Boeing 737-297
Service difficulty reports · 454
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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 = '737297' 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 = '737297' 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 KNNA147071110KACYHydraulic Line · leakingTHE "A" SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT TO KACY (ATLANTIC CITY IAP, NJ). COMPLETED CHECKLIST 6.77 OF THE AFM.SDR KNNA20090001Seal · failedNR 1 ENGINE OIL QUANTITY DROPPED TO ZERO DURING FLIGHT FOLLOWED BY DROP IN OIL PRESSURE LEADING TO ENGINE SHUT DOWN AND DECLARATION OF AN EMERGENCY. IT WAS DISCOVERED DURING TROUBLE SHOOTING THAT BOTH THE STARTER SEAL AND THE FUEL PUMP SEALS WERE LEAKING. BSDR PIDR07001Skin · crackedCRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 TO BS 757 FROM STR 14 RT TO STR 20 RT DUE PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROSDR PIDR07002Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURESDR PIDR07003Stringer · damagedSTRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2.SDR KNNA200700011Frame · misdrilledFOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212.SDR KNNA200700018Frame · crackedFOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212.SDR KNNA200700017Vertical Beam · crackedFOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.SDR KNNA200700015Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.SDR KNNA200700014Frame · crackedFOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212.SDR KNNA200700012Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,SDR KNNA200700010Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 .SDR KNNA200700013Skin · damagedE/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR .SDR KNNA200700016Stringer Splice · activeFOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75.SDR KNNA200300001Skin · crackedAIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SKSDR CA020528005Duct · ruptured(CAN) SHORTLY AFTER TAKEOFF CREW OBSERVED NR 1 ENGINE OVERHEAT - WHEN POWERLEVER RETARDED, IND. EXTINGUISHED. WHEN POWERLEVER FOR NR 1 ENGINE ADVANCED, OVERHEAT WARNING ILLUMINATED. CREW DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. CFR ON STANDBY.SDR CA020502004Fitting · missing(CAN) ENROUTE PILOT NOTICED THE OIL QUANTITY WAS AT ZERO ON THE NR 1 ENGINE - BOTH OIL PRESSURE AND OIL TEMPERATURE WERE NORMAL. SHORTLY THERE AFTER THE OIL PRESSURE STARTED TO FLUCTUATE AND THE OIL PRESSURE WARNING LIGHT ILLUMINATED.FLIGHT CREW SHUTDOWN NR 1 SDR CA020408017Wheel · cracked(CAN) FLIGHT CREW REPORTED ON TAXI THE AIRCRAFT SEEMED TO REQUIRE MORE POWER THAN NORMAL - AIRCRAFT DEPARTED WITHOUT INCIDENT.ON NEXT LANDING THE CREW NOTICED THE SAME AND REPORTED TO YLW MAINTENANCE. INSPECTION FOUND THE MAIN BRAKE ON NR 2 MAIN WHEEL ASSEMBLYSDR CA020305003Wire · chafed(CAN) DURING FLT A/C EXPERIENCED FLICKERING LT WING BODY OVERHEAT INDICATION WITH INCREASING FREQ. OVERHEAT LIGHT ILLUMINATED OFF & FLICKERED ON & OFF CONTINUOUSLY WHEN LT ENGINE BLEED VALVE & ISOLATION VALVE WERE CLOSED (WITH APU OFF). FLT CREW CONTACTED MCSDR P2EA2002M001Actuator · crackedAfter Landing Lost A System Hydraulics upon exiting taxi way at MCI.Inspected and found the #1 Ground Spoiler actuator with crack. R&R #1 Ground Spoiler actuator IAW Boeing MM 27-62-101 op's check and leak checks good.SDR CA011120004Control Unit · leaking(CAN) RETURNED TO YHM DUE TO LOSS OF 'A' SYS HYDRAULIC FLUID. SHORTLY AFTER TAKEOFF OUT OF YHM CREW NOTICED HYD MASTER CAUTION LIGHT HAD ILLUMIINATED, THE 'A' SYS HYDRAULIC FLUID HAD DEPLETED & THE HYDRAULIC LOW PRESSURE WARNING LIGHTS HAD ILLUMINATED. CREW SDR P2EA2001M0005CouplerMach Trim "fail" light illumimnates intermitently. Corrective action: Defferred Mach Trim system per MEL 22-5, CI#M005089 per MX CNTL Mic. Removed and replaces Mach Trim Coupler IAW MM 22-21-31, operational check normal. This clears MEL CI#M005089. See 005 LogSDR P2EA01193Computer · faultyFLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHECSDR P2EA01089Hydraulic Line · inoperativeFLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRAULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PARSDR CA010504024Tube · worn(CAN) CREW REPORTED NR 1 ENGINE EPR INDICATION FLUCTUATING TO .20 EPR LOWER THAN NR 1 ENGINE. N1, N2 AND FUEL FLOWS WERE STEADY. INSPECTION FOUND A CHAFED WIRE AT THE R/H ANTI-ICE VALVE HAD ARCHED AND WORN A HOLE THRU THE SIDE OF THE LINE FROM THE PT 7 PROBE. SDR P2EA01025Skin · puncturedFLT 350 - MDW - PUNCTURE THROUGH SKIN AT BS 933 WL 203 BETWEEN