Boeing 737-724
Service difficulty reports · 3,423
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 = '737724' 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 = '737724' 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 CALA2014031800342Floorbeam · corrodedSEVERAL CORROSION WERE FOUND ON UPPER SURFACE OF CABIN FLOORBEAM UPPER TEE BS 328 RBL 6 - 50. BLENDED OUT DAMAGE IAW SRM 51-10-02 GEN REV 51. INSTALLED REPAIR PARTS IAW SRM 53-10-51 REPAIR 8 REV 51.SDR CALA2014031800341Sill · corrodedRT NR 2 ENTRY DOOR CUT OUT LOWER MAIN SILL INNER CHORD SEVERAL CORROSION S=4"*2" STATION 890 - STATION 1010, RBL 40 - RBL 60. REMOVED THE CORROSION PART IAW SRM 51-40-02 P1 REV 51. LOCATED & DRILLED HOLES IAW SRM51-40-02 P1 REV 51 FOUND SHORT EDGE MARGE SEE SDR CALA2014031800340Frame · crackedCRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S8L - S9L. STA787 L=0.15" FABRICATED ANGLES PER EA5310-04716 REVF STEP9 FIG3. REMOVED CRACK PER EA5310-04716 REVF STEP9 FIG3. INSTALLED REPAIR PARTS.SDR CALA2014031700336Floorbeam · corrodedFLOORBEAM STATION 344 LBL 11 TO RBL 6 CORROSION. FLOORBEAM REPAIRED IAW ECRA 5320-02211.SDR CALA2014031700335Frame · crackedCRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S-8R AND S-9R.STA827 L= 0.5" FABRICATED ANGLES PER EA 5310-04716 REV F STEP 9 FIG 3 STEP 9 FIG 3 AND NR-51-008. INSTALLED REPAIR PARTS. ACP RII INSPECTION PER ALL CRITICAL STEPS IN GMM09-25-0SDR CALA2014031700331Frame · crackedCRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN S-8R AND S-9R STA 500L L=0.15" FABRICATED ANGLES PER EA 5310-04716 REVF STEP9 FIG3. REMOVED THE DAMAGE PER EA5310-04716 REVF STEP9 FIG3. INSTALLED REPAIR PARTS. ACP RII INSPECTION PER ALL CSDR CALA2014031700334Frame · crackedCRACK WAS FOUNDED ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN STRINGER 8L - STRINGER 9L, STATION 500A, L=0.25INCHES. FABRICATED ANGLES IAW EA 5310-04716 STEP 9 FIG 3 LOCATED & DRILLED THE HOLE IN THE REPAIR PART. INSTALLED REPAIR PARTS, APPLIED CIC ASDR CALA2014031700333Frame · crackedCRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN STRINGER 8R - STRINGER 9R, STATION 480 L=0.1 INCH. FABRICATED ANGLES IAW EA 5310-04716 REV F STEP 9 FIG 3. LOCATED & DRILLED THE HOLE IN THE REPAIR PARTS. COLD WORKING 7075-TO CLAD AL SHEETSDR CALA2014031700332Frame · crackedCRACK WAS FOUND ON THE FRAME HOLES WHICH ATTACH THE BRACKET BETWEEN STRINGER 8R - STRINGER 9R, STATION 747 L=0.1 INCH. FABRICATED ANGLES IAW EA 5310-04716 REV F STEP 9 FIG 3. MATERIAL 7075-TO CLAD AL SHEET. REMOVED CRACK IAW EA 5310-04716 REV F STEP 9 FIG 3SDR CALA2014031000301Frame · crackedAD 2009-01-02 BETWEEN STRINGER 8L & 9L AT THE AIR CONDITIONING OUTLET EXTRUSION, SUPPORT ATTACHMENT TO THE FUSELAGE FRAME FOUND CRACK AT STATION 500C LT ON MFEC IAW EA 5310-04716 REV F OP 1. FRAME 500C LT HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.SDR CALA2014030300272Connector · looseENG 1 VIBRATION WENT AS HIGH AS 5.6 & DEBRIS NOTED ON FAN BLADES. ENG 1 VIB INDICATOR PLACARD MEL. PILOT REPORTED AFTER LANDED