JASC 5345
Service difficulty reports · 822
Reports filed under 5345 · Fuselage, Equipment Attach Fittings, newest first.
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 jasc_code = '5345' 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 jasc_code = '5345' 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 TWAA0106228Fitting · corrodedDURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION AROUND LAV MOUNT HOLES AT STA 219 AND BL 16L. REMOVED CORROSION PER SPM 6-80-01. PAINTED AND TREATED PER SRM 51-10-3.SDR CALA0100274Mount · corrodedINSPECTION FOUND G-2 GALLEY FORWARD INBOARD LOWER MOUNT CORRODED AT STA 336, RBL 12. THE MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR TWAA0105808Fitting · corrodedDURING CHECK-C MAINT IN THE FWD CABIN THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 45. REPLACED CASTING PER SRM 51-10-4 AND SPM 06-70-01.SDR TWAA0105807Fitting · corrodedDURING CHECK-C MAINT IN THE FWD CABIN, THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 51. REPLACED CASTING PER SRM 51-10-4 AND SPM 06-70-01.SDR AALA20010461Mount · corrodedTUL - FOUND CORROSION ON FORWARD LAVATORY INBOARD AFT MOUNT, FS 253. INSTALLED NEW MOUNT PLATE SRM 51-01-00. (M)SDR 2001UALA00239Mount · crackedSTATION 178 IS CRACKED AT THE RADAR ANTENNA MOUNT. THIS IS CONSIDERED A MAJOR REPAIR. INSTALLED DOUBLER TO AFFECTED AREA. ACCOMPLISHED MAJOR REPAIR.SDR AALA20010219Fitting · corrodedTUL - FOUND INBOARD GALLEY TIE DOWN CORRODED STATION 218. REMOVED AND REPLACED GALLEY TIE DOWN PER SRM 53-01-00. (M)SDR AALA20010220Fitting · corrodedTUL - FOUND FORWARD GALLEY INBOARD TIEDOWN FITTING CORRODED 2 INCHES BY 8 INCHES, STATION 160. REMOVED AND REPLACED FORWARD INBOARD GALLEY TIE DOWN FITTING PER SRM 51-01. (M)SDR CA010110004Bracket · worn(CAN) - MASTER CYLINDER MOVEMENT IN BRACKET SEEMED EXCESSIVE- FOUND BRACKET PIN HOLE WORN, PIN (CLEVIS) WON, AND TAB ON BRACKET WORN APPROXIMATELY 33% FROM ORIGINAL THICKNESS.SDR RAIA0011035Mount · corrodedMX-STL-DURING MAINTENANCE CHECK FOUND CORROSION AT GALLEY RIGHT AFT FOOT MOUNT. MAINTENANCE REPLACED GALLY RIGHT AFT FOOT MOUNT IAW ATR42 SRM.SDR DHL200080193CFitting · corrodedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.0, L-30 RT. REMOVED DAMAGED FITTING IAW SRM 51-1-20D, PAGE 24, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PAGE SDR DHL200080192CFitting · crackedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.0, L-32 RT. REMOVED DAMAGED FITTING IAW SRM 51-1-20D, PAGE 21, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PAGE 9. REFSDR DHL200080191CFitting · corrodedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.00, L-27LT. REMOVED DAMAGED FITTING IAW SRM 51-2-20D, PAGE 21, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9.SDR DHL2000801133Beam · brokenAFT ACCESSORY COMPT BEAM ANGLE BROKEN AT STA 1660.000, L24 L. REMOVED BROKEN ANGLE PER SRM 51-1-21. FABRICATED NEW ANGLE IAW SRM 53-2-0. TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW ANGLE PER SRM 51-1-21.SDR CALA0000611Fitting · corrodedR1 DOOR GIRT BAR FITTING IS CORRODED. REMOVED AND REPLACED FITTING PER SRM 51-30-1.SDR CA000511045Mount Bracket · cracked(CAN) DURING A 200-HOUR INSPECTION, LOOSENESS WAS FOUND AT THE CABIN STEP ATTACHMENT. THE STEP AND SUPPORT WERE REMOVED FOR RE-BUSHING. THE SUPPORT ASSEMBLY WAS INSPECTED AND FOUND CRACKED. THE CAUSE OF THE LOOSENESS IN THE STEP WAS CORROSION AND WEAR IN THSDR CA000316005Support Bracket · failed(CAN) ON LANDING ROLL, THE PILOT EXPERIENCED A LEFT BRAKE FAILURE. MAINTENANCE FOUND THE BRAKE CYLINDER HAD TORN THE MOUNTING HOLE OUT OF THE CYLINDER MOUNTING BRACKET. THE RIGHT HAND BRAKE CYLINDER MOUNTING BRACKET WAS FOUND IN POOR CONDITION ALSO.SDR CA000118041Attach Angle · cracked(CAN) DURING SCHEDULED INSPECTION MAINTENANCE FOUND THE FLAP ACTUATOR SUPPORT STRUCTURE CRACKED.SDR 99FDEA00271Bolt · corrodedDUR A/C P-F CONV CORROSION WAS FOUND IN ALL FOUR HOLE BORES COMMON TO ABA7003-2 & ABA7172 FITTINGS. THREE BOLTS FAILED IN TENSION. REMOVED AND REPLACED BOLTS FROM BORES IAW FEDEX EA NR 8-5311-41885.SDR AU971527Fitting · cracked(AUS) HOIST BEAM ATTACHMENT FITTING CRACKED.SDR 97ZZZX4573Hinge · crackedDURING LOWERING OF THE OPTIONAL EQUIPMENT DECK PANEL, NOTED THE LEFT HAND HINGE ASSY WAS CRACKED IN HALF. FURTHER INSPECTION REVEALED RIGHT HAND HINGE CRACKED AND FAILURE WAS IMMINENT. MATERIAL THICKNESS AND TYPE ARE NOT SUFFICIENT TO SUPPORT PANEL WITH OPTISDR EGRA9548Release Pin · failedWIRE STRIKE KIT RELEASE PIN FAILED. BEARINGS AT END OF RELEASE PIN FELL OUT. PART SCRAPPED AT KHC. REPLACED WITH NEW RELEASE PIN.
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