Boeing 737-214
Service difficulty reports · 209
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 = '737214' 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 = '737214' 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 CALA9801831Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WAS LOST AFTER TAKEOFF. A MANUAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE GEAR DID NOT EXTEND ON FIRST PULL OF HANDLE. THE HANDLE WAS PULLED AGAIN AND THE GEAR EXTENDED BUT NOSE EXTENSION CABLE WOULD NOT RETRACT FUSDR BJNA980901Light · inoperativeEMERGENCY EXIT LIGHT ABOVE L-2 DOOR INOP. REPLACED EMERGENCY LIGHT ASSY IAW BMM 33-51-101, GROUND CHECKS NORMAL. (M)SDR VJ9800381R1Brake · fireNR 3 BRAKE CAUGHT ON FIRE AFTER HIGH SPEED TAXI TEST WAS PERFORMED; TEST COMMENCED AT 100 KNOTS AND AT 80 KNTS LOST PRESSURE AND WENT TO STOP ON RIGHT BRAKES. ATC ALERTED FLIGHT CREW FIRE WAS EMINATING FROM THE RIGHT WHEEL WELL AREA. BROUGHT THE AIRCRAFT TO SDR VJ9800316Power Supply · inoperativeRT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.SDR VJ0900298Battery Charger · inoperativeRT OVERWING EMERGENCY LIGHTS INOP. REPLACED THE LIGHT BATTERY CHARGER ASSY.SDR VJ9800296Battery Pack · dischargedRT FUSELAGE EXTERNAL OVERWING EMERGENCY LIGHT FOUND INOPERATIVE DURING LAYOVER CHECK. REPLACED BATTERY PACK.SDR VJ9800227Battery Pack · dischargedEMERGENCY LIGHTING BATTERY PACK INOP. REPLACED BATTERY PACK.SDR BJNA980701Sensor · malfunctionedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RELEASED PER MEL 26-12, DMI 701, ITEM TRANSFERRED TO DMI LOG AND PLACARDED. REF: DMI 701, REMOVED AND REPLACED OVERHEAT LOOP IN APU COMPARTMENT IAW 26-18. OPS CHECKS NORMAL. (LOG PAGE 10721). (X)SDR BJNA980604Insulator · mislocatedON GROUND LEFT WING BODY OVERHEAT ILLUMINATED. IN THE APU COMPARTMENT, THE OVERHEAT LOOP ELEMENT IS POSITIONED A FEW INCHES ABOVE THE BLEED AIR SUPPLY DUCT. THIS ELEMENT IS HELD IN POSITION BY NUMEROUS CLAMPS WITH INSULATORS DURING TROUBLESHOOTING, AN INSULASDR BJNA980603Detector · out of positionNR 1 WING BODY OVERHEAT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT BFF WITH BLEEDS OFF, APU ON TAKEOFF, REMAINED OFF AFTER BLEEDS RECONFIGURED. DISCOVERED OVERHEAT DETECTOR AGAINST APU BLEED SUPPLY DUCT, RELOCATED AND RAN APU AT MAX TEMP FOR 40 MIN, NO DISCRSDR VJ9800198Gearbox · leakingENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND OIL QTY WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. FOUND THAT THE NR 2 ENGINE HAD A BANJO FITTING BROKEN FROM THE GEARBOX LOSING OIL. REMOVED THE GEARBOX. THE HELICOIL WAS PULLED OUT OF THE GSDR VJ9800197Light · inoperativeFOUND EMERGENCY EXIT LIGHT INOP AT L-2 DOOR DURING THE LAYOVER CHECK. REPLACED THE LIGHT ASSY.SDR BJNA980506Overheat Light · illuminatedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING THE DESCENT INTO KEKO. AIRCRAFT RELEASED PER MEL 26-12, DMI 