ALL OTHER PARAMETER NORMAL INSP INLET & EXHAUST NO DAMAGE NOTED TO FAN BOOSTER OR TURBINE DEBRIS FOUND TO BE FAN LUBE WHICH WAS CLSDR CALA2014022800243Frame · crackedBETWEEN STRINGER 8R & 9R AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 787R FRAME 787R BETWEEN STRINGER 8R & 9R HAS BEEN REPAIRED IAW EA 6310- 04716 REV F OP 1.SDR CALA2014022800242Frame · crackedBETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 480R. REPAIRED CRACK IN FRAME AT STATION 480R BETWEEN STRINGER 8 & STRINGER 9 IAW EA 5310-04716 REV F OP 1.SDR CALA2014022800241Frame · crackedBETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 500C RT. REPAIRED CRACK IN FRAME AT STATION 500C BETWEEN STRINGER 8R & STRINGER 9R IAW EA 5310-04716 REV F OP 1.SDR CALA2014022800240Frame · damagedBETWEEN STRINGER 8L & 9L AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME. FRAME AT STATION 747L BETWEEN STRINGER 8L & 9L HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.SDR CALA2014022700239Frame · crackedBETWEEN STRINGER 8L & 9L AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 727D LT CRACK IS ON THE FRAME. FRAME SUPPORT ATTACHMENT BRACKET FRAME 727D LT HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.SDR CALA2014022700238Frame · crackedBETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME, FOUND CRACK AT STATION 727D RT. REPAIRED FRAME AT STATION 727D RT BETWEEN STRINGER 8 & STRINGER 9 IAW EA 5310-04716 REV F.SDR CALA2014022600236Frame · crackedBETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET, EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME CRACKED AT STATION 500A LT. REPAIRED FRAME IAW EA5310-04716 REV F.SDR CALA2014022600235Frame · crackedBETWEEN STRINGER 8 & STRINGER 9 AT THE AIR CONDITIONING OUTLET, EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME FOUND CRACK AT STATION 440L. REPAIRED FRAME IAW EA 5310-04716 REV F.SDR CALA2014022500234Frame · crackedBETWEEN STRINGER 8R & 9R AT THE AIR CONDITIONING OUTLET, EXTRUSION SUPPORT ATTACHMENT TO FUSELAGE FRAME FOUND CRACK AT STATION 500A RT. FRAME 500A RT HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.SDR CALA2014022500233Frame · crackedBETWEEN STRINGER 8L & 9L AT THE AIR CONDITIONING OUTLET, EXTRUSION SUPPORT ATTACHMENT TO THE FUSELAGE FRAME FOUND CRACK AT STATION 380L. FRAME 380L HAS BEEN REPAIRED IAW EA 5310-04716 REV F OP 1.SDR CALA2014022400226Engine · vibrationNR 1 ENG ROLL BACK INFLIGHT AT FL 400 DROPPED TO 67% N!, THEN RECOVERED, AS WE CONTINUED VIBRATION GOT GRADUALLY WORSE & VIOLENT ON FINAL, LANDED WITH NR 2 ENG POWER & NR 1 ENG AT IDLE VIBRATING. R & R NR 1 ENG IAW WORK CARD 29-7100-1-0900 & 29-7100-1-4900. SDR CALA2014022400225Control Panel · failedPOWER FAILS & WXR FAIL MESSAGE. IAW QRH RECYCLED P6-1-013. FL 360 MACH 76, TIME 0801Z RETURNED IAW MX CNTRL. TROUBLE SHOT IAW WDM 34-41-11 SHEET 1. CHECKED M101 PINS 7 & 11. GND WIRES CHECKED OK. CHECKED POWER TO PINS 2 & 9 ALL CHECKED NORMAL. R & R WXR SDR CALA2014021300194Skin · dentedC 1 DOOR EXTERIOR SKIN HAS MULTIPLE DENTS. NR 1 DENT 20 