STRINGER 20L AND 21L. (M)SDR P2EA01028Skin · puncturedMDW - FLT 350 - PUNCTURE THROUGH SKIN AT BS 933, WL 203 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 53-30-3. (M)SDR TSAA0133015Battery Pack · dischargedREPLACED BATTERY FOR THE NR 3 AND NR 4 POSITION FOR THE EMERGENCY FLOOR PROX LIGHT. OPS CHECK OK. AIRCRAFT RETURNED SERVICE. (M)SDR 2001F00633Tire · separatedLOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAULIC LINES AND CONTROL CABLES LOCATED IN THE LEFT WHEEL WELL. ALSO, DAMAGE FROM FLYING RUBBER TO LEFT FORE FLAP, MID FLAP AND TRAILING EDGE SDR P2EA00460Skin · crackedSJO - DURING Q-CHECK, FOUND THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 WITH CRACK. L = 1.1250 INCHES. W = 0.001 INCH. REPAIRED THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 IAW BOEING SRM 52-00-3 FIG 3. (X)SDR P2EA00451Fitting · crackedSJO - DURING Q-CHECK, FOUND LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO WITH CRACK L = 2.00 INCHES. W = 0.002 INCH. REPLACED THE LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)SDR P2EA00424Clip · crackedDURING Q CHECK, FOUND THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L WITH CRACK. REPLACE THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L.SDR P2EA00414Floor Support · crackedDURING Q CHECK, FOUND THE PASSENGER CABIN AT BS 727 RBL 65 WITH CRACKED ANGLE ON FLOOR SUPPORT. L/0.050 W/0.005 REPAIRED THE PASSENGER CABIN FLOOR SUPPORT ANGLE AT BS 727 RBL 65.SDR P2EA00407Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE BS 178 BULKHEAD AT WL 196 FROM LBL 25 TO RBL 25 WITH CRACK. L = 1.00 INCH. W = 0.001 INCH. REPLACED THE BS 178 BULKHEAD INTERCOSTAL AT WL 196 FROM LBL 25 TO RBL 25 IAW BOEING SB 737-53A1173 REV 3 DATED MAY 6, 1999, SECTION IISDR P2EA00396Channel · corrodedSJO - DURING Q-CHECK, THE CABIN FLOOR CHANNEL AT BS 296.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS, LENGTH 2.5 INCH, WIDTH 2 INCHES, DEPTH .025 INCH. REPLACED THE CABIN FLOOR CHANNEL AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 IASDR P2EA00413Floor Support · corrodedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 0.50 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5SDR P2EA00412Floor Support · corrodedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO BS 312 LBL 11 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 1.00 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO SDR P2EA00449Channel · crackedDURING Q CHECK, FOUND THE RT HAND WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK L/0.50 W/0.005 REPLACED RT HAND WING TE CAVITY LOWER CHORD CHANNEL.SDR P2EA00389Channel · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK. (M)SDR P2EA00457Web · crackedDURING Q CHECK, FOUND THE FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END, WITH CRACK. L/1.00 W/0.001. REPAIRED FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END.SDR P2EA00387Crossbeam · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR NR 5 CROSSBEAM WEB AFT END WITH CRACK. (M)SDR P2EA00455Flap Track · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NR'S 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS .313 LENGTH, .001 INCH WIDE, AND .250 INCH LENGTH, .001 INCH WIDE. REPLACED THE RIGHT WING OUTBOARD FLAP TRSDR P2EA00459Angle · corrodedDURING Q CHECK, FOUND APU TORQUE BOX RT SIDE ANGLE FROM BS 1118 TO 1138 WITH CORROSION, OUT OF LIMITS L/12.00 W/1.250 D/0.50. REPLACED THE APU TORQUE BOX RT SIDE ANGLE.SDR P2EA00435Frame · crackedDURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23,24R.SDR P2EA00440Frame · crackedDURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R.SDR P2EA00384Flap Track · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NRS 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS. (M)SDR P2EA00386Angle · corrodedSJO - DURING Q-CHECK, FOUND THE APU TORQUE BOX RIGHT ANGLE FROM BS 1118 TO 1138 WITH CORROSION OUT OF LIMITS. (M)SDR P2EA00379Web · crackedSJO - DURING Q-CHECK, FOUND THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 WITH CRACK. L = 0.500 INCH. W = 0.005 INCH. REPAIRED THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 IAW BOEING SRM 51-40-2 FIG 1. (X)SDR P2EA00380Channel · crackedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)SDR P2EA00393Slat Track · crackedSJO - DURING Q-CHECK, FOUND THE LT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK LENGTH .50 INCH, WIDTH .50 INCH. REWORKED THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER AND WAS FOUND TO BE WITHIN LIMITS IAW BOEING SRM 57-20-1 F
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