10508, ITEM PLACARDED AND TRANSFERRED TO DMI LOG. (M)SDR BJNA980505Fire Detector · malfunctionedLEFT WING BODY OVERHEAT ILLUMINATES, QRH PROCEDURE, LIGHT WENT OUT THEN CONTINUED FLICKERING DURING DESCENT. CHECKED ALL LOOPS WITH OHM METER AND MAGER, FOUND NO PROBLEM CHANGED FIRE DETECT ASSY UNIT TEST FLEW AIRCRAFT COULD NOT DUPLICATE PROBLEM. (M)SDR BJNA980504Clamp · looseLEFT WING BODY OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURE AND AFTER A FEW MOMENTS THE OVERHEAT LIGHT WENT OUT. RETORQUED CLAMP ON INBOARD END OF AIR CLEANER AT FORWARD END OF LEFT A/C BAY PER BMM 36-19-11, GRUOND CHECKS NORMAL. (M)SDR BJNA980503Connector · dirtyLEFT WING BODY OVERHEAT ILLUMINATES INTERMITTENTLY. CLEANED CONNECTORS ON FORWARD AND AFT KEEL BEAM SENSOR, OPS CHECK NORMAL. OK FOR SERVICE. (M)SDR BJNA980502Connector · dirtyLEFT WING BODY OVERHEAT LIGHT CAME ON DURING DESCENT. CLEANED CONNECTORS OF SENSING ELEMENT ON LEFT ENGINE STRUT CAVITY TESTED WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM PER BMM 26-18-0, PAGE 501, TO 502, TEST OK. (M)SDR BJNA980501Overheat Light · illuminatedLEFT WING BODY OVERHEAT LIGHT CAME ON EN ROUTE. REMOVED AND REPLACED COMP OVERHEAT UNIT PER BMM 26-17-0, OPS TEST PERFORMED PER BMM 26-18-0, TEST OK. (M)SDR BJNA9803007Connector · failedENGINE OVERHEAT LIGHT FLICKERED ON AND OFF. REMOVED AND REPLACED CONNECTOR PER BSWM 20-67-14, OPS CHECK NORMAL PER BMM 26-11-0. (M)SDR BJNA9803006Fire Loop · chafedLEFT ENGINE OVERHEAT LIGHT COMES ON INTERMITTENTLY. DISCOVERED CHAFED WIRES ON FIRE LOOP CONNECTORS, LT ENGINE, AFT. REMOVED AND REPLACED CONNECTORS PER BSWPM 20-62-16, OPS CHECKS NORMAL. (X)SDR BJNA9800303Connectors · dirtyNR 1 ENGINE OVERHEAT LIGHT ON. CLEANED OVERHEAT LOOP CONNECTORS, REPLACED COPPER GASKETS. OPS CHECKED OK, IAW BMM 26-10-00. (M)SDR BJNA9803005Control Module · defectiveNR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN-FLIGHT INTERMITTENTLY. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL MODULE, RAN ENGINE, NO LEAKS FOUND. CHECKED WIRING, ALL OK. REF MM 26-21-41, AND 26-21-0. (X)SDR BJNA9803004Fire Detector · defectiveLEFT ENGINE OVERHEAT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION ACCESSORY UNIT PER bMM20-10-111, GROUND TEST NORMAL PER BMM 26-11-0. (EKO) (X).SDR BJNA9800302Connector · dirtySLT - NR 1 ENGINE OVERHEAT LIGHT IS ON INTERMITTENT IN FLIGHT, ON 100 PERCENT ON GROUND. AIRCRAFT RELEASED PER MEL 26-2, DMI 0402, PER PLACARD INSTALLED. CLEANED OIL FROM CONNECTORS ON NR 1 ENGINE PER BMM 26-11-0. TESTS NORMAL PER BMM 26-11-0. (M)SDR BJNA980202Battery Pack · dischargedL2 DOOR EMERGENCY SLIDE BATTERY WEAK. REMOVE AND REPLACE BATTERY PACK PER BMM 33-51-71, GROUND CHECKS NORMAL. (M)SDR VJ9800009Switch · failedEMERGENCY EXIT LIGHT WILL NOT ARM, ON FLIGHT CREW PRE FLIGHT. REMOVED AND REPLACED MICRO SWITCH IAW MM 33-51-121; OPS CHECKED GOOD.SDR BJNA980201Snubber · misinstalledAIR LEAK IN L1 DOOR, GROUND PRESSURIZED AIRCRAFT. FOUND LOWER DOOR HINGE SNUBBER INSTALLED BACKWARDS. REPOSITIONED SNUBBER IAW BOEING MM CHAPTER 52-11-0 PAGE 406. REPLACED FLAPPER SEAL IAW STANDARD PRACTICES. OPS NORMAL. (M)SDR BJNA980102Fire Loop · chafedNR 2 ENGINE FIRE WARNING SYSTEM INTERMITTENT LIGHT AND BELL, 3 SECONDS IN LENGTH IN CRUISE AND APPROACH EKO. REPAIRED CHAFED WIRE FOR UPPER LOOP AT STATIONARY COWL FORWARD SUPPORT PER BSWP MANUAL, 20-00-11. GROUND CHECKS NORMAL. RAN ENGINE, NO PNEUMATICS LESDR 98ZZZM160Lamp · missingDURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (M)SDR 98ZZZM159Lens · missingDURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (M)SDR BJNA980101Connector · looseFIRE WARNING ENGINE NR 2 LIGHT AND BELL ALARM. DISCOVERED LOOSE AND WATER SOAKED CONNECTOR ON ENGINE NR 2, FIRE DETECTION LOOP. CLEANED CONNECTOR AND TIGHTENED PER BMM 26-11-0. OPS CHECK NORMAL. (M)SDR ZZDA5324297Angle · crackedDURING C-CHECK AT AERO CORP, FOUND CRACK AT AFT CARGO COMPARTMENT OF APPROXIMATELY 1 INCH IN STRINGER TO FRAME REINFORCEMENT ANGLE AT STA 907, RIGHT, STR 26 UNDER TRANSITION PANEL. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-30-2. BLENDED OUT CRACK SDR BJNA971001Fire Detector · failedAPU FIRE DETECTION SYSTEM INOPERABLE. REMOVED AND REPLACED APU FIRE DETECTION ELEMENT PER BMM 26-15-11. OPS CHECK GOOD. (X)SDR ZZDA3325297Lamp · inoperativeDURING LAYOVER CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT INOPERABLE, ROW 15. RELAMPED ROW 15 FLOOR TRACK EMERGENCY LAMP IAW MM 33-51-00. OPS CHECK GOOD. (X)SDR ZZDA3325097Power Supply · fireRIGHT OVERWING EXTERIOR LIGHT INOPERABLE. INSPECTED POWER SUPPLY ASSY. REMOVED C/P, CHECKED CIRCUIT BOARD. INSTALLED IN RT POWER SUPPLY AND OPS CHECKED GOOD. LT BATTERY PACK INSTALLED IN RT POWER SUPPLY LIGHT STAYS ON, EVEN IN ARM. UPON REINSTALLING, RT BSDR ZZDA5721197Skin · dentedDURING C-CHECK AT AERO CORP, FOUND RIGHT WING INBOARD FLAP L/E HAS 1.0 INCH BY 2.0 INCH DENT AT WBL 80.0 OUT OF LIMITS. CUT OUT DENT AREA IAW B 737 57-50-4 FIG 3. FABRICATED FILLERS AND DOUBLER IAW B 737 SRM 57-50-4 FIG 3. ALODINED AND PRIMED IAW B 737 SRM SDR ZZDA5322197Skin · corrodedDURING C-CHECK AT AERO CORP, AT AFT CARGO PIT FROM STA 727B TO STA 767, FOUND CORROSION AROUND NUTPLATES (30 EACH) AT UNDERSIDE OF THE LT TRANSITION PANEL TO BE BEYOND LIMITS. REMOVED THE TRANSITION PANEL FROM BS 727 - BS 767, REMOVED CORROSION STA 745 AND STSDR BJNA970911Handle · crackedRIGHT EMERGENCY EXIT DOOR UPPER HANDLE CRACKED. REMOVED AND REPLACED RIGHT EMERGENCY EXIT DOOR UPPR HANDLE PER BMM 52-21-0. (M)SDR BJNA970910Handle · crackedLEFT EMERGENCY EXIT DOOR UPPER HANDLE CRACKED. REMOVED AND REPLACED LEFT EMERGENCY EXIT DOOR UPPER HANDLE PER BMM 52-21-0. (M)SDR BJNA970912Battery · dischargedL2 DOOR EMERGECY LIGHT VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PER BMM 33-51-41. GROUND