Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  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 06FDEA03254Keelbeam · corrodedFOUND CORROSION AFT CARGO BAY LT KEELBEAM (STR 29L) O/B FLANGE BS 978. REMOVED CORROSION LT KEELBEAM BS 978 AND REPAIRED IAW SR27-53-023.Sep 12, 2006 · N285FE · Boeing 727233 · Fuselage Main, KeelSDR 06FDEA03252Keelbeam · corrodedFOUND CORROSION LT KEELBEAM (STR 29L) O/B FLANGE BS 950B PLUS 4. REMOVED CORROSION ON LT KEELBEAM BS 950B PLUS 4 AND REPAIRED IAW SR27-53-023.Sep 12, 2006 · N285FE · Boeing 727233 · Fuselage Main, KeelSDR 06FDEA03251Keelbeam · corrodedFOUND CORROSION LT KEELBEAM (STR29L) O/B FLANGE BS 950A TO PLUS 9. REMOVED CORROSION ON LT KEELBEAM BS 950A TO 950A PLUS 9 AND REPAIRED IAW SR27-53-023.Sep 12, 2006 · N285FE · Boeing 727233 · Fuselage Main, KeelSDR 06FDEA03250Keelbeam · corrodedFOUND CORROSION RT KEELBEAM S29R O/B FLANGE BS 950A PLUS 1. REMOVED CORROSION ON RT KEELBEAM BS 950A PLUS 1 AND REPAIRED IAW SR27-53-023Sep 12, 2006 · N285FE · Boeing 727233 · Fuselage Main, KeelSDR 06FDEA03245Depressor · damagedNR 2 CARGO DOOR UPPER FWD SEAL DEPRESSOR CHAFED. REMOVED AND REPLACED NR 2 CARGO DOOR UPPER FWD SEAL DEPRESSOR IAW SRM 51-30-2, 51-30-5 AND 51-30-8.Sep 11, 2006 · N282FE · Boeing 727233 · Cargo/Baggage DoorsSDR 06FDEA03244Frame · damagedFUSELAGE UPPER LOBE, DRILL START IN FRAME FWD SIDE, 3.5" BELOW STR 8L, BS 720E. REMOVED DRILL START IN FRAME FWD SIDE 3.5" BELOW STR 8L BS 720E AND REPAIRED IAW SRM 51-40-3 FIG 1.Sep 11, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03243Stringer · misrepairedEXISTING STRINGER REPAIR AT STA 540, RT STRINGER 7. (DOT 48) REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING STRINGER REPAIR AT BS 540 WAS NOT INSTALLED EPR FAA APPROVED DATA. REMOVED EXISTINSep 11, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03242Unknown · unknownEXISTING EXTERNAL DOUBLER REPAIR APPROX 11" BY 5" AT STA 440, RT STRINGER 27. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER AT STA 440 STR 27R AND REPLACED IAW SRM Sep 11, 2006 · N282FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA03241Shear Tie · unknownAFT CARGO BAY FRAME SHEAR TIE STA 950E BETWEEN STR 28L - 29L. REPAIRED SHEAR TIE BETWEEN STR 28L-29L BS 950E IAW SRM 53-10-4, 53-10-1.Sep 11, 2006 · N282FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA03229Frame · damagedEXISTING FRAME REPAIR AT STA 700, RT STRINGER 24 (DOT NR 43). REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS FOUND NOT TO BE IAW SRM. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER I.ASep 7, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03228Structure · chafedRIGHT OVERWING AFT EXIT CHAFING ALONG BOTTOM EDGE. REMOVED DAMAGE ALONG BOTTOM SIDE OF R/H OVERWING EXIT AND REPAIRED IAW SRM 52- 00-2 FIG. 2.Sep 7, 2006 · N282FE · Boeing 727233 · Emergency ExitsSDR 06FDEA03189Shear Tie · corrodedFOUND CORROSION C53-111-01 AFT CARGO BAY FRAME SHEAR TIE STA 950F BETWEEN STR 28L - 29L. REMOVED CORROSION ON SHEAR TIE STA 950F BETWEEN STR 28L-29L AND REPAIRED IAW SRM 53-10-1.Sep 5, 2006 · N282FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA03164Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP CRACKED AT BS 680 STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.Sep 1, 2006 · N282FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 06FDEA03163Stringer Clip · gougedFUSELAGE UPPER LOBE, STRINGER CLIP GOUGED AT BS 660 STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.Sep 1, 2006 · N282FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 06FDEA03162Rib · chafedVERT STAB RT AND LT FIN STA 55.9 PANEL SUPPORT RIB CHAFED. BLENDED DAMAGE, OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED PER FED EX EA 7-5530-100583.Sep 1, 2006 · N282FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 