Boeing 727-277
Service difficulty reports · 627
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 = '727277' 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 = '727277' 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 97FDEA00184Fitting · corrodedNR 0467 008, WHILE WORKING CARD NR 7-5530-7-2310 F, FOUND CORROSION ON LT AND RT AFT CLOSURE RIB FITTING; CORROSION LOCATED AROUND BUSHING OUTSIDE DIAMETER. *S/D* REMOVED AND REPLACED LT AND RT AFT CLOSURE RIB FITTINGS IAW FED-EX EA NR 7-5510-32916.SDR 97FDEA00183Flap · disbondedNR 0470 007, RIGHT WING I/B AFT FLAP HAS SEVERAL DENTS ON THE MID SECTION OF UPPER SKIN. *S/D* REPAIRED RIGHT WING I/B AFT FLAP DENTS IAW FED-EX SRM 51-40-6.SDR 97FDEA00182Flap · disbondedLEFT INBOARD FOREFLAP IS DAMAGED AND DISBONDED AT INBOARD LOWER CORNER.SDR 97FDEA00179Reinforce Chord · corrodedNR 0086 003, CORROSION (C53-224-08) ON REINFORCEMENT CHORD AT BS 1176, LBL 48 AND 60, WL 208. *S/D* REMOVED CORROSION ON CHORD, FOUND TO BE OUT OF LIMITS PER FEX 727 SRM 53-10-1. REMOVED DAMAGED AREA, REPAIRED STA 1176 LT PER BOEING DRAWING NR 65C33557.SDR 97FDEA00177Flap · dentedNR 0469 006, REMOVED DAMAGE 5.5 BY 1.5 OF DAMAGE RIGHT WING I/B AFT FLAP UPPER SURFACE APPROXIMATELY 2.5 O/B OF I/B END.SDR 97FDEA00175Frame · crackedNR 0169 005, CRACK IN FRAME AT BS 640, RBL 13, WL 154. *S/D* REPAIRED CRACKED FRAME IAW FED-EX SRM 53-10-4.SDR 97FDEA00176Shear Tie · corrodedNR 0163 004, CORROSION (C53-113-01) ON SHEAR TIE IN DISTRIBUTION BAY AT BS 720E BETWEEN STR 26 AND 25 RT. *S/D* REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED PER FED-EX SRM 53-10-4.SDR 97FDEA00174Stringer · corroded0238 002, CORROSION (C53-113-01, 2) ON STRINGER 30, BL 0 AT BS 1100 AND 1120. *S/D* REMOVED DAMAGED STRINGER AT BS 1080 TO 1140, STR 30 AND REPAIRED IAW FED-EX SRM 53-10-3.SDR AU970244Compressor · stalled(AUS) NO2 ENGINE COMPRESSOR STALL.SDR 97FDEA00186Skin · corrodedNR 0084 010, BULGES IN EXTERNAL SKIN AT BS 1104 AND 1124, STR 30. *S/D* REMOVED DAMAGED SKIN AT BS 1104 AND 1124, REPAIRED AS PER FED-EX SRM 53-30-03.SDR 97FDEA00180Midflap · delaminatedNR 0345 003 L/W INBOARD MIDFLAP TIE WEDGE CORRODED IN SEVERAL PLACES ON UPPER SURFACE. REPAIRED CORRODED AREAS ON UPPER SURFACE OF LT WING INBOARD MIDFLAP TIE IAW FED-EX SRM 51-40-6.SDR 97FDEA00151Floorbeam · corrodedNR 0465 002 CORROSION (53-224-01) ON BS 344 FLOORBEAM BETWEEN RBL 12 AND LBL 55, WL 208. REMOVED UPPER CHORD ON FLOORBEAM AT BS 344, RBL 4 - LBL 65, WL 208 AND FABRICATED NEW UPPER CHORD AND SPLICE ANGLES PER FED-EX DRAWING SR 27-53-007. INSTALLED FASTENERS PSDR 97FDEA00144Floorbeam · corrodedNR 0167 001 CORROSION ON FLOORBEAM BS 1130, RBL 54 TO LBL 54 UNDER NUTPLATE CLIPS WL 200. REMOVED DAMAGED PART AT BS 1130. FABRICATED REPAIR PARTS ALODINED, PRIMED, DRILLED, PAINTED AND INSTALLED PER FED-EX EA NR 7-5310-32960 AT BS 1130, RBL 54 TO LBL 54.SDR AU970453Fuselage · corroded(AUS) FUSELAGE CONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTIONSDR CA970428009Main Gear Box · failed(CAN) ENGINE WOULD NOT START. DISASSEMBLY OF MAIN GEARBOX FOUND THE PROBLEM TO BE THE DISPLACEMENT OF THE BEVEL DRIVE AND THE SPUR GEAR SHAFT REAR BEARING LINER. THE THREE PINS SECURING THIS LINER SHEARED ALLOWING THE LINER AND THE GEAR SHAFT TO MOVE FORWARD. SDR AU970697Adc · faulty(AUS) NO1 AIR DATA COMPUTER FAILED. WORKSHOP INSPECTION FOUND THAT THE PITOT AND STATIC TRANSDUCERS FAILED THE CALIBRATION TEST BUT WERE NOT CONSIDERED TO BE THE CAUSE OF THE FAILURE. FURTHER INVESTIGATION FOUND A DRY SOLDER JOINT ON ONE OF THE DC POWER SUPPLYSDR 97FDEA00115Beam · corrodedNR 0674 12, CORROSION IN GEAR BEAM AT O/B BOLT HOLE NR 4 FLAP TRACK ATTACH HOLE. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED NEW BUSHING AND SPECIAL WASHER PER EA 7-5710-28983 DATED 2/10/97.SDR 97FDEA00114Beam · corrodedNR 0673 011, CORROSION IN I/B HOLE IN GEAR BEAM FOR NR 4 FLAP TRACK ATTACH. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED BUSHING PER EA 7-5710-28983 DATED 2/10/97.SDR 97FDEA00107Stringer · crackedNR 0693 009, ICE LIGHT RT SIDE STA 720B FWD STRINGER END CRACKED. INSTALLED NEW SECTION OF STRINGER AT STA 720B, STR 15R FWD OF LIGHT PER SRM 53-10-3.SDR 97FDEA00108Stringer · crackedNR 0056 008, STR 21L HAS DOUBLE AND TRIPLE DRILLED HOLES IN SIDE OF STR BETWEEN STA 460 AND 480. REPAIRED STR 21L IAW SRM 53-10-3 FIG 1.SDR 97FDEA00104Stringer · crackedNR 0714 012, STR 15L CRACKED AT STA 720B AND 5, FWD OF EXTERIOR LIGHT HOUSING. INSTALLED STR U-CHANNEL REPAIR PER SRM 53-10-3.SDR 97FDEA00102Floorbeam · corrodedNR 0785 010, STA 1070 RBL 50, FLOORBEAM HAS CORROSION AROUND NUTCLIP HOLE. REPAIRED FLOORBEAM WITH DOUBLERS, CUTOUT DAMAGED AREA AND REPLACED WITH FILLER PER SRM 53-10-8.SDR 97FDEA00106Support · corrodedNR 1038 015, COCKPIT FLIGHT ENG'S SEAT AFT TRACK SUPPORT BEAM UNDER FLOOR PNL CORRODED. INSTALLED NEW SEAT TRACK SUPPORT BEAM PER SRM 51-10-1.SDR 97FDEA00105Stringer · crackedNR 0715 013 STR 15L IS CRACKED AT STA 720B AND 15, AFT OF EXTERIOR LIGHT FIXTURE. STOP DRILLED CRACK IAW SRM 51-10-01. REPAIRED STR 15L IAW SRM 53-10-3.SDR 97FDEA00103Floorbeam · corrodedNR 0782 011, STA 1130 RBL 60 FLOORBEAM HAS CORROSION AND PIECE OF FLOORBEAM GROUND OFF BELOW SEAT