CHECKS NORMAL. (M)SDR ZZDA5326897Skin · misdrilledDURING C-CHECK AT AERO CORP, FOUND BELLY SKIN HAS DOUBLER DRILLED HOLES AT STA 328 BETWEEN STR 25 - STR 26. FABRICATED DOUBLER FROM 2024 T3 .050 INCH 12 INCHES BY 16 INCHES IAW B 737 SRM 53-30-3. INSTALLED IAW B 737 SRM 53-30-3, FIG 1. (X)SDR ZZDA5327097Support · corrodedDURING C-CHECK AT AERO CORP, FOUND CABIN BS 344 - BS 380 RBL 15 FLOOR SUPPORT UPPER SURFACE CORRODED BS 350 - BS 354. FABRICATED SUPPORT FROM 7075 T6 .060 INCH 15 INCHES BY 2 INCHES AND FILLER FROM 7075 T6 .100 INCH 12 INCHES BY 2 INCHES IAW B 737 SRM 51-40-4SDR ZZDA5321697Support · corrodedDURING C-CHECK AT AERO CORP, FOUND FORWARD CABIN CORRODED ON FLOOR SUPPORTS WL 208.1 FROM STA 251.6 TO STA 328 BL AND BL 12R. REMOVED THE CORRODED FLOOR SUPPORTS, CORRODED BEYOND LIMITS IAW B 737 SRM 53-10-1 FIG 1. REMOVED FWD LAVATORY VANITY, COCKPIT DOOR, SDR ZZDA5327697Seat Track · broken offDURING C-CHECK AT AERO CORP, LT INBD SEAT TRACK LUGS AT STATIONS 480-520, AND STATIONS 540-597 ARE BROKEN OFF. FABRICATED SEAT TRACKS FROM BAC 1500-841 44.50 INCHES AND BAC 1520 792 77.5 INCHES BY 3.5 INCHES IAW B 737 SRM 53-10-5, FIG 1. INSTALLED IAW B 737 SSDR ZZDA5322097Skin · crackedDURING C-CHECK AT AERO CORP, FOUND 5 EACH FASTENERS WITH CRACK INDICATIONS W/HFEC RT SECTION 41 SKIN. REMOVED COCKPIT SIDE PANELS AND INSULATION FOR ACCESS. REMOVED CRACKED AREAS AND HFEC INSPECTED FOR VERIFICATION OF REMOVAL IAW SRM 51-00-00 PART 6 FIG 23. SDR ZZDA5323197Seat Track · corrodedDURING C-CHECK AT AERO CORP, FOUND OUTBOARD SEAT TRACK HAS CORROSION OUT OF LIMITS FROM BS 360 TO BS 480. REMOVED SEAT TRACK AND REPLACED WITH NEW TRACK (1A-24092-1) BAC 1520-792 7178T6 EXTRUSION STA 360 - STA 480, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRISDR ZZDA5321997Chord · corrodedDURING C-CHECK AT AERO CORP, FOUND T-CHORD FROM BS 324 - BS 360 STR 28R CORRODED BEYOND LIMITS. FABRICATED ANGLE REPAIR FROM 301 1/2 CRES STAINLESS STEEL .050 INCH IAW RES 04403 AND NEW BRACKET FROM 7075 T6 .003 INCH. DIMENSIONS: ANGLES 11.6250 INCHES BY 1 SDR ZZDA5321897Chord · corrodedDURING C-CHECK AT AERO CORP, FOUND T-CHORD HAS HEAVY CORROSION FROM STA 360 - STA 294.5, STR 28L. FOUND TO BE BEYOND LIMITS. REMOVED DAMAGED T-CHORD FROM STA 294.5 - STA 360 IAW BAC 737 SRM 51-30-2. REPLACED DAMAGED T-CHORD WITH A NEW SECTION OF T-CHORD IAWSDR ZZDA5326797Skin · corrodedDURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOVED AND REPLACED SKINS AT STA 259.5 - STA 360, BL ZERO, STR 24L AND 24R IAW B 737 SRM 51-30-2 AND BASDR ZZDA5323497Support · corrodedDURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY LONGITUDINAL FLOOR SUPPORT AT BS LBL 14 HAS CORROSION. BLENDED CORROSION MATERIAL LOSS 50 PERCENT BEYOND LIMITS IAW B 737 SRM 53-10-1 AND FORMED NEW SUPPORT, DRILLED, DEBURRED, TREATED, PRIMED, AND PAINTED IAW B
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