06FDEA03165Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT STA 1070, RBL 10 - RBL 65, DOT NR 47. REPAIR REQUIRES MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR WAS FOUND NOT TO BE ACCOMPLISHED PER FAA APPROVED DATA. REMSep 1, 2006 · N282FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA03139Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 9" BY 9" AT STA 685, BETWEEN RT STRINGER 20 AND 21. (DOT #6) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION A AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMING REPLACED EXISTING REPAIR DOUAug 30, 2006 · N282FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA03141Skin · crackedNR 2 ENGINE INLET INTERIOR SKIN IS CRACKED AT TE 12 O`CLOCK. REPARIED NR 2 ENGINE INLET SKIN PER SRM 54-10-3.Aug 30, 2006 · N282FE · Boeing 727233 · Nacelle/Pylon, Plate/SkinSDR 06FDEA03129Frame · chafedFOUND MAIN CABIN 1130 FRAME IS CHAFED AT STR 5L. REPAIRED FRAME AT BS 1130 STR 5L IAW SRM 51-40-3.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03128Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, CRACK IN STRINGER CLIP, STR 7L, BS 720A. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 7L IAW SRM 51-30-2 AND SRM 51-30- 5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 06FDEA03127Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, STR 7R, BS 660. REMOVED AND REPLACED STR CLIP BS 660 STR 7R IAW SRM 51-30-2 AND SRM 51-30-5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03126Stringer Clip · crackedFOUND FUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, STR 7R, BS 680. REMOVED AND REPLACED STRINGER CLIP AT BS 680 STR 7R IAW SRM 51-30-2 AND SRM 51-30-5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03125Stringer Clip · corrodedFOUND FUSELAGE UPPER LOBE, STRIGNER CLIP CORRODED, STR 8R, BS 720A. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 8R IAW SRM 51-30-2 AND SRM 51-30- 5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03124Frame · dentedFOUND FWD CARGO BAY FRAME IS DENTED 2 PLACES BS 680 STR 23L AND STR 24L. REMOVED DAMAGE AND REPAIRED DENTED FRAME AT BS 680 STR 23L AND 24L IAW SRM 51-40- 3.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03123Frame · gougedAFT CARGO BAY FRAME GOUGED AT BS 950E STR 25L UPPER SURFACE. REMOVED AND REPLACED GOUGED FRAME SPLICE AT BS 950E STR 25L IAW SRM 51-20-1 AND 51-30-2.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03122Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, BS 720E, STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 720E STR 7R IAW SRM 51-30-2 AND SRM 51- 30-5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 06FDEA03121Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED BS 720D, STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 720D STR 7R IAW SRM 51-30-2 AND 51-30-5.Aug 28, 2006 · N282FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 06FDEA03089Hydraulic Line · brokenEN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN. REMOVED AND REPLACED BOTH NR 1 AND NR 2 HYDRAULIC Aug 25, 2006 · N257FE · Boeing 727233 · Hydraulic System, MainSDR 06FDEA3089Hydraulic Line · brokenEN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN.Aug 25, 2006 · N257FE · Boeing 727233 · Hydraulic System, MainSDR 06FDEA03070Stringer · crackedFUSELAGE UPPER LOBE, STRINGER IS CRACKED AT FWD SIDE OF WING ILLUMINATION LIGHT, STR 15R, RB 720B PLUS 4.5". REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED. ALL WORK DONE IAW SRM 53-10-3.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03071Stringer · crackedFUSELAGE UPPER LOBE, CRACK IN STRINGER FWD OF WING ILLUMINATION LIGHT, STR 15L, BS 720B PLUS 3.5. COMING FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-3.