TRACK. REMOVED CORROSION, TREATED AND PRIMED AREA, INSTALLED ANGLE REPAIR PER EA 7-5310-28980 DATED 2-4-97.SDR 97FDEA00111Stringer · crackedLOWER FWD CARGO STRINGER 25L CRACKED AND DAMAGED BETWEEN STA 620 TO 640. STOPPED DRILLED CRACKS AND ROUTED OUT DAMAGE. CONFIRMED BY DYE-PENETRANT INSPECTION. INSTALLED STRINGER U-CHANNEL REPAIR DOUBLER PER SRM 53-10-3.SDR 97FDEA00109Doubler · corrodedNR 1068 006, LOWER FWD CARGO LEVELING COMPOUND IS RAISING UP O/B SIDE OF STR 27R STA 520 TO 540. CORROSION FOUND UNDER LEVELING COMPOUND. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-30-3.SDR 97FDEA00113Floorbeam · corrodedNR 0379 001, UPPER LOBE STA 344 FLOORBEAM CORRODED AT CLIP NUTS HOLES, LBL 35 TO LBL 40. REMOVED CORRODED SECTION OF FLOORBEAM AND INSTALLED REPAIR PER DRAWING SR 27-53-007.SDR 97FDEA00112Stringer · crackedNR 0328 002, FUSE STRINGER 3L BENT AND CRACKED IN UPPER LEG AT FUSE STA 1040. CRACK LENGTH APPROX 0.312. STRAIGHTENED STRINGER AND STOP DRILLED ENDS OF CRACK, CONFIRMED BY DYE PENETRANT INSP. INSTALLED REPAIR DOUBLER TO STRINGER 3L UPPER LEG PER SRM 53-10-3SDR CA970203015Engine · failed(CAN) ON #3 ENGINE START N2 IMMEDIATELY ROSE TO 35 PERCENT THEN DROPPED TO 30 PERCENT AND FLUCTUATED. NO N1 ROTATION. OIL QUANTITY DROPPED TO ONE GALLON. ENGINE REPLACED.SDR 97FDEA00042Accessory Unit · failedLANDING GEAR WOULD NOT RETRACT UNLESS WE USED LATCH LEVER RELEASE. REMOVED AND REPLACED GEAR ACCESSORY UNIT IAW 32-09-121 PG 401, FUNCTIONAL TEST GOOD IAW 32-09-122 PG 501 TO 505.SDR 97FDEA00037Sensor · dirtyGEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. RETRACTED GEAR USING LEVER LOCK OVERRIDE. GEAR EXTENDED NORMALLY FOR LANDING. FOUND ICE ON AIR GROUND SAFETY SENSOR. CLEANED AND LUBED AS REQUIRED.SDR CA970117004Rudder Tab · delaminated(CAN) LOWER RUDDER TRIM TAB DELAMINATED. REPLACED.SDR 96FDEA01699Window · failed sealerPASSING THROUGH 10,000 FT WITH CABIN AT 30 PSI AIR SPEED GOING THROUGH 300 KTS A LOUD NOISE FOLLOWED BY A WHISTLING CAME FROM CAPTAINS L1 WINDOW LEFT SIDE. FOUND TAPE HAD COME OFF OUTSIDE OF L 1 WINDOW EXPOSING UNCURED SEALANT. CLEANED SEALANT FROM A/C FUSELSDR CA960916019Door · req adjust(CAN) UNABLE TO MAINTAIN PRESSURIZATION AT 20,000 FEET TORQUE TUBE AND LOWER ADJUSTMENT ARM ADJUSTED. TEST SERVICEABLE.SDR AU961175Atomizer · holed(AUS) NO3 ENGINE COMBUSTION CHAMBER NO4 ATOMISER HOLED - FOUND DURING BORESCOPE INSPECTION IAW PWJ-72-40-72SDR 96FDEA01339Pos Transmitter · malfunctionedSPLIT FLAP ON T/O, ON RETRACT TO 5 OUTBOARD FLAPS STOPPED AT 15 INBOARD FLAPS TO 5. ACCOMP EMERGENCY PROCED FLAPS EXTENDED NORMAL TO 30 DEGREE AND RECOVERED