N271FL, cancelled Mar 20, 2003
Service difficulty reports · 108
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N271FL' AND deregistration_id = 'N271FL-2003-03-20' 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 n_number = 'N271FL' AND deregistration_id = 'N271FL-2003-03-20' 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 F3LA200200357Cargo Track · corrodedDURING A C 2 CHECK, CORROSION WAS FOUND IN THE CARGO TIE DOWN TRACK AT LBL 17, WL 157, BS 813. TIE DOWN TRACK WAS REPLACED IAW SRM 53-10-05 AND SRM 51-10-02.SDR F3LA200200353Structure · crackedDURING C 2 CHECK, THE FORWARD CARGO DOOR, LOWER CORNER, WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED USING SB 737-52A1100 AND COMPLIED WITH THE REQUIREMENTS OF AD 2000-07-06 UNDER ENGINEERING REQUEST 02-1333SDR F3LA200200346Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED LT WING FIXED LE CRACKED ON INBD SIDE OF NR 2 SLAT, INBD AUX TRACK CUTOUT. REPAIRED CRACK PER SRM 57-20-L1 AND MM 51-21-021.SDR F3LA200200345Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, RBL 8, WL 157. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-5 AND 51-30-02.SDR F3LA200200344Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0.SDR F3LA200200343Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM, BS 813, LBL 8, WL 157. REPAIRED DAMAGED AREA PER SRM 53-10-1 AND 53-10-5.SDR F3LA200200342Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, LBL 12, WL 157. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-10-5 AND 51-30-02.SDR F3LA200200341Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD SPLICE STRAP, BS 772, WL 157. REPLACED STRAP PER SRM 51-30-2.SDR F3LA200200340Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SPLICE, BS 504, WL 155. REPLACED STRAP PER SRM 51-30-02.SDR F3LA200200339Clip · damagedDURING C-2 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SUB THRESHOLD "T" CLIP, BS 440, RBL 16. REPLACED "T" CLIP PER SRM 51-30-02.SDR F3LA200200337Support · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 786, RBL 21, WL 157. REPLACED SIDEWALL SUPPORT PER SRM 51-30-02, FIG. 1, AND SRM 51-30-02, FIG. 9.SDR F3LA200200338Support · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A - BS 520, RBL 25, WL 156. FABRICATED AND INSTALLED REPLACEMENT SIDEWALL SUPPORT PER SRM 53-10-1, 53-10-2. 51-21-21 AND 51-30-2.SDR F3LA200200336Frame · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 747, RBL 6, WL 148. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-4, 53-10-1 AND 51-30-02.SDR F3LA200200335Structure · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD ENTRY DOOR AFT LOWER THRESHOLD CRACKED AT FWD EDGE. REPAIRED PER SRM 52-30-3 AND BOEING DRAWING 65-02938.SDR F3LA200200333Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACKED SKIN AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER, APPROX .25 INCH IN LENGTH. REPAIRED PER SRM 53-30-3, FIGURE 24.SDR F3LA200200334Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD SERVICE DOOR CUTOUT SKIN CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM 53-30-3.SDR F3LA200200364Stringer · corrodedDURING C 2 CHECK, CORROSION WAS FOUND ON THE STRINGER AT STA 520, STR 26L.THE STRINGER WAS REPAIRED BY REMOVING THE DAMAGED SECTION BETWEEN STA 510 AND 540 AT STR 26L. NEW PARTS WERE FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-10-3,SDR F3LA200200349Skin · corrodedDURING C 2 CHECK, CORROSION WAS FOUND ON THE SKIN AT BS 470, ON THE EXTERIOR, UNDER THE DME ANTENNAE. REPAIR WAS PERFORMED IN ACCORDANCE WITH SRM 53-30-3, FIGURE 2SDR F3LA200200256Sensing Element · faultyAIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH THRUST REDUCED TO IDLE. ALL ENGINE INDICATIONS APPEARED NORMAL. REPLACED NR 2 ENGINE UPPER FIRE SENSING ELEMENT. REMOVED