Boeing 727-243
Service difficulty reports · 534
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 = '727243' 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.
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 = '727243' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CAL960272Channel Support · corrodedSTATION 31J - INSPECTION FOUND CORROSION ON CHANNEL SUPPORT AT BS 803, BL 0. THE CORROSION WAS REMOVED AND A 'T' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. (M)SDR CAL960271Panel Support · corrodedSTATION 31J - INSPECTION FOUND LOWER FUSELAGE PANEL SUPPORT CORRODED AT BS 880, LBL 9 AND RBL 9. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL960274Flap Track · corrodedSTATION 31J - INSPECTION FOUND CORROSION AT RIGHT MLG BEAM INBOARD FLAP INBOARD TRACK ATTACH POINT. THE AREA WAS REPAIRED IAW ECRA 5750-02438. (M)SDR CAL960273Beam · corrodedINSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORMED IAW ECRA 5750-02437 AND SRM 51-10-6 AD SRM 51-10-2. (X)SDR CAL960269Floor Beam · corrodedSTATION 31J - INSPECTION FOUND ELONGATED HOLES AND PITTING CORROSION IN FLOOR BEAM AND SEAT TRACK AT BS 1010, RBL 55. THE AREA OF ELONGATED HOLES WAS CUT OUT. REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. (M)SDR CAL960265Floor Beam · corrodedINSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1110, RBL 26 TO RBL 44. THE CORRODED SECTION OF FLOOR BEAM UPPER CHORD WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, SRM 51-10-2, AND MM 51-20-151. (X)SDR CAL960258Support · corrodedSTATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, RBL 9 BETWEEN HEAT EXCHANGERS. THE CORRODED AREA WAS CUT OUT, TWO 'L' ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0SDR CAL960257Support · corrodedSTATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, LBL 9 BETWEEN LEFT AND RIGHT HEAT EXCHANGER. THE CORROSION WAS REMOVED IAW SRM 51-10-2, AN 'L' ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20SDR CAL960256Support · corrodedSTATION 31J - INSPECTION FOUND CORROSION ON INBOARD SIDE OF PANEL SUPPORT AT BS 780, LBL 9. THE CORROSION WAS MECHANICALLY REMOVED. TWO BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 2. (M)SDR CAL960264Rib · chafedINSPECTION FOUND A .3125 INCH CHAFED HOLE IN WEB AT INNER SKIN FLANGE OF RT WING L/E SLAT NR 7 OUTBOARD RIB. THE AREA WAS DRESSED OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9. (X)SDR CAL960263Floor Support · brokenINSPECTION FOUND FLOOR SUPPORT BROKEN AT BS 760, LBL 2. THE BROKEN SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)SDR CAL960262Door Frame · corrodedINSPECTION FOUND R-1 DOOR INTERIOR LOWER FORWARD FRAME CORRODED AT BS 380, RBL 60. THE CORRODED AREA WAS CUT OUT. AN ANGLE AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-40-3, FIGURE 1. (X)SDR CAL960267Beam · crackedINSPECTION FOUND CORROSION ON TOP SIDE OF DELTA BEAM AT BS 803, RBL 9 AND A 1.5 INCH CRACK AT BS 812. THE CORROSION WAS REMOVED IAW SRM 51-10-2. A TEE SECTION WAS FABRICATED AND INSTALLED IAW MM 51-20. (X)SDR CAL960261Floor Beam · corrodedINSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 344, RBL 20 TO LBL 20. THE CORRODED UPPER CHORD WAS REMOVED. A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. FIGURE 3. (X)SDR CAL960260Threshold Angle · corrodedINSPECTION FOUND THRESHOLD ANGLE AT DRAIN PAN CORRODED AT BS 344. THE CORRODED AREA WAS CUT OUT. A THRESHOLD ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)SDR CAL960259Floor Beam · corrodedSTATION 31J - INSPECTION FOUND FLOOR BEAM CORRODED AT BS 380, RBL 40 TO RBL 60. A NEW FLOOR BEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3, 51-10-2, AND 51-20-0. (M)SDR CAL960250Door Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN INBOARD UPPER SURFACE OF BS 620 FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME COVER WEB. THE CRACKED AREA WAS REMOVED FROM THE WEB. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2, ANDSDR CAL960252Skin · crackedSTATION 31J - INSPECTION FOUND A .5 INCH CRACK IN LOWER SKIN PANEL OUTBOARD OF PANEL 8505R AT RIGHT WING STATION 304. THE CRACKED AREA WAS REMOVED. A NEW ATTACH ANGLE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-30-3, FIGURE 4. (M)SDR CAL960270Former · corrodedSTATION 31J - INSPECTION FOUND CORROSION ON HORIZONTAL FORMER AT BS 774, RBL 9-35. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL960268Rib Web · crackedSTATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING LEADING EDGE RIB WEB. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)SDR CAL960255Support · corrodedSTATION 31J - INSPECTION FOUND KEEL BEAM PANEL SUPPORT AT BS 850 LBL 10 CORRODED THROUGH AND BOTTOM OF SUPPORT HAS SURFACE CORROSION FROM RBL 10 TO LBL 10. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL960253Beam · crackedSTATION 31J - INSPECTION FOUND A .75 INCH CRACK AT TERMINAL FITTING ATTACH POINT OF BS 870 HORIZONTAL BEAM IN FORWARD UPPER OUTBOARD CORNER OF LEFT WHEEL AT STRINGER 18A. THE CRACKED SECTION OF BEAM WAS REMOVED. AN ANGLE AND DOUBLER WERE FABRICATED AND INSTASDR CAL960254Fitting Rib · crackedSTATION 31J - INSPECTION FOUND A 1.75 INCH CRACK IN LEFT ELEVATOR FITTING RIB BETWEEN BAYS 3 AND 4. THE LEFT ELEVATOR FITTING RIB WAS REMOVED AND REPLACED IAW MM 55-20-0 AND SRM 51-30-2. (M)SDR CAL960015Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN L-1 DOOR INTERNAL SKIN AT TORQUE BOX CUT OUT. THE CRACKED AREA WAS BLENDED OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-2, SRM 51-10-1, AND SRM 51-20-4. (X)SDR CAL960034Stringer · corrodedINSPECTION FOUND STR 29R CORRODED AT SPLICE AND UNDER LEVELING COMPOUND AT CENTER OF STRINGER IN AFT CARGO BIN BS 1000. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A STRINGER SPLICE AND REPAIR DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SRSDR CAL960035Stringer · corrodedINSPECTION FOUND STR 29L CORRODED AT STA 972 IN AFT PIT. THE CORROSION WAS BLENDED OUT IAW SRM 51-10-6. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW ECRA 5310-03205. (X)SDR CAL960027Strap · corrodedINSPECTION FOUND DOUBLER STRAP CORRODED AROUND C-1 ENTRANCE AT STA 560 ABOVE STR 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230-01298 AND SRM 51-30-2. (X)SDR CAL960022Support · corrodedINSPECTION FOUND FORWARD CARGO FLOOR SUPPORT STRUCTURE AT STA 640 CENTER SECTION CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6, AN 'L' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND SRM 53-10-8. (X)SDR CAL960036Stringer · corrodedINSPECTION FOUND STR 28L CORRODED BETWEEN STA 985 AND STA 994, IN THE AFT PIT. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND MM 51-40-5. (X)SDR CAL9690026Stringer · corrodedINSPECTION FOUND STR 26R CORRODED AT STA 520 - STA 560. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-10-2, SRM 51-30-2, AND SRM 51-40-5. (X)SDR CAL960040Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD FITTING AT S28L. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-2. L-ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM'S 51-30-2, 53-10-3, 51-10-2, AND 51-20-4. (X)SDR CAL960039Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD CORNER FITTING AT S28R. A NEW STRINGER SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, SRM 53-10-3, AND ECRA 5340-01256. (X)SDR CAL960038Frame · corrodedINSPECTION FOUND UPPER SURFACE OF BELT FRAME LOWER FLANGE IN AFT CARGO BIN CORRODED AT BS 990, LBL 16. THE CORROSION WAS REMOVED IAW SRM 51-10-6. (X)SDR CAL960037Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT FS 990 BETWEEN STR 28L AND STR 29L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 53-10-4, 51-10-1, 51-10-2, AND 51-30-2. (X)SDR CAL960030Stringer · corrodedINSPECTION FOUND STR 27L CORRODED IN AFT CARGO COMPARTMENT AT BS 1015. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-30-2. A STRINGER REPAIR AND HAT SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)SDR CAL960029Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED BETWEEN S27R AND S28R AND STA 1010. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960028Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED AT STA 1166. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X)SDR CAL960025Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 580 AND CENTER OF FLOOR STRUCTURE. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960024Support · corrodedINSPECTION FOUND FORWARD CARGO RIGHT FLOOR SUPPORT STRUCTURE CORRODED AT BS 480 - BS 560. A REPAIR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, AND SRM 51-30-2. (X)SDR CAL960023Frame · crackedINSPECTION FOUND FORWARD CARGO FRAME STA 640 CRACKED AT S29R (.50 INCH), S29L (1.5 INCHES), AND S28L (.25 INCH). A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960020Frame · crackedINSPECTION FOUND A .3750 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, STR 28R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X)SDR CAL960018Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 600 AND CENTER FLOOR STRUCTURE. THE CRACKED SECTION OF FRAME WAS CUT OUT IAW SRM 51-40-3. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-30-2. (X)SDR CAL960017Frame · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FORWARD CARGO FRAME AT STA 720, LBL 6. THE CRACKED SECTION OF FRAME WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960016Floor Beam · corrodedINSPECTION FOUND CABIN FLOOR BEAM CORRODED FROM LBL 20 TO LBL 60, STA 344. THE CORRODED SECTION OF FLOOR BEAM WAS CUT OUT. REPAIR PARTS WERE FABRICATED, TREATED, AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10-2. (X)SDR CAL960021Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT BS 680, LBL 6. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960019Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, LBL 24. THE CORRODED SECTION OF FRAME WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-40-2, SRM 51-30-1, SRM 51-20-2, AND SRM 51-30-2. (X)SDR CAL951128Fuse · blownFLT NR 0631 - EWR - A PREFLIGHT INSPECTION, FOUND FORWARD SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE FROM ROW 1-7. MAINTENANCE FOUND A FUSE BLOWN ON FORWARD POWER SUPPLY. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M)SDR CAL951049Duct · rupturedFLT NR 0382 - FLL - THE NR 3 ENGINE LIGHT ILLUMINATED AFTER TAKEOFF FROM FLL. ENGINE POWER WAS REDUCED AFTER LEVELING OFF AND THE ENGINE FIRE WARNING LIGHT EXTINGUISHED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO FLL WHERE IT LANDED WITHOUT INCIDENT. SDR CAL951038Noz Guide Vane · separatedMSY - FLT 1528 - THE NR 3 ENGINE FAILED ON TAKEOFF FROM MSY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED WITHOUT INCIDENT. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESDR CAL950822Actuator · inoperativeEWR - FLT 1900 - THE NR 8 LEADING EDGE SLAT WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE FLAPS WERE CYCLED WITH NO EFFECT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 8 LEADING EDGE SLAT ACTUATOR AT FAULT. T
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