Boeing 737-281
Service difficulty reports · 120
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 = '737281' 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 = '737281' 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 ABXA201004120047Beam · crackedRIGHT ENGINE PYLON OUTBOARD BEAM THAT RUNS ACROSS LOWER PART OF HYD BAY ACCESS DOOR IS CRACKED AT 3RD NUT PLATE HOLE FROM FWD END. REMOVED DAMAGED SECTION OF RIGHT ENGINE OUTBOARD PYLON BEAM IN LOWER PART OF HYD BAY ACCESS DOOR AND SPLICED. REPAIRED PER REA SDR CA041105003Fire Loop · inoperative(CAN) ENGINE NR 1 FIRE WARNING AT 8000 ASL ON APPROACH. FIRE BOTTLES AND SQUIBS REPLACED IAW MM. NR 1 LOWER FIRE LOOP REPLACED AND CONNECTOR D1098 IAW MM. SYSTEM TESTED SERVICEABLE.SDR CA040825010Line · ruptured(CAN) HYDRAULIC QUANTITY INDICATOR SHOWED RAPID DEPLETION TO 1 GAL AFTER TAKEOFF. FOUND RUPTURED HYDRAULIC LINE P/N BACH8B04NN0214T IN NOSE LANDING GEAR WHEEL WELL.LINE REPLACED IAW 20-10-52. ENGINE HYDRAULIC CASE DRAIN FILTERS CHECKED FOR METAL CONTAMINATION,SDR CA031208004Control Valve · malfunctioned(CAN) ON CLIMB OUT THROUGH 25,000 FT. FLIGHT CREW REPORTED, DUCT OVERHEAT ON RT PACK. COULD NOT CONTROL TEMPERATURE WITH RT PACK ON. AIRCRAFT LOST ALL PRESSURIZATION AT ABOUT 25,000 FT. AND COULD NOT CONTROL CABIN PRESSURE IN MANUAL. CREW CONTACTED ATC AND COSDR CA030902002Circuit Board · failed(CAN) AIRCRAFT REPORTS SHORTLY AFTER TAKE OFF ROTATION, NUMEROUS THREE PHASE CIRCUIT BREAKERS (2 AND 3 THRUST REVERSER, GASPER FAN AND PANEL INSTRUMENT INDICATOR NR 1 DC) POPPED CAUSING LOSS OF SEVERAL SYSTEMS AND ANNUNCIATIONS. NR 2SDR CA030611002Pcu · broken(CAN) DURING LANDING THROUGH APPROXIMATELY 60 KNOTS, AIRCRAFT EXPERIENCED A COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. (NOTE: 'A' PUMPS ON WITH LOW PRESSURE LIGHTS ILLUMINATED - MAX 1.5 MINUTES) MAINTENANCE INSPECTION REVEALED POSITION NR 1 LOWER AILERON PCU FILTSDR CA030313007Engine · failed(CAN) FLIGHT 41, NR 1 ENG FAILURE ON CLIMBOUT SHORTLY AFTER TAKEOFF THROUGH 3200 FT ASL, CREW HEARD A BANG FROM NR 1 ENG AFTER CLIMB THRUST WAS SET & FLAPS HAD RETRACTED. CREW IDENTIFIED PROBLEM AS NR 1 ENG NOT PRODUCING THRUST & THE 'EGT' WAS PEGGED HIGH OFFSDR CA030224003Fire Loop · malfunctioned(CAN) CREW REPORTED, AT CRUISING ALTITUDE, 20 MINUTES OUT OF YLW THEY EXPERIENCED A VIBRATION FOLLOWED BY AN APU FIRE WARNING. CREW SHUTDOWN APU WITH THE FIRE HANDLE AND APU FIRE BOTTLES WERE DISCHARGED. A/C COMPLETED AN (ABNORMAL LANDING CONFIGURATION) IN YLSDR CA021209007Bolt · cracked(CAN) ON APPROACH FLIGHT CREW REPORTED UPON SELECTION OF FLAPS TO NR 1 POSITION THE NR 4 SLAT HUNG UP UNTIL FLAPS WERE SELECTED TO '15' POSITION. ALL INDICATIONS WERE NORMAL AFTER FLAPS '15' SELECTION AND NO CONTROL DIFFICULTIES. MAINTENANCE INSPECTION REVEALESDR CA020823003Housing · split(CAN) ON APPROACH CREW REPORTED COMPLETE LOSS OF HYD FLUID FROM 'A' SYS UPON SELECTION OF FLAPS & MLG. CREW CONDUCTED MISSED APPROACH & PROCEEDED TO COMPLETE 'LOSS OF SYS HYDRAULICS NON NORMAL CHECKLIST. CREW PERFORMED VISUAL APPROACH & LANDED A/C WITHOUT INSDR CA020429003A/C Pack · smoke(CAN) SHORTLY AFTER TAKOFF, F/A NOTIFIED CREW BOTH SMOKE DETECTORS HAD ACTIVATED AND THERE WAS A SMELL OF SMOKE IN THE