIN HAS CORROSION AROUND ANTENNA CUTOUT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR TO FUSELAGE SKIN IAW FX B727-200 SRM 53-30-1, 53-30-2 FIG 2, 53-30-3 FIG 1, 51-10-2 AND 51-30-2.Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2535Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED STA 1300 LT ABOVE AIR STAIR CUTOUT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED. REPAIR ALL IAW B727-200 SRM 53-30-1, 53-30-2 FIG 3, 53-30-3 FIG 1, 51-10-2.Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2533Skin · bentE&E COMPARTMENT DOOR EXTERNAL SKIN BENT AT CTR FWD. REMOVED AND REPLACED E & E COMPARTMENT DOOR IAW SRM 52-00-2.Jul 11, 2006 · N201FE · Boeing 727200 · Electrical/Electronic Compartment DoorsSDR 06FDEA2417Floorbeam · corrodedN01255 (CORROSION C53-224-01) FLOORBEAM WEB AT BS 880, LBL 47, WL 204 CORRODED. REPAIRED FLOORBEAM WEB PER FEDEX EA 7-5310-103078.Jun 28, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2416Flap Track · corrodedN00269 RIGHT WING NUMBER 6 FLAP TRACK CORRODED AT AFT ATTACH POINT. REPLACED R/W #6 FLAP TRACK WITH SERVICABLE TRACK, PER WORK CARD 27X5708-03.Jun 28, 2006 · N281FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2408Skin · damagedN00227 EXTERIOR SKIN GOUGED AND CREASED BS 1133 BETWEEN STR. 16 RT-18 RT. REMOVED GOUGES IN EXTERIOR SKIN IAW SRM 53-30-1.Jun 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2407Skin · gougedEXTERIOR SKIN GOUGED BS 1112-1140 BETWEEN STR. 17 RT-16 RT. REPAIR TO BE INCORPORATED ON FED EX WORK CARD N00227Jun 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2389Sensor · faultyAT ROTATION, STICK SHAKER ACTIVATED ON BOTH STICKS CONTINOUSLY. PULLED STALL WARNING DC CIRCUIT BREAKER STICK SHAKER STOPPED. RETURNED TO MEM. CYCLED GEAR AT 6K MSL IN ATTEMPT TO CLEAR PROBLEM BUT PROBLEM REMAINED AFTER GEAR UP AND THROUGHOUT THE ATTEMPTEDJun 22, 2006 · N477FE · Boeing 727200 · Stall Warning SystemSDR 06FDEA2370Fitting · corrodedNR 6 FLAP TRACK FORWARD FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER STANDARD REWORK DRAWING SR 27-57-020A.Jun 19, 2006 · N493FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2369Attach Fitting · corrodedNR 1 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPAIRED PER FED EX EA 7-5740-102247.Jun 19, 2006 · N493FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2368Attach Fitting · corrodedNR 8 FLAP TRACK FORWARD ATTACH FITTING IS CORRODED ON INBOARD FACE. REPAIRED PER FED EX EA 7-5740-102247.Jun 19, 2006 · N493FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2333Fuel Control · out of adjustNR 2 ENGINE IDLE OUT OF LIMITS. ADJUSTED NR 2 ENGINE IDLE TRIM PER JRH CHAPT 6. DOWN TRIMMED ENGINE 4.5 COMPLETE TURNS. RAN ENG FOR OPS CHECK. OK FOR SERVICE.Jun 16, 2006 · N478FE · Boeing 727200 · Fuel Controlling SystemSDR 06FDEA2315Attach Fitting · corrodedCORROSION ON FWD ATTACH FITTING AT NR 3 FLAP TRACK.Jun 15, 2006 · N269FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2270Stringer Clip · damagedSTRINGER