Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 ASAA961267Skin · corrodedTUL - FOUND CORROSION ON SKIN INBOARD OF RT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697 DATED 8-9-96. (M)SDR AALA961269Skin · crackedTUL - FOUND SKIN BULGED AND CRACKED STATION 670-680 AT STRINGER 26R AT SKIN LAP. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR AALA961268Stringer · corrodedTUL - FOUND CORROSION ON SKIN AND STRINGER. REMOVED FASTENERS, CLEANED SKIN. INSTALLED STRINGER REPAIR PER SRM 53-10-5 FIG 1. (M)SDR AALA961266Skin · corrodedTUL - FOUND CORROSION ON SKIN INBOARD OF LT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697, DATED 8-9-96. (M)SDR AALA961265Floor Beam · corrodedTUL - FOUND CORROSION ON FLOOR BEAM UPPER FLANGE STATION 1166, LBL 39. CUT OUT CORRODED AREA AND REPAIRED PER SRM 53-10-8 PG 9C-9E. (M)SDR 96FDEA01396Overheat Loop · out of positionLWR AFT BODY OVERHEAT LIGHT BLINKED ON MOMENTARILY ONCE WHILE IN FLIGHT. REMOVED GILLINER PANELS LOWER AFT CARGO COMPARTMENT. INSPECTED SENSOR, FOUND NUMEROUS SPOTS SENSOR RUBBING METAL BRACKETS. REPOSITIONED SAME, REMOVED KEEL BEAM PANEL, INSPECTED SENSOR SDR 96FDEA01394Shear Tie · corrodedNR 0648 AND 030, CORROSION ON CHORD BS 350 RBL 18 TO LBL 18 WL 148 UNDER NUTPLATES.SDR 96FDEA01393Overheat Loop · out of positionLOWER AFT BODY OVERHEAT LIGHT FLASHED ON AND OFF INTERMITTENTLY IN FLIGHT, BOTH PACKS ON BLEEDS 1 ENGINE 2 APU BLEED AND ENGINE 3 BLEED OPEN. LIGHT DOES NOT STAY ILLUMINATED LONG ENOUGH TO ISOLATE PROBLEM USING ABNORMAL CHECK LIST. ALSO, AFT CARGO SELECTED OSDR AALA961244Light · defectiveDFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE R1 DOOR INOPERATIVE. REPLACED THE EMERGENCY EXIT LIGHT ABOVE R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR CALA9601181Actuator · leakingTHE NR 7 LEADING EDGE SLAT WOULD NOT RETRACT AFTER TAKEOFF. THE FLAPS WERE CYCLED AND THE LEADING EDGE DEVICE RETRACTION FAILURE CHECKLIST WAS COMPLIED, BUT THE NR 7 SLAT WOULD NOT RETRACT. SOME LOSS OF THE A-SYSTEM HYDRAULIC QUANTITY WAS ALSO OBSERVED. THESDR 96FDEA01386Engine · damagedADVANCED POWER FOR TAKEOFF AND HAD LARGE AIRFRAME VIBRATION. THROTTLES RETARDED AND TAKEOFF ABORTED. EPR MADE IT AS FAR AS 1.3, BUT NOT UP TO 1.4. SUBSEQUENT POST FLIGHT INSPECTION REVEALED DAMAGE TO THE NUMBER ONE ENGINE. REMOVED AND REPLACED THE NUMBER OSDR CALA9601180Hyd Line · leakingAIRCRAFT LOST A-SYSTEM HYDRAULICS WHILE EN ROUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A-HYDRAULIC SYSTEM RETURN FLEX LINE LEAKING IN S-DUCT AREA. THE FLEX LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. IN SDR SCNA96219Battery Pack · dischargedL-1 ENTRY DOOR, R-1 SERVICE DOOR AND FWD FLOOR TRACK EMERGENCY LIGHTS VERY DIM. REMOVED AND REPLACED FWD FLOOR TRACK BATTERY POWER SUPPLY, OPS CHECKED GOOD.SDR SCNA96218Battery Pack · dischargedAFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.SDR AALA961201Contl Panel · defectiveDFW - FLT 1269 - AFTER DEPARTURE DFW DURING CLIMB-OUT AT FL 210, CABIN ALTITUDE BEGAN TO CLIMB. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED CABIN PRESSURIZATION CONTROL PANEL. ACCOMPLISHED GROUND ENGINE RUSDR CA960826012Engine · failed(CAN) DURING CLIMBOUT, THE START VALVE OPEN LIGHT ILLUMINATED, #3 ENGINE OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE STARTED TO DROP, FOLLOWED BY A DECAY IN N1 AND N2 WITH AN INCREASE IN EGT. ENGINE FAILURE AND SHUTDOWN DRILL AND CHECKLIST ACCOMPLISHED. AIRCRSDR CALA9601113Hyd Line · leakingAIRCRAFT LOST THE A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 A-PUMP PRESSURE LIGHT. THE HYDRAULIC QUANTITY LOSS AND HYDRAULIC SYSTEM FAILURE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT IAH WITSDR SCNA96202Battery Pack · dischargedAFT AIRSTAIR OVERHEAD EMERGENCY LIGHT FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK IN LIGHT ASSEMBLY IN ACCORDANCE WITH MM 33-50-61. OPS CHECKED GOOD.SDR AALA961076Skin · corrodedTUL - FOUND SKIN BULGED STATION 660 AND STRINGER 28 RT. CUT OUTCORRODED AREA AND INSTALLED SKIN DOUBLER AND STRINGER SECTION PER SRM53-30-3 P 1-10 53-10-3 PAGE 1-10. (M)SDR AALA961075Stringer · corrodedTULE - FOUND STRINGER 28R CORRODED, STATION 650-680. INSTALL STRINGER REPAIR PER SRM 53-10-3. (M)SDR AALA961074Stringer · corrodedTUL - FOUND STRINGER 27L CORRODED BETWEEN OUTER SKIN AND STRINGER. INSTALLED NEW STRINGER SECTION FROM STATION 640 TO 680, PER SRM 53-10-3 FIG 1. (M)SDR AALA961073Stringer · corrodedTULE - FOUND STRINGER CORROSION FS 530-680, STRINGER 28L. REPLACED STRINGER. (M)SDR AALA961072Floor Beam · crackedTULE - FOUND CRACK IN FLOOR BEAM WEB STATION 826.95 BELOW RIGHT LIGHTING HOLE CUTOUT. CRACKS ENDS IN RIVET HOLE. INSTALLED REPAIR PER SRM 61-40-2 PG 1-66. (M)SDR AALA961047Floor Beam · crackedTUL - CRACK IN FLOOR BEAM WEB AT HOLE, STA 823.95, INBOARD, RT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2, PAGES 1-6. TST: 41,665 HOURS. CYCLES: 21,768. (X)SDR AALA961046Stringer · corrodedTUL - STRINGER CORRODED 27L, STA 650 - STA 680. CUT OUT CORRODED STRINGER SECTION. INSTALLED NEW SECTION, SRM 53-10-3, FIGURE 1. TST: 41,665 HOURS. CYCLES: 21,768. (X)SDR AALA961045Stringer · corrodedTUL - STR 28R CORRODED. CUT OUT CORRODED SECTION, INSTALLED STRINGER PER SRM 53-10-3, FIG. 1. TST: 41,665 HOURS. CYCLES: 21,768. (X)SDR TAOA069614Light · brokenOVERHEAD AISLE EMERGENCY LIGHT AT ROW 10 INOP. REPLACED LIGHT ASSEMBLY. (M)SDR AALA960991Angle · corrodedTUL - CORROSION ON FRONT SPAR LOWER CHORD ANGLE, STA 196. REMOVED CORROSION. INSTALLED DOUBLER PER ESO 11697 DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960990Skin · corrodedTUL - CRACK AT RIVET HEAD. FOUND CORROSION UPON SKIN REPAIR. CUT OUT CORRODED SKIN, REPAIRED PER ESO 11697 DATED 6-21-96. INSTALLED TRIPLE DOUBLER. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960989Skin · crackedTUL - BEAR STRAP CRACKED LOWER AFT CORNER FORWARD GALLEY DOOR. STOP DRILLLED CRACK AND INSTALLED REPAIR AT LOWER AFT CORNER PER BSB 727-53-0188. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960988Skin · crackedTUL - CRACK IN SKIN, LEFT SIDE OF VERTICAL STABILIZER (JUST ABOVE FUSELAGE MATE POINT), STA 1342. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 727-55-82. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960987Beam · corrodedTUL - LEFT HORIZONTAL STABLIZER TRAILING EDGE BEAM CORRODED INBOARD OF NR 4 ELEVATOR HINGE BEARING. REMOVED CORROSION, REPAIRED PER SRM ESO 11697, DATED 6-20-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960986Belt Frame · corrodedTUL - CORROSION ON BELL FRAME AND ANGLE AT STA 344 AT STR 25R. CUT OUT CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 51-40-3, PAGES 1-6. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960985Spar · corrodedTUL - CORROSION LOWER LEADING EDGE WING PANELS OUTBOARD NR 8 SLAT ACTUATOR. REMOVED CORROSION, NDT CHECK, INSTALL DOUBLER STRAP PER SRM 57-30-00, FIGURE NR 2. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960984Spar · corrodedTUL - LEFT STABILIZER REAR SPAR CORD HAS CORROSION TOP SIDE OF LEFT STABILIZER AT REAR SPAR CORD INBOARD END. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER ESO 11697, DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960983Skin · dentedTUL - DENT AT STA 416, STR 24L, IN FUSELAGE SKIN. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 3. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960982Angle · corrodedTUL - ANGLE, LOWER CORD ANGLE, BADLY CORRODED AROUND RIVETS BELOW LEFT EDGE FUEL TANK PLATE. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771441, DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960981Spar · corrodedTUL - CORRODED AND BULGED AROUND RIVETS. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771442, DATED 6-17-56. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960980Skin · corrodedTUL - LOWER WING SKIN CORRODED ABOVE LEFT PRIMARY HEAT EXCHANGE. REMOVED CORROSION, INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3, PAGE 25. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA961425Door Frame · corrodedTUL - FOUND CORROSION ON FRAME 377 ABOVE FLOOR LINE, FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER SECTION OF DOOR FRAME FORWARD SIDE OF GALLEY DOOR PER SRM 51-30-2. (M)SDR CALA9600996Track · crackedINSPECTION FOUND A .75 INCH CRACK IN OUTBOARD SIDE OF NR 4 FLAP TRACK TO MAIN LANDING GEAR BEAM ATTACH BOLT AREA. THE FLAP TRACK WAS REMOVED AND REPLACED IAW SRM 57-10-0 AND MM 27-51-0.SDR CALA9600995Skin · dentedINSPECTION FOUND A DENT IN LT FUSELAGE SKIN JUST BELOW AND AFT OF FORWARD ENTRANCE DOOR AREA AT STA 350 BETWEEN STRINGER 17L AND 18L. THE DENTED AREA WAS CUT OUT, A FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9600994Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT OUTBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. A 1.5 INCH CRACK WAS ALSO FOUND IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. THE CRACKED AREAS WERE CUT OUT, REPAIRS WERE FABRICSDR CALA9600993Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANGLE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.SDR CALA9600992Skin · debondedINSPECTION FOUND UPPER AND LOWER SKIN OF RT WING LOWER FIXED PANEL DEBONDING FORWARD OF WHEEL WELL DOOR RELEASE HANDLE. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-40-05 AND REINSTALLED.SDR CALA9600991Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN AT AFT END OF OUTBOARD HOOK CUTOUT FOR NR 6 SLAT. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-4.SDR CALA9600990Circumferential · corrodedINSPECTION FOUND CIRCUMFERENTIAL CORRODED IN AFT CARGO COMPARTMENT AT STA 950A, STRINGER 30R. THE CORRODED TEE WAS REMOVED, A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9600989Battery · dischargedINSPECTION FOUND EMERGENCY LIGHT AT AFT ENTRY INOPERATIVE. THE BATTERY PACK WAS CHARGED AND REINSTALLED.SDR CALA9600826Duct · blownTHE NR 3 ENGINE FIRE WARNING BELL AND LIGHT ACTIVATED SHORTLY AFTER TAKEOFF FROM IAH WITH ENGINE AT CLIMB POWER. THE THROTTLE WAS RETARDED AND THE FIRE WARNING CEASED. WHEN THE NR 3 THROTTLE WAS ADVANCED TO CLIMB POWER THE FIRE WARNING BELL AND LIGHT ACTIVATSDR AALA960920Control Unit · defectiveRDU - FLT 1880 - EN ROUTE MIA/DTW DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT BEGAN TO FLICKER. SHORTLY AFTER BEGINNING QRH PROCEDURE, LIGHTS STOPPED FLICKERING AND SYSTEM WOULD NOT TEST. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. REPLACED FIRE
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