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 CALA9900377Power Supply · inoperativeTHE INTERIOR EMERGENCY EXIT LIGHTS FOR LEFT OVERWING DOOR WOULD NOT ILLUMINATE. THE POWER SUPPLY WAS REMOVED AND REPLACED.SDR CALA9900372Wedge · debondedINSPECTION FOUND RT WING O/B MID FLAP T/E WEDGE DEBONDED. THE TRAILING WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 1.SDR CALA9900371Tab · dentedINSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9900370Bulkhead Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN FWD BULK VERT ANGLE AT RT WHEEL WELL BS 870 KEEL BEAM. THE FWD BULK VERT ANGLE WAS REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-5, PAGE 1.SDR CALA9900369Pressure Deck · crackedINSPECTION FOUND A 3.5 INCH CRACK IN NOSE WHEEL WELL PRESSURE DECK AT FS 270, LBL 14. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2.SDR CALA9900368Chord · crackedINSPECTION FOUND A .375 INCH AND .125 INCH CRACK AT LT WING NR 2 SLAT LOWER CHORD BELOW TELESCOPING ANT-ICE TUBE. THREE ACCESS PANELS WERE REMOVED PER SRM 51-30-2 AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, PAGE 6B. AN ANGLE REPAIR DOUBLER WAS INSTALLESDR CALA9900367Chord · crackedINSPECTION FOUND A .3125 INCH CRACK AT LT WING NR 1 SLAT LOWER CHORD AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND AN ANGLE REPAIR WAS INSTALLED IAW SRM 57-30-2.SDR CALA9900366Chord · crackedINSPECTION FOUND A 3 INCH AND .375 INCH CRACK AT RT WING NR 7 SLAT LOWER CHORD. THE LOWER SLAT PANEL WAS REMOVED FOR ACCESS AND REMOVED ANGLE IAW SRM 51-30-2, PAGE 1. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-20 AND 51-30-2. REINSTALLED ACCESS PANEL IAW SRM 5SDR CALA9900365Floorbeam Web · crackedINSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM WEB AT FS 294, RBL 48. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, SHEET 6.SDR CALA9900364Skin · debondedINSPECTION FOUND RT O/B FLAP AFT SEGMENT DEBONDED AT TRAILING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.SDR CALA9900363Skin · dentedINSPECTION FOUND LT O/B FLAP AFT SEGMENT UPPER SURFACE DENTED AND DEBONDED. THE FLAP WAS REPAIRED IAW SRM 51-40-6.SDR CALA9900362Skin · debondedINSPECTION FOUND LT INBOARD AFT FLAP LOWER SURFACE DEBONDED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2.SDR CALA9900143Battery · dischargedINSPECTION FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD.SDR CALA9900142Duct · failedNR 3 ENG FIRE WARNING ACTIVATED AFTER T/O FROM BWI. THE A/C WAS RETURNED TO BWI WHERE IT LANDED W/O INCIDENT. MX FOUND THE PNEUMATIC DUCT LEADING TO NR 3 NOSE COWL ANTI-ICE VALVE BLOWN. THE NOSE COWL FLANGE FITTING FOR COWL ANTI-ICE INLET WAS ALSO BLOWN. TSDR CALA9900115Duct · brokenA FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGISDR 99ZZZM144Battery Pack · dischargedFLT 441 MIA - VARIOUS EMERGENCY EXIT LIGHTS IN CABIN INOPERATIVE. REMOVED AND REPLACED VARIOUS EMERGENCY EXIT LIGHT POWER SUPPLIES, FOUR BATTERY PACKS.SDR GAIA0001Bulb · failedDURING POST FLIGHT, MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT OVER THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE RE-LAMPED THE LIGHT ASSEMBLY AND PERFORMED AN SATISFACTORY OPS CHECK IAW BOEING 727 MM 33-50-4. THE AIRCRAFT WAS THEN RELEASED BACK TO SERVSDR CALA9802196Anti Ice Duct · brokenTHE NR 3 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB-OUT OF IAH. THE ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. WHEN POWER WAS ADVANCED THE WARNING LIGHT CAME ON AGAIN. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT SDR CALA9802172Chord · corrodedINSPECTION FOUND AFT RT LAV FLOOR REINFORCEMENT CHORD CORRODED AT BS 1176, RBL 26. THE CORRODED AREA WAS BLENDED OUT. A FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5310-03799 AND BOEING SKETCH CAL-MIA-98-CC55TR.SDR CALA9802171Track · corrodedTHE RT WING NR 5 FLAP TRACK WAS FOUND CORRODED. THE NR 5 FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-57-31.SDR CALA9802170Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1.SDR CALA9802168Cylinder · corrodedINSPECTION FOUND THE RT MLG OUTER CYLINDER THREADS FOR GLAND NUT CORRODED. THE RT MLG WAS REMOVED AND REPLACED.SDR CALA9802167Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7.SDR CALA9802166Fitting · corrodedINSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-19297.SDR CALA9802165Mount Pad · corrodedINSPECTION FOUND NR 5 FLAP TRACK AFT MOUNTING FLANGE ON FALSE SPAR WORN AND CORRODED. THE MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 1.SDR CALA9802164Skin · bentINSPECTION FOUND LT INBOARD FOREFLAP INBOARD MOST UPPER SKIN LOOSE AND BENT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3.SDR CALA9802158Power Supply · inoperativeINSPECTION FOUND LT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW MM 33-50-0.SDR CALA9802157Power Supply · inopINSPECTION FOUND RT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-0.SDR CALA9802156Stiffener · corrodedINSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.SDR CALA9802155Skin · debondedINSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, PAGE 18 AND 51-8-4.SDR CALA9802154Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 34. A REPAIR WAS INSTALLED IAW ECRA 5310-03790.SDR CALA9802153Angle · crackedINSPECTION FOUND A 5 INCH CRACK IN L ANGLE AT FORWARD I/B CORNER OF RT MLG WHEEL WELL, BEHIND APU, STA 870. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9802152Bracket · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT ELEVATOR NR 4 ATTACH HINGE BRACKET AT ELEVATOR STA 99.79. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2, PAGE 1, 51-10-1, AND 51-10-2.SDR CALA9802151Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED IAW EA 5762-01050.SDR CALA9802150Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IAW SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-4 AND 51-10-2, PAGE 21.SDR CALA9802149Skin · corrodedINSPECTION FOUND LT O/B AILERON TAB LOWER SURFACE CORRODED AT O/B END AND A SMALL DEBONDED AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PAGE 401-403.SDR CALA9802148Chord · corrodedINSPECTION FOUND CHORD CORRODED IN COCKPIT FLOOR PANEL AT F/E SEAT AFT STOP. THE CHORD WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.SDR CALA9802147Rib · crackedINSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 3, 51-40-3, 51-10-6, PAGE 1, AND 51-10-1, PAGE 1.SDR CALA9802146Skin · dentedINSPECTION FOUND RT O/B AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9802124Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT STA 420, RBL 62. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW 53-30-2 AND 51-30-2.SDR CALA9802123Web · corrodedINSPECTION FOUND WEB CORRODED WHERE R-1 FORWARD DRAIN LINE FITTING ATTACHES, FS 378. THE CORRODED AREA OF WEB WAS REMOVED IAW SRM 51-40-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, PAGE 7 AND 51-10-2, PAGE 2.SDR CALA9802122Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-7.SDR CALA9802121Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 1110, RBL 44. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8, PAGE 44.SDR CALA9802111Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR CALA9802104Chord · crackedINSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9802102Skin · corrodedINSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14.SDR CALA9802097Floorbeam · corrodedINSPECTION FOUND AFT CARGO FLOORBEAM CORRODED AT STA 1070, RBL 12 TO 48. A REPAIR WAS INSTALLED IAW SRM 53-10-8.SDR CALA9802094Angle · crackedINSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED IAW SRM 51-30-2, PAGE 3 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-2, PAGE 12 AND 51-30-2 SDR CALA9802093Stiffener · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9801919Skin · delaminatedINSPECTION FOUND THE RT WING NR 8 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401-404.
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