CABIN. AIRCRAFT IMMEDIATELY RETURNED TO YYC AND DID AN OVERWEIGHT LANDING - MAINTENANCE INSPECTION FOUND CAUSE OF ODOUR FRON LEFT HAND AIR COSDR CA020422006Structure · damaged(CAN) DURING REGULAR SCHEDULED MAINTENANCE INSPECTION (AD:02-01-01)THE RT ELEVATOR FAILED THE TAB HINGE FREEPLAY CHECK AT THE NR 2 ELEVATOR TAB HINGE POSITION - SUSPECTED CRACK AT ELEVATOR REAR SPAR. EDDY CURRENT INSPECTION CARRIED OUT ON RT ELEVATOR REAR SPARSDR CA020405001Structure · cracked(CAN) SCHEDULED MAINTENANCE;DURING REGULAR SCHEDULED MAINITENANCE INSPECTION, MAINTENANCE ENGINEER SUSPECTED A CRACK AT THE NOSE LANDING GEAR ACTUATOR ATTACH SUPPORT BRACKET (FORWARD SIDE UPPER R/H SIDE). NDT CALLED IN AND 3/8 INCH CRACK CONFIRMED BY HFEC METHSDR CA020319004Duct · missing(CAN) SHORTLY AFTER DEPARTING, FLIGHT CREW RECEIVED A NR 1 ENGINE OVERHEAT INDICATION AND IMMEDIATELY RETURNED TO BASE - AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED THE CLAMP FOR THE 8TH STAGE ANTI ICE VALVE WAS MISSING AND THE BLEED DUCTSDR CA020204002Bullet · separated(CAN) FLT CREW RPTED DURING CLIMB AFTER TAKEOFF THEY EXPERIENCED SERIES OF LOUD BANGS FROM NR 2 ENGINE ACCOMPANIED BY ABNORMAL HIGH EGT & LOW N 2 RPM. ALL IND.S WERE NORMAL PRIOR TO NOICE. PROBLEM OCCURRED AFTER CLIMB THRUST SET. THE CREW REDUCED NR 2 THRUST SDR CA010907014Tire · separated(CAN) RECAP SEPARATED FROM TIRE ON TAKEOFF FROM YVR WAS NOT NOTICED UNTIL AIRCRAFT ARRIVED IN YLW. NO OTHER REPORTABLE DAMAGE AS A RESULT OF THIS INCIDENT.SDR CA010921007Engine · failed(CAN) ENROUTE FROM YVR TO YYC EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE. UPON ESTABLISHING CRUISE POWER SETTNG, CREW HEARD LOUD POP, FOLLOWED 20 SEC LATER BY ANOTHER POP (SEVERE COMPRESSOR STALL) & ASSOCIATED NR 1 ENGINE PRESSURE RATIO (EPR), N1 POWER SURSDR CA010625028Connector · misinstalled(CAN) IN TROUBLE SHOOTING A HISTORY OF INTERMITTENT ANTI-SKID PROBLEMS IT WAS DISCOVERED THAT THE HYDRAULIC BRAKE PRESSURE LINES FROM THE AIRFRAME TO THE TOP OF THE R.H LANDING GEAR SWIVELS THE CONNECTORSTOTHE WHEEL SPEED TRANSDUCERS WERE SWAPPED TO THE OPPOSISDR CA010406005Connector · damaged(CAN) THE AIRCRAFT WAS DEPARTING WHEN THE CREW EXPERIENCED AN APU FIRE INDICATION. THEY FOLLOWED PROCEDURES INCLUDING DISCHARGING THE EXTINGUISHER BOTTLE THEN RETURNED TO BASE. THE APU WAS INSPECTED BY MAINTENANCE AND THERE WAS NO INDICATION OF FIRE DAMAGE. THSDR CA010322012Compressor · making metal(CAN) THE AIRCRAFT WAS CLIMBING OUT OF VANCOUVER WHEN THE APU DID AN AUTO SHUT DOWN AND THE APU FIRE HANDLE ILLUMINATED. THE FIRE HANDLE WAS PULLED BUT THE BOTTLE WAS NOT DISCHARGED DUE TO THE FIRE INDICATION GOING OUT. THE AIRCRAFT RETURNED TO VANCOUVER WHERESDR CA010129013Transmitter · failed(CAN) ON CLIMB ENGINE OIL PRESSURE WAS NOTICED TO DROP TO 41 PSI AND DID NOT RESPOND TO THROTTLE MOVEMENT. THE FLIGHT CREW ELECTED TO RETURN WHERE MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTRER ON THE NR 2 ENGINE.SDR CA001122029Fire Loop · chafed(CAN) APU FIRE WARNING IN CRUISE, APU FIRE HANDLED & WARNING CEASED, BOTTLE DISCHARGED. AIRCRAFT CARRIED OUT A NORMAL LANDING. MAINTENANCE INSPECTED APU & AREA AND FOUND NO INDICATIONS OF FIRE OR OVERHEAT. THE AIRCRAFT WAS RELEASED UNDER THE PROVISIONS