INCHES FROM UPPER EDGE & 23 INCHES FROM FWD EDGE. NR 2 DENT 23 INCHES FROM UPPER EDGE & 21 INCHES FROM FWD EDGE. CUTOUT DAMAGE & INSTALLED DOUBLER IAW SRM 52-00-01, REPAIR 3.SDR CALA2014021300193Bulkhead · gougedFWD PRESS BULKHEAD HAS A GOUGE APPROXIMATELY 1 INCH IN LENGTH. RUNNING VERTICALLY, LOCATED RT BELOW THE 11`CLOCK POSITION RADOME MOUNTING BRACKET. REMOVED DAMAGED AREA & PERFORMED HFE, NO CRACKS NOTED. ALODINED PRIMED & PAINTED IAW ECRA 5310-05449 REV A.SDR CALA2014021000174Bulkhead · canningAFT PRESS BULKHEAD FOUND OIL CANNING AT RT SIDE BETWEEN STRINGERS 14RT & 15RT, 6 INCHES X 4 AT WL 240 APPROXIMATELY. COMPLIED WITH INTERIM REPAIR TO BS 1016 APB WEB AT WL 241, RBL 52 IAW ECRA 5380-01101.SDR CALA2014021000172Floorbeam · corrodedAFT WET AREA FLOOR BEAM HAS LIGHT CORROSION ON UPPER SURFACE AT STATION 986, RBL 3. REMOVED DAMAGED UPPER CHORD OF STATION 986.5 FLOOR BEAM IN ITS ENTIRETY. INSTALLED PERMANENT REPAIR OF ENTIRE UPPER CHORD IAW SRM 53-7 0-51 REPAIR 4 ALTERNATIVE 1 & ECRA 5310-SDR CALA2014020600155Stiffener · crackedCRACKED STIFFENER LOCATED FWD SIDE ON LT VAPOR BARRIER IN WW STATION 663, LBL 6 TO 31.83. R & R STIFFENER PN 111A1301U5 ON LT VAPOR BARRIER WW STATION 663 LBL 6.13 TO LBL 31.83.SDR CALA2014020300134Frame · crackedCABIN FRAME 480L HAS CRACK AT INBD FASTENER HOLE FOR AIRCRAFT SUPPORT BRACKET BETWEEN STRINGER 8 & 9 IAW EA 5310-04716. REPAIRED CRACKED FRAME AT STATION 480 BETWEEN STRINGER 8L & 9L IAW EA 5310-04716 REV F FIG 3 OP 1.SDR CALA2014020300133Frame · crackedCABIN FRAME 480R CRACKED AT INBD FASTENER HOLE FOR AIRCRAFT SUPPORT BRACKET BETWEEN STRINGER 8 & 9 IAW EA 5310-04716. REPAIRED CABIN FRAME480R BETWEEN STRINGER 8 & 9 IAW EA5310-047 16 REV F OP 1 FIG 3.SDR CALA2014020300132Frame · crackedCABIN FRAME 500A LT CRACKED AT INBD FASTENER HOLE FOR AIRCRAFT SUPPORT BRACKET BETWEEN STRINGER 8 & 9 IAW EA 5310-04716. REPAIRED CABIN FRAME 500A LT BETWEEN 8 & 9 IAW EA 5310-04716 REV F OP 1.SDR CALA2014020300131Frame · crackedCABIN FRAME 747R SHOWS CRACK INDICATION AT INBD FASTENER HOLE FOR AIRCRAFT SUPPORT BRACKET BETWEEN STRINGER 8 & 9 IAW EA 5310-04716. REPAIRED CRACKED FRAME AT STATION 747 BETWEEN STRINGER 8R & 9R IAW EA 5310-04716 REV F OP 1 FIG 3.SDR CALA2014020300130Frame · crackedCABIN FRAME 500A RT SHOWS CRACK INDICATION AT INBD FASTENER HOLE FOR A/C SUPPORT BRACKET BETWEEN STRINGER 8 & 9 IAW EA 5310-04 716. MARKED REPAIRED CABIN FRAME AT STATION 500A RT BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 OP 1 REV F FIG. 3.SDR CALA2014012000087Transmitter · unserviceableAFTER TAKEOFF WITH FLAPS UP FMC VNAV SHOWED FLAPS 1 SPEED 206 FLAPS. VERIFIED FLAPS UP. TROUBLE SHOOT FLAP IAW AMM 22-11-00. PERFORMED FLAP RIGGING TEST FOUND RT FLAP POSITION TRANSMITTER TO BE OUT OF DEGREES LIMIT. R & R RT FLAP POSITION TRANSMITTER IAW ASDR CALA2013120200884Frame · crackedFRAME 500A LT SHOWS CRACK INDICATION BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-04716. REPAIRED FRAME STATION 500A LT IAW EA 5310-04716 REV F OP1.SDR CALA2013112700877Frame · crackedFRAME 787L CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED REPAIR AT STATION 787L BETWEEN STRINGER 8 & 9 IAW EA5310-04716 REV F FIG 3.SDR CALA2013112700876Frame · crackedFRAME 727D LT BETWEEN STRINGER 8 & 9 CRACKED AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION BRACKET IAW EA 5310-04716. INSTALLED REPAIR AT FRAME STATION 727D LT IAW EA A5310-04716 OP 01 REV F FIG 3.SDR CALA2013112700875Frame · crackedFRAME 480R CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. REPAIRED CABIN FRAME STATION 480R IAW EA 5310-04716 OP1 REV F.SDR CALA2013112700874Frame · crackedFRAME 500A RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-0 4716. REPAIRED CABIN FRAME STATION 500A RT IAW EA 5310-04716 OP1 REV F.SDR CALA2013112700873Frame · crackedFRAME 400R CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. REPAIRED FRAME STATION 400R IAW EA 5310-04716 OP1 REV F.SDR CALA2013112700872Frame · crackedFRAME 727B RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION REF EA 5310- 04716. REPAIRED CABIN FRAME STATION 727B RT IAW EA 5310-04716 OP1 REV F.SDR CALA2013112700871Frame · crackedFRAME 747L CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. PERFORMED FRAME REPAIR AT STATION 747L BETWEEN STRINGER 8 & 9 IAW EA53 10-04716 OP 01 REV F FIG 3.SDR CALA2013112700870Frame · crackedFRAME 727D RT CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET IAW EA 5310-04716. REPAIRED CABIN FRAME STATION 727D RT IAW EA 5310-04716 OP 1 REV F.SDR CALA2013112700869Frame · crackedFRAME 500C RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA5310-047 16. INSTALLED FRAME REPAIR AT FRAME 500C BETWEEN STRINGER 8 & 9 FOR AC OUTLET EXTRUSION IAW EA5310-04716.SDR CALA2013112700868Frame · crackedFRAME 480L BETWEEN STRINGER 8 & 9 CRACKED AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED REPAIR AT STATION 480L BETWEEN STRINGER 8 & 9 IAW EA5310-04716 REV F FIG 3.SDR CALA2013112700880Frame · crackedFRAME 727A RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-04716. COMPLETED REPAIR OF FRAME 727A RT CRACK BETWEEN STRINGER 8 AND 9 AT INBD HOLE SUPPORT BRACKET EXTRUSION IAW EA 5310-04716 REV FSDR CALA2013112700879Frame · crackedFRAME 440L HAS CRACK BETWEEN STRINGER 8 & 9 INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED DOUBLER REPAIR AT FRAME STATION 440L BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV F FIG 3.SDR CALA2013112700878Frame · crackedFRAME 440R SHOWS CRACK INDICATION BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION, IAW EA 5310-04716. REPAIRED CABIN FRAME STATION 440R IAW EA 5310-04716 REV F OP 1.SDR CALA2013112600866Sign · crackedEMERGENCY EXIT SIGN AFT OF R2 DOOR CRACKED. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01-960-802.SDR CALA2013112100859Battery Pack · dischargedON WALK AROUND INSPECTION FOUND LT SIDE EMERGENCY LIGHTING INOPERATIVE IN CABIN. REPLACED POWER SUPPLY IAW AMM 33-51-06-960-806. REPLACED BATTERY BACK IAW AMM 33-51-06-200-801, OPERATIONS CHECKED GOOD.
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