PLACARD.SDR F3LA200200255Connector · dirtyAIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING HANDLE ILLUMINATED MOMENTARILY ON THREE OCCASIONS DURING DEPARTURE. CLEANED CONNECTORS A AND B ON LOWER FIRE DETECTOR ELEMENT AND CHECKED OKAY.SDR F3LA200200254Module · malfunctionedAIR TURNBACK. FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING ILLUMINATED APPROXIMATELY 5 MINUTES AFTER TAKEOFF. FIRE WARNING WENT OUT WHEN THRUST REDUCED, ALL INDICATIONS NORMAL. WHEN MORE THRUST ADDED, FIRE WARNING ILLUMINATED AGAIN. REDUCED THRUST TO IDLESDR F3LA200100132Odor · detectedUPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT AND CONTINUED TAKEOFF ROLL, WHICH APPEARED NORMAL. ALSO REPORTED A STRONG BURNING RUSDR F3LA200100Odor · detectedUPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED A STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT. CONTINUED TAKEOFF ROLL WHICH APPEARED NORMAL. AT GEAR RETRACTION, A STRONG BURNISDR F3LA200100124Controller · failedAIR TURN BACK. FLIGHT CREW REPORTED LOUD RUMBLE NOISE NEAR RT. PACK, ASSOCIATED WITH STRONG SMELL. TURNED PACK AND RT. BLEED OFF AND SMELL AND NOISE WENT AWAY. LOW VIBRATION CONTINUED. MAINTENANCE RAN RT. PACK AND COULD NOT DUPLICATE DISCREPANCY. OPENED PASDR F3LA200100114Actuator · failedUPON ARRIVAL, FLIGHT CREW REPORTED "A" SYSTEM HYDRAULIC QUANTITY AND PRESSURE FELL TO ZERO AFTER LANDING. REPLACED NO. 8 GROUND SPOILER ACTUATOR PER MM 27-62-101. PERFORMED OPERATIONAL CHECK, LEAK CHECK AND RIG CHECK. REPLACED NO. 1 AND NO. 2 ENGINE DRIVEN SDR F3LA200100108Coupling · disconnectedAIR TURN BACK. FLIGHT CREW REPORTED FLAPS DID NOT RETRACT AFTER TAKEOFF. LT. TORQUE TUBE COUPLING AT NO. 4 FLAP TRANSMISSION WAS DISCONNECTED. RECONNECTED COUPLING PER MM 27-51-251. ADJUSTED TRAILING EDGE FLAPS PER MM 27-51-01 AND PERFORMED OPERATIONAL TESSDR F3LA200100100B-Nut · looseAIR TURNBACK, FLIGHT CREW REPORTED LOSS OF A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. TIGHTENED NR 1 ENGINE SUPPLY LINE B-NUT, REPLACED NR 1 ENGINE CASE DRAIN FILTER. PERFORMED LEAK CHECK AND OPERATIONAL CHECK AND CHECKED OKAY.SDR F3LA200100093Web · crackedDURING C-1 CHECK, FLIGHT CREW REPORTED SEVERAL CRACKS FROM RIVET HOLE BEHIND THE 178 BULKHEAD IN THE FLOOR STRUCTURE AT BS 180, WL 207. MAINTENANCE REMOVED CRACKS FROM RIVET HOLE AND INSTALLED REPAIR PARTS PER SRM 51-40-02.SDR F3LA200100056Aileron · delaminatedPRIOR TO DEPARTURE, MAINTENANCE REPORTED OTBD SIDE OF RT AILERON DELAMINATED. REPLACED AILERONS IN LT AND RT POSITIONS PER MM 27-11-11, RIGGED AILERONS, AND PERFORMED OPERATIONAL CHECK PER MM 27-11-11.SDR F3LA200100008Engine · vibrationAIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE VIBRATION ON CLIMBOUT AT 20,000 FT. NR 1 ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PHX WITHOUT INCIDENT. THE NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. AN ADDENDUM WILL BESDR F3LA200100005Teleflex Cable · out of adjAIR TURN BACK. FLIGHT CREW REPORTED GEAR HANDLE WOULD NOT MOVE TO "UP" POSITION AFTER TAKEOFF AND LANDING GEAR WARNING HORN WOULD NOT SILENCE AFTER FLAPS WERE RETRACTED. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY PER MM 32-07-100. ADJUSTED GROUND SDR F3LA200100004Fire Detector · malfunctionedFLIGHT CREW REPORTED APU FIRE WARNING ILLUMINATED IN FLIGHT FROM PHX TO DEN. THE APU FIRE BOTTLE WAS DISCHARGED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT.AN INSPECTION REVEALED NO SIGNS OF OVERHEATING OR FIRESDR F3LA200000272Cooling Fan · inoperativeUPON ARRIVAL, FLIGHT CREW REPORTED EQUIPMENT COOLING FAN "OFF" LIGHT ILLUMINATED IN FLIGHT. SELECTED ALT NORMAL BLOWER AND COOLING FAN CIRCUIT BREAKER TRIPPED, FOLLOWED BY AN ELECTRICAL BURNING ODOR. ALT FAN CONTINUED TO OPERATE NORMALLY. MAINTENANCE