OF THESDR CA001016008Stator · cracked(CAN) DURING A SCHEDULED C-2 FAN CHANGE ON WING THE 2ND STAGE STATOR WAS FOUND COMPLETELY CRACKED THROUGH A ONE BLADE LOCATION, INBOARD OF THE MID SPAN SHROUD. THE ENGINE ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA000905017Fan Blade · bird strike(CAN) ON ROTATION AT TAKEOFF CREW REPORTED THEY HEARD A BANG & FELT THE AIRCRAFT YAW TO THE RIGHT. THE CREWFLEW AROUND TO REDUCE THE FUEL LOAD AND RETURNED TO THE STATION (YEG). A BIRD STRIKE INSPECTION WAS CARRIED OUT AND SLIGHT DAMAGE WAS FOUND ON THE C1 FANSDR CA000905016Bleed Valve · failed(CAN) ON TWO OCCASIONS, THE CREW EXPERIENCED A FIRE INDICATION ON THE APU WHILE THE AIRCRAFT WAS AT CRUISING ALTITUDE. ON BOTH OCCASIONS, THE APU SHUT DOWN AND THROUGH CREW PROCEDURES, THE APU FIRE BOTTLE WAS DISCHARGED. IN BOTH OCCURRENCES, MAINTENANCE INSPECSDR CA000804016Motor · seized(CAN) DURING THE CLIMB FROM 4XS (SASKATOON) THE CREW BECAME AWARE OF A STRANGE ODOR / SMELL IN THE CABIN. THERE WAS NO SMOKE OBSERVED BUT THE CREW ELECTED TO RETURN TO THE STATION AS A PRECAUTION. ON THE GROUND THE CREW CHECKED AND FOUND THE GASPER FAN C/B POPSDR CA000511009Attach Fitting · broken(CAN) ON APPROACH WHEN LANDING GEAR LOWERED CREW REPORTED A BANGING NOISE FROM THE AREA OF THE NOSE. INSPECTION AT THE GATE FOUND THE TAXI LIGHT SUPPORT HAD BROKEN AND THE TAXI LIGHT WAS TRAILING THE GEAR BY THE WIRE HARNESS. REPAIRED.SDR CA000128017Gearbox · leaking(CAN) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.SDR AU000128017Oil Filter · leaking(AU) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.SDR P2EA99354Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM WEB CORRODED AT BS 259.5, FROM WL 208.5 TO WL 206, BETWEEN LBL 13 INCH TO RBL 13 INCH. DEFECT SIZE, LENGTH 16 INCHES, WIDTH 5 INCHES. REPAIRED FLOORBEAM WEB AT BS 259.5 BETWEEN LBL 17 INCH AND RBL 14.5 INCH FROM WL 208.5 TO WL 193. SDR P2EA99351Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM CORROSION AT BS 259.5, WL 208.5, BETWEEN LBL 20 AND RBL 15 INCHES. DEFECT SIZE, LENGTH 14 INCHES, WIDTH 4 INCHES. REPAIRED FLOORBEAM ANGLE AT BS 259 FROM LBL 23 INCHES TO RBL 21.5 INCHES WL 208. ALSO, REPLACED FLOOR BEAM UPPER ANGLESDR P2EA99350Angle · corrodedSJO - C-CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 270, WL 208.5, BETWEEN RBL 17 INCHE LBL 10 INCH. DEFECT SIZE, LENGTH 10 INCH, WIDTH 2 INCH. REPAIRED FLOOR SUPPORT ANGLE AT BS 270, WL 208.5, BETWEEN LBL 54 INCH TO RBL 25.5 INCH PER COOPESA EO COO-3-53-714-9SDR P2EA99342Skin · delaminatedSJO - C-CHECK, LEFT AC BAY DOOR DELAMINATED. REPAIRED LEFT AC BAY DOOR PER EO COO-CMP-3-53-704-99 DATED DECEMBER 4, 1999. (M)SDR P2EA99335Bulkhead · crackedSJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT BS 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 240 AND WL 230.5 PER SRM 53-10-11 FIG 1. (M)SDR P2EA99352Rib · crackedSJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99345Skin · dentedSJO - C-CHECK, E/E DOOR HAS A DENT OUT OF LIMITS, DEFECT SIZE, LENGTH 1.75 INCH, WIDTH 1.5 INCH, DEPTH .045 INCH. REPLACED DOOR SKIN PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)SDR P2EA99355Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 727 TO BS 727A BETWEEN STRINGER 14 RT AND 16 RT. DEFECT SIZE LENGTH 1.75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 TO BS 727A PLUS 9.9, BETWEEN STRINGER 16 AND 20 RT PER BOEING FAX COO-SJO-990060 DATED DECESDR P2EA99336Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 268 TO BS 277, BETWEEN STRINGER 15 RT AND 16 RT. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 263.5 TO BS 280, BETWEEN STRINGER 14 RT AND STRINGER 17 RT PER SRM 53-30-3, FIG 17. (M)SDR P2EA99311Transmitter · inoperativeFLT 588 - MCI - ABORTED TAKEOFF, NO EMERGENCY DECLARED. DURING TAKEOFF ROLL, NR 2 EPR GAUGE READS ZERO. REPLACED NR 2 EPR TRANSMITTER AND NR 2 EPR INDICATOR PER MM 77-11-21, OPS CHECK OK. (M)SDR P2EA99253Skin · crackedSJO - C-CHECK, LEFT RAM DOOR INNER SKIN CRACKED, DEFECT SIZE, LENGTH 3 INCHES AND WIDTH 1 INCH. REPAIRED RAM DOOR INTERNAL SKIN PER COOPESA EO COO-3-52-708-99 DATED DECEMBER 4, 1999. (M)SDR P2EA99220Door · missingNSP - FLT 707 - THIS IS A SUPPLEMENTAL/CLOSING ACTION FOR MRR 99220. ON WALK-AROUND INSPECTION AFTER FLIGHT MAINTENANCE, CREW DISCOVERED THE CENTER BOOST PUMP DOOR P/N 65-45487-7 MISSING. DEFERRED PER CDL 57-30-4. REQUESTED PANEL. REF: DEFERRED ITEM C2199SDR P2EA99195Pump · leakingPIT - FLT 588 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. TOTAL LOSS OF SYSTEM 'A' HYDRAULICS. FOUND NR 2 ENGINE SYSTEM 'A' HDYRAULIC PUMP SHAFT SEAL BLOWN. REPLACED NR 2 (SYSTEM 'A') ENGINE HYDRAULIC PUMP PER MM 29-11-31A. OPERATION AND LEAK CHECKS OK. SDR CA990603008Control Rod · cracked(CAN) DURING INSPECTION, THE THRUST REVERSER FOLLOW-UP CONTROL ROD FORWARD ROD END BEARING WAS FOUND ADRIFT, FURTHER INSPECTION FOUND THE ROD END WAS CRACKED AND SPLITTING APART. REPLACED.SDR P2EA99090Mechanism · wornMCI - FLT 819 - RETRACTING FLAPS FROM 5 TO 1 DEGREE OUT OF MDW, FELT HEAVY FLUTTER. GOING FROM FLAPS 1 TO 5 ON LANDING AT MCI FELT MINOR FLUTTER. LANDING AT MCI, SELECTED FLAPS 25 AND GAUGE INDICATED 15. SELECTED FLAPS 30 AND GAUGE INDICATED BETWEEN 25 AND 30SDR P2EA99001Valve · failedMSP - FLT 404 - DURAL BLEED INDICATION DURING TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS, RETURNED TO GATE. DEFERRED PER MEL 36-6, CI M219725 ASSIGNED. FEF CI M219725. DUAL BLEED INDICATION INOPERATIVE. REPLACED APU LOAD CONTROL VALVE PER MM 49-52-11A, CLEARED SDR P2EA98312Window · crackedMCI - FLT 586 - THE AIRCRAFT DEPARTED MCI AND 35 MINUTES INTO FLIGHT THE FIRST OFFICERS SLIDING WINDOW CRACKED. THE AIRCRAFT RETURNED TO MCI WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE CRACKED F/O WINDOW AND WINDOW HEAT CONTROL UNIT. (M)SDR P2EA98311Skin · crackedSJO - NR 1 THRUST REVERSER LOWER BUCKET EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH 2.75 INCH. REPAIRED THRUST REVERSER PER COOPESA EO COO-3-78-754-98 DATED DEC 17, 1998. (M)SDR P2EA98305Skin · damagedSJO - PROVISIONAL REPAIR AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSELAGE SKIN SECTION FROM BS 299 TO BS 305 BETWEEN STRINGER 12 RT AND STRINGER 14 RT PER SRM 53-30-3 FIG 31, DETAIL III. (M)SDR P2EA98296Slat · delaminatedSJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98307Skin · delaminatedSJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M)
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