AT IND. F/F O/B FLAP POS IND. RAN FLAPS, FOUND O/B NEEDLES SPLIT AND OUT OF BAND AT POSITION EO DEGRSDR CA960715006Sequence Valve · cracked(CAN) ON DEPARTURE A SYSTEM HYDRAULIC FLUID LOST. LH MLG DOOR LOCK OPERATED SEQUENCE VALVE HOUSING CRACKED. REPLACED.SDR 96FDEA01163Connector · dirtyLT MGD RED LIGHT REMAINED ON AFTER RAISING GEAR. ACCOMPLISHED RED PAGES PROCEDURES, LIGHT WENT OUT AFTER RECYCLING GEAR. LIGHT FLICKERED AGAIN IN CRUISE, SLOWED TO 270 KNOTS LIGHT CONTINUED TO FLICKER THROUGHOUT FLIGHT. FOUND PLUG FOR DOOR SWITCH UNLOCKED. SDR AU960980Piston · fractured(AUS) NO6 LEADING EDGE KRUEGER FLAP ACTUATOR PISTON PNO 1110-15 BROKEN IN TWO IN THE RADIUS OF THE EXTENDED LOCKING KEY GROOVESDR AU960765Skin · corroded(AUS) REAR FUSELAGE LOWER SKIN CONTAINED EXFOLIATION CORROSION AT FUSELAGE STATION 1050 AND BENEATH STRINGER 27 - DURING PROBING INSPECTION SKIN BROKE AWAY LEAVING A 12.7MM (0.5IN) HOLE - SUSPECT CAUSED BY SALT WATER SPILLAGESDR 96FDEA00805Skin · damagedDAMAGED EXTERIOR SKIN AT BS 295 STR 11 RT. CUT OUT DAMAGED SKIN AND REPAIRED IAW SRM 53-30-3 AND ER NR 041986JDW.SDR 96FDEA00803Stringer · corrosionCORROSION (C53-113-01) BS 1098 TO 1070 STR 29R. REMOVED AND REPLACED CHANNEL AT BS 1070 TO 1098 AT STR 29R, ALL WORK DONE IAW FEDEX SRM 51-30-2.SDR 96FDEA00790Skin · dentTWO DENTS ON SKIN BS 344 STR 19 RT, .5 BY .065 DEPTH OUT OF LIMITS. CUT OUT DAMAGED AREA ON SKIN BS 344 STR 19 RT, FABRICATED REPAIR PARTS, INSTALLED COUNTER SINK FILLERS AND FASTENED INTO PLACE WET WITH SEALENT. ALL WORK ACCOMPLISHED PER FEDEX SRM 53-30-3.SDR 96FDEA00789Skin · corrosionCORROSION (C53-100-01, -4) ON EXTERNAL SKIN AT BS 1052 STR 28L. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGE AND REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3.SDR 96FDEA00786Stringer · corrodedNR0338 AND 004 STR 28L AT BS 1052 IS CORRODED. REPAIRED STR AT 28L BS 1052 REMAINING FASTENERS TO BE INSTALLED ON NR0119. ALL WORK DONE IAW FEDEX SRM 53-10-3.SDR 96FDEA00765Frame · gougedMCD AFT SIDE FRAME IS GOUGED ON PREVIOUS REPAIR DOUBLER 17 INCHES UP FROM THE BOTTOM OF DOOR. *S/D* REPLACED REPAIR DOUBLER PER DWG SR 27-52-009.SDR 96FDEA00764Frame · gougeMCD FWD SIDE FRAME IS GOUGED 56 INCHES UP FROM THE BOTTOM OF THE DOOR. *S/D* REPAIRED FRAME PER EA 7-5230-28057.SDR 95FDEA00763Stringer · corrosionCORROSION (C53-113-01) BS 1098 TO 1070 STR 24R. *S/D* REMOVED AND REPLACED CHANNEL AT BS 1070 TO 1098 AT STR 29R. ALL WORK DONE IAW FEDEX SRM 51-30-2.SDR AU960332Probe · blocked(AUS) NO1 ENGINE PT2 PROBE BLOCKED WITH INSECT REMAINS
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