REPLACEDSDR F3LA00110Channel · corrodedDEN - DURING C-7 CHECK, INSPECTION REPORTED FORWARD LAVATORY AFT WALL HAT SECTION CORRODED AT BS 306, LBL 45, LBL 65. MAINTENANCE REPLACED HAT SECTION PER SRM 53-10-2 AND 53-10-3. (M)SDR F3LA00111Skin · bulgedDEN - DURING C-7 CHECK, INSPECTION REPORTED NR 1 DME ANTENNA BASE HAD SEALANT BLOWN OUT OF GAP, REVEALING A BULGE IN THE SKIN. MAINTENANCE REMOVED DME ANTENNA PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 53-10-2. INSTALLED DME ANTENNA PER MM 34-55-11 AND PERFSDR F3LA00103Fairing · crackedDEN - DURING C-7 CHECK, INSPECTION REPORTED A 2 INCH CRACK IN THE NR 2 ENGINE THRUST REVERSER FAIRING FORWARD WEB STIFFENER UNDER FIRE SEAL. MAINTENANCE REPLACED WEB ANGLE PER SRM''S 51-10-2, 51-40-3. 51-20-1, AND 51-10-1. (X)SDR F3LA00082Intercostal · crackedDEN - DURING C-7 CHECK, INSPECTION REPORTED A 1 INCH CRACK IN INTERCOSTAL AT LBL 5.7 FORWARD PRESSURE BULKHEAD BETWEEN WL 195 AND WL 194 BEHIND LANDING GEAR LEVER U SWITCH. MAINTENANCE REPAIRED CRACK PER SRM 53-10-11, FIGURE 8. (M)SDR F3LA00074Angle · crackedDEN - DURING C-7 CHECK, INSPECTION REPORTED CRACK IN LOWER AFT ANGLE OF C2 DOOR. MAINTENANCE REPLACED DAMAGED ANGLE PER SRM 51-40-3. (M)SDR F3LA00072Beam · crackedDURING C-7 CHECK INSPECTION REPORTED CRACK IN AFT CARGO DOOR LOWER REAR CROSSBEAM WEB. MAINTENANCE INSTALLED NEW LOWER REAR CROSSBEAM WEB CHORD PER SRM 51-30-2. (M)SDR F3LA00071Beam · crackedDURING C-7 CHECK INSPECTION, REPORTED AFT CARGO DOOR LOWER AFT BEAM INNER WEB CRACKED. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 51-40-3. (M)SDR F3LA00068Skin · crackedDEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN INTERIOR PANEL SKIN JUST FORWARD OF L-2 DOOR CENTER. MAINTENANCE FABRICATED REPAIR STRAP AND REPAIRED AREA PER EA 53-737-065. (M)SDR F3LA00043Web · tornDURNG C-7 CHECK INSPECTION, REPORTED WEB TORN BETWEEN BS 294 AND BS 312, BELOW TOP CHORD AT STIFFENER. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-10-2 AND 51-30-2. (M)SDR F3LA00055Frame · corrodedDEN - DURING C-7 CHECK, INSPECTION REPORTED E/E FRAME CORRODED AT BS 312, STRINGER 26L. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR SECTION PER SRM 51-40-3. (M)SDR F3LA00045Channel · crackedDEN - DURING C-7 CHECK INSPECTION, REPORTED 1.6 INCH CRACKED IN RIGHT ENGINE INBOARD FIXED COWL AT LAST RIB, UPPER CROSS U-CHANNEL. MAINTENANCE FABRICATED REPLACEMENT U-CHANNEL, SHIMS AND CORNER BRACE PER SRM 54-10-2. (M)SDR F3LA00059Angle · crackedDEN - DURING C-7 CHECK INSPECTION REPORTED CRACK IN AIRSTAIR DOOR TRACK SUPPORT ANGLE AT BS 351 STRINGER 22. MAINTENANCE REPAIRED TRACK SUPPORT ANGLE PER SRM 51-40-3. (M)SDR F3LA00058Structure · damagedDEN - DURING C-7 CHECK INSPECTION REPORTED A HOLE IN THE NR 2 ENGIEN INLET. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M)SDR F3LA00070Frame · crackedDURING C-7 INSPECTION, FOUND FRAME CRACKED IN RADIUS FORWARD OF E/E BAY DOOR AT BS 294.5, STRINGER 23R. MAINTENANCE REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-10-4. (M)SDR F3LA00057Mount · corrodedDEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON SUPPORTS AND MOUNTING SKIN OF AFT LAVATORY HEATED WATER DRAIN MAST, BS 987, STRINGER 23-24. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-10-2 FIG 5, 51-30-2 ASDR F3LA00042Web · crackedDEN - DURING C-7 CHECK INSPECTION, REPORTED CRACK IN LIGHTENING HOLE ON R-1 DOOR TORQUE BOX WEB. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-3. (M)SDR F3LA00069Track · crackedDEN - DURING C-7 CHECK INSPECTION REPORTED, CRACK IN RIGHT FORWARD CARGO DOOR TRACK INBOARD OF DOOR CENTER AT BS 460, STRINGER 27R. MAINTENANCE INSTALLED NEW TRACK AND NEW NUT PLATES ON TRACK TO ATTACH FLOORBOARDS PER SRM 53-20-1. (M)
Back to N271FL, cancelled Mar 20, 2003