Boeing 727-2A1
Service difficulty reports · 502
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 = '7272A1' 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 = '7272A1' 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 C8GA20090077Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THE NR 11 SPOILER UPPER TRAILING EDGE SURFACE HAS DELAMINATION. DAMAGED AREA WAS REMOVED DIM 1.5 INCH BY 3 INCH, FABRICATED REPAIR FILLER, FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WSDR C8GA20090076Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THE NR 12 SPOILER UPPER TRAILING EDGE SURFACE HAS DELAMINATION. DAMAGED AREA WAS REMOVED, FABRICATED REPAIR FILLER, FABRICATED DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS WERE NOTED. ASDR C8GA20090073Skin · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS 2 GOUGES WERE NOTED ON THE NR 8 SLAT T/E UPPER SURFACE OTBD HOOK. THE DAMAGED AREA WAS TRIMMED OUT. FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090074Skin · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS 2 GOUGES WERE NOTED ON THE NR 7 SLAT INBD HOOK. THE DAMAGED AREA WAS TRIMMED OUT. FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090072Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS A BULGE WAS NOTED IN THE LOWER FUSELAGE SKIN AT STATION 950E STR. 29R. THE DAMAGE WAS REMOVED DIM 6.5 INCH BY 4.312 INCH. FABRICATED FILLER, DOUBLER AND TRIPLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTEDSDR C8GA20090071Skin · tornWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER FUSELAGE SKIN IS TORN AT AIR STAIR FWD CUTOUT BS 1230. DAMAGE AREA WAS REMOVED DIM 1.5 INCH BY 2 INCH, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED.SDR C8GA20090070Angle · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE MAIN CARGO COMPARTMENT 9G BARRIER DOOR UPPER DOOR FRAME WAS DAMAGED. DAMAGED AREA WAS REMOVED DIM 9 INCH BY 1 INCH. INSTALLED NEW ANGLES P/N AE727-2-360-12 AND AE727-2-360-11. NO OTHER DSDR C8GA20090069Skin · puncturedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 1 ENGINE NOSE COWL LEADING EDGE EXTERIOR SKIN HAS A DEEP DENT PUNCTURE. DAMAGED AREA WAS REMOVED DIM 3 INCH BY 2 INCH. FABRICATED NEW REPAIR FROM 2024 T3 .063 INCH DIM 7 INCH BY 5 1/8 INCH, INSTALLED REPAISDR C8GA20090002Sensor · malfunctionedFLT 1705 FROM MSP TO TOL. AFTER LIFT OFF THE STALL WARNING STICK SHAKER CAME ON. AIRCRAFT RETURNED TO MSP WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. THE ANGLE OF ATTACK SENSOR AND THE STALL WARNING MODULE WAS REMOVED AND REPLASDR C8GA20090001Valve · inoperativeSHORTLY AFTER TAKEOFF THE CAPTAIN'S RMI OFF FLAG WITH HDG LIGHT ON COMPARATOR. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 2 COMPASS RACK AND RT FLUX VALVE WAS REMOVED AND REPLACED. OPS CHECK OF THE NR 2 SDR C8G2008F00011Connector · looseAFTER TAKEOFF DURING CLIMB OUT THE NR 1 GENERATOR EXPERIENCED A SPEED FAULT WITH THE NR 3 GENERATOR PREVIOUSLY DEFERRED. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. NR NR 1 CSD A SPEED SWITCH CONNECTOSDR C8G2008F00006Generator · malfunctionedAFTER TAKEOFF DURING CLIMB OUT, THE NR 1 GENERATOR EXPERIENCED A SPEED FAULT WITH THE NR 3 GENERATOR PREVIOUSLY DEFERRED. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. THE NR 1 CSD SPEED SWITCH CONNECTOSDR C8GA20080007Accessory Unit · malfunctionedFLT 706 FROM TOL TO MSP, AFTER TAKEOFF FROM TOL ,THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE LANDING GEAR ACCESSORY UNIT WAS AT FAULT. RESDR C8GA20070011Control Unit · malfunctionedFLT 738 FROM TOL TO SLW - DURING CRUISE OPERATION THE LOWER CARGO FIRE WARNING CAME ON. AIRCRAFT DIVERTED TO EVV, EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, LOWER CARGO COMPARTMENT WAS EMPTY NO DEFESDR C8GA20060018Warning System · false activationFLT 720 FROM TOL TO ATL, IN CRUISE APPROX 80 MILES NW OF ATL AT FL 270, THE LOWER AFT FIRE WARNING WENT OFF. CREW RAN APPROPRIATE CHECKLIST, EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT IN ATL. UPON LANDING THE AIRCRAFT WAS CHECKED AND NO EVIDENCE OF SSDR C8GA20060017Wire · shortedFLT 1711 FROM SAN TO TOL. DURING CRUISE OPERATION NR 1 ENGINE STARTER VALVE CONTROL LIGHT REMAINED ILLUMINATED. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED TO PHX. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE START VALVE AND START VALVE ANNUNICASDR C8GA20060001Engine · activatedFLT 737 FROM MMMY TO TOL. WHILE CLIMBING THRU 10,000 FEET NUMBER ONE ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN, EMERGENCY WAS DECLARED, AIRCRAFT WAS DIVERTED TO LRD AND LANDED WITHOUT INCIDENT. ENGINE WAS INSPECTED AND METSDR C8GA20050011Radome · lightning strikeFLT 716 FROM TOL TO MEM, DURING CRUISE OPERATION, AIRCRAFT FLEW THROUGH HEAVY WEATHER. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND LARGE HOLE IN RADOME APPROXIMATELY ONE FOOT IN DIAMETER. AFTER INSPECTION, DETERMINED TO BE LIGHTNING STSDR C8GA20050008Volt Regulator · inoperativeFLT 738 FROM MMIO TO MGDL. AFTER V1, NR 2 GENERATOR 3 LIGHT TRIP. COULD NOT RE-ESTABLISH BUS TIE BREAKER. RETURNED TO MMIO AND LANDED WITHOUT FURTHER INCIDENT. PLACED NR 2 GENERATOR/CSD ON MEL. AIRCRAFT RETURNED TO SERVICE. ON 3/13/05, REMOVED AND REPLACESDR C8GA20050006Line · rupturedFLT 721 FROM FLL TO RDU, AFTER TAKEOFF, BOTH "A" HYDRAULIC PRESSURE LOW LIGHTS ILLUMINATED FOLLOWED BY LOSS OF SYSTEM PRESSURE AND QUANTITY. AIRCRAFT RETURNED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. FOUND RUPTURED FLEXIBLE HYDRAULIC LINE TO NOSE GEAR ACTSDR C8GA20040028Engine · flamed outFLT 725 FROM PHL TO TOL, AFTER LANDING, WHILE ON ROLL-OUT, NR 3 ENGINE FLAME OUT OCCURRED. AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION. ICING CONDITIONS WERE NOTED BUT NO ICE INGESTION WAS EVIDENT. NO DAMAGE WAS NOTED IN ENGINE INSDR C8GA20040026Connector · looseFLT 737 FROM GDL TO MTY, ON TAKEOFF ROLL, NR 2 GENERATOR SHOWED UNDERVOLTAGE WITH ASSOCIATED THREE LIGHT TRIP. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DEFERRED NR 2 GENERATOR UNDER MEL 24-1. AIRCRAFT RETURNED TO SERVICE. TWO LEGS LATER IN TOSDR C8GA20040025Control Cable · out of adjustFLT 717 FROM ELP TO STL. NO RUDDER PEDAL STEERING DURING TAKEOFF. TAKEOFF ABORTED. AIRCRAFT RETURNED TO BLOCKS WITH NO FURTHER INCIDENT. PLACED RUDDER PEDAL STEERING ON MEL 32-14, CONTROL NUMBER 12-01-01-C-11. AIRCRAFT RETURNED TO SERVICE. ON 12/02/04, ASDR C8GA20040014Smoke Detector · defectiveFLT 707 FROM