CLIP AT BS 950A STR 7 RT HAS 2 EA EXTRANEOUS HOLES. REMOVED STRINGER CLIP AT BS950A STR 7 RT AND REPLACED WITH REPLACEMENT STRINGER CLIP AT BS 950A STR 7 RT PER SRM 51-30-2 AND SRM 51-30-5.Jun 12, 2006 · N493FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2256Frame · misdrilledDOUBLE HOLE AT BS 600 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2255Frame · misdrilledDOUBLE HOLE AT BS 520 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2254Frame · misdrilledDOUBLE HOLE AT BS 500 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2259Safety Switch · dirtyON LANDING AT APPROX 60 KTS, BRAKE PEDALS WERE FULLY DEPRESSED DID NOT NOTICE ANY CYCLING OF ANTISKID BRAKES, AND AIRCRAFT DID NOT APPEAR TO HAVE NORMAL AMOUNT OF BRAKING. ANTISKID LIGHT REMAINED OFF. OPERATED BRAKES, FOUND THAT NR 2 AND NR 3 BRAKES WOULD NOJun 8, 2006 · N463FE · Boeing 727200 · Landing Gear Position and WarningSDR 06FDEA2253Support Angle · chafedLEFT O/B AILERON I/B BALANCE PANEL FWD HINGE SUPPORT ANGLE HAS CHAFING DAMAGE AT I/B AND O/B ENDS. REPAIRED PER FED EX EA 7-5710-100548.Jun 8, 2006 · N493FE · Boeing 727200 · AileronsSDR 06FDEA2252Hinge Fitting · damagedLEFT WING OUTBOARD AILERON OUTBOARD BALANCE BAY, FWD HINGE HALF ATTACH POINT IS ABRAIDED AT THE OUTBOARD AND INBOARD EDGES AT THE APEX OF THE BENDS. REPAIRED PER FED EX EA 7-5710-100548.Jun 8, 2006 · N493FE · Boeing 727200 · AileronsSDR 06FDEA2247Beam · corrodedWHILE WORKING CARD N00862, FOUND CORROSION AT WBL 206, LOWER CHORD OF SPOILER BEAM LOWER SURFACE, RIGHT WING. *S/D* REPAIRED CORROSION RIGHT WING LOWER CHORD OF SPOILER BEAM LWR SURFACE AT WBL 206 IAW FED EX EA 7-5710-100546.Jun 7, 2006 · N269FE · Boeing 727200 · SpoilersSDR 06FDEA2246Web · misdrilledWHILE WORKING CUST CARD N00346 FOUND LOWER SIDE OF THE FLOOR WEB AT BS 1175 RBL 26 WL 208 FASTENER HOLES -SNOWMANNED-. REPAIRED FLOOR WEB AT BS 1175, RBL 26, WL 208 IAW SRM 53-10-1 FIG 1.Jun 7, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2248Skin · dentedMAIN CARGO DOOR EXTERNAL SKIN DENTED 20 INCHES FROM AFT EDGE AND 47 INCHES FROM BOTTOM EDGE. REPAIRED DENT PER FED EX EA 7-5230-102256.Jun 7, 2006 · N269FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA2220Strap · corrodedBS 950E STR 29 RT IS CORRODED. FOUND CORROSION TO BE ON REPAIR STRAP, REMOVED AND REPLACED REPAIR STRAP BS 950E STR 29R IAW SRM 51-30-2 AND FED EX DWG SR27-53-023 REV A.Jun 6, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2219Repair · damagedEXTERNAL DOUBLER REPAIR 12" X 37" ON LOWER FUSELAGE BETWEEN BS 680-BS 690 STR 26L-27R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED DOUBLER AT BS 680 TO BS 720, STR 26L TO SJun 6, 2006 · N269FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2218Floorbeam · corrodedWHILE WORKING FOUND CORROSION ON FLOORBEAM LOWER FLANGE BS 720 RBL 30 AT NUT PLATE HOLE. REPAIRED FLOORBEAM PER SRM 53-10-8.Jun 6, 2006 · N493FE · Boeing 727200 · Fuselage Main, Floor Beam
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