N44214, cancelled Feb 18, 1998
Service difficulty reports · 27
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N44214' AND deregistration_id = 'N44214-1998-02-18' 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 n_number = 'N44214' AND deregistration_id = 'N44214-1998-02-18' 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 CALA9701680Hyd Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE FLEX LINE LEAKING. THE LINE WAS REPLACED WISDR CALA9701355Hyd Line · rupturedTHE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ILLUMINATION OF A PUMP LOW PRESSURE LIGHTS. THE A-SYSTEM HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULC PRESSURE LISDR CALA9701250Stud · failedTHE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE ENROUTE FROM CAE TO EWR. THE ENG WAS SHUTDOWN AND THE A/C WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTTOM STUD ON NR 1SDR CALA9701223Hyd Line · leakingTHE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHT WHILE AT CRUISE. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SUPPLY LINE LESDR CALA9700843Hydraulic Line · chafedTHE A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO NEAR ZERO WHILE EN ROUTE. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC PRESSURE LINE ON RT WING IN ENGINE PYLON SDR CALA9700071Hyd Line · leakingTHE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS FLICKERED AND THE A-SYSTEM HYRDAULIC QUANTITY GAUGE READ ZERO ON APPROACH PRIOR TO GEAR AND FLAP EXTENSION. THE HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND A MANUAL GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDESDR CALA9601911Hydraulic Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY FLEX LINE IN RIGHT ENGINE PYLON AREA LEAKING. THE LINE WAS REMOVED AND REPLACED AND LEAK CHESDR CALA9601876Hyd Line · leakingTHE A HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT INTO EWR. THE A SYSTEM PUMPS WERE TURNED OFF AND THE HYDRAULIC LOSS CHECKLIST WAS ACCOMPLISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT ENGINE A SYSTEM PRESSURE LISDR CALA9601603Skin · crackedINSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF C-2 DOOR AFT CUTOUT. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLERS WERE INSTALLED IAW ECRA 5330-02460.SDR CALA9601561Bulkhead Skin · crackedINSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-11.SDR CALA9601560Shear Web · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD RADIUS OF SHEAR WEB AT S18A, LT B.S. 664. NEW REPAIR ANGLES WERE INSTALLED IAW BOEING DRAWING NR 65C29228 AND SRM 51-30-2.SDR CALA9601555Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD SKIN AT LOWER AFT CORNER OF C-2 DOOR CUTOUT. THE CRACKED SECTION OF SKIN WAS REMOVED. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND ENGINEERING ORDER REO-02348.SDR CALA9601554Bulkhead Skin · crackedINSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2.SDR CALA9601553Bulkhead Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFENER AT WL 218, RT SIDE. THE CRACKED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2SDR CALA9601556Frame · crackedINSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE AT LOWER AFT CORNER OF LT STA 520 WING TO BODY ATTACH FRAME. THE FASTENERS AND EXISTING ANGLE WERE REMOVED. AN ATTACH ANGLE, REPAIR ANGLE, AND CLIPS WERE FABRICATED AND INSTALLED IAW ECRA 5350-01227, SRM SDR CAL960560Hydraulic Line · chafedEWR - FLT 0674 - THE B-HYDRAULIC SYSTEM LOW QUANTITY ILLUMINATED ON APPROACH TO DWR. THE 'A' AND 'B' SYSTEMS REMAINED AT 3,000 PSI WITH 2 GALLONS QUANTITY. THE GEAR AND FLAPS EXTENDED NORMALLY. THE QUANTITY WENT TO 1 GALLON WITH T/R ACTIVATED AND RETURNED TSDR CAL960386Hyd Line · leakingBUF - FLT 1420 - AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM EWR TO BUF. THE AIRCRAFT LANDED IN BUF WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT SYSTEM 'A' MODULAR UNIT LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLASDR 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 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 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 CAL950440Lap Seam · corroded31J - INSPECTION FOUND CORROSION IN THE LAP SEAM AT BS 420, STR 27R. THE CORRODED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-03. (X)SDR CAL950437Fitting · cracked31J - INSPECTION FOUND A .3750 INCH CRACK IN THE RT BS 695 FRAME AFT LOWER FITTING AT THE OUTBOARD FASTENERS IN THE AFT HORIZONTAL FLANGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SB 737-53-1080, REV. 2 AND BOEING DRAWING 65C34490. (X)SDR CAL950439Shear Beam · cracked3LJ - A .3750 INCH CRACK WAS FOUND IN THE RADIUS OF THE INBOARD FLANGE AT THE FORWARD END OF THE LT S18A SHEAR BEAM, AFT SIDE OF BS 664 BULKHEAD. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-40-3, SRM 51-10-2, SRM SDR CAL950438Frame · cracked31J - A 1 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF THE L-2 DOOR FRAME. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5210-01224. (X)SDR CAL950101Battery Charger · inoperativeTPA - FLT 1790 - THE FLIGHT ATTENDANT REPORTED A SMOKY ODOR IN CABIN DURING CLIMB-OUT. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE ODOR SUBSIDED. THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BATTERY CHASDR CAL950001Hyd Line · chafedFLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A' SYSTEM LOW PRESSURE LIGHTS BEGAN TO FLICKER ON AND OFF WHILE ON FINAL APPROACH. THE AIRCRAFT LA
Back to N44214, cancelled Feb 18, 1998