KPHX TO KMCI. DURING CRUISE, THE LOWER AFT CARGO FIRE WARNING CAME ON. FOLLOW ALL CCIA AOM ABNORMAL PROCEDURES, CONTACTED ATC AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO KGCK AND LANDED WITHOUT INCIDENT. UPON LANDING, THE AIRCRAFT WAS THENSDR C8GA20040006Bolt · mislocatedON WALK AROUND IN KDEN, FOUND THE LT MAIN GEAR BOLT DOWNLOCK LINK PIVOT IMPROPERLY INSTALLED AS PER BOEING IPC 32-10-01-04. A SPECIAL MAINTENANCE FERRY FLIGHT WAS ISSUED ON 6-14-2004 FROM KDEN TO KTOL. PRIOR TO FLIGHT, A VISUAL INSPECTION WAS PERFORMED IN THSDR C8GA20040004Indicator · failedFLT 1815 FROM KEWR TO KTOL. AT FL310 NR 2 ENGINE DISPLAYED EXCESSIVELY HIGH OIL TEMPERATURE, DESCENDED TO FL240 AND RAN ALL APPLICABLE CCIA CHECKLIST. IN-FLIGHT SHUT DOWN OF THE NR 2 ENGINE AS A PRECAUTIONARY, ADVISED ATC AND DECLARED EMERGENCY. AIRCRAFT LANDESDR C8GA20030028B-Nut · looseFLT 737 FROM MMGL TO MMMY. DURING CLIMB, THE NR 1 ENGINE EPR INDICATION WENT EXCESSIVELY HIGH. AIRCRAFT DIVERTED TO KBRO AND LANDED WITHOUT INCIDENT. UPON LANDING, FOUND THE B-NUT ON THE PT-2 LINE AND A SENSE LINE ON THE PRVC LOOSE. TIGHTENED BOTH LINES AND ASSDR C8GA20030026Adc · faultyFLT 738 FROM TOL TO SLW. SHORTLY AFTER TAKEOFF, THE CAPTAIN'S ALTIMETER AND THE ALTITUDE ALERTER FLAGGED AND THE AUTOPILOT WOULD NOT ENGAGE. THE CREW TRIED CYCLING THE CIRCUIT BREAKER FOR THE AIR DATA COMPUTER BUT IT WOULD GO OFF AGAIN AFTER ONE SECOND. NO SDR C8GA20030024Access Panel · openFLT 738 FROM TOL TO MMIO. DURING CLIMB OUT THROUGH FL270 A NOISE VIBRATION COMING FROM OUTSIDE RIGHT COCKPIT CAUSING AIRCRAFT TO GIVE ABNORMAL CRUISE READING. NOISE INCREASE WITH AIRSPEED INCREASE, NOSE GEAR LIGHT INDICATED CORRECTLY AT THIS TIME. HOWEVER, NOSSDR C8GA20030023Accessory Unit · defectiveFLT 711 FROM DEN TO TOL. ON TOUCHDOWN IN TOL, THE LT, RT & NOSE RED GEAR UNSAFE LIGHTS CAME ON IN CONJUNCTION WITH THE THREE LIGHTS. INITIATED GO AROUND, RECYCLE GEAR AND GREEN LIGHTS CAME ON. AGAIN ON TOUCHDOWN, THE THREE RED GEAR UNSAFE LIGHTS CAME ON. RECYCSDR C8GA20030015Sensor · defectiveFLT 707 FROM PHX TO TOL. THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. FOLLOWED ALL CCIA PROCEDURES AND THE LOWER BODY OVERHEAT LIGHT REMAIN ON. ADVISED CCIA FLIGHT FOLLOWING AND ATC IN PHX OF THE PROBLEM AND AIR TURN BACK TO PHX. AIRCRAFT LANDESDR C8GA20030007Indicator · defectiveFLT 723 FROM ROC TO TOL. AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATOR INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO ROC AND AIRCRAFT LANDED WITHOUT INCIDESDR C8GA20020006Rod End · brokenFlight DAE001 from MIA to PTY. After takeoff during climb, crew could not keep aircraft level. Applied 5 units of trim and left rudder required to maintain level flight. Aircraft returned to MIA and landed without further incident. Upon landing found 2 rigSDR UPS02237913Light · inoperativeINSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT AND OPS CHECK NORMAL IAW B727 MM 33-50-101.SDR UPS01237375Battery · dischargedINSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD.SDR C8GA20010018Indicator · overheatedFLT 739 FROM DEN TO MCI. UPON APPROACHING THE PARKING RAMP AREA AFTER LANDING IN MCI, SMOKE WAS OBSERVED RISING FROM CENTER PEDESTAL OF THROTTLE