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03069Stringer · crackedFUSELAGE UPPER LOBE, CRACK IN STRINGER AFT OF WING ILLUMINATION LIGHT STR 15L, BS 720B PLUS 15. REPAIRED STRINGER PER SRM 53-10-3, FIG 5.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03073Skin · damagedEXISTING FLUSH REPAIR APPROX 3" BY 2 1/2" AT STA 645, RT STRINGER 22. (DOT #5) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMING FOUND REPAIR NOT TO BE FAA APPROVED DATA. REPAIRED PEAug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA03072Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 12" BY 16" AT STA 1120-STA 1132, BETWEEN LT STRINGER 29 AND RT STRINGER 29 (DOT #23) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ADDED FASTENERSAug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA3073Skin · damagedEXISTING FLUSH REPAIR APPROX 3" BY 2 1/2" AT STA 645, RT STRINGER 22 (DOT NR 5). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA3072Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 12" BY 16" AT STA 1120-STA 1132, BETWEEN LT STRINGER 29 AND RT STRINGER 29 (DOT NR 23) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA3071Stringer · crackedFOUND FUSELAGE UPPER LOBE, CRACK IN STRINGER FWD OF WING ILLUMINATION LIGHT, STR 15L, BS 720B PLUS 3.5.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA3070Stringer · crackedFOUND FUSELAGE UPPER LOBE, STRINGER IS CRACKED AT FWD SIDE OF WING ILLUMINATION LIGHT, STR 15R, RB 720B PLUS 4.5 INCH.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA3069Stringer · crackedFOUND FUSELAGE UPPER LOBE, CRACK IN STRINGER AFT OF WING ILLUMINATION LIGHT STR 15L, BS 720B PLUS 15.Aug 24, 2006 · N282FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA03065Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 1050 BETWEEN STR 25L UPPER SURFACE. COMING CUT OUT DAMAGE ON FRAME AT BS 1050 BETWEEN STR 25L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03064Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 950F STR 26L UPPER SURFACE. COMING DUPLICATE ENTRY, SEE 06-3063 CUT OUT DAMAGE ON FRAME AT BS 950F STR 26L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-2.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA03063Frame · dentedFOUND AFT CARGO BAY FRAME DENTED AT BS 950F STR 26L UPPER SURFACE. COMING CUT OUT DAMAGE ON FRAME AT BS 950F STR 26L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-2.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA3062Floor Support · corrodedFOUND FWD CARGO BAY FLOOR SUPPORT HAS CORROSION AT FASTENER HOLES STA 700 TO 720 LBL 13.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 06FDEA3063Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 950F STR 26L UPPER SURFACE.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA3064Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 950F STR 26L UPPER SURFACE.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA3065Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 1050 BETWEEN STR 25L UPPER SURFACE.Aug 23, 2006 · N282FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2710Skin · damagedEXTERNAL DOUBLER REPAIR APPROX 8" BY 5" ON RIGHT LOWER FWD CORNER OF AFT CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR, REPAIRED DAMAGE AND INSTALLED NEW REPAIRJul 27, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2709Stop Fitting · gougedAFT LOWER CARGO, AFT NR 2 (FROM BOTTOM) STOP PIN FITTING GOUGED). REPAIRED NR 2 (FROM BOTTOM) CARGO DOOR STOP PIN FITTING IAW FED EX EA 7-5230-100556.Jul 27, 2006 · N281FE · Boeing 727233 · Cargo/Baggage DoorsSDR 06FDEA2676Stiffener · crackedFOUND VERTICAL STIFFNER IN RIGHT WHEEL WELL FOR KEEL BEAM CRACKED.Jul 24, 2006 · N271FE · Boeing 727233 · Fuselage Main, KeelSDR FDEA200607212648Warning Light · illuminatedMAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning System
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