N120NJ, cancelled Nov 22, 2005
Service difficulty reports · 30
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 = 'N120NJ' AND deregistration_id = 'N120NJ-2005-11-22' 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 = 'N120NJ' AND deregistration_id = 'N120NJ-2005-11-22' 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 P2EA2001M0004ComputerAuto Pilot twitches in pitch on VG1. Auto Pilot pulls back on controls continuiously when operated on system "A". Corrective action: Removed and replaced Pitch Computer IAW MM 22-11-151A, operatoinal check normal. See A/C 120 Log pages 92743 and 92744. This reSDR P2EA2001M0006Control PanelHeading Hold will not hold heading with Auto Pilot in B channnel. Corrective action: Deffered Heading Hold per MEL 22-1, CI#M120076 per MX CNTL Mic. Replaced Mode Control Panel, operational check normal IAW MM 22-11-191, This clears CI#M120079. See A/C 120 LogSDR P2EA2001M0003Gyro · faultyAUTO PILOT ON HDG2 HOLD WILL NOT MAINTAIN BANK AND ROLL LEVEL AND OCCASIONALLY JERKS ABRUPTLY. REPLACED NR 1 VERTICAL GYRO PER MM 34-22-11, OPERATIONAL CHECK OKAY.SDR P2EA01193Computer · faultyFLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHECSDR P2EA01167Skin · crackedSJO - DURING Q-CHECK, RIGHT WING OUTBOARD MID FLAP WBL 304.5, SKIN WITH CRACK. RIGHT WING OUTBOARD MID FLAP L/E OF CENTER TRACK CAVITY SKIN SECTION REPAIRED IAW COOPESA EO NR COO-3-57-452-01. (M)SDR P2EA01166Bulkhead · crackedSJO - DURING Q-CHECK, INSPECTION PER S/B 737-53A1173, BS 178 FORWARD PRESSURE BULKHEAD WEB WITH CRACK AT WL 210 AND RBL 8.5. FORWARD PRESSURE BULKHEAD BS 178, VERTICAL CHORD CRACKED AT INBOARD FLANGE WL 184 AND LBL 5.7. REPAIRED FORWARD PRESSURE BULKHEAD WEBSDR P2EA01162Skin · dentedSJO - DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 500A PLUS 12, BETWEEN STRINGER 1 AND STRINGER 2L. REPAIRED FUSELAGE SKIN SECTION FROM BS 500A PLUS 7 INCHES TO 500B, BETWEEN STRINGER 2 LEFT AND STRINGER 2 RIGHT DUE TO DENT IAW SRM 53-30-3 FISDR P2EA01163Cargo Track · corrodedDURING Q-CHECK, FOUND FORWARD CARGO COMPARTMENT FROM BS 380 TO BS 520 LBL 18.5, CARGO TRACK WITH CORROSION. (M)SDR P2EA01164Floor Support · corrodedDURING Q-CHECK, AFT CARGO COMPARTMENT BETWEEN BS 767 AND BS 847 AT STRINGER 25 RIGHT FLOOR SUPPORT WITH CORROSION. (M)SDR P2EA01168Skin · damagedDURING Q-CHECK, EXTERNAL FUSELAGE, SKIN WITH SCRATCH AND DENT FROM BS 306 TO BS 307, BETWEEN STRINGER 20 AND 21 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 296.5 TO BS 318, BETWEEN STRINGER 20 AND 25 RT DUE TO DENT IAW COOPESA EO COO-3-53-430-01. (M)SDR P2EA01156Doubler · crackedSJO - DURING Q-CHECK, EXTERNAL FUSELAGE DOUBLER WITH CRACK AT BS 1138, WL 266 LEFT SIDE. (M)SDR P2EA01161Skin · crackedSJO - DURING Q-CHECK, R1 DOOR, LOWER AFTER CORNER CUT OUT WITH CRACK. REPAIRED FUSELAGE SKIN FORWARD GALLEY DOOR CUT OUT FROM BS 314 TO BS 340, BETWEEN STRINGER 16 AND 18 RIGHT DUE TO CRACK IAW SRM 53-30-3, FIG 26. (M)SDR P2EA01159Skin · canningDURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M)SDR P2EA01158Stringer · dentedSJO - DURING Q-CHECK, LOWER FUSELAGE TAIL CONE STRINGER 27 LEFT WITH DENT AT BS 1035. REPAIRED STRINGER 27 LEFT FROM BS 1032 TO BS 1045 DUE TO DENT IAW SRM 53-10-3, FIG 01. (M)SDR P2EA01157Bulkhead · crackedDURING Q-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD BS 178, WEB CRACKED AT RBL 11.5-WL 213, PRESSURE BULKHEAD BS 178 FLOOR WEB SECTION CRACKED AT SL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD BSDR P2EA01151Frame · crackedDURING Q-CHECK, FUSELAGE AFT CARGO COMPARTMENT AT FRAME BS 807, BETWEEN STRINGER 27 LEFT AND 27 RIGHT, LOWER SECTION WITH CRACK. S/D - REPAIRED FRAME SECTION AT BS 807 BETWEEN STRINGER 27 RIGHT AND STRINGER LEFT DUE TO CRACK IAW SRM 53-10-4, FIG 06. (M)SDR P2EA01154Skin · dentedDURING Q-CHECK, FOUND EXTERNAL SKIN WITH DENT AT BS 500A PLUS 12 INCHES, BETWEEN STRINGER 1 AND 2 LEFT. (M)SDR P2EA01153Skin · dentedDURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 590, STRINGER 1. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 590 TO BS 599 BETWEEN STRINGER 2 LEFT AND 2 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 7. (M)SDR P2EA01150Skin · dentedDURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1040, BETWEEN STRINGER 27 LEFT AND 27 RIGHT. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 1030 TO BS 1057 BETWEEN STRINGER 27 RIGHT AND STRINGER 24 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)SDR P2EA01145Skin · dentedDURING Q-CHECK, FOUND TWO DENTS RIGHT SIDE OF AFT OUT FLOW VALVE. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 922 BETWEEN STRINGER 21 RIGHT AND 23 RIGHT DUE TO DENTS IAW SRM 53-30-3, FIG 28. (M)SDR P2EA01146Skin · dentedDURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1051, BETWEEN STRINGER 16 LEFT AND 17 LEFT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1047.5 TO BS 1055.5 BETWEEN STRINGER 16 LEFT AND 17 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 19. (M)SDR P2EA01152Floorbeam · corrodedSJO - DURING Q-CHECK, FOUND PAX CABIN AT BS 294, BETWEEN BL 0 AND RBL 40 INCHES, WL 208, UPPER SECTION AND BS 294.5 BETWEEN BL 0 AND LBL 30, FLOORBEAM WITH CORROSION. (M)SDR P2EA01149Stringer · corrodedDURING Q-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 968, STRINGER 27 RIGHT WITH CORROSION. S/D - REPAIRED STRINGER 27 RIGHT FROM BS 958.5 TO BS 976 DUE TO CORROSION IAW SRM 53-10-3, FIG 01. (M)SDR P2EA01148Skin · dentedSJO - DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 807, BETWEEN STRINGER 26 LEFT AND 27 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 789.5 TO BS 815 BETWEEN STRINGER 25 LEFT TO STRINGER 26 RT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)SDR P2EA01122Indicator · inoperativeMCI - FLT 350 - DURING CRUISE AT 33,000 FEET CABIN RATE OF CHANGE WAS PLUS 250 FEET PER MINUTE AND CABIN PRESSURE WAS AT 9,500 FEET AND SHOULD BE AT 800 FEET FOR NORMAL. STANDBY WAS SELECTED WITH NO IMPROVEMENT. DURING DESCENT WITH THROTTLES AT IDLE, CABIN RSDR P2EA00221Gasper Fan · malfunctionedFLT 307 - MYR - SMOKE AND FUMES NOTED IN COCKPIT. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO MYR LANDING UNEVENTFUL. FOUND FAULTY GASPER FAN, DEFERRED PER MEL 21-24, CONTROL M120626 PER MX CONTROL. REMOVED AND REPLACED GASPER FAN PER MM 21-24-21, OPERATINOSDR P2EA00212Control Cable · looseMCI - FLT 589 - EMERGENCY DECLARED, NR 1 ENGINE SHUT DOWN 5 MINUTES BEFORE LANDING, AIRCRAFT RETURNED TO MCI, LANDING UNEVENTFUL. LOST THROTTLE CONTROL NR 1 ENGINE: EPR 2.09, N1 91 PERCENT, EGT 450, N2 91 PERCENT, AND FUEL FLOW NORMAL. FOUND LOOSE HARDWARE SDR P2EA00202Skin · delaminatedYYC - DURING C-CHECK, RIGHT OUTBOARD FOREFLAP, REPAIR DELAMINATED ON UPPER SURFACE 87 INCHES OUTBOARD OF INBOARD END. REPAIRED FOREFLAP IAW SRM 51-40-6, PAGE 8 PARAGRAPH 11. (M)SDR P2EA00203Skin · dentedYYC - DURING C-CHECK, FOUND DENT WITH SHARP CREASE AT BS 860, BETWEEN STRINGERS 15L AND 16L. REPAIRED DENT AT BS 860 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-30-3, FIG 1. (M)SDR P2EA99275Engine · bird strikeMDW - FLT 815 - ABORTED TAKEOFF, NO EMERGENCY DECLARED, RETURNED TO BLOCKS. AT APPROXIMATELY 100 KNOTS DURING TAKEOFF ROLL, INGESTED BIRD IN NR 1 ENGINE. (X)
Back to N120NJ, cancelled Nov 22, 2005