QUADRANT. FLIGHT ENGINEER DEPOWERED AIRCRAFT COMPLETELY AND MAINTENANCE PERSONNEL ARRIVED TO TROUBLESHOOT THE AIRSDR UPS01237193Bulkhead · corrodedINSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT STANDING ON AIRSTAIRS JUST O/B OF NR 2 ENGINE GENERATOR FEEDER CABLES NUMEROUS FASTENERS ARE CORRODED AS IS A STIFFENER. CLEANED AND TREATED SDR UPS01236956Mechanism · out of rigON DEPARTUE FROM LAN AT GEAR RETRACT (GEAR HANDLE UP) RED DOOR LIGHT (FRONT) AND " LEFT GEAR DOOR" ILLUMINATED, PER CHECKLIST RECYCLED O F GEAR (BACK DOWN) RED "LT GEAR AND RT GEAR" AND "LT GEAR DOOR AND R T GEAR DOOR ILLUMINATED. PER CHECKLIST LEFT GEAR HANDSDR C8GA2001017Probe · cloggedFLT 287 FROM MCO TO MCO PART 91 TRAINING FLIGHT. ON TAKEOFF ROLL NO AIRSPEED INDICATION ON FIRST OFFICER'S INSTRUMENT. DISCONTINUED TAKEOFF AND RETURNED TO BLOCK WITHOUT INCIDENT. PERFORMED PITOT LEAK TEST AND FOUND FOD ON FIRST OFFICER PITOT PROBE. REMOVESDR UPS01236767Window · crackedINSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11.SDR UPS01236380Light · malfunctionedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR ILLUM IN FLIGHT. *S/D* REMOVED AND REPLACED ENTRY DOOR EMERGENCY EXIT LIGHT GROUND OPS NORMAL.SDR UPS01236195Wire · brokenINSPECTION TYPE:C, AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA 560 PER WDM 20-30-12 OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00, OPS CHECKED GOOD.SDR UPS01236193Wire · brokenINSPECTION TYPE:N/A AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA-560 PER WDM-20-30-12. OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00. OPS CHECKS GOOD.SDR UPS01236152Battery · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES.SDR C8GA20010005Gcu · contaminatedFLT BX742 FROM TOL TO OMA. NR 1 IN LINE FOR TAKEOFF, NR 1 GENERATOR HAD A 3 LIGHT TRIP WITH A BRIEF LOSS OF NR 2 & 3 GCB''S AND ESSENTIAL POWER (SELECTED ON NR 3 AT THE TIME). CREW REPORTED SMELLING SMOKE IN THE COCKPIT. AIRCRAFT RETURNED TO BLOCKS WITHOUT SDR UPS01235476Web · crackedINSPECTION TYPE: C, TWO CRACKS AND ONE MISSING FASTENER ON UPPER FLANGE OF WEB BETWEEN BS 400 AND BS 420, WL 206, BL 0. REMOVED WEB AND L ANGLE FABRICATED NEW WEB AND L ANGLE AND INSTALLED IAW SRM 51-10-3, 51-20-1, 51-20-2 AND 51-20-15SDR UPS01235403Terminal · damagedAMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED PER MEL 52-4 AND COMPLIED WITH DMP VERIFYING THAT MAIN CARGO DOOR CLOSED AND LOCKED PRIOR TO DEPARTURE. ITEM DEFERRED M211761 PLACARD INSTLD SDR UPS01235460Stiffener · corrodedINSPECTION TYPE:C CORROSION IN RT MLG WW ON STIFFENER AND LOWER CHANNEL AT BS 919, WL 188, RBL 65 REMOVED CORRODED STIFFENER, FABRICATED AND INSTALLED PER SRM 51-10-6, 51-30-2, 51-10-1 AND BOEING DRAWING 65-16335 PL AND SHT 2 AT BS 919, WL 188, RBL 65SDR UPS01235041Line · leakingINSPECTION TYPE:PFLT 1ST OBS 02 PRESS LINE LEAKING. *S/D* REMOVED CAP AND INSTALLED NEW O2 FLEX LINE (P/N 10-60174-36) (SP0707172) PER M/M 35-00-00/201-204. INSTALLED DEMAND DILUTER REGULATOR AND TESTED PER M/M 35-11-31, LEAKED CK''ED BOTH LINE AND REGULATSDR UPS01235239Skin · crackedINSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. REPAIRED PER SRM 57-50-4.
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