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.

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.Oct 22, 2002 · N271FL · Boeing 7372L9 · Fuselage, Seat/Cargo Attach FittingsSDR 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 02-1333Oct 21, 2002 · N271FL · Boeing 7372L9 · Cargo/Baggage DoorsSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Wing, Plate/SkinSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor BeamSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Galley DoorsSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor BeamSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Floor BeamSDR F3LA200200341Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD SPLICE STRAP, BS 772, WL 157. REPLACED STRAP PER SRM 51-30-2.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR F3LA200200340Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SPLICE, BS 504, WL 155. REPLACED STRAP PER SRM 51-30-02.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, FrameSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Passenger/Crew DoorsSDR 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.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/SkinSDR F3LA200200334Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD SERVICE DOOR CUTOUT SKIN CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM 53-30-3.Oct 8, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/SkinSDR 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,Sep 29, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, StructureSDR 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 2Sep 29, 2002 · N271FL · Boeing 7372L9 · Fuselage Main, StructureSDR 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.Aug 29, 2002 · N271FL · Boeing 7372L9 · Fire DetectionSDR 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.Aug 24, 2002 · N271FL · Boeing 7372L9 · Fire DetectionSDR 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 IDLEAug 24, 2002 · N271FL · Boeing 7372L9 · Fire DetectionSDR 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 RUNov 30, 2001 · N271FL · Boeing 7372L9 · Air Distribution SystemSDR 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 BURNINov 30, 2001 · N271FL · Boeing 7372L9 · Air Distribution SystemSDR 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 PANov 14, 2001 · N271FL · Boeing 7372L9 · Cabin Temperature ControllerSDR 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 Oct 22, 2001 · N271FL · Boeing 7372L9 · Drag Control ActuatorSDR 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 TESSep 24, 2001 · N271FL · Boeing 7372L9 · Trailing Edge Flap Control SystemSDR 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.Aug 21, 2001 · N271FL · Boeing 7372L9 · Hydraulic System, MainSDR 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.Jun 25, 2001 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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.Apr 23, 2001 · N271FL · Boeing 7372L9 · AileronsSDR 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 BEJan 21, 2001 · N271FL · Boeing 7372L9 · Engine (Turbine/Turboprop)SDR 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 Jan 9, 2001 · N271FL · Boeing 7372L9 · Drag Control SystemSDR 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 FIREJan 5, 2001 · N271FL · Boeing 7372L9 · Fire DetectionSDR 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 REPLACEDDec 15, 2000 · N271FL · Boeing 7372L9 · Air Distribution FanSDR 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)May 31, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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 PERFMay 26, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, Plate/SkinSDR 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)May 21, 2000 · N271FL · Boeing 7372L9 · Engine Thrust ReverserSDR 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)May 5, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage DoorsSDR 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)Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage DoorsSDR 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)Apr 29, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage DoorsSDR 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)Apr 27, 2000 · N271FL · Boeing 7372L9 · Passenger/Crew DoorsSDR 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)Apr 20, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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)Apr 20, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, FrameSDR 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)Apr 18, 2000 · N271FL · Boeing 7372L9 · Nacelle/Pylon StructureSDR 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)Apr 17, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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)Apr 17, 2000 · N271FL · Boeing 7372L9 · Nacelle/Pylon StructureSDR 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)Apr 16, 2000 · N271FL · Boeing 7372L9 · Fuselage Main, FrameSDR 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 AApr 16, 2000 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 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)Apr 15, 2000 · N271FL · Boeing 7372L9 · Passenger/Crew DoorsSDR 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)Apr 14, 2000 · N271FL · Boeing 7372L9 · Cargo/Baggage Doors
Back to N271FL, cancelled Mar 20, 2003