Boeing 737-130
Service difficulty reports · 287
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 = '737130' 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 = '737130' 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 CAL960346Doubler · crackedGSO - INSPECTION FOUND .25 INCH CRACKS IN SEVERAL AREAS OF DOUBLER FOR EXTERNAL POWER RECEPTACLE. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-2 AND SRM 51-30-2.SDR CAL960345Floor Beam · corrodedGSO - INSPECTION FOUND FLOOR BEAM UPPER CAP CORRODED AT STA 328, RBL 45 TO RBL 65. THE FLOOR BEAM UPPER CAP WAS REMOVED IAW SRM 53-10-9. A NEW CAP AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND SRM 51-30-0. (X)SDR CAL960340Intercostal · corrodedGSO - INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO COMPARTMENT AT FS 870 - FS 887, STR 20R TO STR 21R. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2, A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2. A DOUBLER WAS FABRICATED AND INSTALLED ISDR CAL960480Skin · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT NR 2 SLAT AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, SR 51-10-2, AND SRM 51-30-2. (X)SDR CAL960490Frame · crackedGSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME. THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED WEB WAS CUT OUT. REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND SRM 51-30-2. (X)SDR CAL960341Panel · corrodedGSO - INSPECTION FOUND NOSE WHEELWELL UPPER FORWARD PANEL CORRODED. THE PANEL WAS REPAIRED IAW E.A. 5310-02452. (X)SDR CAL960365Frame · crackedGSO - INSPECTION FOUND THE LT LOWER FRAME IN FORWARD PIT STA 480 CRACKED TWO PLACES AT NUTPLATE LOCATIONS FOR CARGO LINER. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE FRAME WAS REPAIRED IAW E.A. 5310-01211. (X)SDR CAL960364Floor Beam · corrodedGSO - INSPECTION FOUND FLOOR BEAM AND WEB CORRODED IN COCKPIT UNDER CAPTAIN'S SEAT. THE AREA WAS REPAIRED IAW SRM 51-40-2 AND ECRA 5310-03239. (X)SDR CAL960357Stringer · crackedGSO - INSPECTION FOUND TWO EACH .25 INCH CRACKS AT FASTENER HOLES OF STR 23R, STA 360 TO STA 440. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)SDR CAL960349Frame · crackedGSO - INSPECTION FOUND LEFT LOWER FRAME IN FORWARD PIT, STA 460, CRACKED AT NUTPLATES FOR CARGO LINER. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE FRAME WAS REPAIRED IAW E.A. 5310-01211. (X)SDR CAL960361Stringer · corrodedGSO - INSPECTION FOUND STR 24R IN FORWARD PIT CORRODED AT STA 478. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65-45768. (X)SDR CAL960352Act Fitting · crackedGSO - INSPECTION FOUND A 1 INCH CRACK AT ROD ATTACH POINT OF NR 5 SPOILER INBOARD ACTUATOR FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)SDR CAL960190Lamp · inoperativeFLT NR 591 - MSP - THE RIGHT MLG GREEN LIGHT DID NOT ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH TO MSP, AND IT WOULD NOT TEST. CHANGING BULBS DID NOT HELP. THE GEAR WAS VISUALLY INSPECTED AND CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WISDR CAL960185Hyd Line · chafedFLT NR 1036 - GSO - THE 'A' HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM BNA TO EWR. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE IN LSDR CAL960343Skin · crackedGSO - INSPECTION FOUND CRACKS AROUND FASTENERS IN LT EXTERNAL SKIN AT BS 188 TO BS 251, WL 207 THROUGH WL 234. THE CRACK LENGTHS WERE NOT IDENTIFIED, BUT THE REPAIRED AREAS WERE LESS THAN 6 INCHES IN DIAMETER. THE CRACKS WERE CUT OUT. REPAIR DOUBLERS AND FISDR CAL960175Reservoir · low fluidFLT NR 1627 - EWR - THE FLAPS WOULD NOT RETRACT FROM 5 DEGREE POSITION AFTER DEPARTURE FROM EWR. ALTERNATE FLAP EXTENSION WAS USED PER 'ABNORMAL' PROCEDURES AND THE FLAPS EXTENDED TO 15 DEGREES. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDESDR CAL960344Frame · crackedGSO - INSPECTION FOUND A DENT AND .50 INCH CRACK IN FORWARD PIT BELT FRAME AT STA 400, STR 23L TO STR 25L. THE FRAME WAS REPAIRED BY FABRICATING AND INSTALLING ANGLE, DOUBLER, AND FILLER IAW SRM 51-40-3. (X)SDR CAL960363Skin · corrodedGSO - INSPECTION FOUND SKIN CORRODED AT STA 295 TO STA 340, STR 18R TO STR 19R. THE CORRODED SKIN WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)SDR CAL960360Stringer · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN RT WING STR 13 AT WBL 92.5. REPAIR ANGLES AND SPLICES WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C34533 AFTER STOP DRILLING CRACK. (X)SDR CAL960369Bear Strap · crackedGSO - INSPECTION FOUND A .3750 INCH CRACK IN BEAR STRAP AT C-1 DOOR CUT-OUT, LOWER AFT CORNER. THE SKIN WAS REPLACED AND A DOUBLER INSTALLED IAW ECRA 5330-02366. (X)SDR CAL960152Hyd Line · leakingFLT NR 1446 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE LEAKING AT CLAMP. THE PRESSURE LINE WAS RSDR CAL960067Hyd Line · leakingFLT NR 1069 - TPA - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE IN FLIGHT WITH THE QUANTITY GAUGE INDICATING ZERO. THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO 'A' HYDRAULIC SYSTEM PRESSURE MODULE LEAKING. THE LINE WAS REPLACED USSDR CAL960062Hyd Line · chafedFLT NR 1069 - TPA - AIRCRAFT LOST THE 'A' SYSTEM HYDRAULICS WHILE EN ROUTE FROM GSO TO TPA. QRH CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM HYDRAULIC PRESSURE LINE ABOVE LEFT MLG CHAFEDSDR CAL960011Floor Beam · crackedHOU - INSPECTION FOUND A 1.5 INCH CRACK IN FLOOR BEAM AT STA 663, BL ZERO, WING CENTER BOX. A REPAIR WAS INSTALLED IAW ECRA 5710-01708. (X)SDR CAL960012Skin · puncturedHOU - INSPECTION FOUND A .25 INCH DENT WITH A .1250 INCH HOLE IN RT FUSELAGE SKIN AFT OF EXTERNAL POWER PANEL AT STA 235. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02346. (X)SDR CAL960044Web · crackedHOU - INSPECTION FOUND 2 CRACKS ON REAR SPAR WEB AT RBL 54.21. ONE CRACK WAS 1.5 INCHES LONG AT UPPER PANEL, AND THE OTHER CRACK WAS 2.3 INCHES LONG AT LOWER PANEL. A REPAIR WAS INSTALLED IAW ECRA 5750-02420. (X)SDR CAL960010Skin · gougedHOU - INSPECTION FOUND THE LEFT WING INBOARD MID-FLAP UPPER SKIN GOUGED AT INBOARD END. THE GOUGE APPROXIMATED AN AREA OF 1.7 INCH BY 3 INCHES. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5750-02421. (X)SDR CAL960013Skin · corrodedHOU - INSPECTION FOUND CORROSION IN E AND E BAY CUTOUT SKIN AT STR 27R. DOUBLERS WERE INSTALLED IAW ECRA 5330-02350. (X)SDR CAL951157Tee Chord · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN TEE CHORD AT STA 685, BL ZERO. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5710-01705. (X)SDR CAL951147Skin · corrodedGSO - INSPECTION FOUND THE FUSELAGE SKIN AND DOUBLERS CORRODED AT AFT LOWER CORNER OF C-1 DOORWAY. THE CORROSION WAS REMOVED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 5330-02343. (X)SDR CAL951145Light · inoperativeGSO - INSPECTION FOUND THE LEFT OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED, RECHARGED, AND INSTALLED. (M)SDR CAL951144Battery Pack · dischargedGSO - INSPECTION FOUND THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 23 INOPERATIVE. THE EMERGENCY EXIT LIGHT BATTERY PACK WAS REMOVED AND REPLACED. (M)SDR CAL951143Light · inoperativeGSO - INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. (M)SDR CAL951142Battery Pack · dischargedGSO - INSPECTION FOUND BOTH RT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M)SDR CAL951130Stringer · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN RT WING STR 13 AT WBL 92.5 AND A 1.5 INCH CRACK IN SAME STRINGER AT WBL 114. THE STRINGER WAS REPAIRED IAW BOEING DWG 65C34533. (X)SDR CAL951131Chord · crackedGSO - INSPECTION FOUND STA 727 RT CHORD CRACKED AT STR 18A. THE CRACK WAS LOCATED AT BOTH FORWARD AND AFT FASTENERS AND TOTALED 1 INCH IN LENGTH. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BOEING DWG 65C33722. (X)SDR CAL951129Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 440. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-10-04 AND SRM 51-30-0. (X)SDR CAL951036Eel · inoperativeGSO - INSPECTION FOUND THE RT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE RT AFT EXTERIOR LIGHT ASSY WAS REMOVED AND REPLACED IAW MM 33-51-01. (X)SDR CAL951035Battery Pack · dischargedGSO - INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACKS FOR THE LT AND RT OVERWING EMERGENCY LIGHTS WERE REMOVED AND REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X)SDR CAL950984Pcu · leakingFLT NR 1790 - THE B-HYDRAULIC SYSTEM HAD A PARTIAL DROP IN QUANTITY WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE B-SYSTEM AILERON PCU LEAKING. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71 AND OPERATIOSDR CAL950980Actuator · inoperativeFLT NR 1598 - GSO - THE NR 4 SLAT WOULD NOT RETRACT DURING CLIMB-OUT OF GSO, THE AIRCRAFT WAS RETURNED TO GSO. MAINTENANCE FOUND THE NR 4 LEADING EDGE SLAT ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (MSDR CAL950924Angle · crackedGSO - INSPECTION FOUND A 2.5 INCH CRACK IN RADIUS OF RT LOWER FORWARD SHEAR BEAM ATTACH ANGLE AT STA 664. THE CRACKED ANGLE WAS REMOVED AND SHEAR BEAM MODIFICATION KIT PART NR 5310-02450-10 WAS INSTALLED IAW EA 5310-02450. (X)SDR CAL950925Floor Beam · crackedGSO - INSPECTION FOUND FLOOR BEAM WEB CRACKED AT FIVE EACH LOWER FASTENER HOLES BETWEEN BS 700-BS 717, BBL 0.07. THE COMBINED CRACK LENGTH WAS APPROXIMATELY 5 INCHES. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW WEB AND DOUBLER WERE FABRICATED AND INSTALSDR CAL950840Skin · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FORWARD GALLEY DOOR UPPER HINGE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02315. (M)SDR CAL950873Track · crackedEWR - INSPECTION FOUND A .25 INCH CRACK IN LT OUTBOARD TRAILING EDGE FLAP TRACK. THE CRACKED AREA WAS REPAIRED IAW ECRA 5750-02364. (X)SDR CAL950857Skin · corrodedIAH - INSPECTION FOUND A POPPED FASTENER WITH CORROSION IN SKIN AT LAP JOINT FORWARD OF C-1 DOOR THRESHOLD STATION 400. THE CORRODED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 16. (M)SDR CAL950630Circuit Breaker · poppedEWR - FLT 1482 - WHEN LANDING GEAR WAS EXTENDED ON FINAL APPROACH TO EWR, THE GEAR 'DOWN AND LOCKED' LIGHTS DID NOT ILLUMINATE. A 'GO AROUND' WAS INITIATED AND THE CREW OBSERVED THE CIRCUIT BREAKER ON P6-3 PANEL LABELED 'SECT 5' POPPED. THE CIRCUIT BREAKER WSDR CAL950537Chord · crackedSTA 31J - INSPECTION FOUND A 14 INCH CRACK IN THE LEFT MLG WHEEL WELL AFT BULKHEAD LOWER CIRCUMFERENTIAL ANGLE (PREVIOUSLY STOP DRILLED). THE CHORD WAS REPLACED IAW SERVICE BULLETIN 737-53-1088 AND ECRA 5310-03133. (M)SDR CAL950463Uplock Sensor · inoperativeFLT NR 9860 - CLE - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE RT MLG UPLOCK SENSOR WAS REMOVED AND REPLACED. THE GEAR WAS SWSDR CAL950519T-Angle · corroded31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X)
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